The invention provides a new concept vertical take-off and landing aircraft. The aircraft comprises a fuselage, wings, flaps, ailerons, horizontal stabilizers, elevators, a vertical stabilizer, a rudder, an undercarriage and engines, wherein each wing comprises an upper wing and a lower wing; the upper wing is connected with the upper part of the fuselage and the lower wing is connected with the lower part of the fuselage; the root of the upper wing is vertically connected with the root of the lower wing; the tail end of the lower wing is smoothly connected with the tail end of the upper wing obliquely upward; an upper shutter and a lower shutter are arranged on the upper wing; in the wings, driving belts are wound around driving fluted discs and guide wheels and are uniformly connected with a plurality of wing-shaped plates; the wing-shaped plates incline toward the movement direction; the driving fluted discs and the driving belts carry out driving in a matching mode; axles of the driving fluted discs are connected with clutch speed change gears; the clutch speed change gears are connected with the engines by drive mechanisms.


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    Titel :

    New concept vertical take-off and landing aircraft


    Beteiligte:
    LIU XINGUANG (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge