Thermal cycling behavior and failure mechanism of LaTi_2Al_9O_(19)/YSZ thermal barrier coatings exposed to gas flame

摘要

As a potential thermal barrier coating (TBC) material, lanthanum titanium aluminum oxide (LaTi_2Al_9O_(19), LTA) possesses excellent phase stability between room temperature and 1600°C and desirable thermo-physical properties, but its thermal cycling performance is rather poor partially due to the low fracture toughness. In this work, LTA/yttria stabilized zirconia (YSZ) double ceramic layer TBC was prepared and its thermal cycling lifetime was assessed by a gas burner facility at a coating surface temperature of 1300±50°C. Chipping of LTA layer, which was different from the failure mechanism of the traditional plasma-sprayed TBCs, was visible in the center part of the TBC after about 3000cycles, equaling to a holding time of 500h at 1300±50°C. The failure of the LTA layer was mainly due to the decomposition and sintering of LTA exposed to extremely high-temperature gas flame. Followed by another 1000cycles, the YSZ layer was also cracked along its interface to the bond coat.