| 发明名称 |
GAS TURBINE ENGINE COMPOSITE AIRFOIL TRAILING EDGE |
| 摘要 |
An airfoil for a gas turbine engine includes first pressure and suction side layers forming a cavity and terminating in ends near a trailing edge. The first and second suction side layers are constructed from a composite material. A bridge is wrapped about the ends. |
| 申请公布号 |
US2015377046(A1) |
申请公布日期 |
2015.12.31 |
| 申请号 |
US201414767394 |
申请日期 |
2014.02.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Duelm Shelton O.;McCaffrey Michael G. |
| 分类号 |
F01D9/02 |
主分类号 |
F01D9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An airfoil for a gas turbine engine comprising:
first pressure and suction side layers forming a cavity and terminating in ends near a trailing edge, the first and second suction side layers constructed from a composite material; and a bridge wrapped about the ends. |
| 地址 |
Hartford CT US |
