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Page Date 03/12/2012 Designed MMR Checked MVV Title Doc No. : Min Mz = 8300.327 kN = 229.159 kNm = 7.991 kNm = 95.373 kN EFFECTIVE LENGTH IN Z DIR L z = 3m EFFECTIVE LENGTH IN Y DIR L y = 3m ENTER THE SECTION = A g = 32000 mm 2 I Z = 1.42E+09 mm 4 I Y = 5.36E+08 mm 4 b f = 400 mm t f = 20 mm t w = 32 mm H = 540 mm Z ez = 5.24E+06 mm 3 Z ey = 2.68E+06 mm 3 r z = 210.32 mm r y = 129.46 mm Z pz = 2 b f t f (H-t f ) / 2 + t w (H-2t f ) 2 /4 = 6160000 mm 3 Z py = 2 b f 2 t f / 4 + (H-2t f ) t w 2 /4 = 1728000 mm 3 I t = (2 b f t f 3 + (H-t f ) t w 3 ) / 3 = 7.813E+06 mm 4 I w = (H-t f ) 2 I y / 4 = 3.625E+13 mm 4 E = 2.E+05 N/mm 2 FACTORED MOMENT IN Z DIRECTION M z FACTORED MOMENT IN Y DIRECTION M y FACTORED AXIAL LOAD ON THE COLUMN F x or N or P 1) PROPERTIES OF SECTION FACTORED MAX. SHEAR FORCE F y or V REFER SHEET 1 OF THIS FILE Design of Top Chord-TC Grafix Engineering Consultants Pvt. Ltd. LATA TAPOVAN HEP (3X75MW), UTTARAKHAND LATA BRIDGE Project Details X X Y Y
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Jan 29, 2016

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Page 1: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Mz

= 8300.327 kN

= 229.159 kNm

= 7.991 kNm

= 95.373 kN

EFFECTIVE LENGTH IN Z DIR Lz = 3 m

EFFECTIVE LENGTH IN Y DIR Ly = 3 m

ENTER THE SECTION =

Ag = 32000 mm2

IZ = 1.42E+09 mm4

IY = 5.36E+08 mm4

bf = 400 mm

tf = 20 mm

tw = 32 mm

H = 540 mm

Zez = 5.24E+06 mm3

Zey = 2.68E+06 mm3

rz = 210.32 mm

ry = 129.46 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 6160000 mm

3

Zpy = 2 bf2

tf / 4 + (H-2tf) tw2/4 = 1728000 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 7.813E+06 mm

4

Iw = (H-tf)2Iy / 4 = 3.625E+13 mm

4

E = 2.E+05 N/mm2

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

Design of Top Chord-TC

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project Details

X X

Y

Y

Page 2: Design Sheets

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

13.4 23.2 26.5 33.2 PLASTIC 1

Web d/tw

31.3 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

Nd = Agfy/ mo = 11636.36 kN > 8300.327 kN SAFE

Minimum web thickness requirement

= 15.63 against 158.11 OK

= 15.63 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 3961.15 N/mm

2

lw = (fy / 3 tcr) = 0.24

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 3695.04 kN > 95.373 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 2240.00 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 628.36 kNm

(b) V>0.6Vd (9.2.1)

= 4160000 mm3

Mfdz = Z 'pzfy/ mo

= 1512.73 kNm

= (2V/Vd-1)2

= 0.899

Mdvz = Mdz - (Mdz – Mfdz) = 1585.876 kNm

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Change in major axis only (since only F y and not Fz is considered)

Plastic modulus of section excluding shear area Z 'pz

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

Page 3: Design Sheets

(c) Bending resistance

Final Mdz = 2240.00 kNm > 229.159 kNm SAFE

Final Mdy = 628.36 kNm > 7.991 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

n = N/Nd = 0.713

= 856.25 kNm > 229.159 kNm SAFE

= 514.00 kNm > 7.991 kNm SAFE

For I & H sections

1 =5n ≥ 1 = 3.57

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= 0.07 < 1 SAFE

N/Nd + Mz / Mdz + My / Mdy = NA NA NA

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 9701.46 N/mm2

lz = fy / fcr = 0.203

= 0.521

= 1.00

fcdz = zfy/ mo = 363.24 N/mm2

Pdz = Aefcdz = 11623.78 kN > 8300.327 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 3675.73 N/mm2

y = = 0.330

= 0.586

= 0.93

fcdy = yfy/ mo = 339.58 N/mm2

Pdy = Aefcdy = 10866.57 kN > 8300.327 kN SAFE

b = 1.00

= 31183.546 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.281

LT = 0.49 Welded Section

= 0.5594

= 0.9588

Non-dimsional lateral torsional slenderness ratio

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

z = 0.5(1 + az (lz - 0.2) + lz2)

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Reduced plastic moment resistance about major axis

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

Page 4: Design Sheets

fbd = LTfy/ mo = 348.6462 N/mm2

Mdz = bZpzfbd = 2147.66 kNm > 229.159 kNm SAFE

= 1.002

Cmz (for sway buckling mode) = 0.9

= 1.099

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.764

= 0.9387

= 0.87 < 1 SAFE

= 0.814 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Determination of moment amplification factors

Lateral torsional buckling resistance

Page 5: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

400 500 20 20 16 268 0 0 0

Location of centroid A

Xb 200 mm mm2

Yb 270 mm

W = 251.2 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 210.3172 mm

Iyy = mm4 ryy 129.4578 mm

Section modulus

Zxx 5.24E+06 mm3

Zyy 2.68E+06 mm3

Member Properties of Top Chord-TC

5.36E+08

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Total area of section

32000

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

1.42E+09

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 6: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Max Fx

= 1925.491 kN

= 51.311 kNm

= 41.054 kNm

= 29.544 kN

EFFECTIVE LENGTH IN Z DIR Lz = 6 m

EFFECTIVE LENGTH IN Y DIR Ly = 6 m

ENTER THE SECTION =

Ag = 17600 mm2

IZ = 5.22E+08 mm4

IY = 1.97E+08 mm4

bf = 300 mm

tf = 16 mm

tw = 20 mm

H = 432 mm

Zez = 2.42E+06 mm3

Zey = 1.31E+06 mm3

rz = 172.25 mm

ry = 105.82 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 2796800 mm

3

Zpy = 2 bf2

tf / 4 + (H-2tf) tw2/4 = 760000 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 1.929E+06 mm

4

Iw = (H-tf)2Iy / 4 = 8.526E+12 mm

4

E = 2.E+05 N/mm2

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

LATA BRIDGE

Project Details

Design of Bottom Chord - BC

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

X X

Y

Y

Page 7: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

15.0 23.2 26.5 33.2 PLASTIC 1

Web d/tw

40.0 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

Nd = Agfy/ mo = 6400.00 kN > 1925.491 kN SAFE

Minimum web thickness requirement

= 20.00 against 158.11 OK

= 20.00 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 2417.69 N/mm

2

lw = (fy / 3 tcr) = 0.31

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1847.52 kN > 29.544 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 1017.02 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 276.36 kNm

(b) V>0.6Vd (9.2.1)

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Change in major axis only (since only F y and not Fz is considered)

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Page 8: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

= 1996800 mm3

Mfdz = Z 'pzfy/ mo

= 726.11 kNm

= (2V/Vd-1)2

= 0.937

Mdvz = Mdz - (Mdz – Mfdz) = 744.419 kNm

(c) Bending resistance

Final Mdz = 1017.02 kNm > 51.311 kNm SAFE

Final Mdy = 276.36 kNm > 41.054 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

n = N/Nd = 0.301

= 948.05 kNm > 51.311 kNm SAFE

= 232.52 kNm > 41.054 kNm SAFE

For I & H sections

1 =5n ≥ 1 = 1.50

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= 0.08 < 1 SAFE

N/Nd + Mz / Mdz + My / Mdy = NA NA NA

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 1626.88 N/mm2

lz = fy / fcr = 0.496

= 0.673

= 0.89

fcdz = zfy/ mo = 322.20 N/mm2

Pdz = Aefcdz = 5670.71 kN > 1925.491 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 613.94 N/mm2

y = = 0.807

= 0.975

= 0.66

fcdy = yfy/ mo = 239.15 N/mm2

Pdy = Aefcdy = 4208.96 kN > 1925.491 kN SAFE

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Reduced plastic moment resistance about major axis

Plastic modulus of section excluding shear area Z 'pz

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

z = 0.5(1 + az (lz - 0.2) + lz2)

