发明名称 Thermal management for aircraft auxiliary power unit compartment
摘要 An improved passive cooling system for an aircraft APU compartment that includes a lightweight annular air-cooled oil cooler that is strategically oriented and shrouded to face its annular inlet away axially downstream from the exhaust of the APU to make it inherently fireproof to flames from the APU or any location within the APU compartment that fuel can accumulate.
申请公布号 US7337605(B2) 申请公布日期 2008.03.04
申请号 US20040963363 申请日期 2004.10.11
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 HAGSHENAS BEZHAD
分类号 F02C7/06;B64D33/08;B64D41/00;F01D25/12;F02C7/12;F02C7/25;F02G3/00 主分类号 F02C7/06
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