| 发明名称 |
Ceramic matrix composite platform assembly for an airfoil of a gas turbine engine and corresponding rotor disk assembly |
| 摘要 |
A ceramic matrix composite (CMC) platform for an airfoil (66C) of a gas turbine engine (20) includes a CMC platform segment (86,88) which at least partially defines an airfoil profile. A corresponding rotor disk assembly (64c) is also provided. |
| 申请公布号 |
EP2570603(A2) |
申请公布日期 |
2013.03.20 |
| 申请号 |
EP20120169221 |
申请日期 |
2012.05.24 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;ALVANOS, IOANNIS;DYE, CHRISTOPHER M.;LEVASSEUR, GLENN |
| 分类号 |
F01D5/28;C04B35/80;F01D5/14;F01D5/22;F01D11/00;F01D25/24 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