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Page 9: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

b = 1.00

= 2500.520 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.669

LT = 0.49 Welded Section

= 0.8386

= 0.7439

fbd = LTfy/ mo = 270.4929 N/mm2

Mdz = bZpzfbd = 756.51 kNm > 51.311 kNm SAFE

= 1.100

Cmz (for sway buckling mode) = 0.9

= 1.278

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.457

= 0.9126

= 0.67 < 1 SAFE

= 0.492 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Non-dimsional lateral torsional slenderness ratio

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Determination of moment amplification factors

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Page 10: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 400 16 16 10 240 0 0 0

Location of centroid A

Xb 150 mm mm2

Yb 216 mm

W = 138.16 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 172.2521 mm

Iyy = mm4 ryy 105.8157 mm

Section modulus

Zxx 2.42E+06 mm3

Zyy 1.31E+06 mm3

17600

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

5.22E+08

1.97E+08

Member Properties of Bottom Chord-BC

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Total area of section

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 11: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Max Fx

= 1832.621 kN

= 0 kNm

= 0 kNm

= 1.978 kN

EFFECTIVE LENGTH IN Z DIR Lz = 6 m

EFFECTIVE LENGTH IN Y DIR Ly = 6 m

ENTER THE SECTION =

Ag = 11720 mm2

IZ = 1.21E+08 mm4

IY = 1.25E+08 mm4

bf = 300 mm

tf = 12 mm

tw = 20 mm

H = 250 mm

Zez = 9.70E+05 mm3

Zey = 8.31E+05 mm3

rz = 101.73 mm

ry = 103.13 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 1112180 mm

3

Zpy = 2 bf2

tf / 4 + (H-2tf) tw2/4 = 562600 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 9.803E+05 mm

4

Iw = (H-tf)2Iy / 4 = 1.765E+12 mm

4

E = 2.E+05 N/mm2

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

LATA BRIDGE

Project Details

Design of Elevation Bracing EBR-1

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

X X

Y

Y

Page 12: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

20.0 23.2 26.5 33.2 PLASTIC 1

Web d/tw

22.6 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

Nd = Agfy/ mo = 4261.82 kN > 1832.621 kN SAFE

Minimum web thickness requirement

= 11.30 against 158.11 OK

= 11.30 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 7573.63 N/mm

2

lw = (fy / 3 tcr) = 0.17

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1043.85 kN > 1.978 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 404.43 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 204.58 kNm

(b) V>0.6Vd (9.2.1)

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Change in major axis only (since only F y and not Fz is considered)

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Page 13: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

= 856800 mm3

Mfdz = Z 'pzfy/ mo

= 311.56 kNm

= (2V/Vd-1)2

= 0.992

Mdvz = Mdz - (Mdz – Mfdz) = 312.266 kNm

(c) Bending resistance

Final Mdz = 404.43 kNm > 0 kNm SAFE

Final Mdy = 204.58 kNm > 0 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

n = N/Nd = 0.430

= 307.36 kNm > 0 kNm SAFE

= 200.57 kNm > 0 kNm SAFE

For I & H sections

1 =5n ≥ 1 = 2.15

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= 0.00 < 1 SAFE

N/Nd + Mz / Mdz + My / Mdy = NA NA NA

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 567.42 N/mm2

lz = fy / fcr = 0.840

= 0.961

= 0.70

fcdz = zfy/ mo = 254.44 N/mm2

Pdz = Aefcdz = 2982.06 kN > 1832.621 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 583.22 N/mm2

y = = 0.828

= 0.997

= 0.64

fcdy = yfy/ mo = 234.36 N/mm2

Pdy = Aefcdy = 2746.69 kN > 1832.621 kN SAFE

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Reduced plastic moment resistance about major axis

Plastic modulus of section excluding shear area Z 'pz

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

z = 0.5(1 + az (lz - 0.2) + lz2)

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Page 14: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

b = 1.00

= 972.768 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.676

LT = 0.49 Welded Section

= 0.8453

= 0.7393

fbd = LTfy/ mo = 268.8468 N/mm2

Mdz = bZpzfbd = 299.01 kNm > 0 kNm SAFE

= 1.393

Cmz (for sway buckling mode) = 0.9

= 1.419

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.667

= 0.8711

= 0.67 < 1 SAFE

= 0.615 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Non-dimsional lateral torsional slenderness ratio

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Determination of moment amplification factors

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Page 15: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 226 12 12 10 240 0 0 0

Location of centroid A

Xb 150 mm mm2

Yb 125 mm

W = 92.002 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 101.7275 mm

Iyy = mm4 ryy 103.1346 mm

Section modulus

Zxx 9.70E+05 mm3

Zyy 8.31E+05 mm3

11720

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

1.21E+08

1.25E+08

Member Properties of Elevation Bracing-EB1

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Total area of section

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 16: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Member End Forces

Beam L/C Node Fx kN Fy kN Fz kN Mx kNm My kNm Mz kNm

Max Fx 1181 315 LOAD GENERATION, LOAD #315, (38 of 40)442 863.518 0 -0.965 0 0 0

Min Fx 2124 315 LOAD GENERATION, LOAD #315, (38 of 40)442 -846.784 0 0.965 0 0 0

Max Fy 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Min Fy 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Max Fz 1138 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y111 252.642 0 0.965 0 0 0

Min Fz 1138 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y453 255.217 0 -0.965 0 0 0

Max Mx 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Min Mx 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Max My 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Min My 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Max Mz 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Min Mz 1121 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL443 414.282 0 -0.715 0 0 0

Max Fx

= 863.518 kN

= 0 kNm

= 0 kNm

= 0 kN

EFFECTIVE LENGTH IN Z DIR Lz = 5 m

EFFECTIVE LENGTH IN Y DIR Ly = 5 m

Distance between sections = 100 mm

Final Depth of section "D" = 250 mm

Final Width of section "B" = 200 mm

ISMC 200

Ag = 5700 mm2

IZ = 63291300 mm4

IY = 36600000 mm4

R1 = 11 mm

bf = 57.8 mm

tf = 11.4 mm

tw = 6.2 mm

dw = 155.2 mm

Zez = 506330.4 mm3

Zey = 366000.0 mm3

ry = 80.13 mm

rz = 105.37 mm

DESIGN OF Elevation Bracing - EB2

LATA BRIDGE

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED MAX. SHEAR FORCE Fy or V

1) PROPERTIES OF SECTION

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

Y

Y

Z Z

b

d

Page 17: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :LATA BRIDGE

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

Zpz = 5.87E+05 mm3

Zpy = 4.20E+05 mm3

E = 2.E+05 N/mm2

fy = 250 N/mm2

= 250 / fy = 1.00

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

5.1 9.4 10.5 15.7 PLASTIC 1

Web d/tw

25.0 42.0 42.0 42.0 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

Nd = Agfy/ mo = 1295.45 kN > 863.518 kN SAFE

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

Minimum web thickness requirement

= 28.58 against 200 OK

= 28.58 against 345 OK

Design Shear Strength Vd = Vn/ mo = (Av*fyw/(3)0.5

)/ mo = 345.84 kN > 0 kN SAFE

V < 0.6Vd

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Type of beam 2 Simply Supported

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 133.43 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 95.42 kNm

(b) V>0.6Vd (9.2.1)

= 302312 mm3

Mfdz = Z 'pzfy/ mo = 68.71 kNm

= (2V/Vd-1)2

= 1

Mdvz = Mdz - b(Mdz – Mfdz) = 68.71 kNm

(c) Bending resistance

Final Mdz = 133.44 kNm > 0 kNm SAFE

Final Mdy = 95.42 kNm > 0 kNm SAFE

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

aw = (Aw)/A <= 0.5 = 0.46

af = (Af)/A <= 0.5 = 0.44

Plastic modulus of section excluding shear area Z 'pz

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

Change in major axis only (since only F y and not F z is considered)

Y

Page 18: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :LATA BRIDGE

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

n = N/Nd = 0.67

= 57.87 kNm > 0 kNm SAFE

= 41.38 kNm > 0 kNm SAFE

For Rectangular tubes

1 =1.66/(1-1.13*n2)<=6 = 3.30

=1.66/(1-1.13*n2)<=6 = 3.30

(Mz / Mndz)2 + (My / Mndy)

1 = 0.00 < 1 SAFE

(N/Nd) +(Mz / Mdz)+ (My / Mdy) = NA NA NA

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Major Axis

Buckling class (Table 10 of IS:800-2007) = c Channel

Imperfection factor ( z) (for buckling class c) = 0.49

fccz = 2E / (1.1KLz/rz)

