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Design Internal Pressure (for test) 0.5000 bars Design Internal Temperature 100 °C Test Position Vertical Projection of Nozzle from Vessel Top 200.00 mm. Projection of Nozzle from Vessel Bottom 200.00 mm. Minimum Design Metal Temperature -29 °C Miscellaneous Weight Percent 0.0 Use Higher Longitudinal Stresses (Flag) Y Select t for Internal Pressure (Flag) Y Select t for External Pressure (Flag) Y Select t for Axial Stress (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 bars User defined MAWP 0.0000 bars User defined MAPnc 0.0000 bars
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 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 No Wind Loads
Seismic Design Code No Seismic
Design Nozzle for Des. Press. + St. Head 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
Element To Node 20 Element Type Torisphe. Description Bottom head Distance "FROM" to "TO" 50.000 mm. Inside Diameter 2450.0 mm. Element Thickness 6.0000 mm. Internal Corrosion Allowance 0.0000 mm. Nominal Thickness 8.0000 mm. External Corrosion Allowance 0.0000 mm. Design Internal Pressure 0.5000 bars Design Temperature Internal Pressure 100 °C Design External Pressure 0.3000 bars Design Temperature External Pressure 100 °C Effective Diameter Multiplier 1.2 Material Name X5CrNi18-10, EN10028-7:2007 Allowable Stress, Ambient 180.01 N./mm^2 Allowable Stress, Operating 150.01 N./mm^2 Material Density 0.007840 kg./cm^3 Efficiency, Longitudinal Seam 0.7 Efficiency, Circumferential Seam 0.7 Tori Head Crown Radius 2450.0 mm. Tori Head Knuckle Radius 245.00 mm.
Element From Node 10 Detail Type Liquid Detail ID LIQ Dist. from "FROM" Node / Offset dist -474.21 mm. Height/Length of Liquid 524.21 mm. Liquid Density 0.0009996 kg./cm^3
Element From Node 10 Detail Type Nozzle Detail ID N2 Dist. from "FROM" Node / Offset dist 0.0000 mm. Nozzle Diameter 4.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8695 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 20 Element To Node 30 Element Type Cylinder Description Shell Distance "FROM" to "TO" 2350.0 mm. Inside Diameter 2450.0 mm. Element Thickness 6.0000 mm. Internal Corrosion Allowance 0.0000 mm. Nominal Thickness 6.0000 mm. External Corrosion Allowance 0.0000 mm. Design Internal Pressure 0.5000 bars
Design Temperature Internal Pressure 100 °C Design External Pressure 0.3000 bars Design Temperature External Pressure 100 °C Effective Diameter Multiplier 1.2 Material Name X5CrNi18-10, EN10028-7:2007 Efficiency, Longitudinal Seam 0.7 Efficiency, Circumferential Seam 0.7
Element From Node 20 Detail Type Liquid Detail ID LIQ Dist. from "FROM" Node / Offset dist 0.0000 mm. Height/Length of Liquid 2350.0 mm. Liquid Density 0.0009996 kg./cm^3
Element From Node 20 Detail Type Nozzle Detail ID N9 Dist. from "FROM" Node / Offset dist 280.00 mm. Nozzle Diameter 2.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8547 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 20 Detail Type Lug Detail ID SUPPORT LUG Dist. from "FROM" Node / Offset dist 1500.0 mm. Number of Lugs 4 Dist. from OD to Lug Cntrline(dlug) 350.00 mm. Height of Gusset Plates (hgp) 450.00 mm. Force Bearing Width (wfb) 200.00 mm. Weight of Lug 13.608 Kgf Lug Start Angle (degrees) 0.0
Element From Node 30 Element To Node 40 Element Type Torisphe. Description Top head Distance "FROM" to "TO" 50.000 mm. Inside Diameter 2450.0 mm. Element Thickness 6.0000 mm. Internal Corrosion Allowance 0.0000 mm. Nominal Thickness 8.0000 mm. External Corrosion Allowance 0.0000 mm. Design Internal Pressure 0.5000 bars Design Temperature Internal Pressure 100 °C Design External Pressure 0.3000 bars Design Temperature External Pressure 100 °C Effective Diameter Multiplier 1.2
Material Name X5CrNi18-10, EN10028-7:2007 Efficiency, Longitudinal Seam 0.7 Efficiency, Circumferential Seam 0.7 Tori Head Crown Radius 2450.0 mm. Tori Head Knuckle Radius 245.00 mm.
Element From Node 30 Detail Type Liquid Detail ID LIQ Dist. from "FROM" Node / Offset dist 0.0000 mm. Height/Length of Liquid 524.21 mm. Liquid Density 0.0009996 kg./cm^3
Element From Node 30 Detail Type Nozzle Detail ID M Dist. from "FROM" Node / Offset dist 800.00 mm. Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 10 Layout Angle 0.0 Blind Flange (Y/N) Y Weight of Nozzle ( Used if > 0 ) 177.93 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N1 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 3.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 40.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 30.303 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N3 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 2.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 60.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 50.516 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N4 Dist. from "FROM" Node / Offset dist 850.00 mm.
Nozzle Diameter 6.0 in. Nozzle Schedule 80S Nozzle Class 10 Layout Angle 90.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8695 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N5 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 2.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 120.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 37.526 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N6 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 1.0 in. Nozzle Schedule 80S Nozzle Class 10 Layout Angle 140.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8547 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N7 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 2.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 160.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 14.424 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N8 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 1.0 in. Nozzle Schedule 80S Nozzle Class 10 Layout Angle 180.0
Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 1.7228 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N10 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 1.0 in. Nozzle Schedule 80S Nozzle Class 10 Layout Angle 200.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 1.7228 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N11 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 3.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 220.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8695 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N12 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 1.0 in. Nozzle Schedule 80S Nozzle Class 10 Layout Angle 240.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 8.1104 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N13 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 2.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 260.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8695 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Nozzle Detail ID N14 Dist. from "FROM" Node / Offset dist 850.00 mm. Nozzle Diameter 3.0 in. Nozzle Schedule 40S Nozzle Class 10 Layout Angle 280.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3.8547 Kgf Grade of Attached Flange 6E0 Nozzle Matl X5CrNi18-10
Element From Node 30 Detail Type Weight Detail ID AGITATOR Dist. from "FROM" Node / Offset dist 0.0000 mm. Miscellaneous Weight 200.00 Kgf Offset from Element Centerline 0.0000 mm.
