Effects of Axial and Normal Stresses on Fretting Fatigue Properties of DD3 and DZ125 Nickel-based Alloys
摘 要
在自行设计的微动疲劳试验装置上进行了各向异性镍基合金DD3和DZ125与粉末高温镍基合金FGH95配对接触的微动疲劳试验,对接触区域萌生裂纹的断口形貌进行了观察,分析了轴向和法向应力对微动疲劳寿命以及微动接触区最大等效应力(Von-Mises等效应力)、滑移幅值、法向应变幅值等微动疲劳参数的影响。结果表明:保持法向应力不变,增大轴向应力将会降低DD3和DZ125合金的微动疲劳寿命;保持轴向应力不变,法向应力对微动疲劳寿命的影响不如轴向应力的显著;微动接触区域的最大等效应力和法向应变幅值受法向应力和轴向应力的共同影响,而滑移幅值仅受轴向应力的影响。
Abstract
A fretting fatigue test apparatus was self-designed and manufactured to carry out the fretting fatigue test for specimens of anisotropic nickel-based alloys DD3 and DZ125 contacted with pad of powder metallurgy superalloy FGH95. The fractures initiating cracks on contact zone were observed, and the effects of axial and normal stress on fretting fatigue life and fretting fatigue parameters, such as maximum equivalent stress(Von-Mises equivalent stress), slip amplitude and normal strain amplitude, were analyzed. The results show that the fretting fatigue life reduce with an increase in axial stress while keeping normal stress at a constant value. Also, the influence of normal stress is not obvious on fretting fatigue life as the effects of axial stress. The maximum equivalent stress and normal strain amplitude are affected by normal stress and axial stress, while the slip amplitude is only affected by axial stress.
中图分类号 V223
所属栏目 试验研究
基金项目
收稿日期 2013/9/18
修改稿日期 2014/9/2
网络出版日期
作者单位点击查看
备注石炜(1980-),男,湖北蕲春人,博士研究生。
引用该论文: SHI Wei,WEN Wei-dong,CUI Hai-tao. Effects of Axial and Normal Stresses on Fretting Fatigue Properties of DD3 and DZ125 Nickel-based Alloys[J]. Materials for mechancial engineering, 2014, 38(11): 10~15
石炜,温卫东,崔海涛. 轴向和法向应力对DD3和DZ125镍基合金微动疲劳性能的影响[J]. 机械工程材料, 2014, 38(11): 10~15
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【4】丁智平,陈吉平,尹泽勇,等.一种镍基单晶合金多轴低周疲劳损伤参量[J].航空动力学报,2006,21(3):538-544.
【5】石多奇,杨晓光,于慧臣.一种镍基单晶和定向结晶合金的疲劳寿命模型[J].航空动力学报,2010,25(8):1871-1875.
【6】周仲荣.关于微动磨损与微动疲劳的研究[J].中国机械工程,2000,11(10):1146-1150.
【7】卫中山,王珉,李亮,等.TC4合金微动疲劳损伤研究[J].机械工程材料,2006,30(1):30-32.
【8】朱旻昊,罗唯力,周仲荣.表面工程技术抗微动损伤的研究现状[J].机械工程材料,2003,27(4):1-3.
【9】徐进,阎兵,周仲荣,等.一种典型齿形紧配合面微动损伤机理研究[J].中国机械工程,2002,13(17):1452-1454.
【10】SZOLWINSKI M P, FARRIS T N. Observation, analysis and prediction of fretting fatigue in 2024-T351 aluminum alloy[J].Wear,1998,221:24-36.
【11】NEU R W. Progress in standardization of fretting fatigue terminology and testing[J].Tribology International,2011,44:1371-1377.
【12】石炜, 温卫东, 崔海涛. 微动疲劳加载装置的设计及其在典型合金上的应用[J].机械工程材料,2014,38(1):11-14.
【13】ASTM E2789-2010 Standard guide for fretting fatigue testing[S].
【14】《中国航空材料手册》编辑委员会.中国航空材料手册第2卷:变形高温合金 铸造高温合金[M].北京:中国标准出版社,2001.
【15】《中国航空材料手册》编辑委员会.中国航空材料手册第5卷:粉末冶金材料 精密合金与功能材料[M].北京:中国标准出版社,2001.
【16】FARRIS T N, MURTHY H. Fundamentals of fretting applied to anisotropic materials: high-temperature fretting fatigue of single-crystal nickel[R].[S.l]:[s.n.],2006.
【17】ARORA P R, JACOB M S D, SAPUAN M S, et al. Experimetal evaluation of fretting fatigue test apparatus[J].International Journal of Fatigue,2007,29:1328-1338.
【18】SURESH S.材料的疲劳[M].第2版.王中光,译. 北京: 国防工业出版社,1999.
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