AIRCRAFT
    2.
    发明公开
    AIRCRAFT 审中-公开

    公开(公告)号:EP3998207A1

    公开(公告)日:2022-05-18

    申请号:EP21158191.3

    申请日:2021-02-19

    摘要: The invention refers to an aircraft, particularly an aircraft capable of vertical take-off and landing, comprising a fuselage, and a variable lift body defining an aerofoil and being moveably attached to the fuselage, wherein the variable lift body is pivotable around a first axis extending in the wing span direction; wherein a rotary actor adapted to cause the variable lift body to pivot in relation to the fuselage arranged within the aerofoil.

    AIRCRAFT
    3.
    发明公开
    AIRCRAFT 审中-公开

    公开(公告)号:EP3998206A1

    公开(公告)日:2022-05-18

    申请号:EP21158188.9

    申请日:2021-02-19

    摘要: The invention refers to an aircraft (2), particularly an aircraft (2) capable of vertical take-off and landing, comprising a load carrying structure (4), and a variable lift body (6) defining an aerofoil (55) and being moveably attached to the load carrying structure (4), wherein the variable lift body (6) is pivotable around a first axis;
    wherein a rotary actor is adapted to cause the variable lift body (6) to pivot in relation to the load carrying structure (4) arranged within the aerofoil (55).

    AIRCRAFT FLAP-TO-FLAP SEAL
    4.
    发明公开

    公开(公告)号:EP3998195A1

    公开(公告)日:2022-05-18

    申请号:EP21158224.2

    申请日:2021-02-19

    IPC分类号: B64C7/00 B64C9/02 B64C29/00

    摘要: The invention refers to an aircraft, in particular to a vertical take-off and landing aircraft, and to a wing of such aircraft comprising a plurality of actuated flaps (2) each having at least one propulsion unit (4) included, the flaps BEING arranged next to each other along the wing span and independently actuated to pivot and further comprising an elastic seal in a gap between at least two of the flaps.