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European Std: EN 13445-3: 2009(E) Issue 1 (2009-07)
Torispherical Head From 10 To 20 X5CrNi18-10 at 100 °C
Bottom head
Design Stress at Ambient Temperature = 180.006 N./mm^2
Required thickness = 3.071 mm. Required thickness in the crown = 0.972 mm.
This is not a Korbbogen, Kloepper or Elliptical HeadTreated as a Torispherical Head (Korbbogen if nozzle is outside 80%)
The Material is Austenitic Steel which affects value of fb:
Buckling Strs at ope. fb = Yield/1.5 = 157.029/1.5 = 104.686 N./mm^2 Buckling Strs at amb. fb = Yield/1.5 = 260.009/1.5 = 173.339 N./mm^2Although head is Austenititic Steel, Rp0,20% is used
Geometry factors per EN13445 7.5.3.5: - Design Condition:
Pressure including hydro head P : 0.8331 bars Inside Head Diameter (new) Di : 2450.0000 mm. Head Crown Radius (new) R : 2450.0000 mm. Head Knuckle Radius (new) r : 245.0000 mm. Head Thickness (new) e : 6.0000 mm.
Head Corrosion Allowance Internal ci : 0.0000 mm. Head Corrosion Allowance External co : 0.0000 mm. Joint Efficiency Z : 0.7000
Inside Corroded Head Depth [h]: = L - Sqrt( ( L - Di / 2) * ( L + Di / 2 - 2 * r ) ) = 2450.00 -Sqrt((2450.00 -2450.00/2)*(2450.00 +2450.00/2-2*245.00 )) = 474.747 mm.
Y = Min(e/R, 0.04) = Min(3.07068/2450.0000, 0.04) = 0.0012533 Z = Log10(1 / Y) = Log10(1 / 0.001) = 2.9019 X = r / Di = 245.0000 / 2450.0000 = 0.10000 N = 1.006 - 1 / ( 6.2+( 90 * Y )^4) ) = 1.006-1 / (6.2+( 90*0.0013)^4) = 0.84471
The hydrotest pressure is controlled by the buckling stress fb and cannotbe a higher pressure. That is why MAPNC is the same as hydrotest pressure
Elongation of the extreme fiber: For a spun head per EN 13445-4 Para 9.2.1 [F]: Assuming the blank is 20% larger than the head diameter = 100 * ln( 2959.200/( 2450.000 - 2 * 8.000 ) ) = 18.883 %
For a segmented head per EN 13445-4 Para 9.2.5 [F]: = 100 * e/R = 100 * 0.315/48.386 = 0.651 %
If F exceeds 5% PWHT may be required. Please referto EN 13445 Part 4 Table 9.4.1
Required Thickness of Straight Flange = 0.972 mm.
Cylindrical Shell From 20 To 30 X5CrNi18-10 at 100 °C
Shell
Design Stress at Ambient Temperature = 180.006 N./mm^2
Thickness due to internal pressure [e]: = P * Di / ( 2 * f * z - P ) EN13445 Equation: 7.4.2: = 0.78 * 2450.00/( 2 * 150.008 * 0.700 - 0.078 ) + c + cext = 0.9124 + 0.0000 + 0.0000 = 0.9124 mm.
The shell is suitable for the design pressure.
Maximum Working Pressure Hot and Corroded [MAWP]: = ( 2 * f * ecor * z ) / (Di + ecor) - Phead = ( 2 * 150.01 * 6.0000 * 0.700 )/(2450.00 + 6.0000 )-0.28 = 0.485 N./mm^2
Maximum Pressure New and Cold [MAPNC]: = ( 2 * fa * e * z ) / ( D + e ) = ( 2 * 180.01 * 6.00 * 0.700 )/( 2450.00 + 6.00 ) = 0.616 N./mm^2
Torispherical Head From 30 To 40 X5CrNi18-10 at 100 °C
Top head
Design Stress at Ambient Temperature = 180.006 N./mm^2
Required thickness = 2.720 mm. Required thickness in the crown = 0.638 mm.
Note: This head has a nozzle located outside the 80% diameter limit! This modifies the value of Beta (Beta_k) per paragraph 7.7.3.
This is not a Korbbogen, Kloepper or Elliptical HeadTreated as a Torispherical Head (Korbbogen if nozzle is outside 80%)
The Material is Austenitic Steel which affects value of fb:
Buckling Strs at ope. fb = Yield/1.5 = 157.029/1.5 = 104.686 N./mm^2 Buckling Strs at amb. fb = Yield/1.5 = 260.009/1.5 = 173.339 N./mm^2Although head is Austenititic Steel, Rp0,20% is used
Geometry factors per EN13445 7.5.3.5: - Design Condition:
Pressure including hydro head P : 0.5465 bars Inside Head Diameter (new) Di : 2450.0000 mm. Head Crown Radius (new) R : 2450.0000 mm. Head Knuckle Radius (new) r : 245.0000 mm. Head Thickness (new) e : 6.0000 mm. Head Corrosion Allowance Internal ci : 0.0000 mm. Head Corrosion Allowance External co : 0.0000 mm. Joint Efficiency Z : 0.7000
The nozzle is outside the 80% limit: Nozzle corroded inside Diameter di : 609.6000 mm.
Inside Corroded Head Depth [h]: = L - Sqrt( ( L - Di / 2) * ( L + Di / 2 - 2 * r ) ) = 2450.00 -Sqrt((2450.00 -2450.00/2)*(2450.00 +2450.00/2-2*245.00 )) = 474.747 mm.
Y = Min(e/R, 0.04) = Min(2.72027/2450.0000, 0.04) = 0.0011103 Z = Log10(1 / Y) = Log10(1 / 0.001) = 2.9546 X = r / Di = 245.0000 / 2450.0000 = 0.10000 N = 1.006 - 1 / ( 6.2+( 90 * Y )^4) ) = 1.006-1 / (6.2+( 90*0.0011)^4) = 0.84471
Assuming the blank is 20% larger than the head diameter = 100 * ln( 2959.200/( 2450.000 - 2 * 8.000 ) ) = 18.883 %
For a segmented head per EN 13445-4 Para 9.2.5 [F]: = 100 * e/R = 100 * 0.315/48.386 = 0.651 %
If F exceeds 5% PWHT may be required. Please referto EN 13445 Part 4 Table 9.4.1
Required Thickness of Straight Flange = 0.638 mm.
