Composite ceramics thermal barrier coatings of yttria stabilized zirconia for aero-engines

被引：136
作者：
Liu, Qiaomu [1 ]
Huang, Shunzhou [1 ]
He, Aijie [1 ]
机构：
[1] AECC Sichuan Gas Turbine Estab, Chengdu 610500, Sichuan, Peoples R China
来源：
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY | 2019年 / 35卷 / 12期
关键词：
Composite ceramics; Thermal barrier coatings; Aero-engine; Yttria stabilized zirconia; Phase stability; Thermal conductivity; Failure mechanism; EB-PVD TBCS; PHASE-STABILITY; INTERDIFFUSION BEHAVIOR; OXIDATION BEHAVIOR; CYCLIC OXIDATION; ALUMINUM-OXIDE; HOT CORROSION; GROWN OXIDE; CONDUCTIVITY; MECHANISMS;
D O I：
10.1016/j.jmst.2019.08.003
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Composite ceramics thermal barrier coatings (TBCs) are widely used in the aero-engines field due to their excellent thermal insulation, which improves the service life and durability of the inherent hot components. The most typical, successful and widely used TBCs material is yttria stabilized zirconia (YSZ). In this paper, fabrication methods, coating structures, materials, failure mechanism and major challenges of YSZ TBCs are introduced and reviewed. The research tendency is put forward as well. This review provides a good understanding of the YSZ TBCs and inspires researchers to discover versatile ideas to improve the TBCs systems. (C) 2019 Published by Elsevier Ltd on behalf of The editorial office of Journal of Materials Science & Technology.
引用
收藏
页码：2814 / 2823
页数：10
相关论文
共 84 条
[1]  
Angenete J, 2004, SURF COAT TECH, V176, P272, DOI 10.1016/S0257(03)00767-9
[2]   Cyclic oxidation and interdiffusion behavior of a NiAlDy/RuNiAl coating on a Ni-based single crystal superalloy [J].
Bai, Bo ;
Guo, Hongbo ;
Peng, Hui ;
Peng, Liquan ;
Gong, Shengkai .
CORROSION SCIENCE, 2011, 53 (09) :2721-2727
[3]   Thermal properties of oxides with magnetoplumbite structure for advanced thermal barrier coatings [J].
Bansal, Narottam P. ;
Zhu, Dongming .
SURFACE & COATINGS TECHNOLOGY, 2008, 202 (12) :2698-2703
[4]   Interdiffusion behaviour in aluminide-coated Rene 80H at 1150 degrees C [J].
Basuki, E ;
Crosky, A ;
Gleeson, B .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1997, 224 (1-2) :27-32
[5]   PACK CEMENTATION ALUMINIDE COATINGS ON SUPERALLOYS - CODEPOSITION OF CR AND REACTIVE ELEMENTS [J].
BIANCO, R ;
RAPP, RA .
JOURNAL OF THE ELECTROCHEMICAL SOCIETY, 1993, 140 (04) :1181-1190
[6]  
Bornhorst B.R., 1961, X57072 NASA, P227
[7]   THERMAL BARRIER COATING LIFE AND ISOTHERMAL OXIDATION OF LOW-PRESSURE PLASMA-SPRAYED BOND COAT ALLOYS [J].
BRINDLEY, WJ ;
MILLER, RA .
SURFACE & COATINGS TECHNOLOGY, 1990, 43-4 (1-3) :446-457
[8]   Ceramic materials for thermal barrier coatings [J].
Cao, XQ ;
Vassen, R ;
Stoever, D .
JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 2004, 24 (01) :1-10
[9]  
Cao XQ, 2001, J AM CERAM SOC, V84, P2086, DOI 10.1111/j.1151-2916.2001.tb00962.x
[10]   Calcium-magnesium-alumina-silicate (CMAS) delamination mechanisms in EB-PVD thermal barrier coatings [J].
Chen, X .
SURFACE & COATINGS TECHNOLOGY, 2006, 200 (11) :3418-3427
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