Effects of microstructure on fretting fatigue crack initiation behavior of Ti-6Al-4V

被引:43
作者
Mall, S [1 ]
Namjoshi, SA
Porter, W
机构
[1] USAF, Inst Technol, Dept Aeronaut & Astronaut, Wright Patterson AFB, OH 45433 USA
[2] Univ Dayton, Inst Res, Dayton, OH 45469 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2004年 / 383卷 / 02期
关键词
fretting fatigue; microstructure; titanium alloy; crack initiation; crack propagation;
D O I
10.1016/j.msea.2004.05.019
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Fretting fatigue crack initiation behaviour was investigated for its dependence on the microstructure of a alpha/beta titanium alloy, which ranged from homogeneous duplex to the fully transformed heterogeneous lamellar texture by increasing the Widmanstatten colony size. When the microstructure changed from homogeneous duplex to the fully transformed heterogeneous lamellar texture, the resistance to fretting fatigue crack initiation decreased. And, this was just the opposite of short and long crack behaviour where the resistance to crack growth increases when the microstructure changes from homogeneous duplex to the fully transformed heterogeneous lamellar structure. Published by Elsevier B.V.
引用
收藏
页码:334 / 340
页数:7
相关论文
共 34 条
[1]   Effects of microstructure on the short fatigue crack initiation and propagation characteristics of biomedical α/β titanium alloys [J].
Akahori, T ;
Niinomi, M ;
Fukunaga, K ;
Inagaki, I .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2000, 31 (08) :1949-1958
[2]   Mixed-mode, high-cycle fatigue-crack-growth thresholds in Ti-6Al-4V: Role of bimodal and lamellar microstructures [J].
Campbell, JP ;
Ritchie, RO .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2001, 32 (03) :497-503
[3]   Interaction of high-cycle and low-cycle fatigue on fretting behavior of Ti-6-4 [J].
Cortez, R ;
Mall, S ;
Calcaterra, JR .
FRETTING FATIGUE: CURRENT TECHNOLOGY AND PRACTICES, 2000, 1367 :183-198
[4]   High cycle fatigue in aircraft gas turbines - An industry perspective [J].
Cowles, BA .
INTERNATIONAL JOURNAL OF FRACTURE, 1996, 80 (2-3) :147-163
[5]   Cu-bearing high-strength low-alloy steels: The influence of microstructure on the initiation and growth of small fatigue cracks [J].
Davidson, DL ;
Chan, KS ;
McClung, RC .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1996, 27 (09) :2540-2556
[6]   FATIGUE CRACKING CHARACTERISTICS OF BETA-ANNEALED LARGE COLONY TI-11 ALLOY [J].
EYLON, D ;
BANIA, PJ .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1978, 9 (09) :1273-1279
[7]   FATIGUE BEHAVIOR OF BETA-PROCESSED TITANIUM-ALLOY IMI-685 [J].
EYLON, D ;
HALL, JA .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1977, 8 (06) :981-990
[8]  
EYLON D, 1998, SUMMARY AVAILABLE IN
[9]  
GREGORY JK, 1994, HDB FATIGUE CRACK PR
[10]   NON-CLOSURE OF CRACKS AND FATIGUE CRACK GROWTH IN BETA-HEAT TREATED TI-6A1-4V [J].
HALLIDAY, MD ;
BEEVERS, CJ .
INTERNATIONAL JOURNAL OF FRACTURE, 1979, 15 (01) :R27-R30