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:
Apr. 05, 2016

Filed:

Jul. 29, 2014
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Stephan Hoetzeldt, Bremen, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 3/02 (2006.01); B32B 37/10 (2006.01); B32B 5/24 (2006.01); B32B 7/04 (2006.01); B32B 27/08 (2006.01); B29C 70/46 (2006.01); B29C 37/00 (2006.01); B29L 31/30 (2006.01); B29C 33/42 (2006.01);
U.S. Cl.
CPC ...
B32B 37/10 (2013.01); B29C 37/0053 (2013.01); B29C 70/465 (2013.01); B32B 5/24 (2013.01); B32B 7/045 (2013.01); B32B 27/08 (2013.01); B29C 33/424 (2013.01); B29K 2995/0089 (2013.01); B29L 2031/3041 (2013.01); B29L 2031/3076 (2013.01); B32B 2250/02 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2309/12 (2013.01); B32B 2605/18 (2013.01); Y10T 428/24802 (2015.01); Y10T 428/24851 (2015.01);
Abstract

A method of producing a panel for lining or cladding an aircraft interior, such as an aircraft cargo hold includes arranging at least one resin layer of a thermo-plastic polymer and at least one reinforcement layer of reinforcement fibers upon one another in a stack, wherein each resin layer extends adjacent and/or substantially parallel to each reinforcement layer; and consolidating the stack to form a panel by applying heat and pressure to the stack. The pressure is applied to the stack in a direction substantially perpendicular to a primary plane of the layers. The pressure is applied to the stack in a non-constant distribution over the primary plane. A corresponding panel for lining or cladding an aircraft interior, such as a cargo hold is also described.


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