Lug 0-5 ton Design

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  • 7/28/2019 Lug 0-5 ton Design

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    EVERSENDAI ENGINEERING W.L.L Sheet of

    PROJECT Job No Designed by

    DOHA CONVENTION CENTER & TOWER - QATAR

    Date Checked by

    SUBJECT TYPICAL LIFTING LUG DESIGN FOR 5 Tons 12.2.11Reference Code & Journal

    Notation definition:

    Load Calculation ts = Thickness of stiffner

    Self Weight = 5.000 t Ss = Size of weld for stiffner

    Additional Weight Due to Impact (25%) = 1.250 t Sl = Size of weld for lug

    tl = Thickness of lug

    Total Weight = 6.250 t dh = Dia of hole

    dd = Dia of de-shackle

    Total Nos. of Lifting Lug = 1 Nos. Ws = Width of stiffner

    No of Lifting Lug sharing the Load 1 Nos. W l = Width of lug

    Hl = Hight of lug

    Weight / Lug = Total Weight / 1 Hs = Hight of stiffner

    = 6.250 t E = Distance from edge of hole to edge

    ~ 6.250 t ~ kN of plate parallel force direction

    Capacity of DEE SHACKLES = 10 t Table. 13 Approved Code of Practice

    For Load - Lifting Rigging

    Rope Diameter (Wire Ropes With Fibre = 20 mm Table. 7 Approved Code of Practice

    Core - 1770 Tensile Strength Steel) For Load - Lifting Rigging

    Lifting Lug Specification

    Hl = mm Wh = mm

    Hs = mm a = mm

    W l = mm b = mm

    tl = mm ts = mm

    Ed = mm Ss = mm

    dh = mm Sl = mm

    dd = mm Ws = mm

    Material Specification

    Attached drawing only for reference

    Lifting Lug Connecting Member Weld Specification

    Grade = S275 Grade =ASTM 572M Type = E70XX

    Yield Strength = N/mm2 Yield Strength = N/mm2 Nominal Strength = N/mm2

    Tensile Strength = N/mm2

    Notation definition contd:

    Ty a = Least plate width in lug

    T T - Rope Tension b = Max plate widh of lug

    T = Tx = Ty Conservative Side Wh = Critical width of plate

    Ty

    170

    75

    200

    125

    16

    65 8

    12

    410

    345255

    STV

    NVP

    165

    40

    120

    10

    62.5

    291

    50

    32

    SENDAI

  • 7/28/2019 Lug 0-5 ton Design

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    EVERSENDAI ENGINEERING W.L.L Sheet of

    PROJECT Job No Designed by

    DOHA CONVENTION CENTER & TOWER - QATAR

    Date Checked by

    SUBJECT TYPICAL LIFTING LUG DESIGN FOR 5 Tons 12.2.11

    Reference Code & Journal

    STV

    NVP

    SENDAI

    I.CHECK FOR LIFTING LUG

    1. Tensile Capacity

    i. Tensile Yielding (Ref. ANSI/AISC 360-05, D2-a)

    ft Pn = ft fyAg= 605.88 kN > kN Safe

    ii. Tensile Rupture (Ref. ANSI/AISC 360-05, D5)

    = ft 2 t beff Fu

    beff = 2t + 16= 48 mm

    Tensile Rupture Capacity = 472.32 kN

    Safe Working Load = Pn/5

    = 94.464 kN > kN Safe

    Provide washer plate of 10 mm thickness on both side of lifting lugs = 10 mm

    Total thickness of lifting lug (t) = 36

    beff = 2t + 16

    = 88

    Tensile Rupture Capacity = 1948.32

    Safe Working Load = Pn/5

    = 389.664 > kN Safe

    iii. Tensile Blockout Failure (Ref.Design and Construction of Lifting Beam by DAVID.T.RICKER)

    P = (1.67 Fb t e2)/d

    Fb = 0.9 Fy (Ref. ANSI/AISC 360-05,F1)

    = 229.5 N/mm2

    P = 518.174 kN

    Safe Working Load = P/1.8

    by DAVID.T.RICKER

    = 287.875 kN > kN Safe

    2. Shear Capacity

    i. Shear Yielding (Ref. ANSI/AISC 360-05, J4-2a)

    fRn = f0.6fyAg= 403.92 kN > kN Safe

    ft Pn

    63

    63

    63

    63

    mm

    kN 63

    mm

  • 7/28/2019 Lug 0-5 ton Design

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    EVERSENDAI ENGINEERING W.L.L Sheet of

    PROJECT Job No Designed by

    DOHA CONVENTION CENTER & TOWER - QATAR

    Date Checked by

    SUBJECT TYPICAL LIFTING LUG DESIGN FOR 5 Tons 12.2.11

    Reference Code & Journal

    STV

    NVP

    SENDAI

    ii. Shear Rupture (Ref. ANSI/AISC 360-05, D5-1b)

    fPn = f 0.6 Fu Asf

    Asf = 2t ( a+ d/2 )

    = 2880 mm2

    Shear Rupture Capacity Pn = 531.36 kN

    Safe Working Capacity = Pn/1.8

    = 295.2 kN > kN Safe

    3. Bearing Capacity (Ref.Design and Construction of Lifting Beam by DAVID.T.RICKER)

    Pp = 0.9 Fy t d

    = 117.504

    Safe Working Capacity = Pp/1.8

    = 65.28 kN > kN Safe

    Provide washer 10 mm plates around the hole on both side of lug

    Therefore thickness of lug = 36

    Pp = 0.9 Fy t d

    = 264.384 kN

    Safe Working Capacity = Pp/1.8

    = 146.88 kN > Safe

    4. Flexural Capacity

    i. In-Plane Bending (Ref. ANSI/AISC 360-05, F1)

    Moment = P e

    = 4.6875 kN-m

    Moment Capacity = Z - Section Modulus

    Z = 107083 mm3

    Conservatively

    = 24.5756 kN-m > kN-m Safe

    ii. Out of Plane Bending (Ref. ANSI/AISC 360-05, F1)

    Moment = P e q - Angle for out of plane bending= 1.60322 kN-m q = degree Conservatively

    Moment Capacity = Z - Section Modulus

    Z = 236315 mm3

    Conservatively

    = 54.2344 kN-m > kN-m Safe

    5. Interaction Check

    =

    = 0.20011 < 1 Safe

    5

    2

    63

    70

    63

    63

    fb Mn fb Fy Z

    fb Mn fb Fy Z

    (T+M)2+R2

    mm

  • 7/28/2019 Lug 0-5 ton Design

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    EVERSENDAI ENGINEERING W.L.L Sheet of

    PROJECT Job No Designed by

    DOHA CONVENTION CENTER & TOWER - QATAR

    Date Checked by

    SUBJECT TYPICAL LIFTING LUG DESIGN FOR 5 Tons 12.2.11

    Reference Code & Journal

    STV

    NVP

    SENDAI

    II.CHECK FOR WELD

    1. Tensile Capacity

    fRnt = f 0.707w lw Fw s - Size of weld

    - Nominal Strength of weld

    = 740.653 kN > kN Safe

    2. Shear Capacity

    fRnu = f0.6 lw 0.707s Fw

    = 444.392 > kN Safe

    3. Flexural Capacity

    i. In-Plane Bending (Ref. ANSI/AISC 360-05, F1)

    Moment = P e

    = 4.6875 kN-m

    Z - Section Modulus

    Moment Capacity fb Mn = fb Fw Z Conservatively

    Z = 118452 mm3

    Moment Capacity = 31.0225 kN-m > kN-m Safe

    ii. Out of Plane Bending (Ref. ANSI/AISC 360-05, F1)

    Moment = P e q - Angle for out of plane bending= 1.60322 kN-m q = degree Conservatively

    Moment Capacity = Z - Section Modulus

    Z = 121166 mm3

    Conservatively

    Moment Capacity = 31.7333 kN-m > kN-m Safe

    5. Interaction Check

    =

    = 0.19488 < 1 Safe

    III.CHECK FOR SUPPORTING MEMBER

    Here the lifting lug designed typically to use for erection purpose. Beofre lifting suppprting member should be checkedfor local strength/buckling.

    70

    (T+M)2+R2

    2

    63

    5

    Fw

    63

    fb Mn fb Fy Z

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    DEE-SACKLE