Abstract
Screening multifunctional thermal/environmental barrier coatings (T/EBCs) for ceramic matrix composites (CMCs) and alloys contribute to developing highly efficient hypersonic vehicles and aeroengines. This work elucidates that Zr–Ta–O composites are T/EBCs for Al2O3 fiber-reinforced Al2O3 (Al2O3f/Al2O3) CMCs and alloys. Zr–Ta–O composites have superiorities of glass-like thermal conductivity (1.4 W m–1 K–1), thermal expansion coefficients (8.6–12.3 × 10–6 K–1) matching to Al2O3f/Al2O3 and alloys, and high toughness (3.4 MPa m1/2). The origins of high toughness are elucidated from crack-propagation models and formation of micro-cracks, which consume lots of crack fracture energy and relieve the stress concentration of indentation tips. The long-range-ordered and short-range-disordered arrangements of cations and the highly twisting lattices of Ta2Zr6O17 significantly contribute to their glass-like thermal conductivity. This work motivates upcoming study and application of Zr–Ta–O composites as T/EBCs with working temperature reaching 1500°C.
Original language | English |
---|---|
Pages (from-to) | 6508-6516 |
Number of pages | 9 |
Journal | Journal of the American Ceramic Society |
Volume | 105 |
Issue number | 11 |
Early online date | 12 Jun 2022 |
DOIs | |
Publication status | Published - Nov 2022 |
Scopus Subject Areas
- Ceramics and Composites
- Materials Chemistry
User-Defined Keywords
- fracture toughness
- microstructures
- nano-indentation
- T/EBCs
- thermal conductivity