The present invention relates to a method of forming a reinforced panel component and a related apparatus. The method of forming a reinforced panel may include engaging a reinforcement component having a faying surface with a first portion of a heated press, engaging an uncured panel component with an opposing second portion of the press, the panel component having a faying surface complementarily-configured with respect to the faying surface of the reinforcement component, treating the faying surface of the reinforcement component such that the faying surface is active for co-bonding with respect to the panel component, actuating the press to direct the first and second portions of the press toward each other, such that the faying surfaces are complementarily engaged under pressure; and heating the first and second portions of the press to a curing temperature associated with the panel component to substantially simultaneously co-bond the faying surfaces of the reinforcement componentand the panel component together, cure the panel component, and form the reinforced panel.

    本申请涉及形成加强面板的方法和装置、形成加强部件的方法。一种形成加强面板的方法,该方法可包括:将具有搭接面的加强部件与加热的压机的第一部分接合;将未固化的面板部件与压机的相对的第二部分接合;面板部件具有相对于加强部件的搭接面互补地配置的搭接面;处理加强部件的搭接面使得搭接面为活性以与面板部件共同粘接;致动压机以彼此相对地引导压机的第一部分和第二部分,使得搭接面在压力下互补地接合;以及将压机的第一部分和第二部分加热至与面板部件相关联的固化温度从而将加强部件和面板部件的搭接面基本同时共同粘接在一起,固化面板部件,并且形成加强面板。


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    Title :

    METHOD OF FORMING A REINFORCED PANEL COMPONENT AND A RELATED APPARATUS


    Additional title:

    形成加强面板的方法和装置、形成加强部件的方法



    Publication date :

    2021-01-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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 / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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