The invention relates to the technical field of unmanned aerial vehicles, and particularly discloses a lift fuselage aircraft based on passive hinging, which comprises a lift fuselage, a power supply, a main controller, a sub-controller and a plurality of power assemblies, the lifting fuselage is provided with arms, and the power assemblies are rotatably arranged at the ends of the arms; the power assembly comprises a cantilever, a connecting piece and two propellers; the two propellers are arranged at the two ends of the cantilever correspondingly, and the central axis of the two propellers is perpendicular to the central axis of the cantilever. The connecting piece is fixedly arranged in the middle of the cantilever; the connecting piece is configured to be rotationally connected with the vehicle arm, and the central axis of the cantilever is configured to be perpendicular to the central axis of the vehicle arm; the propellers are configured to be electrically connected with the sub-controllers, and the sub-controllers are configured to be connected with the main controller; the sub-controller is used for controlling the propeller according to the information issued by the main controller; the lift fuselage aircraft based on passive hinging can realize the function of tilting rotors without using a tilting steering engine, and is high in maneuverability.
本发明涉及无人机技术领域,具体公开一种基于被动铰接的升力机身飞行器,包括升力机身、电源、主控制器、子控制器和多个动力组件;升力机身具有机臂,动力组件可转动地配置在机臂端部;动力组件包含有悬臂、连接件和两个推进器;两个推进器分别设置在悬臂的两端,且两个推进器的中轴线与悬臂的中轴线垂直;连接件固定地配置在悬臂的中部;连接件配置为与机臂转动连接,悬臂的中轴线配置为与机臂的中轴线垂直;推进器配置为与子控制器电性连接,子控制器配置为与主控制器连接;子控制器用于根据主控制器发布的信息控制推进器;该基于被动铰接的升力机身飞行器不使用倾转舵机即可实现倾转旋翼的功能,机动性高。
Lift fuselage aircraft based on passive hinging
一种基于被动铰接的升力机身飞行器
2024-05-03
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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