Hydrostatic Test Pressure Results:
Note: The Hydrotest Pressure Derivation is an Iterative Process
Limited by: Torisph. Head Bottom headHydrotest pressure is based upon stress (ftest) in the weakest element:
Note: 1.5 / 1.05 = 1.429, The PED requirement is 1.43
Test allowable per Table 6-1 [ftest]: = 270.039 N./mm^2
Test Pressure = Calc Test Press - Liquid Head = 2.277 - 0.333 = 1.943 bars
Stresses on Elements due to Test Pressure:
From To Stress Allowable Ratio ---------------------------------------------------------------------- Bottom head 66.6 270.0 0.247 Shell 65.1 270.0 0.241 Top head 58.3 270.0 0.216 ----------------------------------------------------------------------
Elements Suitable for Internal Pressure.
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| | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia | From| To | Bet. Stiff.| Bet. Stiff.| Required | Available | | | mm. | mm. | cm**4 | cm**4 | ------------------------------------------------------------------- 10| 20| No Calc | No Calc | No Calc | No Calc | 20| 30| 2829.80 | 4120.69 | No Calc | No Calc | 30| 40| No Calc | No Calc | No Calc | No Calc |
Elements Suitable for External Pressure.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Element and Detail Weights : Step: 5 5:35p Aug 24,2014
Element and Detail Weights
| | Element | Element | Corroded | Corroded | Extra due | From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % | | | kg. | Cm3 | kg. | Cm3 | kg. | --------------------------------------------------------------------------- 10| 20| 400.162 | 1.691E+06 | 400.162 | 1.691E+06 | 40.0162 | 20| 30| 852.949 | 11.08E+06 | 852.949 | 11.08E+06 | 85.2949 | 30| 40| 400.162 | 1.691E+06 | 400.162 | 1.691E+06 | 40.0162 | --------------------------------------------------------------------------- Total 1653 14463567.00 1653 14463567.00 165
Total Weight of Liquid 14452.2 Total Weight of Nozzles 384.2 Total Weight of Lugs 59.9 Total Weight of Weights 200.0 --------------------------------------------------------------- Sum of the Detail Weights 15096.3 kg.
Note that the above value for the miscellaneous weight percent hasbeen applied to the shells/heads/flange/tubesheets/tubes etc. in theweight 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 2262.7 kg. Shop Test Wt. - Fabricated Weight + Water ( Full ) 16717.4 kg. Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 2262.7 kg. Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 2462.7 kg. Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 2462.7 kg. Operating Wt. - Empty Wt + Operating Liq. Uncorroded 16914.9 kg. Field Test Wt. - Empty Weight + Water (Full) 16717.4 kg. Mass of the Upper 1/3 of the Vertical Vessel 6625.2 kg.
Outside Surface Areas of Elements
| | Surface | From| To | Area | | | cm^2 | ---------------------------- 10| 20| 63069.9 | 20| 30| 181763. | 30| 40| 63069.9 | ----------------------------- Total 307902.969 cm^2
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 | | | kg. | kg. | kg. | Kg-m. | kg. | --------------------------------------------------------------------------- 10| 20| 444.434 | 2132.31 | 2134.83 | ... | 444.434 | 20|Lugs| 601.586 | 7670.07 | 7670.06 | 3.38658 | 601.586 | Lugs| 30| 340.899 | 4346.37 | 4346.37 | 1.91906 | 340.899 | 30| 40| 1015.91 | 2706.31 | 2506.31 | 116.609 | 1015.91 |
Cumulative Vessel Weight
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Element and Detail Weights : Step: 5 5:35p Aug 24,2014
Note: The cumulative operating weights no liquid in the column above are the cumulative operating weights minus the operating liquid weight minus any weights absent in the empty condition.
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25
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Natural Frequency Calculation : Step: 7 5:35p Aug 24,2014
The Natural Frequencies for the vessel have been computed iterativelyby solving a system of matrices. These matrices describe the massand 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 184.735 Hz.
The Natural Frequency for the Vessel (Ope...) is 64.2468 Hz.
The Natural Frequency for the Vessel (Filled) is 64.9981 Hz.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
29
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Longitudinal Stresses Due to . . . Step: 11 5:35p Aug 24,2014
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.
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31
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Stress due to Combined Loads : Step: 12 5:35p Aug 24,2014
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.
Case types WE, WF, and CW are in the Un-Corroded condition.
A blank stress and stress ratio indicates that the correspondingstress comprising those components that did not contribute to thattype of stress.
For PD:5500 and EN-13445, computed stress intensities are comparedto the design stress f and the compressive stress is compared to theallowable compressive as Rat 4.
An asterisk (*) in the final column denotes overstress.
