发明名称 Stabilizer torque box assembly and method
摘要 In an embodiment of the disclosure, there is provided an apparatus to provide a panel stiffening element. The apparatus has an outer braided thermoplastic tube and an inner braided thermoplastic tube disposed within the outer braided thermoplastic tube. The apparatus further has a separation ply layer co-consolidated between the outer braided thermoplastic tube and the inner braided thermoplastic tube. The separation ply layer provides reinforcement and impact damage resistance to the inner braided thermoplastic tube in order to avoid a loss in structural loading capability.
申请公布号 US8844873(B2) 申请公布日期 2014.09.30
申请号 US201113244258 申请日期 2011.09.23
申请人 The Boeing Company 发明人 Marcoe Jeffery Lee
分类号 B64C1/06;B32B1/08;B64C3/00;B32B5/02;B32B27/12;B64C3/18;B32B15/08 主分类号 B64C1/06
代理机构 代理人
主权项 1. An apparatus to provide panel stiffening, the apparatus comprising: a plurality of braided thermoplastic tubular spar caps, each braided thermoplastic tubular spar cap comprising: an outer braided thermoplastic tube;an inner braided thermoplastic tube disposed within the outer braided thermoplastic tube; and,a separation ply layer co-consolidated between the outer braided thermoplastic tube and the inner braided thermoplastic tube and around an entire circumference of the inner braided thermoplastic tube, the separation ply layer comprising a metal foil and the separation ply layer providing reinforcement and impact damage resistance to the inner braided thermoplastic tube in order to avoid a loss in structural loading capability; and, one or more braided thermoplastic tubular truss ribs connected to the plurality of braided thermoplastic tubular spar caps via one or more connection assemblies.
地址 Chicago IL US