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:
Feb. 27, 2024

Filed:

Feb. 07, 2022
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Aurelien Vayssiere, Niederschoenenfeld GT Feldheim, DE;

Hubert Neukirch, Dilligen, DE;

Markus Kammerer, Alerheim, DE;

Bernhard Rein, Rain Am Lech, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 1/12 (2006.01); B64D 27/26 (2006.01); B64D 45/00 (2006.01); B64C 27/06 (2006.01);
U.S. Cl.
CPC ...
B64C 27/006 (2013.01); B64C 1/12 (2013.01); B64C 27/00 (2013.01); B64D 27/26 (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, 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, wherein the firewall arrangement comprises at least one gasket for tightening pass-through of a torque tube that connects the at least one aircraft engine to a main gear box of the rotary wing aircraft, and wherein the at least one gasket comprises at least two fire proof shells and a ring-shaped flexible fire proof bellows.


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