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Thermal barrier coatings by electron beam-physical vapor deposition of zirconia co-doped with yttria and niobia
2010
Journal of Aerospace Technology and Management
The most usual ceramic material for coating turbine blades is yttria doped zirconia. Addition of niobia, as a co-dopant in the Y 2 O 3 -ZrO 2 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
doi:10.5028/jatm.2010.02026910
fatcat:keu7n53ehjfljnagf2yorghrse