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Effect of hot compressive deformation on the martensite transformation of Ti-10V-2Fe-3Al titanium alloy

机译:热压缩变形对Ti-10V-2Fe-3Al钛合金马氏体相变的影响

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摘要

The hot deformation behavior of as-cast TB6 alloy was investigated by isothermal hot compressive deformation from 800℃ to 1150℃ at the strain rates between 10~(-3)s~(-1) and 10s~(-1). The microstruc-tural evolution of martensite transformation of the deformed TB6 was observed, and the volume fraction of martensite was also studied. The results show that the deformation temperature plays an important role on the stress-induced martensite transformation for TB6 titanium alloy. When the strain rate is 0.001 s~(-1), 0.01 s~(-1),0.1 s~(-1),1 s~(-1), and 10 s~(-1), the deformation temperature with more martensite content is 900-975 ℃, 925-1050 ℃, 825-1100 ℃, 910-1000 ℃, and 925-1100 ℃, respectively.
机译:在10〜(-3)s〜(-1)至10s〜(-1)的应变速率下,通过800℃至1150℃的等温热压缩变形,研究了铸态TB6合金的热变形行为。观察了变形的TB6的马氏体相变的微观结构演变,并研究了马氏体的体积分数。结果表明,变形温度对TB6钛合金的应力诱发马氏体相变起着重要作用。当应变率为0.001 s〜(-1),0.01 s〜(-1),0.1 s〜(-1),1 s〜(-1)和10 s〜(-1)时,变形温度为马氏体含量分别为900-975℃,925-1050℃,825-1100℃,910-1000℃和925-1100℃。

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  • 来源
    《Materials Science and Engineering》 |2011年第2011期|p.591-601|共11页
  • 作者单位

    Titanium Alloys Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095, China;

    Titanium Alloys Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095, China;

    State Key Laboratory of Metal Matrix Composites, Shanghai Jiaotong University, Shanghai 200240, China;

    State Key Laboratory of Metal Matrix Composites, Shanghai Jiaotong University, Shanghai 200240, China;

    State Key Laboratory of Metal Matrix Composites, Shanghai Jiaotong University, Shanghai 200240, China;

    Institute of Commercial Aircraft Company, Shanghai 200120, China;

    Department of Materials Science and Engineering, Nanchang Hongkong University, Nanchang 330063, China;

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

    microanalysis; titanium alloys; martensitic transformations;

    机译:显微分析;钛合金;马氏体相变;

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