Thermomechanical fatigue experiment and failure analysis on a nickel-based superalloy turbine blade

被引:44
|
作者
Wang, R. [1 ,2 ,3 ]
Zhang, B. [1 ]
Hu, D. [1 ,2 ,3 ]
Jiang, K. [4 ]
Liu, H. [1 ]
Mao, J. [1 ]
Jing, F. [5 ]
Hao, X. [1 ]
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
[3] Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
[4] Aero Engine Grp Corp China, Hunan Aviat Powerplant Res Inst, Zhuzhou 412002, Peoples R China
[5] Aero Engine Grp Corp China, Aero Engine Acad China, Beijing 101304, Peoples R China
基金
中国国家自然科学基金;
关键词
Thermomechanical fatigue; Nickel-based superalloy; Turbine blade; Failure analysis; Fractography; Metallography; THERMAL-MECHANICAL FATIGUE; CRYSTAL; CMSX-4; SPECIMENS; BEHAVIOR; TMF;
D O I
10.1016/j.engfailanal.2019.04.023
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Thermomechanical fatigue (TMF) experiment with dwell times on a nickel-based superalloy turbine blade was conducted. The strain field and temperature field of the test section were simulated well through adjusting gripping fixture and induction coil. In addition to the loading, heating, cooling and control subsystems, high temperature strain measurement subsystem was introduced into the experiment to ensure the accuracy of the simulation results of service condition for the test section. In the whole experiment, the service condition of the test section was reproduced. The experiment result showed that TMF crack initiated at the trailing edge of the test section and propagated along the leading edge direction. Using the scanning electron microscope (SEM), multiple crack sources at the surface of turbine blade were observed and the crack surface was oxidized seriously. In addition, based on the fractographic and metallographic observation, the mixed features of intergranular fracture and transgranular fracture were found. The interaction of oxidation, creep damage and fatigue damage is an important reason for the TMF failure of the turbine blade.
引用
收藏
页码:35 / 45
页数:11
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