MSET ENGINEERING CORPORATION SDN BHD
DOCUMENT TITLE: DESIGN CALCULATION DATE: 11.01.2015
DOC. REF. NO.: MSET/M2-251/S-6011/DC REVISION: 02
SUBJECT: TITLE PAGE JOB NO: M2-251
SERIAL NO.: M2-251/002
DESIGN CALCULATION
Fuel Gas Filter Coalescer TAG NO: S-6011
PROJECT NAME: E6 Development Project
CLIENT NAME: VME Process
02 11.01.15 Issued for Approval Mohd Faizal Yahasliza Azahar 01 10.12.14 Issued for Review Muhd Faizal Yahasliza Azahar
Rev. No.
Date Description of Revision Prepared
by Reviewed
by Approved
by
MSET ENGINEERING CORPORATION SDN BHD
DOCUMENT TITLE: DESIGN CALCULATION DATE: 11.01.2015
DOC. REF. NO.: MSET/M2-251/S-6011/DC REVISION: 02
SUBJECT: TITLE PAGE JOB NO: M2-251
SERIAL NO.: M2-234/002
DESIGN DATA
ITEM NO. FUEL GAS FILTER COALESCER
DESIGN CODE ASME SEC.VIII DIV.1, 2013 EDITION +
DEP 31.22. 20.31
DESIGN PRESSURE (barg) (Int./Ext.) 18/FV
TEMPERATURE (⁰C) (Max./Min) 50/0
OPERATING PRESSURE (barg) (In / Out) 7 / 6.8
TEMPERATURE (⁰C) (In / Out) 24.8-38.9 / 24.7-38.8
TEST PRESSURE
HYDROTEST (barg) (1.3xMAPxLSR)(note1) (UG-99c)
24.625 (Horizontal Position)
PNEUMATIC NO
MAWP (hot & corroded) (barg) 18.347
MAP (new & cold) (barg) 18.998
OUTSIDE DIAMETER / SEAM TO SEAM (mm) 219.1/3120
TYPE OF HEAD 2:1 ELLIP HEAD/BODY FLANGE
MATERIAL OF CONSTRUCTION (SHELL & HEAD) SA 312 TP 316/316L & SA 403 WP 316/316L
HEAT TREATMENT
NORMALISED NO
PWHT NO
IMPACT TEST NO
MDMT (⁰C) 0
RADIOGRAPHY HEAD: 100%, SHELL: 100%
JOINT EFFICIENCY HEAD:1.0 , SHELL: 1.0
CORROSION ALLOWANCE (mm) 0
CONTENTS HC LIQUID/GAS
ERECTION WEIGHT (kg) 390
CAPACITY (m3) 0.11
PRESSURE VESSEL DESIGN CALCULATION Note: 1.MAP will be used in lieu of MAWP for determining hydro test pressure (As per DEP 31.22.20.31-Gen, Jan 09)
MSET ENGINEERING CORPORATION SDN BHD
DOCUMENT TITLE: DESIGN CALCULATION DATE: 11.01.2015
DOC. REF. NO.: MSET/M2-251/S-6011/DC REVISION: 02
SUBJECT: TITLE PAGE JOB NO: M2-251
SERIAL NO.: M2-251/002
TABLE OF CONTENT
NO CONTENT PAGE NO.
1 Input Echo 4
2 Flg Calc [Int P] : A1 (flange) 20
3 Flg Calc [Int P] : A1 (blind) 25
4 Internal Pressure Calculations 29
5 External Pressure Calculations 33
6 Element and Detail Weights 37
7 Nozzle Flange MAWP 42
8 Wind Load Calculation 44
9 Earthquake Load Calculation 45
10 Wind / Earthquake Shear, Bending 47
11 Wind Deflection 49
12 Stress due Combined Loads 55
13 Center of Gravity Calculation 61
14 Sup. Lug Calc 62
15 Nozzle Calculation 78
16 Nozzle Schedule 213
17 Nozzle Summary 217
18 MDMT Summary 220
19 Vessel Design Summary 222
20 Attachment 1 : Wind Pressure Calc 225
21 Attachment 2 : Transportation Calc 227
22 Attachment 3 : Trunnion Calc 266
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015
PV Elite Vessel Analysis Program: Input Data
Design Internal Pressure (for test) 18.000 bar
Design Internal Temperature 50 °C
Type of Test UG-99(c)
Test Position Horizontal
Projection of Nozzle from Vessel Top 200.00 mm
Projection of Nozzle from Vessel Bottom 200.00 mm
Minimum Design Metal Temperature 0 °C
Type of Construction Welded
Special Service None
Degree of Radiography RT 1
Miscellaneous Weight Percent 0.0
Use Higher Longitudinal Stresses (Flag) Y
Select t for Internal Pressure (Flag) N
Select t for External Pressure (Flag) N
Select t for Axial Stress (Flag) N
Select Location for Stiff. Rings (Flag) N
Consider Vortex Shedding N
Perform a Corroded Pressure test N
Is this a Heat Exchanger No
User Defined Test Press. (Used if > 0) 0.0000 bar
User defined MAWP 0.0000 bar
User defined MAPnc 0.0000 bar
Load Case 1 NP+EW+WI+FW+BW
Load Case 2 NP+EW+EE+FS+BS
Load Case 3 NP+OW+WI+FW+BW
Load Case 4 NP+OW+EQ+FS+BS
Load Case 5 NP+HW+HI
Load Case 6 NP+HW+HE
4
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Load Case 7 IP+OW+WI+FW+BW
Load Case 8 IP+OW+EQ+FS+BS
Load Case 9 EP+OW+WI+FW+BW
Load Case 10 EP+OW+EQ+FS+BS
Load Case 11 HP+HW+HI
Load Case 12 HP+HW+HE
Load Case 13 IP+WE+EW
Load Case 14 IP+WF+CW
Load Case 15 IP+VO+OW
Load Case 16 IP+VE+EW
Load Case 17 NP+VO+OW
Load Case 18 FS+BS+IP+OW
Load Case 19 FS+BS+EP+OW
Wind Design Code User Defined
Wind Profile Height mm Pressure kPa
10000.0000 0.7500
0.0000 0.0000
0.0000 0.0000
0.0000 0.0000
0.0000 0.0000
0.0000 0.0000
0.0000 0.0000
0.0000 0.0000
Damping Factor (Beta) for Wind (Ope) 0.0100
Damping Factor (Beta) for Wind (Empty) 0.0000
Damping Factor (Beta) for Wind (Filled) 0.0000
Seismic Design Code G Loading
Seismic Importance Factor 1.000
G Loading Coefficient Gx 0.500
G Loading Coefficient Gz 0.500
5
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 G Loading Coefficient Gy -2.000
Percent Seismic for Test 0.000
Design Nozzle for M.A.W.P. (maximum) Y
Consider MAP New and Cold in Noz. Design N
Consider External Loads for Nozzle Des. Y
Use ASME VIII-1 Appendix 1-9 N
Material Database Year Current w/Addenda or Code Year
Configuration Directives:
Do not use Nozzle MDMT Interpretation VIII-1 01-37 No
Use Table G instead of exact equation for "A" Yes
Shell Head Joints are Tapered Yes
Compute "K" in corroded condition Yes
Use Code Case 2286 No
Use the MAWP to compute the MDMT Yes
Using Metric Material Databases, ASME II D No
Complete Listing of Vessel Elements and Details:
Element From Node 10
Element To Node 20
Element Type Elliptical
Description Head
Distance "FROM" to "TO" 55.000 mm
Element Outside Diameter 219.07 mm
Element Thickness 7.1565 mm
Internal Corrosion Allowance 0.0000 mm
Nominal Thickness 8.1788 mm
External Corrosion Allowance 0.0000 mm
Design Internal Pressure 18.000 bar
6
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Design Temperature Internal Pressure 50 °C
Design External Pressure 1.0342 bar
Design Temperature External Pressure 50 °C
Effective Diameter Multiplier 1.2
Material Name SA-403 316L
Allowable Stress, Ambient 115.15 MPa
Allowable Stress, Operating 115.15 MPa
Allowable Stress, Hydrotest 155.14 MPa
Material Density 8027.2 kg/m³
P Number Thickness 0.0000 mm
Yield Stress, Operating 165.40 MPa
External Pressure Chart Name HA-4
UNS Number S31603
Product Form Smls. & wld. fittings
Efficiency, Longitudinal Seam 1.0
Efficiency, Circumferential Seam 1.0
Elliptical Head Factor 2.0
Element From Node 10
Detail Type Nozzle
Detail ID N3
Dist. from "FROM" Node / Offset dist 0.0000 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 90.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
--------------------------------------------------------------------
7
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Element From Node 20
Element To Node 30
Element Type Cylinder
Description Shell
Distance "FROM" to "TO" 3120.0 mm
Element Outside Diameter 219.07 mm
Element Thickness 7.1565 mm
Internal Corrosion Allowance 0.0000 mm
Nominal Thickness 8.1788 mm
External Corrosion Allowance 0.0000 mm
Design Internal Pressure 18.000 bar
Design Temperature Internal Pressure 50 °C
Design External Pressure 1.0342 bar
Design Temperature External Pressure 50 °C
Effective Diameter Multiplier 1.2
Material Name SA-312 TP316L
Allowable Stress, Ambient 115.15 MPa
Allowable Stress, Operating 115.15 MPa
Allowable Stress, Hydrotest 155.14 MPa
Material Density 8027.2 kg/m³
P Number Thickness 0.0000 mm
Yield Stress, Operating 165.40 MPa
External Pressure Chart Name HA-4
UNS Number S31603
Product Form Smls. & wld. pipe
Efficiency, Longitudinal Seam 1.0
Efficiency, Circumferential Seam 1.0
Element From Node 20
Detail Type Liquid
Detail ID LIQUID (LOWER)
Dist. from "FROM" Node / Offset dist 0.0000 mm
Height/Length of Liquid 650.00 mm
8
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Liquid Density 803.23 kg/m³
Element From Node 20
Detail Type Nozzle
Detail ID N1
Dist. from "FROM" Node / Offset dist 1200.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 0.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 67.101 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID N2
Dist. from "FROM" Node / Offset dist 2920.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 285.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 67.101 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID N4
Dist. from "FROM" Node / Offset dist 1425.0 mm
Nozzle Diameter 2.0 in.
9
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Nozzle Schedule None
Nozzle Class 150
Layout Angle 90.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 67.101 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID N5
Dist. from "FROM" Node / Offset dist 3000.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 345.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 67.101 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID N6
Dist. from "FROM" Node / Offset dist 200.00 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 90.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 67.101 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
10
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015
Element From Node 20
Detail Type Nozzle
Detail ID K1A
Dist. from "FROM" Node / Offset dist 770.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 20.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K1B
Dist. from "FROM" Node / Offset dist 170.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 20.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K2A
Dist. from "FROM" Node / Offset dist 1010.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
11
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Nozzle Class 150
Layout Angle 315.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID K2B
Dist. from "FROM" Node / Offset dist 170.00 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 315.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID K3A
Dist. from "FROM" Node / Offset dist 570.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 225.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
12
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Element From Node 20
Detail Type Nozzle
Detail ID K3B
Dist. from "FROM" Node / Offset dist 170.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 225.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K4A
Dist. from "FROM" Node / Offset dist 750.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 165.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K4B
Dist. from "FROM" Node / Offset dist 350.00 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
13
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Layout Angle 165.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K6A
Dist. from "FROM" Node / Offset dist 1895.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 340.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
Detail Type Nozzle
Detail ID K6B
Dist. from "FROM" Node / Offset dist 1445.0 mm
Nozzle Diameter 2.0 in.
Nozzle Schedule None
Nozzle Class 150
Layout Angle 340.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-182 F316
Element From Node 20
14
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Detail Type Nozzle
Detail ID K7A
Dist. from "FROM" Node / Offset dist 1795.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 225.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K7B
Dist. from "FROM" Node / Offset dist 1445.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 225.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K8A
Dist. from "FROM" Node / Offset dist 1950.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 165.0
15
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K8B
Dist. from "FROM" Node / Offset dist 1550.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 165.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
Detail ID K5A
Dist. from "FROM" Node / Offset dist 1850.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 30.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Nozzle
16
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Detail ID K5B
Dist. from "FROM" Node / Offset dist 1500.0 mm
Nozzle Diameter 3.0 in.
Nozzle Schedule 80S
Nozzle Class 150
Layout Angle 30.0
Blind Flange (Y/N) N
Weight of Nozzle ( Used if > 0 ) 0.0000 N
Grade of Attached Flange GR 2.2
Nozzle Matl SA-312 TP316L
Element From Node 20
Detail Type Lug
Detail ID LUG
Dist. from "FROM" Node / Offset dist 2567.0 mm
Number of Lugs 2
Dist. from OD to Lug Cntrline(dlug) 600.00 mm
Height of Gusset Plates (hgp) 250.00 mm
Force Bearing Width (wfb) 200.00 mm
Weight of Lug 133.44 N
Lug Start Angle (degrees) 0.0
Element From Node 20
Detail Type Weight
Detail ID FILTER
Dist. from "FROM" Node / Offset dist 1700.0 mm
Miscellaneous Weight 980.60 N
Offset from Element Centerline 0.0000 mm
Element From Node 20
Detail Type Weight
Detail ID LIQUID (UPPER)
Dist. from "FROM" Node / Offset dist 1908.0 mm
17
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Miscellaneous Weight 156.90 N
Offset from Element Centerline 0.0000 mm
--------------------------------------------------------------------
Element From Node 30
Element To Node 40
Element Type Flange
Description Body Flange (DN200)
Distance "FROM" to "TO" 101.60 mm
Flange Inside Diameter (OD for Blinds) 345.00 mm
Element Thickness 28.448 mm
Internal Corrosion Allowance 0.0000 mm
Nominal Thickness 8.1788 mm
External Corrosion Allowance 0.0000 mm
Design Internal Pressure 18.000 bar
Design Temperature Internal Pressure 50 °C
Design External Pressure 1.0342 bar
Design Temperature External Pressure 50 °C
Effective Diameter Multiplier 1.2
Material Name SA-182 F316L
Allowable Stress, Ambient 115.15 MPa
Allowable Stress, Operating 115.15 MPa
Allowable Stress, Hydrotest 155.14 MPa
Material Density 8027.2 kg/m³
P Number Thickness 0.0000 mm
Yield Stress, Operating 223.30 MPa
External Pressure Chart Name HA-4
UNS Number S31603
Class / Thickness / Grade :: > 5
Product Form Forgings
Perform Flange Stress Calculation (Y/N) Y
Weight of ANSI B16.5/B16.47 Flange 0.0000 N
18
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Input Echo : Step: 1 1:14p Jan 11,2015 Class of ANSI B16.5/B16.47 Flange
Grade of ANSI B16.5/B16.47 Flange
--------------------------------------------------------------------
Element From Node 40
Element To Node 50
Element Type Flange
Description Blind Flange (DN200)
Distance "FROM" to "TO" 28.448 mm
Flange Inside Diameter (OD for Blinds) 345.00 mm
Element Thickness 28.448 mm
Internal Corrosion Allowance 0.0000 mm
Nominal Thickness 0.0000 mm
External Corrosion Allowance 0.0000 mm
Design Internal Pressure 18.000 bar
Design Temperature Internal Pressure 50 °C
Design External Pressure 1.0342 bar
Design Temperature External Pressure 50 °C
Effective Diameter Multiplier 1.2
Material Name SA-182 F316L
Perform Flange Stress Calculation (Y/N) Y
Weight of ANSI B16.5/B16.47 Flange 0.0000 N
Class of ANSI B16.5/B16.47 Flange
Grade of ANSI B16.5/B16.47 Flange
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
19
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015
Flange Input Data Values Description: A1 (flange) :
Body Flange (DN200)
Description of Flange Geometry (Type) Integral Weld Neck
Design Pressure P 18.00 bar
Design Temperature 50 °C
Internal Corrosion Allowance ci 0.0000 mm
External Corrosion Allowance ce 0.0000 mm
Use Corrosion Allowance in Thickness Calcs. No
Flange Inside Diameter B 202.692 mm
Flange Outside Diameter A 345.000 mm
Flange Thickness t 28.4480 mm
Thickness of Hub at Small End go 7.1564 mm
Thickness of Hub at Large End g1 20.6184 mm
Length of Hub h 73.1520 mm
Flange Material SA-182 F316L
Flange Material UNS number S31603
Flange Allowable Stress At Temperature Sfo 115.15 MPa
Flange Allowable Stress At Ambient Sfa 115.15 MPa
Bolt Material SA-193 B7
Bolt Allowable Stress At Temperature Sb 172.38 MPa
Bolt Allowable Stress At Ambient Sa 172.38 MPa
Diameter of Bolt Circle C 298.500 mm
Nominal Bolt Diameter a 19.0500 mm
Type of Threads TEMA Thread Series
Number of Bolts 8
Flange Face Outside Diameter Fod 269.748 mm
20
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 Flange Face Inside Diameter Fid 202.692 mm
Flange Facing Sketch 1, Code Sketch 1a
Gasket Outside Diameter Go 263.652 mm
Gasket Inside Diameter Gi 233.426 mm
Gasket Factor m 0.0000
Gasket Design Seating Stress y 0.00 MPa
Column for Gasket Seating 2, Code Column II
Gasket Thickness tg 3.1750 mm
ANSI Flange Class 150
ANSI Flange Grade GR 2.2
ASME Code, Section VIII, Division 1, 2010, 2011a
Hub Small End Required Thickness due to Internal Pressure:
= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)
= (18.00*(202.6920/2+0.0000))/(115.15*1.00-0.6*18.00)+Ca
= 1.5995 mm
Hub Small End Hub MAWP:
= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)
= (115.15 * 1.00 * 7.1564 )/(101.3460 + 0.6 * 7.1564 )
= 77.993 bar
Corroded Flange ID, Bcor = B+2*Fcor 202.692 mm
Corroded Large Hub, g1Cor = g1-ci 20.618 mm
Corroded Small Hub, g0Cor = go-ci 7.156 mm
Code R Dimension, R = (C-B)/2 - g1 27.286 mm
Gasket Contact Width, N = (Go - Gi) / 2 15.113 mm
Basic Gasket Width, bo = N / 2 7.557 mm
21
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 Effective Gasket Width, b = Cb sqrt(bo) 6.927 mm
Gasket Reaction Diameter, G = Go (Self-Energizing) 263.652 mm
Basic Flange and Bolt Loads:
Hydrostatic End Load due to Pressure [H]:
= 0.785 * G² * Peq
= 0.785 * 263.6520² * 18.000
= 98276.719 N
Contact Load on Gasket Surfaces [Hp]:
= 2 * b * Pi * G * m * P
= 2 * 6.9270 * 3.1416 * 263.6520 * 0.0000 * 18.00
= 0.000 N
Hydrostatic End Load at Flange ID [Hd]:
= Pi * Bcor² * P / 4
= 3.1416 * 202.6920² *18.0000/4
= 58084.695 N
Pressure Force on Flange Face [Ht]:
= H - Hd
= 98276 - 58084
= 40192.023 N
Operating Bolt Load [Wm1]:
= max( H + Hp + H'p, 0 )
= max( 98276 + 0 + 0 , 0 )
= 98276.719 N
Gasket Seating Bolt Load [Wm2]:
= y * b * Pi * G + yPart * bPart * lp
= 0.00*6.9270*3.141*263.652+0.00*0.0000*0.00
= 0.000 N
Required Bolt Area [Am]:
= Maximum of Wm1/Sb, Wm2/Sa
= Maximum of 98276/172 , 0/172
= 570.182 mm²
22
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015
ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:
= 2a + 6t/(m + 0.5)
= 2 * 19.050 + 6 * 28.448/(0.00 + 0.5)
= 379.476 mm
Actual Circumferential Bolt Spacing [Bs]:
= C * sin( pi / n )
= 298.500 * sin( 3.142/8 )
= 114.231 mm
ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:
= max( sqrt( Bs/( 2a + t )), 1 )
= max( sqrt( 114.231/( 2 * 19.050 + 28.448 )), 1 )
= 1.3102
Bolting Information for TEMA Imperial Thread Series (Non Mandatory):
-----------------------------------------------------------------------------
Minimum Actual Maximum
-----------------------------------------------------------------------------
Bolt Area, mm² 570.182 1558.706
Radial distance bet. hub and bolts 28.575 27.286
Radial distance bet. bolts and the edge 20.637 23.250
Circumferential spacing between bolts 44.450 114.231 379.476
-----------------------------------------------------------------------------
Flange Design Bolt Load, Gasket Seating [W]:
= Sa * ( Am + Ab ) / 2
= 172.38 * ( 570.1817 + 1558.7064 )/2
= 183467.95 N
Gasket Load for the Operating Condition [HG]:
= Wm1 - H
= 98276 - 98276
23
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (flange) Flng: 3 1:14p Jan 11,2015 = 0.00 N
Moment Arm Calculations:
Distance to Gasket Load Reaction [hg]:
= (C - G ) / 2
= ( 298.5000 - 263.6520 )/2
= 17.4240 mm
Distance to Face Pressure Reaction [ht]:
= ( R + g1 + hg ) / 2
= ( 27.2856 + 20.6184 + 17.4240 )/2
= 32.6640 mm
Distance to End Pressure Reaction [hd]:
= R + ( g1 / 2 )
= 27.2856 + ( 20.6184/2.0 )
= 37.5948 mm
Summary of Moments for Internal Pressure:
Loading Force Distance Bolt Corr Moment
End Pressure, Md 58085. 37.5948 1.3102 2862. N-m
Face Pressure, Mt 40192. 32.6640 1.3102 1721. N-m
Gasket Load, Mg 0. 17.4240 1.3102 0. N-m
Gasket Seating, Matm 183468. 17.4240 1.3102 4190. N-m
Total Moment for Operation, Mop 4583. N-m
Total Moment for Gasket seating, Matm 4190. N-m
Note: User choose not to perform Stress Calculations on this ANSI Flange.
Pressure rating of the flange will be used to check code compliance.
