A method for manufacturing a structural component comprising a skin formed from a plurality of layers of composite material, a plurality of stringers made of composite material secured to the skin, and a plurality of ribs made of composite material secured to the skin, the structural component having a plurality of sub-panels joined to each other, and each sub-panel includes a sub-skin defined by a first layer of composite material, at least one stringer and at least one rib secured to an inner surface of the sub-skin; wherein the structural component comprises a continuous sub-wall defined by a complex of outer surfaces (6b) of sub-skins (6) of interconnected sub-panels (5); a second layer of composite material is laminated on the first layer to define a continuous outer upper skin disposed in layers on the sub-wall; the skin is defined by a group of sub-skins and an upper skin, and consists of a first layer and a second layer.

    一种用于制造结构部件的方法,结构部件包括由复合材料的多个层形成的蒙皮、固定到蒙皮的由复合材料制成的多个纵梁以及固定到蒙皮的由复合材料制成的多个肋状物,结构部件具有多个子面板,多个子面板互相连结,并且每个子面板包括由复合材料的第一层限定的子蒙皮、固定到子蒙皮的内表面的至少一个纵梁和至少一个肋状物;其中结构部件包括由互相连结的子面板(5)的子蒙皮(6)的外表面(6b)的联合体限定的连续的子壁;复合材料的第二层层压在第一层上,以限定在子壁上分层设置的连续的外部的上蒙皮;蒙皮由子蒙皮和上蒙皮的组限定、并且由第一层和第二层组成。


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    Title :

    Method for producing reinforced structural component made of composite material, and structural component


    Additional title:

    用于制造由复合材料制成的加固结构部件的方法以及结构部件



    Publication date :

    2025-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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