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FGH96 合金带孔平板疲劳失效机理及寿命预测方法研究

  • Chengli Dong
  • , Jiangbo Fan
  • , Qiyu Lu
  • , Duoqi Shi
  • , Guangping Guo*
  • *此作品的通讯作者
  • Beijing Institute of Aeronautical Materials
  • Aero Engine Corporation of China
  • Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

Fatigue tests were conducted on FGH96 flat plates containing a hole at 600 ℃. Utilizing a viscoplastic constitutive model, the stress and plastic strain distributions within these plates were meticulously calculated. Scanning electron microscopy (SEM) was employed to analyze the fatigue failure mechanism. Based on SEM observations and the geometric attributes of the FGH96 plates with holes, the critical fatigue damage and stress concentration coefficient were defined. Subsequently, the CDM (cumulative damage model) was refined accordingly. The findings revealed that, in comparison to conventional fatigue life prediction techniques, the revised CDM model, which incorporates critical fatigue damage and stress concentration coefficients, exhibited enhanced prediction accuracy for the fatigue life of FGH96 flat plates with holes. Notably, all prediction results fell within a ±2 error band.

投稿的翻译标题Research on fatigue failure mechanism and life prediction method of FGH96 flat plate with a hole
源语言繁体中文
页(从-至)102-109
页数8
期刊Journal of Aeronautical Materials
45
2
DOI
出版状态已出版 - 1 4月 2025

关键词

  • cumulative damage model
  • failure mechanism
  • fatigue
  • flat plate with a hole
  • life prediction

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