Abstract
Space thin-walled components call for thermal barrier coatings (TBCs) that can withstand temperatures up to 1600 °C for extended durations. However, samples coated with pure yttria-stabilized zirconia (YSZ) coatings failed after only 90 s of exposure to this temperature. In this study, we propose durable GdTaO4/YSZ double-ceramic-layer TBCs to resist ultrahigh-temperature thermal shock. Compared with the pure YSZ coatings, the GdTaO4/YSZ coatings demonstrated significantly extended service lifetimes under thermal shock at 1600 °C. Cracking induced by thermally grown oxide (TGO) emerged as a primary failure mode for GdTaO4/YSZ-coated samples at this temperature. These findings enhance confidence in the application of TBCs in space engines operating at temperatures up to 1600 °C.
| Original language | English |
|---|---|
| Pages (from-to) | 29781-29791 |
| Number of pages | 11 |
| Journal | Ceramics International |
| Volume | 51 |
| Issue number | 19 |
| DOIs | |
| State | Published - Aug 2025 |
Keywords
- Space thin-walled components
- Spalling
- Stress
- Thermal barrier coatings
- Ultrahigh-temperature thermal shock
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