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. 15, 2019

Filed:

Oct. 20, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Herbert Chidsey Roberts, Middletown, OH (US);

Richard William Albrecht, Jr., Fairfield, OH (US);

Michael John McCarren, South Lebanon, OH (US);

Peter Andrew Flynn, Delmar, NY (US);

Michael Francis Xavier Gigliotti, Jr., Glenville, NY (US);

Eric Alan Estill, Morrow, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 5/06 (2006.01); F01D 5/32 (2006.01); F01D 5/34 (2006.01); B22F 7/06 (2006.01); B22F 3/105 (2006.01); B22F 5/00 (2006.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); B22F 5/04 (2006.01); F01D 5/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/30 (2013.01); B22F 3/1055 (2013.01); B22F 5/009 (2013.01); B22F 5/04 (2013.01); B22F 7/062 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F01D 5/02 (2013.01); F01D 5/026 (2013.01); F01D 5/06 (2013.01); F01D 5/066 (2013.01); F01D 5/3061 (2013.01); F01D 5/32 (2013.01); F01D 5/34 (2013.01); F05D 2230/31 (2013.01); Y02P 10/295 (2015.11); Y02T 50/673 (2013.01);
Abstract

A bladed disk for a gas turbine engine is provided. The bladed disk includes a rotor disk, a plurality of rotor blades, and an interlocking transition zone. The rotor disk includes a plurality of fused layers of a first material formed via additive manufacturing and defines an outer rim. The plurality of rotor blades includes a plurality of fused layers of a second material formed via additive manufacturing. The interlocking transition zone includes a plurality of projections alternately extending from the outer rim of the rotor disk and the plurality of rotor blades, respectively, to undetachably couple the rotor disk and the plurality of rotor blades.


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