发明名称 INTEGRATED AIRCRAFT FLOOR WITH LONGITUDINAL BEAMS
摘要 An integrated floor for an aircraft fuselage includes a composite panel forming a floor surface and composite beams bonded to the floor panel. The beams extend longitudinally within the fuselage and support the floor.
申请公布号 US2010243803(A1) 申请公布日期 2010.09.30
申请号 US20090411615 申请日期 2009.03.26
申请人 THE BOEING COMPANY 发明人 WESTRE WILLARD N.;RETZ KEVIN M.
分类号 B64C1/18 主分类号 B64C1/18
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