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    考虑焊接残余变形的动车组车顶稳定性分析

    Electric Multiple Unit Roof Stability Analysis Considering Welding Residual Deformation

    • 摘要: 根据某动车组车顶部件典型连接形式,制备对接、搭接和角接3种熔化极活性气体保护电弧焊接头,分别基于热弹塑性法和温度载荷法建立有限元模型,对接头焊接变形进行模拟及验证;在300 kN载荷下模拟计算了考虑和未考虑焊接变形的车顶屈曲变形,分析了车顶稳定性。结果表明:热弹塑性法和温度载荷法模拟得到3种接头最大角变形与试验结果的相对误差均小于5%;两模型预测焊接变形的准确性均较高。与热弹塑性法相比,温度载荷法的网格数量和计算时间均减少了90%以上,故选择温度载荷法进行车顶稳定性分析。基于子模型计算,未考虑焊接变形时车顶一阶屈曲因子为2.494,大于安全系数(1.5),说明不存在焊接变形时,300 kN载荷下车顶未发生失稳;考虑焊接变形时一阶屈曲因子为1.131,说明结构中存在焊接变形时300 kN载荷下发生失稳。

       

      Abstract: According to the typical connection form of the roof components of a certain electric multiple unit, three typical fusion-active gas shielded arc welding joints including butt joint, lap joint and fillet joint were prepared. Finite element models were established based on the thermal elastoplastic method and the temperature load method respectively to simulated and verify the welding deformation of the joints. The buckling deformation of the roof under a load of 300 kN was simulated and calculated considering and not considering the welding residual deformation, and the stability of the roof was analyzed. The results show that relative errors between the maximum angular deformation of the three joints simulated by the thermo-plasticity method and the temperature load method and the experimental results were all less than 5%. The accuracy of the welding deformation predicted by the two models was both relatively high. Compared with the thermal elastoplastic method, the temperature load method reduced the number of meshes and calculation time by more than 90%, so the temperature load method was selected for the stability analysis of the roof. According to the sub-model calculation, the first-order buckling factor of the roof without considering the welding deformation was 2.494, which was greater than the safety factor (1.5), indicating that the roof did not lose stability under a load of 300 kN without welding deformation. When considering the welding deformation, the first-order buckling factor was 1.131, indicating that the roof lost stability under a load of 300 kN when there was welding deformation.

       

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