Vorderkantenvorrichtung für ein Aerodynamisches Bauteil und Verfahren zur Herstellung einer Vorderkantenvorrichtung für ein Aerodynamisches Bauteil

Details

Veröffentlichungs-Nr.

EP4527732

Aktenzeichen

EP23199406

Anmeldetag

25. September 2023

Veröffentlichung

26. März 2025

Rechtsraum

EP

IPC

B64C3/28B64C3/18B64C9/22

Abstract

The invention relates to a leading-edge device (1) for an aerodynamic component (120). The leading-edge device (1) comprises a first skin element (10) having an inner surface (11) and an aerodynamic outer surface (12), and further comprises a second skin element (20) having an inner surface (21) and an aerodynamic outer surface (22). The leading-edge device (1) further comprises a first coupling element (13) protruding from the inner surface (11) of the first skin element (10) and a second coupling element (23) protruding from the inner surface (21) of the second skin element (20). The first and second coupling elements (13, 23) are coupled to each other in a coupling region (30). The first skin element (10) and the first coupling element (13) are formed as a single-piece structure. The invention also relates to a method for manufacturing a leading-edge device (1) for an aerodynamic component (100).

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete