Critical compressive strain and interfacial damage evolution of EB-PVD thermal barrier coating
Jing FL4; Yang JJ3; Yang ZM(杨正茂)2; Zeng W1
刊名MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING
2020-03-03
卷号776页码:9
关键词Thermal barrier coating Critical compressive strain Interfacial damage evolution Isothermal and cyclic oxidation Life prediction
ISSN号0921-5093
DOI10.1016/j.msea.2020.139038
英文摘要

The durability evaluation of electron beam physical vapor deposited (EB-PVD) thermal barrier coating (TBC) systems is one of the critical issues in engineering applications. The interfacial toughness degradation as a function of the thickness of thermally grown oxide (TGO) was investigated through isothermal oxidation and cyclic oxidation tests for single-crystal superalloy specimens with an EB-PVD TBC. The critical strain criterion of TBC compression spalling was proposed through compression tests at room temperature according to noncontact full-field strain measurement technology and the digital image correlation (DIC) method. Based on a simplified mechanical model of TBC systems and elastic buckling theory, the interfacial damage was described by the critical compressive strain at spallation considering residual stress in the ceramic top coat (TC). The results indicated that the damage induced by cyclic oxidation is greater than that induced by isothermal oxidation at the same TGO thickness, showing additional damage induced in thermal cycles. Then, a new TBC life prediction model based on the nonlinear accumulation of oxidation damage and cyclic damage was developed, and the error between the damage prediction and the testing results was found to be no more than +/- 10%.

学科主题界面力学与表面力学 ; 损伤力学 ; 实验固体力学 ; 航空、航天推进系统
分类号一类
资助项目China Natural Science Foundation[51905510]
WOS关键词FAILURE CHARACTERISTICS ; LIFE PREDICTION ; OXIDATION ; MECHANISMS ; PROGRESS ; SYSTEM ; MODEL
WOS研究方向Science & Technology - Other Topics ; Materials Science ; Metallurgy & Metallurgical Engineering
语种英语
WOS记录号WOS:000517665100043
资助机构China Natural Science Foundation
其他责任者Yang, Junjie
内容类型期刊论文
源URL[http://dspace.imech.ac.cn/handle/311007/81571]  
专题空天飞行科技创新研究中心(筹)
作者单位1.Tsinghua Univ, Sch Aerosp Engn, Beijing, Peoples R China
2.Chinese Acad Sci, Inst Mech, Beijing, Peoples R China;
3.Tsinghua Univ, Inst Aero Engine, Beijing, Peoples R China;
4.Aero Engine Grp Corp China, Aero Engine Acad China, Beijing, Peoples R China;
推荐引用方式
GB/T 7714
Jing FL,Yang JJ,Yang ZM,et al. Critical compressive strain and interfacial damage evolution of EB-PVD thermal barrier coating[J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING,2020,776:9.
APA Jing FL,Yang JJ,Yang ZM,&Zeng W.(2020).Critical compressive strain and interfacial damage evolution of EB-PVD thermal barrier coating.MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING,776,9.
MLA Jing FL,et al."Critical compressive strain and interfacial damage evolution of EB-PVD thermal barrier coating".MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING 776(2020):9.
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace