A physically based model for correlating the microstructural degradation and residual creep lifetime of a polycrystalline Ni-based superalloy

被引:16
作者
Li, Shaolin [1 ,2 ]
Wang, Bingxue [1 ]
Shi, Duoqi [1 ,2 ]
Yang, Xiaoguang [1 ,2 ]
Qi, Hongyu [1 ,2 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Microstructure evolution; Lifetime degradation; K417; alloy; Creep-rupture time; Analytical model; SERVICE INDUCED DEGRADATION; TURBINE BLADE; MECHANICAL-PROPERTIES; FAILURE ANALYSIS; EVOLUTION; PRECIPITATION; K417; PROPERTY; EXPOSURE; BEHAVIOR;
D O I
10.1016/j.jallcom.2018.11.417
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The microstructure evolution and creep property degradation of the Ni-based superalloy K417 were studied at different high-temperature thermal exposure conditions. The results showed that the equivalent radius of gamma' precipitates increased with the exposure time at all the temperatures and displayed spherical morphologies. Moreover, small blocky-type Cr-rich M23C6 carbides were observed due to the decomposition of the primary MC after exposure to 950 degrees C for 200 h and 50 h both at 1000 degrees C and 1050 degrees C. The creep-rupture lifetimes deteriorated with increased exposure time and temperature due to gamma' precipitates coarsening and the decomposition of the primary carbides. Furthermore, a physically based analytical model was developed to describe the influence of the microstructural evolution of the gamma' precipitates on the residual creep lifetime. (C) 2018 Elsevier B.V. All rights reserved.
引用
收藏
页码:565 / 573
页数:9
相关论文
共 40 条
[1]  
[Anonymous], 1968, Experimental Correlations for HighTemperature Creep
[2]  
[Anonymous], 2008, SUPERALLOYS FUNDAMEN, DOI DOI 10.1017/CBO9780511541285
[3]   Review Progress in Ostwald ripening theories and their applications to the γ′-precipitates in nickel-base superalloys -: Part II -: Nickel-base superalloys [J].
Baldan, A .
JOURNAL OF MATERIALS SCIENCE, 2002, 37 (12) :2379-2405
[4]   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
[5]   Common failures in gas turbine blades [J].
Carter, TJ .
ENGINEERING FAILURE ANALYSIS, 2005, 12 (02) :237-247
[6]   VHCF life evolution after microstructure degradation of a Ni-based single crystal superalloy [J].
Cervellon, A. ;
Cormier, J. ;
Mauget, F. ;
Hervier, Z. .
INTERNATIONAL JOURNAL OF FATIGUE, 2017, 104 :251-262
[7]   Metallurgical considerations for life assessment and the safe refurbishment and requalification of gas turbine blades [J].
Daleo, JA ;
Ellison, KA ;
Boone, DH .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2002, 124 (03) :571-579
[8]  
Duhl M.G.D., 1980, Superalloys Warrendale, V41
[9]  
Epishin A, 2008, SUPERALLOYS 2008, P725, DOI 10.7449/2008/Superalloys_2008_725_731
[10]   Influence of thermal exposure on the microstructural evolution and mechanical properties of a wrought Ni-base superalloy [J].
Kim, I. S. ;
Choi, B. G. ;
Hong, H. U. ;
Do, J. ;
Jo, C. Y. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2014, 593 :55-63