EB-PVD TBCs of zirconia co-doped with yttria and niobia, a microstructural investigation

被引:17
作者
Almeida, DS
Silva, CRM
Nono, MCA
Cairo, CAA
机构
[1] AMR CTA, Div Mat, Ctr Tecn Aeroespacial, BR-12228904 Sao Jose Dos Campos, Brazil
[2] INPE, LAS, Sao Jose Dos Campos, SP, Brazil
基金
巴西圣保罗研究基金会;
关键词
SEM; X-ray diffraction; electron beam evaporation; niobium oxide; zirconium oxide;
D O I
10.1016/j.surfcoat.2005.04.051
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Turbine blades of airplanes and thermoelectric plants work in adverse conditions, with corrosive environment and high temperature and pressure. One way to improve the life and/or the working temperature of the blades is the use of special coatings over metallic material applied by Electron Beam-Physical Vapor Deposition (EB-PVD). The most usual material for this application is yttria doped zirconia. Addition of mobia, as a co-dopant in the Y2O3-ZrO2 system, can reduce the thermal conductivity and improve mechanical properties of the coating. The purpose of this work is to show the influence of the addition of niobia on the microstructure of ceramic coatings by using X-ray diffraction (XRD) techniques and scanning electron microscopy (SEM) observations. SEM on fractured cross-section shows a columnar structure and the results of XRD show only zirconia tetragonal phase in the ceramic coating for the chemical composition range studied. As the difference (NbO2.5-YO1.5) mol% increases, the ratio c/a (tetragonality) increases. Considering that the t-ZrO2 solid solutions begins unstable when the relation c/a exceeds 1.020, it is possible to evaluate the maximum niobia content that can be added to the coating without losses in its mechanical properties. SEM on ceramic coatings polished cross-section shows color bands associated with chemical composition changes due to the differences in saturation vapor pressure of the individual components. As the niobia content increases, there is a tendency to reduction of the ceramic coating theoretical density. (c) 2005 Elsevier B.V. All rights reserved.
引用
收藏
页码:2827 / 2833
页数:7
相关论文
共 30 条
[1]  
ALMEIDA DS, 2002, AN C BRAS ENG CIEN M
[2]  
Bernier J. S., 2003, SURF COAT TECH, V95-99, P163
[3]  
COUTO P, 2003, FLASH METHOD STANDAR
[4]  
Czek N., 1999, SURF COAT TECH, V113, P157
[5]   Mechanics-based scaling laws for the durability of thermal barrier coatings [J].
Evans, AG ;
He, MY ;
Hutchinson, JW .
PROGRESS IN MATERIALS SCIENCE, 2001, 46 (3-4) :249-271
[6]   Progress in coatings for gas turbine airfoils [J].
Goward, GW .
SURFACE & COATINGS TECHNOLOGY, 1998, 108 (1-3) :73-79
[7]   Microstructure investigation on gradient porous thermal barrier coating prepared by EB-PVD [J].
Guo, HB ;
Bi, XF ;
Gong, SK ;
Xu, HB .
SCRIPTA MATERIALIA, 2001, 44 (04) :683-687
[8]   Effect of niobia on the defect structure of yttria-stabilized zirconia [J].
Guo, X ;
Wang, Z .
JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 1998, 18 (03) :237-240
[9]  
HASS DD, 2001, THESIS U VIRGINIA MA
[10]   X-RAY INTERACTIONS - PHOTOABSORPTION, SCATTERING, TRANSMISSION, AND REFLECTION AT E=50-30,000 EV, Z=1-92 [J].
HENKE, BL ;
GULLIKSON, EM ;
DAVIS, JC .
ATOMIC DATA AND NUCLEAR DATA TABLES, 1993, 54 (02) :181-342