Analysis of Load Case 1 : NP+EW+WI+FW+BW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.093 0.095 0.000 0.001 0.001 0.000 0.000 20 0.328 0.328 0.000 0.002 0.002 0.000 0.005
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Stress due to Combined Loads : Step: 12 5:35p Aug 24,2014
30 0.256 0.256 0.000 0.001 0.001 0.000 0.004
Analysis of Load Case 2 : NP+EW+EE+FS+BS From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.093 0.095 0.000 0.001 0.001 0.000 0.000 20 0.328 0.328 0.000 0.002 0.002 0.000 0.005 30 0.256 0.256 0.000 0.001 0.001 0.000 0.004
Analysis of Load Case 3 : NP+OW+WI+FW+BW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.451 0.453 0.000 0.003 0.003 0.000 0.000 20 1.535 1.535 0.000 0.009 0.009 0.000 0.025 30 0.256 0.256 0.000 0.001 0.001 0.000 0.004
Analysis of Load Case 4 : NP+OW+EQ+FS+BS From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.451 0.453 0.000 0.003 0.003 0.000 0.000 20 1.535 1.535 0.000 0.009 0.009 0.000 0.025 30 0.256 0.256 0.000 0.001 0.001 0.000 0.004
Analysis of Load Case 5 : NP+HW+HI From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.451 0.453 0.000 0.002 0.002 0.000 0.000 20 0.328 0.328 0.000 0.001 0.001 0.000 0.004 30 0.256 0.256 0.000 0.001 0.001 0.000 0.003
Analysis of Load Case 6 : NP+HW+HE From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.451 0.453 0.000 0.002 0.002 0.000 0.000 20 0.328 0.328 0.000 0.001 0.001 0.000 0.004 30 0.256 0.256 0.000 0.001 0.001 0.000 0.003
Analysis of Load Case 7 : IP+OW+WI+FW+BW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.315 5.584 22.897 0.096 0.031 0.153 0.000 20 19.301 3.667 22.885 0.107 0.020 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Stress due to Combined Loads : Step: 12 5:35p Aug 24,2014
Analysis of Load Case 8 : IP+OW+EQ+FS+BS From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.315 5.584 22.897 0.096 0.031 0.153 0.000 20 19.301 3.667 22.885 0.107 0.020 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
Analysis of Load Case 9 : EP+OW+WI+FW+BW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities [Uchk A-2] ----------- Stress Ratios ----------------------------------------------------------------------- 10 3.085 3.085 0.000 0.017 0.017 0.000 0.050 20 2.635 2.635 0.000 0.70 0.015 0.015 0.000 0.042 20 4.620 4.620 0.000 0.71 0.026 0.026 0.000 0.074 30 3.341 3.341 0.000 0.019 0.019 0.000 0.054
Analysis of Load Case 10 : EP+OW+EQ+FS+BS From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities [Uchk A-2] ----------- Stress Ratios ----------------------------------------------------------------------- 10 3.085 3.085 0.000 0.017 0.017 0.000 0.050 20 2.635 2.635 0.000 0.70 0.015 0.015 0.000 0.042 20 4.620 4.620 0.000 0.71 0.026 0.026 0.000 0.074 30 3.341 3.341 0.000 0.019 0.019 0.000 0.054
Analysis of Load Case 11 : HP+HW+HI From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.792 19.792 0.000 0.070 0.070 0.000 0.000 20 20.243 20.245 0.000 0.072 0.072 0.000 0.000 20 19.464 19.546 0.000 0.069 0.070 0.000 0.000 30 19.536 19.617 0.000 0.070 0.070 0.000 0.000
Analysis of Load Case 12 : HP+HW+HE From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.792 19.792 0.000 0.070 0.070 0.000 0.000 20 20.243 20.245 0.000 0.072 0.072 0.000 0.000 20 19.464 19.546 0.000 0.069 0.070 0.000 0.000 30 19.536 19.617 0.000 0.070 0.070 0.000 0.000
Analysis of Load Case 13 : IP+WE+EW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.673 5.226 22.897 0.098 0.029 0.153 0.000 20 18.094 4.873 22.885 0.101 0.027 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
Analysis of Load Case 14 : IP+WF+CW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Stress due to Combined Loads : Step: 12 5:35p Aug 24,2014
Analysis of Load Case 15 : IP+VO+OW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.315 5.584 22.897 0.096 0.031 0.153 0.000 20 19.301 3.667 22.885 0.107 0.020 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
Analysis of Load Case 16 : IP+VE+EW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.673 5.226 22.897 0.098 0.029 0.153 0.000 20 18.094 4.873 22.885 0.101 0.027 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
Analysis of Load Case 17 : NP+VO+OW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 0.000 0.000 0.000 0.000 0.000 0.000 0.000 20 0.451 0.453 0.000 0.003 0.003 0.000 0.000 20 1.535 1.535 0.000 0.009 0.009 0.000 0.025 30 0.256 0.256 0.000 0.001 0.001 0.000 0.004
Analysis of Load Case 18 : FS+BS+IP+OW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities ------------------- Stress Ratios ----------------------------------------------------------------------- 10 19.268 5.134 24.402 0.107 0.029 0.163 0.000 20 17.315 5.584 22.897 0.096 0.031 0.153 0.000 20 19.301 3.667 22.885 0.107 0.020 0.153 0.000 30 11.143 4.917 15.979 0.062 0.027 0.107 0.000
Analysis of Load Case 19 : FS+BS+EP+OW From f1-f2 f2+0.5p Hoop+.5p Rat 1 Rat 2 Rat 3 Rat 4 Node --------- Stress Intensities [Uchk A-2] ----------- Stress Ratios ----------------------------------------------------------------------- 10 3.085 3.085 0.000 0.017 0.017 0.000 0.050 20 2.635 2.635 0.000 0.70 0.015 0.015 0.000 0.042 20 4.620 4.620 0.000 0.71 0.026 0.026 0.000 0.074 30 3.341 3.341 0.000 0.019 0.019 0.000 0.054
Absolute Maximum of the all of the Stress Ratio's 0.7138
Governing Element: ShellGoverning Load Case 9 : EP+OW+WI+FW+BW
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Stress due to Combined Loads : Step: 12 5:35p Aug 24,2014
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
36
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Center of Gravity Calculation : Step: 13 5:35p Aug 24,2014
Shop/Field Installation Options :
Note : The CG is computed from the first Element From Node
Center of Gravity of Liquid 1225.255 mm. Center of Gravity of Nozzles 3123.184 mm. Center of Gravity of Lugs 1775.000 mm. Center of Gravity of Added Weights (Operating) 2400.000 mm. Center of Gravity of Added Weights (Empty) 2400.000 mm.
Center of Gravity of Bare Shell New and Cold 1225.000 mm. Center of Gravity of Bare Shell Corroded 1225.000 mm.
Vessel CG in the Operating Condition 1284.176 mm. Vessel CG in the Fabricated (Shop/Empty) Condition 1629.951 mm. Vessel CG in the Test Condition 1521.537 mm.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
Type of Geometry : Gussets with Top Plate Number of Support Lugs Nlug 4 Distance from Vessel OD to Lug Contact Point Dlug 350.0000 mm. Lug Support Force Bearing Width Wfb 200.0000 mm. Lug Material P235GH, EN 10028-2:1992 Lug Yield Stress 190.01 N./mm^2 Radial Width of bottom Support Lug Plate Wpl 500.0000 mm. Effective Force Bearing Length Lpl 400.0000 mm. Thickness of bottom Support Lug Plate Tpl 20.0000 mm. Distance between Gussets Dgp 350.0000 mm. Mean Width of Gusset Plate Wgp 225.0000 mm. Height of Gusset Plate Hgp 450.0000 mm. Thickness of Gusset Plate Tgp 14.0000 mm. Radial Width of Top Bar Plate Wtp 100.0000 mm. Thickness of Top Plate Ttp 20.0000 mm.
