发明名称 |
AUXILIARY POWER UNIT WITH INTERCOOLER |
摘要 |
An auxiliary power unit for an aircraft, having a compressor, an intercooler including first conduit(s) having an inlet in fluid communication with the compressor outlet and second conduit(s) configured for circulation of a coolant therethrough, an engine core having an inlet in fluid communication with an outlet of the first conduit(s), and a bleed conduit in fluid communication with the outlet of the first conduit(s) through a bleed air valve. The auxiliary power unit may include a generator in driving engagement with the shaft of 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 |
WO2016205932(A1) |
申请公布日期 |
2016.12.29 |
申请号 |
WO2016CA50722 |
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;B64D33/08;B64D41/00 |
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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