Fatigue reliability and sensitivity analysis of turbine disk with fuzzy failure status

Low-cycle fatigue is typical failure mode of aero-engine turbine disk, traditional reliability analysis method based on the binary state assumption has certain limitations for turbine disk reliability evaluation, because it doesn't consider the change of damage strength parameter caused by load...

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Bibliographic Details
Main Authors: Huang Xiaoyu, Wang Pan, Li Haihe, Zhang Zheng
Format: Article
Language:zho
Published: EDP Sciences 2021-12-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/full_html/2021/06/jnwpu2021396p1312/jnwpu2021396p1312.html