Pad Width along Circumference C11P 550.000 mm. Pad Length along Vessel Axis C22P 600.000 mm. Pad Thickness Tpad 6.000 mm.
Bolt Material 42CrMo5-6, EN 10269:1999 Bolt Allowable Stress at Design Temperature 215.01 N./mm^2 Thread Series UNC Bolt Diameter 25.40 mm.
Results for Support Lugs: Description: SUPPORT LUG
Overturning Moment at Support Lug 0. Kg-m. Weight Load at the top of one Lug 4214. Kgf
Force on one Lug, Operating Condition [Flug]: = ( W/Nlug + Mlug/( Rlug * Nlug/2 ) ) = ( 16855/4 + 0/( 1581.00 * 4/2 )) = 4213.76 Kgf
Top Bar Plate Stress per Bednar p.154 [Stpl]: = 0.75*( Flug*Dlug*Lpl )/( Ttp*Wtp²*Hgp ) = 0.75*( 4213 *350.000 *400.000 )/( 20.0000 *100.000²*450.000 ) = 48.21 N./mm^2
Bottom Plate Required Thickness (Uniform Load) 14.0777 mm.
Bottom Plate Required Thickness based on ADM S 3/4 [trAD]: = 0.71 * Dgp * (( Flug / ( Lpl * Wfb ))/Spa )½ = 0.71*350.00*((4213/(400.00*200.00))/126.673)½ = 15.869 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.
Note :There was no uplift. Please choose an appropriate boltsize for this support design.
Input Echo, WRC107/537 Item 1, Description: SUPPORT LUG
Diameter Basis for Vessel Vbasis ID Cylindrical or Spherical Vessel Cylsph Cylindrical Internal Corrosion Allowance Cas 0.0000 mm. Vessel Diameter Dv 2450.000 mm. Vessel Thickness Tv 6.000 mm.
Parameter C11 C11 350.00 mm. Parameter C22 C22 450.00 mm.
Thickness of Reinforcing Pad Tpad 6.000 mm. Pad Parameter C11P C11p 550.000 mm. Pad Parameter C22P C22p 600.000 mm.
Design Internal Pressure Dp 0.500 bars Include Pressure Thrust No
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 Kgf Global Force (SUS) Fy 4213.8 Kgf Global Force (SUS) Fz 0.0 Kgf Global Moment (SUS) Mx 0.0 Kg-m. Global Moment (SUS) My 0.0 Kg-m. Global Moment (SUS) Mz 1474.8 Kg-m.
Internal Pressure (SUS) P 0.50 bars Include Pressure Thrust No
Use Interactive Control No WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads: Radial Load P 0.0 Kgf Circumferential Shear VC 0.0 Kgf Longitudinal Shear VL 4213.8 Kgf Circumferential Moment MC 0.0 Kg-m. Longitudinal Moment ML -1474.8 Kg-m. Torsional Moment MT 0.0 Kg-m.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
44
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Sup. Lug Calcs: Test : Step: 15 5:35p Aug 24,2014
Support Lug Calculations: Test Case
INPUT ECHO OF SUPPORT LUG INPUT
Type of Geometry : Gussets with Top Plate Number of Support Lugs Nlug 4 Distance from Vessel OD to Lug Contact Point Dlug 350.0000 mm. Lug Support Force Bearing Width Wfb 200.0000 mm. Lug Material P235GH, EN 10028-2:1992 Lug Yield Stress 225.01 N./mm^2 Radial Width of bottom Support Lug Plate Wpl 500.0000 mm. Effective Force Bearing Length Lpl 400.0000 mm. Thickness of bottom Support Lug Plate Tpl 20.0000 mm. Distance between Gussets Dgp 350.0000 mm. Mean Width of Gusset Plate Wgp 225.0000 mm. Height of Gusset Plate Hgp 450.0000 mm. Thickness of Gusset Plate Tgp 14.0000 mm. Radial Width of Top Bar Plate Wtp 100.0000 mm. Thickness of Top Plate Ttp 20.0000 mm.
Pad Width along Circumference C11P 550.000 mm. Pad Length along Vessel Axis C22P 600.000 mm. Pad Thickness Tpad 6.000 mm.
Bolt Material 42CrMo5-6, EN 10269:1999 Bolt Allowable Stress at Design Temperature 215.01 N./mm^2 Thread Series UNC Bolt Diameter 25.40 mm.
Results for Support Lugs: Description: SUPPORT LUG
Overturning Moment at Support Lug 0. Kg-m. Weight Load at the top of one Lug 4164. Kgf
Force on one Lug, Test Condition [Flug]: = ( W/Nlug + Mlug/( Rlug * Nlug/2 ) ) = ( 16657/4 + 0/( 1581.00 * 4/2 )) = 4164.39 Kgf
Top Bar Plate Stress per Bednar p.154 [Stpl]: = 0.75*( Flug*Dlug*Lpl )/( Ttp*Wtp²*Hgp ) = 0.75*( 4164 *350.000 *400.000 )/( 20.0000 *100.000²*450.000 ) = 47.65 N./mm^2
Bending Stress in bottom Plate (Unif. Load) Per Bednar p.156 [Spl2]: = Beta1 * Flug/Ba * Wfb² / Tpl² per Roark & Young 5th Ed. = 1.215 * 4164.4/800.000 * 200.000²/20.000²
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Sup. Lug Calcs: Test : Step: 15 5:35p Aug 24,2014
= 62.03 N./mm^2
Bottom Plate Required Thickness (Uniform Load) 12.8606 mm.
Bottom Plate Required Thickness based on ADM S 3/4 [trAD]: = 0.71 * Dgp * (( Flug / ( Lpl * Wfb ))/Spa )½ = 0.71*350.00*((4164/(400.00*200.00))/150.005)½ = 14.497 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.
Note :There was no uplift. Please choose an appropriate boltsize for this support design.
Input Echo, WRC107/537 Item 1, Description: SUPPORT LUG
Diameter Basis for Vessel Vbasis ID Cylindrical or Spherical Vessel Cylsph Cylindrical Internal Corrosion Allowance Cas 0.0000 mm. Vessel Diameter Dv 2450.000 mm. Vessel Thickness Tv 6.000 mm.
