Influence of bondcoat pre-treatment and surface topology on the lifetime of EB-PVD TBCs

被引:63
作者
Lau, H [1 ]
Leyens, C
Schulz, U
Friedrich, C
机构
[1] DLR, Inst Mat Res, German Aerosp Ctr, D-5000 Cologne, Germany
[2] MTU Aero Engn GmbH, Munich, Germany
关键词
thermally grown oxide; surface topology; pre-treatment; aspect ratio; PtAl; NiCoCrAlY;
D O I
10.1016/S0257-8972(02)00726-0
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
In the present study two types of bondcoats (BC) were used, a NiCoCrAlY overlay coating produced by electron beam physical vapor deposition (EB-PVD) and a platinum aluminide diffusion coating (Ni,Pt)-Al. The coatings were deposited onto nickel-base IN100 and Rene142 substrates and were pre-treated in vacuum or Ar-H gas mixture prior to the deposition of an EB-PVD yttria partially stabilized zirconia top coat. The specimens were thermal cyclically tested in air at 1100 degreesC (50 min at 1100 degreesC/ 10 min forced air cooling). The microstructures of the thermally grown oxide (TGO) layers prior and after testing were examined by scanning electron microscopy and electron energy dispersive spectroscopy. Heat-treatment in Ar-H significantly improved the lifetime of the thermal barrier coatings (TBC) system with IN100+PtA1 BC, whereas reduced lifetimes were found on IN100+ NiCoCrAlY BC and Rene142+PtA1. High Y-contents of the NiCoCrAlY BC significantly reduced TBC lifetimes. Furthermore, the results for IN100+PtA1 and Rene142+PtA1 demonstrated that early TBC failure was associated with high TGO surface roughness of the metal/oxide interface, indicating that surface roughness has a significant effect on TBC system performance. (C) 2002 Elsevier Science B.V. All rights reserved.
引用
收藏
页码:217 / 223
页数:7
相关论文
共 17 条
[11]   Substrate and bond coat compositions: factors affecting alumina scale adhesion [J].
Pint, BA ;
Wright, IG ;
Lee, WY ;
Zhang, Y ;
Prussner, K ;
Alexander, KB .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1998, 245 (02) :201-211
[12]   PVD thermal barrier coating applications and process development for aircraft engines [J].
Rigney, DV ;
Viguie, R ;
Wortman, DJ ;
Skelly, DW .
JOURNAL OF THERMAL SPRAY TECHNOLOGY, 1997, 6 (02) :167-175
[13]   Substrate alloy element diffusion in thermal barrier coatings [J].
Schilbe, JE .
SURFACE & COATINGS TECHNOLOGY, 2000, 133 :35-39
[14]   Influence of substrate material on oxidation behavior and cyclic lifetime of EB-PVD TBC systems [J].
Schulz, U ;
Menzebach, M ;
Leyens, C ;
Yang, YQ .
SURFACE & COATINGS TECHNOLOGY, 2001, 146 :117-123
[15]   Mechanisms of spallation of electron beam physical vapor deposited thermal barrier coatings with and without platinum aluminide bond coat ridges [J].
Vaidyanathan, K ;
Gell, M ;
Jordan, E .
SURFACE & COATINGS TECHNOLOGY, 2000, 133 :28-34
[16]  
WARNES BM, 1997, SURF COAT TECH, V1, P94
[17]  
Wright PK, 1998, MAT SCI ENG A-STRUCT, V245, P191, DOI 10.1016/S0921-5093(97)00850-2