Drehflügelflugzeug mit einer Stabilisatoranordnung

Details

Veröffentlichungs-Nr.

EP4011767

Aktenzeichen

EP20400026

Anmeldetag

14. Dezember 2020

Veröffentlichung

8. November 2023

Erteilung

8. November 2023

Rechtsraum

EP

IPC

B64C5/02B64C27/82B64C5/16B64C39/12B64C39/00

Abstract

A rotary wing aircraft (100) extending along an associated roll axis (R) between a nose region (101) and an aft region (102) and that comprises a fuselage (110) with a front section (112) and a rear section (114), the rotary wing aircraft (100) comprising: a main rotor (120) that is rotatably mounted at the front section (112), and a stabilizer arrangement (130) that is arranged at the rear section (114) in the aft region (102), wherein the rear section (114) extends between the front section (112) and the stabilizer arrangement (130) and comprises an asymmetrical cross-sectional profile (190) in direction of the associated roll axis (R).

Anmelder

Firma

AIRBUS HELICOPTERS DEUTSCHLAND GmbH

Land

🇩🇪 Deutschland

Fachgebiete