Microstructural influences on the growth of small cracks in Ti-6Al-4V

被引:10
作者
Jin, O
Hamm, RW
Johnson, WS [1 ]
机构
[1] Georgia Inst Technol, Sch Mat Sci & Engn, Atlanta, GA 30332 USA
[2] USAF, Inst Technol, Wright Patterson AFB, OH 45433 USA
[3] Procter & Gamble Co, Cincinnati, OH USA
[4] Georgia Inst Technol, George W Woodruff Sch Mech Engn, Atlanta, GA 30332 USA
关键词
constant amplitude loading; double edge notch specimen; large cracks; microstructures; small fatigue cracks; titanium alloy;
D O I
10.1046/j.1460-2695.2002.00500.x
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The effects of microstructure on the growth of small cracks in Ti-6Al-4 V under fatigue loading are presented. The small crack growth is compared with large crack growth. Two large crack tests were per formed at a stress ratio of 0.4 and a frequency of 15 Hz. For small crack growth tests, double edge notch specimens were loaded under constant amplitude at four maximum stresses with a stress ratio of 0.4 and a frequency of 15 Hz. A plastic replication technique was used to monitor the small fatigue crack growth rate. The microstructure consists of bands of alpha and beta phases. The present study indicates that the crack growth direction and shape are dependent upon the grain size and grain orientations, and that the crack growth rate seems to be affected by the spacing of alpha-rich and beta-rich bands. Small cracks are propagated at stress intensity factors well below the large crack threshold stress intensity factor.
引用
收藏
页码:563 / 574
页数:12
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