Ceramic matrix composites (CMCs) are extensively utilized in aero engines due to their high-temperature stability; however, they are prone to environmental corrosion at high temperatures, and environmental barrier coatings (EBCs) are necessary to resist oxidation and corrosion. Among various EBC materials, AlTaO
4 offers high cost-effectiveness and low thermal expansion coefficients (TECs), but its resistance to SiO
2 erosion and high-temperature stability remain unclear. We investigated the influences of SiO
2 additions on the structures and thermal properties of AlTaO
4; and AlTaO
4 mixtures containing 10 wt.% SiO
2 were kept at 1400 °C for 30–120 h. AlTaO
4 exhibited excellent high-temperature phase stability, and SiO
2 dissolved into AlTaO
4 to generate a solid solution. XRD Rietveld refinement was employed to confirm the position of Si in the lattices, while SEM and EDS characterizations demonstrated the homogeneous distribution of Si, Al, and Ta elements. At 1200 °C, the TECs of SiO
2-AlTaO
4 (4.65 × 10
−6 K
−1) were close to those of SiC (4.5–5.5 × 10
−6 K
−1). Additionally, the addition of SiO
2 could reduce TECs of AlTaO
4, a feature that helped alleviate the interface thermal stress between AlTaO
4 and the Si bond coat in the EBC systems. At 900 °C, the thermal conductivity was reduced by 26.9% compared to that of AlTaO
4, and the lowest value was 1.65 W·m
−1·K
−1. Accordingly, SiO
2 will enter the lattices of AlTaO
4 after heat treatments at 1400 °C, and SiO
2 additions will reduce the thermal conductivity and TECs of AlTaO
4, which is beneficial for its EBC applications.
Full article