151702959 built up steel column

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    A.Intermediateframe

    6.A.1 Loads:

    6. COLUMN

    -Checking the member for the following combination of loads:

    Vmax = Fy,max = 780 kN -maxm. shear force

    -the beam is connected at the face of column. Forces to be tranferred at the centroid of column:

    Offset, o = 750 mm -offset of column in major axis directn.

    6.A.2 Sectional properties & end conditions:

    Section: 4 x 300 NB 6 THK. TATA STRUCTURA

    Properties: Individualmember-

    ##

    Izz = Iyy = 79288969 mm yCompositesection-

    It = 158.58 x10

    Acomp. = 25143.8 mm

    mm4

    z

    ##

    Self-wt.comp = 197.4 kg/m

    4

    Fig. 4.a Columnc/s

    Izz,comp. = 14.46 x10

    Iyy,comp. = 1.32 x10

    mm

    mm4

    x10

    9

    mm6 4

    -warping const.

    Self-wt. = 49.34 kg/m

    Outer diameter of pipe = 323.9 mm

    Thickness = 6.3 mm

    Inner diameter of pipe

    A

    =

    =

    311.3 mm

    6286 mm2

    For load case 1.2 [DL+OL+LL+WL_135DEG], for member no. 401 in STAAD file

    Case 2: Fx = 710 kN -maxm. axial compression

    Mz = 1650 kN-m -moment

    For load case 1.5 [DL+OL+WL_0DEG], for member no. 401 in STAAD file

    Case 1: Fx = -750 kN -maxm. axial tension

    Mz = 1730 kN-m -moment

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    It,comp = 15.78 x10 mm

    -torsional constant

    zpz,comp = 18.86 x10

    zpy,comp = 5.03 x10

    zez,comp = 15.86 x10

    zey,comp = 3.65 x10

    rz = 758.36 mm

    ry = 229.38 mm

    fy = 310 MPa

    fu = 450 MPa

    mm3

    mm3 mm3 mm3

    -plastic section modulus

    -elastic section modulus

    -radius of gyration

    Structural restrain:L = 12000 mm -unrestrained length

    LLT = 0.8 L

    = 12000 mm

    2

    24000 mm

    07]

    0.5

    2007], (full torsionall warping restrain)

    -for effective length of compression member (one end fixed, other free)

    rr2

    I

    y Iw

    GIt LLT 2

    -elastic critical moment

    Mcr =

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    LLT 2

    Iy +

    rr2

    I

    y

    [Annex. E-1.1, IS 800- 2007]

    E

    G

    -extreme fibre bending

    compressive stress

    Section Classification:

    51.4

    0.90

    1462.'. b = 0.84 As section is semi-compact

    Mdz = bzpfbd

    = 4468.4 kN-m

    -moment capacity @ major axis

    Mz,max = Mz + (F x o) F- axial force, o-offset

    6.A.4 Tensile strength:-considering yeilding of gross section

    Td = Agfy/mo

    [As per Cl. 6.2 of IS 800- 2007]

    = 7086.0 kN -design tensile strength

    Tmax = 750 kN -maxm. axial tension

    Td > Tmax OK

    6.A.5 Compressive strength:

    = 2292.5 kN-m for case I

    = 2182.5 kN-m for case II

    Mdz > Mz,max OK

    Mcr = 150655.8 kN-m

    fcr,b =

    =

    Mcr / Zpx

    7989.0 MPa

    .'. fbd = 281.8 MPa

    = 200000 MPa -Young's modulus

    = 79300 MPa -modulus of rigidity

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    1.05 x (kL/rmin) = 109.86 mm -for laced column

    07]

    Buckling class = c

    fc = 101.19 MPa

    tions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 2544.3 kN -design compressive strength

    Pmax = 710.0 kN -maxm. axial compression Pd > Pmax OK

    COMBINEDCHECKS:

    6.A.6 Section strength: [As per Sec. 9.3.1 of IS 800- 2007]

    N My

    Mz

    1.0

    Nd + Mdy + Mdz

    Nd + Mdy + Mdz

    = 0.59 -for Case II

    6.A.7 Overall member strength:

    A) Bending + Axial tension [As per Sec. 9.3.2.1, IS 800- 2007]

