Elevated temperature fatigue crack growth and time dependent behaviour in Ti-6246

被引:0
作者
Jones, JP [1 ]
Bache, MR [1 ]
Evans, WJ [1 ]
Williams, S [1 ]
机构
[1] Univ Coll Swansea, IRC Comp Aided Mat Engn, Swansea SA2 8PP, W Glam, Wales
来源
TITANIUM ALLOYS AT ELEVATED TEMPERATURE: STRUCTURAL DEVELOPMENT AND SERVICE BEHAVIOUR | 2001年 / 755卷 / 04期
关键词
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Fatigue crack propagation behaviour of the titanium alloy Ti-6246 has been investigated at room and elevated temperatures. Using stress intensity range, DeltaK, as a correlating parameter, fatigue crack growth rates were found to be insensitive to variations in positive mean stress and waveform at 20 degreesC. This is attributed, in part, to the refined microstructure. However, a fine grain size is often associated with inferior high temperature creep behaviour and can accentuate the diffusion of aggressive species along grain boundaries. As a result, at the higher temperatures measured growth rates generally increased and became dependent on R ratio and periods of dwell loading at peak stress. Additional testing under a hard vacuum condition have been implemented to characterise creep-environmental fatigue interactions.
引用
收藏
页码:177 / 185
页数:9
相关论文
共 10 条
[1]  
BACHE MR, 1998, P 3 ENG FDN INT C, P179
[2]  
CHESNUTT JC, 1994, P 10 INT C STRENGTH, P533
[3]  
Evans W. J., 1997, International Journal of Fatigue, V19, pS177, DOI 10.1016/S0142-1123(97)00035-2
[4]  
Evans WJ, 2000, FATIGUE 2000: FATIGUE & DURABILITY ASSESSMENT OF MATERIALS, COMP ONENTS AND STRUCTURES, P587
[5]   Effects of temperature and environment interactions on fatigue crack propagation in a Ti alloy [J].
Lesterlin, S ;
SarrazinBaudoux, C ;
Petit, J .
SCRIPTA MATERIALIA, 1996, 34 (04) :651-657
[6]  
LESTERLIN S, 1996, TIT 95 SCI TECHN P 8, V2, P1211
[7]  
MOM AJA, 1986, 86019L NLR TR
[8]  
PETIT J, 1995, MODELLING INTRINSIC, P131
[9]  
Pickard A.C., 1986, APPL 3 DIMENSIONAL F
[10]  
SPENCE SH, 1996, SCRIPTA METALL, V34, P1571