摘要
A protective coating, yttrium silicate/glass multi-layer for carbon/carbon (C/C) composites for the applications in aerospace and aircraft engines was discussed. It was observed that the SiC/gradient yttrium silicate/glass multilayer coating produced by pack cementation, plasma spray and sintering had excellent thermal shock resistance. This thermal shock resistance was found to be a good oxidation protective coating for C/C composites. It was found that the thermal shock resistance could protect the C/C composites from oxidation perfectly in air flowing by natural convection at 1773 K for 164 h.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 2356-2359 |
| 页数 | 4 |
| 期刊 | Carbon |
| 卷 | 42 |
| 期 | 11 |
| DOI | |
| 出版状态 | 已出版 - 2004 |
指纹
探究 'A new SiC/yttrium silicate/glass multi-layer oxidation protective coating for carbon/carbon composites' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver