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Ca含量对AMCa镁合金超高周疲劳断裂行为的影响
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  • 英文篇名:Influence of Ca Content on Ultra-High Cycle Fatigue Fracture Behavior of AMCa Magnesium Alloy
  • 作者:张艳斌 ; 孙东洋 ; 张继旺
  • 英文作者:ZHANG Yanbin;SUN Dongyang;ZHANG Jiwang;School of Mechanical Engineering,Southwest Jiaotong University;State Key Laboratory of Traction Power,Southwest Jiaotong University;
  • 关键词:镁合金 ; 超高周疲劳 ; 裂纹萌生机制 ; 双S-N曲线
  • 英文关键词:magnesium alloy;;ultra-high cycle fatigue;;fatigue crack initiation mechanism;;double S-N curve
  • 中文刊名:XNJT
  • 英文刊名:Journal of Southwest Jiaotong University
  • 机构:西南交通大学机械工程学院;西南交通大学牵引动力国家重点实验室;
  • 出版日期:2018-12-27 09:34
  • 出版单位:西南交通大学学报
  • 年:2019
  • 期:v.54;No.246
  • 基金:中央高校基本科研业务费专项资金资助项目(2682017CX039)
  • 语种:中文;
  • 页:XNJT201902020
  • 页数:7
  • CN:02
  • ISSN:51-1277/U
  • 分类号:167-173
摘要
为了阐明Ca含量对镁合金疲劳性能的影响,采用旋转弯曲疲劳试验机对两种AMCa镁合金进行超高周疲劳实验,并利用扫描电子显微镜SEM (scanning electron microscope)和X射线能谱仪EDS (X-ray energy dispersive spectroscopy)观察疲劳试样的断口形貌,分析了两种镁合金疲劳S-N(疲劳应力-疲劳寿命)曲线特性和疲劳断裂行为,讨论了Ca元素含量增加对镁合金疲劳寿命和疲劳裂纹萌生机制的影响.结果表明,AM1.77 Ca镁合金S-N曲线没有传统的疲劳极限,呈现曲线连续下降趋势;AM1.85 Ca镁合金具有双S-N曲线特性,在130 MPa左右出现转折点;Ca元素含量增加导致镁合金产生微观结构缺陷,使材料的疲劳裂纹萌生模式从AM1.77 Ca镁合金的表面萌生模式转变为AM1.85 Ca镁合金的两种疲劳裂纹萌生模式,即表面萌生和次表面萌生模式,这种转变对材料抗疲劳性能的提升不利.
        In order to investigate the effect of Ca content on the fatigue properties of magnesium alloys,the ultrahigh cycle fatigue tests were carried out for two AMCa magnesium alloys using a rotating bending fatigue machine. The fracture morphologies of the fatigue specimens were observed by using scanning electron microscopy(SEM) and X-ray energy dispersive spectroscopy(EDS). Based on the experimental results, the fatigue S-N(fatigue strength-fatigue life) curves features and the fatigue fracture behavior were analyzed. Then,the influence of the Ca content on the fatigue life and fatigue crack initiation mechanism was discussed. The results indicate that the S-N curve of the AM1.77 Ca magnesium alloy shows a trend of continuous decline without a traditional fatigue limit,and the AM1.85 Ca magnesium alloy shows double S-N curve characteristics with a turning point around 130 MPa. The fatigue crack initiation mode is the surface initiation mode for the AM1.77 Ca magnesium alloy. However, the AM1.85 Ca magnesium alloy has two types of fatigue crack initiation modes,namely,the surface initiation mode and sub-surface initiation mode,which is due to the increase in the Ca content. The change that AM1.85 Ca magnesium alloy has two types of fatigue crack initiation modes is not conducive to improve the anti-fatigue performance.
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