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Stochastic modeling of fatigue crack growth for bolt holes in turbine disc

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

科研成果: 期刊稿件文章同行评审

摘要

The stochastic fatigue crack growth (FCG) modeling method is established for bolt holes in the turbine disc. Through analyzing the FCG experimental of standard compact tension (CT) specimens, a Wiener process is firstly established based on the failure mechanism to describe the stochastic FCG process, and then extended to the component-like and component level. The accuracy of the established model is verified by the experiments of bolt hole plate (BHP) specimens. Finally, the reliability analysis framework is constructed and verified for the turbine disc with multiple cracks based on the Copula function.

源语言英语
文章编号107504
期刊International Journal of Fatigue
169
DOI
出版状态已出版 - 4月 2023

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