According to the technical scheme, the electric tilting rotor aircraft is characterized by comprising an aircraft body, a wing system, an empennage, a rotor system and a tilting device, the wing system comprises wings and canards, the wings are symmetrically arranged along the two sides of the aircraft body, and the canards are arranged at the head of the aircraft body and symmetrically arranged along the two sides of the aircraft body; the tail part of the aircraft body is provided with an empennage, the rotor system comprises auxiliary rotor wings and tilting rotor wings, the auxiliary rotor wings are arranged at the wing ends of the wings, the tilting rotor wings are respectively arranged at the wing ends of the canards and the empennage, and the tilting device is used for connecting the rotor system with the wing system and the empennage. The electric tilt-rotor aircraft has the advantages of being capable of vertically taking off and landing, high in level flight speed, long in endurance time and excellent in aerodynamic performance.

    本发明公开了一种电动倾转旋翼飞行器,其技术方案要点是包括机体、机翼系统、尾翼、旋翼系统和倾转装置,所述机翼系统包括机翼和鸭翼,所述机翼沿机体两侧对称设置,所述鸭翼设置于机体的头部,并沿机体两侧对称设置,所述机体尾部设置有尾翼,所述旋翼系统包括辅翼旋翼和倾转旋翼,所述辅翼旋翼设置于机翼的翼端,所述倾转旋翼分别设置于鸭翼和尾翼的翼端,所述倾转装置用于将旋翼系统与机翼系统和尾翼连接。本发明一种电动倾转旋翼飞行器,具有可垂直起降、平飞速度大、续航时间长和气动性能优异的优点。


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    Title :

    Electric tilt rotor aircraft


    Additional title:

    电动倾转旋翼飞行器


    Contributors:
    FENG XUBI (author) / HE HAIBIN (author) / YANG CHAO (author) / LI YIHENG (author) / SUN JIAN (author)

    Publication date :

    2022-10-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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