Effect of dwell condition on fatigue behavior of a high-Nb TiAl alloy at 750 °C

被引:8
|
作者
Dong, Chengli [1 ]
Jiao, Zehui [1 ]
Yu, Huichen [1 ]
Zhou, Haitao [2 ]
Kong, Fantao [2 ]
Chen, Yuyong [2 ]
机构
[1] AECC Beijing Inst Aeronaut Mat, Sci & Technol Adv High Temp Struct Mat Lab, Beijing Key Lab Aeronaut Mat Testing & Evaluat, Aviat Key Lab Sci & Technol Aeronaut Mat Testing, Beijing 100095, Peoples R China
[2] Harbin Inst Technol, Sch Mat Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
关键词
High-Nb TiAl; Low cycle fatigue (LCF); Creep-fatigue interaction (CFI); Dwell condition; Continuum damage accumulation (CDA); LOW-CYCLE FATIGUE; MECHANICAL-PROPERTIES; TENSILE PROPERTIES; DAMAGE MECHANISM; STAINLESS-STEEL; CREEP; MICROSTRUCTURE; TEMPERATURE; TRANSFORMATION;
D O I
10.1016/j.intermet.2017.07.006
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The strain-controlled low cycle fatigue (LCF) and creep-fatigue interaction (CFI) tests of a newly developed Ti45A1-8Nb-0.2W-0.213-0.02Y (at.%) alloy were carried out at 750 C in air. The hysteresis loop, cyclic stress response and life modeling as well as failure mechanism of the alloy were investigated in detail. It was revealed that the tensile and compressive mean stresses would generate when the dwell condition was introduced at minimum and maximum strain, respectively. In addition, the dwell condition, especially for the compressive dwell condition, would significantly decrease the fatigue life. The typical continuum damage accumulation (CDA) and modified CDA life models proposed in the present study were employed to predict both LCF and CFI life of the alloy, which showed that the modified CDA life model had a higher accuracy than the typical CDA life one. Moreover, only single crack initiation source was observed at 92% (ie. 11/12) of LCF fracture while multiple crack initiation sources at 84% (ie. 31/37) of CFI fracture. Apparently different from LCF specimen showing more transgranular appearance, CFI specimen shows more intergranular appearance.
引用
收藏
页码:1 / 7
页数:7
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