Journal
COATINGS
Volume 13, Issue 2, Pages -Publisher
MDPI
DOI: 10.3390/coatings13020404
Keywords
thermal barrier coatings (TBCs); calcium-magnesium-alumina-silicate (CMAS); Hf6Ta2O17 ceramic; corrosion behavior; corrosion resistance mechanism
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Thermal barrier coatings (TBCs) face a serious threat from calcium-magnesium-alumina-silicate (CMAS) corrosion. The search for new ceramic coatings with excellent resistance to CMAS corrosion for TBCs is ongoing. This study investigates the CMAS corrosion resistance behavior and mechanism of a promising Hf6Ta2O17 ceramic coating. Results show that temperature is the most important factor affecting CMAS behavior and mechanism, with different corrosion products formed at different temperatures.
Thermal barrier coatings (TBCs) have been seriously threatened by calcium-magnesium-alumina-silicate (CMAS) corrosion. The search for novel ceramic coatings for TBCs with excellent resistance to CMAS corrosion is ongoing. Herein, CMAS corrosion resistance behavior and the mechanism of a promising Hf6Ta2O17 ceramic coating for TBCs are investigated. The results show that temperature is the most important factor affecting the CMAS behavior and mechanism. At 1250 degrees C, the corrosion products are composed of dense reaction products (HfSiO4, CaXHf6-xTa2O17-x) and CMAS self-crystallization products. At 1300 and 1400 degrees C, the corrosion products are mainly dense CaTa2O6 and HfO2, which prevent further CMAS infiltration.
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