A method and a tool for repairing a composite-material panel of an aircraft with at least one repair part made of composite material without using an autoclave. The repair method includes the steps of preparing the panel, placing at least one repair part made of composite material on the second face to cover a damaged zone, positioning a vacuum bag configured to sealingly cover the repair part, polymerizing or consolidating the repair part, compressing the vacuum bag against the repair part using a compression plate concomitantly with the step in which the repair part is polymerized or consolidated.


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    Title :

    PROCEDE DE REPARATION D'UN PANNEAU EN MATERIAU COMPOSITE D'UN AERONEF ET OUTILLAGE POUR SA MISE EN OEUVRE


    Contributors:

    Publication date :

    2017-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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




    OUTILLAGE POUR LA FABRICATION D'UN PANNEAU EN MATERIAU COMPOSITE, EN PARTICULIER D'UN FUSELAGE D'AERONEF

    MEYER CEDRIC / GAUDIN JOCELYN | European Patent Office | 2018

    Free access

    OUTILLAGE POUR LA FABRICATION D'UN PANNEAU EN MATERIAU COMPOSITE, EN PARTICULIER D'UN FUSELAGE D'AERONEF

    MEYER CEDRIC / GAUDIN JOCELYN | European Patent Office | 2017

    Free access

    PROCEDE DE REPARATION D'UN FUSELAGE COMPOSITE D'UN AERONEF

    TARDU GILLES / DUBOIS PHILIPPE | European Patent Office | 2017

    Free access