2( as per table 7 of IS:800-2007) = 724.56 N/mm

2

z = ( fy / fccz)0.5 = 0.587

= 0.767

= 0.79

fcdz = zfy/ mo = 180.19 N/mm2

Pdz = Aefcdz = 1027.07 kN > 863.518 kN SAFE

Minor Axis

Buckling class (Table 10 of IS:800-2007) = c Channel

Imperfection factor ( y) (for buckling class c) = 0.49

fccy = 2E / (1.1KLy/ry)

2( as per table 7 of IS:800-2007) = 419.00 N/mm

2

y =( fy / fccy)0.5 = 0.772

= 0.939

= 0.68

fcdy = yfy/ mo = 154.42 N/mm2

Pdy = Aefcdz = 880.22 kN > 863.518 kN SAFE

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

b = 1.00

= 364.87 kNm

LT = ( bZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.54

LT = 0.49 Welded Section

= 0.7291

= 0.8204

fbd = LTfy/ mo = 186.45 N/mm2

Non-dimsional lateral torsional slenderness ratio

Reduction factor lateral torsional buckling

FLT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

LT =1/ [ LT + ( LT2- LT

2)0.5

]

Lateral torsional buckling resistance

z = 0.5(1 + z ( z - 0.2) + z2)

z =1/ [ z + ( z2- z

2)0.5

]

y = 0.5(1 + y ( y - 0.2) + y2)

y =1/ [ y + ( y2- y

2)0.5

]

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }

0.5

Reduced plastic moment resistance about major axis

Mndz = Mdz (1-n)/(1-0.5aw) ≤ Mdz

Reduced plastic moment resistance about minor axis

Mndy = Mdy (1-n)/(1-0.5af) ≤ Mdy

Check for biaxial bending

Page 19: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :LATA BRIDGE

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

Mdz = bZpzfbd = 109.46 kNm > 0 kNm SAFE

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

= 1.326

Cmz (for sway buckling mode) = 0.9

= 1.562

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Column

ny = P / Pdy = 0.981

= 0.85

= 0.99 < 1 SAFE

= 0.841 < 1 SAFE(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

Determination of moment amplification factors

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Page 20: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Mz

= 1601.542 kN

= 1827.235 kNm

= 704.827 kNm

= 3654.47 kN

EFFECTIVE LENGTH IN Z DIR Lz = 4 m

EFFECTIVE LENGTH IN Y DIR Ly = 6.5 m

ENTER THE SECTION =

Ag = 51500 mm2

IZ = 3.41E+09 mm4

IY = 2.13E+09 mm4

bf = 550 mm

tf = 25 mm

tw = 40 mm

H = 650 mm

Zez = 1.05E+07 mm3

Zey = 7.76E+06 mm3

rz = 257.21 mm

ry = 203.59 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 12193750 mm

3

Zpy = 2 bf2 tf / 4 + (H-2tf) tw

2/4 = 4021250 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 1.906E+07 mm

4

Iw = (H-tf)2Iy / 4 = 2.085E+14 mm

4

E = 2.E+05 N/mm2

G = 76923 N/mm2

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

LATA BRIDGE

Project Details

Design of End Portal Column - EPC

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

X X

Y

Y

Page 21: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

18.8 23.2 26.5 33.2 PLASTIC 1

Web d/tw

30.0 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

Nd = Agfy/ mo = 18727.27 kN > 1601.542 kN SAFE

Minimum web thickness requirement

= 15.00 against 158.11 OK

= 15.00 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 4298.12 N/mm

2

lw = (fy / 3 tcr) = 0.23

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 5542.56 kN > 3654.47 kN SAFE

V > 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 4434.09 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 1462.27 kNm

(b) V>0.6Vd (9.2.1)

= 8593750 mm3

Mfdz = Z 'pzfy/ mo

= 3125.00 kNm

= (2V/Vd-1)2

= 0.102

Mdvz = Mdz - (Mdz – Mfdz) = 4301.133 kNm

(c) Bending resistance

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Change in major axis only (since only F y and not Fz is considered)

Plastic modulus of section excluding shear area Z 'pz

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Page 22: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

Final Mdz = 4301.13 kNm > 1827.235 kNm SAFE

Final Mdy = 1462.27 kNm > 704.827 kNm SAFE

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 8161.54 N/mm2

lz = fy / fcr = 0.221

= 0.528

= 0.99

fcdz = zfy/ mo = 360.88 N/mm2

Pdz = Aefcdz = 18585.25 kN > 1601.542 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 1936.50 N/mm2

y = = 0.454

= 0.666

= 0.87

fcdy = yfy/ mo = 315.67 N/mm2

Pdy = Aefcdy = 16257.11 kN > 1601.542 kN SAFE

b = 1.00

= 32411.411 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.388

LT = 0.49 Welded Section

= 0.6213

= 0.9037

fbd = LTfy/ mo = 328.6134 N/mm2

Mdz = bZpzfbd = 4007.03 kNm > 1827.235 kNm SAFE

= 1.002

Cmz (for sway buckling mode) = 0.9

= 1.025

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Column

ny = P / Pdy = 0.099

6) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Non-dimsional lateral torsional slenderness ratio

y =1/ [Fy + (Fy2-ly

2)0.5

]

7) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

8) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Determination of moment amplification factors

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

z = 0.5(1 + az (lz - 0.2) + lz2)

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Page 23: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

= 0.9891

= 0.96 < 1 SAFE

= 0.736 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Page 24: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

550 600 25 25 20 470 0 0 0

Location of centroid A

Xb 275 mm mm2

Yb 325 mm

W = 404.275 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 257.206 mm

Iyy = mm4 ryy 203.5905 mm

Section modulus

Zxx 1.05E+07 mm3

Zyy 7.76E+06 mm3

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Member Properties of End Portal Column-EPC

Total area of section

51500

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

3.41E+09

2.13E+09

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 25: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Member End Forces

Beam L/C Node Fx kN Fy kN Fz kN Mx kNm My kNm Mz kNm

Max Fx 1015 35 1.35DL+1.75SIDL WC+1.35SNL+1.5-BF+1.5*0.3SL-X+1.5*SL-Z+1.5*0.3SL-Y436 32.405 6.215 0.898 0 -3.593 -24.858

Min Fx 137 299 LOAD GENERATION, LOAD #299, (22 of 40)442 -394.065 2.047 -3.557 0 -2.629 -27.387

Max Fy 3439 197 LOAD GENERATION, LOAD #197, (40 of 40)75 -182.256 41.342 4.179 0 0 0

Min Fy 3465 27 1.0DL+1.0SIDL WC+1.0SNL+1.0PLL+0.75-BF+WL-X+WL-Z+WL-Y+TL104 -168.521 -39.637 -4.182 0 0 0

Max Fz 1015 227 LOAD GENERATION, LOAD #227, (30 of 40)436 -64.141 2.527 7.303 -0.002 -7.211 -46.106

Min Fz 125 227 LOAD GENERATION, LOAD #227, (30 of 40)436 -190.488 2.527 -7.303 -0.002 -7.211 -46.106

Max Mx 125 189 LOAD GENERATION, LOAD #189, (32 of 40)5 -141.486 -23.908 -3.736 0.003 0 0

Min Mx 126 27 1.0DL+1.0SIDL WC+1.0SNL+1.0PLL+0.75-BF+WL-X+WL-Z+WL-Y+TL6 -168.435 23.886 4.318 -0.003 0 0

Max My 125 167 LOAD GENERATION, LOAD #167, (10 of 40)436 -178.693 -1.886 7.274 0.003 7.095 51.545

Min My 125 227 LOAD GENERATION, LOAD #227, (30 of 40)436 -190.488 2.527 -7.303 -0.002 -7.211 -46.106

Max Mz 145 197 LOAD GENERATION, LOAD #197, (40 of 40)446 -238.956 -4.464 6.821 0 5.285 61.854

