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.
Method for manufacturing composite barrel sections for aircraft fuselages
Verfahren zur Herstellung Verbundszylinderteile für Flugzeugrümpfe
Procédé de fabrication de sections composites cylindriques pour fuselages d'avion
2016-09-28
Patent
Electronic Resource
English
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 / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C |
Composite barrel sections for aircraft fuselages and methods for manufacturing such barrel sections
European Patent Office | 2016
|European Patent Office | 2016
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