钢结构第三章习题答案

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3-2 解: (1)

w

f w f N l f11

10.7h ×2=

(KN) 351540×0.65N 1== (mm) 1210×2.1max ==f h

mm)

(6.5145.15.11min ===t h f (mm) 1210×2.1max ==f h

取mm 10=f h

mm 7.156160

×10×0.7×210×3513

1

==w l (mm)

177 176.710×27.156211==+=+=f w h l l f f h h <177<608

(KN) 189540×35.02==N

)mm (6.5145.15.11min ===t h f )mm (89)2~1(10max 或=-=f h 取mm 8=f h

mm 47.105160

×8×0.7×210×8913

1

==w l mm 251 47.2118×247.105222取=+=+=f w h l l (2)

(KN) 163.968160×1.22×100×6×0.7×2h ×0.7×2f 3===w f f f b N β

)KN (016.2692163.968

-540×65.02311==-

∂=N N N

)KN (016.1072

163.968-540×35.02322==-

∂=N N N mm)(16.2001606×0.7×210016.2690.7h ×23

f111

=⨯⨯==w

f

w f N l (m m) 102206.16616.20011==+=+=f w h l l

mm)(625.791606×0.7×210016.1070.7h ×23

f221

=⨯⨯==w

f

w f N l (mm)90625.586625.7922==+=+=f w h l l

(1)

min max 112

2123

1.5 6.7

1.2 1.21416.810

540449.3540299.5||02

2170170210320449.310100.3220.710320f f f x y x w f x f e w f h mm h t mm h mm

N kN N N kN d d M N d kN m

l d d h mm N MPa

h l στ==≈==⨯===

=≈==

≈+=-==+-=+-⨯=⨯==≈⨯⨯⨯=取3

299.51066.9220.710320106160()10y

e w w

f f N MPa

h l MPa f MPa h mm

⨯=≈⨯⨯⨯=≈<=∴=合格 (2)

12234436

max

410,449.3

,299.5,320,160150190

||449.3|190|8.98622

1

20.71032038231012449.3108.98610320137.92220.7103203823102w f x y w f x z x w f e w z h mm N kN N kN l mm f MPa d d M N d kN m I mm N l M M h l I σ=====+-=-=⨯-==⨯

⨯⨯⨯≈⨯⨯⨯=+=+⨯≈⨯⨯⨯⨯3

299.51066.9220.710320131.3160()y

f e w w f Pa N MPa

h l MPa f MPa τ⨯==≈⨯⨯⨯=≈<=合格

)m KN (76.1112.098⋅=⨯==Fe M

)mm (1011)2~1(12max 2或=-=f h 取mm 102=f h )mm (1011)2~1(12max 3或=-=f h 取mm 103=f h

形心距腹板底端的距离X

)cm (674.1314

7.029.57.07.06.18285.20147.0)35.06.18(9.57.02)2/6.18(7.06.182=⨯+⨯⨯+⨯⨯⨯⨯++⨯⨯⨯+⨯⨯⨯=x

322240.718.62(13.6749.3)18.60.720.7 5.9 5.2760.77.1761983.505(cm )

12w I ⎡⎤

⨯=⨯+-⨯⨯+⨯⨯⨯+⨯=⎢⎥⎣⎦

w

f f <=⨯⨯⨯=)MPa (62.4426.7510

505.19831076.114

61σ w f f <=⨯⨯⨯=)MPa (072.8174.13610

505.19831076.1146max

σ )MPa (63.3710

7.0186210983

1=⨯⨯⨯⨯=τ

w f f f f <=+=+)MPa (367.7663.37)22

.1072.81()(

22

221τβσ 则2f f ,3f f 均满足要求。

弯矩主要由翼缘承担,剪力F 主要由腹板承担,焊缝1f f 基本不承担力,因此按构造配置。

)mm (1011)2~1(12max 1或=-=f h )mm (2.5125.15.11min ===t h f 取mm 101=f h

22443

1215,185,125,,0.12176

12612(176126)1761221321261217612

176

12612(176126132)17612(132)990.1102

12612(176126132)9374412612(w w w c t v z z z f MPa f MPa f MPa V F M e F F y mm

I mm S mm S ======⨯⨯+++⨯⨯=

≈⨯+⨯=⨯⨯++-+⨯⨯-≈⨯=⨯⨯++-==⨯⨯3

31max

4

6

114

633176132

176126132)12(176132)1053602

101053600.887125140.9990.11012

0.1210(1761212132)0.824185224.5990.1100.12109w z v z w t z z mm VS F F f MPa F kN I t M F h F f MPa F kN I M F h I τσσ-++-+⨯-⨯

=⨯⨯==≈≤=⇒≤⨯⨯⨯==⨯++-≈≤=⇒≤⨯⨯=

=4

6

4

34

132 1.6215134.490.1100.1210(176132)0.533990.11010937440.789990.11012

1.467 1.1 1.1185203.5138.7w

c z z z w t F f MPa F kN M F h F I VS F F I t F f MPa F kN

στ⨯≈≤=⇒≤⨯⨯==⨯-≈⨯⨯⨯==≈⨯⨯=≈<=⨯=⇒≤腹板上最靠近翼缘处的焊缝

max min{140.9,224.5,134.4,138.7}134.4F kN

∴==

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