发明名称 Auxiliary power unit assembly
摘要 An embodiment of the technology described herein is an auxiliary power unit assembly (10). The auxiliary power unit assembly (10) includes an auxiliary power unit being installable in an aircraft (18) having a cabin (22), a duct (28) connecting the cabin (22) and the auxiliary power unit, and a noise reduction feature (26) in the duct (28).
申请公布号 EP1918201(A1) 申请公布日期 2008.05.07
申请号 EP20070119514 申请日期 2007.10.29
申请人 GENERAL ELECTRIC COMPANY 发明人 SHELDON, KARL EDWARD;SEELEY, CHARLES ERKLIN;HABER, LUDWIG CHRISTIAN;WOOD, TREVOR HOWARD;LUEDKE, JONATHAN GLENN;SHIEH, CHINGWEI MICHAEL
分类号 B64D33/02;B64D41/00;F02C7/045;F02C7/32 主分类号 B64D33/02
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