发明名称 Variable pitch airfoils
摘要 An apparatus may comprise an inflatable control surface for an aircraft and an end of the inflatable control surface configured for attachment to a fuselage of the aircraft. The end of the inflatable control surface may be configured to be rotated about an axis to control movement of the aircraft during flight.
申请公布号 US8393576(B2) 申请公布日期 2013.03.12
申请号 US201213445708 申请日期 2012.04.12
申请人 LUTKE KEVIN REED;KUTZMANN AARON JONATHAN;THE BOEING COMPANY 发明人 LUTKE KEVIN REED;KUTZMANN AARON JONATHAN
分类号 B64C3/00 主分类号 B64C3/00
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