A method for manufacturing a section of a fuselage, the method comprising: positioning a plurality of uncured stiffeners on a mandrel assembly; laminating fiber tape over the uncured stiffeners on the rotating mandrel assembly; and cocuring the uncured stiffeners and the fiber tape.
Composite barrel sections for aircraft fuselages and methods for manufacturing such barrel sections
Verbundzylinderteile für Flugzeugrümpfe und Verfahren zur Herstellung derartiger Zylinderteile
Sections de barillet composites pour fuselages d'avion et procédés pour la fabrication de telles sections de barillet
2016-12-28
Patent
Electronic Resource
English
European Patent Office | 2016
|Method for manufacturing composite barrel sections for aircraft fuselages
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