发明名称 Dual flow APU inlet and associated systems and methods
摘要 Dual flow auxiliary power unit (APU) inlets and associated systems and methods are disclosed. An inlet in accordance with one embodiment of the invention includes an entrance aperture and a divider positioned in the inlet and located to separate a first portion of the inlet from a second portion of the inlet. The first portion can be configured to couple to an engine air intake of an APU, and the second portion can be configured to direct air away from the air intake. The divider can be positioned to direct air having a first total pressure level and a first distortion level to the first portion of the inlet, and direct air having a second total pressure level and second distortion level to the second portion of the inlet. The first total pressure level can be approximately the same as or higher than the second total pressure level, or the second distortion level can be approximately the same as or higher than the first distortion level, or both.
申请公布号 US7344107(B2) 申请公布日期 2008.03.18
申请号 US20040974167 申请日期 2004.10.26
申请人 THE BOEING COMPANY 发明人 CAMPBELL THOMAS A.;CHAMBERS DAVID S.;WILLIE ROBERT H.;RUST CHARLES W.
分类号 B64D41/00;F02C6/06;F02C7/04;F02C7/042 主分类号 B64D41/00
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