Design Temperature 21.11 °C
Attachment Type Type Rectangular
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Sup. Lug Calcs: Test : Step: 15 5:35p Aug 24,2014
Parameter C11 C11 350.00 mm. Parameter C22 C22 450.00 mm.
Thickness of Reinforcing Pad Tpad 6.000 mm. Pad Parameter C11P C11p 550.000 mm. Pad Parameter C22P C22p 600.000 mm.
Design Internal Pressure Dp 0.500 bars Include Pressure Thrust No
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 Kgf Global Force (SUS) Fy 600.7 Kgf Global Force (SUS) Fz 0.0 Kgf Global Moment (SUS) Mx 0.0 Kg-m. Global Moment (SUS) My 0.0 Kg-m. Global Moment (SUS) Mz 210.3 Kg-m.
Internal Pressure (SUS) P 0.50 bars Include Pressure Thrust No
Global Force (OCC) Fx 0.0 Kgf Global Force (OCC) Fy 3563.7 Kgf Global Force (OCC) Fz 0.0 Kgf Global Moment (OCC) Mx 0.0 Kg-m. Global Moment (OCC) My 0.0 Kg-m. Global Moment (OCC) Mz 1247.3 Kg-m.
Occasional Internal Pressure (OCC) Pvar 1.58 bars
Use Interactive Control No WRC107 Version Version March 1979
Include Pressure Stress Indices per Div. 2 No Compute Pressure Stress per WRC-368 No
WRC 107 Stress Calculation for SUStained loads: Radial Load P 0.0 Kgf Circumferential Shear VC 0.0 Kgf Longitudinal Shear VL 600.7 Kgf Circumferential Moment MC 0.0 Kg-m. Longitudinal Moment ML -210.3 Kg-m. Torsional Moment MT 0.0 Kg-m.
Dimensionless Parameters used : Gamma = 102.58
Dimensionless Loads for Cylindrical Shells at Attachment Junction: -------------------------------------------------------------------
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Sup. Lug Calcs: Test : Step: 15 5:35p Aug 24,2014
Pressure for Reinforcement Calculations P 0.833 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10, EN10028-7:2007, EN10028-7:2007 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 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.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 0.00 deg Diameter 4.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N2
Actual Inside Diameter Used in Calculation 4.026 in. Actual Thickness Used in Calculation 0.237 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.833 * 102.260/( 2 * 127.341 * 1.000 - 0.083 ) + 0.000 = 0.033 mm.
EN13445 Section 9 - Pressure Area Design Method:Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((114.3000 - 6.0198 )*6.0198 , 150.0000 ) = 25.5309 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 25.531 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.754 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10, EN10028-7:2007, EN10028-7:2007 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Diameter of Cylindrical Shell Di 2450.00 mm. Shell Finished (Minimum) Thickness ea 6.0000 mm. Shell Internal Corrosion Allowance c 0.0000 mm. Shell External Corrosion Allowance co 0.0000 mm.
Distance from Bottom/Left Tangent 330.0000 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 0.00 deg Diameter 2.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm. User Defined Nozzle/Shell Centerline Angle 45.0000 deg.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N9
Actual Inside Diameter Used in Calculation 2.067 in. Actual Thickness Used in Calculation 0.154 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.754 * 52.502/( 2 * 127.341 * 1.000 - 0.075 ) + 0.000 = 0.016 mm.
EN13445 Section 9 - Pressure Area Design Method:
Nozzle Angle from vessel normal to surface used 45.000 deg.
Inside Radius per paragraph 9.5-3 [ris]: = ( Di + 2 * cs )/2 = ( 2450.000 + 2 * 0.000 )/2 = 1225.0000 mm.
Credit Distance Along the Nozzle per 9.5-76 [Ibo]: = min( sqrt( ( deb - 2 * cext - eab) * eab), ho ) = min(sqrt((60.325 -2*0.000 -3.912 )*3.912 ),150.000 ) = 14.8549 mm.
Credit Distance Along the Nozzle per 9.5-77 [Ibi]: = min(hi, 0.5*Ibo) = min(0.000 , 05*14.855 ) = 0.0000 mm.
Compute area in the re-pad [Afp]: = Ip * ep = 0.000 * 0.000 = 0.0000 cm^2
Calculate the Pressure Area per 9.5-29 [Aps]: Note: do (nozzle O/Dia.) taken as the diameter of the hole in the shell = ris * (Iso + do / 2 ) * ris + do/2 *( eas + eap ) = ris * (121.392 + 60.325/2)*1225.000 + 2.375/2*(6.000 +0.000 ) = 1.8584 x 10^3 cm^2
Slant Angle Area per 9.5-112 [APpsi] = di² * tan(Psi)/2 = 52.502² * tan(45.000 )/2 = 13.7822 cm^2
Pressure Area of Nozzle per using dib and Ibo [Apb]: (This is an inserted nozzle) = Ibo * dib/2 = 14.855 * 52.502/2
Force Term per 9.5.2.1.1 [Pa]: = P( Aps + Apb + 0.5 * APpsi ) = 0.754 ( 1858.352 + 3.900 + 0.5*13.782 ) = 1.4377 x 10^3 Kgf
Since Fa >= Pa, Code Requirements are satisfied.
The Drop for this Nozzle is : 0.3714 mm.The Cut Length for this Nozzle is, Drop + Ho + H + T : 156.3714 mm.
For possible nozzle interference - See Nozzle Summary
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59
PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Nozzle Calcs. : M Nozl: 18 5:35p Aug 24,2014
INPUT VALUES, Nozzle Description: M From : 30
Pressure for Reinforcement Calculations P 0.513 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 800.0000 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN10028-7:2007 Allowable Stress at Temperature fn 150.01 N./mm^2 Allowable Stress At Ambient fna 180.01 N./mm^2
Diameter Basis (for tr calc only) OD Layout Angle 0.00 deg Diameter 24.0000 in.
Size and Thickness Basis Actual Actual Thickness tn 8.0000 mm.
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 6.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Pad Material X5CrNi18-10, EN10028-7:2007 Pad Allowable Stress at Temperature f2 150.01 N./mm^2 Pad Allowable Stress At Ambient f2a 180.01 N./mm^2 Diameter of Pad along vessel surface d2 820.0001 mm. Thickness of Pad e2 6.0000 mm. Weld leg size between Pad and Shell Wp 6.0000 mm. Groove weld depth between Pad and Nozzle Wgpn 6.0000 mm. Reinforcing Pad Width 105.2000 mm. This is a Manway or Access Opening.
