A vertical take-off and landing unmanned plane comprises a body, a motor, a propeller and wings, and further comprises ailerons and vertical fins; the ailerons are in hinged connection with the wings, the number of the vertical fins is three or more, at least one vertical fin is arranged on the upper side of the vertical take-off and landing unmanned plane, at least one vertical fin is arranged on the lower side of the vertical take-off and landing unmanned plane, and the tail edges of at least part of the vertical fins are located at the rear parts of the tail edges of the wings. The tail edges of at least part of the vertical fins are located at the rear parts of the tail edges of the wings, so that when the vertical take-off and landing unmanned plane is vertically placed, the tail edges of the vertical fins are used as an undercart for supporting the vertical take-off and landing unmanned plane. The ailerons are in hinged connection with the wings, so that the vertical take-off and landing unmanned plane flight attitude can be changed by turning the ailerons, vertical takeoff and landing or sky hovering of the vertical take-off and landing unmanned plane can be realized, and high speed horizontal flight of the vertical take-off and landing unmanned plane can be realized.


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    Titel :

    Vertical take-off and landing unmanned plane


    Beteiligte:
    ZHANG JIE (Autor:in)

    Erscheinungsdatum :

    2016-02-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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