发明名称 AIRCRAFT CABIN AIRFLOW NOZZLES AND ASSOCIATED SYSTEMS AND METHODS
摘要 Aircraft cabin airflow nozzles and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes a cabin air nozzle (220) that in turn has a first passageway (223a) bounded at least in part by a first wall portion (222a) and a second wall portion (222b) spaced apart from the first wall portion. The second wall portion (222b) can have a first surface exposed to air within the first passageway (223a), and a second surface facing away from the first surface. The first passageway (223a) can have an exit (232) between the first and second wall portions, and the second passageway (223b) can be positioned to direct air along the second surface of the wall portion.
申请公布号 WO2009032497(A1) 申请公布日期 2009.03.12
申请号 WO2008US73043 申请日期 2008.08.13
申请人 THE BOEING COMPANY;HLAVKA, BRIAN D.;PATTIE, JODY H. 发明人 HLAVKA, BRIAN D.;PATTIE, JODY H.
分类号 B64D13/00 主分类号 B64D13/00
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