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.
STRUCTURAL INTERNAL REINFORCEMENT ELEMENT FOR A FUSELAGE, AND PROCEDURE FOR THE MANUFACTURE OF SAID STRUCTURAL ELEMENT
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
2023-08-09
Patent
Electronic Resource
English
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