摘要
SiCf/SiC ceramic matrix composites meet the high thrust-to-weight ratio requirements of next-generation aeroengines but require environmental barrier coatings for protection under extreme high-temperature conditions. Current environmental barrier coatings inevitably develop cracks during service, necessitating self-healing coatings for autonomous crack repair. In this study, based on Yb2Si2O7, Yb2Si2O7-SiC and Yb2Si2O7-Yb2SiO5 were fabricated via spark plasma sintering and pressureless sintering, respectively. The self-healing behavior of these composites was investigated to evaluate their feasibility as environmental barrier coating materials. Results show that adding 5wt% ~10wt% SiC to Yb2Si2O7 promoted crack healing after 1 h at 1100 °C in air, driven by SiO2 formation from SiC oxidation, which filled cracks through volume expansion. However, at 1300 °C, excessive SiC oxidation caused significant volumetric stress, generating new cracks within the composites. Yb2SiO5 addition enhanced material densification and crack healing. The composite with 50wt% Yb2SiO5 achieved optimal healing efficiency (78%), attributed to thermally induced compressive stress from higher thermal expansion coefficient of Yb2SiO5. This stress facilitated crack closure in the Yb2Si2O7 matrix.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 217-225 |
| 页数 | 9 |
| 期刊 | Materials China |
| 卷 | 44 |
| 期 | 3 |
| DOI | |
| 出版状态 | 已出版 - 2025 |
| 已对外发布 | 是 |
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