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

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

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:- a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CUETOS GÓMEZ, María del Mar, SALAMERO LAORDEN, Juan, RUIZ DEALBERT, Miguel, ESTAL VERA, Roberto
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung: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.