Verfahren und System zur Herstellung eines Verbundbauteils

Details

Veröffentlichungs-Nr.

EP4506147

Aktenzeichen

EP24182151

Anmeldetag

14. Juni 2024

Veröffentlichung

20. August 2025

Erteilung

20. August 2025

Rechtsraum

EP

IPC

B29C70/54// B29C70/44B29L31/00

Abstract

A method (300) for manufacturing a composite component (50) includes providing a tool (100) switchable between a deposition configuration (105) and a flange-forming configuration (107). The tool (100) includes a first portion (110) including a first deposition surface (111), a second portion (120) including a second deposition surface (121) and a pre-form support surface (122), and a flange-forming block (130) including a curved surface (131). The method (300) further includes depositing a composite material at least partially on each of the first deposition surface (111) and the second deposition surface (121) in the deposition configuration (105) to provide a composite pre-form (140). The method (300) further includes moving the second portion (120) relative to the first portion (110) to transition the tool (100) to the flange-forming configuration (107), which causes the composite pre-form (140) to at least partially engage each of the pre-form support surface (122) and the curved surface (131). The curved surface (131) defines a radius (51R) of a flange (51) of the composite component (50).

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien

Fachgebiete