发明名称 Wing fold system
摘要 A wing fold system may move a second portion of a wing with respect to a first portion of the wing between flight position 301 and folded position 303. A first link may rotate in response to actuating an actuator. A second link may move in response to rotating of the first link. The second portion of the wing may move in response to moving the second link and the second portion may move with respect to the first portion of the wing. One of the first portion and the second portion may be a fixed portion of the wing and the other of the first portion and the second portion may be a wingtip of the wing.
申请公布号 US9415857(B2) 申请公布日期 2016.08.16
申请号 US201313962952 申请日期 2013.08.09
申请人 THE BOEING COMPANY 发明人 Fox Stephen John;Sakurai Seiya;Munsen Victor A.;Noble Jack S.;Skomorowski John Tony
分类号 B64C3/56;B64C23/06 主分类号 B64C3/56
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method of folding a wing, the method comprising: connecting a first opening in a first fixed portion of a wing to a first opening in an unfixed portion of a wing at a first joint; aligning a first opening in a first link to a second opening in the fixed portion at a second joint, the second joint being located in the fixed portion and distinct from the unfixed portion; actuating a link actuator that engages the first link and causes the first link to rotate concentrically about the first opening of the first link and the second joint; connecting the first link to a second link via aligning a second opening of the first link with a first opening in the second link at a third joint located distinct from both the fixed portion and the unfixed portion; aligning and connecting a second opening in the second link to a second opening in the unfixed portion at a fourth joint, such that rotating the first link concentrically about the first opening of the first link and the second joint causes rotating the second link about a fourth joint and thereby moving the unfixed portion of the wing with respect to the fixed portion of the wing via rotating the unfixed portion of the wing concentrically about the first joint and the first opening of the unfixed portion; said method further comprising sensing a position of one of the first link and the second link via a group of sensors; and a link actuator driving a torque tube having at least one toothed member, the toothed member fitting with teeth engaging the first link and causing the third joint to rotate about the second joint located in the first fixed portion of the wing,the toothed member being located between the first joint and the second joint.
地址 Chicago IL US