Creep-fatigue life prediction and interaction diagram in nickel-based GH4169 superalloy at 650 °C based on cycle-by-cycle concept

被引:92
|
作者
Wang, Run-Zi [1 ]
Zhang, Xian-Cheng [1 ]
Gong, Jian-Guo [1 ]
Zhu, Xu-Min [1 ]
Tu, Shan-Tung [1 ]
Zhang, Cheng-Cheng [2 ]
机构
[1] East China Univ Sci & Technol, Sch Mech & Power Engn, Key Lab Pressure Syst & Safety, Minist Educ, Meilong Rd 130, Shanghai 200237, Peoples R China
[2] AECC Commercial Aircraft Engine Co LTD, Shanghai Engn Res Ctr Commercial Aircraft Engine, Shanghai 201108, Peoples R China
基金
中国国家自然科学基金;
关键词
Creep-fatigue; Strain energy density; Cycle-by-cycle; Life prediction; Interaction diagram; HIGH-CHROMIUM STEELS; TYPE-347 WELD METAL; STAINLESS-STEEL; HOLD TIME; PART II; DAMAGE; ENERGY; TEMPERATURE; BEHAVIOR; DEFORMATION;
D O I
10.1016/j.ijfatigue.2016.11.021
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The purposes of the present work are to extend the previous energy-based model on the basis of strain energy density exhaustion and to estimate creep-fatigue endurance and accumulated damage using cycle-by-cycle concept in tension-hold-only tests. The nickel-based GH4169 superalloy at 650 degrees C is employed to fit material constants and to verify the prediction capacity of the present model under various loading conditions. The present model exhibits a higher accuracy than some existing models, especially for certain loading waveforms, where the half-life cycle cannot be considered as a representative one. In addition, the trajectory for time-dependent accumulated damage during the operating period can be monitored in the creep-fatigue interaction diagram. (C) 2016 Published by Elsevier Ltd.
引用
收藏
页码:114 / 123
页数:10
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