帽子出入口5.计算结果

1、 midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B400 x10号:100) (型钢 B:midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B400 x10号:100) (型钢 B:y截面名构件长2. 截面轴弯端部弯高腹 板 厚 翼 缘 宽400.000 上 翼 缘 厚 度 腹 板 中 心 390.000 下 翼 缘 厚 度 Fxx=-116.59(LCB:My=-4241.3, Mz = -面 Myi=-5054.8,Myj=-4241.3(forLb) Myi=-5054.8,Myj=-4241.3(for

2、Ly) Mzi=29943.0,Mzj=-32304(forFyy =19.1602 (LCB: 剪力Fzz=-5.9316 (LCB:3. 设计长计算长度系等效弯矩系Ly=3486.51, Lz =3486.51, Lb =Ky = 2.00, Kz = Beta_my= 0.85, Beta_mz= 4. KL/r = 44.1 150.0 (Memb:146,LCB: N/Nrc = 116.59/2957.85=0.039My/Mry = 4241/425399=0.010Mz/Mrz = 32304/425399=0.076整体稳定验算 (压缩+弯曲 Rmax = MAX Rmax1

3、, Rmax2, Rmax3 = 0.120 1.000Vy/Vry =0.023Vz/Vrz =0.007M ing, egrated Design &ysisSoftware Gen Pr Date/Time : 12/09/2013 ProjectFile midas GeSteel Checking z1. 设计设计规体系材料:Q235 (号(midas GeSteel Checking z1. 设计设计规体系材料:Q235 (号(型钢 P:y截面名构件长2. 截面轴弯端部弯外壁Fxx=-164.68(LCB:My=6863.19, Mz =面 Myi=-5146.6,Myj=-211

4、36(forLb) Myi=-5146.6,Myj=-3237.7(forLy) Fyy=7.27648 (LCB: 剪力Fzz=12.3263 (LCB: 3. 设计长计算长度系等效弯矩系Ly=10723.0, Lz =10723.0, Lb =Ky = 1.00, Kz = Beta_my= 1.00, Beta_mz= 4. =177.4200.0(Memb:31,LCB: N/Nrc =164.680/755.674=0.218My/Mry = 6863/103845=0.066Mz/Mrz 整体稳定验算 (压缩+弯曲Rmax = Rmax1 = 0.286 Vy/Vry =0.011

5、Vz/Vrz =0.019M ing, egrated Design &ysisSoftware Gen Date/Time : 12/09/2013 ProjectFile midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 260 x180 x10 (号:10) (型钢B260 x180 x10).:y截面midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 260 x180 x10 (号:10) (型钢B260 x180 x10).:y截面名构件长2. 截面轴弯端部弯高腹 板 厚 翼 缘 宽180.000

6、上 翼 缘 厚 度 腹 板 中 心 170.000 下 翼 缘 厚 度 Fxx=-38.171(LCB: My= -20038, Mz =Myi=-12666,Myj=0.00000(forLb) Myi= -12666, Myj= -21121 (forLy) Fyy =11.7707 (LCB: 面 剪力Fzz=-24.653 (LCB: 3. 设计长计算长度系等效弯矩系Ly=7284.00, Lz =7284.00, Lb =Ky = 1.00, Kz = Beta_my= 1.00, Beta_mz= 4. KL/r =119.9 150.0 (Memb:1,LCB: N/Nrc =

7、38.171/948.677=0.040My/Mry = 20038/121690=0.165Mz/Mrz = 7454.7/99760.0=0.075整体稳定验算 (压缩+弯曲 Rmax = MAX Rmax1, Rmax2, Rmax3 = 0.250 1.000Vy/Vry =0.032Vz/Vrz =0.049M ing, egrated Design &ysisSoftware Gen Pr Date/Time : 12/09/2013 ProjectFile midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号HW200 x200 x8/12

8、(号:30) (HW200 x200 x8/12).:y截面名构件midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号HW200 x200 x8/12 (号:30) (HW200 x200 x8/12).:y截面名构件长2. 截面轴弯端部弯高腹 板 厚 上 翼 缘 宽 度 200.000上 翼 缘 厚 度 下 翼 缘 宽 度 200.000下 翼 缘 厚 度 Fxx=22.2375 (LCB: My=1535.39, Mz =Myi=0.00000,Myj=0.00000(forLb) Myi=0.00000,Myj=0.00000(forLy) Mzi=

9、0.00000,Mzj=0.00000(forFyy =0.00000 (LCB: 面 剪力Fzz=1.49336 (LCB: 3. 设计长计算长度系等效弯矩系Ly=4112.56, Lz =4112.56, Lb =Ky = 1.00, Kz = Beta_my= 1.00, Beta_mz= 4. =84.4150.0 (Memb:289,LCB:N/Nrt = 22.24/1365.89=0.016My/Mry = 1535/101480=0.015Mz/Mrz = 0.0/34400.0=0.000整体稳定验算 Rmax = Rmax1 = 0.031 Vy/Vry =0.000Vz/

10、Vrz =0.008M ing, egrated Design &ysisSoftware Gen Date/Time : 12/09/2013 ProjectFile midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 400 x250 x12 (号:31) (型钢B400 x250 x12).:y截面名构件midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 400 x250 x12 (号:31) (型钢B400 x250 x12).:y截面名构件长2. 截面轴弯端部弯高腹 板 厚 翼 缘 宽250.000

11、上 翼 缘 厚 度 腹 板 中 心 238.000 下 翼 缘 厚 度 Fxx=30.2868 (LCB: My=21443.6, Mz =-面 Myi= -34805,Myj= -34805 (forLb) Myi= -34805, Myj= -34805 (forMzi=-5033.2,Mzj=-5033.2(forFyy =-41.016 (LCB: Fzz=-61.277 (LCB: 剪力3. 设计长计算长度系等效弯矩系Ly=4000.00, Lz =4000.00, Lb =Ky = 1.00, Kz = Beta_my= 1.00, Beta_mz= 4. =39.2150.0 (

12、Memb:143,LCB:N/Nrt = 30.29/3096.00=0.010My/Mry = 21444/330670=0.065Mz/Mrz = 5033/257355=0.020整体稳定验算 Rmax = Rmax1 = 0.090 Vy/Vry =0.066Vz/Vrz =0.067M ing, egrated Design &ysisSoftware Gen Date/Time : 12/09/2013 ProjectFile midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 200 x120 x8 (号:32) (型钢B200 x120

13、 x8).:y截面名midas GeSteel Checking z1. 设计设计规范体系材料:Q235 (号B 200 x120 x8 (号:32) (型钢B200 x120 x8).:y截面名构件长2. 截面轴弯端部弯高腹 板 厚 翼 缘 宽120.000 上 翼 缘 厚 度 腹 板 中 心 112.000 下 翼 缘 厚 度 Fxx=-87.563(LCB:My=11457.6, Mz =-面 Myi=10262.7,Myj=11483.6(forLb) Mzi=-1843.7,Mzj=-2047.3 (forFyy =1.39788 (LCB: 剪力Fzz=-8.7080 (LCB: 3. 设计长计算长度系等效弯矩系Ly=5144.80, Lz =5144.80, Lb =Ky = 1.00, Kz = Beta_my= 1.00, Beta_mz= 4. KL/r =108.2150.0 (Memb:286,LCB: N/Nrc =