Enhanced cerium migration in ceria-stabilised zirconia

被引:32
作者
Thornton, J [1 ]
Majumdar, A [1 ]
McAdam, G [1 ]
机构
[1] Def Sci & Technol Org, Aeronaut & Maritime Res Lab, Port Melbourne, Vic 3207, Australia
关键词
zirconia; cerium; thermal barrier coatings; diffusion;
D O I
10.1016/S0257-8972(97)00487-8
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The metal components inside jet engines which are exposed to hot combustion gases often must be thermally insulated with thermal barrier coatings. Most thermal barrier coatings consist of a porous zirconia layer deposited over a NiCoCrAlY layer. However, the zirconia Layer can spall during thermal cycling unless it is stabilised to prevent the zirconia changing between its tetragonal and monoclinic phases. We have studied thermal barrier coatings in which the zirconia was stabilised by alloying with 2.5 wt.% yttria and 25 wt.% ceria. The spatial distributions of the cerium in the zirconia layer before and after heat treatment were studied using electron microscopy (backscattered electron imaging and X-ray analysis). The different phases present were identified by X-ray diffraction. We found that the cerium distribution in the newly-formed zirconia layer was essentially uniform. However, hearing at 1200 degrees C could cause the formation of cerium-rich zones provided the coating was not separated from the NiCoCrAlY layer and the substrate before heating. This implied an interaction between the zirconia and the underlying metal. Experiments in the presence of oxygen getters and experiments in vacuum both suggest that cerium migration in ceria-stabilised zirconia is enhanced at high temperatures (1100 degrees C) under reducing conditions. (C) 1997 Elsevier Science S.A.
引用
收藏
页码:112 / 117
页数:6
相关论文
共 20 条
[1]   FORMATION OF MONOCLINIC ZIRCONIA AT THE ANODIC FACE OF TETRAGONAL ZIRCONIA POLYCRYSTALLINE SOLID ELECTROLYTES [J].
BADWAL, SPS ;
NARDELLA, N .
APPLIED PHYSICS A-MATERIALS SCIENCE & PROCESSING, 1989, 49 (01) :13-24
[2]  
BAVONLEON A, 1992, ACTA METALL MATER, V40, P2717
[3]  
BENNETT A, 1986, MATER SCI TECH SER, V2, P257, DOI 10.1179/026708386790123378
[4]   A PHILOSOPHY FOR THERMAL BARRIER COATING DESIGN AND ITS CORROBORATION BY 10000-H SERVICE EXPERIENCE ON RB211 NOZZLE GUIDE VANES [J].
BENNETT, A ;
TORIZ, FC ;
THAKKER, AB .
SURFACE & COATINGS TECHNOLOGY, 1987, 32 (1-4) :359-375
[5]   PHASE-STABILITY OF ZIRCONIA-BASED THERMAL BARRIER COATINGS .2. ZIRCONIA CERIA ALLOYS [J].
BRANDON, JR ;
TAYLOR, R .
SURFACE & COATINGS TECHNOLOGY, 1991, 46 (01) :91-101
[6]  
CAWLEY JD, 1984, OVERVIEW ZIRCONIA RE
[7]  
CLARE JH, 1982, ASTM METALS HDB, V5, P361
[8]  
CLYNE TW, 1994, P 3 INT S STRUCT FUN
[9]  
JCPDS-Joint Commite on Powder Diffraction Standars, 1995, INT CTR DIFFR DAT
[10]   THE DEVELOPMENT OF HOT-CORROSION-RESISTANT ZIRCONIA THERMAL BARRIER COATINGS [J].
JONES, RL .
MATERIALS AT HIGH TEMPERATURES, 1991, 9 (04) :228-236