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. 01, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Melbourne James Myers, Woodruff, SC (US);

Camilo Andres Sampayo, Greer, SC (US);

Xiuzhang James Zhang, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/14 (2006.01); F01D 5/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/082 (2013.01); F01D 5/147 (2013.01); F05D 2240/304 (2013.01); F05D 2240/80 (2013.01); F05D 2260/20 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbomachine blade is disclosed including an airfoil including a cooling fluid plenum extending therein and a trailing edge cooling opening extending from the cooling fluid plenum through a trailing edge of the airfoil. A platform may couple the airfoil to a shank, the platform including a trailing edge extending downstream relative to the shank. At least one cooling conduit delivers a cooling fluid radially inward from at least one of the cooling fluid plenum and the trailing edge cooling opening to a wheel space that is adjacent the shank and radially inward from the trailing edge of the platform. A related turbomachine is also disclosed.


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