The invention provides an omnidirectional five-rotor aircraft and a control method. The aircraft is provided with five rotors and four pipelines for mounting the rotors, and each pipeline comprises acentral pipe arranged in the middle of the aircraft and three edge pipes which are arranged around the central pipe by taking the central pipe as a symmetric center and have the same specification; each rotor comprises a main rotor group arranged in the corresponding central pipe and auxiliary rotors which are arranged in the edge pipes respectively and have the same specification; the edge pipesand the auxiliary rotors in the edge pipes are combined to form a guide pipe fan with variable blade angles; and complex operation work can be completed, and the defects that a traditional miniature aircraft vertically taking off and landing is limited in freedom degree and the like are overcome.

    本发明提出一种全向五旋翼飞行器及控制方法,所述飞行器设有五个旋翼和四个用于安装旋翼的管道,所述管道包括设于飞行器中部的一个中央管和三个以中央管为对称中心来环绕其设置的相同规格的边沿管;所述旋翼包括装于中央管内的主旋翼组,还包括分设于各边沿管内的相同规格的副旋翼;所述边沿管与其管内的副旋翼组合为桨叶角度可变的导管风扇;本发明可以完成复杂的操作工作,并克服传统垂直起飞和着陆的微型飞行器在自由度方面限制性能等缺陷。


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    Titel :

    Omnidirectional five-rotor aircraft and control method


    Weitere Titelangaben:

    一种全向五旋翼飞行器及控制方法


    Beteiligte:
    LEI YAO (Autor:in) / FENG ZHICHENG (Autor:in) / MA CHENSONG (Autor:in)

    Erscheinungsdatum :

    2020-12-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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