High-frequency metal fatigue:: the high-cycle fatigue behavior of ULTIMET® alloy

被引:29
作者
Jiang, L
Brooks, CR
Liaw, PK
Wang, H
Rawn, CJ
Klarstrom, DL
机构
[1] Univ Tennessee, Dept Mat Sci & Engn, Knoxville, TN 37996 USA
[2] Oak Ridge Natl Lab, Div Met & Ceram, Oak Ridge, TN 37831 USA
[3] Haynes Int Inc, Kokomo, IN 46904 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2001年 / 314卷 / 1-2期
基金
美国国家科学基金会;
关键词
high-cycle fatigue; high-frequency; temperature increase; crack initiation; cobalt-based alloy;
D O I
10.1016/S0921-5093(00)01928-6
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
ULTIMET (R) alloy is a relatively new commercial Co-26Cr-9Ni (wt.%) alloy, which exhibits good resistance to both wear and corrosion. A state-of-the-art high-frequency, 1000-Hz, material test system was used to study the high-cycle fatigue behavior of ULTIMET alloy up to 10 degrees cycles. Fatigue experiments were conducted at high (1000 Hz) and conventional (20 Hz) frequencies in air at room temperature. The effects of the test frequency. the temperature increase during fatigue, and the change of crack initiation sites from the surface to subsurface on fatigue life are discussed. Although the fatigue life was comparable at test frequencies of 1000 and 20 Hz. the equilibrium temperature at 1000 Hz was considerably higher than that at 20 Hz. The fractographic study showed different morphologies of fracture surfaces at various frequencies. The high-cycle fatigue behavior of ULTIMET alloy at both high- and low-frequencies exhibited a typical two-stage fatigue-crack-growth process, i.e., (a) stage I fatigue-crack initiation in which the cracks formed on those planes most closely aligned with the maximum sheer-stress direction in the grains of the fatigue specimen; and (b) stage II fatigue-crack growth in which the maximum principal tensile stress controlled crack propagation in the region of the crack tip. (C) 2001 Elsevier Science B.V. All rights reserved.
引用
收藏
页码:162 / 175
页数:14
相关论文
共 26 条
[1]   SUBSURFACE CRACK INITIATION IN HIGH CYCLE FATIGUE IN TI6A14V AND IN A TYPICAL MARTENSITIC STAINLESS-STEEL [J].
ATRENS, A ;
HOFFELNER, W ;
DUERIG, TW ;
ALLISON, JE .
SCRIPTA METALLURGICA, 1983, 17 (05) :601-606
[2]  
BATHIAS C, 1993, AM SOC TEST MATER, V1211, P141, DOI 10.1520/STP15083S
[3]  
CROOK P, 1991, ADVMAT 91
[4]  
Crook P., 1992, ASM HDB, V18, P766
[5]  
FARHANGI H, 1989, MATER SCI ENG, V114, P25
[6]  
Halford GR., 1966, THESIS U ILLINOIS UR
[7]  
*HAYN INT, 1994, ULTIMET ALL, P3
[8]  
HOCKENHULL BS, 1971, INT CORR FAT C U CON, P453
[9]  
Jiang L, 2000, SUPERALLOYS 2000, P583, DOI 10.7449/2000/Superalloys_2000_583_591
[10]  
JIANG L, 2001, IN PRESS MAT SCI E A