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微动疲劳影响因素及钛合金微动疲劳行为
引用本文:刘道新,何家文.微动疲劳影响因素及钛合金微动疲劳行为[J].航空学报,2001,22(5):454-457.
作者姓名:刘道新  何家文
作者单位:1. 西北工业大学腐蚀与防护研究室, 陕西西安 710072;2. 西安交通大学金属材料强度国家重点实验室, 陕西西安 710049
基金项目:航空基础科学基金 ( 98H5 30 86 ),陕西省自然科学研究计划 ( 2 0 0 0 C0 1)资助项目
摘    要:综述了影响材料微动疲劳 ( FF)行为的各因素及其相互联系,通过实验探讨了接触压力、位移幅度、接触几何及残余应力状态等重要因素对 Ti6Al4 V合金 FF行为的影响规律及交互作用。结果表明,钛合金 FF寿命随接触压力和位移幅度的变化均是非单调性的,原因是名义接触压力的变化改变了接触区应力分布、应力集中状况和微动位移幅,从而影响裂纹的萌生几率,而位移幅影响了疲劳和磨损因素在 FF过程中的作用主次。接触几何则通过改变接触区应力集中状况而影响裂纹萌生几率的大小。残余压应力主要抑制 FF裂纹扩展,在部分滑动条件下它对提高钛合金 FF抗力的作用更加显著。

关 键 词:微动疲劳  微动磨损  航空结构  钛合金  喷丸强化  残余应力  
文章编号:1000-6893(2001)05-0454-04
收稿时间:2000-07-20
修稿时间:2000年7月20日

REVIEW OF FACTORS THAT INFLUENCE FRETTING FATIGUE (FF) AND INVESTIGATION ON FF BEHAVIOR OF Ti-ALLOY
LIU Dao xin ,HE Jia wen.REVIEW OF FACTORS THAT INFLUENCE FRETTING FATIGUE (FF) AND INVESTIGATION ON FF BEHAVIOR OF Ti-ALLOY[J].Acta Aeronautica et Astronautica Sinica,2001,22(5):454-457.
Authors:LIU Dao xin  HE Jia wen
Institution:1. Corrosion & Protection Research Lab., Northwestern Polytechnical University, Xi'an 710072, China;2. Xi'an Jiaotong University, Xi'an 710049, China
Abstract:The factors that influence fretting fatigue process are reviewed and the interactions between these factors are outlined. The effects of major factors, including slip amplitude, contact pressure, contact geometry and surface residual stress, on FF behavior of Ti6Al4V alloy were investigated by experiments. The results show that these major factors affect the action of fatigue and wear in FF process, resulting in the change of crack initiation probability and crack propagating rate. Therefore, the FF life of Ti alloy doesn't change in a monotone way with the slip amplitude and contact pressure increasing. The effect of surface compressive residual stress (SCRS) on FF resistance depends not only on the value and distribution of SCRS, but also on the other major parameters in FF tests. SCRS plays a more important role in improving FF resistance in partial slip situation than in gross slip. This is due to the fact that SCRS restrains crack propagation more remarkably than arrests crack initiation.
Keywords:fretting fatigue  fretting wear  aeronautic structure  titanium alloy  shot peening  residual stress
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