The invention discloses an automatic wing folding mechanism which comprises a wing fixing seat, a first main wing and a second main wing are hinged to the left end and the right end of the wing fixing seat respectively, a telescopic rod is arranged below the wing fixing seat, and the two ends of the telescopic rod are hinged to the first main wing and the second main wing respectively. The extension or folding of the first main wing and the second main wing can be completed through the telescopic rod, and the occupied area can be reduced through folding while the light weight is ensured.

    本发明公开了一种机翼自动折叠机构,包括机翼固定座,所述机翼固定座的左右两端分别铰接有第一主机翼和第二主机翼,所述机翼固定座的下方设置有伸缩杆,所述伸缩杆的两端分别与所述第一主机翼和所述第二主机翼铰接。本发明通过伸缩杆可以完成第一主机翼和第二主机翼的伸展或折叠,在保证轻量化的同时可以通过折叠减少占用的面积。


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    Titel :

    Automatic wing folding mechanism


    Weitere Titelangaben:

    一种机翼自动折叠机构


    Beteiligte:
    ZHAO WEI (Autor:in) / YANG GUOSHE (Autor:in)

    Erscheinungsdatum :

    18.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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