Effects of slip on fretting behavior: experiments and analyses

被引:101
作者
Jin, O [1 ]
Mall, S [1 ]
机构
[1] USAF, Inst Technol, Dept Aeronaut & Astronaut, ENY, Wright Patterson AFB, OH 45433 USA
关键词
finite element; analysis; relative slip; fretting behavior;
D O I
10.1016/S0043-1648(03)00510-6
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The role of relative slip on fretting behavior was investigated by conducting experiments and analyses. The first series of tests was conducted at different substrate applied stress amplitudes, and the second series at different applied fretting pad displacements with a constant substrate stress amplitude. A fretting map was developed using fretting fatigue life, relative slip range and normal force. This map provides useful information about the inter-relationships between these parameters and contact conditions (partial and gross slip) as well as about damages induced by these conditions. Partial and gross slip conditions were modeled using finite element analysis (FEA). FEA showed that gross slip simply shifted the stress distribution and the location of the trailing edge without any appreciable change in magnitude. Modified shear stress range (MSSR) parameter, a critical plane-based multi-axial fatigue model, was used to characterize fretting fatigue crack initiation behavior. With increasing applied relative slip, the MSSR parameter initially increased and the fatigue life decreased; thereafter the MSSR remained constant but the fatigue life increased. This increase in the fatigue life appears to be due to an increased wear rate. There was thus a competition between crack initiation and material removal during fretting as the contact condition changed from partial slip to gross slip. (C) 2003 Elsevier B.V. All rights reserved.
引用
收藏
页码:671 / 684
页数:14
相关论文
共 35 条
  • [1] The effects of contact stress and slip distance on fretting fatigue damage in Ti6Al-4V/17-4PH contacts
    Anton, DL
    Lutian, MJ
    Favrow, LH
    Logan, D
    Annigeri, B
    [J]. FRETTING FATIGUE: CURRENT TECHNOLOGY AND PRACTICES, 2000, 1367 : 119 - 140
  • [2] *ASTM, 1989, ANN BOOK ASTM STAND, P946
  • [3] ATTIA MH, 1992, ASTM STP, V1159, P1
  • [4] MATERIAL EFFECTS IN FRETTING WEAR - APPLICATION TO IRON, TITANIUM, AND ALUMINUM-ALLOYS
    BLANCHARD, P
    COLOMBIE, C
    PELLERIN, V
    FAYEULLE, S
    VINCENT, L
    [J]. METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1991, 22 (07): : 1535 - 1544
  • [5] Interaction of high-cycle and low-cycle fatigue on fretting behavior of Ti-6-4
    Cortez, R
    Mall, S
    Calcaterra, JR
    [J]. FRETTING FATIGUE: CURRENT TECHNOLOGY AND PRACTICES, 2000, 1367 : 183 - 198
  • [6] A CRITICAL PLANE APPROACH TO MULTIAXIAL FATIGUE DAMAGE INCLUDING OUT-OF-PHASE LOADING
    FATEMI, A
    SOCIE, DF
    [J]. FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 1988, 11 (03) : 149 - 165
  • [7] FINDLEY WN, 1957, T ASME, V79, P1337
  • [8] ANALYSIS OF SLIDING BEHAVIOR FOR FRETTING LOADINGS - DETERMINATION OF TRANSITION CRITERIA
    FOUVRY, S
    KAPSA, P
    VINCENT, L
    [J]. WEAR, 1995, 185 (1-2) : 35 - 46
  • [9] Quantification of fretting damage
    Fouvry, S
    Kapsa, P
    Vincent, L
    [J]. WEAR, 1996, 200 (1-2) : 186 - 205
  • [10] An elastic-plastic shakedown analysis of fretting wear
    Fouvry, S
    Kapsa, P
    Vincent, L
    [J]. WEAR, 2001, 247 (01) : 41 - 54