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PV Elite 2013 FileName : V-8304-V8305_R0 -------------------------------Nozzle Calcs. : M Nozl: 18 5:35p Aug 24,2014
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Isolated Nozzle Calculation per EN 13445, Description: M
Actual Outside Diameter Used in Calculation 24.000 in. Actual Thickness Used in Calculation 0.315 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.513 * 593.600/( 2 * 150.008 * 1.000 - 0.051 ) + 0.000 = 0.102 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
WARNING: Nozzle or Reinforcement Pad is outside Spherical D Limit !
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((609.6000 - 8.0000 )*8.0000 , 150.0000 ) = 69.3743 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 69.374 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 40.00 deg Diameter 3.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N1
Actual Inside Diameter Used in Calculation 3.068 in. Actual Thickness Used in Calculation 0.216 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 77.927/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.016 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((88.9000 - 5.4864 )*5.4864 , 150.0000 ) = 21.3925 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 21.393 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 60.00 deg Diameter 2.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N3
Actual Inside Diameter Used in Calculation 2.067 in. Actual Thickness Used in Calculation 0.154 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 52.502/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.011 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((60.3250 - 3.9116 )*3.9116 , 150.0000 ) = 14.8549 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 14.855 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 90.00 deg Diameter 6.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 80S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N4
Actual Inside Diameter Used in Calculation 5.761 in. Actual Thickness Used in Calculation 0.432 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 146.329/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.030 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((168.2750 - 10.9728 )*10.9728 , 150.0000 ) = 41.5457 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 41.546 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 120.00 deg Diameter 2.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N5
Actual Inside Diameter Used in Calculation 2.067 in. Actual Thickness Used in Calculation 0.154 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 52.502/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.011 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((60.3250 - 3.9116 )*3.9116 , 150.0000 ) = 14.8549 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 14.855 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 140.00 deg Diameter 1.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 80S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N6
Actual Inside Diameter Used in Calculation 0.957 in. Actual Thickness Used in Calculation 0.179 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 24.308/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.005 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((33.4010 - 4.5466 )*4.5466 , 150.0000 ) = 11.4538 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 11.454 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 160.00 deg Diameter 2.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N7
Actual Inside Diameter Used in Calculation 2.067 in. Actual Thickness Used in Calculation 0.154 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 52.502/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.011 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((60.3250 - 3.9116 )*3.9116 , 150.0000 ) = 14.8549 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 14.855 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 180.00 deg Diameter 1.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 80S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N8
Actual Inside Diameter Used in Calculation 0.957 in. Actual Thickness Used in Calculation 0.179 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 24.308/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.005 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((33.4010 - 4.5466 )*4.5466 , 150.0000 ) = 11.4538 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 11.454 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 200.00 deg Diameter 1.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 80S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N10
Actual Inside Diameter Used in Calculation 0.957 in. Actual Thickness Used in Calculation 0.179 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 24.308/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.005 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((33.4010 - 4.5466 )*4.5466 , 150.0000 ) = 11.4538 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 11.454 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 220.00 deg Diameter 3.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N11
Actual Inside Diameter Used in Calculation 3.068 in. Actual Thickness Used in Calculation 0.216 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 77.927/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.016 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((88.9000 - 5.4864 )*5.4864 , 150.0000 ) = 21.3925 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 21.393 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 240.00 deg Diameter 1.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 80S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N12
Actual Inside Diameter Used in Calculation 0.957 in. Actual Thickness Used in Calculation 0.179 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 24.308/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.005 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((33.4010 - 4.5466 )*4.5466 , 150.0000 ) = 11.4538 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 11.454 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 260.00 deg Diameter 2.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N13
Actual Inside Diameter Used in Calculation 2.067 in. Actual Thickness Used in Calculation 0.154 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 52.502/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.011 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((60.3250 - 3.9116 )*3.9116 , 150.0000 ) = 14.8549 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 14.855 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
Pressure for Reinforcement Calculations P 0.515 bars Temperature for Internal Pressure Temp 100 °C Design External Pressure Pext 0.30 bars Temperature for External Pressure Tempex 100 °C
Shell Material X5CrNi18-10 Shell Allowable Stress at Temperature f 150.01 N./mm^2 Shell Allowable Stress At Ambient fa 180.01 N./mm^2
Inside Crown Radius of Torispherical Head L 2450.0000 mm. Inside Knuckle Radius of Torispherical Head r 245.0000 mm. Head Finished (Minimum) Thickness ea 6.0000 mm. Head Internal Corrosion Allowance c 0.0000 mm. Head External Corrosion Allowance co 0.0000 mm.
Distance from Head Centerline L1 850.0001 mm.
Type of Element Connected to the Shell : Nozzle
Nozzle Material X5CrNi18-10, EN 10217-7:2005 Allowable Stress at Temperature fn 127.34 N./mm^2 Allowable Stress At Ambient fna 166.67 N./mm^2
Diameter Basis (for tr calc only) ID Layout Angle 280.00 deg Diameter 3.0000 in.
Size and Thickness Basis Nominal Nominal Thickness eb 40S
Flange Material X5CRNI18-10 Flange Type Weld Neck Flange
Corrosion Allowance can 0.0000 mm.
Outside Projection ho 150.0000 mm. Weld leg size between Nozzle and Pad/Shell Wo 10.0000 mm. Groove weld depth between Nozzle and Vessel Wgnv 4.0000 mm. Inside Projection h 0.0000 mm. Weld leg size, Inside Element to Shell Wi 0.0000 mm.
Class of attached Flange PN10 Grade of attached Flange 6E0
The Pressure Design option was Design Pressure + static head.
Nozzle Sketch (may not represent actual weld type/configuration)
Isolated Nozzle Calculation per EN 13445, Description: N14
Actual Inside Diameter Used in Calculation 3.068 in. Actual Thickness Used in Calculation 0.216 in.
Required Thickness of Nozzle Neck due to Internal Pressure: = P * Di / ( 2 * f * z - P ) + c EN-13445 Equation: 7.4.2: = 0.515 * 77.927/( 2 * 127.341 * 1.000 - 0.051 ) + 0.000 = 0.016 mm.
