Plattenelement und Flugzeuginnenteil

Details

Veröffentlichungs-Nr.

EP4752056

Anmeldetag

20. November 2025

Veröffentlichung

3. Juni 2026

Rechtsraum

EP

Abstract

Disclosed are a panel element, in particular for use as an aircraft interior part, comprising at least one plate component having a front side and a rear side, and a stiffening structure forming enforced areas of the plate component, wherein the stiffening structure comprises at least an edge protection frame surrounding outer edges of the at least one plate component, and local stiffening elements extending over adjacent surface areas of the front side and the rear side, wherein the stiffening structure is visible in a final state of the panel element on both sides, and an aircraft interior part comprising at least one panel element.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland