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

Details

Veröffentlichungs-Nr.

EP4371872

Aktenzeichen

EP22208197

Anmeldetag

17. November 2022

Veröffentlichung

22. Mai 2024

Rechtsraum

EP

IPC

B64C9/24// B64C3/18

Abstract

The invention relates to leading edge device (10) for an aerodynamic component (100), comprising a skin element (12) defining an aerodynamic profile and being formed of a single-piece structure, wherein the skin element (12) has an inner surface (14) and an outer surface (16). The leading edge device (10) further comprises a support structure (20) having at least one support element (22), wherein the at least one support element (22) is bonded to the inner surface (14) of the skin element (12) via a connecting zone (15) that at least partially extends across the inner surface (14) of the skin element (12). The outer surface (16) of the skin element (12) defines a surface region (17) opposite to the connecting zone (15) where the outer surface (16) is closed. The invention also relates to a method for manufacturing a leading edge (10) device for an aerodynamic component (100).

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete