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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    Title :

    Camber adjustment systems and methods for aircraft wings


    Contributors:

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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