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:
Jan. 05, 2016

Filed:

Dec. 23, 2010
Applicants:

Toby George Darkins, Jr., Loveland, OH (US);

John Peter Heyward, Loveland, OH (US);

Eric Alan Estill, Morrow, OH (US);

Joshua Brian Jamison, Liberty Township, OH (US);

James Herbert Deines, Mason, OH (US);

Mark Willard Marusko, Springboro, OH (US);

James Thomas Hawkins, Loveland, OH (US);

Inventors:

Toby George Darkins, Jr., Loveland, OH (US);

John Peter Heyward, Loveland, OH (US);

Eric Alan Estill, Morrow, OH (US);

Joshua Brian Jamison, Liberty Township, OH (US);

James Herbert Deines, Mason, OH (US);

Mark Willard Marusko, Springboro, OH (US);

James Thomas Hawkins, Loveland, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/284 (2013.01); F01D 5/147 (2013.01); Y02T 50/672 (2013.01);
Abstract

Hybrid turbine airfoil components containing a ceramic material, in which detailed features of the components are formed of materials other than ceramic materials. The components include a first component formed of a ceramic-based material and a second component formed of a metallic material. The first component comprises an airfoil portion and a nub, and the second component is separately formed and attached to the first component by casting the metallic material around the nub of the first component. The second component includes a platform portion between the airfoil portion and the nub of the first component and a dovetail portion on the nub of the first component. Each of the platform and dovetail portions has at least one off-axis geometric feature that results in the second component having a more complex geometry than the first component.


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