基于有限元分析的铝合金热变形损伤行为研究

    Study on Hot Deformation Damage Behavior of Aluminum Alloy Based on Finite Element Analysis

    • 摘要: 采用Gleeble-3500热模拟试验机对2024铝合金进行了变形温度为723 K、应变速率为1 s-1,不同压下量下的热模拟压缩试验,结合Deform 3D有限元软件对此变形条件下的材料热变形损伤参数进行了分析。试验过程中随着压下量的增加,试样鼓肚不断增大,最后发生开裂。模拟结果显示,随着加载压下量的增加,试样的等效应力值逐渐升高;损伤值也不断提高,主要分布在试样鼓肚位置,对比试验可以确定2024铝合金的损伤临界值在0.121~0.272。从应力三轴度分布结果可以发现,试样的开裂与拉应力状态的出现有关。

       

      Abstract: With Gleeble-3500 thermal simulation test system, the isothermal compression experiments of 2024 aluminum alloy were carried out under deformation temperature of 723 K, strain rate of 1 s-1 and different reductions. Combined with Deform 3D finite element software, the damage during deformation was studied. With the increase of the reduction, the drum belly of the specimen increases, finally it cracks. The simulation results show that with the increase of the reduction, the effective stress of the sample increases, and the damage rises, which is mainly distributed in the specimen drum belly. Comparing with the experimental results, the damage threshold of the alloy is between 0.121-0.272. From the distribution of stress triaxiality, it can be verified that the specimen cracking is associated with the presence of the tensile stress state.

       

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