Abstract

TBCs are increasingly susceptible to degradation by airborne CMAS deposits. In order to mitigate the CMAS attack, we fabricated a dense, crack-free alumina overlay for TBCs by electrophoretic deposition (EPD) technique. Overlay coatings of controlled thickness were successfully fabricated for YSZ TBCs, by EPD followed by controlled sintering at 1200 °C. YSZ with alumina overlay coatings were tested for CMAS attack at 1300 °C. Detailed examination of microstructural changes and phase evolution in CMAS tested specimens was performed by X-ray diffraction and electron microscopy. Dense alumina overlay produced by EPD was found to physically suppress the infiltration of CMAS. Furthermore, CMAS was found to crystallize into anorthite (CaAl 2Si 2O 8) and MgAl 2O 4 spinel by chemically interacting with EPD α-Al 2O 3. A shift in CMAS glass composition to a crystallizable Al-rich glass composition promoted the formation of anorthite platelets (CaAl 2Si 2O 8) and localized enrichment of Mg promoted the formation of MgAl 2O 4 spinel. EPD alumina overlay on commercial-production TBCs retained its adhesion and structural integrity after 20 cycles of 1-hour furnace thermal cycle test at 1100 °C.

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