Verfahren zur Herstellung einer Faserverbundkomponente, ein Stützkern und auch eine Faserverbundkomponente

Details

Veröffentlichungs-Nr.

EP2662202

Aktenzeichen

EP13164983

Anmeldetag

23. April 2013

Veröffentlichung

12. Januar 2022

Erteilung

12. Januar 2022

Rechtsraum

EP

IPC

B29C70/44B29D99/00B29D22/00

Abstract

The invention concerns in the first instance a method for the manufacture of a reinforcement section 24 of a fibre composite component 94, which bounds a cavity 96, whereby a supporting core 40, with an elastic sleeve 42 bounding an interior space 44, is temporarily positioned in the cavity 96, with the steps: a) laying down of fibrous material 10 on a base moulding tool 12 to form a base element 14 of the fibre composite component 94, b) draping of fibrous material 10 in a negative mould 26, c) arrangement of the supporting core 40 on an inner surface 66 of the fibrous material 10 of the reinforcement section 24 in the negative mould 26, d) positioning of the negative mould 26, fitted with the fibrous material 10 and the supporting core 40, on the base element 14 to form the reinforcement section 24, e) forming of a vacuum chamber 60 accommodating the negative mould 26 and the base element 14 by covering by means of a vacuum film 58, f) evacuation of the vacuum chamber 60, and g) curing of the fibrous material 10, whereby when using a dry fibrous material 10 a matrix material, in particular a resin material 90, is injected into the fibrous material 10 after the evacuation. In addition the invention has as its subject a supporting core 40 for the execution of the method, and also a fibre composite component 94 produced in accordance with the method.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete