Devices and systems of the inventive concept provide an aircraft flap system is deflected to achieve minimum drag in cruise, maximum coefficient of lift (CL) at low speed, and minimum download in hover. It does so by opening a gap or slot between an aircraft's wing body and an associated trailing flap during hover flight, while providing a continuous aerodynamic contour under other conditions.


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    Titel :

    Slotted Wing Flaps For A VTOL Aircraft


    Beteiligte:
    KAREM ABE (Autor:in) / PARCELL JOHN PAUL (Autor:in)

    Erscheinungsdatum :

    30.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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