Heat Treatment of a Ni3Al-based Single Crystal Alloy IC32

被引:7
作者
Cui, Dongliang [1 ]
Xie, Xiaoying [1 ]
Li, Shusuo [1 ]
Zhang, Heng [1 ]
Gong, Shengkai [1 ]
机构
[1] Beihang Univ, Sch Mat Sci & Engn, Beijing 100191, Peoples R China
来源
HIGH PERFORMANCE STRUCTURE MATERIALS | 2013年 / 747-748卷
关键词
Ni3Al-based single crystal alloy; Heat treatment; Microstructure; NI-BASE SUPERALLOY; CREEP STRENGTH; MICROSTRUCTURE; 3RD-GENERATION; IMPROVEMENT; EVOLUTION;
D O I
10.4028/www.scientific.net/MSF.747-748.665
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
IC32 is a new type of Ni3Al-based single crystal alloy, which has been designed to serve at 1200 degrees C. The effect of heat treatment on the microstructure of single crystal superalloy IC32 was investigated. The microstructure after heat treatment under different solution and aging temperature was examined by using optical microscope (OM), scanning electron microscopy(SEM) and electron probe microscopic analyzer (EPMA). The as-cast microstructure of IC32 consisted of a two-phase gamma/gamma' microstructure, and primary bulky gamma' phase which priciptated in the interdendritic region. The incipient melting temperature of IC32 is 1360 degrees C, and the heat treatment window is about 40 degrees C. Considering high contents of refractory elements Re and Ta, a complicate 18 hours solution heat treatment at different temperatures was conducted to elimate the segregation and dissolove the primary bulky gamma' phase. The optimum heat treatment of IC32 alloy is 1325 degrees C/4h+1335 degrees C/4h+1345 degrees C/10h, ac + 1165 degrees C/2h, ac + 870 degrees C/32h, ac.
引用
收藏
页码:665 / 671
页数:7
相关论文
共 14 条
[1]   ON THE EFFECTS OF HEAT-TREATMENTS ON THE CREEP-BEHAVIOR OF A SINGLE-CRYSTAL SUPERALLOY [J].
CARON, P ;
HENDERSON, PJ ;
KHAN, T ;
MCLEAN, M .
SCRIPTA METALLURGICA, 1986, 20 (06) :875-880
[2]   Evolution of Ni-based superalloys for single crystal gas turbine blade applications [J].
Caron, P ;
Khan, T .
AEROSPACE SCIENCE AND TECHNOLOGY, 1999, 3 (08) :513-523
[3]   IMPROVEMENT OF CREEP STRENGTH IN A NICKEL-BASE SINGLE-CRYSTAL SUPER-ALLOY BY HEAT-TREATMENT [J].
CARON, P ;
KHAN, T .
MATERIALS SCIENCE AND ENGINEERING, 1983, 61 (02) :173-184
[4]  
Davis J.R., 1997, ASM SPECIALTY HDB, P255
[5]   Improvement of creep strength of a third generation, single-crystal Ni-base superalloy by solution heat treatment [J].
Fuchs G.E. .
Journal of Materials Engineering and Performance, 2002, 11 (01) :19-25
[6]   Solution heat treatment response of a third generation single crystal Ni-base superalloy [J].
Fuchs, GE .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2001, 300 (1-2) :52-60
[7]   Effect of heat treatment on microstructures and tensile properties of Ni-base superalloy M963 [J].
He, LZ ;
Zheng, Q ;
Sun, XF ;
Guan, HR ;
Hu, ZQ ;
Tieu, AK ;
Lu, C ;
Zhu, HT .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2005, 398 (1-2) :128-136
[8]   Designing homogenization-solution heat treatments for single crystal superalloys [J].
Hegde, S. R. ;
Kearsey, R. M. ;
Beddoes, J. C. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2010, 527 (21-22) :5528-5538
[9]  
Hu Z. Q., 2005, AEROENGINE, V31, P1
[10]   Influence of precipitate size and crystallographic orientation on strength of a single crystal Ni-base superalloy [J].
Kakehi, K .
MATERIALS TRANSACTIONS JIM, 1999, 40 (02) :159-167