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. 23, 2014

Filed:

May. 14, 2008
Applicants:

Gary H. Bray, Murrysville, PA (US);

Dhruba J. Chakrabarti, Woodside, NY (US);

Diana K. Denzer, Lower Burrell, PA (US);

Jen C. Lin, Export, PA (US);

John Newman, Export, PA (US);

Gregory B. Venema, Bettendorf, IA (US);

Cagatay Yanar, Bethel Park, PA (US);

Julien Boselli, Pittsburgh, PA (US);

Inventors:

Gary H. Bray, Murrysville, PA (US);

Dhruba J. Chakrabarti, Woodside, NY (US);

Diana K. Denzer, Lower Burrell, PA (US);

Jen C. Lin, Export, PA (US);

John Newman, Export, PA (US);

Gregory B. Venema, Bettendorf, IA (US);

Cagatay Yanar, Bethel Park, PA (US);

Julien Boselli, Pittsburgh, PA (US);

Assignee:

Alcoa Inc., Pittsburgh, PA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C22C 21/10 (2006.01); B64C 3/26 (2006.01); C22F 1/053 (2006.01); B64C 3/18 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 3/26 (2013.01); C22F 1/053 (2013.01); B64C 3/185 (2013.01); Y02T 50/42 (2013.01); B64C 3/182 (2013.01); C22C 21/10 (2013.01); B64C 3/187 (2013.01); B64C 2001/0081 (2013.01);
Abstract

Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.


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