发明名称 AIRCRAFT WING WITH KNUCKLED RIB STRUCTURE
摘要 An aircraft wing has hinged ribs, and a skin covering the ribs. The ribs each include plural rib sections, array from the leading edge of the wing, to the trailing edge of the wing, and a lock to hold the rib sections together in a deployed state or condition. The wings are initially in a stowed state, with the ribs and the rib sections having a curved chord, and deploy to the deployed state, in which the ribs have a straightened chord that defines an airfoil state. The wing may have foam material between the ribs to allow the wings to expand in the wingspan direction, for instance after the ribs have been placed in the deployed state.
申请公布号 US2013099050(A1) 申请公布日期 2013.04.25
申请号 US201113278477 申请日期 2011.10.21
申请人 SANDERSON TERRY M.;CHERRY MICHAEL S.;REANY JACK W. 发明人 SANDERSON TERRY M.;CHERRY MICHAEL S.;REANY JACK W.
分类号 B64C3/56;B64C3/38 主分类号 B64C3/56
代理机构 代理人
主权项
地址