Flügelanordnung für ein Flugzeug

Details

Veröffentlichungs-Nr.

EP3998194

Aktenzeichen

EP21161129

Anmeldetag

5. März 2021

Veröffentlichung

18. Mai 2022

Rechtsraum

EP

IPC

B64C3/48B64C9/16B64C29/00B64D27/02B64D27/12B64C39/12B64C11/00

Abstract

The present invention relates to a wing assembly (10) for an aircraft with a fuselage and at least one pair of wings, the wing assembly (10) defining a direction of flow (F) with respect to which the wing assembly (10) is configured to create lift for the aircraft, comprising a main section (12), which is configured to be mounted to the fuselage in a fixed manner so as to extend from the fuselage in an extension direction of the wing; and a plurality of flap sections (14) each with a body part (16), which are mounted to the main section (12) in a pivotable manner so as to be individually pivotable around a pivot axis (A) by means of a pivoting means (18) over a range of angular orientations including a horizontal orientation in which the body part (16) of the flap section (14) is substantially aligned with the main section (12) to form an elongate and substantially continuous cross-section; and a vertical orientation in which the flap section (14) is angled downwards with respect to the main section (12). The invention further relates to an aircraft equipped with at least one pair of such wing assemblies.

Anmelder

Firma

Lilium eAircraft GmbH

Land

🇩🇪 Deutschland

Fachgebiete