The invention discloses a multifunctional coaxial double-rotor-wing four-shaft aircraft. Four supporting arms are arranged on a machine body. A drive device is arranged at one end of each supporting arm, and comprises a fixed base. A third motor and a fourth motor are arranged in each fixed base. A first rotating shaft and a second rotating shaft which are coaxial are arranged on each fixed base. Each second rotating shaft is sleeved with the corresponding first rotating shaft. A first rotor wing is arranged on the top of each first rotating shaft. A second rotor wing is arranged on the top of each second rotating shaft. Each first rotor wing and the corresponding second rotor wing are opposite in rotating direction. The output of each third motor is connected with the corresponding first rotating shaft, and the output of each fourth motor is connected with the corresponding second rotating shaft. A multifunctional system is integrated on the aircraft. A coaxial double-rotor-wing simplified control system is adopted by the aircraft, and the load capacity is improved; solar power generation and wireless charging are adopted, ultra-long runtime is achieved, and the flight distance is increased; multiple functions are integrated, and the utilization rate is increased.


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    Titel :

    Multifunctional coaxial double-rotor-wing four-shaft aircraft


    Beteiligte:
    LIANG CHAO (Autor:in) / LIANG HAO (Autor:in) / HE HUAGUANG (Autor:in) / CHEN WEIQI (Autor:in)

    Erscheinungsdatum :

    2015-09-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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