本发明涉及一种共轴双旋翼飞行器,属于飞行器的上下旋翼操纵系统技术领域。该共轴双旋翼飞行器包括主轴、第一驱动系统、第一旋翼系统、第一变距系统、第二变距系统、第二旋翼系统、第二驱动系统、支架机构和太阳能供电系统;第一驱动系统、第一旋翼系统、第一变距系统、第二变距系统、第二旋翼系统、第二驱动系统共轴装配在主轴上,第一旋翼系统和第二旋翼系统能绕主轴转动,第一旋翼系统和第二旋翼系统的旋转方向相反,第一旋翼系统在第一驱动系统的作用下顺时针旋转或逆时针旋转,第二旋翼系统在第二驱动系统的作用下逆时针旋转或顺时针旋转;太阳能供电系统共轴安装在主轴的顶端,支架机构共轴安装在主轴的底部。

    The invention relates to a coaxial dual-rotor aircraft, and belongs to the technical field of upper and lower rotor control systems of aircrafts. The coaxial dual-rotor aircraft comprises a main shaft, a first driving system, a first rotor system, a first variable-pitch system, a second variable-pitch system, a second rotor system, a second driving system, a bracket mechanism and a solar power supply system, the first driving system, the first rotor wing system, the first variable-pitch system, the second variable-pitch system, the second rotor wing system and the second driving system are coaxially assembled on the main shaft, the first rotor wing system and the second rotor wing system can rotate around the main shaft, and the rotation directions of the first rotor wing system and the second rotor wing system are opposite; the first rotor system rotates clockwise or anticlockwise under the action of the first driving system, and the second rotor system rotates anticlockwise or clockwise under the action of the second driving system; the solar power supply system is coaxially mounted at the top end of the spindle, and the support mechanism is coaxially mounted at the bottom of the spindle.


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    Title :

    一种共轴双旋翼飞行器


    Publication date :

    2024-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U