The invention discloses a tiltable rotor unmanned aerial vehicle, which comprises a vehicle body, wherein in the axial direction, one end of the vehicle body is provided with a vehicle head, the otherend of the vehicle body is provided with a vehicle tail, and an empennage is arranged on the vehicle tail; wings are arranged on the two sides of the vehicle body in pairs, tilting mechanisms are arranged at the ends, which are away from the vehicle body, of the wings in the extending direction of the wings, and each tilting mechanism comprises a tilting base connected with the corresponding wingthrough a connecting piece, a motor unit arranged on the tilting base and a propeller connected with the motor unit; when the tilting mechanism is located at a first station, the motor unit drives the motor to work so as to enable the propeller to rotate on a first rotating plane, and the first rotating plane is parallel to the plane where the wing is located; and when the tilting mechanism is located at a second station, the motor unit drives the motor to work so as to enable the propeller to rotate on a second rotating plane, and the second rotating plane is perpendicular to the plane wherethe wing is located. In addition, the invention further discloses a using method of the tiltable rotor wing unmanned aerial vehicle.

    本发明公开了一种可倾转旋翼无人机,其包括:机身,沿轴向方向上,机身一端为机头,另一端为机尾,所述机尾上设有尾翼;机翼成对设于机身的两侧,沿机翼延展方向远离机身端设有倾转机构,倾转机构包括:通过连接件与机翼连接的倾转底座,设于所述倾转底座上的电机机组以及与电机机组连接的螺旋桨;其中,当所述倾转机构处于第一工位时,电机机组驱动电机工作,以使得螺旋桨在第一旋转平面旋转,第一旋转平面与机翼所在平面平行;当所述倾转机构处于第二工位时,所述电机机组驱动电机工作,以使得螺旋桨在第二旋转平面旋转,所述第二旋转平面与机翼所在平面垂直。此外,本发明还公开了上述可倾转旋翼无人机的使用方法。


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    Titel :

    Tiltable rotor unmanned aerial vehicle and using method thereof


    Weitere Titelangaben:

    一种可倾转旋翼无人机及其使用方法


    Beteiligte:
    XIE ZHONGLIANG (Autor:in) / WANG XUERUI (Autor:in) / CHEN JIAPING (Autor:in) / LIU SHENGPENG (Autor:in) / CHEN YONG (Autor:in) / WEN ZHENGGUO (Autor:in) / TIAN WENCHAO (Autor:in) / ZHOU JINZHU (Autor:in) / GAO HONGWEI (Autor:in) / SHI JING (Autor:in)

    Erscheinungsdatum :

    2020-10-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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