退火温度对Ti-51.1Ni形状记忆合金超弹性的影响
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  • 英文篇名:Effect of annealing temperature on superelasticity of Ti-51. 1Ni shape memory alloy
  • 作者:冯辉 ; 贺志荣 ; 王芳 ; 刘康凯 ; 杜雨青
  • 英文作者:Feng Hui;He Zhirong;Wang Fang;Liu Kangkai;Du Yuqing;School of Materials Science and Engineering,Shaanxi University of Technology;Library,Shaanxi University of Technology;
  • 关键词:Ti-51. ; 1Ni形状记忆合金 ; 退火 ; 超弹性 ; 应力诱发马氏体相变 ; 超弹性残余应变
  • 英文关键词:Ti-51.1Ni shape memory alloy;;annealing;;superelasticity;;stress-induced martensitic transformation;;superelasticity residual strain
  • 中文刊名:JSRC
  • 英文刊名:Heat Treatment of Metals
  • 机构:陕西理工大学材料科学与工程学院;陕西理工大学图书馆;
  • 出版日期:2019-03-25
  • 出版单位:金属热处理
  • 年:2019
  • 期:v.44;No.499
  • 基金:国家重点研发计划(2016YFE0111400);; 汉中市科技计划(HZGXW1602);; 陕西理工大学研究生创新基金(SLGYCX1830)
  • 语种:中文;
  • 页:JSRC201903029
  • 页数:4
  • CN:03
  • ISSN:11-1860/TG
  • 分类号:127-130
摘要
用拉伸试验研究了退火温度(T_a)对Ti-51. 1Ni形状记忆合金超弹性的影响。结果表明:随T_a升高,Ti-51. 1Ni合金的应力诱发马氏体相变临界应力σ_M先降低后升高,极小值550 MPa在400℃退火后取得,极大值660 MPa在600℃退火后取得; 350~700℃退火态Ti-51. 1Ni合金的超弹性残余应变ε_r均较小(0. 27%~0. 36%);随应力-应变循环次数增加,350~700℃退火态Ti-51. 1Ni合金保持超弹性,应力应变滞后回线面积和ε_r减小,超弹性及其稳定性提高;要使该合金获得优异、稳定的超弹性,应对其进行500~600℃退火处理和应力-应变循环试验。
        Effect of annealing temperature(T_a) on the superelasticity of Ti-51. 1 Ni shape memory alloy was investigated by tensile test. The results show that with increase of T_a,the critical stress of stress-induced martensitic transformation σ_M decreases firstly and then increases,the minimum of 550 MPa can be obtained when the alloy is annealed at 400 ℃,the maximum of 660 MPa can be obtained when the alloy is annealed at 600 ℃. The superelasticity residual strain ε_r of the Ti-51. 1 Ni alloy annealed at 350-700 ℃ is very small( 0. 27% ~ 0. 36%).With the increase of stress-strain cycling number,the Ti-51. 1 Ni alloy annealed at 350-700 ℃ keeps superelasticity,the hysteresis loop area of stress-strain cycles and ε_r decrease,and the superelasticity and its stability increase. In order to obtain excellent and stable superelasticity in the Ti-51. 1 Ni alloy,the annealing treatment at 500-600 ℃ and the stress-strain cycling test should be carried out for the alloy.
引文
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