The invention relates to a single-rotor unmanned aerial vehicle system structure, and provides the single-rotor unmanned aerial vehicle system structure aiming at the structural blank of a single rotor of an unmanned aerial vehicle. The technical difficulty of the single-rotor unmanned aerial vehicle is how to solve the problem of reaction torque caused by a single rotor. In order to solve the reaction torque caused by single-rotor rotation, the invention provides a balance system structure additionally arranged on the single-rotor unmanned aerial vehicle, and besides the structure of a commonunmanned aerial vehicle, the balance system focuses on solving the reaction torque caused by single-rotor rotation. Torque brought by high-speed rotation of a rotor in the balance system and reactiontorque of the single rotor are counteracted, and the stability of the single-rotor unmanned aerial vehicle is guaranteed.

    本申请涉及一种单旋翼无人机系统结构,针对无人机单旋翼这一结构空白,本发明提供了一种单旋翼无人机系统结构。单旋翼无人机的技术难点在于如何解决有由单旋翼带来的反作用扭矩。为了解决单旋翼旋转带来的反作用扭矩,本发明提出为单旋翼无人机加装平衡系统结构,除去一般无人机所具有结构外,平衡系统将着重解决单旋翼旋转的反作用扭矩。通过平衡系统内部转子高速转动带来扭矩与单旋翼的反作用扭矩相互抵消,保证单旋翼无人机稳定性。


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    Title :

    Single-rotor unmanned aerial vehicle system structure


    Additional title:

    一种单旋翼无人机系统结构


    Contributors:
    DIWU FANGYUAN (author) / DONG BAOJIA (author) / XIE MINGMING (author) / WANG YINRUI (author)

    Publication date :

    2021-02-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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