FATIGUE CRACK-PROPAGATION BEHAVIOR UNDER VARIABLE AMPLITUDE LOADING IN THE NEAR-THRESHOLD REGION OF A HIGH-STRENGTH LOW-ALLOY STEEL

被引:4
作者
HENAFF, G [1 ]
PETIT, J [1 ]
JOURNET, B [1 ]
机构
[1] AEROSPATIALE,CTR COMMUN RECH LOUIS BLERIOT,DEPT MAT,F-92152 SURESNES,FRANCE
关键词
D O I
10.1111/j.1460-2695.1992.tb00040.x
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The near-threshold behaviour of a high-strength low-alloy steel used in helicopter rotors under variable amplitude loading is investigated in ambient air and in vacuum. Strong sequence effects occur, in particular a high decrease in crack growth rates after overloads of 40% on maximum load while keeping the amplitude constant. A detailed study of the retardation phenomenon due to the overloads provides an explanation for the different behaviour observed in air and in vacuum and has laid the basis for a method of predicting crack propagation under helicopter loading spectra.
引用
收藏
页码:1155 / 1170
页数:16
相关论文
共 12 条
[1]  
ALIAGA D, 1987, ASTM STP, V592, P491
[2]  
Baudin G., 1988, FATIGUE CRACK GROWTH, P292
[3]  
BENOIT D, 1981, MEM ETUD SCI REV MET, P569
[4]  
BERNARD PJ, 1972, ASTM STP, V595, P78
[5]  
De Koning A., 1981, ASTM STP
[6]  
EDWARDS PR, 1984, STANDARDISED FATIGUE
[7]  
HENAFF G, 1992, UNPUB ACTA MET MATER
[8]   REALIZATION OF A DYNAMIC TESTING SYSTEM UNDER VACUUM OR CONTROLLED ENVIRONMENTS [J].
PETIT, J ;
NADEAU, A ;
LAFARIE, MC ;
RANGANATHAN, N .
REVUE DE PHYSIQUE APPLIQUEE, 1980, 15 (04) :919-923
[9]  
RANGANATHAN N, 1990, ASTM STP, V1049, P374
[10]  
ROBIN C, 1988, FATIGUE CRACK GROWTH, P87