    NMy = 0.62 OK -for Case I

    N = 750 kN -axial tension

    My=

    =

    710 kN

    0 kN-m

    -axial compression

    -no moment acting @ minor axis

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    Meff = [M-TZec/A] Md

    = 1 -T & M cannot vary independently Meff = 2292.50 kN-m

    Md > Meff OK

    B) Bending + Axial compression [As per Sec. 9.3.2.2, IS 800- 2007]

    p pdy +

    Cmy My Ky

    Mdy

    + KLT

    Mz Mdz

    1.0

    Cmy My

    Ky

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    + Kz

    Cmz Mz

    1.0

    pdz + 0.6

    Mdy

    Mdz

    KLT =

    LT ny

    1

    CmLT

    0.25

    Ky = 1+(y-0.2)ny 1 + 0.8ny

    Kz = 1+(z-0.2)nz 1 + 0.8nz

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    0.1ny

    1 C 0.25

    z

    =

    y =

    fcc =

    fy

    fcc

    rr2

    kL 2

    r

    fcc,z = 1970.9 MPa

    0.40

    P/Pd

    0.279

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    fy

    LT =

    fcr,b

    fcr,b = 7989.0 MPa

    LT = 0.20

    CmLT = 0.7

    Cmy = Cmz = 0.7

    IS 800- 2007]

    M1 = 0.2)

    p pdy

    + Ky

    CmyMy Mdy

    Mz

    + KLT

    Ky = Kz = 1.1

    KLT = 0.99

    My = 0 kN-m -no moment acting @ minor axis

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    dz

    = 0.76 OK

    CmyMy

    K

    K Cmz Mz

    = 0.64 OK

    pdz + 0.6 y

    Mdy +

    z Mdz

    6.A.8 Design of Lacings:

    -Lacings are designed to take the shear force on the column section Lacings would be of two types:

    i) Primary: these take shear force obtained by analysis acting along the y directn. (Fig. 4.a)ii) Secondary: these take shear = 2.5% of axial load along the z directn. (Fig. 4.a)

    Fy s P

    (shear)

    % of axial

    orce

    1500 400

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    Fig.4.b-Lacingarrangement

    i) Primary Lacings:

    Loads-

    Fy,max = 780 kN -maxm. SF in the column

    -c/s area

    Ixx = Iyy = 7.33 x10

    It = 14.65 x10

    mm4

    mm4

    -second moment of area

    -torsional const.

    zp = (d 3

    - d 3)/6 -plastic section modulus

    = 116.10 x103 mm3

    ze = 89 x10

    mm3

    -elastic section modulus

    rmin = 56.8 mm -radius of gyration

    fy = 310 MPa -grade of steel fu = 450 MPa

    Structuralrestrain-k = 1

    OtherParameters-

    -both ends pinned, as lacings take only axial loads

    s = 3000 mm -spacing of lacing system

    P = 551.5 kN

    = 45

    ks/r1 50

    0.7 (kL/rmin)comp.

    -axial compression on each lacing element

    [As per Cl. 7.6.5.1, IS 800- 2007]

    r1 - radius of gyration of individual member being laced together

    0.7 (kL/rmin)comp. = 73.24 mm (kL/rmin)comp. -for the composite section

    r1 = 112.31 mm

    ks/r1 = 26.7 mm OK

    Compressioncapacity-

    L = 2121 mm

    kL/rmin = 37.35 mm

    -c/c length of each lacing member

    Inner diameter of pipe

    A

    =

    =

    156.1 mm

    2270 mm2

    Self-wt. = 17.82 kg/m

    Section: 150 NB 4.5 THK.

    Properties:

    TATA STRUCTURA

    Outer diameter of pipe = 165.1 mmThickness = 4.5 mm

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    Buckling class = a

    fc = 263.15 MPa

    ions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 597.5 kN -design compressive strength

    Pmax = 551.5 kN -maxm. axial compression Pd > Pmax OK

    ii) Secondary Lacings:

    Loads-

    P = 47.6 kN -2.5% of (P + M/d)

    Section: 32 NB 3.2 THK. TATA STRUCTURA

    Properties:

    Outer diameter of pipe = 33.7 mm Thickness = 3.2 mm

    Inner diameter of pipe = 27.3 mm

    A = 307 mm2 -c/s area Self-wt. = 2.41 kg/m

    Ixx = Iyy = 0.04 x10

    It = 0.07 x10

    mm4

    mm4

    -second moment of area

    -torsional const.

    zp = (d 3

    - d 3)/6 -plastic section modulus

    x103 mm3

    z x103

    mm3

    -elastic section modulus

    rminfy fu

    mm -radius of gyration

    MPa -grade of steel MPa

    Structuralrestrain-k

    OtherParameters-

    -considering both ends pinned

    s = 750 mm -spacing of lacing system @ z-axis

    P = 32.6 kN

    =

    =

    =

    10.8

    310

    450

    = 1

    =

    =

    2.99

    2

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    = 43

    ks/r1 50

    0.7 (kL/rmin)comp.

