TC2钛合金薄壁型材下陷成形工艺参数分析及优化
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中国航发北京航空材料研究院,北京 100095

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TG316.1

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航材院钛合金型材应用研究项目(KZ82171509)


Parameter Analysis and Optimization of Subsidence Deformation for Thin-walled TC2 Alloy Profiles
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AECC Beijing Institute of Aeronautical Materials,Beijing 100095

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    摘要:

    采用试验和计算机模拟相结合的方法,对TC2钛合金薄壁型材的单边下陷成形工艺开展研究。通过在室温至600 ℃范围内对TC2合金型材的热拉伸变形行为进行分析,建立了该型材热拉伸的Johnson-Cook本构模型。在此基础上,对L截面TC2钛合金型材的单边下陷过程进行计算机模拟,分析了下陷过程中型材应力、应力三轴度的分布。结果表明,下陷区L拐角处容易产生应力集中,由于变形前段该区域的应力三轴度Rd>0,呈拉应力状态,因此微裂纹容易在应力集中处形核并沿型材纵向扩展。通过对成形温度、下陷段长度和过渡圆角半径进行优化,得到最佳工艺参数条件为成形温度300 ℃,下陷区长度21 mm,过渡圆角半径49 mm。

    Abstract:

    In this paper, the subsidence deformation processing of the thin-walled TC2 alloy profile was studied by thermal tensile tests and computer simulations. First, the hot tensile deformation behavior of the TC2 alloy profile was analyzed in the temperature range from room temperature to 600 ℃. Then, Johnson-Cook constitutive model was used to describe the hot tensile deformation behavior. Through computer simulations, the distributions of stress and stress triaxiality during subsidence deformation were analyzed. The results show that stress concentration is easy to occur at the corner of L in the subsidence area, and it is tensile stress due to the stress triaxial Rd>0 of the area before deformation. With the increasing deformation, the crack extends in lengthwise direction of the profile. By optimizing the forming temperature, the length of the subsidence area and the transition radius, the best subsidence deformation processing parameters for the TC2 alloy profile are deformation temperature is 300 ℃, length of subsidence deformation zone is 21 mm, interim fillet radius is 49 mm.

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张明杰,齐立春,黄利军,李雪飞,吴泽浩. TC2钛合金薄壁型材下陷成形工艺参数分析及优化[J].宇航材料工艺,2023,53(1):43-49.

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  • 收稿日期:2022-01-20
  • 最后修改日期:2023-02-20
  • 录用日期:2022-04-22
  • 在线发布日期: 2023-03-29
  • 出版日期:
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

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