| 发明名称 |
GAS TURBINE ENGINE WITH DISTRIBUTED FANS |
| 摘要 |
A gas generator has at least one compressor rotor, at least one gas generator turbine rotor and a combustion section. A fan drive turbine is positioned downstream of a path of the products of combustion having passed over the at least one gas generator turbine rotor. The fan drive turbine drives a shaft and the shaft engages gears to drive at least three fan rotors. |
| 申请公布号 |
US2015226117(A1) |
申请公布日期 |
2015.08.13 |
| 申请号 |
US201514597510 |
申请日期 |
2015.01.15 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;McCune Michael E.;Chandler Jesse M.;Epstein Alan H.;O'Flarity Steven M.;Hanlon Christopher J.;Schneider William F.;Staubach Joseph B.;Kenyon James A. |
| 分类号 |
F02C3/107;F02C9/18;F02C3/067;F02C3/06 |
主分类号 |
F02C3/107 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a gas generator with at least one compressor rotor, at least one gas generator turbine rotor and a combustion section, and there being a fan drive turbine positioned downstream of a path of the products of combustion having passed over said at least one gas generator turbine rotor, said fan drive turbine driving a shaft and said shaft engaging gears to drive at least three fan rotors. |
| 地址 |
Hartford CT US |
