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196 条记录 (耗时 0.022 秒)

    FLIGHT CONTROL SURFACE
    4.
    发明公开
    FLIGHT CONTROL SURFACE 审中-公开

    公开(公告)号：EP4345000A1

    公开(公告)日：2024-04-03

    申请号：EP23197104.5

    申请日：2023-09-13

    申请人： Airbus Operations Limited

    发明人： FAMILY, Oliver

    IPC分类号： B64C9/20 ,  B64C3/50

    摘要： An aircraft wing with an array of moveably flight control surfaces (20), each flight control surface (20) having a trailing edge (16) with a moveable tab (15) attached to the flight control surface trailing edge (16). A flight control system coupled to a flight control surface (20) drive system which moves the flight control surfaces (20); a tab drive system which moves the moveable tabs (15) and one or more aircraft angle of attack sensors. The flight control system stores a set of angular deflections to deflect the tabs upwardly when the angle of attack reaches a threshold.

    WING FOR AN AIRCRAFT
    5.
    发明公开
    WING FOR AN AIRCRAFT 审中-公开

    公开(公告)号：EP4303123A1

    公开(公告)日：2024-01-10

    申请号：EP23181114.2

    申请日：2023-06-23

    申请人： Airbus Operations GmbH

    发明人： BENSMANN, Stefan

    IPC分类号： B64C9/02 ,  B64C3/50 ,  B64C9/22 ,  B64C9/16 ,  B64C9/08 ,  B64C13/28 ,  B64C9/18 ,  B64C9/24 ,  B64C3/18 ,  B64C3/28 ,  F16H19/04 ,  B64C9/14

    摘要： A wing for an aircraft is proposed, comprising a leading edge as a first chordwise edge, a trailing edge as a second chordwise edge, an upper skin extending between the leading edge and the trailing edge, a lower skin extending between the leading edge and the trailing edge, at least one spar extending between the upper skin and the lower skin in a spanwise direction to create wing box with the upper skin and the lower skin, and at least one high lift control surface movably supported at at least one of the chordwise edges by a support device, wherein the support device is attached inside or reaches into the wing box at least partially.