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Fatigue life dispersity and distribution characteristics of laser direct energy deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy

  • Beihang University
  • Beijing Institute of Aeronautical Materials

科研成果: 期刊稿件文章同行评审

摘要

Additive manufactured titanium alloys exhibit distinct microstructures and internal defects compared to forged alloys. This has a significant impact on its fatigue failure behavior and fatigue life distribution. Fatigue life dispersity and distribution characteristics of laser direct energy deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy were investigated by a relatively large sample fatigue test, fracture morphology characterization, and statistical analytic method. Then, the intrinsic causes of fatigue life dispersity and distribution characteristics were clarified by correlating with fatigue failure origin modes (FFOMs). The test and analysis results indicate that the existence of internal pores significantly influences FFOMs, fatigue life dispersity, and distribution pattern. The FFOMs of microstructure and interior pores have little effect on fatigue life dispersion. In contrast, FFOMs of surface and subsurface pores present a relatively lower fatigue life and are responsible for fatigue life dispersion. Besides, two competitive effects of FFOMs with different applied stress highly affect fatigue life distribution. A bimodal Weibull model is more suitable for describing fatigue life distribution with multiple FFOMs. However, if there is no fast-computing procedure for the parameter estimation of the Bimodal Weibull model, relatively conservative and simple P-S-N curves based on the Weibull distribution model are recommended in engineering applications.

源语言英语
文章编号103514
期刊Chinese Journal of Aeronautics
38
6
DOI
出版状态已出版 - 6月 2025

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