| 发明名称 |
GAS TURBINE ENGINE AND COMPOSITE PARTS. |
| 摘要 |
High strength, fracture tough, high temperature oxidatively stable, gas turbine engine core engine components are described made of silicon carbide fiber reinforced ceramic matrix or silicon carbide fiber reinforced glass matrix material. A gas turbine engine containing core engine components as above described is also disclosed. |
| 申请公布号 |
EP0131630(A4) |
申请公布日期 |
1986.07.08 |
| 申请号 |
EP19840901242 |
申请日期 |
1984.01.18 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PREWO, KARL, M.;BRENNAN, JOHN, J. |
| 分类号 |
B32B18/00;C03C14/00;C04B35/80;F01D5/28;F01D25/00;F23R3/00;(IPC1-7):B32B5/08;B32B5/12 |
主分类号 |
B32B18/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
