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:
Sep. 03, 2019

Filed:

Apr. 07, 2014
Applicant:

Constellium Issoire, Issoire, FR;

Inventors:

Christophe Sigli, Grenoble, FR;

Bernard Bes, Seyssins, FR;

Frank Eberl, Issoire, FR;

Assignee:

CONSTELLIUM ISSOIRE, Issoire, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
C22C 21/18 (2006.01); C22C 21/12 (2006.01); C22C 21/16 (2006.01); C22F 1/057 (2006.01); B22D 7/00 (2006.01); C22C 21/14 (2006.01);
U.S. Cl.
CPC ...
C22C 21/18 (2013.01); B22D 7/005 (2013.01); C22C 21/12 (2013.01); C22C 21/14 (2013.01); C22C 21/16 (2013.01); C22F 1/057 (2013.01);
Abstract

A method for producing a rolled product 0.5 to 10 mm thick made from an aluminum alloy comprising, in particular, copper and lithium, in which, after solution annealing and quenching, a short heat treatment is carried out in which the sheet reaches a temperature of between 145° C. and 175° C. for 0.1 to 45 minutes, the speed of heating being between 3 and 600° C./min. The sheet obtained at the end of the method according to the invention has high corrosion resistance and is capable of being shaped for producing a structural element for an aircraft, in particular an aircraft fuselage skin.


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