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.


    Access

    Download


    Export, share and cite



    Title :

    Wing-adjustment controlled helicopter


    Contributors:
    YU DAICHUAN (author)

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Novel helicopter stub wing and helicopter

    XU WEI / CHEN HONGYU / XU JINPENG et al. | European Patent Office | 2021

    Free access

    Active spinning wing helicopter

    TAN YOUJUN | European Patent Office | 2021

    Free access

    Flip-wing helicopter structure

    JIANG HUAZHI / HE YINGLONG / HE YINGJUN | European Patent Office | 2021

    Free access

    Electric tilting helicopter wing

    ZHANG XIYUE / CHEN ZHIYOU / MENG XIANGJI et al. | European Patent Office | 2025

    Free access

    Helicopter rotor wing variable-pitch rod, helicopter automatic inclinator and helicopter

    NI MING / LI CHAOYANG / ZHENG YIHUA | European Patent Office | 2020

    Free access