Systems are provided for fabricating a preform for a fuselage section of an aircraft. The system includes advancing a series of arcuate mandrel sections in a process direction through an assembly line, laying up fiber reinforced material onto the arcuate mandrel sections via layup stations, uniting the series of arcuate mandrel sections into a combined mandrel; and splicing the fiber reinforced material laid-up onto the arcuate mandrel sections.


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    Title :

    Composite Assembly For Unhardened Fuselage Components



    Publication date :

    2023-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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



    COMPOSITE ASSEMBLY FOR UNHARDENED FUSELAGE COMPONENTS

    SMITH DANIEL R / JONES DARRELL D / PRITCHARD PAUL T et al. | European Patent Office | 2022

    Free access

    Composite assembly for unhardened fuselage components

    SMITH DANIEL R / JONES DARRELL D / PRITCHARD PAUL T et al. | European Patent Office | 2023

    Free access

    COMPOSITE ASSEMBLY FOR UNHARDENED FUSELAGE COMPONENTS

    SMITH DANIEL R / JONES DARRELL D / PRITCHARD PAUL T et al. | European Patent Office | 2022

    Free access

    COMPOSITE ASSEMBLY FOR UNHARDENED FUSELAGE COMPONENTS

    DANIEL R SMITH / DARRELL D JONES / PAUL T PRITCHARD et al. | European Patent Office | 2022

    Free access

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