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High cycle fatigue life prediction on TC4 titanium alloy after overload treatment

  • Beihang University
  • Beijing Key Laboratory of Aero-Engine Structure and Strength
  • United Research Center of Mid-Small Aero-Engine
  • Aero Engine Corporation of China

科研成果: 期刊稿件文章同行评审

摘要

In this study, single edge notched specimens of TC4 titanium alloy are overloaded and then employed to perform high cycle fatigue tests. It is shown that overload treatment has a significant improvement on fatigue life, with a range of 2.28–2.81 times increase. Considering the theory of critical distance brings relatively big error, a critical distance method modified by high stress zone is proposed to describe the difference both in high stress zone and critical distance after overload treatment. The scatter factor is improved from 4.0 to 3.0 without introducing additional parameters, demonstrating a higher accuracy of the proposed model.

源语言英语
文章编号107095
期刊International Journal of Fatigue
163
DOI
出版状态已出版 - 10月 2022

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