Min Mz 142 27 1.0DL+1.0SIDL WC+1.0SNL+1.0PLL+0.75-BF+WL-X+WL-Z+WL-Y+TL445 -176.569 4.07 -6.818 0 -5.273 -60.28

Max Mz

= 238.956 kN

= 61.854 kNm

= 5.285 kNm

= 4.464 kN

EFFECTIVE LENGTH IN Z DIR Lz = 5 m

EFFECTIVE LENGTH IN Y DIR Ly = 5 m

Distance between sections = 100 mm

Final Depth of section "D" = 250 mm

Final Width of section "B" = 200 mm

ISMC 200

Ag = 5700 mm2

IZ = 63291300 mm4

IY = 36600000 mm4

R1 = 11 mm

bf = 57.8 mm

tf = 11.4 mm

tw = 6.2 mm

dw = 155.2 mm

Zez = 506330.4 mm3

Zey = 366000.0 mm3

ry = 80.13 mm

rz = 105.37 mm

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED MAX. SHEAR FORCE Fy or V

1) PROPERTIES OF SECTION

LATA BRIDGE

DESIGN OF Elevation Vertical - EV

Y

Y

Z Z

b

d

Page 26: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Zpz = 5.87E+05 mm3

Zpy = 4.20E+05 mm3

E = 2.E+05 N/mm2

fy = 250 N/mm2

= 250 / fy = 1.00

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

5.1 9.4 10.5 15.7 PLASTIC 1

Web d/tw

25.0 42.0 42.0 42.0 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

Nd = Agfy/ mo = 1295.45 kN > 238.956 kN SAFE

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

Minimum web thickness requirement

= 28.58 against 200 OK

= 28.58 against 345 OK

Design Shear Strength Vd = Vn/ mo = (Av*fyw/(3)0.5

)/ mo = 345.84 kN > 4.464 kN SAFE

V < 0.6Vd

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Type of beam 2 Simply Supported

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 133.43 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 95.42 kNm

(b) V>0.6Vd (9.2.1)

= 302312 mm3

Mfdz = Z 'pzfy/ mo = 68.71 kNm

= (2V/Vd-1)2

= 0.95

Mdvz = Mdz - b(Mdz – Mfdz) = 71.95 kNm

(c) Bending resistance

Final Mdz = 133.44 kNm > 61.854 kNm SAFE

Final Mdy = 95.42 kNm > 5.285 kNm SAFE

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

aw = (Aw)/A <= 0.5 = 0.46

af = (Af)/A <= 0.5 = 0.44

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

Change in major axis only (since only F y and not F z is considered)

Plastic modulus of section excluding shear area Z 'pz

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Y

Page 27: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

n = N/Nd = 0.18

= 133.44 kNm > 61.854 kNm SAFE

= 95.42 kNm > 5.285 kNm SAFE

For Rectangular tubes

1 =1.66/(1-1.13*n2)<=6 = 1.73

=1.66/(1-1.13*n2)<=6 = 1.73

(Mz / Mndz)2 + (My / Mndy)

1 = 0.27 < 1 SAFE

(N/Nd) +(Mz / Mdz)+ (My / Mdy) = NA NA NA

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Major Axis

Buckling class (Table 10 of IS:800-2007) = c Channel

Imperfection factor ( z) (for buckling class c) = 0.49

fccz = 2E / (1.1KLz/rz)

2( as per table 7 of IS:800-2007) = 724.56 N/mm

2

z = ( fy / fccz)0.5 = 0.587

= 0.767

= 0.79

fcdz = zfy/ mo = 180.19 N/mm2

Pdz = Aefcdz = 1027.07 kN > 238.956 kN SAFE

Minor Axis

Buckling class (Table 10 of IS:800-2007) = c Channel

Imperfection factor ( y) (for buckling class c) = 0.49

fccy = 2E / (1.1KLy/ry)

2( as per table 7 of IS:800-2007) = 419.00 N/mm

2

y =( fy / fccy)0.5 = 0.772

= 0.939

= 0.68

fcdy = yfy/ mo = 154.42 N/mm2

Pdy = Aefcdz = 880.22 kN > 238.956 kN SAFE

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

b = 1.00

= 364.87 kNm

LT = ( bZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.54

LT = 0.49 Welded Section

= 0.7291

= 0.8204

fbd = LTfy/ mo = 186.45 N/mm2

y =1/ [ y + ( y2- y

2)0.5

]

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }

0.5

Reduced plastic moment resistance about major axis

Mndz = Mdz (1-n)/(1-0.5aw) ≤ Mdz

Reduced plastic moment resistance about minor axis

Mndy = Mdy (1-n)/(1-0.5af) ≤ Mdy

Check for biaxial bending

Non-dimsional lateral torsional slenderness ratio

Reduction factor lateral torsional buckling

FLT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

LT =1/ [ LT + ( LT2- LT

2)0.5

]

Lateral torsional buckling resistance

z = 0.5(1 + z ( z - 0.2) + z2)

z =1/ [ z + ( z2- z

2)0.5

]

y = 0.5(1 + y ( y - 0.2) + y2)

Page 28: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project

DetailsLATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Mdz = bZpzfbd = 109.46 kNm > 61.854 kNm SAFE

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

= 1.090

Cmz (for sway buckling mode) = 0.9

= 1.155

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Column

ny = P / Pdy = 0.271

= 0.96

= 0.78 < 1 SAFE

= 0.722 < 1 SAFE(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

Determination of moment amplification factors

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Page 29: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Member End Forces

Beam L/C Node Fx kN Fy kN Fz kN Mx kNm My kNm Mz kNm

Max Fx 955 237 LOAD GENERATION, LOAD #237, (40 of 40)123 201.326 0.457 0 0 0 0

Min Fx 954 237 LOAD GENERATION, LOAD #237, (40 of 40)92 -201.339 0.457 0 0 0 0

Max Fy 954 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y92 107.861 0.617 0 0 0 0

Min Fy 954 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y414 107.861 -0.617 0 0 0 0

Max Fz 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Min Fz 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Max Mx 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Min Mx 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Max My 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Min My 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Max Mz 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Min Mz 924 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL404 113.065 0.457 0 0 0 0

Max Fx

= 201.326 kN

= 0 kNm

= 0 kNm

= 0.457 kN

ACTUAL LENGTH IN Z DIR Lz = 3.92 m

ACTUAL LENGTH IN Y DIR Ly = 3.92 m

Effective Length factor Kz = 0.85

Effective Length factor Ky = 0.85

EFFECTIVE LENGTH IN Z DIR Lz = 3.332 m

EFFECTIVE LENGTH IN Y DIR Ly = 3.332 m

Thickness of gusset plate = 8 mm

b/t =

d/t =

(b+d)/t =

STAR ISA 90x90x8

Ag = 2760 mm2

Cx = 25.1 mm

Cy = 25.1 mm

IZ = 4.42E+06 mm4

IY = 4.42E+06 mm4

rz = 40.01 mm

ry = 40.01 mm

rv = 34.7 mm

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 250 N/mm2

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project

Details

Grafix Engineering Consultants Pvt. Ltd.

1) PROPERTIES OF SECTION

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED MAX. SHEAR FORCE Fy or V

DESIGN OF Top Plan Bracing - TB1

Page 30: Design Sheets

Major Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( z) (for buckling class c) = 0.49

fccz = 2E / (KLz/rv)

2 ( as per table 7 of IS:800-2007) = 214.08 N/mm2

z = ( fy / fcr)0.5 = 1.081

= 1.300

= 0.49

fcdz = zfy/ mo = 112.42 N/mm2

Pdz = Aefcdz = 310.28 kN > 201.326 kN SAFE

Minor Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( y) (for buckling class c) = 0.49

fccy = 2E / (KLy/rv)

2 ( as per table 7 of IS:800-2007) = 214.08 N/mm2

y =( fy / fcr)0.5 = 1.081

= 1.300

= 0.49

fcdy = yfy/ mo = 112.42 N/mm2

Pdz = Aefcdz = 310.28 kN > 201.326 kN SAFE

MEMBER BUCKLING RESISTANCE IN COMPRESSION (7.1.2 )

z = 0.5(1 + z ( z - 0.2) + z2)

z =1/ [ z + ( z2- z

2)

0.5]

y = 0.5(1 + y ( y - 0.2) + y2)

y =1/ [ y + ( y2- y

2)0.5

]

Page 31: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Member End Forces

Beam L/C Node Fx kN Fy kN Fz kN Mx kNm My kNm Mz kNm

Max Fx 973 237 LOAD GENERATION, LOAD #237, (40 of 40)117 107.472 0.377 0 0 0 0

Min Fx 972 237 LOAD GENERATION, LOAD #237, (40 of 40)86 -106.746 0.377 0 0 0 0

Max Fy 972 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y86 58.049 0.509 0 0 0 0

Min Fy 972 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y420 58.049 -0.509 0 0 0 0

Max Fz 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Min Fz 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Max Mx 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Min Mx 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Max My 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Min My 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Max Mz 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Min Mz 942 24 1.0DL+1.0SIDL WC+1.0SNL+1.0BF+0.6WL+X+0.6WL+Z+0.6WL+Y+0.6TL410 61.39 0.377 0 0 0 0

Max Fx

= 107.472 kN

= 0 kNm

= 0 kNm

= 0.377 kN

ACTUAL LENGTH IN Z DIR Lz = 5 m

ACTUAL LENGTH IN Y DIR Ly = 5 m

Effective Length factor Kz = 0.85

Effective Length factor Ky = 0.85

EFFECTIVE LENGTH IN Z DIR Lz = 4.25 m

EFFECTIVE LENGTH IN Y DIR Ly = 4.25 m

Thickness of gusset plate = 8 mm

b/t =

d/t =

(b+d)/t =

STAR ISA 75x75x8

Ag = 2280 mm2

Cx = 21.4 mm

Cy = 21.4 mm

IZ = 2.65E+06 mm4

IY = 2.65E+06 mm4

rz = 34.10 mm

ry = 34.10 mm

rv = 28.8 mm

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 250 N/mm2

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project

Details

Grafix Engineering Consultants Pvt. Ltd.

