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:
Sep. 04, 2018

Filed:

Dec. 04, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Fred Thomas Willett, Jr., Burnt Hills, NY (US);

Eric David Roush, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 5/14 (2006.01); F01D 11/00 (2006.01); F01D 5/24 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/082 (2013.01); F01D 5/081 (2013.01); F01D 5/147 (2013.01); F01D 5/24 (2013.01); F01D 5/3015 (2013.01); F01D 11/003 (2013.01); F01D 11/006 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/30 (2013.01); F05D 2240/55 (2013.01); F05D 2240/81 (2013.01); F05D 2260/20 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbomachine blade may include an airfoil and a shank coupled to the airfoil. The shank may include a cover plate having a first circumferential face and a second, opposing circumferential face. A radial cooling groove is positioned in the first circumferential face and is configured to allow a cooling fluid to pass from a first radial position to a second, different radial position relative to the platform. The radial cooling groove provides cover plate and shank cooling. In addition, the radial cooling groove may deliver fluid for purging gaps between blade platforms and cover plates, which prevents the ingestion of hot gas from the turbine flowpath.


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