A camber adjustment system for a wing of an aircraft includes a droop panel that is configured to pivotally couple to a portion of a main body of a wing, a flap, and a coupler having a track that moveably couples the droop panel to the flap. The droop panel is configured to move in response to movement of the flap via the coupler.


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    Titel :

    CAMBER ADJUSTMENT SYSTEMS AND METHODS FOR AIRCRAFT WINGS


    Beteiligte:
    TSAI KEVIN R (Autor:in)

    Erscheinungsdatum :

    2019-10-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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