Estimated Finished Weight of Flange at given Thk. 19.5 kgm
Estimated Unfinished Weight of Forging at given Thk 49.9 kgm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
24
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015
Flange Input Data Values Description: A1 (blind) :
Blind Flange (DN200)
Description of Flange Geometry (Type) Blind
Design Pressure P 18.00 bar
Design Temperature 50 °C
Internal Corrosion Allowance ci 0.0000 mm
External Corrosion Allowance ce 0.0000 mm
Use Corrosion Allowance in Thickness Calcs. Yes
Flange Outside Diameter A 345.000 mm
Flange Thickness t 28.4480 mm
Flange Material SA-182 F316L
Flange Material UNS number S31603
Flange Allowable Stress At Temperature Sfo 115.15 MPa
Flange Allowable Stress At Ambient Sfa 115.15 MPa
Bolt Material SA-193 B7
Bolt Allowable Stress At Temperature Sb 172.38 MPa
Bolt Allowable Stress At Ambient Sa 172.38 MPa
Diameter of the Load Reaction, Long Span D 0.000 mm
Diameter of the Load Reaction, Short Span d 0.000 mm
Perimeter along the Center of the Bolts L 937.765 mm
Diameter of Bolt Circle C 298.500 mm
Nominal Bolt Diameter a 19.0500 mm
Type of Threads TEMA Thread Series
Number of Bolts 8
Flange Face Outside Diameter Fod 269.748 mm
25
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 Flange Face Inside Diameter Fid 184.150 mm
Flange Facing Sketch 1, Code Sketch 1a
Gasket Outside Diameter Go 263.652 mm
Gasket Inside Diameter Gi 233.426 mm
Gasket Factor m 0.0000
Gasket Design Seating Stress y 0.00 MPa
Column for Gasket Seating 2, Code Column II
Gasket Thickness tg 3.1750 mm
ANSI Flange Class 150
ANSI Flange Grade GR 2.2
ASME Code, Section VIII, Division 1, 2010, 2011a
Gasket Contact Width, N = (Go - Gi) / 2 15.113 mm
Basic Gasket Width, bo = N / 2 7.557 mm
Effective Gasket Width, b = Cb sqrt(bo) 6.927 mm
Gasket Reaction Diameter, G = Go (Self-Energizing) 263.652 mm
Basic Flange and Bolt Loads:
Hydrostatic End Load due to Pressure [H]:
= 0.785 * G² * Peq
= 0.785 * 263.6520² * 18.000
= 98276.719 N
Contact Load on Gasket Surfaces [Hp]:
= 2 * b * Pi * G * m * P
= 2 * 6.9270 * 3.1416 * 263.6520 * 0.0000 * 18.00
= 0.000 N
Operating Bolt Load [Wm1]:
26
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 = max( H + Hp + H'p, 0 )
= max( 98276 + 0 + 0 , 0 )
= 98276.719 N
Gasket Seating Bolt Load [Wm2]:
= y * b * Pi * G + yPart * bPart * lp
= 0.00*6.9270*3.141*263.652+0.00*0.0000*0.00
= 0.000 N
Required Bolt Area [Am]:
= Maximum of Wm1/Sb, Wm2/Sa
= Maximum of 98276/172 , 0/172
= 570.182 mm²
ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:
= 2a + 6t/(m + 0.5)
= 2 * 19.050 + 6 * 28.448/(0.00 + 0.5)
= 379.476 mm
Actual Circumferential Bolt Spacing [Bs]:
= C * sin( pi / n )
= 298.500 * sin( 3.142/8 )
= 114.231 mm
ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:
= max( sqrt( Bs/( 2a + t )), 1 )
= max( sqrt( 114.231/( 2 * 19.050 + 28.448 )), 1 )
= 1.3102
Bolting Information for TEMA Imperial Thread Series (Non Mandatory):
-----------------------------------------------------------------------------
Minimum Actual Maximum
-----------------------------------------------------------------------------
Bolt Area, mm² 570.182 1558.706
Radial distance bet. bolts and the edge 20.637 23.250
27
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Flg Calc [Int P] : A1 (blind) Flng: 4 1:14p Jan 11,2015 Circumferential spacing between bolts 44.450 114.231 379.476
-----------------------------------------------------------------------------
Flange Design Bolt Load, Gasket Seating [W]:
= Sa * ( Am + Ab ) / 2
= 172.38 * ( 570.1817 + 1558.7064 )/2
= 183467.95 N
Gasket Load for the Operating Condition [HG]:
= Wm1
= 98276.72 N
Moment Arm Calculations:
Distance to Gasket Load Reaction [hg]:
= (C - G ) / 2
= ( 298.5000 - 263.6520 )/2
= 17.4240 mm
Note: User choose not to perform Stress Calculations on this ANSI Flange.
Pressure rating of the flange will be used to check code compliance.
Estimated Finished Weight of Flange at given Thk. 21.3 kgm
Estimated Unfinished Weight of Forging at given Thk 21.3 kgm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
28
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:14p Jan 11,2015
Element Thickness, Pressure, Diameter and Allowable Stress :
| | Int. Press | Nominal | Total Corr| Element | Allowable |
From| To | + Liq. Hd | Thickness | Allowance | Diameter | Stress(SE)|
| | bar | mm | mm | mm | MPa |
---------------------------------------------------------------------------
Head| 18.051 | 8.1788 | ... | 219.07 | 115.15 |
Shell| 18.051 | 8.1788 | ... | 219.07 | 115.15 |
Body Flang| 18.000 | 8.1788 | ... | 345.00 | 115.15 |
Blind Flan| 18.000 | ... | ... | 345.00 | 115.15 |
Element Required Thickness and MAWP :
| | Design | M.A.W.P. | M.A.P. | Minimum | Required |
From| To | Pressure | Corroded | New & Cold | Thickness | Thickness |
| | bar | bar | bar | mm | mm |
----------------------------------------------------------------------------
Head| 18.0000 | 79.8661 | 79.9173 | 7.15645 | 1.69354 |
Shell| 18.0000 | 77.1854 | 77.2366 | 7.15645 | 1.70673 |
Body Flang| 18.0000 | 18.3984 | 18.9983 | 28.4480 | No Calc |
Blind Flan| 18.0000 | 18.3984 | 18.9983 | 28.4480 | No Calc |
Minimum 18.347 18.998
Note : The M.A.W.P is Governed by a Standard Flange !
Flange MAWP including Static Pressure: 18.347 = 18.398 - 0.051 bar
Internal Pressure Calculation Results :
ASME Code, Section VIII, Division 1, 2010, 2011a
Elliptical Head From 10 To 20 SA-403 316L at 50 °C
29
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:14p Jan 11,2015
Head
Longitudinal Joint: Seamless
Circumferential Joint: Full Radiography per UW-11(a) Type 1
Material UNS Number: S31603
Required Thickness due to Internal Pressure [tr]:
= (P*Do*Kcor)/(2*S*E+2*P*(Kcor-0.1)) per Appendix 1-4 (c)
= (18.051*219.0750*1.000)/(2*115.15*1.00+2*18.051*(1.000-0.1))
= 1.6935 + 0.0000 = 1.6935 mm
Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:
Less Operating Hydrostatic Head Pressure of 0.051 bar
= (2*S*E*t)/(Kcor*Do-2*t*(Kcor-0.1)) per Appendix 1-4 (c)
= (2*115.15*1.00*7.1565)/(1.000*219.0750-2*7.1565*(1.00-0.1))
= 79.917 - 0.051 = 79.866 bar
Maximum Allowable Pressure, New and Cold [MAPNC]:
= (2*S*E*t)/(K*Do-2*t*(K-0.1)) per Appendix 1-4 (c)
= (2*115.15*1.00*7.1565)/(1.000*219.0750-2*7.1565*(1.000-0.1))
= 79.917 bar
Actual stress at given pressure and thickness, corroded [Sact]:
= (P*(Kcor*Do-2*t*(Kcor-0.1)))/(2*E*t)
= (18.051*(1.000*219.0750-2*7.1565*(1.000-0.1)))/(2*1.00*7.1565)
= 26.009 MPa
Straight Flange Required Thickness:
= (P*Ro)/(S*E+0.4*P) + ca per Appendix 1-1 (a)(1)
= (18.051*109.5375)/(115.15*1.00+0.4*18.051)+0.000
= 1.707 mm
30
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:14p Jan 11,2015
Straight Flange Maximum Allowable Working Pressure:
Less Operating Hydrostatic Head Pressure of 0.051 bar
= (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)
= (115.15 * 1.00 * 8.1788 )/(109.5375 - 0.4 * 8.1788 )
= 88.610 - 0.051 = 88.559 bar
SA-403 316L, Min Metal Temp without impact per UHA-51: -196 °C
Cylindrical Shell From 20 To 30 SA-312 TP316L at 50 °C
Shell
Longitudinal Joint: Seamless
Circumferential Joint: Full Radiography per UW-11(a) Type 1
Material UNS Number: S31603
Required Thickness due to Internal Pressure [tr]:
= (P*Ro) / (S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.051*109.5375)/(115.15*1.00+0.4*18.051)
= 1.7067 + 0.0000 = 1.7067 mm
Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:
Less Operating Hydrostatic Head Pressure of 0.051 bar
= (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)
= (115.15*1.00*7.1565)/(109.5375-0.4*7.1565)
= 77.237 - 0.051 = 77.185 bar
Maximum Allowable Pressure, New and Cold [MAPNC]:
= (S*E*t)/(Ro-0.4*t) per Appendix 1-1 (a)(1)
= (115.15*1.00*7.1565)/(109.5375-0.4*7.1565)
= 77.237 bar
31
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Internal Pressure Calculations : Step: 5 1:14p Jan 11,2015
Actual stress at given pressure and thickness, corroded [Sact]:
= (P*(Ro-0.4*t))/(E*t)
= (18.051*((109.5375-0.4*7.1565))/(1.00*7.1565)
= 26.911 MPa
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Hydrostatic Test Pressure Results:
Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 23.851 bar
Pressure per UG99b[34] = 1.3 * Design Pres * Sa/S 23.400 bar
Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 24.625 bar
Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 20.182 bar
Pressure per PED = 1.43 * MAWP 26.236 bar
Horizontal Test performed per: UG-99c
Please note that Nozzle, Shell, Head, Flange, etc MAWPs are all considered
when determining the hydrotest pressure for those test types that are based
on the MAWP of the vessel.
Stresses on Elements due to Test Pressure:
From To Stress Allowable Ratio Pressure
----------------------------------------------------------------------
Head 35.5 155.1 0.229 24.65
Shell 36.7 155.1 0.237 24.65
----------------------------------------------------------------------
Elements Suitable for Internal Pressure.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
32
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015
External Pressure Calculation Results :
ASME Code, Section VIII, Division 1, 2010, 2011a
Elliptical Head From 10 to 20 Ext. Chart: HA-4 at 50 °C
Head
Elastic Modulus from Chart: HA-4 at 50 °C : 0.192E+06 MPa
Results for Maximum Allowable External Pressure (MAEP):
Tca OD D/t Factor A B
7.156 219.07 30.61 0.0045370 83.75
EMAP = B/(K0*D/t) = 83.7457/(0.9000 *30.6122 ) = 30.3922 bar
Results for Required Thickness (Tca):
Tca OD D/t Factor A B
0.579 219.07 378.29 0.0003671 35.22
EMAP = B/(K0*D/t) = 35.2178/(0.9000 *378.2943 ) = 1.0343 bar
Check the requirements of UG-33(a)(1) using P = 1.67 * External Design
pressure for this head.
Material UNS Number: S31603
Required Thickness due to Internal Pressure [tr]:
= (P*Do*Kcor)/(2*S*E+2*P*(Kcor-0.1)) per Appendix 1-4 (c)
= (1.727*219.0750*1.000)/(2*115.15*1.00+2*1.727*(1.000-0.1))
= 0.1641 + 0.0000 = 0.1641 mm
Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:
= ((2*S*E*t)/(Kcor*Do-2*t*(Kcor-0.1)))/1.67 per Appendix 1-4 (c)
33
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015 = ((2*115.15*1.00*7.1565)/(1.000*219.0750-2*7.1565*(1.00-0.1)))/1.67
= 47.855 bar
Maximum Allowable External Pressure [MAEP]:
= min( MAEP, MAWP )
= min( 30.39 , 47.8547 )
= 30.392 bar
Thickness requirements per UG-33(a)(1) govern the required
thickness of this head.
Cylindrical Shell From 20 to 30 Ext. Chart: HA-4 at 50 °C
Shell
Elastic Modulus from Chart: HA-4 at 50 °C : 0.192E+06 MPa
Results for Maximum Allowable External Pressure (MAEP):
Tca OD SLEN D/t L/D Factor A B
7.156 219.07 3192.06 30.61 14.5706 0.0011983 65.86
EMAP = (4*B)/(3*(D/t)) = (4*65.8589 )/(3*30.6122 ) = 28.6811 bar
Results for Required Thickness (Tca):
Tca OD SLEN D/t L/D Factor A B
1.939 219.07 3192.06 112.96 14.5706 0.0000914 8.76
EMAP = (4*B)/(3*(D/t)) = (4*8.7631 )/(3*112.9565 ) = 1.0342 bar
Results for Maximum Stiffened Length (Slen):
Tca OD SLEN D/t L/D Factor A B
7.156 219.07 88373.64 30.61 50.0000 0.0011797 65.64
EMAP = (4*B)/(3*(D/t)) = (4*65.6350 )/(3*30.6122 ) = 28.5836 bar
External Pressure Calculations
34
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015
| | Section | Outside | Corroded | Factor | Factor |
From| To | Length | Diameter | Thickness | A | B |
| | mm | mm | mm | | MPa |
---------------------------------------------------------------------------
10| 20| No Calc | 219.075 | 7.15645 | 0.0045370 | 83.7457 |
20| 30| 3192.06 | 219.075 | 7.15645 | 0.0011983 | 65.8589 |
30| 40| No Calc | ... | 28.4480 | No Calc | No Calc |
40| 50| No Calc | ... | 28.4480 | No Calc | No Calc |
External Pressure Calculations
| | External | External | External | External |
From| To | Actual T. | Required T.|Des. Press. | M.A.W.P. |
| | mm | mm | bar | bar |
----------------------------------------------------------------
10| 20| 7.15645 | 1.50000 | 1.03420 | 30.3922 |
20| 30| 7.15645 | 1.93946 | 1.03420 | 28.6811 |
30| 40| 28.4480 | No Calc | 1.03420 | No Calc |
40| 50| 28.4480 | No Calc | 1.03420 | No Calc |
Minimum 28.681
External Pressure Calculations
| | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia |
From| To | Bet. Stiff.| Bet. Stiff.| Required | Available |
| | mm | mm | mm**4 | mm**4 |
-------------------------------------------------------------------
10| 20| No Calc | No Calc | No Calc | No Calc |
20| 30| 3192.06 | 88373.6 | No Calc | No Calc |
30| 40| No Calc | No Calc | No Calc | No Calc |
40| 50| No Calc | No Calc | No Calc | No Calc |
35
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- External Pressure Calculations : Step: 6 1:14p Jan 11,2015 Elements Suitable for External Pressure.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
36
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015
Element and Detail Weights
| | Element | Element | Corroded | Corroded | Extra due |
From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % |
| | kgm | m³ | kgm | m³ | kgm |
---------------------------------------------------------------------------
10| 20| 5.97865 | 0.0029355 | 5.97865 | 0.0029355 | 0.29893 |
20| 30| 137.032 | 0.10276 | 137.032 | 0.10276 | 6.85162 |
30| 40| 19.5277 | 0.0032789 | 19.5277 | 0.0032789 | 0.97638 |
40| 50| 21.3476 | ... | 21.3476 | ... | 1.06738 |
---------------------------------------------------------------------------
Total 183 0.11 183 0.11 9
Weight of Details
| | Weight of | X Offset, | Y Offset, |
From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description
| | kgm | mm | mm |
-------------------------------------------------
10|Nozl| 3.82814 | ... | -51.1905 | N3
20|Liqd| 17.1931 | ... | 325.000 | LIQUID (LOWER)
20|Nozl| 7.18497 | 127.781 | 1200.00 | N1
20|Nozl| 7.18497 | 127.781 | 2920.00 | N2
20|Nozl| 7.18497 | 127.781 | 1425.00 | N4
20|Nozl| 7.18497 | 127.781 | 3000.00 | N5
20|Nozl| 7.18497 | 127.781 | 200.000 | N6
20|Nozl| 8.15833 | 146.831 | 770.000 | K1A
20|Nozl| 8.15833 | 146.831 | 170.000 | K1B
20|Nozl| 7.18496 | 127.781 | 1010.00 | K2A
20|Nozl| 7.18496 | 127.781 | 170.000 | K2B
20|Nozl| 8.15833 | 146.831 | 570.000 | K3A
20|Nozl| 8.15833 | 146.831 | 170.000 | K3B
37
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 20|Nozl| 8.15833 | 146.831 | 750.000 | K4A
20|Nozl| 8.15833 | 146.831 | 350.000 | K4B
20|Nozl| 7.18496 | 127.781 | 1895.00 | K6A
20|Nozl| 7.18496 | 127.781 | 1445.00 | K6B
20|Nozl| 8.15833 | 146.831 | 1795.00 | K7A
20|Nozl| 8.15833 | 146.831 | 1445.00 | K7B
20|Nozl| 8.15833 | 146.831 | 1950.00 | K8A
20|Nozl| 8.15833 | 146.831 | 1550.00 | K8B
20|Nozl| 8.15833 | 146.831 | 1850.00 | K5A
20|Nozl| 8.15833 | 146.831 | 1500.00 | K5B
20|Lugs| 28.5768 | ... | 2692.00 | LUG
20|Wght| 100.000 | ... | 1700.00 | FILTER
20|Wght| 16.0000 | ... | 1908.00 | LIQUID (UPPER)
Total Weight of Each Detail Type
Total Weight of Liquid 17.2
Total Weight of Nozzles 166.4
Total Weight of Lugs 28.6
Total Weight of Weights 116.0
---------------------------------------------------------------
Sum of the Detail Weights 328.2 kgm
Weight Summation
Fabricated Shop Test Shipping Erected Empty Operating
------------------------------------------------------------------------------
193.1 388.1 193.1 388.1 193.1 388.1
... 108.9 ... ... ... 17.2
166.4 ... 166.4 ... ... ...
28.6 ... 28.6 ... ... ...
... ... ... ... ... 116.0
38
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 ... ... ... ... ... ...
... ... ... ... 166.4 ...
... ... ... ... 28.6 ...
------------------------------------------------------------------------------
388.1 497.0 388.1 388.1 388.1 521.2 kgm
Miscellaneous Weight Percent: 5.0 %
Note that the above value for the miscellaneous weight percent has
been applied to the shells/heads/flange/tubesheets/tubes etc. in the
weight calculations for metallic components.
Note: The shipping total has been modified because some items have
been specified as being installed in the shop.
Weight Summary
Fabricated Wt. - Bare Weight W/O Removable Internals 388.1 kgm
Shop Test Wt. - Fabricated Weight + Water ( Full ) 497.0 kgm
Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 388.1 kgm
Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 388.1 kgm
Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 388.1 kgm
Operating Wt. - Empty Wt + Operating Liq. Uncorroded 521.2 kgm
Field Test Wt. - Empty Weight + Water (Full) 497.0 kgm
Mass of the Upper 1/3 of the Vertical Vessel 102.1 kgm
Outside Surface Areas of Elements
| | Surface |
From| To | Area |
| | mm² |
----------------------------
39
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 10| 20| 91207.0 |
20| 30| 2.167E+06 |
30| 40| 148106. |
40| 50| 124315. |
-----------------------------
Total 2530993.000 mm²
Element and Detail Weights
| To | Total Ele.| Total. Ele.|Total. Ele.| Total Dtl.| Oper. Wgt. |
From| To | Empty Wgt.| Oper. Wgt.|Hydro. Wgt.| Offset Mom.| No Liquid |
| | kgm | kgm | kgm | N-m | kgm |
---------------------------------------------------------------------------
10| 20| 10.1057 | 10.1057 | 13.0394 | ... | 10.1057 |
20|Lugs| 252.132 | 361.718 | 336.627 | 182.714 | 347.572 |
Lugs| 30| 54.3161 | 77.9237 | 72.5184 | 39.3614 | 74.8763 |
30| 40| 20.5040 | 20.5040 | 23.7810 | ... | 20.5040 |
40| 50| 22.4150 | 22.4150 | 22.4150 | ... | 22.4150 |
Cumulative Vessel Weight
| | Cumulative Ope | Cumulative | Cumulative |
From| To | Wgt. No Liquid | Oper. Wgt. | Hydro. Wgt. |
| | kgm | kgm | kgm |
-------------------------------------------------------
10| 20| ... | ... | ... |
20|Lugs| -10.1057 | -10.1057 | -13.0394 |
Lugs| 30| 117.795 | 120.843 | 118.714 |
30| 40| 42.9191 | 42.9191 | 46.1960 |
40| 50| 22.4150 | 22.4150 | 22.4150 |
Note: The cumulative operating weights no liquid in the column above
are the cumulative operating weights minus the operating liquid
40
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Element and Detail Weights : Step: 7 1:14p Jan 11,2015 weight minus any weights absent in the empty condition.
Cumulative Vessel Moment
| | Cumulative | Cumulative |Cumulative |
From| To | Empty Mom. | Oper. Mom. |Hydro. Mom.|
| | N-m | N-m | N-m |
-------------------------------------------------
10| 20| ... | ... | ... |
20|Lugs| 182.714 | 182.714 | 182.714 |
Lugs| 30| 39.3614 | 39.3614 | 39.3614 |
30| 40| ... | ... | ... |
40| 50| ... | ... | ... |
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41
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Flange MAWP : Step: 8 1:14p Jan 11,2015
Nozzle Flange MAWP Results :
Nozzle ----- Flange Rating
Description Operating Ambient Temperature Class Grade|Group
bar bar °C
----------------------------------------------------------------------------
N3 18.4 19.0 50 150 GR 2.2
N1 18.4 19.0 50 150 GR 2.2
N2 18.4 19.0 50 150 GR 2.2
N4 18.4 19.0 50 150 GR 2.2
N5 18.4 19.0 50 150 GR 2.2
N6 18.4 19.0 50 150 GR 2.2
K1A 18.4 19.0 50 150 GR 2.2
K1B 18.4 19.0 50 150 GR 2.2
K2A 18.4 19.0 50 150 GR 2.2
K2B 18.4 19.0 50 150 GR 2.2
K3A 18.4 19.0 50 150 GR 2.2
K3B 18.4 19.0 50 150 GR 2.2
K4A 18.4 19.0 50 150 GR 2.2
K4B 18.4 19.0 50 150 GR 2.2
K6A 18.4 19.0 50 150 GR 2.2
K6B 18.4 19.0 50 150 GR 2.2
K7A 18.4 19.0 50 150 GR 2.2
K7B 18.4 19.0 50 150 GR 2.2
K8A 18.4 19.0 50 150 GR 2.2
K8B 18.4 19.0 50 150 GR 2.2
K5A 18.4 19.0 50 150 GR 2.2
K5B 18.4 19.0 50 150 GR 2.2
----------------------------------------------------------------------------
Minimum Rating 18.4 19.0 bar
42
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Flange MAWP : Step: 8 1:14p Jan 11,2015 Note: ANSI Ratings are per ANSI/ASME B16.5 2009 Metric Edition
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
43
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Natural Frequency Calculation : Step: 9 1:14p Jan 11,2015
The Natural Frequencies for the vessel have been computed iteratively
by solving a system of matrices. These matrices describe the mass
and the stiffness of the vessel. This is the generalized eigenvalue/
eigenvector problem and is referenced in some mathematical texts.