1) PROPERTIES OF SECTION

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED MAX. SHEAR FORCE Fy or V

DESIGN OF Top Plan Bracing - TB2

Page 32: Design Sheets

Major Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( z) (for buckling class c) = 0.49

fccz = 2E / (KLz/rv)

2 ( as per table 7 of IS:800-2007) = 90.64 N/mm2

z = ( fy / fcr)0.5 = 1.661

= 2.237

= 0.27

fcdz = zfy/ mo = 60.84 N/mm2

Pdz = Aefcdz = 138.72 kN > 107.472 kN SAFE

Minor Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( y) (for buckling class c) = 0.49

fccy = 2E / (KLy/rv)

2 ( as per table 7 of IS:800-2007) = 90.64 N/mm2

y =( fy / fcr)0.5 = 1.661

= 2.237

= 0.27

fcdy = yfy/ mo = 60.84 N/mm2

Pdz = Aefcdz = 138.72 kN > 107.472 kN SAFE

MEMBER BUCKLING RESISTANCE IN COMPRESSION (7.1.2 )

z = 0.5(1 + z ( z - 0.2) + z2)

z =1/ [ z + ( z2- z

2)

0.5]

y = 0.5(1 + y ( y - 0.2) + y2)

y =1/ [ y + ( y2- y

2)0.5

]

Page 33: Design Sheets

Page

Designed Date

Checked 03/12/2012

Title Doc No. :

Member End Forces

Beam L/C Node Fx kN Fy kN Fz kN Mx kNm My kNm Mz kNm

Max Fx 243 237 LOAD GENERATION, LOAD #237, (40 of 40)92 110.96 1.114 0.107 0 0 0

Min Fx 956 237 LOAD GENERATION, LOAD #237, (40 of 40)415 -111.826 -0.457 -0.107 0 0.27 -1.983

Max Fy 217 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y66 -51.004 1.503 -0.206 0 0 0

Min Fy 932 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y97 50.304 -1.503 0.206 0 0 0

Max Fz 238 317 LOAD GENERATION, LOAD #317, (40 of 40)87 37.839 0.414 0.402 0 0 0

Min Fz 971 317 LOAD GENERATION, LOAD #317, (40 of 40)420 -39.789 0.472 -0.402 0 1.015 0.073

Max Mx 218 34 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+1.5*0.3SL+X+1.5*SL+Z+1.5*0.3SL+Y67 -25.599 0.605 -0.199 0.002 0 0

Min Mx 218 550 LOAD GENERATION, LOAD #550, (33 of 40)67 23.36 0.612 -0.233 -0.002 0 0

Max My 238 317 LOAD GENERATION, LOAD #317, (40 of 40)420 37.839 -0.472 0.402 0 1.015 0.073

Min My 219 309 LOAD GENERATION, LOAD #309, (32 of 40)409 46.326 0.617 -0.397 0 -1.002 -2.677

Max Mz 220 30 1.35DL+1.75SIDL WC+1.35SNL+1.15BF+1.5WL+X+1.5WL+Z+1.5WL+Y410 -42.305 -0.625 -0.278 0 -0.702 0.46

Min Mz 217 28 1.35DL+1.75SIDL WC+1.35SNL+1.5BF+0.9WL+X+0.9WL+Z+0.9WL+Y407 -51.004 0.617 -0.206 0 -0.519 -2.677

Max Fx

= 110.96 kN

= 0 kNm

= 0 kNm

= 1.114 kN

ACTUAL LENGTH IN Z DIR Lz = 3.92 m

ACTUAL LENGTH IN Y DIR Ly = 3.92 m

Effective Length factor Kz = 0.85

Effective Length factor Ky = 0.85

EFFECTIVE LENGTH IN Z DIR Lz = 3.332 m

EFFECTIVE LENGTH IN Y DIR Ly = 3.332 m

Thickness of gusset plate = 8 mm

b/t =

d/t =

(b+d)/t =

STAR ISA 100x100x8

Ag = 3080 mm2

Cx = 27.6 mm

Cy = 27.6 mm

IZ = 5.98E+06 mm4

IY = 5.98E+06 mm4

rz = 44.05 mm

ry = 44.05 mm

rv = 38.8 mm

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 250 N/mm2

DESIGN OF Top Cross Beam - TCB1

1) PROPERTIES OF SECTION

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED MAX. SHEAR FORCE Fy or V

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project

Details

Grafix Engineering Consultants Pvt. Ltd.

Page 34: Design Sheets

Major Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( z) (for buckling class c) = 0.49

fccz = 2E / (KLz/rv)

2 ( as per table 7 of IS:800-2007) = 267.66 N/mm2

z = ( fy / fcr)0.5 = 0.966

= 1.155

= 0.56

fcdz = zfy/ mo = 127.19 N/mm2

Pdz = Aefcdz = 391.75 kN > 110.96 kN SAFE

Minor Axis

Buckling class (Table 10 of IS:800-2007) = c Angle

Imperfection factor ( y) (for buckling class c) = 0.49

fccy = 2E / (KLy/rv)

2 ( as per table 7 of IS:800-2007) = 267.66 N/mm2

y =( fy / fcr)0.5 = 0.966

= 1.155

= 0.56

fcdy = yfy/ mo = 127.19 N/mm2

Pdz = Aefcdz = 391.75 kN > 110.96 kN SAFE

y =1/ [ y + ( y2- y

2)0.5

]

MEMBER BUCKLING RESISTANCE IN COMPRESSION (7.1.2 )

z = 0.5(1 + z ( z - 0.2) + z2)

z =1/ [ z + ( z2- z

2)

0.5]

y = 0.5(1 + y ( y - 0.2) + y2)

Page 35: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Mz

= 726.106 kN

= 22.657 kNm

= 0.036 kNm

= 7.74 kN

EFFECTIVE LENGTH IN Z DIR Lz = 2.5 m

EFFECTIVE LENGTH IN Y DIR Ly = 2.5 m

ENTER THE SECTION =

Ag = 11720 mm2

IZ = 1.21E+08 mm4

IY = 1.25E+08 mm4

bf = 300 mm

tf = 12 mm

tw = 20 mm

H = 250 mm

Zez = 9.70E+05 mm3

Zey = 8.31E+05 mm3

rz = 101.73 mm

ry = 103.13 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 1112180 mm

3

Zpy = 2 bf2

tf / 4 + (H-2tf) tw2/4 = 562600 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 9.803E+05 mm

4

Iw = (H-tf)2Iy / 4 = 1.765E+12 mm

4

E = 2.E+05 N/mm2

Design of Top End Portal Beam-TEPB

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project Details

1) PROPERTIES OF SECTION

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

X X

Y

Y

Page 36: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project Details

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

20.0 23.2 26.5 33.2 PLASTIC 1

Web d/tw

22.6 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 1 PLASTIC OK

Nd = Agfy/ mo = 4261.82 kN > 726.106 kN SAFE

Minimum web thickness requirement

= 11.30 against 158.11 OK

= 11.30 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 7573.63 N/mm

2

lw = (fy / 3 tcr) = 0.17

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1043.85 kN > 7.74 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 1.00

Mdz = bZpzfy/ mo = 404.43 kNm

Minor Axis

b = 1.00

Mdy = bZpyfy/ mo = 204.58 kNm

(b) V>0.6Vd (9.2.1)

Change in major axis only (since only F y and not Fz is considered)

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

d/tw ≤ 200 (Serviceability requirement)

