A camber adjustment system for a wing of an aircraft includes a droop panel that is configured to moveably couple to a portion of the wing, a flap, a cam rod moveably coupled to the droop panel, a bell crank cam arm moveably coupled to the flap, and a jackscrew interface between the cam rod and the bell crank cam arm. The droop panel is configured to move in response to movement of the flap via the jackscrew interface.


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    Title :

    CAMBER ADJUSTMENT SYSTEMS AND METHODS FOR AIRCRAFT WINGS


    Contributors:

    Publication date :

    2020-01-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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