The invention discloses a tailless delta wing unmanned aerial vehicle, and belongs to the field of aircrafts. The problems that an existing unmanned aerial vehicle is low in battery energy mass ratio, limited in flight distance and flight time and high in site requirement during take-off and landing are solved. According to the technical scheme, the tailless delta wing unmanned aerial vehicle comprises an unmanned aerial vehicle body, a power system and a control system, the unmanned aerial vehicle body comprises a vehicle body, a first wing and a second wing, and the power system comprises a first energy supply device, a lift force balance assembly, at least one first rotor wing power assembly and at least one second rotor wing power assembly.

    本发明公开一种无尾三角翼无人机,属于飞行器领域。目的是解决现有无人机中电池能质比低,飞行距离和飞行时间受限,起降时对场地要求高的问题。技术方案是,提供一种无尾三角翼无人机,包括无人机主体、动力系统和控制系统,无人机主体包括机身、第一机翼和第二机翼,动力系统包括第一供能装置、升力平衡组件、至少一组第一旋翼动力组件和至少一组第二旋翼动力组件。


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    Titel :

    Tailless delta wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种无尾三角翼无人机


    Beteiligte:
    PU KUIRU (Autor:in)

    Erscheinungsdatum :

    14.09.2021


    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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