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Investigation on the hot formability of TA15 titanium alloy sheet

机译:TA15钛合金薄板热成形性研究

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摘要

The hot formability of TA15 titanium alloy sheet was studied experimentally and theoretically. The hot uniaxial tensile tests were conducted for further investigation on hot formability. Based on the finite element models in different thermal conditions, the punch displacement-force curves were compared to test data to investigate the influence of sheet temperature distribution on limit strain. The simulation results indicated that the hot punch was essential for keeping the temperature of sheet center region. Meanwhile, the non-uniform sheet temperature distribution that the temperature of central sheet was higher than the one at sheet edge, was positive for making the damage occur at an appropriate region due to the good deformability of central sheet with higher temperature. The theoretical FLCs of TA15 titanium alloy sheet were predicted by introducing Hill48 yield criterion and temperature path into M-K model. The results proved that the monotonic decreasing temperature path had no effect on sheet formability, and the Nakazima test results depended on the final temperature of region at where the fracture or necking occurred. The comparison results also indicated that the test data agreed well with the theoretical FLC at 810 ℃.
机译:通过实验和理论研究了TA15钛合金薄板的热成形性。进行了热单轴拉伸试验,以进一步研究热成型性。基于不同热条件下的有限元模型,将冲头位移力曲线与测试数据进行比较,以研究板料温度分布对极限应变的影响。仿真结果表明,热冲压对于保持板材中心区域的温度至关重要。同时,由于中央片材具有较高的高温变形性,因此中央片材的温度高于片材边缘处的片材温度分布不均匀,有利于在适当区域发生损伤。通过将Hill48屈服准则和温度路径引入M-K模型,对TA15钛合金薄板的理论FLC进行了预测。结果证明,单调下降的温度路径对片材的成形性没有影响,中岛试验结果取决于发生断裂或颈缩的区域的最终温度。对比结果还表明,试验数据与810℃时的理论FLC吻合良好。

著录项

  • 来源
    《Materials & design》 |2016年第3期|9-16|共8页
  • 作者单位

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Forming limit curve; Sheet metal; TA15 titanium alloy; M-K model; Temperature;

    机译:成形极限曲线;钣金;TA15钛合金;M-K模型;温度;

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