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:
Oct. 16, 2018

Filed:

Aug. 25, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Stephen Francis Bancheri, Albany, NY (US);

Venkat Subramaniam Venkataramani, Clifton Park, NY (US);

Glen Harold Kirby, Liberty Township, OH (US);

Neelesh Nandkumar Sarawate, Niskayuna, NC (US);

Nicholas Edward Antolino, Schenectady, NY (US);

Edip Sevincer, Watervliet, NY (US);

Anthony Christopher Marin, Saratoga Springs, NY (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 9/04 (2006.01); F01D 25/00 (2006.01); F16J 15/08 (2006.01); B05D 1/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/003 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 25/005 (2013.01); F16J 15/0887 (2013.01); B05D 1/005 (2013.01); F05D 2230/90 (2013.01); F05D 2240/11 (2013.01); F05D 2240/80 (2013.01); Y02T 50/672 (2013.01);
Abstract

A coated seal slot system for turbomachinery includes a first turbine component comprising a first groove having at least one first coating attached to at least a portion of the first groove of the first turbine component, a second turbine component comprising a second groove having at least one second coating attached to at least a portion of the second groove of the second turbine component. The first and the second turbine components are disposable adjacent to each other with the first groove having the first coating and the second groove having the second coating together forming a coated seal slot extending across a gap between the first turbine component and the second turbine component. A seal is disposable in the coated seal slot and extendable across the gap between the first and the second turbine components and engageable with the first coating and the second coating to inhibit leakage of gas through the gap.


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