| 发明名称 |
AUXILIARY POWER UNIT WITH EXCESS AIR RECOVERY |
| 摘要 |
An auxiliary power unit for an aircraft, having an engine core, a compressor having an outlet in fluid communication with the engine core inlet, a turbine section in fluid communication with the engine core outlet, and an excess air duct having a first end in fluid communication with the compressor outlet and a second end in fluid communication with a turbine inlet of the turbine section. The excess air duct defines a flow path between the compressor outlet and the turbine section separate from the engine core. The auxiliary power unit may include a generator in driving engagement with the engine core to provide electrical power for the aircraft. A method of providing compressed air and electrical power to an aircraft is also discussed. |
| 申请公布号 |
US2016376022(A1) |
申请公布日期 |
2016.12.29 |
| 申请号 |
US201514750187 |
申请日期 |
2015.06.25 |
| 申请人 |
Pratt & Whitney Canada Corp. |
发明人 |
ULLYOTT Richard;JONES Anthony;JULIEN Andre;THOMASSIN Jean |
| 分类号 |
B64D41/00;H02K7/18;F02C3/04;F02B41/10;F02B53/02 |
主分类号 |
B64D41/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An auxiliary power unit for an aircraft, comprising:
an engine core; a compressor having an outlet in fluid communication with an inlet of the engine core; a turbine section in fluid communication with an outlet of the engine core; and an excess air duct having a first end in fluid communication with the outlet of the compressor and a second end in fluid communication with an inlet of a turbine of the turbine section, the excess air duct defining a flow path between the outlet of the compressor and the turbine section separate from the engine core. |
| 地址 |
Longueuil CA |