EN13445 Section 9 - Pressure Area Design Method:Note: This Is a Hillside Nozzle (Offset)
Crown Radius per 9.5.1 [ris]: = R + cs = 2450.000 + 0.0000 = 2450.0000 mm.
Outside Crown Diameter per paragraph 9.4.5.3 [De]: = ( ris + eas ) * 2 = ( 2450.000 + 6.000 ) * 2 = 4912.0000 mm.
Credit Distance Along the Shell per 9.5.1 [Iso]: = sqrt((2*ris+eas)*eas) = sqrt(2*2450.000 + 6.000 ) * 6.000 ) = 171.5692 mm.
Credit Distance Along the Nozzle outside per 9.5.7.1 [Ibo]: = min( sqrt( ( de - eab )*eab ), ho ) = min( sqrt((88.9000 - 5.4864 )*5.4864 , 150.0000 ) = 21.3925 mm.
Credit Distance Along the Nozzle per inside 9.5.7.1 [Ibi]: = min(hi, 0.50 * Ibo) = min(0.000 , 0.50 * 21.393 ) = 0.0000 mm.
Mean radius of Head per Figure 9.4-10 [rm]: = ris + eas/2 = 2450.000 + 6.000/2 = 2453.0000 mm.
The Cut Length is the Outside Projection + Inside Projection + Drop +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 mustbe 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 smallerand 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. ------------------------------------------------------------------------------ M X5CrNi18-10, EN10028 6.000 10.000 6.000 6.000 - N1 X5CrNi18-10, EN 1021 4.000 10.000 - - - N10 X5CrNi18-10, EN 1021 4.000 10.000 - - - N11 X5CrNi18-10, EN 1021 4.000 10.000 - - - N12 X5CrNi18-10, EN 1021 4.000 10.000 - - - N13 X5CrNi18-10, EN 1021 4.000 10.000 - - - N14 X5CrNi18-10, EN 1021 4.000 10.000 - - - N2 X5CrNi18-10, EN 1021 4.000 10.000 - - - N3 X5CrNi18-10, EN 1021 4.000 10.000 - - - N4 X5CrNi18-10, EN 1021 4.000 10.000 - - - N5 X5CrNi18-10, EN 1021 4.000 10.000 - - - N6 X5CrNi18-10, EN 1021 4.000 10.000 - - - N7 X5CrNi18-10, EN 1021 4.000 10.000 - - - N8 X5CrNi18-10, EN 1021 4.000 10.000 - - -
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. ---------------------------------------------------------------------------- M 0.00 150.00 0.00 Top head N1 40.00 150.00 0.00 Top head N10 200.00 150.00 0.00 Top head N11 220.00 150.00 0.00 Top head N12 240.00 150.00 0.00 Top head N13 260.00 150.00 0.00 Top head N14 280.00 150.00 0.00 Top head N2 0.00 150.00 0.00 Bottom head N3 60.00 150.00 0.00 Top head N4 90.00 150.00 0.00 Top head N5 120.00 150.00 0.00 Top head N6 140.00 150.00 0.00 Top head N7 160.00 150.00 0.00 Top head N8 180.00 150.00 0.00 Top head N9 330.000 0.00 150.00 0.00 Shell
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013
Description Pressure Area Result --------------------------------------------------------------------------- N2 Pressure Area Passed N9 Pressure Area Passed M Pressure Area Passed N1 Pressure Area Passed N3 Pressure Area Passed N4 Pressure Area Passed N5 Pressure Area Passed N6 Pressure Area Passed N7 Pressure Area Passed N8 Pressure Area Passed N10 Pressure Area Passed N11 Pressure Area Passed N12 Pressure Area Passed N13 Pressure Area Passed N14 Pressure Area Passed ---------------------------------------------------------------------------
Check the Spatial Relationship between the Nozzles
Design Code: European Std: EN13445-3 2009(E) Issue 1 (2009-07)
Diameter Spec : 2450.000 mm. ID Vessel Design Length, Tangent to Tangent 2450.00 mm.
Distance of Bottom Tangent above Grade 0.00 mm. Specified Datum Line Distance 0.00 mm.
Shell Material X5CrNi18-10, EN10028-7:2007 Lug Material P235GH, EN 10028-2:1992 Nozzle Material X5CrNi18-10, EN 10217-7:2005 Nozzle Material X5CrNi18-10, EN10028-7:2007 Re-Pad Material X5CrNi18-10, EN10028-7:2007
Internal Design Temperature 100 °C Internal Design Pressure 0.500 bars
External Design Temperature 100 °C External Design Pressure 0.300 bars
Maximum Allowable Working Pressure 1.407 bars External Max. Allowable Working Pressure 0.435 bars Hydrostatic Test Pressure 1.943 bars
Wind Design Code No Wind Loads Earthquake Design Code No Seismic
Element Pressures and MAWP: bars
Element Desc | Design Pres. | External | M.A.W.P | Corrosion | + Stat. head | Pressure | | Allowance --------------------------------------------------------------------- Bottom head 0.833 0.300 1.943 0.0000 Shell 0.782 0.300 4.849 0.0000 Top head 0.551 0.300 1.407 0.0000
Liquid Level: 3398.42 mm. Dens.: 0.001 kg./cm^3 Sp. Gr.: 1.000
Element "To" Elev Length Element Thk R e q d T h k Joint Eff Type mm. mm. mm. Int. Ext. Long Circ ----------------------------------------------------------------------- Torisph 50.0 50.0 8.0 3.1 2.5 0.70 0.70 Cylinder 2400.0 2350.0 6.0 0.9 5.2 0.70 0.70 Torisph 2450.0 50.0 8.0 2.7 2.5 0.70 0.70
Element thicknesses are shown as Nominal if specified, otherwise are Minimum
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: Fabricated - Bare W/O Removable Internals 2262.7 kg. Shop Test - Fabricated + Water ( Full ) 16717.4 kg. Shipping - Fab. + Rem. Intls.+ Shipping App. 2262.7 kg. Erected - Fab. + Rem. Intls.+ Insul. (etc) 2462.7 kg. Empty - Fab. + Intls. + Details + Wghts. 2462.7 kg. Operating - Empty + Operating Liquid (No CA) 16914.9 kg. Field Test - Empty Weight + Water (Full) 16717.4 kg.
PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013