    -axial compression on each lacing element

    [As per Cl. 7.6.5.1, IS 800- 2007]

    r1 - radius of gyration of individual member being laced together

    0.7 (kL/rmin)comp. = 73.24 mm (kL/rmin)comp. -for the composite section

    r1 = 112.31 mm

    ks/r1 = 6.7 mm OK

    Compressioncapacity-

    L = 548 mm

    kL/rmin = 50.57 mm

    -c/c length of each lacing member

    Buckling class = a

    fc = 247.06 MPa

    ions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 75.8 kN -design compressive strength

    Pmax = 32.6 kN -maxm. axial compression Pd > Pmax OK

    6.A.9 Welded connection between lacing & column:

    i) Primary Lacing-

    -Using fillet weld for the joint

    Weld capacity =

    fu

    y

    mw

    Weld thickness = 4 mm

    tt

    mw

    =

    =

    2.83 mm

    1.25

    Grade of weld=

    =

    32.6 kN

    Fe 540

    -for secondary lacing

    fu = 540 MPa

    fy = 410 MPa

    Force to be transmitted, Fmax = 551.5 kN -for primary lacing

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    t

    t

    N/mm

    -effective throat thickness of weld

    -for shop fabrications= 587.9 N/mm

    m

    -using welded gusset plated connection for the member:

    m

    m

    OK

    Fig.4.c-Typicalweldedgussetplatedconnection

    ii) Secondary Lacing-

    -Using fillet weld for the joint

    -effective throat thickness of weld

    -for shop fabrications

    6.A.10 Welded connection between gusset plate & column CHS:

    -Gusset plate is provided for primary lacings

    -Gusset plate transfers force from lacings to column members

    -thickness of gusset plate

    Grade of weld = Fe 540

    fu = 540 MPa

    fy = 410 MPa

    -Using fillet weld for the joint

    Weld capacity =

    fy t =

    =

    410 MPa

    6 mm

    Weld thickness = 6 mm

    tt

    mw

    =

    =

    4.24 mm

    1.25

    Force transferred, F = 551.5 kN

    Grade of plate = Fe 540

    fu = 540 MPa

    tt

    mw

    =

    =

    2.12 mm

    1.25

    Weld capacity = 440.9 N/mm

    Weld length reqd.

    Provided weld length

    =

    =

    74.0 mm

    105.9 mmOK

    Weld thickness = 3 mm

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    fu

    y

    mw

    t

    t

    N/mm

    -effective throat thickness of weld

    -for shop fabrications

    B.Endframe

    6.B.1 Loads:

    -Checking the member for the following combination of loads:

    Vmax = Fy,max = 240 kN -maxm. shear force

    -the beam is connected at the face of column. Forces to be tranferred at the centroid of column:

    Offset, o = 750 mm -offset of column in major axis directn.

    6.B.2 Sectional properties & end conditions:

    Section: 4 x 200 NB 6 THK. TATA STRUCTURAProperties: Individualmember-

    ##

    Izz = Iyy = 22819474 mm y

    Thickness = 6 mm

    Inner diameter of pipe

    A

    =

    =

    207.1 mm

    4017 mm2

    Self-wt. = 31.53 kg/m

    Mz = 510 kN-m -moment

    Outer diameter of pipe = 219.1 mm

    Mz = 475 kN-m -moment

    For load case 1.2 [DL+OL+LL+WL_135DEG], for member no. 401 in STAAD file

    Case 2: Fx

    = 245 kN -maxm. axial compression

    Provided weld length = 700 mm -providing weld on both sides

    For load case 1.5 [DL+OL+WL_0DEG], for member no. 401 in STAAD file

    Case 1: Fx = -230 kN -maxm. axial tension

    = 1058.2 N/mm

    Weld length reqd. = 521.2l = 350.0 mm -length of plate

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    Compositesection-

    It = 45.64 x10

    Acomp. = 16067.36 mm

    mm4

    z

    ##

    Self-wt.comp = 126.1 kg/m4

    Fig. 4.a Columnc/s

    Izz,comp. = 9.13 x10

    Iyy,comp. = 0.73 x10

    mm

    mm4

    x10

    9

    mm6 4

    -warping const.

