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:
Feb. 22, 2011

Filed:

Nov. 28, 2006
Applicants:

Daniel Edward Wines, Cincinnati, OH (US);

Randy Joseph Ketterer, Cincinnati, OH (US);

Barbara Ann Link, West Chester, OH (US);

Mark Dean Pezzutti, Mason, OH (US);

Charles William Carrier, West Chester, OH (US);

Terrence Owen Dyer, Cincinnati, OH (US);

Richard Gordon Menzies, Eden, UT (US);

Andrew John Lammas, Greenville, OH (US);

Inventors:

Daniel Edward Wines, Cincinnati, OH (US);

Randy Joseph Ketterer, Cincinnati, OH (US);

Barbara Ann Link, West Chester, OH (US);

Mark Dean Pezzutti, Mason, OH (US);

Charles William Carrier, West Chester, OH (US);

Terrence Owen Dyer, Cincinnati, OH (US);

Richard Gordon Menzies, Eden, UT (US);

Andrew John Lammas, Greenville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method for fabricating a rotor assembly for a turbine, the turbine including a central rotational axis is provided. The method includes forging a first rotor component from a first material, separately forging a second rotor component from a second material, and coupling the second rotor component to the first rotor component at a location radially inward of the first rotor component. The second rotor component is coupled to the first rotor component in at least one axial-circumferential plane that is at least one of substantially parallel and obliquely oriented with respect to the central rotational axis.


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