The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 25, 2025

Filed:

Apr. 10, 2024
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauwörth, DE;

Inventors:

Axel Fink, Donauwörth, DE;

Manuel Kempf, Donauwörth, DE;

Philipp Walch, Rain am Lech, DE;

Luca Specht, Petershausen, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 1/12 (2006.01); B64C 27/06 (2006.01); B64D 27/02 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/006 (2013.01); B64C 1/12 (2013.01); B64D 27/02 (2013.01); B64D 45/00 (2013.01); B64C 27/06 (2013.01); B64D 2045/009 (2013.01);
Abstract

A rotary wing aircraft with a fuselage that forms an aircraft interior region, the fuselage comprising an upper primary skin that separates the aircraft interior region from an aircraft upper deck arranged above the fuselage, the upper primary skin being mounted on top of a predetermined number of supporting beams; wherein the aircraft upper deck comprises an engine accommodating region with a firewall arrangement, the engine accommodating region accommodating at least one aircraft engine within the firewall arrangement such that the firewall arrangement defines a fire proof separation at least between the at least one aircraft engine and the aircraft interior region; and wherein the firewall arrangement comprises at least a funnel-shaped lower firewall arranged between the at least one aircraft engine and the upper primary skin of the fuselage.


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