The Natural Frequency for the Vessel (Empty.) is 11.6100 Hz.
The Natural Frequency for the Vessel (Ope...) is 11.3756 Hz.
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44
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:14p Jan 11,2015
Note: Using the User Defined Wind Profile ...
Wind Vibration Calculations
This evaluation is based on work by Kanti Mahajan and Ed Zorilla
Nomenclature
Cf - Correction factor for natural frequency
D - Average internal diameter of vessel mm
Df - Damping Factor < 0.75 Unstable, > 0.95 Stable
Dr - Average internal diameter of top half of vessel mm
f - Natural frequency of vibration (Hertz)
f1 - Natural frequency of bare vessel based on a unit value of (D/L²)(104)
L - Total height of structure mm
Lc - Total length of conical section(s) of vessel mm
tb - Uncorroded plate thickness at bottom of vessel mm
V30 - Design Wind Speed provided by user km/hr
Vc - Critical wind velocity km/hr
Vw - Maximum wind speed at top of structure km/hr
W - Total corroded weight of structure N
Ws - Cor. vessel weight excl. weight of parts which do not effect stiff. N
Z - Maximum amplitude of vibration at top of vessel mm
Dl - Logarithmic decrement ( taken as 0.03 for Welded Structures )
Vp - Vib. Chance, <= 0.314E-05 (High); 0.314E-05 < 0.393E-05 (Probable)
P30 - wind pressure 30 feet above the base
Check other Conditions and Basic Assumptions:
#1 - Total Cone Length / Total Length < 0.5
0.000/3305.048 = 0.000
45
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Load Calculation : Step: 10 1:14p Jan 11,2015 #2 - ( D / L² ) * 104 < 8.0 (English Units)
- ( 0.72/10.84² ) * 104 = 60.973 [Geometry Violation]
Compute the vibration possibility. If Vp > 0.393E-05 no chance. [Vp]:
= W / ( L * Dr²)
= 5111/( 3305.05 * 204.762² )
= 0.36885E-04
Since Vp is > 0.393E-05 no further vibration analysis is required !
Wind Loads on Masses/Equipment/Piping
ID Wind Area Elevation Pressure Force
mm² mm kPa N
-------------------------------------------------------------------------
FILTER 0.00 1755.00 0.75 0.00
LIQUID (UPPER 0.00 1963.00 0.75 0.00
The Natural Frequency for the Vessel (Ope...) is 11.3756 Hz.
Wind Load Calculation
| | Wind | Wind | Wind | Wind | Element |
From| To | Height | Diameter | Area | Pressure | Wind Load |
| | mm | mm | mm² | kPa | N |
---------------------------------------------------------------------------
10| 20| 62.0931 | 262.890 | 26506.0 | 0.75000 | 19.8791 |
20| 30| 1666.19 | 262.890 | 820217. | 0.75000 | 615.148 |
30| 40| 3276.99 | 245.715 | 24964.6 | 0.75000 | 18.7230 |
40| 50| 3342.01 | 245.715 | 6990.09 | 0.75000 | 5.24244 |
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46
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Earthquake Load Calculation : Step: 11 1:14p Jan 11,2015
Earthquake Loading Specified in G's
Horizontal Acceleration factor (GX) 0.500
Horizontal Acceleration factor (GZ) 0.500
Vertical Acceleration factor (GY) -2.000
The Natural Frequency for the Vessel (Ope...) is 11.3756 Hz.
Earthquake Load Calculation
| | Earthquake | Earthquake | Element | Element |
From| To | Height | Weight | Ope Load | Emp Load |
| | mm | N | N | N |
--------------------------------------------------------------
10| 20| 27.5000 | 99.0967 | 70.0719 | 70.0719 |
20|Lugs| 2622.00 | 3547.01 | 2508.11 | 1748.26 |
Lugs| 30| 2898.50 | 764.119 | 540.314 | 376.621 |
30| 40| 3225.80 | 201.063 | 142.173 | 142.173 |
40| 50| 3290.82 | 219.802 | 155.423 | 155.423 |
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47
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind/Earthquake Shear, Bending : Step: 12 1:14p Jan 11,2015
The following table is for the Operating Case.
Wind/Earthquake Shear, Bending
| | Distance to| Cumulative |Earthquake | Wind | Earthquake |
From| To | Support| Wind Shear | Shear | Bending | Bending |
| | mm | N | N | N-m | N-m |
---------------------------------------------------------------------------
10| 20| 2618.25 | ... | ... | ... | ... |
20|Lugs| 1283.50 | 19.8791 | 70.0719 | 0.074501 | 0.26261 |
Lugs| 30| 276.500 | 152.876 | 907.982 | 655.864 | 3060.82 |
30| 40| 603.800 | 23.9655 | 297.596 | 1.55896 | 25.2343 |
40| 50| 668.824 | 5.24244 | 155.423 | 0.074598 | 2.21161 |
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48
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Wind Deflection : Step: 13 1:14p Jan 11,2015
Wind Deflection Calculations:
The following table is for the Operating Case.
Wind Deflection
| | Cumulative | Centroid | Elem. End | Elem. Ang. |
From| To | Wind Shear | Deflection |Deflection | Rotation |
| | N | mm | mm | |
--------------------------------------------------------------
10| 20| ... | 0.010864 | 0.021727 | ... |
20|Lugs| 19.8791 | -0.39317 | ... | ... |
Lugs| 30| 152.876 | -0.42107 | -0.31128 |-0.00039289 |
30| 40| 23.9655 | -0.29111 | -0.27093 |-0.00039289 |
40| 50| 5.24244 | -0.26528 | -0.25963 |-0.00039289 |
Critical Wind Velocity for Tower Vibration
| | 1st Crit. | 2nd Crit. |
From| To | Wind Speed | Wind Speed |
| | km/hr | km/hr |
-------------------------------------
10| 20| 53.6847 | 335.529 |
20| 30| 53.6847 | 335.529 |
30| 40| 50.1773 | 313.608 |
40| 50| 50.1773 | 313.608 |
Allowable deflection at the Tower Top (Ope)( 6.000"/100ft. Criteria)
Allowable deflection : 16.525 Actual Deflection : 0.022 mm
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49
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stress Constants : Step: 14 1:14p Jan 11,2015
Longitudinal Stress Constants
| | Metal Area | Metal Area |New & Cold | Corroded |
From| To | New & Cold | Corroded |Sect. Mod. | Sect. Mod. |
| | mm² | mm² | mm ³ | mm ³ |
--------------------------------------------------------------
10| 20| 4764.49 | 4764.49 | 244454. | 244454. |
20| 30| 4764.49 | 4764.49 | 244454. | 244454. |
30| 40| 4764.49 | 4764.49 | 244454. | 244454. |
40| 50| 4764.49 | 4764.49 | 244454. | 244454. |
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50
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Allowable Stresses : Step: 15 1:14p Jan 11,2015
Longitudinal Allowable Stresses
| | | Hydrotest | | Hydrotest |
From| To | Tensile | Tensile | Compressive | Compressive |
| | MPa | MPa | MPa | MPa |
-------------------------------------------------------------------
10| 20| 138.176 | 186.165 | -109.117 | -111.814 |
20|Lugs| 138.176 | 186.165 | -109.117 | -111.814 |
Lugs| 30| 138.176 | 186.165 | -109.117 | -111.814 |
30| 40| 138.176 | 186.165 | -109.117 | -111.814 |
40| 50| 138.176 | 186.165 | -109.117 | -111.814 |
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51
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p Jan 11,2015
Longitudinal Stress Report
Note: Longitudinal Operating and Empty Stresses are computed in the
corroded condition. Stresses due to loads in the hydrostatic test
cases have been computed in the new and cold condition.
Longitudinal Stresses Due to . . .
| | Long. Str. | Long. Str. |Long. Str. |
From| To | Int. Pres. | Ext. Pres. |Hyd. Pres. |
| | MPa | MPa | MPa |
-------------------------------------------------
10| 20| 12.5173 | -0.81833 | 17.1242 |
20| 30| 12.5173 | -0.81833 | 17.1242 |
30| 40| ... | ... | ... |
40| 50| ... | ... | ... |
Longitudinal Stresses Due to . . .
| | Wght. Str. | Wght. Str. |Wght. Str. | Wght. Str. | Wght. Str. |
From| To | Empty | Operating |Hydrotest | Emp. Mom. | Opr. Mom. |
| | MPa | MPa | MPa | MPa | MPa |
---------------------------------------------------------------------------
10| 20| ... | ... | ... | ... | ... |
20|Lugs| 0.020801 | 0.020801 | ... | 0.74720 | 0.74720 |
Lugs| 30| -0.24246 | -0.21334 | ... | 0.16097 | 0.16097 |
30| 40| -0.088341 | -0.088341 | ... | ... | ... |
40| 50| -0.046137 | -0.046137 | ... | ... | ... |
Longitudinal Stresses Due to . . .
| | Wght. Str. | Bend. Str. |Bend. Str. | Bend. Str. | Bend. Str. |
52
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p Jan 11,2015 From| To | Hyd. Mom. | Oper. Wind |Oper. Equ. | Hyd. Wind | Hyd. Equ. |
| | MPa | MPa | MPa | MPa | MPa |
---------------------------------------------------------------------------
10| 20| ... | ... | ... | ... | ... |
20|Lugs| ... | 0.00030467 | 0.0010739 | ... | ... |
Lugs| 30| ... | 2.68212 | 12.5171 | ... | ... |
30| 40| ... | 0.0063753 | 0.10319 | ... | ... |
40| 50| ... | 0.00030506 | 0.0090443 | ... | ... |
Longitudinal Stresses Due to . . .
| | Long. Str. | Long. Str. |Long. Str. | EarthQuake |
From| To | Vortex Ope.| Vortex Emp.|Vortex Tst.| Empty |
| | MPa | MPa | MPa | MPa |
--------------------------------------------------------------
10| 20| ... | ... | ... | ... |
20|Lugs| ... | ... | ... | 0.0010739 |
Lugs| 30| ... | ... | ... | 8.71229 |
30| 40| ... | ... | ... | 0.10319 |
40| 50| ... | ... | ... | 0.0090443 |
Longitudinal Stresses Due to . . .
| | Long. Str. | Long. Str. |
From| To | Y Forces W | Y ForceS S |
| | MPa | MPa |
-------------------------------------
10| 20| ... | 0.041602 |
20|Lugs| ... | 1.53066 |
Lugs| 30| ... | -0.49746 |
30| 40| ... | -0.17668 |
40| 50| ... | -0.092274 |
53
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Longitudinal Stresses Due to . . . Step: 16 1:14p Jan 11,2015 Long. Stresses due to User Forces and Moments
| |Wind For/Mom| Eqk For/Mom|Wnd For/Mom| Eqk For/Mom|
From| To | Corroded | Corroded | No Corr. | No Corr. |
| | MPa | MPa | MPa | MPa |
--------------------------------------------------------------
10| 20| ... | ... | ... | ... |
20|Lugs| ... | ... | ... | ... |
Lugs| 30| ... | ... | ... | ... |
30| 40| ... | ... | ... | ... |
40| 50| ... | ... | ... | ... |
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
54
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015
Stress Combination Load Cases for Vertical Vessels:
Load Case Definition Key
IP = Longitudinal Stress due to Internal Pressure
EP = Longitudinal Stress due to External Pressure
HP = Longitudinal Stress due to Hydrotest Pressure
NP = No Pressure
EW = Longitudinal Stress due to Weight (No Liquid)
OW = Longitudinal Stress due to Weight (Operating)
HW = Longitudinal Stress due to Weight (Hydrotest)
WI = Bending Stress due to Wind Moment (Operating)
EQ = Bending Stress due to Earthquake Moment (Operating)
EE = Bending Stress due to Earthquake Moment (Empty)
HI = Bending Stress due to Wind Moment (Hydrotest)
HE = Bending Stress due to Earthquake Moment (Hydrotest)
WE = Bending Stress due to Wind Moment (Empty) (no CA)
WF = Bending Stress due to Wind Moment (Filled) (no CA)
CW = Longitudinal Stress due to Weight (Empty) (no CA)
VO = Bending Stress due to Vortex Shedding Loads ( Ope )
VE = Bending Stress due to Vortex Shedding Loads ( Emp )
VF = Bending Stress due to Vortex Shedding Loads ( Test No CA. )
FW = Axial Stress due to Vertical Forces for the Wind Case
FS = Axial Stress due to Vertical Forces for the Seismic Case
BW = Bending Stress due to Lat. Forces for the Wind Case, Corroded
BS = Bending Stress due to Lat. Forces for the Seismic Case, Corroded
BN = Bending Stress due to Lat. Forces for the Wind Case, UnCorroded
BU = Bending Stress due to Lat. Forces for the Seismic Case, UnCorroded
General Notes:
Case types HI and HE are in the Un-Corroded condition.
55
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015
Case types WE, WF, and CW are in the Un-Corroded condition.
A blank stress and stress ratio indicates that the corresponding
stress comprising those components that did not contribute to that
type of stress.
An asterisk (*) in the final column denotes overstress.
Analysis of Load Case 1 : NP+EW+WI+FW+BW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.00 138.18 0.00 109.12 0.0000 0.0000
20 0.77 138.18 -0.73 109.12 0.0056 0.0067
20 2.60 138.18 -3.09 109.12 0.0188 0.0283
Analysis of Load Case 2 : NP+EW+EE+FS+BS
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.04 138.18 109.12 0.0003
20 2.30 138.18 109.12 0.0166
20 8.13 138.18 -9.61 109.12 0.0589 0.0881
Analysis of Load Case 3 : NP+OW+WI+FW+BW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.00 138.18 0.00 109.12 0.0000 0.0000
20 0.77 138.18 -0.73 109.12 0.0056 0.0067
20 2.63 138.18 -3.06 109.12 0.0190 0.0280
Analysis of Load Case 4 : NP+OW+EQ+FS+BS
56
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.04 138.18 109.12 0.0003
20 2.30 138.18 109.12 0.0166
20 11.97 138.18 -13.39 109.12 0.0866 0.1227
Analysis of Load Case 5 : NP+HW+HI
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.00 186.17 0.00 111.81 0.0000 0.0000
20 0.00 186.17 0.00 111.81 0.0000 0.0000
20 0.00 186.17 0.00 111.81 0.0000 0.0000
Analysis of Load Case 6 : NP+HW+HE
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.00 186.17 0.00 111.81 0.0000 0.0000
20 0.00 186.17 0.00 111.81 0.0000 0.0000
20 0.00 186.17 0.00 111.81 0.0000 0.0000
Analysis of Load Case 7 : IP+OW+WI+FW+BW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.52 138.18 109.12 0.0906
20 13.29 138.18 109.12 0.0962
20 15.15 138.18 109.12 0.1096
Analysis of Load Case 8 : IP+OW+EQ+FS+BS
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.56 138.18 109.12 0.0909
20 14.82 138.18 109.12 0.1072
20 24.48 138.18 -0.87 109.12 0.1772 0.0080
57
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015
Analysis of Load Case 9 : EP+OW+WI+FW+BW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 138.18 -0.82 109.12 0.0075
20 138.18 -1.55 109.12 0.0142
20 1.81 138.18 -3.87 109.12 0.0131 0.0355
Analysis of Load Case 10 : EP+OW+EQ+FS+BS
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 138.18 -0.78 109.12 0.0071
20 1.48 138.18 -0.02 109.12 0.0107 0.0001
20 11.15 138.18 -14.21 109.12 0.0807 0.1302
Analysis of Load Case 11 : HP+HW+HI
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 17.12 186.17 111.81 0.0920
20 17.12 186.17 111.81 0.0920
20 17.12 186.17 111.81 0.0920
Analysis of Load Case 12 : HP+HW+HE
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 17.12 186.17 111.81 0.0920
20 17.12 186.17 111.81 0.0920
20 17.12 186.17 111.81 0.0920
Analysis of Load Case 13 : IP+WE+EW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.52 138.18 109.12 0.0906
58
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 20 13.29 138.18 109.12 0.0961
20 12.44 138.18 109.12 0.0900
Analysis of Load Case 14 : IP+WF+CW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.52 138.18 109.12 0.0906
20 12.54 138.18 109.12 0.0907
20 12.30 138.18 109.12 0.0890
Analysis of Load Case 15 : IP+VO+OW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.52 138.18 109.12 0.0906
20 13.29 138.18 109.12 0.0961
20 12.46 138.18 109.12 0.0902
Analysis of Load Case 16 : IP+VE+EW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 12.52 138.18 109.12 0.0906
20 13.29 138.18 109.12 0.0961
20 12.44 138.18 109.12 0.0900
Analysis of Load Case 17 : NP+VO+OW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 0.00 138.18 0.00 109.12 0.0000 0.0000
20 0.77 138.18 -0.73 109.12 0.0056 0.0067
20 138.18 -0.37 109.12 0.0034
Analysis of Load Case 18 : FS+BS+IP+OW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
59
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Stress due to Combined Loads : Step: 17 1:14p Jan 11,2015 Node Stress Stress Stress Stress Ratio Ratio
10 12.56 138.18 109.12 0.0909
20 14.82 138.18 109.12 0.1072
20 11.97 138.18 109.12 0.0866
Analysis of Load Case 19 : FS+BS+EP+OW
From Tensile All. Tens. Comp. All. Comp. Tens. Comp.
Node Stress Stress Stress Stress Ratio Ratio
10 138.18 -0.78 109.12 0.0071
20 1.48 138.18 -0.01 109.12 0.0107 0.0001
20 138.18 -1.69 109.12 0.0155
Absolute Maximum of the all of the Stress Ratio's 0.1772
Governing Element: Shell
Governing Load Case 8 : IP+OW+EQ+FS+BS
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
60
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Center of Gravity Calculation : Step: 18 1:14p Jan 11,2015
Shop/Field Installation Options :
Note : The CG is computed from the first Element From Node
Center of Gravity of Liquid 380.000 mm
Center of Gravity of Nozzles 1256.373 mm
Center of Gravity of Lugs 2747.000 mm
Center of Gravity of Added Weights (Operating) 1783.690 mm
Center of Gravity of Bare Shell New and Cold 1928.210 mm
Center of Gravity of Bare Shell Corroded 1928.210 mm
Vessel CG in the Operating Condition 1675.404 mm
Vessel CG in the Fabricated (Shop/Empty) Condition 1700.429 mm
Vessel CG in the Test Condition 1784.015 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
61
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015
Support Lug Calculations: Operating Case
INPUT ECHO OF SUPPORT LUG INPUT
Type of Geometry : Gussets with No Top Plate
Number of Support Lugs Nlug 2
Distance from Vessel OD to Lug Contact Point Dlug 600.0000 mm
Lug Support Force Bearing Width Wfb 200.0000 mm
Lug Material SA-240 316L
Lug Yield Stress 165.40 MPa
Radial Width of bottom Support Lug Plate Wpl 250.0000 mm
Effective Force Bearing Length Lpl 120.0000 mm
Thickness of bottom Support Lug Plate Tpl 10.0000 mm
Distance between Gussets Dgp 90.0000 mm
Mean Width of Gusset Plate Wgp 102.0000 mm
Height of Gusset Plate Hgp 250.0000 mm
Thickness of Gusset Plate Tgp 15.0000 mm
Pad Width along Circumference C11P 160.000 mm
Pad Length along Vessel Axis C22P 300.000 mm
Pad Thickness Tpad 8.000 mm
Bolt Material SA-193 B7
Bolt Allowable Stress at Design Temperature 172.38 MPa
Thread Series TEMA Metric
Bolt Diameter 20.00 mm
Results for Support Lugs: Description: LUG
Overturning Moment at Support Lug 3061. N-m
Weight Load at the top of one Lug 7247. N
62
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Force on one Lug, Operating Condition [Flug]:
= ( W/Nlug + Mlug/( Rlug * Nlug/2 ) )
= ( 14493/2 + 3060/( 709.54 * 2/2 ))
= 11558.71 N
Force on one lug in the Empty Condition [Flugemp]:
= ( -Wemp/Nlug + Mlugemp/( Rlug * Nlug/2 ) )
= ( -3524/2 + 2130/( 709.54 * 2/2 ))
= 1238.85 N
Bottom Support Plate Bending Stress (Point Load) [Spl]:
= ( Flugemp/2*Dgp/2)/((Wpl/6)*Tpl²) (Uplift Condition)
= ( 1238/2*90.000/2)/((250.00/6)*10.0000²)
= 6.69 MPa
Bottom Plate Required Thickness (Point Load) 2.4632 mm
Bottom Plate required thickness for Uplift per ADM S 3/4 [trUpl]:
= 0.72 * sqrt( Flugemp * Dgp / ( ( Wpl - dt ) * Spa ) )
= 0.72 * sqrt( 1238.9 * 90.00/( ( 250.00 - 23.17 ) * 110.267 ) )
= 1.52 mm
Bearing Area [Ba]:
= Lpl * Wfb
= 120.000 * 200.000
= 24000.00 mm²
Bending Stress in bottom Plate (Unif. Load) Per Bednar p.156 [Spl2]:
= Beta1 * Flug/Ba * Wfb² / Tpl² per Roark & Young 5th Ed.
= 0.157 * 11558.7/24000.000 * 200.000²/10.000²
= 30.21 MPa
Bottom Plate Required Thickness (Uniform Load) 5.2346 mm
63
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015
Bottom Plate Required Thickness based on ADM S 3/4 [trAD]:
= 0.71 * Dgp * (( Flug / ( Lpl * Wfb ))/Spa )½
= 0.71*90.00*((11558/(120.00*200.00))/110.267)½
= 4.223 mm
Note: If using the AD Code recommendations, the force bearing width (Wfb) must
be greater than or equal to 1/3 of the bottom plate radial width (Wpl)
plus the pad thickness (Padthk), if there is a pad.
