The invention provides a transverse double-rotor unmanned aerial vehicle and relates to the technical field of unmanned aerial vehicles. The transverse double-rotor unmanned aerial vehicle comprises a vehicle body and two vehicle arms, wherein the two vehicle arms are located on the two sides of the vehicle body respectively, and the two vehicle arms and the vehicle body form a V shape; the vehicle arms and the vehicle body form a V shape, the gravity center of the vehicle body is greatly reduced, and flight stability is enhanced. The ends, away from the vehicle body, of the vehicle arms are provided with running mechanisms, and each running mechanism comprises a rotor wing and a tilting part driving the rotor wing to rotate. The tilting part comprises a tilting body and a steering engine which are connected with each other, the tilting body is connected with the vehicle arms, and an output shaft of the steering engine is fixedly connected with the rotor wings. When the output shaft of the steering engine rotates, the rotor wings can be driven to tilt, and when the rotor wings tilt, posture actions such as pitching, rolling and yawing of the unmanned aerial vehicle can be achieved. The transverse double-rotor unmanned aerial vehicle is more compact in structure, low in production cost, good in flight stability and high in flight efficiency, and the endurance time is greatly prolonged.
本发明提供了一种横列式双旋翼无人机,涉及无人机技术领域。一种横列式双旋翼无人机,包括机体和两个机臂,两个机臂分别位于机体的两侧,并与机体呈“V”型。机臂与机体呈“V”型,机身的重心大大降低,以增强其飞行稳定性能。机臂远离机体的端部设有运行机构,运行机构包括旋翼以及驱动旋翼转动的倾转件。倾转件包括相互连接的倾转主体和舵机,倾转主体与机臂连接,舵机的输出轴与旋翼固定连接。舵机的输出轴转动时可以带动旋翼倾转,当旋翼倾转时,可以实现无人机的俯仰、滚转、偏航等姿态动作。该横列式双旋翼无人机结构更紧凑,生产成本低,飞行稳定性好,飞行效率高,续航时间大大提升。
Transverse double-rotor unmanned aerial vehicle
一种横列式双旋翼无人机
2021-04-13
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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