Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method
In the past decades, the durability of thermal barrier coatings (TBCs) has been extensively studied. The majority of researches emphasized the problem of oxidation, corrosion, and erosion induced by foreign object damage (FOD). TBCs with low thermal conductivity are usually coated on the hot-section...
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doaj-f2b752d46c12426a9b90fb06e480d8c62020-11-25T03:32:37ZengMDPI AGCoatings2079-64122020-07-011073273210.3390/coatings10080732Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element MethodZhong-Chao Hu0Bin Liu1Liang Wang2Yu-Hang Cui3Yan-Wei Wang4Yu-Duo Ma5Wen-Wei Sun6Yong Yang7School of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaCorrosion and Protection Laboratory, Key Laboratory of Superlight Materials and Surface Technology (Harbin Engineering University), Ministry of Education, Nantong ST 145, Harbin 150001, ChinaIntegrated Computational Materials Research Centre, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 201899, ChinaSchool of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaSchool of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaSchool of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaSchool of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaSchool of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, ChinaIn the past decades, the durability of thermal barrier coatings (TBCs) has been extensively studied. The majority of researches emphasized the problem of oxidation, corrosion, and erosion induced by foreign object damage (FOD). TBCs with low thermal conductivity are usually coated on the hot-section components of the aircraft engine. The main composition of the TBCs is top-coat, which is usually regarded as a wear-resistant and heat-insulating layer, and it will significantly improve the working temperature of the hot-section components of the aircraft engine. The application of TBCs are serviced under a complex and rigid environment. The external parts of the TBCs are subjected to high-temperature and high-pressure loading, and the inner parts of the TBCs have a large thermal stress due to the different physical properties between the adjacent layers of the TBCs. To improve the heat efficiency of the hot-section components of aircraft engines, the working temperature of the TBCs should be improved further, which will result in the failure mechanism becoming more and more complicated for TBCs; thus, the current study is focusing on reviewing the failure mechanism of the TBCs when they are serviced under the actual high temperature conditions. Finite element simulation is an important method to study the failure mechanism of the TBCs, especially under some extremely rigid environments, which the experimental method cannot realize. In this paper, the research progress of the failure mechanism of TBCs at high temperature via finite element modeling is systematically reviewed.https://www.mdpi.com/2079-6412/10/8/732thermal barrier coatings (TBCs)finite element methodthermal-mechanicalTGO (thermally growth oxide)failure mechanism |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Zhong-Chao Hu Bin Liu Liang Wang Yu-Hang Cui Yan-Wei Wang Yu-Duo Ma Wen-Wei Sun Yong Yang |
spellingShingle |
Zhong-Chao Hu Bin Liu Liang Wang Yu-Hang Cui Yan-Wei Wang Yu-Duo Ma Wen-Wei Sun Yong Yang Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method Coatings thermal barrier coatings (TBCs) finite element method thermal-mechanical TGO (thermally growth oxide) failure mechanism |
author_facet |
Zhong-Chao Hu Bin Liu Liang Wang Yu-Hang Cui Yan-Wei Wang Yu-Duo Ma Wen-Wei Sun Yong Yang |
author_sort |
Zhong-Chao Hu |
title |
Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method |
title_short |
Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method |
title_full |
Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method |
title_fullStr |
Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method |
title_full_unstemmed |
Research Progress of Failure Mechanism of Thermal Barrier Coatings at High Temperature via Finite Element Method |
title_sort |
research progress of failure mechanism of thermal barrier coatings at high temperature via finite element method |
publisher |
MDPI AG |
series |
Coatings |
issn |
2079-6412 |
publishDate |
2020-07-01 |
description |
In the past decades, the durability of thermal barrier coatings (TBCs) has been extensively studied. The majority of researches emphasized the problem of oxidation, corrosion, and erosion induced by foreign object damage (FOD). TBCs with low thermal conductivity are usually coated on the hot-section components of the aircraft engine. The main composition of the TBCs is top-coat, which is usually regarded as a wear-resistant and heat-insulating layer, and it will significantly improve the working temperature of the hot-section components of the aircraft engine. The application of TBCs are serviced under a complex and rigid environment. The external parts of the TBCs are subjected to high-temperature and high-pressure loading, and the inner parts of the TBCs have a large thermal stress due to the different physical properties between the adjacent layers of the TBCs. To improve the heat efficiency of the hot-section components of aircraft engines, the working temperature of the TBCs should be improved further, which will result in the failure mechanism becoming more and more complicated for TBCs; thus, the current study is focusing on reviewing the failure mechanism of the TBCs when they are serviced under the actual high temperature conditions. Finite element simulation is an important method to study the failure mechanism of the TBCs, especially under some extremely rigid environments, which the experimental method cannot realize. In this paper, the research progress of the failure mechanism of TBCs at high temperature via finite element modeling is systematically reviewed. |
topic |
thermal barrier coatings (TBCs) finite element method thermal-mechanical TGO (thermally growth oxide) failure mechanism |
url |
https://www.mdpi.com/2079-6412/10/8/732 |
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