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汪洪峰, 汪建利, 左敦稳, 宋娓娓, 段杏林. 航空铝合金板材搅拌摩擦连接有限元分析[J]. 焊接学报, 2014, 35(5): 21-25.
引用本文: 汪洪峰, 汪建利, 左敦稳, 宋娓娓, 段杏林. 航空铝合金板材搅拌摩擦连接有限元分析[J]. 焊接学报, 2014, 35(5): 21-25.
WANG Hongfeng, WANG Jianli, ZUO Dunwen, SONG Weiwei, DUAN Xinglin. Finite element analysis on friction stir welding of aviation aluminum alloy plate[J]. TRANSACTIONS OF THE CHINA WELDING INSTITUTION, 2014, 35(5): 21-25.
Citation: WANG Hongfeng, WANG Jianli, ZUO Dunwen, SONG Weiwei, DUAN Xinglin. Finite element analysis on friction stir welding of aviation aluminum alloy plate[J]. TRANSACTIONS OF THE CHINA WELDING INSTITUTION, 2014, 35(5): 21-25.

航空铝合金板材搅拌摩擦连接有限元分析

Finite element analysis on friction stir welding of aviation aluminum alloy plate

  • 摘要: 根据搅拌摩擦连接特点,充分考虑搅拌摩擦连接过程中搅拌针各部位与连接板材之间的摩擦生热及在连接过程中连接板材摩擦系数随温度变化规律,建立了适合搅拌摩擦连接自身特点的动态热元模型,并利用此模型进行了航空铝合金板材搅拌摩擦连接过程的有限元分析模拟.通过模拟结果和试验结果对比验证了所建立的动态热源模型和有限元分析过程是合理的.模拟结果显示搅拌摩擦连接残余拉应力主要集中在连接区,且在连接区中间位置出现最大残余拉应力区,连接区两端及其它部位出现残余压应力.

     

    Abstract: According to characteristics of friction stir welding,the dynamic heat source model for characteristics of friction stir welding process has been established based on fully considering the friction generating heat between the each parts of the tool and the joining plate,and joining plate friction coefficient with the temperature changing law in the friction stir welding process. By which finite element simulation has been studied for friction stir welding of aviation aluminum alloy sheet. By comparison with simulation results and test results,it could be verified that the established dynamic heat source model and finite element analysis process are reasonable. The simulation results show that the friction stir welding residual tensile stress is concentrated in the joint region,the maximum residual tensile stress appears in the middle of the joint region,and the residual compressive stress appears at the both ends in the joint region and other areas.

     

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