Aussenhaut eines Flugzeugrumpfs oder Flugzeugrumpfteils und Verfahren zur Überwachung der Strukturellen Integrität der Aussenhaut eines Flugzeugrumpfs oder Flugzeugrumpfteils

Details

Veröffentlichungs-Nr.

EP4782341

Anmeldetag

23. Januar 2025

Veröffentlichung

29. Juli 2026

Rechtsraum

EP

Abstract

The present invention provides an outer skin of an aircraft fuselage or aircraft fuselage section formed from a fibre reinforced plastic, in particular carbon fibre reinforced plastics (CFRP) in a layered configuration, comprising at least two layers (105a, b) having electrically conductive fibres (400), in particular carbon fibres, placed with alternating fibre orientations within the layers (105a, b) and embedded in a polymer matrix material, and a coating (100) consisting of or comprising magnetically active particles (101) configured to induce a change in physical properties of the coating (100) when exposed to a magnetic field (300), a method for monitoring the structural integrity of the outer skin of an aircraft fuselage or fuselage section and an aircraft having a fuselage or fuselage section provided with such an outer skin.

Anmelder

Firma

AIRBUS Operations GmbH

Land

🇩🇪 Deutschland