A method for manufacturing a panel for an aircraft is provided. The method includes arranging, on a curing surface, a skin of pre-preg composite material, arranging a plurality of pre-formed, uncured composite stringers, each having an open cross section with a web and a base transverse to each other so that a first base portion protrudes toward a first side and a second base portion protrudes toward a second side, arranging the stringers on the skin with the base in contact with the skin, arranging, on each stringer, a respective first mandrel to completely cover the first base portion and a respective second mandrel to completely cover the second base portion, and having the skin and the stringers undergo a co-curing process in autoclave with vacuum bag.


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    Titel :

    MANUFACTURING METHOD OF A STIFFENED PANEL WITH OPEN-SECTION STRINGERS FOR AERONAUTICAL APPLICATION


    Weitere Titelangaben:

    HERSTELLUNGSVERFAHREN FÜR EINE VERSTEIFTE PLATTE MIT HOLMEN MIT OFFENEM QUERSCHNITT FÜR AERONAUTISCHE ANWENDUNGEN
    PROCÉDÉ DE FABRICATION D'UN PANNEAU RAIDI AVEC DES RAIDISSEURS À SECTION OUVERTE POUR APPLICATION AÉRONAUTIQUE


    Beteiligte:
    IAGULLI GIANNI (Autor:in) / TOTARO GIUSEPPE (Autor:in) / RAFFONE MARCO (Autor:in) / FRASCA MICHELE (Autor:in)

    Erscheinungsdatum :

    06.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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