| 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 |
WO2014186011(A2) |
申请公布日期 |
2014.11.20 |
| 申请号 |
WO2014US16056 |
申请日期 |
2014.02.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DUELM, SHELTON O.;MCCAFFREY, MICHAEL G. |
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