The invention provides a wingtip connecting structure and an unmanned aerial vehicle system, and relates to the field of unmanned aerial vehicles, the wingtip connecting structure comprises a first wingtip mounted on flight equipment, and the first wingtip comprises a first wingtip main body; the connector male head is installed on the first side face, away from the flight equipment, of the first wingtip body, and the connector male head is connected with the energy output end of the flight equipment; the second wingtip is mounted on the unmanned aerial vehicle, and the second wingtip comprises a second wingtip main body; the connector female head is installed on the second side face, away from the unmanned aerial vehicle, of the second wingtip body, and the connector female head is connected with the energy input end of the unmanned aerial vehicle; when the flight equipment and the unmanned aerial vehicle are in a flight state, the unmanned aerial vehicle gets close to the flight equipment to enable the connector male head to be inserted into the connector female head, so that the flight equipment supplements energy to the unmanned aerial vehicle. The unmanned aerial vehicle system comprises: a flight device comprising a device body and a first wingtip; the at least one drone includes a drone body and a second wingtip.

    本发明提供了一种翼尖连接结构和无人机系统,涉及无人机领域,翼尖连接结构包括第一翼尖,安装在飞行设备上,第一翼尖包括第一翼尖主体;连接器公头,安装在第一翼尖主体远离所述飞行设备的第一侧面上,连接器公头与飞行设备的能源输出端连接;第二翼尖,安装在无人机上,第二翼尖包括第二翼尖主体;连接器母头,安装在第二翼尖主体远离无人机的第二侧面上,连接器母头与无人机的能源输入端连接;在飞行设备和无人机处于飞行状态的情况下,无人机通过靠近飞行设备以使得连接器公头插入连接器母头,从而使得飞行设备对无人机进行能源补充。无人机系统包括:飞行设备包括设备主体和第一翼尖;至少一个无人机包括无人机身和第二翼尖。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Wingtip connecting structure and unmanned aerial vehicle system


    Weitere Titelangaben:

    翼尖连接结构和无人机系统


    Beteiligte:
    WANG XIANGYU (Autor:in) / DONG ANQI (Autor:in) / WANG BO (Autor:in) / GAO ZIANG (Autor:in) / ZHANG JIAN (Autor:in)

    Erscheinungsdatum :

    2024-01-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



    Wingtip connecting structure of combined unmanned aerial vehicle

    ZHAO XINHUI / YANG YANPING / ZHANG ZIJIAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Wingtip mounting layout of geophysical prospecting unmanned aerial vehicle

    CUI YUELI / WANG CHAO / LYU CHAO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Vertical take-off and landing wingtip hinge combined type unmanned aerial vehicle

    XIE CHANGCHUAN / MENG YANG / ZHANG GUOXING et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Stability Evaluation of a Fixed-Wing Unmanned Aerial Vehicle with Morphing Wingtip

    Oktay, Tuğrul / Eraslan, Yüksel | BASE | 2022

    Freier Zugriff

    Unmanned aerial vehicle paddle connecting structure

    CAO LEI | Europäisches Patentamt | 2020

    Freier Zugriff