THERMOMECHANICAL FATIGUE OF MAR-M247 .1. EXPERIMENTS

被引:73
作者
BOISMIER, DA [1 ]
SEHITOGLU, H [1 ]
机构
[1] UNIV ILLINOIS,DEPT MECH & IND ENGN,URBANA,IL 61801
来源
JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME | 1990年 / 112卷 / 01期
关键词
D O I
10.1115/1.2903189
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Isothermal fatigue tests, out-of-phase and in-phase thermo-mechanical fatigue tests were performed on Mar-M247 nickel-based superalloy. The experiments were conducted in the temperature range 500° C to 871° C. Results indicate that the lives differ with strain-temperature phasing and with strain rate. The results of out-of-phase thermo-mechanical tests correspond well with strain-life data of isothermal tests conducted at the peak temperature (871°C). However, the in-phase thermo-mechanical results differed depending on the strain amplitude. Significant surface and crack tip oxidation and gamma prime depletion has been observed based on metallographic and Auger Spectroscopic analyses. These changes were measured as a function of time. The environment induced changes significantly influenced the fatigue lives in isothermal and out-of-phase thermo-mechanical fatigue cases. In these cases transgranular cracking was observed. Grain boundary crack nucleation and grain boundary crack growth dominated the in-phase thermo-mechanical fatigue cases. Based on these observations the requirements for a life prediction model are outlined. The life prediction model and the predictions are given in Part 2 of this paper. © 1990 by ASME.
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页码:68 / 79
页数:12
相关论文
共 40 条
[1]   LOW-CYCLE FATIGUE BEHAVIOR OF RENE 80 AT ELEVATED-TEMPERATURE [J].
ANTOLOVICH, SD ;
LIU, S ;
BAUR, R .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1981, 12 (03) :473-481
[2]  
ANTOLOVICH SD, 1980, SUPERALLOYS 1980, P605
[3]  
BASHIR S, 1982, THESIS U CINCINNATI
[4]  
BILL RC, 1984, NASA TP2280
[5]  
Bui-Quoc T., 1988, LOW CYCLE FATIGUE, P470
[6]   EFFECT OF FREQUENCY ON CYCLIC STRAIN AND FATIGUE BEHAVIOR OF CAST RENE AT 1600 DEGREES F [J].
COFFIN, LF .
METALLURGICAL TRANSACTIONS, 1974, 5 (05) :1053-1060
[7]  
COOK TS, 1988, ASTM STP, V942, P692
[8]  
ELLIS JR, 1986, NASA HOST M
[9]  
EMBLEY GT, 1984, 1ST PARS INT TURB C
[10]   FATIGUE CRACK INITIATION AND PROPAGATION IN SEVERAL NICKEL-BASE SUPER-ALLOYS AT 650-DEGREES-C [J].
GAYDA, J ;
MINER, RV .
INTERNATIONAL JOURNAL OF FATIGUE, 1983, 5 (03) :135-143