The unmanned aerial vehicle with the rotor wing structure comprises an aerial vehicle body, the top of the aerial vehicle body is connected with a horizontally-arranged unpowered rotor wing through a clutch driving device, the two sides of the aerial vehicle body are fixedly connected with wings, the bottom side wall of each wing is fixedly connected with a mounting rod, and the bottom side wall of each wing is fixedly connected with a rotating shaft. The bottom sides of the two ends of each mounting rod are connected with horizontal propellers through first driving motors, and the tail of the aircraft fuselage is connected with a vertically-arranged tail rotor wing through a direction driving device. According to the aircraft, the advantages that an unmanned aerial vehicle takes off without a runway, takes off and lands vertically, hovers freely and flies flexibly are perfectly combined with the advantages that a rotorcraft is simple in structure, saves energy and is high in safety, and finally the purposes that the carrying capacity is larger, the flight time is longer, the voyage is farther and the flight is safer are achieved.
本发明公开了一种具有旋翼结构的无人驾驶飞行器,包括飞行器机身,所述飞行器机身的顶部通过离合驱动装置连接有水平设置的无动力旋翼,所述飞行器机身的两侧均固定连接有机翼,每个所述机翼的底侧壁上固定连接有安装杆,每个所述安装杆的两端底侧均通过第一驱动电机连接有水平螺旋桨,所述飞行器机身的尾部通过方向驱动装置连接有垂直设置的尾旋翼。本发明的飞行器将无人机无需跑道起飞、垂直起降、自由悬停、飞行灵活的优点以及旋翼机结构简单、节省能耗、安全性高的优点完美的结合起来,并最终实现运载能力更大、航时更久、航程更远、飞行更安全的目的。
Unmanned aerial vehicle with rotor wing structure
一种具有旋翼结构的无人驾驶飞行器
2025-03-21
Patent
Electronic Resource
Chinese
IPC: | B64U |
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