Flügel für ein Flugzeug und Verfahren zum Aufrüsten

Details

Veröffentlichungs-Nr.

EP4613641

Aktenzeichen

EP24162380

Anmeldetag

8. März 2024

Veröffentlichung

10. September 2025

Rechtsraum

EP

IPC

B64C9/22B64C9/02B64C9/24

Abstract

Described is a wing (3) for an aircraft (1) and a method of rigging a high lift assembly to the wing of an aircraft. A wing (3) for an aircraft (1), comprising a main wing (5) and a high lift assembly, the high lift assembly comprising a high lift body comprising a high lift structure, and a connection assembly (209) movably connecting the high lift body (12) to the main wing (5), such that the high lift body is movable between a retracted position and at least one extended position. The connection assembly (209) comprises a first connection profile and a second connection profile, and the connection assembly (209) is mounted to the main wing (5) by a mounting arrangement (214), the mounting arrangement (214) comprising a primary connection interface (216) and a secondary connection interface (218). The primary connection interface (216) is connected to the first connection profile (216) via a corresponding connection member (224) and the secondary connection interface (218) is connected to one of the at least one second connection profiles (218) via a corresponding connection member (224). The secondary connection interface (218) comprises an elongate aperture and an elongate interface component that is located between the corresponding connection member (224) and the secondary interface so as to restrict relative motion between the secondary connection interface (218) and the connection member (224) to secure the connection assembly (209) relative to the main wing (5) and prevent relative motion therebetween.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete