Flugzeug

Details

Veröffentlichungs-Nr.

EP4813834

Anmeldetag

3. Februar 2026

Veröffentlichung

30. September 2026

Rechtsraum

EP

IPC

B64C5/02, B64C5/10, B64C39/04

Abstract

The present invention provides an aircraft (100), having a fuselage (110), a wing assembly (120), a propulsion device (130), and two tail booms (140), each comprising a stem (141) and a stabilizing surface (142), wherein the stabilizing surfaces (142) of the tail booms (140) are each arranged symmetrically with respect to the respective stem (141) of the tail boom (140), wherein the stabilizing surfaces (142) of the tail booms (140) are arranged at an angle to one another in such a way that upper edges of the stabilizing surfaces (142) have a smaller spacing than lower edges of the stabilizing surfaces (142), and wherein each of the stabilizing surfaces (142) has a tilting device (143) for controlling the aircraft (100).

Anmelder

Firma

Airbus Defence and Space GmbH

Land

🇩🇪 Deutschland

Fachgebiete