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:
Aug. 06, 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);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/16 (2006.01); B33Y 80/00 (2015.01); F01D 5/18 (2006.01); F01D 25/06 (2006.01); B22F 5/04 (2006.01); B22F 3/105 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 5/22 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B22F 3/1055 (2013.01); B22F 5/04 (2013.01); B33Y 80/00 (2014.12); F01D 5/16 (2013.01); F01D 5/187 (2013.01); F01D 5/22 (2013.01); F01D 5/288 (2013.01); F01D 25/06 (2013.01); F05D 2220/30 (2013.01); F05D 2230/31 (2013.01); F05D 2230/60 (2013.01); F05D 2230/90 (2013.01); F05D 2240/303 (2013.01); F05D 2240/307 (2013.01); F05D 2240/81 (2013.01); F05D 2260/231 (2013.01); F05D 2260/30 (2013.01); Y02P 10/295 (2015.11); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01); Y02T 50/6765 (2018.05);
Abstract

A rotor blade formed via additive manufacturing is provided. The rotor blade includes an airfoil and a coupled component. The airfoil includes a plurality of fused layers of a first material formed via additive manufacturing and defines a leading edge and a tip at a distal end. The coupled component includes a plurality of fused layers of a second material formed via additive manufacturing. An interlocking transition zone includes a plurality of projections alternately extending from the airfoil and the coupled component, respectively, to undetachably couple the airfoil and the coupled component.


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