An internal structural reinforcement element for fuselages, where the internal structural reinforcement element has a longitudinal direction adapted for its placement in the longitudinal direction of the fuselage and a transversal direction perpendicular to the longitudinal direction, comprising:- an external reinforcement element (1),- an internal reinforcement element (2), located internally to the external reinforcement element (1) in the transversal direction of the structural element,- where both reinforcement elements (1, 2) are manufactured from resin-impregnated fibre,- an intermediate element (3), located between the external reinforcement element (1) and the internal reinforcement element (2) in the transversal direction of the structural element, the intermediate element (3) being manufactured from pre-impregnated composite material.


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    Title :

    STRUCTURAL INTERNAL REINFORCEMENT ELEMENT FOR A FUSELAGE, AND PROCEDURE FOR THE MANUFACTURE OF SAID STRUCTURAL ELEMENT


    Additional title:

    STRUKTURELLES INTERNES VERSTÄRKUNGSELEMENT FÜR EINEN RUMPF UND VERFAHREN ZUR HERSTELLUNG DES STRUKTURELLEN ELEMENTS
    ÉLÉMENT STRUCTURAL DE RENFORCEMENT INTERNE POUR UN FUSELAGE ET PROCÉDURE DE FABRICATION DUDIT ÉLÉMENT STRUCTURAL



    Publication date :

    2023-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand



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