The invention relates to a spinning wheel type unmanned aerial vehicle which comprises a vehicle body and a power device assembled on the vehicle body; the power device comprises one or more spinning wheel assemblies; when one spinning roller assembly is adopted, the spinning roller assembly can be arranged above the gravity center of the fuselage, so that the fuselage is always kept in a natural balance state; when a plurality of spinning roller assemblies are installed, the spinning roller assemblies can be symmetrically installed on the two sides of the machine body, and the machine body keeps dynamic balance. The structure is simple, by arranging the spinning roller assembly, the driving motor outputs the multiple rotor blades, compared with an existing design, the rotational inertia of a power part is reduced, the structural strength and rigidity are improved, and the reliability is improved. Compared with the existing design, the safety performance is improved.

    本发明涉及一种旋轮式无人飞行器,包括机身及装配于所述机身的动力装置,所述动力装置包括一个或多个旋轮组件;当采用一个旋轮组件时,可布置于机身重心之上的位置,使机身始终保持自然平衡状态;当采用安装多个旋轮组件时可对称安装于机身两侧,使机身保持动力平衡;本发明结构简单,通过设置旋轮组件,由驱动电机将多个旋翼片输出,相对于已有设计减小了动力部分的转动惯量,提高了结构强度与刚度,增加了可靠性;相对于已有设计增加了安全性能。


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    Titel :

    Rotary wheel type unmanned aerial vehicle


    Weitere Titelangaben:

    一种旋轮式无人飞行器


    Beteiligte:
    HUANG JIALIN (Autor:in) / CHEN LIXIN (Autor:in)

    Erscheinungsdatum :

    28.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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