A system for a tail-sitter aircraft includes a fuselage having one or more propellers, a wing structure coupled to the fuselage, and a drag rudder assembly coupled to the wing structure, the drag rudder assembly including a first planar member that is coupled to a second planar member. The drag rudder assembly is configured to produce a stabilizing force on the wing structure during higher speeds of the aircraft in tandem rotor flight.


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    Titel :

    VERTICAL TAKE-OFF AND LANDING DRAG RUDDER


    Beteiligte:
    SCOTT MARK W (Autor:in) / CHEREPINSKY IGOR (Autor:in)

    Erscheinungsdatum :

    29.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge