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发布时间 : 星期日 文章七、拉弯、压弯构件更新完毕开始阅读b5655bf2f90f76c661371ab4

?0.65?0.35N??M2M1??0.65?0.3580?10312?0.825

0.825?170?1063?txMx?yA?bW1x0.792?70.6?1022?1.0?0.98?1036.5?102

?14.3?138.1?152.4N/mm?f?215N/mm

070207250401、如图焊接工字形截面压弯杆,承受轴向力设计值800KN,杆件两端铰接并在中央有一侧向支承点,杆中央作用一横向集中荷载P,钢材为Q235–B·F,截面为b类,求保证杆件整体稳定的最大集中力P。已知:E?2.06?105N/mm2, f?215N/mm2,

?x?1.05,

?2?m?1.0fy235,

N?t?0.65?0.35M2M1,

NN?A???tM?bW?f,

?b?1.07?44000?,

?A??mM?)?W(1?0.8N/NE?f,

?A??mM?)W(1??N/NE?f

Q235轴压杆整体稳定系数(b类截面) λ ? 20 30 40 50 60 70 80 90 100 110 120 130 140 0.97 0.94 0.90 0.86 0.81 0.75 0.69 0.62 0.56 0.49 0.44 0.39 0.35 070207250400、解:①截面特性及内力 A=151.2cm2,Ix=133295.2cm4,Wx=3400.4cm3,ix=29.69cm,Iy=3125.0cm4,iy=4.55cm。(6) 构件跨中最大弯矩M?PL/4?2.5P,两端弯矩为0(1) ②弯矩作用平面内稳定

?x?loxix?2100029.7??33.67?????150(3) ?x?0.925(1)

??NEx?EA1.1?2x?2?2.06?105?151?10221.1?33.67?24637kN(2)

N?A???mxM?)?xW1x(1?0.8NNEX800?1032

1.0?2.5P?1060.925?151?10?1.05?3400.4?103?(1?0.8?80024637)89

?f?215

即57.28?0.72P?215 P?219.1kN(3) ③弯矩作用平面外稳定

?y?loyiy?5004.55?109.9(3) ?y?0.491(1)

2?b?1.07?109.944000?0.795(2)

?tx?0.65?0.35?N??02.5P?0.65(2)

32?txMx?yA?bW1x?800?100.491?151?10?1.0?0.65?2.5P?10630.795?3400.4?10?f?215

即107.9?0.6P?215 P?178.5kN(3) 因此最大集中力为Pmax=178.5kN

070207200400、试验算图示的构件“A”,其两端铰支,用I32a(A=67cm2, Wx=692cm3, ix=12.8cm, 截面对强轴X为a类,弱轴Y为b类)作成,Q235钢,承受均布荷载设计值q=28kN/m(使强轴受弯),设此构件上翼缘有刚性铺板连牢,不会产生弯扭屈曲,且截面无削弱。?m?1.0,?t?1.0,E?2.06?105N/mm2,

N?N?A??mxM?)?W(1?0.8N/NE?f,

?mM?)W(1??N/NE?A?f,

N?A???tM?bW?f

λ a类? b类? 20 30 40 50 60 70 80 90 100 110 120 0.98 0.96 0.94 0.92 0.88 0.84 0.78 0.71 0.64 0.56 0.49 0.97 0.94 0.90 0.86 0.81 0.75 0.69 0.62 0.56 0.49 0.44 070207200400、解:①构件“A”的内力计算 由于构件“A”在支座1处的竖向支座反力为承受轴心受压力为N?最大弯矩 M?18ql212ql,故

12?ql?tg60??18212?28?6?tg60??145kN

x?28?6?126kN?m

故知构件“A”为压弯构件。 ②截面验算 a.由于β

mx=1.0,且截面无削弱,故可不必验算强度

90

b.弯矩作用平面内的整体稳定验算

?x?600012.82?46.9,?x?0.924 ???NEx?EA1.1?x2?2?2.06?105?67?10221.1?46.9?5629.9kN

N?xA???mxM32x?)?xW1x(1?0.8N/NEx?

1.0?126?106145?100.924?67?101.05?692?1023?(1?0.8?145/5629.9)2

?23.49?177.06?200.6N/mm?f?215N/mm

c.因不会产生弯扭屈曲,故不必验算弯矩作用平面外的整体稳定。 d.刚度验算?x?46.9?????150

e.局部稳定不必验算,故图示构件“A”可安全承载。

070207200400、某三角形屋架的荷载如图,节点荷载作用下,节间最大正弯矩

M?2.246kN?m,上弦杆轴向力为N??322.86kN,采用2∟110×7,截面为b类,2A?30.39cm,ix?3.41cm,iy?4.86cm,Wx1?119.55cm,Wx2?44.09cm,钢材为33Q235,验算上弦杆的整体稳定。?m??t?0.85

?1x?1.05, ?2x?1.2, NE?2.06?10N/mm52,

?A??mM?)?W(1?0.8N/NE?f, N?A??mM?)W(1??N/NEfy/235

?f,

N?A???tM?bW?f,

NA??mM?)?W(1?1.25N/NE?f, ?b?1?0.0017?λ ? 20 30 40 50 60 70 80 90 100 110 120 130 140 0.97 0.94 0.90 0.86 0.81 0.75 0.69 0.62 0.56 0.49 0.44 0.39 0.35 070207200400、①弯矩作用平面内

?x?loxix?22123.41??62.17 ?x?0.797

??NEx?EA1.1?x2?2?2.06?105?67?10221.1?62.17?1453.3kN

91

N?xA???mxM32x?)?xW1x(1?0.8N/NEx?

0.85?2.246?106322.86?100.797?30.39?101.05?119.55?1023?(1?0.8?322.86/1453.3)2

?133.3?18.5?151.8N/mm?f?215N/mm

NA???mxM?x?2xW2x(1?1.25N/NEx)32

0.85?2.246?106322.86?1030.39?10?1.2?44.09?1023?(1?1.25?322.86/1453.3)2

?106.2?50?56.2N/mm?f?215N/mm

②弯矩作用平面外

loy?2?212?424cm, ?y?loyiy?4244.86?87.24, ??0.639

?b?1.0?0.0017?87.24?0.852

N?yA???txMx?bW1x?322.86?10320.639?30.39?102?1.0?0.85?2.246?10630.852?119.55?102

?166.3?18.7?185.0N/mm?f?215N/mm

070207200401、验算如图所示的天窗侧杆AB,两端铰接,承受轴向压力设计值为N=85.8kN,风荷载设计值q=2.87kN/m,钢材为Q235–B·F,杆件采用2∟100×80×7长肢相并,截面特征:A?24.6cm2, Ix?246cm4, ix?3.16cm,iy?3.46cm,Wx1?82cm3,

Wx2?35.1cm,截面无削弱,为b类:E?2.06?10N/mm352, ?mx?1.0, ?tx?1.0,

?mM?)?W(1?0.8N/NE?f?1xN?1.05,?2x?1.2, ?b?1?0.0017?Nfy235,

N?A??f,

?A??mM?)W(1??N/NE?f,

?A???tM?bW?f,

NA??mM?)?W(1?1.25N/NE

λ ? 20 30 40 50 60 70 80 90 100 110 120 130 140 0.97 0.94 0.90 0.86 0.81 0.75 0.69 0.62 0.56 0.49 0.44 0.39 0.35 92

070207200300