A Review on Ceramic Matrix Composites and Environmental Barrier Coatings for Aero-Engine: Material Development and Failure Analysis

被引:37
作者
Fang, Guangwu [1 ,2 ,3 ]
Gao, Xiguang [2 ,3 ]
Song, Yingdong [2 ,3 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Gen Aviat & Flight, Liyang 213300, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, Nanjing 210016, Peoples R China
关键词
failure modeling; ceramic matrix composites; environmental barrier coatings; aero-engine; SILICON BOND COAT; HIGH-TEMPERATURE; MECHANICAL-PROPERTIES; SIC/SIC COMPOSITES; RESIDUAL-STRESS; CORROSION BEHAVIOR; OXIDATION BEHAVIOR; FATIGUE BEHAVIOR; SIC FIBERS; EVOLUTION;
D O I
10.3390/coatings13020357
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Ceramic matrix composites with environmental barrier coatings (CMC/EBCs) are the most promising material solution for hot section components of aero-engines. It is necessary to access relevant information and knowledge of the physical properties of various CMC and EBCs, the characteristics of defects and damages, and relevant failure mechanisms. Then, effective failure prediction models can be established. Individually assessing the failure of CMC and EBCs is not a simple task. Models considering the synergetic effect of coating properties and substrate fibrous architecture are more reasonable and more challenging. This paper offers a review and a detailed description of the materials features, failure mechanism, and failure modeling for both CMC substrate and EBC coatings. The various methods for failure analyses and their pros and cons are discussed. General remarks on technical development for failure modeling are summarized subsequently.
引用
收藏
页数:17
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