Transition from internal to surface crack initiation of a single-crystal superalloy in the very-high-cycle fatigue regime at 1100 °C

被引:36
|
作者
Zhao, Z. [1 ]
Li, Q. [2 ]
Zhang, F. [2 ]
Xu, W. [3 ]
Chen, B. [4 ]
机构
[1] Beihang Univ, Sch Mat Sci & Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[3] Beijing Inst Aeronaut Mat, Beijing 100095, Peoples R China
[4] Univ Leicester, Sch Engn, Leicester LE1 7RH, Leics, England
基金
英国工程与自然科学研究理事会; 中国国家自然科学基金;
关键词
High-temperature fatigue; Very high cycle fatigue; Oxidation; Single crystal; Ni-base superalloy; HIGH-TEMPERATURE FATIGUE; NICKEL-BASED SUPERALLOY; BASE SUPERALLOY; DYNAMIC EMBRITTLEMENT; MECHANICAL-PROPERTIES; NI; OXIDATION; GROWTH; MICROSTRUCTURE; BEHAVIOR;
D O I
10.1016/j.ijfatigue.2021.106343
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Transition from internal to surface crack initiation is controlled by oxidation assisted fatigue-crack process in the very-high-cycle fatigue regime. Between 760 and 1000 degrees C, single crack initiation site is associated with internal casting defect, followed by a crystallographic Stage I propagation. By contrast, multiple surface crack initiation sites appear at 1100 degrees C, as the consequence of internal oxide penetration. The fatal crack follows a Mode I propagation and oxygen can diffuse into the material along the crack path. gamma'-phase depletion appears surrounding the oxidised and cracked regions, while localised rafting can occur close to the crack tip.
引用
收藏
页数:14
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