A comparison of the thermal properties of ZrO2-Ln2O3 (Ln – Y, La, Nd, Sm, Gd) thermal barrier coatings
A comparison of the thermal properties of ZrO2-Ln2O3 (Ln – Y, La, Nd, Sm, Gd) thermal barrier coatings
Wednesday, May 13, 2015: 4:10 PM
Room 102B (Long Beach Convention and Entertainment Center)
In this work we are to report the results of our recent development in the field of powder synthesis and coating production with zirconia-based compositions and their thermal properties investigation. Four solid solutions and four “stoichiometric” phases from the ZrO2-Ln2O3 (Ln – Y, La, Nd, Sm, Gd) systems were chosen for comparison.
Thermal conductivity of all as-sprayed coatings was shown to be very low (0.35-0.90 W/m·K at 1000°C). During the heat treatment the processes of microstructure evolution, crystal structure ordering and phase transition occurred strongly affecting the thermal properties of coatings (especially in the first ~24 hours). This “initial growth” value is completely different for all thermal barrier coating compositions and microstructures. The present paper focuses on defining the key factors responsible for the difference of 50% to 250% in the coating thermal conductivity growth at the same heat treatment conditions.
See more of: Engineering TBCs and Abradables
See more of: Advanced Coatings for the Aerospace Industry
See more of: Advanced Coatings for the Aerospace Industry