Near-tip strain ratchetting and crack growth at elevated temperature

被引:8
|
作者
Tong, J. [1 ]
Cornet, C. [1 ]
Lin, B. [1 ]
Lupton, C. [1 ]
Li, H. -Y. [2 ]
Bowen, P. [2 ]
Williams, S. [3 ]
Hardy, M. [3 ]
机构
[1] Univ Portsmouth, Sch Engn, Mech Behav Mat Grp, Portsmouth PO1 2UP, Hants, England
[2] Univ Birmingham, Birmingham B15 2TT, W Midlands, England
[3] Rolls Royce Plc, London, England
基金
英国工程与自然科学研究理事会;
关键词
Viscoplasticity; Ratchetting; Accumulated inelastic strain; Crack growth; Nickel-based superalloy; NICKEL-BASED SUPERALLOY; UNIFIED CONSTITUTIVE-EQUATIONS; CYCLIC PLASTICITY; INCONEL; 718; HOLD TIME; FATIGUE; VISCOPLASTICITY; BEHAVIOR; MODEL;
D O I
10.1016/j.ijfatigue.2015.09.006
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this work, we have extended our earlier work on the concept of ratchetting strain as a crack driving force (Tong et al., 2013), to examine the crack growth of a nickel-based superalloy at selected temperatures in vacuum under both fatigue and fatigue-creep loading conditions. The parameters of a unified constitutive model were calibrated against the material data obtained at selected temperatures from 550 to 775 degrees C, and a finite element model was developed to simulate the near-tip stress-strain responses under fatigue and creep-fatigue loading conditions at the experimental temperatures. Both ratchetting strain and accumulated inelastic strain near the crack tip were utilised in the prediction of the crack growth rates collected in vacuum. It seems that, although both ratchetting strain and accumulated inelastic strain correlate with the crack growth rates obtained under fatigue and fatigue-creep loading conditions, the predictions based on accumulated plastic strain are particularly close to the experimental results at all temperatures and loading conditions examined. This is the first time the concept of ratchetting strain has been used to predict the crack growth rates of an engineering alloy at elevated temperature in vacuum, where the influence of oxidation on crack growth is removed. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:514 / 520
页数:7
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