Life prediction and damage analysis of creep-fatigue combined with high-low cycle loading by using a crystal plasticity-based approach

被引:18
作者
Li, Kai -Shang [1 ]
Wang, Run-Zi [1 ]
Xu, Le [2 ]
Zhang, Cheng-Cheng [3 ]
Xia, Xian-Xi [4 ]
Tang, Min-Jin [4 ]
Zhang, Guo-Dong [4 ]
Zhang, Xian-Cheng [1 ,5 ]
Tu, Shan-Tung [1 ]
机构
[1] East China Univ Sci & Technol, Key Lab Pressure Syst & Safety, Minist Educ, Shanghai 200237, Peoples R China
[2] Ritsumeikan Univ, Grad Sch Sci & Engn, 1-1-1 Nojihigashi, Kusatsu, Shiga 5258577, Japan
[3] AECC Commercial Aircraft Engine Co LTD, Shanghai Engn Res Ctr Commercial Aircraft Engine, Shanghai 201108, Peoples R China
[4] Suzhou Nucl Power Res Inst, Suzhou 215004, Peoples R China
[5] East China Univ Sci & Technol, Sch Mech & Power Engn, Key Lab Pressure Syst & Safety, Minist Educ, Meilong Rd 130, Shanghai 200237, Peoples R China
基金
中国国家自然科学基金;
关键词
Crystal plasticity; Creep-fatigue combined with high-low cycle; loading; Life prediction; Damage analysis; NICKEL-BASED SUPERALLOY; 650; DEGREES-C; CRACK INITIATION; ENERGY DENSITY; SLIP IRREVERSIBILITY; MARTENSITIC STEEL; GROWTH MECHANISMS; GRAIN-SIZE; DEFORMATION; BEHAVIOR;
D O I
10.1016/j.ijfatigue.2022.107154
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Many high-temperature rotating components are always subjected to complex loading waveforms, arising the concerns for multi-damage driving crack initiation. In this paper, a series of strain-controlled low cycle fatigue (LCF) and creep-fatigue interaction (CFI) tests as well as the novel creep-fatigue combined with high-low cycle (CF-HL) tests were performed in a nickel-based superalloy at 650 celcius. Then, post-test microstructure observations were carried out to reveal the damage mechanisms under the multi-damaged CF-HL loading based on the EBSD-TEM combinative characterizations. In this aspect, the single-slip-dominated deformation mechanism under CFI loadings transformed to double-slip-dominated one under CF-HL loading was revealed. Computationally, a nu-merical procedure with a combination of crystal plasticity theory and finite element implementation was con-structed for predicting the CF-HL crack initiation life and quantifying the crack initiation mechanisms. With the help of the developed fatigue and creep indicator parameters represented by accumulated energy dissipation, good agreements between experimental data and simulated results were achieved within a scatter band of & PLUSMN; 2 on life prediction. In addition, the simulation results indicate that the combined effects of grain orientation and multiple slip system activation showed great influence on the CF-HL crack initiation.
引用
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页数:16
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