CMAS resistance characteristics of Gd2(Hf0.7Ce0.3)2O7 thermal barrier material at 1300 °C and 1400 °C

The corrosion resistance to calcium‑magnesium‑aluminum-silicate (CMAS) is a key property affecting the long-term durability of thermal barrier coatings (TBCs). Meanwhile, rare-earth hafnates are considered promising TBC candidates due to their low thermal conductivity and suitable thermal expansion coefficients. Thus, this study explores the CMAS corrosion resistance of Gd2(Hf0.7Ce0.3)2O7 (GH7C3) ceramic material under different conditions and compares it with the binary system Gd2Hf2O7 (GH) ceramic material. The findings indicate that GH7C3 can react chemically with CMAS and rapidly form a dense apatite crystalline layer at the interface between GH7C3 ceramic and CMAS, providing excellent CMAS resistance. Furthermore, the composition of the remaining CMAS melt Furthermore, the composition of the remaining CMAS melt undergoes compositional changes upon interaction, ultimately forming spinel in Mg and Al-enriched regions. In the meantime, CeO2 can promote the rapid formation of apatite crystals, significantly enhancing the CMAS resistance of GH7C3 to CMAS at high temperatures compared to GH. •The Gd2(Hf0.7Ce0.3)2O7 (GH7C3) exhibited excellent resistance to CMAS corrosion.•Under the attack of CMAS, the Ce element in GH7C3 can promote the rapid crystallization of Gd-apatite.•In the GH7C3/CMAS system, apatite crystals can form a dense layer that effectively blocks further corrosion by CMAS.