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:
Aug. 15, 2017

Filed:

Feb. 13, 2015
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Thomas Beumler, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B32B 37/12 (2006.01); B32B 37/16 (2006.01); B32B 15/14 (2006.01); B32B 3/06 (2006.01); B32B 3/08 (2006.01); B32B 5/02 (2006.01); B32B 5/12 (2006.01); B32B 7/00 (2006.01); B32B 7/12 (2006.01); B32B 15/20 (2006.01); B32B 15/092 (2006.01);
U.S. Cl.
CPC ...
B64C 1/00 (2013.01); B32B 3/06 (2013.01); B32B 3/08 (2013.01); B32B 5/02 (2013.01); B32B 5/12 (2013.01); B32B 7/005 (2013.01); B32B 7/12 (2013.01); B32B 15/092 (2013.01); B32B 15/14 (2013.01); B32B 15/20 (2013.01); B32B 37/1284 (2013.01); B32B 37/16 (2013.01); B32B 2260/046 (2013.01); B32B 2262/0269 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); B64C 2001/0081 (2013.01);
Abstract

An aircraft panel with a laminate structure is provided that comprises a stack of a plurality of metal sheet layers, at least one fiber reinforced adhesive layer, and at least one cover segment. At least one outer layer of the metal sheet layers comprises at least two separate metal sheets that overlap with each other along their respective commonly adjoining edges, providing an overlapping joint of the two separate metal sheets. The at least one fiber reinforced adhesive layer comprises fiber elements embedded in a matrix structure. One of the at least one fiber reinforced adhesive layers is arranged between two adjacent metal sheet layers. Further, the at least one cover segment is arranged on an outside surface of the laminate structure, the cover segment covering a region of the overlapping joint. Still further, the at least one cover segment comprises at least one layer of reinforcement fibers.


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