The invention provides a fixed-rotor rotation apparatus, comprising a body, a bar shaft, rotation pivots and fixed rotors, wherein the body is of a rectangular cabin structure and is a carrier for supporting and fixing every part, structure and system, the bar shaft is transversely arranged at a centre-of-gravity position located at the middle part of the upper end of the body, and left and right ends of the bar shaft are fixedly connected with the fixed rotors, the rotation pivots are arranged at joints of two sides of the upper end of the body and the bar shaft and can control rotation of the control bar shaft to realize control of the flight attitude of an airplane, and the fixed rotors are arranged at two sides of the body and connected with the bar shaft. The fixed-rotor rotation apparatus provided by the invention realizes safe and reliable control of rotors and is larger in take-off weight and faster in flight speed compared with an American osprey transporter.


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    Titel :

    Fixed-rotor rotation apparatus


    Beteiligte:
    SHEN JUNYONG (Autor:in)

    Erscheinungsdatum :

    24.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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