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:
Jun. 08, 2021

Filed:

Aug. 22, 2018
Applicants:

Airbus Operations S.a.s., Toulouse, FR;

Airbus Sas, Blagnac, FR;

Inventors:

Daniel Kierbel, Toulouse, FR;

Mathias Farouz-Fouquet, Toulouse, FR;

Laurent Malard, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/26 (2006.01); B64C 3/28 (2006.01); B64C 21/10 (2006.01); B21D 53/92 (2006.01); B29C 45/14 (2006.01); B21D 26/021 (2011.01); B64C 3/24 (2006.01); B29C 70/78 (2006.01);
U.S. Cl.
CPC ...
B64C 3/26 (2013.01); B21D 26/021 (2013.01); B21D 53/92 (2013.01); B29C 45/14008 (2013.01); B29C 45/14336 (2013.01); B29C 70/78 (2013.01); B64C 3/24 (2013.01); B64C 3/28 (2013.01); B64C 21/10 (2013.01);
Abstract

A method for manufacturing an aircraft leading edge panel, includes a step of overmoulding a coating onto a sheet positioned in a cavity of a mould, which cavity is delimited by a shaping surface which exhibits an optimized surface finish. The coating includes, after the overmoulding step, an exterior face which corresponds to the exterior face of the panel that is to be obtained and which exhibits an optimized surface finish conferred by the shaping surface of the mould. A panel may be obtained using this method and a leading edge includes at least one such panel. Because of the optimized surface finish of the exterior surface thereof, the panel contributes to extending the regions of laminar flow.


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