The invention provides a wing-adjustment controlled helicopter and relates to the technical field of flight. A top propeller completes action force in the air, a wing adjustment device completes rising, falling, advancing, retreating and turning multiple-direction control flight and air berthing, a propeller mounted at the top is composed of two layers of multiple blades, the wing adjustment device is formed by mounting a plurality of wing plates, work is controlled by a control panel mounted at the front part of a plane shell, a transmission shaft with a clutch is mounted backwards at the upper part of a plane shell framework, a propeller shaft is driven to work, a control table, a control rod, a control panel, a seat, a battery pack installation position, an engine installation position and the like are mounted in the plan shell, an undercarriage is mounted at the lower part of the plan shell, an automatic transverse tuning connection tail piece is mounted at the rear part, multipurpose lamps are mounted at the front part and the tail part, other accessories are mounted, and the design is reasonable and novel.


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    Titel :

    Wing-adjustment controlled helicopter


    Beteiligte:
    YU DAICHUAN (Autor:in)

    Erscheinungsdatum :

    23.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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