ON THE NATURE AND CRYSTALLOGRAPHIC ORIENTATION OF SUBSURFACE CRACKS IN HIGH CYCLE FATIGUE OF TI-6AL-4V

被引:23
|
作者
GILBERT, JL [1 ]
PIEHLER, HR [1 ]
机构
[1] CARNEGIE MELLON UNIV,DEPT MAT SCI & ENGN,PITTSBURGH,PA 15213
来源
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE | 1993年 / 24卷 / 03期
关键词
D O I
10.1007/BF02656635
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Subsurface fatigue damage, in the form of cracking of the alpha phase, was observed in Ti-6Al-4V during high cycle fatigue of total hip prostheses tested in a simulated physiological test geometry and environment. The subsurface cracking was found only in the region of highest fatigue stresses and was present in a zone between 50 and 700 mum beneath the surface. The density of these cracks appeared to depend on the fabrication process used to form the part, where the direction of forging deformation strongly influenced the texture and grain morphology of the near-alpha bimodal microstructure. A novel scanning electron microscopy (SEM) technique, using selected area channeling patterns (SACPs) and electron channeling contrast imaging (ECCI), is described and was used to determine the crystallographic orientation of the fracture plane in the alpha phase. The texture resulting from the forming operation appeared to be such that the basal pole of the hcp lattice became oriented in the direction of flow. Also, the deformation substructure (in the form of dislocation subcells) influenced the formation of the subsurface cracks. Observations based on four independent fractured grains, using the channeling analysis techniques, indicated that the fracture plane for these subsurface fatigue cracks is the pyramidal plane of the hcp lattice.
引用
收藏
页码:669 / 680
页数:12
相关论文
共 50 条
  • [21] EFFECTS OF RESIDUAL STRESSES ON THE HIGH CYCLE FATIGUE BEHAVIOR OF Ti-6Al-4V
    Li, Yu-Jia
    Xuan, Fu-Zhen
    Wang, Zheng-Dong
    Tu, Shan-Tung
    PROCEEDINGS OF THE ASME PRESSURE VESSELS AND PIPING CONFERENCE 2010, VOL 5, 2010, : 397 - 401
  • [22] Impact of Morphology on the High Cycle Fatigue Behavior of Ti-6Al-4V for Aerospace
    Lee, Yoon-Seok
    Cho, Seungchan
    Ji, Changwook
    Jo, Ilguk
    Choi, Moonhee
    METALS, 2022, 12 (10)
  • [23] Evolution and effects of damage in Ti-6Al-4V under high cycle fatigue
    Nicholas, T
    Maxwell, DC
    PROGRESS IN MECHANICAL BEHAVIOUR OF MATERIALS (ICM8), VOL 3: ADVANCE MATERIALS AND MODELLING OF MECHANICAL BEHAVIOUR, 1999, : 1161 - 1166
  • [24] High cycle fatigue behaviour of Ti-6Al-4V alloy at elevated temperatures
    Tokaji, K
    SCRIPTA MATERIALIA, 2006, 54 (12) : 2143 - 2148
  • [25] The effect of microstructure on very high cycle fatigue properties in Ti-6Al-4V
    Oguma, H.
    Nakamura, T.
    SCRIPTA MATERIALIA, 2010, 63 (01) : 32 - 34
  • [26] Frequency and stress ratio effects in high cycle fatigue of Ti-6Al-4V
    Morrissey, RJ
    McDowell, DL
    Nicholas, T
    INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (07) : 679 - 685
  • [27] HIGH CYCLE FATIGUE OF TI-6AL-4V ALLOY IN SIMULATED STEAM ENVIRONMENT
    Li, Yu-Jia
    Mei, Lin-Bo
    Xuan, Fu-Zhen
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 7A, 2015,
  • [28] Ultra-high cycle fatigue behavior of Ti-6Al-4V alloy
    Environmental Corrosion Center, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
    不详
    Jinshu Xuebao, 2007, 7 (705-709):
  • [29] LOW-CYCLE FATIGUE BEHAVIOR OF TI-6AL-4V
    WELLS, CH
    SULLIVAN, CP
    JOURNAL OF METALS, 1968, 20 (01): : A93 - &
  • [30] High cycle fatigue and fatigue crack propagation behaviors of β-annealed Ti-6Al-4V alloy
    Jeong D.
    Kwon Y.
    Goto M.
    Kim S.
    International Journal of Mechanical and Materials Engineering, 2017, 12 (1)