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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

Translated title of the contribution: Research on fatigue failure mechanism and life prediction method of FGH96 flat plate with a hole
  • Chengli Dong
  • , Jiangbo Fan
  • , Qiyu Lu
  • , Duoqi Shi
  • , Guangping Guo*
  • *Corresponding author for this work
  • Beijing Institute of Aeronautical Materials
  • Aero Engine Corporation of China
  • Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Translated title of the contributionResearch on fatigue failure mechanism and life prediction method of FGH96 flat plate with a hole
Original languageChinese (Traditional)
Pages (from-to)102-109
Number of pages8
JournalJournal of Aeronautical Materials
Volume45
Issue number2
DOIs
StatePublished - 1 Apr 2025

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