Experimental and numerical investigation of mixed-mode fatigue crack growth in nickel-based superalloy at high temperature

被引:13
作者
Xie, Qikun [1 ]
Qi, Hongyu [1 ,2 ]
Li, Shaolin [1 ,2 ]
Yang, Xiaoguang [1 ,2 ]
Shi, Duoqi [1 ,2 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Mixed-mode crack; Fatigue crack growth; Numerical investigation; High temperature; PROPAGATION; BEHAVIOR; SIMULATION; PREDICTION;
D O I
10.1016/j.engfracmech.2022.108736
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Fatigue cracking is one of the most common damage modes of aeroengine hot-end components, usually subjected to mixed-mode cracking. In this study, mixed-mode fatigue crack growth experiments at 550 ? are carried out using compact tension shear specimens made of nickel-based superalloy GH4169. Adaptive finite element method was used to verify several models at high temperature. The accuracy of angle dependent models was higher at 550 C, and the rate of da/dN increased and decreased twice with crack propagating, which is different from room temperature (20-25 C). This research could provide a basis for lifespan prediction of aeroengine hot -end components.
引用
收藏
页数:16
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