An aircraft wing has a spoiler movable from a reference position with a deflection angle αref to a given target deflection angle αtarget by an actuator powered mechanism. An upstream edge of the spoiler is interconnected with the aircraft wing exclusively via a strip element made of a resiliently flexible material and via the actuator powered mechanism. A downstream edge of the strip element extends along the whole or at least along a major part of the upstream edge of the spoiler. The actuator powered mechanism is constructed and arranged such that, while moving the spoiler, the strip element is bent with a constant strain along the strip element. A cross-section of the strip element for all deflection angles α assumes the form of a ring segment with a radius R(α) at least within a given margin of failure, with α, αtarget, αrefε[−α1; α2].


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    Titel :

    AIRCRAFT WING WITH SPOILER


    Beteiligte:
    HANSEN HEINZ (Autor:in) / KIRN JOHANNES (Autor:in) / MACHUNZE WOLFGANG (Autor:in) / METZNER CHRISTIAN (Autor:in) / WEBER MARKUS J (Autor:in)

    Erscheinungsdatum :

    06.07.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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