Verkleidung mit Lufteinlassvorrichtung für ein Flugzeug, Herstellungsverfahren dafür und Flugzeug

Details

Veröffentlichungs-Nr.

EP4628401

Aktenzeichen

EP24168787

Anmeldetag

5. April 2024

Veröffentlichung

8. Oktober 2025

Rechtsraum

EP

IPC

B64C7/00B64C21/06

Abstract

A fairing (10), in particular for an aircraft, comprises a wall element (12) comprising an inner surface (16) and an outer surface (14), wherein the outer surface (14) is exposed to a free air flow (F) outside the fairing (10), and at least one stiffener element (18) attached to the inner surface (16) of the wall element (12), to keep the fairing in shape under dynamic pressure loads. The fairing (10) comprises at least one air inlet device (22) comprising an inlet opening (26) to allow a part of the free air flow (F) outside the fairing (10) to pass through the wall element (12) and to enter the interior of the fairing (10). The air inlet device (22) is at least partially integrated into the stiffener element (18), and the inlet opening (26) of the air inlet device (22) is formed in the stiffener element (18) and extends into or through the stiffener element (18). The air inlet device (22) and the stiffener element (18) may be integrally formed as one single part, preferably by 3D printing.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete