The eVTOL aircraft outer wing structure comprises a framework, the framework is covered with a skin, ailerons are installed on one side of the framework, the framework comprises a plurality of stringers, the stringers are distributed in parallel, the two ends of each stringer are connected with a reinforcing frame, an intersection area structure is installed in the middle of each stringer, and the intersection area structure is connected with the skin. A plurality of ribs are installed on the intersection area structure, the side edge of the intersection area structure is connected with an aileron through an aileron connector, a plurality of supporting frames are installed among the stringers, and one side of the reinforcing frame is connected with a motor connecting base. The outer wing structure is light in weight, the outer wing and the motor arm on the outer side are integrally designed into a section, blocks are reduced, and the connecting weight is saved.

    本发明公开了一种eVTOL飞机外翼结构,包括骨架,所述骨架上覆盖有蒙皮,所述骨架一侧安装有副翼,所述骨架包括长桁,所述长桁设有多个,平行分布,所述长桁的两端连接加强框,所述长桁的中部安装有交汇区结构,所述交汇区结构上安装有多个肋,所述交汇区结构侧边通过副翼接头连接副翼,多个所述长桁之间安装有多个支撑框,所述加强框一侧连接有电机连接座。本外翼结构重量轻:把外翼和外侧电机臂集成设计成一个部段,减少分块,节省连接重量。


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    Titel :

    EVTOL aircraft outer wing structure


    Weitere Titelangaben:

    一种eVTOL飞机外翼结构


    Beteiligte:
    YAO YUAN (Autor:in) / ZHANG BAOZHU (Autor:in) / DONG MING (Autor:in)

    Erscheinungsdatum :

    21.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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