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Details for article 12 of 13 found articles
| Title: |
Thermal barrier coating by electron beam-physical vapor deposition of zirconia co-doped with yttria and niobia |
| Author: |
Daniel Soares de Almeida Carlos Alberto Alves Cairo Cosme Roberto M. Silva Maria do Carmo A. Nono |
| Appeared in: |
Journal of aerospace technology and management |
| Paging: | Volume 2 (2010) nr. 2 pages 195-202 |
| Year: |
2010 |
| Contents: |
The most usual ceramic material for coating turbine blades is yttria doped zirconia. Addition of niobia, 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 was to evaluate the influence of the addition of niobia on the microstructure and thermal properties of the ceramic coatings. SEM on coatings 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 percent increases, the tetragonality increases. A significant reduction of the thermal conductivity, measured by laser flash technique in the zirconia coating co-doped with yttria and niobia when compared with zirconia-yttria coating was observed. |
| Publisher: |
Institute of Aeronautics and Space (provided by DOAJ) |
| Source file: |
Elektronische Wetenschappelijke Tijdschriften |
Details for article 12 of 13 found articles
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