The effects of environment and internal oxygen on fatigue crack propagation in Ti-6Al-4V

被引:40
|
作者
Bache, MR
Evans, WJ
McElhone, M
机构
[1] UNIV COLL SWANSEA,IRC MAT HIGH PERFORMANCE APPLICAT,SWANSEA SA2 8PP,W GLAM,WALES
[2] ROLLS ROYCE PLC,DERBY DE2 8BJ,ENGLAND
关键词
titanium; 6/4; fatigue crack growth; internal oxygen; environment;
D O I
10.1016/S0921-5093(97)00402-4
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The role of environmental and internal oxygen on fatigue crack propagation is assessed for the titanium alloy Ti-6Al-4V at laboratory temperature. Growth rates for part through corner cracks are demonstrated to be highly dependent on the amount of oxygen present. Compared to data for conventional plate material at atmospheric conditions, tests conducted under a vacuum of 10(-6) torr illustrate a marked reduction in the rates of growth for the facet dominated phase at low values of Delta K. Intermediate vacuum levels and partial pressures of argon or hydrogen lead to growth rates that are similar to or slightly lower than the conventional atmospheric baseline. Significant growth rate accelerations are observed, however, for 6/4 material containing internal oxygen concentrations in excess of the standard 1700-2300 ppm. This acceleration is enhanced by the application of a high load ratio, R = 0.5. The implications with respect to current ideas on environmental interactions are discussed. (C) 1991 Elsevier Science S.A.
引用
收藏
页码:918 / 922
页数:5
相关论文
共 50 条
  • [31] Fatigue small crack behavior of Ti-6Al-4V alloy
    Hu, Ben-Run
    Wu, Xue-Ren
    Ding, Chuan-Fu
    Hangkong Cailiao Xuebao/Journal of Aeronautical Materials, 2000, 20 (03): : 36 - 37
  • [32] Fretting fatigue crack initiation behavior of Ti-6Al-4V
    Mall, S. (Shankar.Mall@afit.edu), 1600, ASTM Committee E08 on Fatigue and Fracture (American Society for Testing and Materials):
  • [33] Probabilistic modeling of fatigue crack growth in Ti-6Al-4V
    Soboyejo, WO
    Shen, W
    Soboyejo, AO
    PROBABILISTIC METHODS IN FATIGUE AND FRACTURE, 2001, 200 : 81 - 97
  • [34] Prediction of short fatigue crack growth of Ti-6Al-4V
    Wang, K.
    Wang, F.
    Cui, W.
    Hayat, T.
    Ahmad, B.
    FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2014, 37 (10) : 1075 - 1086
  • [35] FATIGUE CRACK CLOSURE AS INFLUENCED BY MICROSTRUCTURE IN TI-6AL-4V
    RAYICHANDRAN, KS
    SCRIPTA METALLURGICA ET MATERIALIA, 1990, 24 (08): : 1559 - 1563
  • [36] Fretting fatigue crack initiation behavior of Ti-6Al-4V
    Mall, S
    Jain, VK
    Oshi, SAN
    Lykins, CD
    FRETTING FATIGUE: ADVANCES IN BASIC UNDERSTANDING AND APPLICATIONS, 2003, 1425 : 338 - 352
  • [37] MICROSTRUCTURAL INFLUENCES ON FATIGUE CRACK GROWTH IN TI-6AL-4V
    IRVING, PE
    BEEVERS, CJ
    MATERIALS SCIENCE AND ENGINEERING, 1974, 14 (03): : 229 - 238
  • [38] EFFECTS OF MICROSTRUCTURE AND TEXTURE ON FATIGUE CRACK-PROPAGATION IN TI-6AL-4V AND TI-6AL-2SN-4ZR-6MO PLATE
    BIDWELL, LR
    EYLON, D
    JOM-JOURNAL OF METALS, 1976, 28 (12): : A63 - A63
  • [39] Influence of Environment on Constant Load and Fatigue Crack Propagation of Titanium Alloys Ti-6Al-4V and Ti-8Al-1Mo-1V.
    Doeker, Hubert
    Forschungsbericht - Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt, 1980, (80-8):
  • [40] FATIGUE THRESHOLD CRACK PROPAGATION IN AIR AND DRY ARGON FOR A Ti-6Al-4V ALLOY.
    Bucci, R.J.
    Paris, P.C.
    Hertzberg, R.W.
    Schmidt, R.A.
    Anderson, A.F.
    1600,