1499 Bridge NReq

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    2 14 2

    42,6

    1,4

    Cross-Section

    1) Draw a general layout

    (1)

    Example:The shown figure illustrated

    to :-

    2) Calculate dead and live loads forfor each element

    3) Design the stringer4) Design the cross-girder5) Design the main girder6) Calculate wind loads7) Ccalculate the internal forces in the

    bracing system

    Given steel used is St.52

    8) Design the bearing

    Solution1) General layout of Deck Bridge

    a simple span deck bridge. it is required

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    14

    Floor system

    2

    Sec.Elevation

    6

    6

    6

    6

    222222222

    1,4

    4

    36

    (2)

    6

    6

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    41

    Upper bracing Lower Bracing

    14

    36

    14

    (3)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    Cross-Section

    2

    2) Loads

    2-1) loads on stringer

    Dead loads

    WDL= o.w.t of stringer + o.w.t of R.c slab+ o.w.t

    of asphalt

    = 0.05+0.1x2.5x2+0.05x2.2x2=0.77 t/m

    2

    6

    WdL=0.77t/m

    (4)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    For New Loads ECP2008

    60

    40

    20

    15

    15

    15

    15

    10

    10

    10

    10

    5 5

    5 5

    0.5

    2

    1.2

    0.9t/m2

    0.25

    t/m2

    0.9t/m2

    0.25t/m2

    0.25t/m2

    0.2

    5t/m2

    0.25t/m2

    0.25t/m2

    If sidewalk width

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    Transverse direction2 14 2

    3 3 3

    15t 10t 5 t 5t15t 10t

    0.25 t/m 0.5 t/m0.5 t/m

    0.25 t/m0.5 t/m0.5 t/m 0.9 t/m

    Path I-I

    Path II-II

    A

    A

    I= 0.4-0.008x6=0.352

    15t10t

    15t

    A0.50

    2.00

    0.50 0.50

    2.00

    A0.50

    2.00

    1.0 1.0

    2.00

    0.9 t/m 0.2 5 t/m

    15t10t

    15t

    0.25

    1.0 0.75 0.25

    15t10t

    15t

    0.25

    1.0 0.75 0.25

    Ra=15x0.5/2+15x1.5/2)x1.352

    10x0.5/2=22.78 t

    Path I-I

    Path II-II

    Wa=(0.9x2x12+0.9x1x1.5/2)x1.352

    +0.25x1.0x0.5/2=2.192 t/m

    (6)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

    0.9 t/m

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    Longitudnal direction

    22.78 t 22.78 t2.192t/m2.192 t/m

    0.9 4.2

    0.9

    B.M.D

    55.44

    21.27

    21.27

    55.44

    22.78 t 22.78 t2.192 t/m

    6.00

    ML+I=54.34 t.m

    a b

    M@b=0.0

    Ra=(22.78x6+22.78x4.8+

    2.192x3.3x1.65)/6=42.99 t

    QL+I=42.99 t.m

    For maximum moment

    For maximum shear

    (7)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    Design of StringerProcedure to design the stringer:-

    1) Determine the straining actions MD+L+I,QD+L+I2) Assume section of stringer {I.P.E, S.I.B, HEA, HEB}

    3) Check bending stress. Pages (16-21) code ECP20014) Check shear stress. Pages (13-15)

    5) Check fatigue stress Pages (35-50)6) Check deflection. Page (132)

    GivenMD=0.77x6^2/8=3.465 t.m ML+I=54.34 t.m

    QD=0.77x6/2=2.31 t QD+L+I= 42.74 t

    assume: the depth of section= span/10=600/10= 60 cmchoose HEA 600

    h=590 mm bf=300 mm tf=25 mm d w=486 mm tw=13 mmr=27 mm Ix=141208 cm^4 Sx=4787 cm^3

