| 发明名称 |
Reverse Core Turbine Engine Mounted Above Aircraft Wing |
| 摘要 |
A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compressor section. A core engine inlet duct is spaced from the fan inlet. A method is also described. |
| 申请公布号 |
US2015300293(A1) |
申请公布日期 |
2015.10.22 |
| 申请号 |
US201314441633 |
申请日期 |
2013.03.04 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Suciu Gabriel L.;Chandler Jesse |
| 分类号 |
F02K1/64;F02C3/04 |
主分类号 |
F02K1/64 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a fan inlet and a fan configured to deliver air to an exhaust nozzle; a core gas turbine engine, including, in serial order extending further into the engine relative to the fan inlet, a core turbine section, a combustor and a core compressor section; and a core engine inlet duct spaced from said fan inlet relative to a fan radial center. |
| 地址 |
Hartford CT US |
