期刊文献+

微动接触应力影响因素研究 被引量:3

Study on Influencing Factors for Fretting Contacting Stresses
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摘要 采用ABAQUS软件建立了圆柱/平面接触的铝合金微动疲劳结构有限元模型,运用该模型将计算的应力值与解析解进行比较,结果相当吻合,证明了所建有限元模型及算法的有效性。通过分析得到了不同影响因素下接触应力的分布规律。结果表明,最大正应力随压头半径的增加而降低,随接触压力的增加而成比例地增加;表面拉应力在粘着区内随压头半径的增加而增加,随接触载荷的增加而降低;参数Q/(fP)对正应力和表面拉应力没有影响,各参数对剪应力的影响因接触区域不同而有较大的差别。 A global finite element model and sub-model of fretting fatigue of aluminum alloy column/plane contact structure was established using ABAQUS software. The effectiveness of the model was validated according to the comparison of analytical solutions and numerical solutions. Distributing rules of contacting stress for different influencing factors were obtained. The results showed that the maximal normal stress decreases as the pad radius increases and increases relevantly as the increasing of the contact load; in the stick region, as the values of pad radius and contact load increase, the pull stress increases and decreases, respectively; the ratio Q/fp) has no effect on the normal stress and pull stress; the effect of these parameters on shear stress has a great difference at different contact region.
出处 《装备环境工程》 CAS 2012年第1期5-9,22,共6页 Equipment Environmental Engineering
基金 国家自然科学基金(50675221 51075394)
关键词 微动疲劳 正应力 有限元 影响因素 fretting fatigue contacting stress finite element influencing factor
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参考文献11

  • 1GOLDEN P J, BARTHA B B, GRANDT A F, et al. Measurement of the Fatigue Crack Propagation Threshold of Fretting Induced Cracks in Ti-6Al-4V[J]. International Journal of Fatigue, 2004,26( 1 ) : 281--288.
  • 2GIANNAKOUPOULOS AE, LINDLEY TC, SURESH S. Application of Fracture Mechanics in Fretting Fatigue Life Assessment[R]. Fretting Fatigue Current Technology and Practices STP, 2000.
  • 3MASSINGHAM M, IRVING P E. The Effect of Variable Amplitude Loading on Stress Distribution within a Cylindrical Contact Subjected to Fretting Fatigue[J]. Tribology International, 2006,39(5) : 1084--1091.
  • 4刘军,刘道新,刘元镛,唐长斌.微动接触应力的有限元分析[J].机械强度,2005,27(4):504-509. 被引量:24
  • 5ZHAO H. The Virtual Contact Loading Method for Contact Problem Considering Material and Geometric Nonlinearities[J]. Comput & Struct, 1996,58 (3) : 621--632.
  • 6ZHAO H. Analysis of Load Distribution within Solid and Hollow Roller Bearing[J]. ASEMJ Tribology, 1998, 120 (1) : 134--139.
  • 7ZHAO H. Stress Concentration Factors within Bolt Bolt-nut Connectors under Elasto Elasto-plastic Deformation[J]. International Journal of Fatigue, 1998,20 ( 3 ) : 651--659.
  • 8赵华,金雪岩,朱民昊,周仲荣.微动接触应力的数值分析[J].四川大学学报(工程科学版),2003,35(5):32-36. 被引量:7
  • 9LEIVA O. Effect of Shear Load on Freeting Fatigue Behavior of Ti-6Al-4V[D]. Dayton: University of Dayton, 2003.
  • 10杨茂胜,陈跃良.微动疲劳结构应力强度因子有限元分析[J].航空学报,2010,31(10):1968-1973. 被引量:2

二级参考文献30

  • 1朱如鹏,潘升材.高低周复合载荷作用下微动疲劳寿命预测研究[J].机械强度,1996,18(3):37-40. 被引量:7
  • 2陈跃良,郁大照,杨茂胜,胡家林.含多处损伤搭接结构应力强度因子有限元分析[J].航空学报,2007,28(3):615-619. 被引量:19
  • 3Golden P J,Bartha B B,Grandt A F,et al.Measurement of the fatigue crack propagation threshold of fretting induced cracks in Ti-6Al-4V[J].International Journal of Fatigue,2004,26(3):281-288.
  • 4Naboulsi S.Application of crack analogy to fretting fatigue[J].Engineering Fracture Mechanics,2005,72(10):1610-1623.
  • 5Datsyshyn O P,Kadyra V M.A fracture mechanics approach to prediction of pitting under fretting fatigue conditions[J].International Journal of Fatigue,2006,28(4):375-385.
  • 6Fadag H A.An investigation of the propagation behavior of fretting fatigue cracks in Ti-6Al-4V[D].Dayton:University of Dayton,2005.
  • 7Leiva O.Effect of shear load on freeting fatigue behavior of Ti-6Al-4V[D].Dayton:University of Dayton,2003.
  • 8Yhksull H I.Effects of shot-peening on high cycle fretting fatigue behavior of Ti-6Al-4V[D].Maxwell:Air Force Institute of Technology at WPAFB,2002.
  • 9Shkarayev S,Mall S.Computational modeling of shot-peening effects on crack propagation under fretting fatigue[J].Journal of Strain Analysis,2003,38(6):495-506.
  • 10James M,Swenson D.FRANC2D/L:a crack propagation simulator for plane layered structures[M].Version 1.4 User's Guide.Manhattan:Kansas State University Press,2002.

共引文献27

同被引文献46

  • 1周小林,向延念,陈秀方.U71Mn50kg·m^(-1)普通碳素钢钢轨疲劳裂纹扩展速率试验研究[J].中国铁道科学,2004,25(3):86-90. 被引量:16
  • 2金学松,张雪珊,张剑,孙丽萍,王生武.轮轨关系研究中的力学问题[J].机械强度,2005,27(4):408-418. 被引量:50
  • 3刘军,刘道新,刘元镛,唐长斌.微动接触应力的有限元分析[J].机械强度,2005,27(4):504-509. 被引量:24
  • 4周文,孙伟明,屠立群,欧红永.微动摩擦力的有限元分析[J].甘肃科技,2007,23(6):93-94. 被引量:6
  • 5李庆芬.断裂力学及其工程应用[M].哈尔滨:哈尔滨工程大学出版社,2007.
  • 6吴学仁.飞机结构金属材料力学性能手册[M].北京:航空工业出版社,1996..
  • 7JACOB M S D, ARORA Prithvi Raj, SALEEM M, et al. Fretting Fatigue Crack Initiation : An Experimental and Th- eoretical Study[J]. International Journal of Fatigue, 2007,29 (3) : 1328-1338.
  • 8RUIZ C, BODDINGTON P H B, CHEN C. An Investigation of Fatigue and Fretting in a Dovetail Joint[J]. Experimental Mechanics, 1998,24 (4) : 208-217.
  • 9LYKINS Christopher D, SHANKAR Mall, JAIN Vinod. An Evaluation of Parameters for Predicting Fretting Fatigue Crack Initiation[J]. International Journal of Fatigue, 2000, 22(2) :703-716.
  • 10GANAPATHY Harish, FARRIS T N. Modeling of Skin/Rivet Contact: Application to Fretting Fatigue, AIAA-97-1340 [R]. 1997.

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