The invention discloses a coaxial double-propeller structure unmanned aerial vehicle with paddle connectors. The coaxial double-propeller structure unmanned aerial vehicle comprises a fuselage assembly, a transmission assembly, an anti-freezing propeller assembly, a tail rotor assembly, a control center, a battery and an undercarriage, wherein the battery is installed on the front side of the interior of the fuselage assembly, the control center is installed on the rear side of the battery, the battery is connected with the control center through a circuit, the transmission assembly is installed in the middle of the fuselage assembly, the anti-freezing propeller assembly is installed on the upper portion of the transmission assembly, the tail rotor assembly is connected with the tail of the fuselage assembly, and the undercarriage is installed at the bottom of the fuselage assembly. Aiming at the phenomenon that the unmanned aerial vehicle passes through a cold air layer and is frozen, the rubber stand columns are arranged in the paddles, when the unmanned aerial vehicle passes through the cold air layer, the interiors of the paddles can automatically recognize and start heating, heat is provided for water drops on the surfaces of the paddles to prevent freezing, and the paddles can be collected to be placed in the vertical direction when not in use through the paddle connectors; and the storage space of the unmanned aerial vehicle is saved.
本发明公开了具有桨叶连接器的共轴双桨结构无人机,包括机身组件、传动组件、防冻螺旋桨组件、尾桨组件、控制中心、电池、起落架,所述电池安装在机身组件内部前侧,所述控制中心安装在电池后侧,电池通过线路和控制中心相连,所述传动组件安装在机身组件中部,所述防冻螺旋桨组件安装在传动组件上部,所述尾桨组件和机身组件尾部相连,所述起落架安装在机身组件底部。本发明针对无人机穿越冷空气层结冰的现象,在桨叶内部设置了橡胶立柱,当遇到冷空气层时桨叶内部能够自动识别并开始发热,给桨叶表面的水滴提供热量防止结冰,桨叶连接器还能够在不使用时将桨叶收束到沿竖直方向放置,节约了无人机的储存空间。
Coaxial double-propeller structure unmanned aerial vehicle with paddle connectors
具有桨叶连接器的共轴双桨结构无人机
2021-06-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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