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. 01, 2022

Filed:

Dec. 26, 2019
Applicant:

Daher Aerospace, Saint Julien de Chedon, FR;

Inventors:

Pascal Hermel, Blagnac, FR;

Luc Gautrand, Labarthe sur Leze, FR;

François Bauvir, Colomiers, FR;

Arnaud Cazelles, Toulouse, FR;

David Clech, Toulouse, FR;

Assignee:

DAHER AEROSPACE, Saint Julien de Chédon, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/26 (2006.01); B64C 3/18 (2006.01); B29L 31/30 (2006.01); B64C 1/12 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 3/26 (2013.01); B64C 3/185 (2013.01); B29L 2031/3082 (2013.01); B29L 2031/3085 (2013.01); B32B 2605/18 (2013.01); B64C 1/12 (2013.01); B64C 3/187 (2013.01); B64C 2001/0072 (2013.01);
Abstract

A leading edge slat of a wing element of an aircraft. The aircraft defining a mark including a main fuselage axis x and a spanwise axis y. The wing procuring a lift along an axis z. The wing element having a skin forming the leading edge slat, a spar linked to the skin and a stiffening structure linked on the leading edge side to the spar and to the skin. The stiffening structure being formed from a formed sheet metal having a plurality of bosses distributed according to the length of the leading edge. The bosses extending between the spar and the inner face of the skin.


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