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. 23, 2021

Filed:

Feb. 22, 2017
Applicant:

Airbus Operations, S.l., Getafe, ES;

Inventors:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 5/02 (2006.01); B64C 1/00 (2006.01); B32B 37/14 (2006.01); B64C 9/00 (2006.01); B64C 3/20 (2006.01); B64D 45/02 (2006.01); B29C 70/24 (2006.01); B32B 5/06 (2006.01); B32B 15/02 (2006.01); B29L 31/30 (2006.01); B32B 38/00 (2006.01);
U.S. Cl.
CPC ...
B32B 5/028 (2013.01); B29C 70/24 (2013.01); B32B 37/14 (2013.01); B64C 1/00 (2013.01); B64C 3/20 (2013.01); B64C 9/00 (2013.01); B64D 45/02 (2013.01); B29L 2031/3085 (2013.01); B32B 5/02 (2013.01); B32B 5/06 (2013.01); B32B 15/02 (2013.01); B32B 2038/008 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2305/076 (2013.01); B32B 2305/72 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); D05D 2209/12 (2013.01); Y02T 50/40 (2013.01);
Abstract

A configuration and manufacturing method for a trailing edge of an aircraft airfoil, such as a control surface or a lifting surface is described. The trailing edge is formed and configured by upper and lower composite covers, which are stitched to each other with a metallic wire, such as the metallic wire is electrically in contact with upper and lower metallic meshes to provide electrical continuity between meshes. According to a method, upper and lower covers configuring the trailing edge, are stitched with the metallic wire before curing the covers, so that the metallic wire gets embedded within the composite material. A trailing edge for an aircraft airfoil, which is easy to manufacture and that at the same time fulfills aerodynamic, mechanical and electrical conductivity requirements is described.


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