Drehflügelflugzeug mit einer Firewall-Anordnung mit mindestens einer Trichterförmigen Unteren Firewall

Details

Veröffentlichungs-Nr.

EP4458669

Aktenzeichen

EP23171892

Anmeldetag

5. Mai 2023

Veröffentlichung

2. Juli 2025

Erteilung

2. Juli 2025

Rechtsraum

EP

IPC

B64C27/00B64C1/40

Abstract

The invention relates to a rotary wing aircraft with a fuselage (2) that forms an aircraft interior region (2b), the fuselage comprising an upper primary skin (2c) that separates the aircraft interior region from an aircraft upper deck (6) arranged above the fuselage (2), the upper primary skin being mounted on top of a predetermined number of supporting beams; wherein the aircraft upper deck (6) comprises an engine accommodating region (7) with a firewall arrangement (10), the engine accommodating region accommodating at least one aircraft engine (11b) within the firewall arrangement (10) such that the firewall arrangement defines a fire proof separation at least between the at least one aircraft engine (11b) and the aircraft interior region (2b); and wherein the firewall arrangement (10) comprises at least a funnel-shaped lower firewall (10d) arranged between the at least one aircraft engine (11b) and the upper primary skin (2c) of the fuselage.

Anmelder

Firma

AIRBUS HELICOPTERS DEUTSCHLAND GmbH

Land

🇩🇪 Deutschland

Fachgebiete