A control surface of an aircraft comprises a fixed skin panel, a first flexurally elastic skin panel and a second flexurally elastic skin panel, which is connected to the first flexurally elastic skin panel and is configured to at least partially overlap the fixed skin panel. Furthermore, the control surface comprises an actuator system, which is configured to move the second flexurally elastic skin panel parallel to the fixed skin panel, wherein the actuator system has a fixed structural element arranged in a root region of the control surface, and a structural element that is movable relative to the fixed structural element.


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    Titel :

    CONTROL SURFACE FOR AN AIRCRAFT, AND AIRCRAFT HAVING A FLEXIBLE CONTROL SURFACE


    Beteiligte:
    BENTIVOGLIO MARC ANTONIO (Autor:in) / BIONDINI MARCO (Autor:in) / HOEFT MICHAEL (Autor:in) / LUETTMANN HENRIK (Autor:in) / WERWER MALTE (Autor:in) / THOMAS ANDRE (Autor:in)

    Erscheinungsdatum :

    21.03.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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