Bottom Support Plate Allowable Stress [Spa]:
= 2/3 * Ylug
= 2/3 * 165
= 110.27 MPa
Gusset Plate Axial Stress ( Force / Gusset Plate Area ) [Sgp]:
= ( Flug/2 )/( Wgp * Tgp )
= ( 11558/2 )/( 102.000 *15.0000 )
= 3.78 MPa
Required Thickness of Gussets per AISC 3.8494 mm
Gusset Plate Allowable Stress [Sga]:
= ( 1-(Klr)²/(2*Cc²))*Fy /( 5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
= ( 1-( 66.67 )²/(2 * 151.74² )) * 165/
( 5/3+3*(66.67 )/(8* 151.74 )-( 66.67³)/(8*151.74³)
= 82.07 MPa
Maximum Compressive Gusset Plate Stress per Bednar [SgpB]:
= Flug*( 3*Dlug-Wpl )/( Tgp* Wpl² * (Sin(Alph_G))² )
= 11558 *( 3*600.000 -250.000 )/( 15.0000 *250.000²*(Sin(40.18 ))² )
= 45.90 MPa
64
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Gusset Plate Allowable Compressive Stress [SgaB]:
= 18000/(1+(1/18000)*( Hgp/Sin(Alph_G)/(0.289*Tgp))² )
= 18000/(1+(1/18000)* (250.000/Sin(40.18 )/(0.289*15.0000 ))² )
= 85.96 MPa
Determine the required bolt area due to Uplift [Abr]:
= Flugemp / Sabolt
= 1238.854/172.375
= 7.19 mm²
The Area available in a single bolt : 217.051 mm² [OK]
Input Echo, WRC107/537 Item 1, Description: LUG
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 204.762 mm
Vessel Thickness Tv 7.156 mm
Design Temperature 50.00 °C
Attachment Type Type Rectangular
Parameter C11 C11 54.00 mm
Parameter C22 C22 200.00 mm
Thickness of Reinforcing Pad Tpad 8.000 mm
Pad Parameter C11P C11p 160.000 mm
Pad Parameter C22P C22p 300.000 mm
Design Internal Pressure Dp 18.000 bar
Include Pressure Thrust No
65
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Vessel Centerline Direction Cosine Vx 0.000
Vessel Centerline Direction Cosine Vy 1.000
Vessel Centerline Direction Cosine Vz 0.000
Nozzle Centerline Direction Cosine Nx 1.000
Nozzle Centerline Direction Cosine Ny 0.000
Nozzle Centerline Direction Cosine Nz 0.000
Global Force (SUS) Fx 0.0 N
Global Force (SUS) Fy 7246.6 N
Global Force (SUS) Fz 0.0 N
Global Moment (SUS) Mx 0.0 N-m
Global Moment (SUS) My 0.0 N-m
Global Moment (SUS) Mz 4349.7 N-m
Internal Pressure (SUS) P 18.00 bar
Include Pressure Thrust No
Global Force (OCC) Fx 1708.0 N
Global Force (OCC) Fy 4312.1 N
Global Force (OCC) Fz 0.0 N
Global Moment (OCC) Mx 0.0 N-m
Global Moment (OCC) My 1025.2 N-m
Global Moment (OCC) Mz 2588.3 N-m
Occasional Internal Pressure (OCC) Pvar 0.00 bar
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
Compute Pressure Stress per WRC-368 No
66
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015
WRC 107 Stress Calculation for SUStained loads:
Radial Load P 0.0 N
Circumferential Shear VC 0.0 N
Longitudinal Shear VL 7246.6 N
Circumferential Moment MC 0.0 N-m
Longitudinal Moment ML -4349.7 N-m
Torsional Moment MT 0.0 N-m
Dimensionless Parameters used : Gamma = 7.25
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.693 4C ! 0.973 (A,B)
N(PHI) / ( P/Rm ) 0.693 3C ! 0.668 (C,D)
M(PHI) / ( P ) 0.417 2C1 0.041 (A,B)
M(PHI) / ( P ) 0.417 1C 0.064 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.380 3A ! 0.292 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.491 1A 0.082 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.588 3B ! 0.760 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.532 1B ! 0.022 (A,B,C,D)
N(x) / ( P/Rm ) 0.565 3C ! 0.668 (A,B)
N(x) / ( P/Rm ) 0.565 4C ! 0.973 (C,D)
M(x) / ( P ) 0.588 1C1 ! 0.052 (A,B)
M(x) / ( P ) 0.588 2C ! 0.034 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.380 4A ! 0.602 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.684 2A ! 0.042 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.588 4B ! 0.331 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.718 2B ! 0.040 (A,B,C,D)
67
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015
Note - The ! mark next to the figure name denotes curve value exceeded.
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 0 0 0 0 0 0 0 0
Circ. Bend. P | 0 0 0 0 0 0 0 0
Circ. Memb. MC | 0 0 0 0 0 0 0 0
Circ. Bend. MC | 0 0 0 0 0 0 0 0
Circ. Memb. ML | 21 21 -21 -21 0 0 0 0
Circ. Bend. ML | 43 -43 -43 43 0 0 0 0
|
Tot. Circ. Str.| 64.9 -21.5 -64.9 21.5 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Long. Memb. P | 0 0 0 0 0 0 0 0
Long. Bend. P | 0 0 0 0 0 0 0 0
Long. Memb. MC | 0 0 0 0 0 0 0 0
Long. Bend. MC | 0 0 0 0 0 0 0 0
Long. Memb. ML | 16 16 -16 -16 0 0 0 0
Long. Bend. ML | 58 -58 -58 58 0 0 0 0
|
Tot. Long. Str.| 74.2 -41.8 -74.2 41.8 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Shear VC | 0 0 0 0 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
68
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Shear MT | 0 0 0 0 0 0 0 0
|
Tot. Shear| 0.0 0.0 0.0 0.0 -1.2 -1.2 1.2 1.2
------------------------------------------------------------------------
Str. Int. | 74.22 41.80 74.22 41.80 2.39 2.39 2.39 2.39
------------------------------------------------------------------------
WARNING: Ratio of Pad Radius/Rm (0.755) is not between 0.01 and 0.571.
Dimensionless Parameters used : Gamma = 14.81
Dimensionless Loads for Cylindrical Shells at Pad edge:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 1.343 4C ! 1.591 (A,B)
N(PHI) / ( P/Rm ) 1.343 3C ! 0.884 (C,D)
M(PHI) / ( P ) 0.957 2C1 ! 0.015 (A,B)
M(PHI) / ( P ) 0.957 1C ! 0.055 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.931 3A ! 0.554 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 1.017 1A ! 0.066 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 1.148 3B ! 1.113 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 1.093 1B ! 0.012 (A,B,C,D)
N(x) / ( P/Rm ) 1.162 3C ! 0.884 (A,B)
N(x) / ( P/Rm ) 1.162 4C ! 1.591 (C,D)
M(x) / ( P ) 1.195 1C1 ! 0.030 (A,B)
M(x) / ( P ) 1.195 2C ! 0.030 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.931 4A ! 1.587 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 1.258 2A ! 0.032 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 1.148 4B ! 0.568 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 1.278 2B ! 0.023 (A,B,C,D)
69
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Note - The ! mark next to the figure name denotes curve value exceeded.
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Edge of Reinforcing Pad
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 0 0 0 0 0 0 0 0
Circ. Bend. P | 0 0 0 0 0 0 0 0
Circ. Memb. MC | 0 0 0 0 0 0 0 0
Circ. Bend. MC | 0 0 0 0 0 0 0 0
Circ. Memb. ML | 45 45 -45 -45 0 0 0 0
Circ. Bend. ML | 53 -53 -53 53 0 0 0 0
|
Tot. Circ. Str.| 99.0 -7.4 -99.0 7.4 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Long. Memb. P | 0 0 0 0 0 0 0 0
Long. Bend. P | 0 0 0 0 0 0 0 0
Long. Memb. MC | 0 0 0 0 0 0 0 0
Long. Bend. MC | 0 0 0 0 0 0 0 0
Long. Memb. ML | 33 33 -33 -33 0 0 0 0
Long. Bend. ML | 86 -86 -86 86 0 0 0 0
|
Tot. Long. Str.| 120.3 -53.1 -120.3 53.1 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Shear VC | 0 0 0 0 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 0 0 0 0 0 0 0 0
70
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 |
Tot. Shear| 0.0 0.0 0.0 0.0 -1.7 -1.7 1.7 1.7
------------------------------------------------------------------------
Str. Int. | 120.35 53.09 120.35 53.09 3.38 3.38 3.38 3.38
------------------------------------------------------------------------
WRC 107 Stress Calculation for OCCasional loads:
Radial Load P 1708.0 N
Circumferential Shear VC 0.0 N
Longitudinal Shear VL 4312.1 N
Circumferential Moment MC -1025.2 N-m
Longitudinal Moment ML -2588.3 N-m
Torsional Moment MT 0.0 N-m
Dimensionless Parameters used : Gamma = 7.25
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 0 0 0 0 0 0 0 0
Circ. Bend. P | -1 1 -1 1 -2 2 -2 2
Circ. Memb. MC | 0 0 0 0 1 1 -1 -1
Circ. Bend. MC | 0 0 0 0 40 -40 -40 40
Circ. Memb. ML | 12 12 -12 -12 0 0 0 0
Circ. Bend. ML | 25 -25 -25 25 0 0 0 0
|
Tot. Circ. Str.| 35.8 -11.9 -41.4 13.6 38.5 -36.9 -45.5 41.3
------------------------------------------------------------------------
71
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Long. Memb. P | 0 0 0 0 0 0 0 0
Long. Bend. P | -2 2 -2 2 -1 1 -1 1
Long. Memb. MC | 0 0 0 0 4 4 -4 -4
Long. Bend. MC | 0 0 0 0 15 -15 -15 15
Long. Memb. ML | 9 9 -9 -9 0 0 0 0
Long. Bend. ML | 34 -34 -34 34 0 0 0 0
|
Tot. Long. Str.| 41.2 -23.2 -47.2 26.5 17.1 -10.0 -22.1 11.1
------------------------------------------------------------------------
Shear VC | 0 0 0 0 0 0 0 0
Shear VL | 0 0 0 0 0 0 0 0
Shear MT | 0 0 0 0 0 0 0 0
|
Tot. Shear| 0.0 0.0 0.0 0.0 -0.7 -0.7 0.7 0.7
------------------------------------------------------------------------
Str. Int. | 41.16 23.23 47.18 26.52 38.49 36.96 45.54 41.27
------------------------------------------------------------------------
WARNING: Ratio of Pad Radius/Rm (0.755) is not between 0.01 and 0.571.
Dimensionless Parameters used : Gamma = 14.81
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Edge of Reinforcing Pad
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | -3 -3 -3 -3 -1 -1 -1 -1
Circ. Bend. P | -2 2 -2 2 -11 11 -11 11
Circ. Memb. MC | 0 0 0 0 5 5 -5 -5
72
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Bend. MC | 0 0 0 0 73 -73 -73 73
Circ. Memb. ML | 27 27 -27 -27 0 0 0 0
Circ. Bend. ML | 31 -31 -31 31 0 0 0 0
|
Tot. Circ. Str.| 52.4 -5.1 -65.4 3.8 65.8 -59.7 -92.0 77.9
------------------------------------------------------------------------
Long. Memb. P | -1 -1 -1 -1 -3 -3 -3 -3
Long. Bend. P | -5 5 -5 5 -6 6 -6 6
Long. Memb. MC | 0 0 0 0 16 16 -16 -16
Long. Bend. MC | 0 0 0 0 28 -28 -28 28
Long. Memb. ML | 20 20 -20 -20 0 0 0 0
Long. Bend. ML | 51 -51 -51 51 0 0 0 0
|
Tot. Long. Str.| 63.6 -27.6 -79.6 35.6 35.7 -9.7 -55.0 14.7
------------------------------------------------------------------------
Shear VC | 0 0 0 0 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 0 0 0 0 0 0 0 0
|
Tot. Shear| 0.0 0.0 0.0 0.0 -1.0 -1.0 1.0 1.0
------------------------------------------------------------------------
Str. Int. | 63.63 27.60 79.59 35.59 65.87 59.76 92.01 77.94
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
73
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Pm (SUS) | 11 13 11 13 11 13 11 13
Circ. Pm (OCC) | 0 0 0 0 0 0 0 0
Circ. Pm(TOTAL)| 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1
Circ. Pl (SUS) | 21 21 -21 -21 0 0 0 0
Circ. Pl (OCC) | 11 11 -13 -13 0 0 -2 -2
Circ. Pl(TOTAL)| 33.6 33.6 -35.6 -35.6 0.8 0.8 -2.1 -2.1
Circ. Q (SUS) | 43 -43 -43 43 0 0 0 0
Circ. Q (OCC) | 23 -23 -27 27 37 -37 -43 43
Circ. Q (TOTAL)| 67.0 -67.0 -70.7 70.7 37.7 -37.7 -43.4 43.4
------------------------------------------------------------------------
Long. Pm (SUS) | 5 5 5 5 5 5 5 5
Long. Pm (OCC) | 0 0 0 0 0 0 0 0
Long. Pm(TOTAL)| 5.7 5.7 5.7 5.7 5.7 5.7 5.7 5.7
Long. Pl (SUS) | 16 16 -16 -16 0 0 0 0
Long. Pl (OCC) | 8 8 -10 -10 3 3 -5 -5
Long. Pl(TOTAL)| 25.2 25.2 -26.5 -26.5 3.5 3.5 -5.5 -5.5
Long. Q (SUS) | 58 -58 -58 58 0 0 0 0
Long. Q (OCC) | 32 -32 -36 36 13 -13 -16 16
Long. Q (TOTAL)| 90.2 -90.2 -94.9 94.9 13.6 -13.6 -16.6 16.6
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pm (OCC) | 0 0 0 0 0 0 0 0
Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
Shear Pl (SUS) | 0 0 0 0 -1 -1 1 1
Shear Pl (OCC) | 0 0 0 0 0 0 0 0
Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -1.9 -1.9 1.9 1.9
Shear Q (SUS) | 0 0 0 0 0 0 0 0
Shear Q (OCC) | 0 0 0 0 0 0 0 0
Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Pm (SUS) | 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1
------------------------------------------------------------------------
Pm (SUS+OCC) | 11.3 13.1 11.3 13.1 11.3 13.1 11.3 13.1
74
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 ------------------------------------------------------------------------
Pm+Pl (SUS) | 33.0 34.8 10.5 10.5 11.6 13.3 11.6 13.3
------------------------------------------------------------------------
Pm+Pl (SUS+OCC)| 45.0 46.8 24.3 22.5 13.0 14.6 9.8 11.5
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 121.0 59.4 115.7 74.0 49.9 24.0 34.4 54.5
------------------------------------------------------------------------
------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 13.12 115.15 | Passed
Pm (SUS+OCC) | 13.12 138.18 | Passed
Pm+Pl (SUS) | 34.84 172.72 | Passed
Pm+Pl (SUS+OCC)| 46.77 207.26 | Passed
Pm+Pl+Q (TOTAL)| 121.04 345.44 | Passed
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Reinforcing Pad Edge
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 24 26 24 26 24 26 24 26
Circ. Pm (OCC) | 0 0 0 0 0 0 0 0
Circ. Pm(TOTAL)| 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7
Circ. Pl (SUS) | 45 45 -45 -45 0 0 0 0
Circ. Pl (OCC) | 23 23 -30 -30 3 3 -7 -7
75
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Circ. Pl(TOTAL)| 69.4 69.4 -76.6 -76.6 3.0 3.0 -7.0 -7.0
Circ. Q (SUS) | 53 -53 -53 53 0 0 0 0
Circ. Q (OCC) | 28 -28 -34 34 62 -62 -84 84
Circ. Q (TOTAL)| 81.9 -81.9 -87.8 87.8 62.8 -62.8 -85.0 85.0
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pm (OCC) | 0 0 0 0 0 0 0 0
Long. Pm(TOTAL)| 12.4 12.4 12.4 12.4 12.4 12.4 12.4 12.4
Long. Pl (SUS) | 33 33 -33 -33 0 0 0 0
Long. Pl (OCC) | 18 18 -22 -22 12 12 -20 -20
Long. Pl(TOTAL)| 51.6 51.6 -55.6 -55.6 13.0 13.0 -20.2 -20.2
Long. Q (SUS) | 86 -86 -86 86 0 0 0 0
Long. Q (OCC) | 45 -45 -57 57 22 -22 -34 34
Long. Q (TOTAL)| 132.3 -132.3 -144.3 144.3 22.7 -22.7 -34.8 34.8
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pm (OCC) | 0 0 0 0 0 0 0 0
Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
Shear Pl (SUS) | 0 0 0 0 -1 -1 1 1
Shear Pl (OCC) | 0 0 0 0 -1 -1 1 1
Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -2.7 -2.7 2.7 2.7
Shear Q (SUS) | 0 0 0 0 0 0 0 0
Shear Q (OCC) | 0 0 0 0 0 0 0 0
Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
------------------------------------------------------------------------
Pm (SUS) | 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7
------------------------------------------------------------------------
Pm (SUS+OCC) | 24.9 26.7 24.9 26.7 24.9 26.7 24.9 26.7
------------------------------------------------------------------------
Pm+Pl (SUS) | 70.7 72.5 21.2 21.2 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS+OCC)| 94.3 96.1 51.7 49.9 29.7 31.0 26.1 27.9
------------------------------------------------------------------------
76
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Sup. Lug Calcs: Ope : Lugs: 2 1:14p Jan 11,2015 Pm+Pl+Q (Total)| 196.4 82.5 187.5 101.1 90.9 36.2 67.4 104.7
------------------------------------------------------------------------
------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.69 115.15 | Passed
Pm (SUS+OCC) | 26.69 138.18 | Passed
Pm+Pl (SUS) | 72.47 172.72 | Passed
Pm+Pl (SUS+OCC)| 96.13 207.26 | Passed
Pm+Pl+Q (TOTAL)| 196.42 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
77
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N3 From : 10
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-403 316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Elliptical Head D 204.76 mm
Aspect Ratio of Elliptical Head Ar 2.00
Head Finished (Minimum) Thickness t 7.1565 mm
Head Internal Corrosion Allowance c 0.0000 mm
Head External Corrosion Allowance co 0.0000 mm
Distance from Head Centerline L1 0.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 90.00 deg
Diameter 2.0000 in.
78
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 150.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 6.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
79
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N3
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 2.375 in.
Actual Thickness Used in Calculation 0.218 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Elliptical Head, Tr [Int. Press]
= (P*K1*D))/(2*S*E-0.2*P) per UG-37(a)(3)
= (18.35*0.900*204.7621)/(2 *115.15*1.00-0.2*18.35)
= 1.4707 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*30.1625)/(115*1.00+0.4*18.35)
= 0.4776 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.2876 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 98.5012 mm
Parallel to Vessel Wall, opening length d 49.2506 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 13.8430 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N3.
This calculation is valid for nozzles that meet all the requirements of
80
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.4776 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6342 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6342 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 3.4200 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 3.420 , max( 1.634 , 1.500 ) ]
= 1.6342 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.4776 , 1.6342 )
= 1.6342 mm
Available Nozzle Neck Thickness = 0.875 * 5.537 = 4.845 mm --> OK
SA-403 316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N3
Intermediate Calc. for nozzle/shell Welds Tmin 5.5372 mm
81
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N3 Nozl: 23 1:14p Jan 11,2015
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 3.8760 = 0.7 * tmin. 4.2420 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 79.866 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 2.4093 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 159.5657 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
82
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N1 From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1255.0001 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 0.00 deg
Diameter 2.0000 in.
83
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
84
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N1
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N1.
This calculation is valid for nozzles that meet all the requirements of
85
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
Stresses on Nozzle due to External and Pressure Loads per the ASME
B31.3 Piping Code (see 319.4.4 and 302.3.5):
Sustained : 15.2, Allowable : 137.9 MPa Passed
Expansion : 0.0, Allowable : 329.5 MPa Passed
Occasional : 1.4, Allowable : 183.4 MPa Passed
Shear : 8.3, Allowable : 96.5 MPa Passed
86
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for
the determination of the expansion stress allowable.
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N1
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
Input Echo, WRC107/537 Item 1, Description: N1 :
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 202.717 mm
87
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm
Design Temperature -195.57 °C
Vessel Material SA-312 TP316L
Vessel Cold S.I. Allowable Smc 115.15 MPa
Vessel Hot S.I. Allowable Smh 115.15 MPa
Attachment Type Type Round
Diameter Basis for Nozzle Nbasis ID
Corrosion Allowance for Nozzle Can 0.0000 mm
Nozzle Diameter Dn 50.800 mm
Nozzle Thickness Tn 13.462 mm
Nozzle Material SA-182 F316
Nozzle Cold S.I. Allowable SNmc 137.90 MPa
Nozzle Hot S.I. Allowable SNmh 137.90 MPa
Design Internal Pressure Dp 18.347 bar
Include Pressure Thrust No
External Forces and Moments in WRC 107/537 Convention:
Radial Load (SUS) P -1040.0 N
Longitudinal Shear (SUS) Vl 1040.0 N
Circumferential Shear (SUS) Vc 1040.0 N
Circumferential Moment (SUS) Mc 380.0 N-m
Longitudinal Moment (SUS) Ml 380.0 N-m
Torsional Moment (SUS) Mt 380.0 N-m
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
88
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads:
Radial Load P -1040.0 N
Circumferential Shear VC 1040.0 N
Longitudinal Shear VL 1040.0 N
Circumferential Moment MC 380.0 N-m
Longitudinal Moment ML 380.0 N-m
Torsional Moment MT 380.0 N-m
Dimensionless Parameters used : Gamma = 14.66
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)
N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)
M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)
M(PHI) / ( P ) 0.324 1C 0.058 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.324 1A 0.081 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)
N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)
N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)
M(x) / ( P ) 0.324 1C1 0.059 (A,B)
M(x) / ( P ) 0.324 2C 0.033 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)
89
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 2 2 2 2 2 2 2 2
Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7
Circ. Memb. MC | 0 0 0 0 -9 -9 9 9
Circ. Bend. MC | 0 0 0 0 -105 105 105 -105
Circ. Memb. ML | -23 -23 23 23 0 0 0 0
Circ. Bend. ML | -32 32 32 -32 0 0 0 0
|
Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6
------------------------------------------------------------------------
Long. Memb. P | 2 2 2 2 2 2 2 2
Long. Bend. P | 7 -7 7 -7 4 -4 4 -4
Long. Memb. MC | 0 0 0 0 -19 -19 19 19
Long. Bend. MC | 0 0 0 0 -51 51 51 -51
Long. Memb. ML | -9 -9 9 9 0 0 0 0
Long. Bend. ML | -55 55 55 -55 0 0 0 0
|
Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2
------------------------------------------------------------------------
Shear VC | 1 1 -1 -1 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 5 5 5 5 5 5 5 5
|
90
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8
------------------------------------------------------------------------
Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 25 26 25 26 25 26 25 26
Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11
Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21
Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1
Shear Q (SUS) | 5 5 5 5 5 5 5 5
------------------------------------------------------------------------
Pm (SUS) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5
------------------------------------------------------------------------
91
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N1 Nozl: 24 1:14p Jan 11,2015 ------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.94 115.15 | Passed
Pm+Pl (SUS) | 53.24 172.72 | Passed
Pm+Pl+Q (TOTAL)| 150.27 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
92
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N2 From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 2975.0002 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 285.00 deg
Diameter 2.0000 in.
