The invention discloses an aircraft withtilt rotors. The aircraft comprises an aircraft body, wings are arranged on the left side and the right side of the aircraft body correspondingly, and a vertical power device is further arranged on the aircraft body; tilt rotor arms are arranged on the wings, tilt driving devices are arranged on the tilt rotor arms, tilt rotor driving motors are connected tothe driving ends of the tilt driving devices, and tilt rotors are connected to the driving ends of the tilt rotor driving motors; the tiltrotor driving motor and the tiltrotor are driven by the tiltdriving device to tilt, and the tiltrotor driving motor and the tiltrotor face the front of the aircraft body or face the upper part of the aircraft body; and the tiltrotors are driven by tiltrotor driving motors to rotate. In the embodiment of the invention, the tiltrotor can provide power for vertical take-off and landing during vertical take-off and landing, the lift force for vertical take-offand landing is increased, the vertical take-off and landing performance of the aircraft is ensured, and the wind resistance of the aircraft under the condition of large wingspan during vertical take-off and landing can be improved.

    本发明公开了一种具有倾转旋翼的飞行器,飞行器包括机身,机身的左右两侧分别设置有机翼,机身上还设置有垂起动力装置;机翼上设置有倾转旋翼臂,倾转旋翼臂上设置有倾转驱动装置,倾转驱动装置的驱动端连接有倾转旋翼驱动电机,倾转旋翼驱动电机的驱动端连接有倾转旋翼;倾转旋翼驱动电机和倾转旋翼在倾转驱动装置的驱动下倾转,倾转旋翼驱动电机和倾转旋翼朝向机身的前方,或倾转旋翼驱动电机和倾转旋翼朝向机身的上方;倾转旋翼在倾转旋翼驱动电机的驱动下旋转。在本发明实施例中,所述倾转旋翼在垂直起降时可以提供垂直起降的动力,增大垂直起降的升力,保证飞行器的垂直起降性能,而且可以提高垂直起降时大翼展情况下的抗风能力。


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    Title :

    Aircraft withtilt rotors


    Additional title:

    一种具有倾转旋翼的飞行器


    Contributors:
    XIE LING (author) / LIU SHIYI (author)

    Publication date :

    2020-10-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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