| 发明名称 |
CERAMIC MATRIX COMPOSITE |
| 摘要 |
A novel ceramic matrix composite is disclosed for forming components that are operable in high temperature environments such those in gas turbine engines and the like. The ceramic matrix composite can include at least one layer of non-crimped fibers positioned substantially parallel to one another. A relatively small diameter elastic fiber can be constructed to stitch the non-crimped fibers together and a ceramic matrix may be deposited around the at least one layer of non-crimped fibers. |
| 申请公布号 |
US2014271161(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201314097857 |
申请日期 |
2013.12.05 |
| 申请人 |
Rolls-Royce Corporation |
发明人 |
Lazur Andrew Joseph |
| 分类号 |
F01D5/28;F01D9/02;F01D5/14 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A ceramic matrix composite comprising:
at least one layer of non-crimped fibers positioned substantially parallel to one another; a relatively small diameter elastic fiber constructed to stitch the non-crimped fibers together, and a ceramic matrix deposited around the at least one layer of non-crimped fibers. |
| 地址 |
Indianapolis IN US |
