The invention discloses an unmanned aerial vehicle modularized wing electric control structure and a using method thereof.The unmanned aerial vehicle modularized wing electric control structure comprises an unmanned aerial vehicle body, a first wing sleeve is fixedly connected to the surface of the unmanned aerial vehicle body, a second wing sleeve is slidably connected into the first wing sleeve, and a round sleeve is fixedly connected to the left end of the second wing sleeve; a first motor is slidably connected to the right side of an inner cavity of the second wing sleeve. A first motor and a screw rod drive a second wing sleeve to slide in a first wing sleeve through an unmanned aerial vehicle body to adjust the length, and then a third motor and a reciprocating screw rod drive a transmission device through a toothed plate and a fluted disc to conduct rotation adjustment with a shaft rod as the center; and finally, a motor II drives a transmission device and a propeller to rotate and adjust by taking a bearing as a center through a gear and a gear sleeve, so that the unmanned aerial vehicle has the advantage of convenience in electric control adjustment, and the problems that in the using process of wings of an existing unmanned aerial vehicle, electric control adjustment cannot be carried out, and a user cannot conveniently use the unmanned aerial vehicle in different environments are solved.
本发明公开了一种无人机模块化机翼电控结构及其使用方法,包括无人机本体,所述无人机本体的表面固定连接有机翼套一,所述机翼套一的内部滑动连接有机翼套二,所述机翼套二的左端固定连接有圆套,所述机翼套二内腔的右侧滑动连接有电机一。本发明由电机一和螺杆通过无人机本体带动机翼套二在机翼套一的内部滑动对长度进行调节,再由电机三和往复丝杆通过齿板和齿盘带动传动装置以轴杆为中心进行转动调节,最后由电机二通过齿轮和齿套带动传动装置和螺旋桨以轴承为中心进行转动调节,从而具备了便于电控调节的优点,解决了现有无人机的机翼在使用过程中,无法进行电控调节,不方便使用者在不同环境对无人机进行使用的问题。
Modularized wing electric control structure of unmanned aerial vehicle and use method of modularized wing electric control structure
一种无人机模块化机翼电控结构及其使用方法
2022-05-24
Patent
Electronic Resource
Chinese
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