93
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
94
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N2
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N2.
This calculation is valid for nozzles that meet all the requirements of
95
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
Stresses on Nozzle due to External and Pressure Loads per the ASME
B31.3 Piping Code (see 319.4.4 and 302.3.5):
Sustained : 15.2, Allowable : 137.9 MPa Passed
Expansion : 0.0, Allowable : 329.5 MPa Passed
Occasional : 1.4, Allowable : 183.4 MPa Passed
Shear : 8.3, Allowable : 96.5 MPa Passed
96
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for
the determination of the expansion stress allowable.
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N2
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
Input Echo, WRC107/537 Item 1, Description: N2 :
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 202.717 mm
97
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm
Design Temperature -195.57 °C
Vessel Material SA-312 TP316L
Vessel Cold S.I. Allowable Smc 115.15 MPa
Vessel Hot S.I. Allowable Smh 115.15 MPa
Attachment Type Type Round
Diameter Basis for Nozzle Nbasis ID
Corrosion Allowance for Nozzle Can 0.0000 mm
Nozzle Diameter Dn 50.800 mm
Nozzle Thickness Tn 13.462 mm
Nozzle Material SA-182 F316
Nozzle Cold S.I. Allowable SNmc 137.90 MPa
Nozzle Hot S.I. Allowable SNmh 137.90 MPa
Design Internal Pressure Dp 18.347 bar
Include Pressure Thrust No
External Forces and Moments in WRC 107/537 Convention:
Radial Load (SUS) P -1040.0 N
Longitudinal Shear (SUS) Vl 1040.0 N
Circumferential Shear (SUS) Vc 1040.0 N
Circumferential Moment (SUS) Mc 380.0 N-m
Longitudinal Moment (SUS) Ml 380.0 N-m
Torsional Moment (SUS) Mt 380.0 N-m
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
98
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads:
Radial Load P -1040.0 N
Circumferential Shear VC 1040.0 N
Longitudinal Shear VL 1040.0 N
Circumferential Moment MC 380.0 N-m
Longitudinal Moment ML 380.0 N-m
Torsional Moment MT 380.0 N-m
Dimensionless Parameters used : Gamma = 14.66
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)
N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)
M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)
M(PHI) / ( P ) 0.324 1C 0.058 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.324 1A 0.081 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)
N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)
N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)
M(x) / ( P ) 0.324 1C1 0.059 (A,B)
M(x) / ( P ) 0.324 2C 0.033 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)
99
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 2 2 2 2 2 2 2 2
Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7
Circ. Memb. MC | 0 0 0 0 -9 -9 9 9
Circ. Bend. MC | 0 0 0 0 -105 105 105 -105
Circ. Memb. ML | -23 -23 23 23 0 0 0 0
Circ. Bend. ML | -32 32 32 -32 0 0 0 0
|
Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6
------------------------------------------------------------------------
Long. Memb. P | 2 2 2 2 2 2 2 2
Long. Bend. P | 7 -7 7 -7 4 -4 4 -4
Long. Memb. MC | 0 0 0 0 -19 -19 19 19
Long. Bend. MC | 0 0 0 0 -51 51 51 -51
Long. Memb. ML | -9 -9 9 9 0 0 0 0
Long. Bend. ML | -55 55 55 -55 0 0 0 0
|
Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2
------------------------------------------------------------------------
Shear VC | 1 1 -1 -1 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 5 5 5 5 5 5 5 5
|
100
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8
------------------------------------------------------------------------
Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 25 26 25 26 25 26 25 26
Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11
Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21
Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1
Shear Q (SUS) | 5 5 5 5 5 5 5 5
------------------------------------------------------------------------
Pm (SUS) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5
------------------------------------------------------------------------
101
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N2 Nozl: 25 1:14p Jan 11,2015 ------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.94 115.15 | Passed
Pm+Pl (SUS) | 53.24 172.72 | Passed
Pm+Pl+Q (TOTAL)| 150.27 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
102
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N4 From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1480.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 90.00 deg
Diameter 2.0000 in.
103
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
104
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N4
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N4.
This calculation is valid for nozzles that meet all the requirements of
105
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
Stresses on Nozzle due to External and Pressure Loads per the ASME
B31.3 Piping Code (see 319.4.4 and 302.3.5):
Sustained : 15.2, Allowable : 137.9 MPa Passed
Expansion : 0.0, Allowable : 329.5 MPa Passed
Occasional : 1.4, Allowable : 183.4 MPa Passed
Shear : 8.3, Allowable : 96.5 MPa Passed
106
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for
the determination of the expansion stress allowable.
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N4
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
Input Echo, WRC107/537 Item 1, Description: N4 :
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 202.717 mm
107
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm
Design Temperature -195.57 °C
Vessel Material SA-312 TP316L
Vessel Cold S.I. Allowable Smc 115.15 MPa
Vessel Hot S.I. Allowable Smh 115.15 MPa
Attachment Type Type Round
Diameter Basis for Nozzle Nbasis ID
Corrosion Allowance for Nozzle Can 0.0000 mm
Nozzle Diameter Dn 50.800 mm
Nozzle Thickness Tn 13.462 mm
Nozzle Material SA-182 F316
Nozzle Cold S.I. Allowable SNmc 137.90 MPa
Nozzle Hot S.I. Allowable SNmh 137.90 MPa
Design Internal Pressure Dp 18.347 bar
Include Pressure Thrust No
External Forces and Moments in WRC 107/537 Convention:
Radial Load (SUS) P -1040.0 N
Longitudinal Shear (SUS) Vl 1040.0 N
Circumferential Shear (SUS) Vc 1040.0 N
Circumferential Moment (SUS) Mc 380.0 N-m
Longitudinal Moment (SUS) Ml 380.0 N-m
Torsional Moment (SUS) Mt 380.0 N-m
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
108
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads:
Radial Load P -1040.0 N
Circumferential Shear VC 1040.0 N
Longitudinal Shear VL 1040.0 N
Circumferential Moment MC 380.0 N-m
Longitudinal Moment ML 380.0 N-m
Torsional Moment MT 380.0 N-m
Dimensionless Parameters used : Gamma = 14.66
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)
N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)
M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)
M(PHI) / ( P ) 0.324 1C 0.058 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.324 1A 0.081 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)
N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)
N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)
M(x) / ( P ) 0.324 1C1 0.059 (A,B)
M(x) / ( P ) 0.324 2C 0.033 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)
109
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 2 2 2 2 2 2 2 2
Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7
Circ. Memb. MC | 0 0 0 0 -9 -9 9 9
Circ. Bend. MC | 0 0 0 0 -105 105 105 -105
Circ. Memb. ML | -23 -23 23 23 0 0 0 0
Circ. Bend. ML | -32 32 32 -32 0 0 0 0
|
Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6
------------------------------------------------------------------------
Long. Memb. P | 2 2 2 2 2 2 2 2
Long. Bend. P | 7 -7 7 -7 4 -4 4 -4
Long. Memb. MC | 0 0 0 0 -19 -19 19 19
Long. Bend. MC | 0 0 0 0 -51 51 51 -51
Long. Memb. ML | -9 -9 9 9 0 0 0 0
Long. Bend. ML | -55 55 55 -55 0 0 0 0
|
Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2
------------------------------------------------------------------------
Shear VC | 1 1 -1 -1 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 5 5 5 5 5 5 5 5
|
110
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8
------------------------------------------------------------------------
Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 25 26 25 26 25 26 25 26
Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11
Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21
Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1
Shear Q (SUS) | 5 5 5 5 5 5 5 5
------------------------------------------------------------------------
Pm (SUS) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5
------------------------------------------------------------------------
111
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N4 Nozl: 26 1:14p Jan 11,2015 ------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.94 115.15 | Passed
Pm+Pl (SUS) | 53.24 172.72 | Passed
Pm+Pl+Q (TOTAL)| 150.27 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
112
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N5 From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 3055.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 345.00 deg
Diameter 2.0000 in.
113
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
114
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N5
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N5.
This calculation is valid for nozzles that meet all the requirements of
115
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
Stresses on Nozzle due to External and Pressure Loads per the ASME
B31.3 Piping Code (see 319.4.4 and 302.3.5):
Sustained : 15.2, Allowable : 137.9 MPa Passed
Expansion : 0.0, Allowable : 329.5 MPa Passed
Occasional : 1.4, Allowable : 183.4 MPa Passed
Shear : 8.3, Allowable : 96.5 MPa Passed
116
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for
the determination of the expansion stress allowable.
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N5
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
Input Echo, WRC107/537 Item 1, Description: N5 :
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 202.717 mm
117
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm
Design Temperature -195.57 °C
Vessel Material SA-312 TP316L
Vessel Cold S.I. Allowable Smc 115.15 MPa
Vessel Hot S.I. Allowable Smh 115.15 MPa
Attachment Type Type Round
Diameter Basis for Nozzle Nbasis ID
Corrosion Allowance for Nozzle Can 0.0000 mm
Nozzle Diameter Dn 50.800 mm
Nozzle Thickness Tn 13.462 mm
Nozzle Material SA-182 F316
Nozzle Cold S.I. Allowable SNmc 137.90 MPa
Nozzle Hot S.I. Allowable SNmh 137.90 MPa
Design Internal Pressure Dp 18.347 bar
Include Pressure Thrust No
External Forces and Moments in WRC 107/537 Convention:
Radial Load (SUS) P -1040.0 N
Longitudinal Shear (SUS) Vl 1040.0 N
Circumferential Shear (SUS) Vc 1040.0 N
Circumferential Moment (SUS) Mc 380.0 N-m
Longitudinal Moment (SUS) Ml 380.0 N-m
Torsional Moment (SUS) Mt 380.0 N-m
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
118
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads:
Radial Load P -1040.0 N
Circumferential Shear VC 1040.0 N
Longitudinal Shear VL 1040.0 N
Circumferential Moment MC 380.0 N-m
Longitudinal Moment ML 380.0 N-m
Torsional Moment MT 380.0 N-m
Dimensionless Parameters used : Gamma = 14.66
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)
N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)
M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)
M(PHI) / ( P ) 0.324 1C 0.058 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.324 1A 0.081 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)
N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)
N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)
M(x) / ( P ) 0.324 1C1 0.059 (A,B)
M(x) / ( P ) 0.324 2C 0.033 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)
119
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 2 2 2 2 2 2 2 2
Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7
Circ. Memb. MC | 0 0 0 0 -9 -9 9 9
Circ. Bend. MC | 0 0 0 0 -105 105 105 -105
Circ. Memb. ML | -23 -23 23 23 0 0 0 0
Circ. Bend. ML | -32 32 32 -32 0 0 0 0
|
Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6
------------------------------------------------------------------------
Long. Memb. P | 2 2 2 2 2 2 2 2
Long. Bend. P | 7 -7 7 -7 4 -4 4 -4
Long. Memb. MC | 0 0 0 0 -19 -19 19 19
Long. Bend. MC | 0 0 0 0 -51 51 51 -51
Long. Memb. ML | -9 -9 9 9 0 0 0 0
Long. Bend. ML | -55 55 55 -55 0 0 0 0
|
Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2
------------------------------------------------------------------------
Shear VC | 1 1 -1 -1 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 5 5 5 5 5 5 5 5
|
120
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8
------------------------------------------------------------------------
Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 25 26 25 26 25 26 25 26
Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11
Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21
Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1
Shear Q (SUS) | 5 5 5 5 5 5 5 5
------------------------------------------------------------------------
Pm (SUS) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5
------------------------------------------------------------------------
121
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N5 Nozl: 27 1:14p Jan 11,2015 ------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.94 115.15 | Passed
Pm+Pl (SUS) | 53.24 172.72 | Passed
Pm+Pl+Q (TOTAL)| 150.27 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
122
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: N6 From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 255.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 90.00 deg
Diameter 2.0000 in.
123
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
124
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: N6
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: N6.
This calculation is valid for nozzles that meet all the requirements of
125
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
Stresses on Nozzle due to External and Pressure Loads per the ASME
B31.3 Piping Code (see 319.4.4 and 302.3.5):
Sustained : 15.2, Allowable : 137.9 MPa Passed
Expansion : 0.0, Allowable : 329.5 MPa Passed
Occasional : 1.4, Allowable : 183.4 MPa Passed
Shear : 8.3, Allowable : 96.5 MPa Passed
126
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 Note : The number of cycles on this nozzle was assumed to be 7000 or less for
the determination of the expansion stress allowable.
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: N6
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
Input Echo, WRC107/537 Item 1, Description: N6 :
Diameter Basis for Vessel Vbasis ID
Cylindrical or Spherical Vessel Cylsph Cylindrical
Internal Corrosion Allowance Cas 0.0000 mm
Vessel Diameter Dv 202.717 mm
127
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 Vessel Thickness Tv 7.156 mm
Design Temperature -195.57 °C
Vessel Material SA-312 TP316L
Vessel Cold S.I. Allowable Smc 115.15 MPa
Vessel Hot S.I. Allowable Smh 115.15 MPa
Attachment Type Type Round
Diameter Basis for Nozzle Nbasis ID
Corrosion Allowance for Nozzle Can 0.0000 mm
Nozzle Diameter Dn 50.800 mm
Nozzle Thickness Tn 13.462 mm
Nozzle Material SA-182 F316
Nozzle Cold S.I. Allowable SNmc 137.90 MPa
Nozzle Hot S.I. Allowable SNmh 137.90 MPa
Design Internal Pressure Dp 18.347 bar
Include Pressure Thrust No
External Forces and Moments in WRC 107/537 Convention:
Radial Load (SUS) P -1040.0 N
Longitudinal Shear (SUS) Vl 1040.0 N
Circumferential Shear (SUS) Vc 1040.0 N
Circumferential Moment (SUS) Mc 380.0 N-m
Longitudinal Moment (SUS) Ml 380.0 N-m
Torsional Moment (SUS) Mt 380.0 N-m
Use Interactive Control No
WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No
128
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads:
Radial Load P -1040.0 N
Circumferential Shear VC 1040.0 N
Longitudinal Shear VL 1040.0 N
Circumferential Moment MC 380.0 N-m
Longitudinal Moment ML 380.0 N-m
Torsional Moment MT 380.0 N-m
Dimensionless Parameters used : Gamma = 14.66
Dimensionless Loads for Cylindrical Shells at Attachment Junction:
-------------------------------------------------------------------
Curves read for 1979 Beta Figure Value Location
-------------------------------------------------------------------
N(PHI) / ( P/Rm ) 0.324 4C 2.100 (A,B)
N(PHI) / ( P/Rm ) 0.324 3C 1.445 (C,D)
M(PHI) / ( P ) 0.324 2C1 0.034 (A,B)
M(PHI) / ( P ) 0.324 1C 0.058 (C,D)
N(PHI) / ( MC/(Rm**2 * Beta) ) 0.324 3A 0.631 (A,B,C,D)
M(PHI) / ( MC/(Rm * Beta) ) 0.324 1A 0.081 (A,B,C,D)
N(PHI) / ( ML/(Rm**2 * Beta) ) 0.324 3B 1.569 (A,B,C,D)
M(PHI) / ( ML/(Rm * Beta) ) 0.324 1B 0.025 (A,B,C,D)
N(x) / ( P/Rm ) 0.324 3C 1.445 (A,B)
N(x) / ( P/Rm ) 0.324 4C 2.100 (C,D)
M(x) / ( P ) 0.324 1C1 0.059 (A,B)
M(x) / ( P ) 0.324 2C 0.033 (C,D)
N(x) / ( MC/(Rm**2 * Beta) ) 0.324 4A 1.280 (A,B,C,D)
M(x) / ( MC/(Rm * Beta) ) 0.324 2A 0.039 (A,B,C,D)
N(x) / ( ML/(Rm**2 * Beta) ) 0.324 4B 0.614 (A,B,C,D)
M(x) / ( ML/(Rm * Beta) ) 0.324 2B 0.042 (A,B,C,D)
129
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015
Stress Concentration Factors Kn = 1.00, Kb = 1.00
Stresses in the Vessel at the Attachment Junction
------------------------------------------------------------------------
| Stress Values at
Type of | (MPa )
---------------|--------------------------------------------------------
Stress Load| Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Memb. P | 2 2 2 2 2 2 2 2
Circ. Bend. P | 4 -4 4 -4 7 -7 7 -7
Circ. Memb. MC | 0 0 0 0 -9 -9 9 9
Circ. Bend. MC | 0 0 0 0 -105 105 105 -105
Circ. Memb. ML | -23 -23 23 23 0 0 0 0
Circ. Bend. ML | -32 32 32 -32 0 0 0 0
|
Tot. Circ. Str.| -49.0 8.2 63.0 -10.5 -106.2 91.5 124.4 -101.6
------------------------------------------------------------------------
Long. Memb. P | 2 2 2 2 2 2 2 2
Long. Bend. P | 7 -7 7 -7 4 -4 4 -4
Long. Memb. MC | 0 0 0 0 -19 -19 19 19
Long. Bend. MC | 0 0 0 0 -51 51 51 -51
Long. Memb. ML | -9 -9 9 9 0 0 0 0
Long. Bend. ML | -55 55 55 -55 0 0 0 0
|
Tot. Long. Str.| -55.5 41.2 73.8 -51.5 -63.2 31.0 77.1 -33.2
------------------------------------------------------------------------
Shear VC | 1 1 -1 -1 0 0 0 0
Shear VL | 0 0 0 0 -1 -1 1 1
Shear MT | 5 5 5 5 5 5 5 5
|
130
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 Tot. Shear| 6.8 6.8 4.4 4.4 4.4 4.4 6.8 6.8
------------------------------------------------------------------------
Str. Int. | 59.77 42.56 75.36 51.99 106.69 91.80 125.36 102.30
------------------------------------------------------------------------
WRC 107/537 Stress Summations:
Vessel Stress Summation at Attachment Junction
------------------------------------------------------------------------
Type of | Stress Values at
Stress Int. | (MPa )
---------------|--------------------------------------------------------
Location | Au Al Bu Bl Cu Cl Du Dl
---------------|--------------------------------------------------------
Circ. Pm (SUS) | 25 26 25 26 25 26 25 26
Circ. Pl (SUS) | -20 -20 26 26 -7 -7 11 11
Circ. Q (SUS) | -28 28 36 -36 -98 98 113 -113
------------------------------------------------------------------------
Long. Pm (SUS) | 12 12 12 12 12 12 12 12
Long. Pl (SUS) | -7 -7 11 11 -16 -16 21 21
Long. Q (SUS) | -48 48 62 -62 -47 47 55 -55
------------------------------------------------------------------------
Shear Pm (SUS) | 0 0 0 0 0 0 0 0
Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1
Shear Q (SUS) | 5 5 5 5 5 5 5 5
------------------------------------------------------------------------
Pm (SUS) | 25.1 26.9 25.1 26.9 25.1 26.9 25.1 26.9
------------------------------------------------------------------------
Pm+Pl (SUS) | 6.3 7.3 51.4 53.2 21.4 23.3 37.0 38.7
------------------------------------------------------------------------
Pm+Pl+Q (Total)| 45.1 56.0 91.7 56.1 81.8 118.7 150.3 75.5
------------------------------------------------------------------------
131
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : N6 Nozl: 28 1:14p Jan 11,2015 ------------------------------------------------------------------------
Type of | Max. S.I. S.I. Allowable | Result
Stress Int. | MPa |
---------------|--------------------------------------------------------
Pm (SUS) | 26.94 115.15 | Passed
Pm+Pl (SUS) | 53.24 172.72 | Passed
Pm+Pl+Q (TOTAL)| 150.27 345.44 | Passed
------------------------------------------------------------------------
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
132
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K1A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 825.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 20.00 deg
Diameter 3.0000 in.
133
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 3.2893 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
134
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K1A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K1A.
This calculation is valid for nozzles that meet all the requirements of
135
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K1A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
136
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1A Nozl: 29 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
137
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K1B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 225.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 20.00 deg
Diameter 3.0000 in.
138
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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| \ | |
| \ | |
|____________\|__|
139
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K1B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K1B.
This calculation is valid for nozzles that meet all the requirements of
140
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K1B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
141
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K1B Nozl: 30 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
142
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 31 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K2A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1065.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 315.00 deg
Diameter 2.0000 in.
143
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 31 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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____________/| |
| \ | |
| \ | |
|____________\|__|
144
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 31 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K2A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K2A.
This calculation is valid for nozzles that meet all the requirements of
145
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 31 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K2A
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
146
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2A Nozl: 31 1:14p Jan 11,2015
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
147
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 32 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K2B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 225.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 315.00 deg
Diameter 2.0000 in.
148
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 32 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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| |
____________/| |
| \ | |
| \ | |
|____________\|__|
149
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 32 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K2B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K2B.
This calculation is valid for nozzles that meet all the requirements of
150
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 32 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K2B
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
151
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K2B Nozl: 32 1:14p Jan 11,2015
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
152
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3A Nozl: 33 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K3A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 625.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 225.00 deg
Diameter 3.0000 in.
153
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3A Nozl: 33 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
154
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3A Nozl: 33 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K3A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K3A.
This calculation is valid for nozzles that meet all the requirements of
155
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3A Nozl: 33 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K3A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
156
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3A Nozl: 33 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
157
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3B Nozl: 34 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K3B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 225.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 225.00 deg
Diameter 3.0000 in.
158
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3B Nozl: 34 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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159
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3B Nozl: 34 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K3B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K3B.
This calculation is valid for nozzles that meet all the requirements of
160
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3B Nozl: 34 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K3B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
161
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K3B Nozl: 34 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
162
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4A Nozl: 35 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K4A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 804.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 165.00 deg
Diameter 3.0000 in.
163
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4A Nozl: 35 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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| \ | |
| \ | |
|____________\|__|
164
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4A Nozl: 35 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K4A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K4A.
