Verstärkungskomponente für eine Struktur eines Luft- oder Raumfahrzeugs, Luft- oder Raumfahrzeug und Verfahren

Details

Veröffentlichungs-Nr.

EP3254830

Aktenzeichen

EP17155096

Anmeldetag

8. Februar 2017

Veröffentlichung

7. April 2021

Erteilung

7. April 2021

Rechtsraum

EP

IPC

B29C65/02B29C45/14B29C45/00B64C1/06B64C1/12B64G1/22// B29L31/30B64C1/00

Abstract

Reinforcing component (11), and its manufacturing method, for a structure of an aircraft or spacecraft (1) which comprises a first component region (13), which is in particular elongate, for reinforcing at least one other element (19), and at least one second component region (17), which is permanently connected to the first component region (13). The reinforcing component (11) is formed using a thermoplastic plastics material in each of the first component region (13) and the second component region (17). In the first component region (13), the thermoplastic plastics material forms a matrix in which continuous reinforcing fibres (31) are embedded, and, in the second component region (17), the reinforcing component (11) comprises discontinuous reinforcing fibres (37) or is free of reinforcing fibres.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete