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8/12/2019 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
8/12/2019 1499 Bridge NReq
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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