The invention discloses a tilting four-rotor aircraft, and belongs to the field of power machinery of space flight. The tilting four-rotor aircraft comprises an aircraft body, a first rotor, a second rotor, a tilting unit and four sets of rotor units, wherein the tilting unit is arranged on the aircraft body, and comprises a first transverse shaft, a second transverse shaft, a first rotor mounting shaft, a second rotor mounting shaft, a third rotor mounting shaft and a fourth rotor mounting shaft; the first transverse shaft and the second transverse shaft are symmetrically arranged on two sides of the aircraft body; the first rotor mounting shaft and the second rotor mounting shaft are respectively fixed at two ends of the first transverse shaft; the first rotor unit is fixed on the first rotor mounting shaft, and the second rotor unit is fixed on the second rotor mounting shaft; the third rotor mounting shaft and the fourth rotor mounting shaft are respectively fixed at two ends of the second transverse shaft; the third rotor unit is fixed on the third rotor mounting shaft, and the fourth rotor unit is fixed on the fourth rotor mounting shaft; each of the rotating shaft of the first rotor unit, the rotating shaft of the second rotor unit, the rotating shaft of the third rotor unit, and the rotating shaft of the fourth rotor unit is perpendicular to the horizontal plane. The aircraft disclosed by the invention is relatively easy to control.


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    Title :

    Tilting four-rotor aircraft


    Contributors:
    HUANG FEI (author) / LEI MING (author) / CAI ZUORONG (author) / GAO HAIJUN (author) / DAI YITAO (author) / WU HUAMING (author) / ZHOU ZIMING (author) / ZHANG ZILONG (author)

    Publication date :

    2015-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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