Fracture behavior of superalloy IN738LC with various precipitate microstructures

被引:37
作者
Balikci, E
Mirshams, RA
Raman, A [1 ]
机构
[1] Louisiana State Univ, Dept Mech Engn, Mat Grp, Baton Rouge, LA 70803 USA
[2] Southern Univ, Dept Mech Engn, Baton Rouge, LA 70813 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 1999年 / 265卷 / 1-2期
关键词
tensile fractures; cleavage fracture; dimple ductile fracture; fracture toughness; decohesion; gamma ' precipitate; carbides; secondary hardening; ductility;
D O I
10.1016/S0921-5093(99)00012-X
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Fracture studies on differently aged specimens of IN738LC, tensile tested to failure at different temperatures with two different strain rates, were carried out using a scanning electron microscope. Specimens with fine-size gamma' precipitates (F) and duplex-size gamma' precipitates (D) exhibited generally more cleavage type fracture than those with medium (M) and coarse (C) size gamma' precipitates. {100}-faceted cleavage-type fracture was dominant at room temperature, while dimple fracture was dominant at 650 degrees C. A different type of cleavage fracture was observed in the specimens broken at 750 degrees C, which is attributed to secondary strengthening and change in flow mechanism at this temperature under slow strain rate conditions. At 850 degrees C, F and D showed wider faceted cleavage fracture, while hi and C showed dimple-ductile fracture. Low tensile fracture toughness correlates with cleavage fracture, while specimens exhibiting dimple fracture have higher ductility and toughness. Presence of few (Ta, Ti)C-type carbide particles along the grain boundaries probably enables easy intergranular crack propagation. Dimples, however, are postulated to be initiated by decohesion at the interface between the gamma' precipitate and the matrix. Notably such decohesion is initiated only on coarsened particles, not on the fine ones. (C) 1999 Published by Elsevier Science S.A. All rights reserved.
引用
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页码:50 / 62
页数:13
相关论文
共 28 条
[1]   INFLUENCE OF PRECIPITATE MORPHOLOGY ON HIGH-TEMPERATURE FATIGUE-CRACK GROWTH OF A SINGLE-CRYSTAL NICKEL-BASE SUPERALLOY [J].
AI, SH ;
LUPINC, V ;
ONOFRIO, G .
SCRIPTA METALLURGICA ET MATERIALIA, 1993, 29 (11) :1385-1390
[2]   LOW-CYCLE FATIGUE CHARACTERISTICS OF (001) AND RANDOMLY ALIGNED SUPERALLOY SINGLE-CRYSTALS [J].
ANTON, DL .
ACTA METALLURGICA, 1984, 32 (10) :1669-1679
[3]  
*ASTM, 1992, E2192 ASTM, P129
[4]  
*ASTM, 1995, E895A ASTM, P56
[5]  
Balikci E, 1999, Z METALLKD, V90, P141
[6]  
Balikci E, 1999, Z METALLKD, V90, P132
[7]   Influence of various heat treatments on the microstructure of polycrystalline IN738LC [J].
Balikci, E ;
Raman, A ;
Mirshams, RA .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1997, 28 (10) :1993-2003
[8]  
BALIKCI E, UNPUB
[9]   MICROSTRUCTURAL PROCESSES IN HIGH-TEMPERATURE LOW-CYCLE FATIGUE OF MAR-M200+HF [J].
BERKOVITS, A ;
NADIV, S ;
SHALEV, G .
ACTA METALLURGICA ET MATERIALIA, 1995, 43 (07) :2605-2613
[10]  
BETTGE D, 1995, Z METALLKD, V86, P190