The microstructure effect on fatigue and dwell-fatigue in a nickel-based superalloy

被引:2
作者
Peng, Zichao [1 ]
Zheng, Zebang [2 ]
Wang, Xuqing [1 ]
Zou, Jinwen [1 ]
机构
[1] Beijing Inst Aeronaut Mat, Sci & Technol Adv High Temp Struct Mat Lab, AECC, Beijing 100095, Peoples R China
[2] Northwestern Polytech Univ, Sch Mat Sci & Engn, State Key Lab Solidificat Proc, Shaanxi Key Lab High Performance Precis Forming T, Xian 710072, Peoples R China
关键词
Fatigue; Dwell-fatigue; gamma' precipitate; Fracture; NI-BASED SUPERALLOY; HIGH-TEMPERATURE; CRACK-GROWTH; TURBINE DISC; CREEP; BEHAVIOR; DEFORMATION; PROPAGATION; STRENGTH; OXYGEN;
D O I
10.1016/j.intermet.2022.107740
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
In this study, the fatigue behaviors of a nickel-based superalloy FGH96 with different microstructural morphologies generated from different heat-treatment processes were investigated. The fatigue and dwell-fatigue tests with the same maximum stress of 1200 MPa were conducted at 650 degrees C. The relationship between the gamma' morphology and the fatigue properties was established. The results indicate that the critical shearing stress of dislocation movement played a key role in affecting fatigue life. No apparent difference can be observed from the fracture morphology at the macroscopic scale for normal fatigue and dwell-fatigue tests. However, in the crack initiation region, the crack was observed to grow along the grain boundary for the dwell-fatigue condition, resulting in the intergranular fracture, similar to creep failure. The introduction of dwell time in the fatigue loading brings larger cyclic strain deformation originates from massive dislocation slip. The dwell debit for the considered loading condition is about 100 times.
引用
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页数:8
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