Systems and methods are provided for fabricating a preform for a fuselage section of an aircraft. The method includes advancing a series of arcuate mandrel sections (112) in a process direction through an assembly line, placing stringer preforms onto the arcuate mandrel sections (112) via stringer placement stations, uniting the series of arcuate mandrel sections (112) into a combined mandrel; and laying up fiber reinforced material onto the combined mandrel and the stringer preforms.


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    Title :

    COMPOSITE ASSEMBLY FOR UNHARDENED FUSELAGE COMPONENTS


    Additional title:

    VERBUNDANORDNUNG FÜR UNGEHÄRTETE RUMPFKOMPONENTEN
    ENSEMBLE COMPOSITE POUR COMPOSANTS DE FUSELAGE NON DURCIS



    Publication date :

    2022-05-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B29B PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED , Vorbereiten oder Vorbehandeln der zu verformenden Masse / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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