The invention relates to an expandable wing module which comprises a module framework and a skin, the skin covers the module framework, the skin is provided with a lifting force duct in the middle of the module framework, the module framework comprises a front edge keel, side wall plates and rear edge plates, the two sides of the front edge keel are each connected with one side wall plate, and the rear edge plates are erected between the two side wall plates. The front edge keel, the side wall plate and the rear edge plate form a rectangular-ambulatory-plane module framework along the lifting force duct; the outer sides of the side wall plates are further provided with quick-release pin buckles connected with other module frameworks. The front edge keel, the side wall plates and the rear edge plate are arranged to form the rectangular-ambulatory-plane module framework, the front edge keel is used for windward stress, the side wall plates on the two sides are used for supporting and being connected with other wing modules, and the rear edge plate is an acute-angle plate and simulates the rear edge section of a wing. According to the design, the main stress framework is externally arranged as much as possible, and the internal space of the wing module is enlarged as much as possible while the structural strength of the wing module is enhanced.

    本发明涉及一种可拓展的机翼模块,包括模块骨架和蒙皮,蒙皮覆盖在模块骨架上,蒙皮在模块骨架中部空缺出升力涵道,所述模块骨架包括前缘龙骨、侧壁板和后缘板,前缘龙骨两侧分别连接一个侧壁板,数个后缘板架设在两个侧壁板之间,前缘龙骨、侧壁板和后缘板沿升力涵道构成回字形的模块骨架;所述侧壁板的外侧还设置有连接其他模块骨架的快拆销扣。本发明通过设置前缘龙骨、侧壁板和后缘板构成回字形的模块骨架,其中前缘龙骨用于迎风受力,两侧的侧壁板用于支撑并与其他机翼模块连接,后缘板为锐角的板件,模拟机翼的后缘截面。此种设计,将主要的受力骨架尽可能地外置,在增强机翼模块结构强度的同时,尽可能地扩大机翼模块内部的空间。


    Access

    Download


    Export, share and cite



    Title :

    Expandable wing module


    Additional title:

    一种可拓展的机翼模块


    Contributors:
    LAI ZHIWEI (author)

    Publication date :

    2025-04-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    Expandable bidirectional winding type solar wing

    LI JING / LUO DAN / BAI PEIKANG et al. | European Patent Office | 2024

    Free access

    EXPANDABLE MODULE APPARATUS FOR VEHICLE

    JUNG KYUNG HUN | European Patent Office | 2020

    Free access

    EXPANDABLE MODULE APPARATUS FOR VEHICLE

    JUNG KYUNG HUN | European Patent Office | 2021

    Free access

    EXPANDABLE MODULE APPARATUS FOR VEHICLE

    European Patent Office | 2021

    Free access

    EXPANDABLE MODULE APPARATUS FOR VEHICLE

    European Patent Office | 2021

    Free access