This calculation is valid for nozzles that meet all the requirements of
165
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4A Nozl: 35 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K4A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
166
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4A Nozl: 35 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
167
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4B Nozl: 36 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K4B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 405.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 165.00 deg
Diameter 3.0000 in.
168
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4B Nozl: 36 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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| \ | |
| \ | |
|____________\|__|
169
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4B Nozl: 36 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K4B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K4B.
This calculation is valid for nozzles that meet all the requirements of
170
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4B Nozl: 36 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K4B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
171
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K4B Nozl: 36 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
172
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6A Nozl: 37 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K6A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1949.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 340.00 deg
Diameter 2.0000 in.
173
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6A Nozl: 37 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
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| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
174
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6A Nozl: 37 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K6A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K6A.
This calculation is valid for nozzles that meet all the requirements of
175
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6A Nozl: 37 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K6A
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
176
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6A Nozl: 37 1:14p Jan 11,2015
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
177
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6B Nozl: 38 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K6B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1500.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-182 F316
Material UNS Number S31600
Material Specification/Type Forgings
Allowable Stress at Temperature Sn 137.90 MPa
Allowable Stress At Ambient Sna 137.90 MPa
Diameter Basis (for tr calc only) ID
Layout Angle 340.00 deg
Diameter 2.0000 in.
178
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6B Nozl: 38 1:14p Jan 11,2015
Size and Thickness Basis Actual
Actual Thickness tn 13.4620 mm
Flange Material SA-182 F316
Flange Type Long Weld Neck
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 9.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
179
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6B Nozl: 38 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K6B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Inside Diameter Used in Calculation 2.000 in.
Actual Thickness Used in Calculation 0.530 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per App. 1 of Nozzle Wall, Trn [Int. Press]
= R( exp([P/(SE)] - 1 ) per Appendix 1-2 (a)(1)
= 25.400(exp([18.35/(137.90*1.00]-1)
= 0.3402 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.3761 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 101.6000 mm
Parallel to Vessel Wall, opening length d 50.8000 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K6B.
This calculation is valid for nozzles that meet all the requirements of
180
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6B Nozl: 38 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.3761 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.3761 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 13.4620 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
SA-182 F316, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K6B
Intermediate Calc. for nozzle/shell Welds Tmin 8.1788 mm
181
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K6B Nozl: 38 1:14p Jan 11,2015
Results Per UW-16.1:
Required Thickness Actual Thickness
Nozzle Weld 5.7252 = 0.7 * tmin. 6.3630 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 7.7460 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 214.9025 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
182
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7A Nozl: 39 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K7A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1850.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 225.00 deg
Diameter 3.0000 in.
183
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7A Nozl: 39 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
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|____________\|__|
184
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7A Nozl: 39 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K7A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K7A.
This calculation is valid for nozzles that meet all the requirements of
185
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7A Nozl: 39 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K7A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
186
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7A Nozl: 39 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
187
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7B Nozl: 40 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K7B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1500.0000 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 225.00 deg
Diameter 3.0000 in.
188
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7B Nozl: 40 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
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____________/| |
| \ | |
| \ | |
|____________\|__|
189
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7B Nozl: 40 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K7B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K7B.
This calculation is valid for nozzles that meet all the requirements of
190
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7B Nozl: 40 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K7B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
191
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K7B Nozl: 40 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
192
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8A Nozl: 41 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K8A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 2004.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 165.00 deg
Diameter 3.0000 in.
193
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8A Nozl: 41 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
194
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8A Nozl: 41 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K8A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K8A.
This calculation is valid for nozzles that meet all the requirements of
195
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8A Nozl: 41 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K8A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
196
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8A Nozl: 41 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
197
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8B Nozl: 42 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K8B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1604.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 165.00 deg
Diameter 3.0000 in.
198
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8B Nozl: 42 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
199
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8B Nozl: 42 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K8B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K8B.
This calculation is valid for nozzles that meet all the requirements of
200
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8B Nozl: 42 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K8B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
201
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K8B Nozl: 42 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
202
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5A Nozl: 43 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K5A From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1904.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 30.00 deg
Diameter 3.0000 in.
203
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5A Nozl: 43 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
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204
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5A Nozl: 43 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K5A
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K5A.
This calculation is valid for nozzles that meet all the requirements of
205
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5A Nozl: 43 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K5A
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
206
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5A Nozl: 43 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
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207
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5B Nozl: 44 1:14p Jan 11,2015
INPUT VALUES, Nozzle Description: K5B From : 20
Pressure for Reinforcement Calculations P 18.347 bar
Temperature for Internal Pressure Temp 50 °C
Design External Pressure Pext 1.03 bar
Temperature for External Pressure Tempex 50 °C
Shell Material SA-312 TP316L
Shell Allowable Stress at Temperature S 115.15 MPa
Shell Allowable Stress At Ambient Sa 115.15 MPa
Inside Diameter of Cylindrical Shell D 202.72 mm
Design Length of Section L 3192.0637 mm
Shell Finished (Minimum) Thickness t 7.1565 mm
Shell Internal Corrosion Allowance c 0.0000 mm
Shell External Corrosion Allowance co 0.0000 mm
Distance from Bottom/Left Tangent 1554.9999 mm
User Entered Minimum Design Metal Temperature 0.00 °C
Type of Element Connected to the Shell : Nozzle
Material SA-312 TP316L
Material UNS Number S31603
Material Specification/Type Smls. & wld. pipe
Allowable Stress at Temperature Sn 115.15 MPa
Allowable Stress At Ambient Sna 115.15 MPa
Diameter Basis (for tr calc only) OD
Layout Angle 30.00 deg
Diameter 3.0000 in.
208
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5B Nozl: 44 1:14p Jan 11,2015
Size and Thickness Basis Nominal
Nominal Thickness tn 80S
Flange Material SA-182 F316
Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm
Joint Efficiency of Shell Seam at Nozzle E1 1.00
Joint Efficiency of Nozzle Neck En 1.00
Outside Projection ho 200.0000 mm
Weld leg size between Nozzle and Pad/Shell Wo 8.0000 mm
Groove weld depth between Nozzle and Vessel Wgnv 7.1564 mm
Inside Projection h 0.0000 mm
Weld leg size, Inside Element to Shell Wi 0.0000 mm
ASME Code Weld Type per UW-16 None
Class of attached Flange 150
Grade of attached Flange GR 2.2
The Pressure Design option was Overall MAWP.
Nozzle Sketch (may not represent actual weld type/configuration)
| |
| |
| |
| |
____________/| |
| \ | |
| \ | |
|____________\|__|
209
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5B Nozl: 44 1:14p Jan 11,2015
Insert Nozzle No Pad, no Inside projection
Reinforcement CALCULATION, Description: K5B
ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45
Actual Outside Diameter Used in Calculation 3.500 in.
Actual Thickness Used in Calculation 0.300 in.
Nozzle input data check completed without errors.
Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]
= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)
= (18.35*101.3587)/(115*1.00-0.6*18.35)
= 1.6309 mm
Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]
= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1)
= (18.35*44.4500)/(115*1.00+0.4*18.35)
= 0.7039 mm
Required Nozzle thickness under External Pressure per UG-28 : 0.4058 mm
UG-40, Limits of Reinforcement : [Internal Pressure]
Parallel to Vessel Wall (Diameter Limit) Dl 147.3200 mm
Parallel to Vessel Wall, opening length d 73.6600 mm
Normal to Vessel Wall (Thickness Limit), no pad Tlnp 17.8911 mm
Note:
Taking a UG-36(c)(3)(a) exemption for nozzle: K5B.
This calculation is valid for nozzles that meet all the requirements of
210
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5B Nozl: 44 1:14p Jan 11,2015 paragraph UG-36. Please check the Code carefully, especially for nozzles
that are not isolated or do not meet Code spacing requirements. To force
the computation of areas for small nozzles go to Tools->Configuration
and check the box to force the UG-37 small nozzle area calculation or
force the Appendix 1-10 computation in Nozzle Design Options.
UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]
Wall Thickness for Internal/External pressures ta = 0.7039 mm
Wall Thickness per UG16(b), tr16b = 1.5000 mm
Wall Thickness, shell/head, internal pressure trb1 = 1.6309 mm
Wall Thickness tb1 = max(trb1, tr16b) = 1.6309 mm
Wall Thickness tb2 = max(trb2, tr16b) = 1.5000 mm
Wall Thickness per table UG-45 tb3 = 4.8000 mm
Determine Nozzle Thickness candidate [tb]:
= min[ tb3, max( tb1,tb2) ]
= min[ 4.800 , max( 1.631 , 1.500 ) ]
= 1.6309 mm
Minimum Wall Thickness of Nozzle Necks [tUG-45]:
= max( ta, tb )
= max( 0.7039 , 1.6309 )
= 1.6309 mm
Available Nozzle Neck Thickness = 0.875 * 7.620 = 6.668 mm --> OK
SA-312 TP316L, Min Metal Temp without impact per UHA-51: -196 °C
Weld Size Calculations, Description: K5B
Intermediate Calc. for nozzle/shell Welds Tmin 7.6200 mm
Results Per UW-16.1:
211
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Calcs. : K5B Nozl: 44 1:14p Jan 11,2015 Required Thickness Actual Thickness
Nozzle Weld 5.3340 = 0.7 * tmin. 5.6560 = 0.7 * Wo mm
NOTE : Skipping the nozzle attachment weld strength calculations.
Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)
(small nozzles) do not require a weld strength check.
Maximum Allowable Pressure for this Nozzle at this Location:
Converged Max. Allow. Pressure in Operating case 77.185 bar
Note: The MAWP of this junction was limited by the parent Shell/Head.
The Drop for this Nozzle is : 10.2665 mm
The Cut Length for this Nozzle is, Drop + Ho + H + T : 217.4230 mm
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015
Nozzle Schedule:
Nominal Flange Noz. Wall Re-Pad Cut
Description Size Sch/Type O/Dia Thk ODia Thick Length
in. Cls in. mm mm mm mm
------------------------------------------------------------------------------
N3 2.000 80S WNF 2.375 5.537 - - 159.57
N1 2.000 150 LWN 3.060 13.462 - - 214.90
N2 2.000 150 LWN 3.060 13.462 - - 214.90
N4 2.000 150 LWN 3.060 13.462 - - 214.90
N5 2.000 150 LWN 3.060 13.462 - - 214.90
N6 2.000 150 LWN 3.060 13.462 - - 214.90
K2A 2.000 150 LWN 3.060 13.462 - - 214.90
K2B 2.000 150 LWN 3.060 13.462 - - 214.90
K6A 2.000 150 LWN 3.060 13.462 - - 214.90
K6B 2.000 150 LWN 3.060 13.462 - - 214.90
K1A 3.000 80S WNF 3.500 7.620 - - 217.42
K1B 3.000 80S WNF 3.500 7.620 - - 217.42
K3A 3.000 80S WNF 3.500 7.620 - - 217.42
K3B 3.000 80S WNF 3.500 7.620 - - 217.42
K4A 3.000 80S WNF 3.500 7.620 - - 217.42
K4B 3.000 80S WNF 3.500 7.620 - - 217.42
K7A 3.000 80S WNF 3.500 7.620 - - 217.42
K7B 3.000 80S WNF 3.500 7.620 - - 217.42
K8A 3.000 80S WNF 3.500 7.620 - - 217.42
K8B 3.000 80S WNF 3.500 7.620 - - 217.42
K5A 3.000 80S WNF 3.500 7.620 - - 217.42
K5B 3.000 80S WNF 3.500 7.620 - - 217.42
General Notes for the above table:
The Cut Length is the Outside Projection + Inside Projection + Drop +
213
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 In Plane Shell Thickness. This value does not include weld gaps,
nor does it account for shrinkage.
In the case of Oblique Nozzles, the Outside Diameter must
be increased. The Re-Pad WIDTH around the nozzle is calculated as follows:
Width of Pad = (Pad Outside Dia. (per above) - Nozzle Outside Dia.)/2
For hub nozzles, the thickness and diameter shown are those of the smaller
and thinner section.
Nozzle Material and Weld Fillet Leg Size Details:
Shl Grve Noz Shl/Pad Pad OD Pad Grve Inside
Nozzle Material Weld Weld Weld Weld Weld
mm mm mm mm mm
------------------------------------------------------------------------------
N3 SA-312 TP316L 7.156 6.000 - - -
N1 SA-182 F316 7.156 9.000 - - -
N2 SA-182 F316 7.156 9.000 - - -
N4 SA-182 F316 7.156 9.000 - - -
N5 SA-182 F316 7.156 9.000 - - -
N6 SA-182 F316 7.156 9.000 - - -
K2A SA-182 F316 7.156 9.000 - - -
K2B SA-182 F316 7.156 9.000 - - -
K6A SA-182 F316 7.156 9.000 - - -
K6B SA-182 F316 7.156 9.000 - - -
K1A SA-312 TP316L 3.289 9.000 - - -
K1B SA-312 TP316L 7.156 9.000 - - -
K3A SA-312 TP316L 7.156 8.000 - - -
K3B SA-312 TP316L 7.156 8.000 - - -
K4A SA-312 TP316L 7.156 8.000 - - -
K4B SA-312 TP316L 7.156 8.000 - - -
K7A SA-312 TP316L 7.156 8.000 - - -
K7B SA-312 TP316L 7.156 8.000 - - -
214
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 K8A SA-312 TP316L 7.156 8.000 - - -
K8B SA-312 TP316L 7.156 8.000 - - -
K5A SA-312 TP316L 7.156 8.000 - - -
K5B SA-312 TP316L 7.156 8.000 - - -
Note: The Outside projections below do not include the flange thickness.
Nozzle Miscellaneous Data:
Elevation/Distance Layout Projection Installed In
Nozzle From Datum Angle Outside Inside Component
mm deg. mm mm
----------------------------------------------------------------------------
N3 90.00 150.00 0.00 Head
N1 1200.000 0.00 200.00 0.00 Shell
N2 2920.000 285.00 200.00 0.00 Shell
N4 1425.000 90.00 200.00 0.00 Shell
N5 3000.000 345.00 200.00 0.00 Shell
N6 200.000 90.00 200.00 0.00 Shell
K2A 1010.000 315.00 200.00 0.00 Shell
K2B 170.000 315.00 200.00 0.00 Shell
K6A 1895.000 340.00 200.00 0.00 Shell
K6B 1445.000 340.00 200.00 0.00 Shell
K1A 770.000 20.00 200.00 0.00 Shell
K1B 170.000 20.00 200.00 0.00 Shell
K3A 570.000 225.00 200.00 0.00 Shell
K3B 170.000 225.00 200.00 0.00 Shell
K4A 750.000 165.00 200.00 0.00 Shell
K4B 350.000 165.00 200.00 0.00 Shell
K7A 1795.000 225.00 200.00 0.00 Shell
K7B 1445.000 225.00 200.00 0.00 Shell
K8A 1950.000 165.00 200.00 0.00 Shell
K8B 1550.000 165.00 200.00 0.00 Shell
215
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Schedule : Step: 42 1:14p Jan 11,2015 K5A 1850.000 30.00 200.00 0.00 Shell
K5B 1500.000 30.00 200.00 0.00 Shell
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015
Nozzle Calculation Summary:
Description MAWP Ext MAPNC UG45 [tr] Weld Areas or
bar bar Path Stresses
---------------------------------------------------------------------------
N3 79.87 ... ... OK 1.63 OK NoCalc[*]
N1 77.19 ... ... OK 1.63 OK NoCalc[*]
N2 77.19 ... ... OK 1.63 OK NoCalc[*]
N4 77.19 ... ... OK 1.63 OK NoCalc[*]
N5 77.19 ... ... OK 1.63 OK NoCalc[*]
N6 77.19 ... ... OK 1.63 OK NoCalc[*]
K1A 77.19 ... ... OK 1.63 OK NoCalc[*]
K1B 77.19 ... ... OK 1.63 OK NoCalc[*]
K2A 77.19 ... ... OK 1.63 OK NoCalc[*]
K2B 77.19 ... ... OK 1.63 OK NoCalc[*]
K3A 77.19 ... ... OK 1.63 OK NoCalc[*]
K3B 77.19 ... ... OK 1.63 OK NoCalc[*]
K4A 77.19 ... ... OK 1.63 OK NoCalc[*]
K4B 77.19 ... ... OK 1.63 OK NoCalc[*]
K6A 77.19 ... ... OK 1.63 OK NoCalc[*]
K6B 77.19 ... ... OK 1.63 OK NoCalc[*]
K7A 77.19 ... ... OK 1.63 OK NoCalc[*]
K7B 77.19 ... ... OK 1.63 OK NoCalc[*]
K8A 77.19 ... ... OK 1.63 OK NoCalc[*]
K8B 77.19 ... ... OK 1.63 OK NoCalc[*]
K5A 77.19 ... ... OK 1.63 OK NoCalc[*]
K5B 77.19 ... ... OK 1.63 OK NoCalc[*]
---------------------------------------------------------------------------
Min. - Nozzles 77.19 K5B
Min. Shell&Flgs 18.35
Computed Vessel M.A.W.P. 18.35 bar
217
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015
[*] - This was a small opening and the areas were not computed or
the MAWP of this connection could not be computed because
the longitudinal bending stress was greater than the hoop stress.
Check the Spatial Relationship between the Nozzles
From Node Nozzle Description Y Coordinate, Layout Angle, Dia. Limit
10 N3 0.000 90.000 98.501
20 N1 1255.000 0.000 101.600
20 N2 2975.000 285.000 101.600
20 N4 1480.000 90.000 101.600
20 N5 3055.000 345.000 101.600
20 N6 255.000 90.000 101.600
20 K1A 825.000 20.000 147.320
20 K1B 225.000 20.000 147.320
20 K2A 1065.000 315.000 101.600
20 K2B 225.000 315.000 101.600
20 K3A 625.000 225.000 147.320
20 K3B 225.000 225.000 147.320
20 K4A 805.000 165.000 147.320
20 K4B 405.000 165.000 147.320
20 K6A 1950.000 340.000 101.600
20 K6B 1500.000 340.000 101.600
20 K7A 1850.000 225.000 147.320
20 K7B 1500.000 225.000 147.320
20 K8A 2005.000 165.000 147.320
20 K8B 1605.000 165.000 147.320
20 K5A 1905.000 30.000 147.320
20 K5B 1555.000 30.000 147.320
The nozzle spacing is computed by the following:
218
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Nozzle Summary : Step: 43 1:14p Jan 11,2015 = Sqrt( ll² + lc² ) where
ll - Arc length along the inside vessel surface in the long. direction.
lc - Arc length along the inside vessel surface in the circ. direction
If any interferences/violations are found, they will be noted below.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
219
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- MDMT Summary : Step: 44 1:14p Jan 11,2015
Minimum Design Metal Temperature Results Summary :
Curve Basic Reduced UG-20(f) Thickness Gov E*
Description MDMT MDMT MDMT ratio Thk
Notes °C °C °C mm
----------------------------------------------------------------------------
Head [16] -196
Shell [16] -196
N3 [15] -196
N1 [15] -196
N2 [15] -196
N4 [15] -196
N5 [15] -196
N6 [15] -196
K1A [15] -196
K1B [15] -196
K2A [15] -196
K2B [15] -196
K3A [15] -196
K3B [15] -196
K4A [15] -196
K4B [15] -196
K6A [15] -196
K6B [15] -196
K7A [15] -196
K7B [15] -196
K8A [15] -196
K8B [15] -196
K5A [15] -196
K5B [15] -196
----------------------------------------------------------------------------
Required Minimum Design Metal Temperature 0 °C
220
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- MDMT Summary : Step: 44 1:14p Jan 11,2015 Warmest Computed Minimum Design Metal Temperature -196 °C
Notes:
[ ! ] - This was an impact tested material.
[ 1] - Governing Nozzle Weld.
[ 4] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(c).
[ 5] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(b).
[ 6] - MDMT Calculations at the Shell/Head Joint.
[ 7] - MDMT Calculations for the Straight Flange.
[ 8] - Cylinder/Cone/Flange Junction MDMT.
[ 9] - Calculations in the Spherical Portion of the Head.
[10] - Calculations in the Knuckle Portion of the Head.
[11] - Calculated (Body Flange) Flange MDMT.
[12] - Calculated Flat Head MDMT per UCS-66.3
[13] - Tubesheet MDMT, shell side, if applicable
[14] - Tubesheet MDMT, tube side, if applicable
[15] - Nozzle Material
[16] - Shell or Head Material
UG-84(b)(2) was not considered.
UCS-66(g) was not considered.
UCS-66(i) was not considered.
Notes:
Impact test temps were not entered in and not considered in the analysis.
UCS-66(i) applies to impact tested materials not by specification and
UCS-66(g) applies to materials impact tested per UG-84.1 General Note (c).
The Basic MDMT includes the (30F) PWHT credit if applicable.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
221
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 Design Code: ASME Code Section VIII Division 1, 2010, 2011a
Diameter Spec : 219.075 mm OD
Vessel Design Length, Tangent to Tangent 3305.05 mm
Distance of Bottom Tangent above Grade 0.00 mm
Specified Datum Line Distance 55.00 mm
Shell Material SA-312 TP316L
Head Material SA-403 316L
Lug Material SA-240 316L
Nozzle Material SA-182 F316
Nozzle Material SA-312 TP316L
Internal Design Temperature 50 °C
Internal Design Pressure 18.000 bar
External Design Temperature 50 °C
External Design Pressure 1.034 bar
Maximum Allowable Working Pressure 18.347 bar
External Max. Allowable Working Pressure 28.681 bar
Hydrostatic Test Pressure 24.625 bar
Required Minimum Design Metal Temperature 0 °C
Warmest Computed Minimum Design Metal Temperature -196 °C
Wind Design Code User Defined
Earthquake Design Code G-Loading
Element Pressures and MAWP: bar
Element Desc | Design Pres. | External | M.A.W.P | Corrosion
222
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 | + Stat. head | Pressure | | Allowance
---------------------------------------------------------------------
Head 18.051 1.034 79.866 0.0000
Shell 18.051 1.034 77.185 0.0000
Body Flange (DN200) 18.000 1.034 18.398 0.0000
Blind Flange (DN200) 18.000 1.034 18.398 0.0000
Liquid Level: 650.00 mm Dens.: 803.232 kg/m³ Sp. Gr.: 0.804
Element "To" Elev Length Element Thk R e q d T h k Joint Eff
Type mm mm mm Int. Ext. Long Circ
-----------------------------------------------------------------------
Ellipse 0.0 55.0 8.2 1.7 1.5 1.00 1.00
Cylinder 3120.0 3120.0 8.2 1.7 1.9 1.00 1.00
Body Flg 3221.6 101.6 28.4 No Calc No Calc 1.00 1.00
Body Flg 3250.0 28.4 28.4 No Calc No Calc 1.00 1.00
Element thicknesses are shown as Nominal if specified, otherwise are Minimum
Total Wind Shear on Support 659. N
Total Earthquake Shear on Support 3416. N
Wind Moment on Support 656. N-m
Earthquake Moment on Support 3061. N-m
Note: Wind and Earthquake moments include the effects of user defined
forces and moments if any exist in the job and were specified
to act (compute loads and stresses) during these cases. Also
included are moment effects due to eccentric weights if any are
present in the input.
