The invention provides an inflatable solar unmanned aerial vehicle which comprises an upper wing, a lower wing and a connecting wing, and the upper wing, the lower wing and the connecting wing are mutually connected to form a box type structure; the upper wing, the lower wing and the connecting wing are all of inflatable structures; the solar cell is arranged on the upper surface of the upper wing; the power device is arranged at the front edge of the upper wing; undercarriages are arranged at two ends of the lower side of the lower wing. The technical scheme has the beneficial effects that the flying wing layout form formed by combining the upper wing and the lower wing is adopted, the upper wing, the lower wing and the connecting wing are all of an inflatable structure, a wing structure of a conventional beam and rib structure is replaced, and the purpose of weight reduction is achieved. The upper wing and the lower wing form a box type structure through the connecting wings, so that the structural rigidity of the unmanned aerial vehicle is improved.

    本发明提供一种充气式太阳能无人机,包括:上机翼、下机翼和连接翼,上机翼、下机翼和连接翼相互连接形成盒式结构;上机翼、下机翼和连接翼均为充气式结构;太阳能电池设置在上机翼的上表面;动力装置设置于上机翼的前缘;起落架设置于下机翼的下侧两端。本发明的技术方案的有益效果在于,采用上机翼和下机翼组合形成的飞翼布局形式,上、下机翼和连接翼均为充气结构,替代常规梁、肋构型的机翼结构,达到减重的目的。上、下机翼通过连接翼组成盒式结构,有利于提高该无人机的结构刚度。


    Access

    Download


    Export, share and cite



    Title :

    Inflatable solar unmanned aerial vehicle


    Additional title:

    一种充气式太阳能无人机


    Contributors:
    YI ZHISHENG (author)

    Publication date :

    2022-04-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



    Unmanned aerial vehicle with inflatable membrane

    BECKMAN BRIAN C / SOREK NOAM | European Patent Office | 2019

    Free access

    Inflatable buffer type unmanned aerial vehicle delivery pod

    ZHAO JIAYUAN / LI CHUNLIN / GONG KE | European Patent Office | 2025

    Free access

    Unmanned aerial vehicle based on distributed power inflatable rotors

    GUO TINGYU / XIE CHUNLEI / WANG REN et al. | European Patent Office | 2024

    Free access

    UNMANNED AERIAL VEHICLE HAVING JOINED WINGS AND INFLATABLE FUSELAGE

    LEE HEE WOO | European Patent Office | 2015

    Free access

    Inflatable wing for air-launched unmanned aerial vehicle and design method

    TANG JIWEI / PU SHUMIN / BAO YONGHONG et al. | European Patent Office | 2024

    Free access