| 发明名称 |
Ceramic matrix composite rotor disk for a gas turbine engine and corresponding rotor module |
| 摘要 |
A ceramic matrix composite (CMC) disk (64C) for a gas turbine engine (20) includes a CMC hub (68C) defined about an axis (A) and a multiple of CMC airfoils (66C) integrated with the CMC hub (68C). A corresponding rotor module (62) is also provided. |
| 申请公布号 |
EP2570601(A2) |
申请公布日期 |
2013.03.20 |
| 申请号 |
EP20120169218 |
申请日期 |
2012.05.24 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;ALVANOS, IOANNIS |
| 分类号 |
F01D5/28;C04B35/80;F01D5/06;F01D5/30;F01D5/34 |
主分类号 |
F01D5/28 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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