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. 31, 2015

Filed:

May. 29, 2009
Applicants:

Kenneth Rees Bain, Loveland, OH (US);

David Paul Mourer, Beverly, MA (US);

Richard Didomizio, Scotia, NY (US);

Timothy Hanlon, Glenmont, NY (US);

Laurent Cretegny, Niskayuna, NY (US);

Andrew Ezekiel Wessman, Walton, KY (US);

Inventors:

Kenneth Rees Bain, Loveland, OH (US);

David Paul Mourer, Beverly, MA (US);

Richard DiDomizio, Scotia, NY (US);

Timothy Hanlon, Glenmont, NY (US);

Laurent Cretegny, Niskayuna, NY (US);

Andrew Ezekiel Wessman, Walton, KY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
C22C 19/05 (2006.01); C22C 30/00 (2006.01); C22C 1/04 (2006.01); C22F 1/10 (2006.01);
U.S. Cl.
CPC ...
C22C 19/056 (2013.01); C22C 1/0433 (2013.01); C22F 1/10 (2013.01); B22F 2998/00 (2013.01);
Abstract

A gamma prime nickel-base superalloy and components formed therefrom that exhibit improved high-temperature dwell capabilities, including creep and hold time fatigue crack growth behavior. A particular example of a component is a powder metallurgy turbine disk of a gas turbine engine. The gamma-prime nickel-base superalloy contains, by weight, 16.0 to 30.0% cobalt, 11.5 to 15.0% chromium, 4.0 to 6.0% tantalum, 2.0 to 4.0% aluminum, 1.5 to 6.0% titanium, up to 5.0% tungsten, 1.0 to 7.0% molybdenum, up to 3.5% niobium, up to 1.0% hafnium, 0.02 to 0.20% carbon, 0.01 to 0.05% boron, 0.02 to 0.10% zirconium, the balance essentially nickel and impurities, wherein the titanium:aluminum weight ratio is 0.5 to 2.0.


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