    It,comp = 9.86 x10 mm

    -torsional constant

    zpz,comp = 12.05 x10

    zpy,comp = 3.21 x10

    zez,comp = 10.62 x10

    zey,comp = 2.37 x10

    rz = 753.78 mm

    ry = 213.73 mm

    fy = 310 MPa

    fu = 450 MPa

    mm3

    mm3 mm3 mm3

    -plastic section modulus

    -elastic section modulus

    -radius of gyration

    Structural restrain:

    L = 12000 mm -unrestrained length

    LLT = 0.8 L

    = 12000 mm

    2

    24000 mm

    07]

    0.5

    2007], (full torsional

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    l warping restrain)

    -for effective length of compression member (one end fixed, other free)

    rr2

    I

    y Iw

    GIt LLT 2

    -elastic critical moment

    Mcr =

    LLT 2

    Iy +

    rr2

    I

    y

    [Annex. E-1.1, IS 800- 2007]

    E

    G

    = 7361.5 MPa

    .'. fbd = 281.8 MPa-extreme fibre bending

    compressive stress

    Section Classification: [Table 2, IS 800- 2007]

    D/t = 36.5

    0.90

    D/t < 522 Section is compact

    As section is compact

    fcr,b = Mcr / Zpx

    = 200000 MPa -Young's modulus

    = 79300 MPa -modulus of rigidity

    Mcr = 88710.3 kN-m

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    Mdz = bzpfbd

    = 3395.8 kN-m

    -moment capacity @ major axis

    Mz,max = Mz + (F x o) F- axial force, o-offset

    Mdz > Mz,max OK

    6.B.4 Tensile strength:

    -considering yeilding of gross section

    Td = Agfy/mo

    [As per Cl. 6.2 of IS 800- 2007]

    = 4528.1 kN -design tensile strength

    Tmax = 230 kN -maxm. axial tension

    Td > Tmax OK

    6.B.5 Compressive strength:

    1.05 x (kL/rmin) = 117.91 mm -for laced column

    07]

    Buckling class = c

    fc = 90.92 MPa

    tions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 1460.9 kN -design compressive strength

    Pmax = 245.0 kN -maxm. axial compression Pd > Pmax OK

    COMBINEDCHECKS:

    6.B.6 Section strength: [As per Sec. 9.3.1 of IS 800- 2007]

    N My

    Mz

    1.0

    = 647.5 kN-m for case I

    = 693.8 kN-m for case II

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    Nd + Mdy + Mdz

    Nd + Mdy + Mdz

    = 0.26 -for Case II

    6.B.7 Overall member strength:

    A) Bending + Axial tension [As per Sec. 9.3.2.1, IS 800- 2007]

    Meff = [M-TZec/A] Md

    = 1 -T & M cannot vary independently Meff = 647.50 kN-m

    Md > Meff OK

    B) Bending + Axial compression [As per Sec. 9.3.2.2, IS 800- 2007]

    p pdy +

    Cmy My Ky

    Mdy

    + KLT

    NMy = 0.24 OK -for Case I

    N = 230 kN -axial tension

    My==

    245 kN0 kN-m

    -axial compression-no moment acting @ minor axis

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    Mz Mdz

    1.0

    Cmy My

    Ky

    + Kz

    Cmz Mz

    1.0

    pdz + 0.6

    Mdy

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    Mdz

    KLT =

    LT ny

    1

    CmLT

    0.25

    0.1ny

    1 C 0.25

    z

    =

    y =

    fcc =

    fy

    Ky = 1+(y-0.2)ny 1 + 0.8ny

    Kz = 1+(z-0.2)nz 1 + 0.8nz

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    fcc

    rr2

    kL 2

    r

    fcc,z = 1947.1 MPa

    0.40

    P/Pd

    0.168

    fy

    LT =

    fcr,b

    fcr,b = 7361.5 MPa

    LT = 0.21

    CmLT = 0.7

    Cmy = Cmz = 0.7

    IS 800- 2007]

    M1 = 0.2)

    Ky = Kz = 1.0

    KLT = 0.99

    My = 0 kN-m -no moment acting @ minor axis

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    p pdy

    + Ky

    CmyMy Mdy

    Mz

    + KLT

    dz

    = 0.37 OK

    CmyMy

    K

    K Cmz Mz

    = 0.32 OK

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    pdz + 0.6 y

    Mdy +

    z Mdz

    6.B.8 Design of Lacings:

    -Lacings are designed to take the shear force on the column section Lacings would be of two types:

    i) Primary: these take shear force obtained by analysis acting along the y directn. (Fig. 4.a)

    ii) Secondary: these take shear = 2.5% of axial load along the z directn. (Fig. 4.a)

    Fy s P

    (shear)

    % of axial

    orce

    1500 400

    i) Primary Lacings:

    Loads-

    Fy,max = 240 kN -maxm. SF in the column

    -c/s area

    Ixx = Iyy = 0.96 x10

    It = 1.93 x10

    mm4

    mm4

    -second moment of area

    -torsional const.

    zp = (d 3

    - d 3)/6 -plastic section modulus

    = 28.85 x103 mm3

    Inner diameter of pipe

    A

    =

    =

    80.9 mm

    1067 mm2

    Self-wt. = 8.38 kg/m

    Section: 80 NB 3.2 THK.

    Properties:

    TATA STRUCTURA

    Outer diameter of pipe = 88.9 mm

    Thickness = 4 mm

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    ze = 22 x10

    mm3

    -elastic section modulus

    rmin = 30.0 mm -radius of gyration

    fy = 310 MPa -grade of steel fu = 450 MPa

    Structuralrestrain-k = 1

    OtherParameters-

    -both ends pinned, as lacings take only axial loads

    s = 3000 mm -spacing of lacing system

    P = 169.7 kN

    = 45

    ks/r1 50

    0.7 (kL/rmin)comp.

    -axial compression on each lacing element

    [As per Cl. 7.6.5.1, IS 800- 2007]

    r1 - radius of gyration of individual member being laced together

    0.7 (kL/rmin)comp. = 78.60 mm (kL/rmin)comp. -for the composite section

    r1 = 75.37 mm

    ks/r1 = 39.8 mm OK

    Compressioncapacity-

    L = 2121 mm

    kL/rmin = 70.59 mm

    -c/c length of each lacing member

    Buckling class = a

    fc = 209.58 MPa

    ions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 223.6 kN -design compressive strength

    Pmax = 169.7 kN -maxm. axial compression Pd > Pmax OK

    ii) Secondary Lacings:

    Loads-

    P = 14.6 kN -2.5% of (P + M/d)

    Section: 32 NB 2.6 THK. TATA STRUCTURA

    Properties:

    Outer diameter of pipe = 33.7 mm Thickness = 3.2 mm

    Inner diameter of pipe = 27.3 mm

    A = 307 mm2 -c/s area Self-wt. = 2.41 kg/m

    Ixx = Iyy = 0.04 x10

    It = 0.07 x10

    mm4

    mm4

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    -second moment of area

    -torsional const.

    zp = (d 3

    - d 3)/6 -plastic section modulus

    x103 mm3

    z x103

    mm3

    -elastic section modulus

    rmin

    fy fu

    mm -radius of gyration

    MPa -grade of steel MPa

    Structuralrestrain-k

    OtherParameters-

    -considering both ends pinned

    s = 750 mm -spacing of lacing system @ z-axis

    P = 10.0 kN

    = 43

    ks/r1 50

    0.7 (kL/rmin)comp.

    -axial compression on each lacing element

    [As per Cl. 7.6.5.1, IS 800- 2007]

    r1 - radius of gyration of individual member being laced together

    0.7 (kL/rmin)comp. = 78.60 mm (kL/rmin)comp. -for the composite section

    r1 = 75.37 mm

    ks/r1 = 10.0 mm OK

    Compressioncapacity-

    L = 548 mm

    kL/rmin

    = 50.57 mm-c/c length of each lacing member

    Buckling class = a

    fc = 247.06 MPa

    ions as per Table-

    00- 2007]

    of IS 800- 2007]

    Pd = 75.8 kN -design compressive strength

    =

    =

    =

    10.8

    310

    450

    = 1

    =

    =

    2.99

    2

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    Pmax = 10.0 kN -maxm. axial compression Pd > Pmax OK

    6.B.9 Welded connection between lacing & column:

    i) Primary Lacing-

    -Using full penetration groove weld for the joint

    Weld thickness = 4 mm

    tt = 4 mm

    -effective throat thickness of weld

    mw = 1.25 -for shop fabrications

    fu

    Weld capacity =

    3 y

    mw

    t

    t

    N/mm

    = 831.4 N/mm

    Weld length reqd. = 204.1 mm

    Provided weld length = 279.3 mm OK

    -providing weld around the whole

    circumference of the tube

    ii) Secondary Lacing-

    Weld thickness = 3 mm -fillet weld

    tt = 2.12 mm

    -effective throat thickness of weld-for shop fabrications

    mw = 1.25

    Weld capacity = 440.9

    Weld length reqd.

    Provided weld length

    =

    =

    22.7 mm

    105.9 mmOK

    Grade of weld=

    =

    10.0 kN

    Fe 540

    -for secondary lacing

    fu = 540 MPafy = 410 MPa

    Force to be transmitted, Fmax = 169.7 kN -for primary lacing