Weights:
223
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : S-6011 ---------------------------------------- Vessel Design Summary : Step: 45 1:14p Jan 11,2015 Fabricated - Bare W/O Removable Internals 388.1 kgm
Shop Test - Fabricated + Water ( Full ) 497.0 kgm
Shipping - Fab. + Rem. Intls.+ Shipping App. 388.1 kgm
Erected - Fab. + Rem. Intls.+ Insul. (etc) 388.1 kgm
Empty - Fab. + Intls. + Details + Wghts. 388.1 kgm
Operating - Empty + Operating Liquid (No CA) 521.2 kgm
Field Test - Empty Weight + Water (Full) 497.0 kgm
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
224
Attachment 1
225
(Ref :Recommended Practice for Plannning,Design & Construction Fixed Offshore(API RP 2A‐WSD,
:Design and Engineering Practice‐Shell (DEP) or Petronas Technical Spec.(PTS) 37.81.10.31)
Density of air, ρ = kg/m3
Max. wind Speed at 10m above MSL, μ = m/sShape coefficient, Cs =
Pressure, p = F/A = (ρ/2)μ2 Cs = kg/ms2
= N/m2
= kg/m2
0.7
749.129
749.129
WIND FORCE CALCULATION
76.336
MSET ENGINEERING CORPORATION SDN BHDDATE : 08.12.2014
DOC. REF. NO.: MSET/M2-251/S-6011/DC
SUBJECT: WIND FORCE CALC.
DOCUMENT TITLE: DESIGN CALCULATION
REVISION: 0
JOB NO: M2-251
1.225
41.8
226
Attachment 2
227
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015
Element and Detail Weights
| | Element | Element | Corroded | Corroded | Extra due |
From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % |
| | kgm | m³ | kgm | m³ | kgm |
---------------------------------------------------------------------------
10| 20| 5.97865 | 0.0029355 | 5.97865 | 0.0029355 | 0.29893 |
20| 30| 137.032 | 0.10276 | 137.032 | 0.10276 | 6.85162 |
30| 40| 19.5277 | 0.0032789 | 19.5277 | 0.0032789 | 0.97638 |
40| 50| 21.3476 | ... | 21.3476 | ... | 1.06738 |
---------------------------------------------------------------------------
Total 183 0.11 183 0.11 9
Weight of Details
| | Weight of | X Offset, | Y Offset, |
From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description
| | kgm | mm | mm |
-------------------------------------------------
10|Nozl| 3.82814 | -51.1905 | ... | N3
20|Sadl| 11.2964 | 350.000 | 192.612 | Left saddle
20|Sadl| 11.2964 | 2770.00 | 192.612 | Right saddle
20|Nozl| 7.18497 | 1200.00 | 127.781 | N1
20|Nozl| 7.18497 | 2920.00 | 127.781 | N2
20|Nozl| 7.18497 | 1425.00 | 127.781 | N4
20|Nozl| 7.18497 | 3000.00 | 127.781 | N5
20|Nozl| 7.18497 | 200.000 | 127.781 | N6
20|Nozl| 8.15833 | 770.000 | 146.831 | K1A
20|Nozl| 8.15833 | 170.000 | 146.831 | K1B
20|Nozl| 7.18496 | 1010.00 | 127.781 | K2A
228
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 20|Nozl| 7.18496 | 170.000 | 127.781 | K2B
20|Nozl| 8.15833 | 570.000 | 146.831 | K3A
20|Nozl| 8.15833 | 170.000 | 146.831 | K3B
20|Nozl| 8.15833 | 750.000 | 146.831 | K4A
20|Nozl| 8.15833 | 350.000 | 146.831 | K4B
20|Nozl| 7.18496 | 1895.00 | 127.781 | K6A
20|Nozl| 7.18496 | 1445.00 | 127.781 | K6B
20|Nozl| 8.15833 | 1795.00 | 146.831 | K7A
20|Nozl| 8.15833 | 1445.00 | 146.831 | K7B
20|Nozl| 8.15833 | 1950.00 | 146.831 | K8A
20|Nozl| 8.15833 | 1550.00 | 146.831 | K8B
20|Nozl| 8.15833 | 1850.00 | 146.831 | K5A
20|Nozl| 8.15833 | 1500.00 | 146.831 | K5B
20|Wght| 100.000 | 1700.00 | ... | FILTER
20|Wght| 16.0000 | 1908.00 | ... | LIQUID (UPPER)
20|Wght| 30.0000 | 2567.00 | ... | LUGS
Total Weight of Each Detail Type
Total Weight of Saddles 22.6
Total Weight of Nozzles 166.4
Total Weight of Weights 146.0
---------------------------------------------------------------
Sum of the Detail Weights 335.0 kgm
Weight Summation
Fabricated Shop Test Shipping Erected Empty Operating
------------------------------------------------------------------------------
193.1 382.1 193.1 382.1 193.1 412.1
229
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 22.6 108.9 22.6 ... 22.6 ...
166.4 30.0 166.4 ... ... ...
... ... ... ... ... 146.0
... ... ... ... ... -30.0
... ... ... ... 166.4 ...
... ... ... ... 30.0 ...
------------------------------------------------------------------------------
382.1 521.0 382.1 412.1 412.1 528.1 kgm
Miscellaneous Weight Percent: 5.0 %
Note that the above value for the miscellaneous weight percent has
been applied to the shells/heads/flange/tubesheets/tubes etc. in the
weight calculations for metallic components.
Note: The shipping total has been modified because some items have
been specified as being installed in the shop.
Weight Summary
Fabricated Wt. - Bare Weight W/O Removable Internals 382.1 kgm
Shop Test Wt. - Fabricated Weight + Water ( Full ) 521.0 kgm
Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 382.1 kgm
Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 412.1 kgm
Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 412.1 kgm
Operating Wt. - Empty Wt + Operating Liq. Uncorroded 528.1 kgm
Oper. Wt. + CA - Corr Wt. + Operating Liquid 528.1 kgm
Field Test Wt. - Empty Weight + Water (Full) 521.0 kgm
Note: The Corroded Weight and thickness are used in the Horizontal
230
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Element and Detail Weights : Step: 7 1:45p Jan 11,2015 Vessel Analysis (Ope Case) and Earthquake Load Calculations.
Outside Surface Areas of Elements
| | Surface |
From| To | Area |
| | mm² |
----------------------------
10| 20| 91207.0 |
20| 30| 2.167E+06 |
30| 40| 148106. |
40| 50| 124315. |
-----------------------------
Total 2530993.000 mm²
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
231
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Wind Load Calculation : Step: 9 1:45p Jan 11,2015
Note: Using the User Defined Wind Profile ...
Platform Load Calculations
ID Wind Area Elevation Pressure Force Cf
mm² mm kPa N
-------------------------------------------------------------------------
Wind Loads on Masses/Equipment/Piping
ID Wind Area Elevation Pressure Force
mm² mm kPa N
-------------------------------------------------------------------------
FILTER 0.00 1700.00 0.75 0.00
LIQUID (UPPER 0.00 1908.00 0.75 0.00
LUGS 0.00 2567.00 0.75 0.00
Wind Load Calculation
| | Wind | Wind | Wind | Wind | Element |
From| To | Height | Diameter | Area | Pressure | Wind Load |
| | mm | mm | mm² | kPa | N |
---------------------------------------------------------------------------
10| 20| 300.000 | 262.890 | 24498.2 | 0.75000 | 18.3732 |
20| 30| 300.000 | 262.890 | 820217. | 0.75000 | 615.148 |
30| 40| 300.000 | 245.715 | 24964.6 | 0.75000 | 18.7230 |
40| 50| 300.000 | 245.715 | 6990.09 | 0.75000 | 5.24244 |
232
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Wind Load Calculation : Step: 9 1:45p Jan 11,2015 PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
233
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Earthquake Load Calculation : Step: 10 1:45p Jan 11,2015
Earthquake Loading Specified in G's
Horizontal Acceleration factor (GX) 0.500
Horizontal Acceleration factor (GZ) 0.500
Vertical Acceleration factor (GY) -2.000
Note: Loads are distributed evenly among all elements for horizontal
geometries.
Earthquake Load Calculation
| | Earthquake | Earthquake | Element |
From| To | Height | Weight | Ope Load |
| | mm | N | N |
-------------------------------------------------
10| 20| 102.381 | 863.036 | 431.518 |
20|Sadl| 102.381 | 863.036 | 431.518 |
Sadl| 30| 102.381 | 863.036 | 431.518 |
20| 30| 102.381 | 863.036 | 431.518 |
30| 40| 102.381 | 863.036 | 431.518 |
40| 50| 102.381 | 863.036 | 431.518 |
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
234
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015
ASME Horizontal Vessel Analysis: Stresses for the Left Saddle
(per ASME Sec. VIII Div. 2 based on the Zick method.)
Horizontal Vessel Stress Calculations : Operating Case
Note: Wear Pad Width (120.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
Minimum Wear Plate Width to be considered in analysis [b1]:
= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )
= 142.9579 mm
Input and Calculated Values:
Vessel Mean Radius Rm 105.96 mm
Stiffened Vessel Length per 4.15.6 L 3175.00 mm
Distance from Saddle to Vessel tangent a 106.00 mm
Saddle Width b 100.00 mm
Saddle Bearing Angle theta 120.00 degrees
Inside Depth of Head h2 51.19 mm
Shell Allowable Stress used in Calculation 115.15 MPa
Head Allowable Stress used in Calculation 115.15 MPa
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Operating Case 13801.04 N
235
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015
Horizontal Vessel Analysis Results: Actual Allowable
-------------------------------------------------------------------
Long. Stress at Top of Midspan -23.44 -977.24 MPa
Long. Stress at Top of Midspan 23.44 115.15 MPa
Long. Stress at Bottom of Midspan 50.09 115.15 MPa
Long. Stress at Top of Saddles 15.57 115.15 MPa
Long. Stress at Bottom of Saddles 12.09 115.15 MPa
Tangential Shear in Shell 19.47 69.09 MPa
Circ. Stress at Horn of Saddle 24.74 143.93 MPa
Circ. Compressive Stress in Shell 1.03 115.15 MPa
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:
= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 657.5/2 + 0 ) * 300.0000/183.5269
= 1612.1 N
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:
= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002
= 4.2 N
Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:
= max( Fl, Friction Force, Sum of X Forces ) * B / Ls
= max( 2589.11 , 0.00 , 0 ) * 300.0000/2420.0002
= 321.0 N
Saddle Reaction Force due to Earthquake Ft [Fst]:
236
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 2589/2 + 0 ) * 300.0000/183.5269
= 6348.4 N
Load Combination Results for Q + Wind or Seismic [Q]:
= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
= 7452 + Max( 4 , 1612 , 320 , 6348 )
= 13801.0 N
Summary of Loads at the base of this Saddle:
Vertical Load (including saddle weight) 13911.82 N
Transverse Shear Load Saddle 1294.55 N
Longitudinal Shear Load Saddle 2589.11 N
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is Welded to the Shell, k = 0.1
The Computed K values from Table 4.15.1:
K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011
K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405
K9 = 0.2711 K10 = 0.0581 K1* = 0.1923
Note: Dimension a is greater than or equal to Rm / 2.
Moment per Equation 4.15.3 [M1]:
= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -13801*106.00[1-(1-106.00/3175.00+(105.959²-51.191²)/
(2*106.00*3175.00))/(1+(4*51.19)/(3*3175.00))]
= -60.3 N-m
237
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Moment per Equation 4.15.4 [M2]:
= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
= 13801*3175/4(1+2(105²-51²)/(3175²))/(1+(4*51)/
(3*3175))-4*105/3175
= 9283.2 N-m
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:
= P * Rm/(2t) - M2/(pi*Rm²t)
= 18.000 * 105.959/(2*7.156 ) - 9283.2/(pi*106.0²*7.156 )
= -23.44 MPa
Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:
= P * Rm/(2t) + M2/(pi * Rm² * t)
= 18.000 * 105.959/(2 * 7.156 ) + 9283.2/(pi * 106.0² * 7.156 )
= 50.09 MPa
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:
= P * Rm/(2t) - M1/(K1*pi*Rm²t)
= 18.000*105.959/(2*7.156)--60.3/(0.1066*pi*106.0²*7.156)
= 15.57 MPa
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:
= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 18.000*105.959/(2*7.156)+-60.3/(0.1923*pi*106.0²*7.156)
= 12.09 MPa
Maximum Shear Force in the Saddle (4.15.5) [T]:
= Q(L-2a)/(L+(4*h2/3))
= 13801 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 51.19/3))
= 12608.5 N
238
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:
= K2 * T / ( Rm * t )
= 1.1707 * 12608.48/( 105.9593 * 7.1565 )
= 19.47 MPa
Decay Length (4.15.22) [x1,x2]:
= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 105.959 * 7.156 )
= 21.479 mm
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:
= -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= -0.7603 * 13801 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )
= -1.03 MPa
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:
= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -13801/(4*7.156 *(100.000 +21.479 +21.479 )) -
3*0.0529 *13801/(2*7.156²)
= -24.74 MPa
Effective reinforcing plate width (4.15.1) [B1]:
= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )
= 142.96 mm
Free Un-Restrained Thermal Expansion between the Saddles [Exp]:
= Alpha * Ls * ( Design Temperature - Ambient Temperature )
= 0.156E-04 * 2420.000 * ( 50.0 - 21.1 )
= 1.093 mm
239
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Results for Vessel Ribs, Web and Base:
Baseplate Length Bplen 210.0000 mm
Baseplate Thickness Bpthk 8.0000 mm
Baseplate Width Bpwid 100.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 2
Rib Thickness Ribtk 8.0000 mm
Web Thickness Webtk 8.0000 mm
Web Location Webloc Center
Moment of Inertia of Saddle - Lateral Direction
Y A AY Io
Shell 4. 1161. 4154. 19819.
Wearplate 12. 1200. 14588. 187335.
Web 126. 1743. 219723. 34594160.
BasePlate 239. 800. 191200. 45701020.
Totals 381. 4904. 429664. 80502336.
Value C1 = Sumof(Ay)/Sumof(A) = 88. mm
Value I = Sumof(Io) - C1*Sumof(Ay) = 42855068. mm**4
Value As = Sumof(A) - Ashell = 3743. mm²
K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035
Fh = K1 * Q = 0.2035 * 13801.044 = 2808.8120 N
Tension Stress, St = ( Fh/As ) = 0.7505 MPa
Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa
d = B - R*Sin(theta) / theta = 260.7126 mm
Bending Moment, M = Fh * d = 732.5896 N-m
240
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015
Bending Stress, Sb = ( M * C1 / I ) = 1.4974 MPa
Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa
Minimum Thickness of Baseplate per Moss :
= ( 3 * ( Q + Saddle_Wt ) * BasePlateWidth / ( 4 * BasePlateLength *
AllStress ))½
= ( 3 * (13801 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½
= 5.480 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress
Effective Baseplate Length [e]:
= ( Bplen - Clearance ) / ( Nribs - 1)
= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm
Baseplate Pressure Area [Ap]:
= e * Bpwid / 2
= 184.6000 * 100.0000/2 = 9229.9990 mm²
Axial Load [P]:
= Ap * Bp
= 9230.0 * 0.66 = 6065.9 N
Area of the Rib and Web [Ar]:
= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk
= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000
= 1271.200 mm²
Compressive Stress [Sc]:
= P/Ar
241
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = 6065.9/1271.2000 = 4.7722 MPa
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
Y A AY Ay² Io
Rib 50.0 634.4 31720.0 0.0 443558.7
Web 50.0 738.4 36920.0 0.0 7876.3
Values 50.0 1372.8 68640.0 0.0 451434.9
Bending Moment [Rm]:
= Fl /( 2 * Bplen ) * e * rl / 2
= 2589.1/( 2 * 210.00 ) * 184.600 * 290.61/2
= 165.422 N-m
KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1
Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/
( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)
Sca = 143.88 MPa
AISC Unity Check on Outside Ribs ( must be <= 1.0 )
Check = Sc/Sca + (Rm/Z)/Sba
Check = 4.77/143.88 + (165.42/9028.698 )/165.48
Check = 0.14
ASME Horizontal Vessel Analysis: Stresses for the Right Saddle
(per ASME Sec. VIII Div. 2 based on the Zick method.)
Note: Wear Pad Width (120.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
242
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015
Minimum Wear Plate Width to be considered in analysis [b1]:
= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )
= 142.9579 mm
Input and Calculated Values:
Vessel Mean Radius Rm 105.96 mm
Stiffened Vessel Length per 4.15.6 L 3175.00 mm
Distance from Saddle to Vessel tangent a 106.00 mm
Saddle Width b 100.00 mm
Saddle Bearing Angle theta 120.00 degrees
Shell Allowable Stress used in Calculation 115.15 MPa
Head Allowable Stress used in Calculation 115.15 MPa
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Operating Case 14208.82 N
Horizontal Vessel Analysis Results: Actual Allowable
-------------------------------------------------------------------
Long. Stress at Top of Midspan -25.49 -977.24 MPa
Long. Stress at Top of Midspan 25.49 115.15 MPa
Long. Stress at Bottom of Midspan 52.14 115.15 MPa
Long. Stress at Top of Saddles 14.26 115.15 MPa
Long. Stress at Bottom of Saddles 12.81 115.15 MPa
Tangential Shear in Shell 20.47 69.09 MPa
Circ. Stress at Horn of Saddle 25.47 143.93 MPa
243
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Circ. Compressive Stress in Shell 1.06 115.15 MPa
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:
= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 657.5/2 + 0 ) * 300.0000/183.5269
= 1612.1 N
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:
= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002
= 4.2 N
Saddle Reaction Force due to Earthquake Fl or Friction [Fsl]:
= max( Fl, Friction Force, Sum of X Forces ) * B / Ls
= max( 2589.11 , 0.00 , 0 ) * 300.0000/2420.0002
= 321.0 N
Saddle Reaction Force due to Earthquake Ft [Fst]:
= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 2589/2 + 0 ) * 300.0000/183.5269
= 6348.4 N
Load Combination Results for Q + Wind or Seismic [Q]:
= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
= 7860 + Max( 4 , 1612 , 320 , 6348 )
= 14208.8 N
Summary of Loads at the base of this Saddle:
Vertical Load (including saddle weight) 14319.59 N
244
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Transverse Shear Load Saddle 1294.55 N
Longitudinal Shear Load Saddle 2589.11 N
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is Welded to the Shell, k = 0.1
The Computed K values from Table 4.15.1:
K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011
K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405
K9 = 0.2711 K10 = 0.0581 K1* = 0.1923
Note: Dimension a is greater than or equal to Rm / 2.
Moment per Equation 4.15.3 [M1]:
= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -14208*106.00[1-(1-106.00/3175.00+(105.959²-0.000²)/
(2*106.00*3175.00))/(1+(4*0.00)/(3*3175.00))]
= -25.2 N-m
Moment per Equation 4.15.4 [M2]:
= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
= 14208*3175/4(1+2(105²-0²)/(3175²))/(1+(4*0)/
(3*3175))-4*105/3175
= 9801.2 N-m
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:
= P * Rm/(2t) - M2/(pi*Rm²t)
= 18.000 * 105.959/(2*7.156 ) - 9801.2/(pi*106.0²*7.156 )
= -25.49 MPa
245
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:
= P * Rm/(2t) + M2/(pi * Rm² * t)
= 18.000 * 105.959/(2 * 7.156 ) + 9801.2/(pi * 106.0² * 7.156 )
= 52.14 MPa
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:
= P * Rm/(2t) - M1/(K1*pi*Rm²t)
= 18.000*105.959/(2*7.156)--25.2/(0.1066*pi*106.0²*7.156)
= 14.26 MPa
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:
= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 18.000*105.959/(2*7.156)+-25.2/(0.1923*pi*106.0²*7.156)
= 12.81 MPa
Maximum Shear Force in the Saddle (4.15.5) [T]:
= Q(L-2a)/(L+(4*h2/3))
= 14208 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 0.00/3))
= 13260.1 N
Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:
= K2 * T / ( Rm * t )
= 1.1707 * 13260.07/( 105.9593 * 7.1565 )
= 20.47 MPa
Decay Length (4.15.22) [x1,x2]:
= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 105.959 * 7.156 )
= 21.479 mm
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:
246
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 = -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= -0.7603 * 14208 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )
= -1.06 MPa
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:
= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -14208/(4*7.156 *(100.000 +21.479 +21.479 )) -
3*0.0529 *14208/(2*7.156²)
= -25.47 MPa
Effective reinforcing plate width (4.15.1) [B1]:
= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )
= 142.96 mm
Results for Vessel Ribs, Web and Base
Baseplate Length Bplen 210.0000 mm
Baseplate Thickness Bpthk 8.0000 mm
Baseplate Width Bpwid 100.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 2
Rib Thickness Ribtk 8.0000 mm
Web Thickness Webtk 8.0000 mm
Web Location Webloc Center
Moment of Inertia of Saddle - Lateral Direction
Y A AY Io
Shell 4. 1161. 4154. 19819.
Wearplate 12. 1200. 14588. 187335.
Web 126. 1743. 219723. 34594160.
247
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 BasePlate 239. 800. 191200. 45701020.
Totals 381. 4904. 429664. 80502336.
