DEVICE FOR MANUFACTURING OMEGA STRINGERS

The invention provides an apparatus (1) for manufacturing composite stringers (9) from a composite laminate (2) comprising a male mould (11), a main caul plate (12), two fixed female mould halves (13), two secondary movable caul plates (14) and retention means (15, 17). The main caul plate is locate...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Martínez Cerezo, Alberto, García García, Aquilino, Cruzado Parla, Gabriel, Galiana Blanco, Jorge, Cuenca Rincón, José, Pérez Pastor, Augusto
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES 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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The invention provides an apparatus (1) for manufacturing composite stringers (9) from a composite laminate (2) comprising a male mould (11), a main caul plate (12), two fixed female mould halves (13), two secondary movable caul plates (14) and retention means (15, 17). The main caul plate is located below the male mould (11), the female mould halves (13) are located at both sides of the main caul plate (12) and the secondary movable caul plates (14), each of them located respectively over each one of the two female mould halves (13). The male mould (11), the main caul plate (12), the two female mould halves (13) and the two secondary caul plates (14) are non developable surfaces. The retention means (15, 17) are adapted to keep each secondary movable caul plate (14) at a predetermined distance of its respective female mould half (13).