A method and apparatus for reducing bending moment on a wing of an aircraft can include at least one sensor provided on the aircraft configured to monitor a shape or position of the wing. The sensor can provide a change in the position or shape of the wing to a controller. The controller can operate one or more spoilers in response to the change in shape or position of the wings to reduce loading on the wings to reduce the bending moment.


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    Title :

    METHOD AND APPARATUS FOR REDUCING AIRCRAFT WING BENDING MOMENT


    Contributors:

    Publication date :

    2019-12-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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