发明名称 |
COMPOUND ENGINE ASSEMBLY WITH DIRECT DRIVE OF GENERATOR |
摘要 |
A compound engine assembly for use as an aircraft auxiliary power unit, having an engine core including internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the engine core inlet, and a turbine section having an inlet in communication with the engine core outlet and configured to compound power with the engine core. The turbine section may include a first stage turbine having an inlet in communication with the engine core outlet, and a second stage turbine having an inlet in communication with the first stage turbine outlet. A method of providing electrical power to an aircraft is also discussed. |
申请公布号 |
WO2016205934(A1) |
申请公布日期 |
2016.12.29 |
申请号 |
WO2016CA50724 |
申请日期 |
2016.06.20 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
ULLYOTT, Richard;JONES, Anthony;JULIEN, André;THOMASSIN, Jean |
分类号 |
F02B53/14;B64D41/00;F02B33/40;F02B37/02;F02B41/10;F02B63/04 |
主分类号 |
F02B53/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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