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 |
DOI | 10.1016/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. |
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