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EP4361026 Art A1 1. Mai 2024

Anmelder: Lilium eAircraft GmbH 🇩🇪

Details

Veröffentlichungs-Nr.
EP4361026
Aktenzeichen
EP22204194
Anmeldetag
27. Oktober 2022
Veröffentlichung
1. Mai 2024
Rechtsraum
EP
IPC
B64C9/18B64C9/38B64C29/00B64C39/12B64C23/06
Offizieller Volltext

Abstract

A wing (1) comprises: a fixed lift generating portion (2) extending along an extension direction of the wing (1); a moveable lift modifying portion (3) which is moveably, preferably pivotably, more preferably about a pivot axis (P) along the extension direction of the wing (1), connected to the fixed lift modifying portion (2), wherein the moveable lift modifying portion (3) comprises at least one propulsion device (31) configured to generate a thrust force along a thrust direction for powering the aerial vehicle, preferably a plurality of propulsion devices (31) arranged along the extension direction. In order to enhance the aerodynamic performance, the at least one propulsion device (31) forms a moveable wing tip end portion (4) located at a tip side along the extension direction of the wing (1), the moveable wing tip end portion (4) comprising an aerodynamic profile, which is in particular part of a winglet.

Anmelder

Firma
Lilium eAircraft GmbH
Land
🇩🇪 Deutschland
🇩🇪 Lilium

Deutsches Unternehmen mit Sitz in Weßling bei München, das elektrisch angetriebene Fluggeräte für den senkrechten Start und die urbane Luftmobilität entwickelt.

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