| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR LINER ASSEMBLY WITH CONVERGENT HYPERBOLIC PROFILE |
| 摘要 |
A heat shield for a combustor of a gas turbine engine includes a first edge with a first set of cantilevered members and a second edge with a second set of cantilevered members. |
| 申请公布号 |
WO2014189556(A2) |
申请公布日期 |
2014.11.27 |
| 申请号 |
WO2014US14819 |
申请日期 |
2014.02.05 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CUNHA, FRANK J.;ERBAS-SEN, NURHAK |
| 分类号 |
F23M5/04;F02C7/12;F23M5/08;F23R3/42 |
主分类号 |
F23M5/04 |
| 代理机构 |
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