一种无旋翼无人机的设计研究

Hongxia Xu, Liang Jiang, Zhongwen Cao, Xiangwen Bao
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引用次数: 0

摘要

利用建模软件Fusion360设计了一种紧凑对称的无旋翼无人机(UAV),旨在解决与高速旋转旋翼叶片相关的安全隐患和高噪音水平。无旋翼无人机使用四个无叶风扇代替外部桨,并放置所需的电机在机身内提供动力。分析了无旋翼无人机通风口、进气口、摄像头和滑架架结构的位置,研究了主要结构供能模块(电池)、电源模块和控制模块的工作参数。探讨并解决了无旋翼无人机在飞行过程中旋翼叶片产生的安全和噪声问题,以及外界因素容易造成电机损坏的问题。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design study of a rotorless Unmanned Aerial Vehicle
The modeling software Fusion360 was used to design a compact and symmetric rotorless Unmanned Aerial Vehicle (UAV) that aims to address the safety hazards and high noise levels associated with rotor blades rotating at high speeds. The rotorless UAV utilizes four bladeless fans instead of external paddles and places the motors needed to provide power inside the fuselage. The locations of the rotorless UAV's air vents, air inlets, camera, and sled mount structures are analyzed, while the operating parameters of the main structural energy supply module (battery), power module, and control module are studied. The safety and noise problems caused by the rotor blades during the flight of the rotorless UAV and the damage of the motor easily caused by external factors are explored and solved.
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