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。


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    Titel :

    Inflatable solar unmanned aerial vehicle


    Weitere Titelangaben:

    一种充气式太阳能无人机


    Beteiligte:
    YI ZHISHENG (Autor:in)

    Erscheinungsdatum :

    05.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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