STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF

The present invention provides a closed composite material structure for aircraft fuselage shaped on a male jig from which it can be separated in a certain direction, said structure comprising a single outer panel and a plurality of inner longitudinal stiffeners integrated in said panel, such that t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARTINEZ CEREZO, ALBERTO, RAMON, MIGUEZ CHARINES, YOLANDA, JORDAN CARNICERO, JAVIER, SANCHEZ FERNANDEZ, JULIAN
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS 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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