Page 37: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project Details

= 856800 mm3

Mfdz = Z 'pzfy/ mo

= 311.56 kNm

= (2V/Vd-1)2

= 0.971

Mdvz = Mdz - (Mdz – Mfdz) = 314.298 kNm

(c) Bending resistance

Final Mdz = 404.43 kNm > 22.657 kNm SAFE

Final Mdy = 204.58 kNm > 0.036 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

n = N/Nd = 0.170

= 404.43 kNm > 22.657 kNm SAFE

= 115.67 kNm > 0.036 kNm SAFE

For I & H sections

1 =5n ≥ 1 = 1.00

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= 0.00 < 1 SAFE

N/Nd + Mz / Mdz + My / Mdy = NA NA NA

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 3268.33 N/mm2

lz = fy / fcr = 0.350

= 0.587

= 0.95

fcdz = zfy/ mo = 343.83 N/mm2

Pdz = Aefcdz = 4029.66 kN > 726.106 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 3359.38 N/mm2

y = = 0.345

= 0.595

= 0.93

fcdy = yfy/ mo = 336.73 N/mm2

Pdy = Aefcdy = 3946.53 kN > 726.106 kN SAFE

z = 0.5(1 + az (lz - 0.2) + lz2)

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

Reduced plastic moment resistance about major axis

Plastic modulus of section excluding shear area Z 'pz

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Page 38: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Project Details

b = 1.00

= 4857.069 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.303

LT = 0.49 Welded Section

= 0.5709

= 0.9478

fbd = LTfy/ mo = 344.6541 N/mm2

Mdz = bZpzfbd = 383.32 kNm > 22.657 kNm SAFE

= 1.027

Cmz (for sway buckling mode) = 0.9

= 1.027

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.184

= 0.9841

= 0.24 < 1 SAFE

= 0.232 < 1 SAFE(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Determination of moment amplification factors

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Non-dimsional lateral torsional slenderness ratio

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Page 39: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 226 12 12 10 240 0 0 0

Location of centroid A

Xb 150 mm mm2

Yb 125 mm

W = 92.002 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 101.7275 mm

Iyy = mm4 ryy 103.1346 mm

Section modulus

Zxx 9.70E+05 mm3

Zyy 8.31E+05 mm3

Total area of section

11720

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

1.21E+08

1.25E+08

Member Properties of Top End Portal Beam-TEPB

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 40: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Max My

= 1136.553 kN

= 55.968 kNm

= 548.904 kNm

= 186.102 kN

EFFECTIVE LENGTH IN Z DIR Lz = 5 m

EFFECTIVE LENGTH IN Y DIR Ly = 2.05 m

ENTER THE SECTION =

Ag = 26800 mm2

IZ = 1.05E+09 mm4

IY = 8.75E+08 mm4

bf = 500 mm

tf = 16 mm

tw = 24 mm

H = 482 mm

Zez = 4.36E+06 mm3

Zey = 3.50E+06 mm3

rz = 198.05 mm

ry = 180.73 mm

Zpz = 2 bf tf (H-tf) / 2 + tw (H-2tf)2/4 = 4943000 mm

3

Zpy = 2 bf2

tf / 4 + (H-2tf) tw2/4 = 2064800 mm

3

It = (2 bf tf3 + (H-tf) tw

3) / 3 = 3.513E+06 mm

4

Iw = (H-tf)2Iy / 4 = 4.752E+13 mm

4

E = 2.E+05 N/mm2

FACTORED MAX. SHEAR FORCE Fy or V

REFER SHEET 1 OF THIS FILE

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

LATA BRIDGE

Project Details

Design of Bottom Cross Beam-BCB1

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

X X

Y

Y

Page 41: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

27.3 23.2 26.5 33.2 SEMI-COMPACT 3

Web d/tw

37.5 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 3 SEMI-COMPACT OK

Nd = Agfy/ mo = 9745.45 kN > 1136.553 kN SAFE

Minimum web thickness requirement

= 18.75 against 158.11 OK

= 18.75 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 2750.80 N/mm

2

lw = (fy / 3 tcr) = 0.29

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 2494.15 kN > 186.102 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 0.88

Mdz = bZpzfy/ mo = 1586.14 kNm

Minor Axis

b = 1.70

Mdy = bZpyfy/ mo = 1273.26 kNm

(b) V>0.6Vd (9.2.1)

d/tw ≤ 200 (Serviceability requirement)

d/tw ≤ 345 f2 (Compression flange buckling requirement)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

Change in major axis only (since only F y and not Fz is considered)

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

Page 42: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

= 3728000 mm3

Mfdz = Z 'pzfy/ mo

= 1355.64 kNm

= (2V/Vd-1)2

= 0.724

Mdvz = Mdz - (Mdz – Mfdz) = 1586.142 kNm

(c) Bending resistance

Final Mdz = 1586.14 kNm > 55.968 kNm SAFE

Final Mdy = 1273.26 kNm > 548.904 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

n = N/Nd = 0.117

= 1586.14 kNm > 55.968 kNm NA

= 524.70 kNm > 548.904 kNm NA

For I & H sections

1 =5n ≥ 1 = 1.00

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= NA NA NA

N/Nd + Mz / Mdz + My / Mdy = 0.58 < 1 SAFE

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 3097.04 N/mm2

lz = fy / fcr = 0.359

= 0.592

= 0.94

fcdz = zfy/ mo = 342.51 N/mm2

Pdz = Aefcdz = 9179.15 kN > 1136.553 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 15341.78 N/mm2

y = = 0.161

= 0.504

= 1.00

fcdy = yfy/ mo = 363.64 N/mm2

Pdy = Aefcdy = 9745.45 kN > 1136.553 kN SAFE

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Reduced plastic moment resistance about major axis

Plastic modulus of section excluding shear area Z 'pz

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

z = 0.5(1 + az (lz - 0.2) + lz2)

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Page 43: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :LATA BRIDGE

Project Details

Grafix Engineering Consultants Pvt. Ltd.

LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

b = 0.88

= 96162.799 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.135

LT = 0.49 Welded Section

= 0.4931

= 1.0000

fbd = LTfy/ mo = 363.6364 N/mm2

Mdz = bZpzfbd = 1586.14 kNm > 55.968 kNm SAFE

= 1.020

Cmz (for sway buckling mode) = 0.9

= 0.996

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.117

= 0.9955

= 0.54 < 1 SAFE

= 0.388 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

Non-dimsional lateral torsional slenderness ratio

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Determination of moment amplification factors

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Page 44: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

500 450 16 16 12 436 0 0 0

Location of centroid A

Xb 250 mm mm2

Yb 241 mm

W = 210.38 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 198.0516 mm

Iyy = mm4 ryy 180.7286 mm

Section modulus

Zxx 4.36E+06 mm3

Zyy 3.50E+06 mm3

8.75E+08

Member Properties of Bottom Cross Beam-BCB1

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Total area of section

26800

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

1.05E+09

t1

s

t2

t3t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 45: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Mz

= 1174.441 kN

= 171.871 kNm

= 1.287 kNm

= 55.987 kN

EFFECTIVE LENGTH IN Z DIR Lz = 5.05 m

EFFECTIVE LENGTH IN Y DIR Ly = 0.3 m

ENTER THE SECTION =

Ag = 15000 mm2

IZ = 6.13E+08 mm4

IY = 7.21E+07 mm4

bf = 300 mm

tf = 16 mm

tw = 12 mm

H = 482 mm

Zez = 2.54E+06 mm3

Zey = 4.80E+05 mm3

rz = 202.07 mm

ry = 69.31 mm

Zpz = bf tf (H-tf) + tw (H-2tf)2/4 = 2844300 mm

3

Zpy = 0.5* bf2 tf = 720000 mm

3

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

DESIGN OF Bottom Cross Beam - BCB2

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

FACTORED MAX. SHEAR FORCE Fy or V

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

REFER SHEET 1 OF THIS FILE

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

X X

Y

Y

Page 46: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

9.0 6.6 7.4 10.8 SEMI-COMPACT 3

Web d/tw

37.5 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 3 SEMI-COMPACT OK

Nd = Agfy/ mo = 5454.55 kN > 1174.441 kN SAFE

Minimum web thickness requirement

= 37.50 against 158.11 OK

= 37.50 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 687.70 N/mm

2

lw = (fy / 3 tcr) = 0.58

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1247.08 kN > 55.987 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 0.89

Mdz = bZpzfy/ mo = 924.19 kNm

Minor Axis

b = 0.67

Mdy = bZpyfy/ mo = 174.70 kNm

(b) V>0.6Vd (9.2.1)

