发明名称 Horizontal Folding Wingtip
摘要 An apparatus of an aircraft, the apparatus may include a wing comprising an unfixed portion and a fixed portion. The unfixed portion movably may connect to the fixed portion. The unfixed portion may include a rotating portion to rotate the unfixed portion between a flight position and a folded position. The fixed portion may connect to the unfixed portion of the wing. A joint may allow rotation of the unfixed portion of the wing with respect to the fixed portion of the wing about a rotation axis.
申请公布号 US2016083074(A1) 申请公布日期 2016.03.24
申请号 US201514961895 申请日期 2015.12.08
申请人 The Boeing Company 发明人 Santini Gregory M.;Sakurai Seiya
分类号 B64C3/10 主分类号 B64C3/10
代理机构 代理人
主权项 1. An apparatus of an aircraft, the apparatus comprising: a wing comprising: an unfixed portion, and a fixed portion; the unfixed portion movably connected to the fixed portion, the unfixed portion comprising a rotating portion of the unfixed portion, the rotating portion configured to rotate between a flight position and a folded position; the fixed portion connected to the unfixed portion of the wing; and a joint configured to allow rotation of the unfixed portion of the wing with respect to the fixed portion of the wing about a rotation axis, the rotation axis being one or more of: vertical, substantially perpendicular to the wing, and substantially parallel to a yaw axis of the aircraft.
地址 Chicago IL US