In-situ SEM and EBSD study on fretting fatigue crack initiation of a directionally solidified Ni-based superalloy

被引:11
|
作者
Han, Qinan [1 ]
Wang, Wei [1 ]
Fang, Jianwen [1 ]
Cui, Haitao [1 ]
Zhang, Hongjian [1 ]
Yang, Xiaolin [1 ,2 ]
Mu, Qinqin [2 ]
Xu, Jian [2 ]
Shi, Huiji [3 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Informat Technol Coll Energy & Power Engn, Aeroengine Thermal Environm & Struct Key Lab, Minist Ind, Nanjing 210016, Peoples R China
[2] Aircraft Strength Res Inst China, Xian 710065, Peoples R China
[3] Tsinghua Univ, Dept Engn Mech, AML, Beijing 100084, Peoples R China
关键词
Fretting fatigue; In-situ SEM; Crack initiation; EBSD; Superalloy; DISLOCATION DENSITY; SLIP; ORIENTATION; TEMPERATURE; FREQUENCY; BEHAVIOR; NICKEL; FORCE; SIZE;
D O I
10.1016/j.ijfatigue.2022.106908
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Fretting fatigue is an important cause of the failure of the turbine blade-disc dovetail joint in aero-engines. In this work in-situ scanning electron microscope (SEM) fretting fatigue experiments using dovetail shape specimens were conducted. The fretting fatigue damage process of Ni-based directionally solidified superalloys including slip trace evolution and crack initiation was captured. The misorientation and geometrically necessary dislocation (GND) density induced by fretting fatigue were quantified by electron back-scattered diffraction (EBSD). The significant correlation between crack path, slip trace, grain boundary microstructure and GND density was revealed. The EBSD analysis achieved good agreement with the in-situ SEM observation.
引用
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页数:12
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