[1]晋小超,侯成,吉新阔,等.热障涂层系统损伤与断裂研究进展[J].中国材料进展,2020,(11):897-910.[doi:10.7502/j.issn.1674-3962.202007027]
 JIN Xiaochao,HOU Cheng,JI Xinkuo,et al.Advances in Damage and Fracture of Thermal Barrier Coatings[J].MATERIALS CHINA,2020,(11):897-910.[doi:10.7502/j.issn.1674-3962.202007027]
点击复制

热障涂层系统损伤与断裂研究进展()
分享到:

中国材料进展[ISSN:1674-3962/CN:61-1473/TG]

卷:
期数:
2020年第11期
页码:
897-910
栏目:
出版日期:
2020-11-30

文章信息/Info

Title:
Advances in Damage and Fracture of Thermal Barrier Coatings
文章编号:
1674-3962(2020)11-0897-14
作者:
晋小超侯成吉新阔陈垚范学领
(西安交通大学航天航空学院 机械结构强度与振动国家重点实验室,陕西 西安 710049)
Author(s):
JIN Xiaochao HOU Cheng JI Xinkuo CHEN Yao FAN Xueling
(State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong University, Xi’an 710049, China)
关键词:
热障涂层损伤断裂失效应力
Keywords:
thermal barrier coating damage fracture failure stress
分类号:
TG174.4
DOI:
10.7502/j.issn.1674-3962.202007027
文献标志码:
A
摘要:
热障涂层(thermal barrier coating, TBC)具有隔热、抗氧化、抗腐蚀和抗冲刷等性能,能进一步提高热端部件服役温度和使用寿命,是航空发动机和燃气轮机关键核心技术之一。在高温、高压、强氧化和强腐蚀的服役环境中,热障涂层系统(thermal barrier coatings, TBCs)易发生涂层脱粘、起泡、屈曲、开裂、剥落等形式的失效,严重影响热端部件的服役寿命。因此,研究TBCs损伤与断裂对于保障高温叶片等热端部件的安全稳定运行具有重要意义。针对TBCs损伤与断裂问题,重点介绍了近年来TBCs的失效机理、本构模型、损伤与断裂的力学分析方法方面的研究成果,在热循环/热冲击和热机械载荷作用下、腐蚀环境下TBCs的损伤与断裂行为,以及TBCs强度试验与损伤检测方法的研究进展,分析总结了TBCs损伤与断裂研究的发展趋势,力求为我国航空发动机和燃气轮机的基础研究和技术开发提供支撑。
Abstract:
Thermal barrier coating (TBC) is one of the key technologies of aeroengine and gas turbine, which can improve the service temperature and service life of hot end components due to their abilities to insulate against the heat transfer and resist the oxidation, corrosion and erosion. Under the conditions with high temperature and pressure, strong oxidation and corrosion, thermal barrier coatings (TBCs) are prone to failure in the form of coating debonding, blistering, buckling, cracking and spalling, which seriously limits the service life of hot end components. Therefore, it is of great significance to study the damage and fracture mechanism of TBCs to ensure the safety and stability of hightemperature blades and other hot end components in service. This article presents a comprehensive overview of development of TBCs,including: ① the damage and fracture behaviors and failure mechanisms of TBCs, ② constitutive model, ③ damage and fracture mechanics method and their behaviors under harsh environment, ④ the development of TBCs strength test and damage detection methods, ⑤ perspective for the study on damage and fracture of TBCs. The aim of this work is to provide support for basic research and technology development of aeroengine and gas turbine in China.

备注/Memo

备注/Memo:
收稿日期:2020-07-20 基金项目:国家自然科学基金资助项目(1171101165,11602188)第一作者:晋小超,男,1990年生,博士,助理教授通讯作者:范学领,男,1979年生,教授,博士生导师, Email: fanxueling@mail.xjtu.edu.cn
更新日期/Last Update: 2020-11-01