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. 20, 2018

Filed:

Dec. 17, 2014
Applicants:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Christian Gregor Endres, Pfaffenhofen, DE;

Hans-Jürgen Weber, Hamburg, DE;

Assignees:

AIRBUS DEFENCE AND SPACE GMBH, Taufkirchen, DE;

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
E04B 1/82 (2006.01); B64C 1/06 (2006.01); B29C 70/08 (2006.01); B29C 70/24 (2006.01); B29C 70/42 (2006.01); G10K 11/168 (2006.01); B29L 31/30 (2006.01); B29K 683/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/066 (2013.01); B29C 70/08 (2013.01); B29C 70/086 (2013.01); B29C 70/24 (2013.01); B29C 70/42 (2013.01); G10K 11/168 (2013.01); B29K 2683/00 (2013.01); B29K 2715/003 (2013.01); B29K 2995/0002 (2013.01); B29L 2031/3041 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3082 (2013.01); Y02T 50/433 (2013.01); Y02T 50/46 (2013.01);
Abstract

The present invention relates to acoustical panels. As to provide a cabin panel to be made as simple as possible and with optimized acoustical properties, an acoustical cabin panel () is provided that comprises a first () and a second layer () which are spaced apart from each other by an intermediate layer () and altogether with a plurality of reinforcement elements () form a core composite component (). Furthermore, the panel comprises at least one intermediate layer () made of a core material () which is arranged in the intermediate layer. The reinforcement elements extend from the first to the second layer through the at least one intermediate film and are tension and pressure resilient in a finished state of the panel. The reinforcement elements can be at least partially infiltrated with a curable matrix material and at least one prepreg () soaked with matrix material is provided in the first and/or second layer. Thereby, the reinforcement elements to be infiltrated with matrix material are connected to the prepreg.


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