The present invention provides a retractable vortex generator system for an aircraft, the system comprising a skin, a slot arranged on the skin, a plate comprising a contour configured for energizing the boundary layer of an air current, and driving means configured for rotating the plate between a first and a second position, wherein in the first position at least part of the contour of the plate protrudes through the slot, and in the second position the plate is retracted within the slot.


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    Title :

    RAZOR VORTEX GENERATOR


    Additional title:

    KLINGENWIRBELGENERATOR
    GÉNÉRATEUR DE VORTEX À LAME


    Contributors:

    Publication date :

    2024-08-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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