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.
Patent No.:
Date of Patent:
Feb. 17, 2015
Filed:
Mar. 03, 2010
Jens Voss, Harsefeld, DE;
Patrique Doemeland, Hamburg, DE;
Ingo Roth, Hamburg, DE;
Airbus Operations GmbH, Hamburg, DE;
Abstract
A decompression assembly (') for an aircraft comprises a first cabin lining element (′) having a boundary area (′) and a second cabin lining element (′) having a boundary area (′), wherein the boundary area (′) of the second cabin lining element (′) is disposed at a smaller distance from an aircraft outer skin (′) than the boundary area (′) of the first cabin lining element (′). An air discharge opening (′) is disposed between the boundary area (′) of the first cabin lining element (′) and the boundary area (′) of the second cabin lining element (′) for discharging air from a cabin (′) of the aircraft into an area (′) of the aircraft located between the cabin lining elements (′) and the aircraft outer skin (′). A decompression element (′) is adapted to release a pressure compensation opening (′) between the cabin (′) of the aircraft and the area (′) of the aircraft located between the cabin lining elements (′) and the aircraft outer skin (′) in the event of decompression and is disposed in an area of the aircraft that is shielded from an interior of the cabin (′) of the aircraft by the first and/or the second cabin lining element (′).