    i) classification of sectionbf/2tf= 300/(2x25)=6 < 16.9/v3.6=8.9 compact flange

    dw/tw=486/13=37.38 < 127/v3.6=66.93 compact web

    section is compact section

    ii) check the laterally supported

    Lc = smaller from {20bf/vFyor 1380 Af. cb/(dFy)}

    = smallre from {316.23 cm or 487.3 cm)= 316.23 cm

    Lu= larger from {1380 Af. cb/(dFy) or 84rTv(cb/Fy)}

    = Larger from { 487.3 or 356.83}= 487.3 cm

    Luns = 600 cm > LuFltb1=800Af. cb/(Luns.d)=

    800x30x2.5x1/(600x59)=1.67 t/cm^2

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    Fltb2= [0.64-(Luns/rT

    )^2 Fy/117600. cb] Fy = [0.64-(74.44^2)x 3.6/117600 x 1)x 3.6=1.69 t/cm^2

    = 2.08 t/cm^2

    Fltb=v(Fltb1^2+Fltb2^2)=v(1.69^2+1.69^2)=2.39 t/cm^2

    = 2.08 t/cm^2

    Check bending

    fact= MD+L+I/Sx=57.8x 100/4787=1.21 t/cm^2 = 2.08 t/cm^2

    O.K

    Check shearFor unstiffened web

    dw/tw=486/13=37.38 < 105/v3.6=55.34

    qb=0.35Fy=1.26 t/cm^2

    q act= 45.05 /(48.6x1.3)=0.713 t/cm^2 < 1.26 t/cm^2 O.KCheck Fatigue

    Detail Category is Detail A, N=2000,000

    Fsr=1.68 t/cm^2Fmax= (M D+0.6ML+I)/Sx= 36.07 x 100/ 4787=0.753 t/cm^2

    Fmin = MD/Sx= 3.465x100/4787=0.072 t/cm^2

    Fmax-Fmin= 0.753-0.072=0.68 t/cm^2 < Fsr = 1.68 t/cm^2O.K

    Check Deflection

    dmax = dall= span/600=600/600= 1.0 cm

    dmax=d1+d2

    d1=(PL^3)[3a/4L-(a/L)^3]/6EI = 22.78x600^3x

    [3x90/4x600-(90/600)^3] /(6x2100x141208)= 0.3 cm

    d2= 2wa(3L^2-2a^2)/96EI

    = (2x2.192/100)x90x(3x600^2-2x90^2)

    /96x2100x141208=0.000147

    dmax=0.3+0.000127=0.300147 cm

    < span/600=1.0 cm

    22.78 t 22.78 t

    0.9 4.2 0.9

    2.192 t/m2.192 t/m

    0.9 4.2 0.9

    (9)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

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    Cross Girder1- Dead Loads

    M@mid-span

    M+ve=17.07x7-2.31x9-0.1x9x4.5-4.62x7-4.62x5-4.62x3

    -4.62x1=20.73 t.m

    Max Shear

    QD=17.07-2.31-0.1x2=14.56 t

    (10)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

    A

    4.624.624.624.624.624.62 2.312.31

    0.1 t/m

    17.07 t 17.07 t

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    2-Live LoadsTransverse Direction

    I=0.4-0.008X 2X 6=0.304RI=2X15X0.9X(1+0.304)=35.21 t

    RII=2X10X0.9 = 18 tRIII=2X5X0.9 = 9 tWI= 2X0.9X(0.5X3.9X0.65)X (1+0.304)=2.98 t/m

    WII=WIII= 2X0.25X (0.5 X3.9X0.65) = 0.634 t/m

    WIV=2X0.25X(0.5X6X1)=1.5 t/mWV=2X0.5X(0.5X6X1)=3 t/m

    (11)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

    14

    2

    6

    6

    6

    60 40 20

    15 15

    15

    10

    10

    10

    10

    5

    5

    5

    5

    0.5 2

    1.2

    0.9 t/m2 0.25 t/m2

    0.9 t/m2

    0.25 t/m2

    0.25 t/m20.25 t/m2

    0.25 t/m20.25 t/m2

    Ifsidewalkwidth

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    Longitudinal Direction

    R=35.2 x 2+18x2+2x9=124.4 t

    X=(35.2x2+18x3+18x5+9x6+9x8)/124.4=2.736 m

    For max.+ve Moment

    RA=1.5x[0.5x(1+0.705)x4.13]+2.98x[0.5x(0.705+0.491)x3]

    + 0.634x[0.5x(0.491+0.062)x6]+1.5x(0.5x0.87x0.062) +

    + 35.2x0.669+35.2x0.526 +18x0.455+18x0.312

    + 9x0.276+9x0.098=70.96 t

    M@ zero shearM+ve=70.96x6.63-1.5x4.13x(4.13/2+2.5)-2.98x2.5x1.25 -35.2x2=362.47 t.m

    For M-ve

    M-ve = (3x2^2)/2 = 6 m.t

    For max shear Qmax

    Qmax=RA= 3x{0.5x(1.143+1)x2}+2.98x{0.5x(1+0.786)x3}

    +0.634x {0.5x(0.786+0.357)x6}+1.5x(0.5x5x0.357)

    + 35.2x0.964+35.2x0.821+18x0.75+18x0.607 + 9x0.536 + 9x0.393=113.544 t

    (12)

    Lectures Notes (Steel III- CT225) by Dr. Essam Abdelaty Mohamed Amoush

    35.2 35.2 18 9 918

    2,74

    35.2 35.2 18 9 918

    124.4 t

    2,74

    5,63

    77

    6,63

    0,37

    124.4 t

    2 2

    4,13

    0,87

    1.50 t/m 2.98 t/m 0.634 t/m 1.5 t/m

    10.705

    0.669

    0.526

    0.491

    0.455

    0.312

    0.276

    0.098

    0.062

    I.L.RA

    A

    35.2 35.2 18 9 918

    5

    3 t/m 2.98 t/m0.634 t/m 1.5 t/m

    10.96

    4

    0.8

    21

    0.786

    0

    .750.607

    0.5360.393

    0.357

    1.143

    I.L.RA

    A 5,5

    8,5

    10,5

    1111,5

    13,5

    142

    7,5