Multiscale TRIP-based investigation of low-cycle fatigue of polycrystalline NiTi shape memory alloys

被引:53
作者
Zhang, Yahui [1 ,2 ]
Moumni, Ziad [1 ,2 ]
You, Yajun [1 ]
Zhang, Weihong [1 ]
Zhu, Jihong [1 ]
Anlas, Gunay [3 ]
机构
[1] Northwestern Polytech Univ, State IJR Ctr Aerosp Design & Addit Mfg, Xian 710072, Shaanxi, Peoples R China
[2] Univ Paris Saclay, ENSTA, IMSIA, UMR 8193,CNRS,EDF,CEA, 828 Blvd Marechaux, F-91762 Palaiseau, France
[3] Bogazici Univ, Dept Mech Engn, TR-34342 Istanbul, Turkey
基金
中国国家自然科学基金;
关键词
Shape memory alloys; Transformation induced plasticity (TRIP); Fatigue crack initiation; Low-cycle fatigue; Thermomechanical coupling; TRANSFORMATION-INDUCED PLASTICITY; STRUCTURAL FATIGUE; CONSTITUTIVE MODEL; MARTENSITIC-TRANSFORMATION; LOCALIZED DEFORMATION; MULTIAXIAL FATIGUE; LIFE-PREDICTION; SINGLE-CRYSTAL; STRESS; STRAIN;
D O I
10.1016/j.ijplas.2018.12.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, a multiscale investigation of fatigue crack initiation in shape memory alloys (SMAs) based on Transformation Induced Plasticity (TRIP) is presented. A mechanism for fatigue crack initiation during cyclic stress-induced phase transformation along with theoretical model is proposed. To validate the TRIP-based model, quasi-static tests at different ambient temperatures, 40 degrees C, 52 degrees C and 65 degrees C, and strain and stress controlled low-cycle fatigue tests at different frequencies ranging from 0.16 Hz to 5 Hz on pseudoelastic NiTi wires are carried out. The results show that, (i) TRIP appearing on phase transformation interfaces is the key factor that drives the fatigue crack initiation during cyclic stress-induced phase transformation in SMAs; (ii) maximum temperature during phase transformation is a relevant indicator to predict low-cycle fatigue of SMAs and, (iii) within the range of pseudoelasticity and below the plastic yield, low-cycle fatigue of SMAs is not directly correlated with the mechanical loads applied at macro-scale, in the sense that, if the maximum temperature reached during loading cycles is kept constant, the fatigue lifetime remains unchanged whatever the amplitude of the mechanical loading is. Based on the findings, a new criterion for pseudoelastic low-cycle fatigue of SMAs as well as fatigue-isolines diagram are proposed and validated experimentally.
引用
收藏
页码:307 / 329
页数:23
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