A method of manufacturing an aircraft structural component for an aircraft, the method comprising: providing a component precursor comprising a web and a flange extending from the web wherein the web has a length, a height shorter than the length, a thickness shorter than the height, a first end proximal to the flange, and a second end distal from the flange; applying a tension to the component precursor in a direction parallel to the length of the web, and the magnitude of the tension varying along the height of the web so as to increase the length of the web to different degrees between the first end of the web and the second end of the web; cutting the part precursor; and releasing the tension to allow the component precursor to be shaped into the desired form of the aircraft structural component.

    本发明公开了一种制造用于飞行器的飞行器结构部件的方法,该方法包括:提供部件前体,该部件前体包括腹板和从腹板延伸的凸缘,其中,腹板具有长度、比长度短的高度、比高度短的厚度、靠近凸缘的第一端部和远离凸缘的第二端部;对部件前体施加与腹板的长度平行的方向上的张力,并且张力的大小沿着腹板的高度变化,以便在腹板的第一端部与腹板的第二端部之间将腹板的长度增加至不同的程度;对部件前体进行剪截;以及释放张力以允许部件前体成形为飞行器结构部件所需的形式。


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    Title :

    Method of manufacturing aircraft structural component


    Additional title:

    制造飞行器结构部件的方法


    Contributors:

    Publication date :

    2024-08-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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