The invention provides a double-wing aircraft which comprises a left rotor wing and a right rotor wing which are fixedly connected, and a connecting frame is arranged between the two rotor wings. The connecting frame is provided with two rotary disc motors, each rotary disc motor is hinged to a telescopic motor, a telescopic rod is installed on each telescopic motor, each rotor wing comprises a frame, a motor base is arranged in the center of the bottom supporting frame, motors are installed on the motor bases, the motors are connected with propellers and drive the propellers to rotate through the motors, and the motor bases are in ball hinge with the motors. The motors can rotate around the motor bases, the motors are further provided with main control rods, and the main control rods are hinged to the telescopic rods on the corresponding telescopic motors.

    本发明提供一种双翼飞行器,包括固定连接的左右两个旋翼,两个旋翼之间具有连接架。连接架设有两个转盘电机,每个转盘电机上均铰接有一伸缩电机,伸缩电机上安装有伸缩杆,所述的旋翼包括框架,底部支撑架的中心设有电机座,电机座上安装有电机,电机连接螺旋桨,通过电机带动螺旋桨转动,电机座与电机为球铰接,电机能够绕电机座转动,电机还设有主控杆,所述的主控杆,与对应的伸缩电机上的伸缩杆铰连接。


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    Title :

    Double-wing aircraft


    Additional title:

    一种双翼飞行器


    Contributors:
    WANG WANYU (author)

    Publication date :

    2021-04-13


    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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