Verfahren und Vorrichtung zur Reparatur eines Verbundwerkstoffelements

Details

Veröffentlichungs-Nr.

EP4813601

Anmeldetag

25. März 2025

Veröffentlichung

30. September 2026

Rechtsraum

EP

IPC

B29C35/02, B29C73/02

Abstract

Method and device for repairing an element (100) of composite material, the method comprising infusing a resin (300) into the internal damaged area (101) of the element (100) of composite material, wherein the method further comprises: drilling on the element (100) of composite material at least one first non-through hole (200a) and at least one second non-through hole (200b), each of the non-through holes (200) running from one face of the element (100) of composite material up to the internal damaged area (101), and infusing the resin (300) from the at least one first non-through hole (200a) until the resin (300) fills at least the internal damaged area (101) of the element (100) of composite material. The method comprises applying vibrations at a given frequency to the element (100) of composite material.

Anmelder

Firmen

Airbus Operations, S.L.U.
Airbus Operations Limited

Land

🇪🇸 Spanien

Fachgebiete