= 2236800 mm3

Mfdz = Z 'pzfy/ mo

= 813.382 kNm

= (2V/Vd-1)2

= 0.828

Mdvz = Mdz - (Mdz – Mfdz) = 924.186 kNm

(c) Bending resistance

Final Mdz = 924.19 kNm > 171.871 kNm SAFE

Final Mdy = 174.70 kNm > 1.287 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

d/tw ≤ 200 (Serviceability requirement)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

Change in major axis only (since only F y and not Fz is considered)

Plastic modulus of section excluding shear area Z 'pz

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

d/tw ≤ 345 f2 (Compression flange buckling requirement)

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Page 47: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

n = N/Nd = 0.215

= 924.19 kNm > 171.871 kNm NA

= 118.07 kNm > 1.287 kNm NA

For I & H sections

1 =5n ≥ 1 = 1.08

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= NA NA NA

N/Nd + Mz / Mdz + My / Mdy = 0.41 < 1 SAFE

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 3160.57 N/mm2

lz = fy / fcr = 0.356

= 0.590

= 0.94

fcdz = zfy/ mo = 343.01 N/mm2

Pdz = Aefcdz = 5145.14 kN > 1174.441 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 105370.53 N/mm2

y = = 0.062

= 0.468

= 1.00

fcdy = yfy/ mo = 363.64 N/mm2

Pdy = Aefcdy = 5454.55 kN > 1174.441 kN SAFE

b = 0.89

= 368473.263 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.053

LT = 0.49 Welded Section

= 0.4652

= 1.0000

fbd = LTfy/ mo = 363.6364 N/mm2

Mdz = bZpzfbd = 924.19 kNm > 171.871 kNm SAFE

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

Reduced plastic moment resistance about major axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

z = 0.5(1 + az (lz - 0.2) + lz2)

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Non-dimsional lateral torsional slenderness ratio

Page 48: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

= 1.036

Cmz (for sway buckling mode) = 0.9

= 0.970

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.215

= 0.9968

= 0.41 < 1 SAFE

= 0.405 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Determination of moment amplification factors

Page 49: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 450 16 16 12 0 0 0 0

Area Calculations :

Area of top flange plate 4800 mm2

1 No

Area of bottom flange plate 4800 mm2

1 No

Area of one web plate 5400 mm2

2 Nos..

Area of top cover plate 0 mm2

1 No.

Area of bottom cover plate 0 mm3

1 No..

Location of centroid A

Xb 150 mm mm2

Yb 241 mm

W = 117.75 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 202.0733 mm

Iyy = mm4 ryy 69.3132 mm

Section modulus

Zxx 2.54E+06 mm3

Zyy 4.80E+05 mm3

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Member Properties of Bottom Cross Beam-BCB2

Total area of section

15000

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

6.13E+08

7.21E+07

t1

s

t2

t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 50: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Fx

= 1354 kN

= 194 kNm

= 0 kNm

= 112 kN

EFFECTIVE LENGTH IN Z DIR Lz = 5.05 m

EFFECTIVE LENGTH IN Y DIR Ly = 0.3 m

ENTER THE SECTION =

Ag = 14616 mm2

IZ = 5.25E+08 mm4

IY = 7.21E+07 mm4

bf = 300 mm

tf = 16 mm

tw = 12 mm

H = 450 mm

Zez = 2.33E+06 mm3

Zey = 4.80E+05 mm3

rz = 189.58 mm

ry = 70.22 mm

Zpz = bf tf (H-tf) + tw (H-2tf)2/4 = 2607372 mm

3

Zpy = 0.5* bf2 tf = 720000 mm

3

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

REFER SHEET 1 OF THIS FILE

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

1) PROPERTIES OF SECTION

2) CROSS SECTION CLASSFICATION (3.7.2 - TABLE 2)

FACTORED MAX. SHEAR FORCE Fy or V

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

DESIGN OF Bottom Joist Beam - BJB1

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

X X

Y

Y

Page 51: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

9.0 6.6 7.4 10.8 SEMI-COMPACT 3

Web d/tw

34.8 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 3 SEMI-COMPACT OK

Nd = Agfy/ mo = 5314.91 kN > 1354 kN SAFE

Minimum web thickness requirement

= 34.83 against 158.11 OK

= 34.83 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 797.02 N/mm

2

lw = (fy / 3 tcr) = 0.54

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1158.40 kN > 112 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 0.90

Mdz = bZpzfy/ mo = 848.96 kNm

Minor Axis

b = 0.67

Mdy = bZpyfy/ mo = 174.69 kNm

(b) V>0.6Vd (9.2.1)

= 2083200 mm3

Mfdz = Z 'pzfy/ mo

= 757.527 kNm

= (2V/Vd-1)2

= 0.651

Mdvz = Mdz - (Mdz – Mfdz) = 848.960 kNm

(c) Bending resistance

Final Mdz = 848.96 kNm > 194 kNm SAFE

Final Mdy = 174.69 kNm > 0 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

d/tw ≤ 345 f2 (Compression flange buckling requirement)

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (9.3.1 )

Change in major axis only (since only F y and not Fz is considered)

Plastic modulus of section excluding shear area Z 'pz

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (8.2.1.2 & 9.2.1)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (9.3.1.1)

d/tw ≤ 200 (Serviceability requirement)

4) SHEAR CAPACITY OF THE SECTION (8.6.1 & 8.4.2.2a)

Page 52: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

n = N/Nd >= a = 0.500

= 565.97 kNm > 194 kNm NA

= 174.69 kNm > 0 kNm NA

For I & H sections

1 =5n ≥ 1 = 1.27

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= NA NA NA

N/Nd + Mz / Mdz + My / Mdy = 0.48 < 1 SAFE

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 2781.77 N/mm2

lz = fy / fcr = 0.379

= 0.602

= 0.93

fcdz = zfy/ mo = 339.73 N/mm2

Pdz = Aefcdz = 4965.42 kN > 1354 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 108131.97 N/mm2

y = = 0.061

= 0.468

= 1.00

fcdy = yfy/ mo = 363.64 N/mm2

Pdy = Aefcdy = 5314.91 kN > 1354 kN SAFE

b = 0.90

= 343171.798 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.052

LT = 0.49 Welded Section

= 0.4651

= 1.0000

fbd = LTfy/ mo = 363.6364 N/mm2

Mdz = bZpzfbd = 848.96 kNm > 194 kNm SAFE

Non-dimsional lateral torsional slenderness ratio

z = 0.5(1 + az (lz - 0.2) + lz2)

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Reduced plastic moment resistance about major axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (8.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (7.1.2 )

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

Page 53: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

LATA BRIDGE

= 1.049

Cmz (for sway buckling mode) = 0.9

= 0.965

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.255

= 0.9962

= 0.48 < 1 SAFE

= 0.488 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Determination of moment amplification factors

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (9.3.2.2)

Page 54: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 418 16 16 12 0 0 0 0

Area Calculations :

Area of top flange plate 4800 mm2

1 No

Area of bottom flange plate 4800 mm2

1 No

Area of one web plate 5016 mm2

2 Nos..

Area of top cover plate 0 mm2

1 No.

Area of bottom cover plate 0 mm3

1 No..

Location of centroid A

Xb 150 mm mm2

Yb 225 mm

W = 114.7356 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 189.5775 mm

Iyy = mm4 ryy 70.21557 mm

Section modulus

Zxx 2.33E+06 mm3

Zyy 4.80E+05 mm3

14616

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

5.25E+08

7.21E+07

Member Properties of Bottom Joist Beam - BJB1

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Total area of section

t1

s

t2

t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc

Page 55: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Min Mz

= 1272.271 kN

= 361.244 kNm

= 0 kNm

= 6.055 kN

EFFECTIVE LENGTH IN Z DIR Lz = 6 m

EFFECTIVE LENGTH IN Y DIR Ly = 0.3 m

ENTER THE SECTION =

Ag = 15600 mm2

IZ = 7.64E+08 mm4

IY = 7.21E+07 mm4

bf = 300 mm

tf = 16 mm

tw = 12 mm

H = 532 mm

Zez = 2.87E+06 mm3

Zey = 4.80E+05 mm3

rz = 221.33 mm

ry = 67.97 mm

Zpz = bf tf (H-tf) + tw (H-2tf)2/4 = 3226800 mm

3

Zpy = 0.5* bf2 tf = 720000 mm

3

E = 2.E+05 N/mm2

G = 76923 N/mm2

fy = 400 N/mm2

e = 250 / fy = 0.79

DESIGN OF Bottom Joist Beam - BCB2

FACTORED AXIAL LOAD ON THE COLUMN Fx or N or P

1) PROPERTIES OF SECTION

2) CROSS SECTION CLASSFICATION (503.7.2 - TABLE 2 of IRC:24-2010)

FACTORED MAX. SHEAR FORCE Fy or V

FACTORED MOMENT IN Z DIRECTION Mz

FACTORED MOMENT IN Y DIRECTION My

REFER SHEET 1 OF THIS FILE

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

X X

Y

Y

Page 56: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

Plastic Compact Semi-compact Section Class

Outstand of flange b/tf

9.0 6.6 7.4 10.8 SEMI-COMPACT 3

Web d/tw

41.7 66.4 83.0 99.6 PLASTIC 1

Therefore overall section classified as 3 SEMI-COMPACT OK

Nd = Agfy/ mo = 5672.73 kN > 1272.271 kN SAFE

Minimum web thickness requirement

= 41.67 against 158.11 OK

= 41.67 against 215.63 OK

Kv ( when transverse stiffeners are provided only at supports) = 5.35

cr,e = Kvp2E / (12(1-m

2)(d/tw)

2) = 557.04 N/mm

2

lw = (fy / 3 tcr) = 0.64

when lw ≤ 0.8 tb = fy / 3

b = 230.94 N/mm2

when lw ≥ 0.8 tb = fy / 3 lw2

Vd = Vcr = dtw b = 1385.64 kN > 6.055 kN SAFE

V < 0.6Vd

Type of beam 3 Neither

(a) V<=0.6Vd (8.2.1.2)

Major Axis

b = 0.89

Mdz = bZpzfy/ mo = 1044.73 kNm

Minor Axis

b = 0.67

Mdy = bZpyfy/ mo = 174.72 kNm

(b) V>0.6Vd (9.2.1)

= 2476800 mm3

Mfdz = Z 'pzfy/ mo

= 900.655 kNm

= (2V/Vd-1)2

= 0.983

Mdvz = Mdz - (Mdz – Mfdz) = 1044.729 kNm

(c) Bending resistance

Final Mdz = 1044.73 kNm > 361.244 kNm SAFE

Final Mdy = 174.72 kNm > 0 kNm SAFE

a = (A-2btf)/A <= 0.5 = 0.50

d/tw ≤ 200 (Serviceability requirement)

4) SHEAR CAPACITY OF THE SECTION (509.6.1 & 509.4)

3) RESISTANCE TO COMPRESSION DUE TO YIELDING (510.3.1.1)

Change in major axis only (since only F y and not Fz is considered)

Plastic modulus of section excluding shear area Z 'pz

when 0.8< w < 1.2; b =[1-0.8( w-0.8)]

5) BENDING RESISTANCE OF THE CROSS-SECTION (509.2.1 )

d/tw ≤ 345 f2 (Compression flange buckling requirement)

6) SECTION STRENGTH UNDER COMBINED BENDING AND AXIAL FORCE (510.3.1.2 )

Page 57: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

n = N/Nd = 0.224

= 1044.73 kNm > 361.244 kNm NA

= 121.59 kNm > 0 kNm NA

For I & H sections

1 =5n ≥ 1 = 1.12

2 = 2.00

(Mz / Mndz)2 + (My / Mndy)

1= NA NA NA

N/Nd + Mz / Mdz + My / Mdy = 0.57 < 1 SAFE

Major Axis

Buckling class = b Welded Section

Imperfection factor ( z) = 0.34

fccz = 2E / (KLz/rz)

2 = 2686.09 N/mm2

lz = fy / fcr = 0.386

= 0.606

= 0.93

fcdz = zfy/ mo = 338.78 N/mm2

Pdz = Aefcdz = 5284.89 kN > 1272.271 kN SAFE

Minor Axis

Buckling class = c Welded Section

Imperfection factor ( y) = 0.49

fccy = 2E / (KLy/ry)

2 = 101327.94 N/mm2

y = = 0.063

= 0.468

= 1.00

fcdy = yfy/ mo = 363.64 N/mm2

Pdy = Aefcdy = 5672.73 kN > 1272.271 kN SAFE

b = 0.89

= 408015.608 kNm

LT = (bbZpzfy / Mcr)0.5

<= (1.2Zezfy / Mcr)0.5 = 0.053

LT = 0.49 Welded Section

= 0.4654

= 1.0000

fbd = LTfy/ mo = 363.6364 N/mm2

Mdz = bZpzfbd = 1044.73 kNm > 361.244 kNm SAFE

Mndy = Mdy [1-((n-a)/(1-a))2] ≤ Mdy

Check for biaxial bending

Mndz = Mdz (1-n) / (1-0.5a) ≤ Mdz

Reduced plastic moment resistance about minor axis

Reduced plastic moment resistance about major axis

y =1/ [Fy + (Fy2-ly

2)0.5

]

8) MEMBER BUCKLING RESISTANCE IN BENDING (509.2.2 )

z =1/ [Fz + (Fz2-lz

2)0.5

]

y = 0.5(1 + ay (ly - 0.2) + ly2)

7) MEMBER BUCKLING RESISTANCE IN COMPRESSION (507.1.2 )

z = 0.5(1 + az (lz - 0.2) + lz2)

LT =1/ [FLT + (FLT2-lLT

2)0.5

]

Lateral torsional buckling resistance

Reduction factor lateral torsional buckling

LT = 0.5(1 + aLT (lLT - 0.2) + lLT2)

Mcr = [ (2EIyhf) / 2(KLy)

2] {1+(1/20) [KLy / ry) / (hf / tf) ]

2 }0.5

Non-dimsional lateral torsional slenderness ratio

Page 58: Design Sheets

Page

Date 03/12/2012

Designed MMR

Checked MVV

Title Doc No. :

Grafix Engineering Consultants Pvt. Ltd.

Project Details LATA TAPOVAN HEP (3X75MW), UTTARAKHAND

POWERHOUSE BRIDGE

= 1.045

Cmz (for sway buckling mode) = 0.9

= 0.969

Cmy (for sway buckling mode) = 0.9

CmLT = 0.600 Beam Ends

ny = P / Pdy = 0.224

= 0.9966

= 0.57 < 1 SAFE

= 0.566 < 1 SAFE

(P / Pdy) +(KyCmyMy / Mdy) +(KLTMz / Mdz)

9) MEMBER STRENGTH UNDER COMBINED BENDING & AXIAL COMPRESSION (510.3.2.2)

(P / Pdz) +(0.6KyCmyMy / Mdy) +(KzCmzMz / Mdz)

KLT = 1-((0.1 LTny) / (CmLT - 0.25)) ≥ 1-((0.1ny) / (CmLT - 0.25))

Check with interaction formula

Kz = 1 + ( z - 0.2)P/Pdz ≤ (1+0.8P/Pdz)

Ky = 1 + ( y - 0.2)P/Pdy ≤ (1+0.8P/Pdy)

Determination of moment amplification factors

Page 59: Design Sheets

a h t1 t2 t3 s tc1 tc2 bc

300 500 16 16 12 0 0 0 0

Area Calculations :

Area of top flange plate 4800 mm2

1 No

Area of bottom flange plate 4800 mm2

1 No

Area of one web plate 6000 mm2

2 Nos..

Area of top cover plate 0 mm2

1 No.

Area of bottom cover plate 0 mm3

1 No..

Location of centroid A

Xb 150 mm mm2

Yb 266 mm

W = 122.46 kg/m

Moment of Inertia calculations :

Radius of gyration

Ixx = mm4 rxx 221.3333 mm

Iyy = mm4 ryy 67.97058 mm

Section modulus

Zxx 2.87E+06 mm3

Zyy 4.80E+05 mm3

Total area of section

15600

Total Weight of the section per m length used

Moment of Inertia about X-X axis & Y-Y axis

7.64E+08

7.21E+07

CALCULATION SHEET FOR MOMENT OF INERTIA FOR SINGLE FLANGE PLATE BUILT-UP SECTIONS

Please note :

1. This sheet is used for calculating Moment of inertia of built up

sections about X-X & Y-Y axes.

2. Input all the values in mm units.

3. This sheet calculates M.O.I for built up section with flange plate

and cover plate.

4. Calculations are disposed assuming the section is symmetrical

about Y-Y AXIS.

5. Xb & Yb are the centroidal distances from the reference as

indicated. 6. in

case of single web plate girder geometric properties are desired "

input half the thickness of webplate for t3 ".

7.if the girder is with only single flange plate input tc1, tc2 & bc =0

User input values

Member Properties of Bottom Joist Beam-BJB2

t1

s

t2

t3

h

a

a

X X

Y

Y

Xb

Yb

tc1

tc2

bc

bc