Research progress in damage mechanism of nickel-based single crystal superalloys under service conditions

被引：1
作者：
Shen J. [1 ,2 ]
Zhou Y. [1 ]
Wang X. [1 ]
机构：
[1] School of Aeronautics, Northwestern Poly technical University, Xi'an
[2] Shanxi Key Laboratory of Impact Dynamic and Its Engineering Application, Xi'an
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2023年 / 45卷 / 04期
关键词：
creep; fatigue; high temperature damage; life prediction; nickel-based single crystal superalloys; thermomechanical fatigue;
D O I：
10.11887/j.cn.202304007
中图分类号：
学科分类号：
摘要：
In order to improve the service life of nickel-based single crystal blades and solve the key technology of aeroengine turbine and gas turbine, domestic and overseas researchers carried out a large number of research on the failure and damage mechanism of nickel-based single crystal superalloys under service conditions in recent years. The research achievements and progress of fatigue, creep and thermomechanical fatigue damage mechanism of nickel-based single crystal superalloys under service conditions were concluded. In addition, in view of the lime and cost increase caused by a large number of experiments, the research works and achievements in life prediction methods of nickel-based single crystal superalloys in recent years were summarized, and the difficulties and challenges in life evaluation and failure analysis of nickel-based single crystal superalloys were proposed. © 2023 National University of Defense Technology. All rights reserved.
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页码：55 / 65
页数：10
相关论文
共 104 条
[1]  
ZHANG J, WANG L, WANG D, Research progress in research and development of nickel-based single crystal superalloys, Acta Metallurgica Sinica, 55, 9, pp. 1077-1094, (2019)
[2]  
TIAN W G, PAN M C, LUO F L, Et al., Borescope and eddy current integrative in-situ detecting defects in aeroengine laminas, Journal of National University of Defense Technology, 31, 5, pp. 101-105, (2009)
[3]  
AVATEFFAZELI M, WEBSTER G, TAHMASBI K, Et al., Very high cycle fatigue at elevated temperatures
[4]  
a review on high temperature ultrasonic fatigue, Journal of Space Safety Engineering, 9, 4, pp. 488-512, (2022)
[5]  
CERVELLON A, CORMIER J, MAUGET F, Et al., Very high cycle fatigue of Ni-based single-crystal superalloys at high temperature, Metallurgical and Materials Transactions A, 49, 9, pp. 3938-3950, (2018)
[6]  
XUAN W D, SONC C, DUAN F M, Et al., Enhanced creep properties of nickel-base single crystal superalloy CMSX-4 by high magnetic field, Materials Science and Engineering
[7]  
A, 803, (2021)
[8]  
TAO X P, DDYL, WANG X G, Et al., Effect of solution cooling rate on the microstructure and creep deformation mechanism of a rhenium-free second-generation single crystal superalloy, Journal of Materials Science & Technology, 131, pp. 14-29, (2022)
[9]  
LIU Y, ZHOU H, WU M M, Et al., Coating-related deterioration mechanism of creep performance at a thermal exposed single crystal Ni-hase superalloy, Materials Characterization, 187, (2022)
[10]  
LONC H B, MAO S C, LIU Y N, Microslructural and compositional design of Ni-based single crystalline superalloys
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