The invention relates to a multipoint-control vertiplane. The vertiplane is driven by lift force to lift off and propelled to fly. The vertiplane in the prior art has the defects that the structure is complicated, the number of elements and components is large, the operation is inconvenient, the degree of balance is not high, and the flight is influenced in complex weathers. The multipoint-control vertiplane comprises a vertiplane body, a propeller and wings, wherein a canopy is arranged on a vertiplane head of the vertiplane body; a seat cabin cover is arranged on a seat cabin of the vertiplane body; a rudder is arranged at the rear end of the vertiplane body; elevating rudders are arranged at side ends of the vertiplane body; and the seat cabin cover and the canopy are made of transparent organic materials. The multipoint-control vertiplane disclosed by the invention has the advantages that the control efficiency is higher, the fuels are saved, high balance degree can be maintained when the multipoint-control vertiplane takes off and lands, and the take-off ability in the complex weathers is remarkable.


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    Titel :

    Multipoint-control vertiplane


    Beteiligte:
    SU XI AN (Autor:in) / CAO YING (Autor:in)

    Erscheinungsdatum :

    10.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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