ecpisd v(r4.3)-c2

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    Job No. Building No. REACTOR Rev.No. 01

    Project I.D. GREEN EGYPT Date: 9/2011

    Description XIS 2-LEVEL 5 Designed By: TAMER

    R 0.782 Checked By: dr.mohamd

    DESIGN OF STEEL RAFTER

    APPLIED FORCES

    Mx 1100.0(t.cm) My 0 (t.cm)

    N -5.000 (ton) Side sway permited yes

    Qy 8.08 (ton)

    0

    SECTION DIMENSION (in cm)

    bft 20 st 37 wind no

    bfb 20

    tsu 0.8 Cb 1.750 FY 2.4

    tsb 0.8T used in stiffness calculation 42.0Bw 0.6 Cmx 0.85

    K 0 Always enter K=0

    T 62

    MEMBER LENGTH 600.0 Cmy 0.85

    SECTION PROPERTIES

    Yb 31 (cm)

    Ix 40982.67 (cm4) area 68.24 (cm2)

    Ix For Stiffness 22502.19 (cm4)

    Iy 1067.75 (cm4)

    Iy For Stiffness 1067.39 (cm4)

    ix 20 (cm2) iy 4.36 (cm2)

    Zy 106.78 (cm3)

    AF 16 (cm2) d 60.4 (cm)

    RT 4.92 (cm)

    ALLOWABLE STRESSES IN COMPRESSION

    Lu 300

    3.6.5.2

    Lu/RT 60.963

    Fltb1 800.Af/(Lu.T).Cb 1.21 (t/cm2)

    Fltb2 0.58FY 1.39 (t/cm2)

    3.6.5.2-(I)

    Fltb2 1.432 (t/cm2)

    3.6.5.2-(II)

    Fltb2 12000/(Lu/RT)2.Cb 5.650 (t/cm2)

    3.6.5.2-(III)

    Fltb 1.392 (t/cm2)

    Province.No.

    (0.60-(Lu/RT)2.Fy/(1.176X10^5.Cb))Fy

    (Fltb12 + Fltb22)0.5

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    Job No. Building No. REACTOR Rev.No. 01

    Project I.D. GREEN EGYPT Date: 9/2011

    Description XIS 2-LEVEL 5 Designed By: TAMER

    R 0.782 Checked By: dr.mohamd

    CHECK ON STABILITY OF WEB 3.7.4

    -0.884 0.737

    0.545 -0.834

    dw/tw for Compact web 74.119 dw/tw for Non-compact web 105.20

    Non - Compact web

    16/(((1+)2+0.112(1)2)0.5+(1+)) 19.959

    0.793

    1.000

    be 32.93 cm bc 32.93 cm

    be1 13.17 cm bt 27.470 cm

    be2 19.76 cm em 0.0000 cm

    ybot 31.000 cm buckled part 0.0 cm

    Area buckled 0.00 cm2

    A gross 68.24 cm2

    I gross 40982.67 cm4

    A effective 68.240 cm2

    I effective 40982.67 cm4

    S effective top 1322.02 cm3

    S effective bottom 1322.02 cm3

    CHECK ON STABILITY OF FLANGE

    a) for Stffinned flanges

    Compact flange

    b) For Unstffinned flanges ( assuming that the outstanding part of flange is totally in compression)

    Non-Compact flange Comp. Flange (top Flange) In case Bot Flange in Comp.

    0.43 0.43

    0.65 0.65103

    1 1

    be 20.00 cm 20.00

    FLANGE BUCKED AREA 0.00 cm2 0.000

    Yb 31.00 cm

    EM 0.000 cm

    A gross 68.24 cm2

    I gross 40982.67 cm4

    A effective 68.24 cm2

    I effective 40982.67 cm4

    S effective top 1322.022 cm3

    S effective bottom 1322.022 cm4

    CHECK ON STRESSES

    Fca (actual compressive stress due to axial load)

    Fca =N/A -0.073 (t/cm2)

    top bot

    K

    p b/t/44 * (fy/K)^0.5

    (p-0.15-0.05) / p^2

    K

    p b/t/44 * (fy/K)^0.5

    (p-0.15-0.05) / p^2

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    Job No. Building No. REACTOR Rev.No. 01

    Project I.D. GREEN EGYPT Date: 9/2011

    Description XIS 2-LEVEL 5 Designed By: TAMER

    R 0.782 Checked By: dr.mohamdGu 2 Kx 2.11

    Lx 1263.57 (cm) Ly 600(cm)

    63.17 137.71

    Fc 7500/ly^2 0.4 (t/cm2)

    Fbx (the bending stresses based on moments about the X-axis)

    Fbx-top=Mx/Zx -0.832 (t/cm2)

    Fbx-bot=Mx/Zx 0.832 (t/cm2)

    Fby (the bending stresses based on moments about the Y-axis)

    Fby-top=My/Zy 0.000 (t/cm2)

    Fby-bot=My/Zy 0.000 (t/cm2)

    Fbcx (the allowable bending stresses about the X-axis)

    A1 0.89 1 3.6.9.1

    Fbcx 1.392 (t/cm2)

    Fbcy (the allowable bending stresses about the Y-axis)

    A2 1.04 1.04 3.6.9.1

    Fbcy 1.39 (t/cm2)

    check on stresses top Fibers(compression)

    yeild equation Fca/(0.58.fy)+Fbx/Fbcx+Fby/Fbcy 0.650 3.6.9.1

    stability equation Fca/fc+(Fbx/Fbcx).A1+(Fby/Fbcy).A2 0.782 3.6.9.1

    check on stresses bot Fibers(tension)

    yeild equation Fca/(0.58.fy)+Fbx/Fbcx+Fby/Fbcy 0.545

    stability equation Fca/fc+(Fbx/Fbcx).A1+(Fby/Fbcy).A2 0.413

    check on shear stresses

    q(allowable) 0.64

    f(combined allowable) 1.39

    q 0.22 Safe 0.349

    f(combined) 0.9643Safe 0.693

    weld size bet. Web& flange 0.07

    x=Lx/ix y=Ly/iy

    Cmx/(1-fca/7500/(x2)) IF A1< 1 ,take A1 =

    Cmy/(1-fca/7500/(y2)) IF A2< 1 ,take A2 =

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    SECTION PROPERTIES SUMMARY

    150x150+6x6+web200x6

    Cb 1

    Lu 100 Lu 150

    Lx 100 Lx 100Ly 100 Ly 100

    lbx 11.4 lbx 11.4

    Lby 29.8 Lby 29.8

    Moment N.Comp Stress Ratio Moment N.Comp Stress Rat

    200 -1 0.68 200 -1 0.68

    200 -3 0.73 200 -3 0.73

    250 -1 0.85 250 -1 0.85

    250 -3 0.9 250 -3 0.9

    Lu 100 Lu 150

    Lx 150 Lx 150

    Ly 150 Ly 150

    lbx 17.1 lbx 17.1

    Lby 44.7 Lby 44.7

    Moment N.Comp tress Ratio Moment N.Comp tress Ratio

    200 -1 0.69 200 -1 0.69

    200 -3 0.74 200 -3 0.74

    250 -1 0.85 250 -1 0.85

    250 -3 0.9 250 -3 0.9

    Lu 100 Lu 150

    Lx 200 Lx 200

    Ly 200 Ly 200

    lbx 22.8 lbx 22.8

    Lby 59.6 Lby 59.6

    Moment N.Comp tress Ratio Moment N.Comp tress Ratio

    150 -4 0.61 150 -4 0.61

    200 -1 0.69 200 -1 0.69

    200 -3 0.75 200 -3 0.75250 -1 0.85 250 -1 0.85

    250 -3 0.91 250 -3 0.91

    Lu 100 Lu 150

    Lx 250 Lx 250

    Ly 250 Ly 250

    lbx 28.5 lbx 28.5

    Lby 74.5 Lby 74.5

    Moment N.Comp tress Ratio Moment N.Comp tress Ratio150 -4 0.62 150 -4 0.62

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    200 -1 0.69 200 -1 0.69

    200 -3 0.76 200 -3 0.76

    250 -1 0.86 250 -1 0.86

    250 -3 0.92 250 -3 0.92

    Lu 100 Lu 150

    Lx 300 Lx 300

    Ly 300 Ly 300

    lbx 34.2 lbx 34.2

    Lby 89.4 Lby 89.4

    Moment N.Comp tress Ratio Moment N.Comp tress Ratio

    150 -3 0.61 150 -3 0.61

    200 -1 0.7 200 -1 0.7

    200 -3 0.77 200 -3 0.77

    250 -1 0.86 250 -1 0.86

    250 -3 0.94 250 -3 0.94

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    Lu 200 Lu

    Lx 100 LxLy 100 Ly

    lbx 11.4 lbx

    Lby 29.8 Lby

    io Moment N.Comp Stress Ratio Moment

    200 -1 0.68 150

    200 -3 0.73 200

    250 -1 0.85 200

    250 -3 0.9 250

    250

    Lu 200

    Lx 150 Lu

    Ly 150 Lx

    lbx 17.1 Ly

    Lby 44.7 lbx

    Lby

    Moment N.Comp tress Ratio

    200 -1 0.69 Moment

    200 -3 0.74 150

    250 -1 0.85 200

    250 -3 0.9 200

    250250

    Lu 200

    Lx 200

    Ly 200 Lu

    lbx 22.8 Lx

    Lby 59.6 Ly

    lbx

    Moment N.Comp tress Ratio Lby

    150 -4 0.61

    200 -1 0.69 Moment

    200 -3 0.75 150250 -1 0.85 200

    250 -3 0.91 200

    250

    250

    Lu 200

    Lx 250

    Ly 250 Lu

    lbx 28.5 Lx

    Lby 74.5 Ly

    lbx

    Moment N.Comp tress Ratio Lby150 -4 0.62

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    200 -1 0.69 Moment

    200 -3 0.76 150

    250 -1 0.86 200

    250 -3 0.92 200

    250

    250

    Lu 200

    Lx 300

    Ly 300 Lu

    lbx 34.2 Lx

    Lby 89.4 Ly

    lbx

    Moment N.Comp tress Ratio Lby

    150 -3 0.61

    200 -1 0.7 Moment

    200 -3 0.77 150

    250 -1 0.86 200

    250 -3 0.94 200250

    250

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    250 Lu 300

    100 Lx 100100 Ly 100

    11.4 lbx 11.4

    29.8 Lby 29.8

    N.Comp Stress Ratio Moment N.Comp Stress Ratio

    -4 0.61 150 -2 0.6

    -1 0.7 200 -1 0.76

    -3 0.75 200 -3 0.81

    -1 0.87 250 -1 0.94

    -3 0.92 250 -3 0.99

    250 Lu 300

    150 Lx 150

    150 Ly 150

    17.1 lbx 17.1

    44.7 Lby 44.7

    N.Comp tress Ratio Moment N.Comp tress Ratio

    -4 0.61 150 -2 0.6

    -1 0.7 150 -4 0.66

    -3 0.75 200 -1 0.76

    -1 0.87 200 -3 0.81-3 0.92 250 -1 0.94

    250 -3 1

    250

    200 Lu 300

    200 Lx 200

    22.8 Ly 200

    59.6 lbx 22.8

    Lby 59.6

    N.Comp tress Ratio

    -4 0.62 Moment N.Comp tress Ratio-1 0.7 150 -2 0.61

    -3 0.76 150 -4 0.67

    -1 0.87 200 -1 0.76

    -3 0.93 200 -3 0.82

    250 -1 0.95

    250

    250 Lu 300

    250 Lx 250

    28.5 Ly 250

    74.5 lbx 28.5Lby 74.5

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    N.Comp tress Ratio

    -3 0.6 Moment N.Comp tress Ratio

    -1 0.71 150 -2 0.62

    -3 0.77 150 -4 0.68

    -1 0.88 200 -1 0.77

    -3 0.94 200 -3 0.83

    250 -1 0.95

    250

    300 Lu 300

    300 Lx 300

    34.2 Ly 300

    89.4 lbx 34.2

    Lby 89.4

    N.Comp tress Ratio

    -3 0.62 Moment N.Comp tress Ratio

    -1 0.71 150 -2 0.63

    -3 0.79 150 -4 0.7-1 0.88 200 -1 0.77

    -3 0.96 200 -3 0.85

    250 -1 0.96

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