Value C1 = Sumof(Ay)/Sumof(A) = 88. mm
Value I = Sumof(Io) - C1*Sumof(Ay) = 42855068. mm**4
Value As = Sumof(A) - Ashell = 3743. mm²
K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035
Fh = K1 * Q = 0.2035 * 14208.821 = 2891.8035 N
Tension Stress, St = ( Fh/As ) = 0.7727 MPa
Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa
d = B - R*Sin(theta) / theta = 260.7126 mm
Bending Moment, M = Fh * d = 754.2352 N-m
Bending Stress, Sb = ( M * C1 / I ) = 1.5416 MPa
Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa
Minimum Thickness of Baseplate per Moss :
= ( 3 * ( Q + Saddle_Wt ) * BasePlateWidth / ( 4 * BasePlateLength *
AllStress ))½
= ( 3 * (14208 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½
= 5.559 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress
Effective Baseplate Length [e]:
= ( Bplen - Clearance ) / ( Nribs - 1)
= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm
248
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015
Baseplate Pressure Area [Ap]:
= e * Bpwid / 2
= 184.6000 * 100.0000/2 = 9229.9990 mm²
Axial Load [P]:
= Ap * Bp
= 9230.0 * 0.68 = 6245.1 N
Area of the Rib and Web [Ar]:
= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk
= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000
= 1271.200 mm²
Compressive Stress [Sc]:
= P/Ar
= 6245.1/1271.2000 = 4.9132 MPa
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
Y A AY Ay² Io
Rib 50.0 634.4 31720.0 0.0 443558.7
Web 50.0 738.4 36920.0 0.0 7876.3
Values 50.0 1372.8 68640.0 0.0 451434.9
Bending Moment [Rm]:
= Fl /( 2 * Bplen ) * e * rl / 2
= 2589.1/( 2 * 210.00 ) * 184.600 * 290.61/2
= 165.422 N-m
KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1
249
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Ope.) : Step: 12 1:45p Jan 11,2015 Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/
( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)
Sca = 143.88 MPa
AISC Unity Check on Outside Ribs ( must be <= 1.0 )
Check = Sc/Sca + (Rm/Z)/Sba
Check = 4.91/143.88 + (165.42/9028.698 )/165.48
Check = 0.14
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
250
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015
ASME Horizontal Vessel Analysis: Stresses for the Left Saddle
(per ASME Sec. VIII Div. 2 based on the Zick method.)
Horizontal Vessel Stress Calculations : Test Case
Note: Wear Pad Width (120.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
Minimum Wear Plate Width to be considered in analysis [b1]:
= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )
= 142.9579 mm
Input and Calculated Values:
Vessel Mean Radius Rm 105.96 mm
Stiffened Vessel Length per 4.15.6 L 3175.00 mm
Distance from Saddle to Vessel tangent a 106.00 mm
Saddle Width b 100.00 mm
Saddle Bearing Angle theta 120.00 degrees
Inside Depth of Head h2 51.19 mm
Shell Allowable Stress used in Calculation 155.14 MPa
Head Allowable Stress used in Calculation 155.14 MPa
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Test Case, no Ext. Forces 2849.23 N
251
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015
Horizontal Vessel Analysis Results: Actual Allowable
-------------------------------------------------------------------
Long. Stress at Top of Midspan 10.65 155.14 MPa
Long. Stress at Bottom of Midspan 25.83 155.14 MPa
Long. Stress at Top of Saddles 18.70 155.14 MPa
Long. Stress at Bottom of Saddles 17.98 155.14 MPa
Tangential Shear in Shell 4.02 93.08 MPa
Circ. Stress at Horn of Saddle 5.11 232.71 MPa
Circ. Compressive Stress in Shell 0.21 155.14 MPa
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:
= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 217.0/2 + 0 ) * 300.0000/183.5269
= 532.0 N
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:
= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002
= 1.4 N
Load Combination Results for Q + Wind or Seismic [Q]:
= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
= 2317 + Max( 1 , 532 , 0 , 0 )
= 2849.2 N
Summary of Loads at the base of this Saddle:
Vertical Load (including saddle weight) 2960.00 N
252
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Transverse Shear Load Saddle 108.49 N
Longitudinal Shear Load Saddle 11.19 N
Hydrostatic Test Pressure at center of Vessel: 24.635 bar
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is Welded to the Shell, k = 0.1
The Computed K values from Table 4.15.1:
K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011
K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405
K9 = 0.2711 K10 = 0.0581 K1* = 0.1923
Note: Dimension a is greater than or equal to Rm / 2.
Moment per Equation 4.15.3 [M1]:
= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -2849*106.00[1-(1-106.00/3175.00+(105.959²-51.191²)/
(2*106.00*3175.00))/(1+(4*51.19)/(3*3175.00))]
= -12.5 N-m
Moment per Equation 4.15.4 [M2]:
= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
= 2849*3175/4(1+2(105²-51²)/(3175²))/(1+(4*51)/
(3*3175))-4*105/3175
= 1916.5 N-m
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:
= P * Rm/(2t) - M2/(pi*Rm²t)
= 24.635 * 105.959/(2*7.156 ) - 1916.5/(pi*106.0²*7.156 )
253
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 10.65 MPa
Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:
= P * Rm/(2t) + M2/(pi * Rm² * t)
= 24.635 * 105.959/(2 * 7.156 ) + 1916.5/(pi * 106.0² * 7.156 )
= 25.83 MPa
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:
= P * Rm/(2t) - M1/(K1*pi*Rm²t)
= 24.635*105.959/(2*7.156)--12.5/(0.1066*pi*106.0²*7.156)
= 18.70 MPa
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:
= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 24.635*105.959/(2*7.156)+-12.5/(0.1923*pi*106.0²*7.156)
= 17.98 MPa
Maximum Shear Force in the Saddle (4.15.5) [T]:
= Q(L-2a)/(L+(4*h2/3))
= 2849 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 51.19/3))
= 2603.0 N
Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:
= K2 * T / ( Rm * t )
= 1.1707 * 2603.02/( 105.9593 * 7.1565 )
= 4.02 MPa
Decay Length (4.15.22) [x1,x2]:
= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 105.959 * 7.156 )
= 21.479 mm
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:
= -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= -0.7603 * 2849 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )
= -0.21 MPa
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:
= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -2849/(4*7.156 *(100.000 +21.479 +21.479 )) -
3*0.0529 *2849/(2*7.156²)
= -5.11 MPa
Effective reinforcing plate width (4.15.1) [B1]:
= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )
= 142.96 mm
Results for Vessel Ribs, Web and Base:
Baseplate Length Bplen 210.0000 mm
Baseplate Thickness Bpthk 8.0000 mm
Baseplate Width Bpwid 100.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 2
Rib Thickness Ribtk 8.0000 mm
Web Thickness Webtk 8.0000 mm
Web Location Webloc Center
Moment of Inertia of Saddle - Lateral Direction
Y A AY Io
Shell 4. 1161. 4154. 19819.
Wearplate 12. 1200. 14588. 187335.
255
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web 126. 1743. 219723. 34594160.
BasePlate 239. 800. 191200. 45701020.
Totals 381. 4904. 429664. 80502336.
Value C1 = Sumof(Ay)/Sumof(A) = 88. mm
Value I = Sumof(Io) - C1*Sumof(Ay) = 42855068. mm**4
Value As = Sumof(A) - Ashell = 3743. mm²
K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035
Fh = K1 * Q = 0.2035 * 2849.231 = 579.8803 N
Tension Stress, St = ( Fh/As ) = 0.1549 MPa
Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa
d = B - R*Sin(theta) / theta = 260.7126 mm
Bending Moment, M = Fh * d = 151.2434 N-m
Bending Stress, Sb = ( M * C1 / I ) = 0.3091 MPa
Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa
Minimum Thickness of Baseplate per Moss :
= ( 3 * ( Q + Saddle_Wt ) * BasePlateWidth / ( 4 * BasePlateLength *
AllStress ))½
= ( 3 * (2849 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½
= 2.528 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress
Effective Baseplate Length [e]:
= ( Bplen - Clearance ) / ( Nribs - 1)
256
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm
Baseplate Pressure Area [Ap]:
= e * Bpwid / 2
= 184.6000 * 100.0000/2 = 9229.9990 mm²
Axial Load [P]:
= Ap * Bp
= 9230.0 * 0.14 = 1252.3 N
Area of the Rib and Web [Ar]:
= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk
= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000
= 1271.200 mm²
Compressive Stress [Sc]:
= P/Ar
= 1252.3/1271.2000 = 0.9852 MPa
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
Y A AY Ay² Io
Rib 50.0 634.4 31720.0 0.0 443558.7
Web 50.0 738.4 36920.0 0.0 7876.3
Values 50.0 1372.8 68640.0 0.0 451434.9
Bending Moment [Rm]:
= Fl /( 2 * Bplen ) * e * rl / 2
= 11.2/( 2 * 210.00 ) * 184.600 * 290.61/2
= 0.715 N-m
257
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1
Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/
( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)
Sca = 143.88 MPa
AISC Unity Check on Outside Ribs ( must be <= 1.0 )
Check = Sc/Sca + (Rm/Z)/Sba
Check = 0.99/143.88 + (0.72/9028.698 )/165.48
Check = 0.01
ASME Horizontal Vessel Analysis: Stresses for the Right Saddle
(per ASME Sec. VIII Div. 2 based on the Zick method.)
Note: Wear Pad Width (120.00) is less than 1.56*sqrt(rm*t)
and less than 2a. The wear plate will be ignored.
Minimum Wear Plate Width to be considered in analysis [b1]:
= min( b + 1.56*sqrt( Rm * t ), 2a )
= min( 100.000 + 1.56*sqrt( 105.9593 * 7.1565 ), 2 * 106.000 )
= 142.9579 mm
Input and Calculated Values:
Vessel Mean Radius Rm 105.96 mm
Stiffened Vessel Length per 4.15.6 L 3175.00 mm
Distance from Saddle to Vessel tangent a 106.00 mm
Saddle Width b 100.00 mm
Saddle Bearing Angle theta 120.00 degrees
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015
Shell Allowable Stress used in Calculation 155.14 MPa
Head Allowable Stress used in Calculation 155.14 MPa
Circumferential Efficiency in Plane of Saddle 1.00
Circumferential Efficiency at Mid-Span 1.00
Saddle Force Q, Test Case, no Ext. Forces 3101.89 N
Horizontal Vessel Analysis Results: Actual Allowable
-------------------------------------------------------------------
Long. Stress at Top of Midspan 9.77 155.14 MPa
Long. Stress at Bottom of Midspan 26.71 155.14 MPa
Long. Stress at Top of Saddles 18.44 155.14 MPa
Long. Stress at Bottom of Saddles 18.13 155.14 MPa
Tangential Shear in Shell 4.47 93.08 MPa
Circ. Stress at Horn of Saddle 5.56 232.71 MPa
Circ. Compressive Stress in Shell 0.23 155.14 MPa
Intermediate Results: Saddle Reaction Q due to Wind or Seismic
Saddle Reaction Force due to Wind Ft [Fwt]:
= Ftr * ( Ft/Num of Saddles + Z Force Load ) * B / E
= 3.00 * ( 217.0/2 + 0 ) * 300.0000/183.5269
= 532.0 N
Saddle Reaction Force due to Wind Fl or Friction [Fwl]:
= max( Fl, Friction Load, Sum of X Forces) * B / Ls
= max( 33.92 , 0.00 , 0 ) * 300.0000/2420.0002
= 1.4 N
259
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Load Combination Results for Q + Wind or Seismic [Q]:
= Saddle Load + Max( Fwl, Fwt, Fsl, Fst )
= 2569 + Max( 1 , 532 , 0 , 0 )
= 3101.9 N
Summary of Loads at the base of this Saddle:
Vertical Load (including saddle weight) 3212.67 N
Transverse Shear Load Saddle 108.49 N
Longitudinal Shear Load Saddle 11.19 N
Hydrostatic Test Pressure at center of Vessel: 24.635 bar
Formulas and Substitutions for Horizontal Vessel Analysis:
Note: Wear Plate is Welded to the Shell, k = 0.1
The Computed K values from Table 4.15.1:
K1 = 0.1066 K2 = 1.1707 K3 = 0.8799 K4 = 0.4011
K5 = 0.7603 K6 = 0.0529 K7 = 0.0529 K8 = 0.3405
K9 = 0.2711 K10 = 0.0581 K1* = 0.1923
Note: Dimension a is greater than or equal to Rm / 2.
Moment per Equation 4.15.3 [M1]:
= -Q*a [1 - (1- a/L + (R²-h2²)/(2a*L))/(1+(4h2)/3L)]
= -3101*106.00[1-(1-106.00/3175.00+(105.959²-0.000²)/
(2*106.00*3175.00))/(1+(4*0.00)/(3*3175.00))]
= -5.5 N-m
Moment per Equation 4.15.4 [M2]:
= Q*L/4(1+2(R²-h2²)/(L²))/(1+(4h2)/( 3L))-4a/L
260
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 3101*3175/4(1+2(105²-0²)/(3175²))/(1+(4*0)/
(3*3175))-4*105/3175
= 2139.7 N-m
Longitudinal Stress at Top of Shell (4.15.6) [Sigma1]:
= P * Rm/(2t) - M2/(pi*Rm²t)
= 24.635 * 105.959/(2*7.156 ) - 2139.7/(pi*106.0²*7.156 )
= 9.77 MPa
Longitudinal Stress at Bottom of Shell (4.15.7) [Sigma2]:
= P * Rm/(2t) + M2/(pi * Rm² * t)
= 24.635 * 105.959/(2 * 7.156 ) + 2139.7/(pi * 106.0² * 7.156 )
= 26.71 MPa
Longitudinal Stress at Top of Shell at Support (4.15.10) [Sigma*3]:
= P * Rm/(2t) - M1/(K1*pi*Rm²t)
= 24.635*105.959/(2*7.156)--5.5/(0.1066*pi*106.0²*7.156)
= 18.44 MPa
Longitudinal Stress at Bottom of Shell at Support (4.15.11) [Sigma*4]:
= P * Rm/(2t) + M1/(K1* * pi * Rm² * t)
= 24.635*105.959/(2*7.156)+-5.5/(0.1923*pi*106.0²*7.156)
= 18.13 MPa
Maximum Shear Force in the Saddle (4.15.5) [T]:
= Q(L-2a)/(L+(4*h2/3))
= 3101 ( 3175.00 - 2 * 106.00 )/(3175.00 + ( 4 * 0.00/3))
= 2894.8 N
Shear Stress in the shell no rings, not stiffened (4.15.14) [tau2]:
= K2 * T / ( Rm * t )
261
PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 = 1.1707 * 2894.78/( 105.9593 * 7.1565 )
= 4.47 MPa
Decay Length (4.15.22) [x1,x2]:
= 0.78 * sqrt( Rm * t )
= 0.78 * sqrt( 105.959 * 7.156 )
= 21.479 mm
Circumferential Stress in shell, no rings (4.15.23) [sigma6]:
= -K5 * Q * k / ( t * ( b + X1 + X2 ) )
= -0.7603 * 3101 * 0.1/( 7.156 * ( 100.00 + 21.48 + 21.48 ) )
= -0.23 MPa
Circ. Comp. Stress at Horn of Saddle, L>=8Rm (4.15.24) [sigma7]:
= -Q/(4*t*(b+X1+X2)) - 3*K7*Q/(2*t²)
= -3101/(4*7.156 *(100.000 +21.479 +21.479 )) -
3*0.0529 *3101/(2*7.156²)
= -5.56 MPa
Effective reinforcing plate width (4.15.1) [B1]:
= min( b + 1.56 * sqrt( Rm * t ), 2a )
= min( 100.00 + 1.56 * sqrt( 105.959 * 7.156 ), 2 * 106.000 )
= 142.96 mm
Results for Vessel Ribs, Web and Base
Baseplate Length Bplen 210.0000 mm
Baseplate Thickness Bpthk 8.0000 mm
Baseplate Width Bpwid 100.0000 mm
Number of Ribs ( inc. outside ribs ) Nribs 2
Rib Thickness Ribtk 8.0000 mm
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web Thickness Webtk 8.0000 mm
Web Location Webloc Center
Moment of Inertia of Saddle - Lateral Direction
Y A AY Io
Shell 4. 1161. 4154. 19819.
Wearplate 12. 1200. 14588. 187335.
Web 126. 1743. 219723. 34594160.
BasePlate 239. 800. 191200. 45701020.
Totals 381. 4904. 429664. 80502336.
Value C1 = Sumof(Ay)/Sumof(A) = 88. mm
Value I = Sumof(Io) - C1*Sumof(Ay) = 42855068. mm**4
Value As = Sumof(A) - Ashell = 3743. mm²
K1 = (1+Cos(beta)-.5*Sin(beta)² )/(pi-beta+Sin(beta)*Cos(beta)) = 0.2035
Fh = K1 * Q = 0.2035 * 3101.894 = 631.3029 N
Tension Stress, St = ( Fh/As ) = 0.1687 MPa
Allowed Stress, Sa = 0.6 * Yield Str = 148.9320 MPa
d = B - R*Sin(theta) / theta = 260.7126 mm
Bending Moment, M = Fh * d = 164.6553 N-m
Bending Stress, Sb = ( M * C1 / I ) = 0.3365 MPa
Allowed Stress, Sa = 2/3 * Yield Str = 165.4800 MPa
Minimum Thickness of Baseplate per Moss :
= ( 3 * ( Q + Saddle_Wt ) * BasePlateWidth / ( 4 * BasePlateLength *
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 AllStress ))½
= ( 3 * (3101 + 110 ) * 100.00/( 4 * 210.000 * 165.480 ))½
= 2.633 mm
Calculation of Axial Load, Intermediate Values and Compressive Stress
Effective Baseplate Length [e]:
= ( Bplen - Clearance ) / ( Nribs - 1)
= ( 210.0000 - 25.4 )/( 2 - 1 ) = 184.6000 mm
Baseplate Pressure Area [Ap]:
= e * Bpwid / 2
= 184.6000 * 100.0000/2 = 9229.9990 mm²
Axial Load [P]:
= Ap * Bp
= 9230.0 * 0.15 = 1363.4 N
Area of the Rib and Web [Ar]:
= ( Bpwid - Clearance - Webtk ) * Ribtk + e/2 * Webtk
= ( 100.000 - 25.4 - 8.000 ) * 8.000 + 184.6000/2 * 8.000
= 1271.200 mm²
Compressive Stress [Sc]:
= P/Ar
= 1363.4/1271.2000 = 1.0726 MPa
Check of Outside Ribs:
Inertia of Saddle, Outer Ribs - Longitudinal Direction
Y A AY Ay² Io
Rib 50.0 634.4 31720.0 0.0 443558.7
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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHD FileName : Transportation -------------------------------- Horizontal Vessel Analysis (Test) : Step: 13 1:45p Jan 11,2015 Web 50.0 738.4 36920.0 0.0 7876.3
Values 50.0 1372.8 68640.0 0.0 451434.9
Bending Moment [Rm]:
= Fl /( 2 * Bplen ) * e * rl / 2
= 11.2/( 2 * 210.00 ) * 184.600 * 290.61/2
= 0.715 N-m
KL/R < Cc ( 15.4214 < 126.0993 ) per AISC E2-1
Sca = (1-(Klr)²/(2*Cc²))*Fy/(5/3+3*(Klr)/(8*Cc)-(Klr³)/(8*Cc³)
Sca = ( 1-( 15.42 )²/(2 * 126.10² )) * 248/
( 5/3+3*(15.42 )/(8* 126.10 )-( 15.42³)/(8*126.10³)
Sca = 143.88 MPa
AISC Unity Check on Outside Ribs ( must be <= 1.0 )
Check = Sc/Sca + (Rm/Z)/Sba
Check = 1.07/143.88 + (0.72/9028.698 )/165.48
Check = 0.01
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Attachment 3
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Input Echo, Leg & Lug Item 1, Description: Trunnion
Design Internal Pressure 0.00 barDesign Temperature for Attachment TEMP 40.00 CVessel Outside Diameter OD 114.300 mm.Vessel Wall Thickness Ts 8.1800 mm.Vessel Corrosion Allowance Cas 0.0000 mm.Vessel Material SA-312 TP316LVessel Material UNS Number S31603Vessel Allowable Stress at Design S 115.23 MPaAnalysis Type: Trunnion
Empty Weight of Vessel Wemp 3826.00 N .Operating Weight of Vessel (vertical load ) W 0.00 N .
Trunnion Material SA-312 TP316LTrunnion Material UNS Number S31603Trunnion Yield Stress SY 171.23 MPaTrunnion Outside Diameter TOD 88.900 mm.Trunnion Length TL 130.0000 mm.Bail/Sling Width TT 15.0000 mm.Pad Outside Diameter POD 139.000 mm.Pad Thickness PTHK 8.0000 mm.Ring Outside Diameter Rod 140.00 mm.Ring Thickness Rthk 8.00 mm.Trunnion Type SolidLift Orientation SolidImpact Factor Impfac 2.00
Force Along Vessel Axis Fax 3826.00 N .Force Normal to Vessel Fn 2209.00 N .Force Tangential to Vessel Ft 383.00 N .Perform WRC-107 Analysis on the Trunnion No
Occasional Load Factor (AISC A5.2) Occfac 1.00
Results for Trunnions, Description : Trunnion
Trunnion Lifting Load [Tlf]:= ((Fa^2 + Ft^2)^1/2)= ((3826.00 ^2 + 383.00 ^2)^1/2) * 2.00= 7690.24 N .
Z = pi * (TOD^4 - TID^4) / (32.0 * TOD)= 3.14 * ( 88.90 ^4 - 88.90 ^4) / (32.0 * 88.90 )= 68977.13 mm.^3
Trunnion Bending Moment [Tmom]:= (TL - 0.5 * TT)/1.001* Tlf= ( 130.00 - 0.5 * 15.00 )/1.001 * 7690.24= 942.44 N-m .
Trunnion Calculated Bending Stress [SBC]:= TMOM * 1.001/ Z= 942.44 *1.001/ 68977.13= 13.67 MPa [Passed] SBC < Min(0.66* SY* Occfac, .75* SY) (113.01)
Trunnion Cross Section Area [Txsa]:= pi / 4 * (TOD^2- TID^2)= 3.14 /4 * ( 88.90^2- 88.90^2)= 6207.17 mm^2
Trunnion Calculated Shear Stress [SSC]:= Tlf / Txsa= 7690.24 / 6207.17= 1.24 MPa [Passed] SSC < 0.4 * SY * Occfac (68.49)
Trunnion Unity Check [UCHK]:= SBC / SBA + SSC / SSA= 13.67 / 113.01 + 1.24 / 68.49= 0.14 [Passed] UCHK, Must be less than 1.
Trunnion Bearing Contact Area [Tbca]:= TOD * TT= 88.90 * 15.00= 1333.50 mm^2
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Trunnion Bearing Stress [SBEC]:= Tlf / Tbca= 7690.24 / 1333.50= 5.77 MPa [Passed] SBEC < Min(0.75* SY* Occfac, 0.9* SY) (128.42)
SUMMARY OF RESULTS:
Trunnion unity check value: 0.1390
Actual Allowable Pass/FailBending Stress (MPa ) 13.67 113.01 PassShear Stress (MPa ) 1.24 68.49 PassBearing Stress (MPa ) 5.77 128.42 Pass
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