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:
Jun. 05, 2018

Filed:

Jul. 16, 2015
Applicant:

General Electric Company;

Inventors:

Aaron Gregory Winn, Piedmont, SC (US);

George Andrew Gergely, Simpsonville, SC (US);

Mary Virginia Holloway, Simpsonville, SC (US);

Paul Kendall Smith, Simpsonville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 25/12 (2006.01); F01D 9/02 (2006.01); F01D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/187 (2013.01); F01D 9/02 (2013.01); F01D 25/12 (2013.01); F05D 2220/30 (2013.01); F05D 2240/122 (2013.01); F05D 2240/128 (2013.01); F05D 2240/81 (2013.01); F05D 2260/2214 (2013.01);
Abstract

Embodiments of the present disclosure provide a cooling structure for a stationary blade, including: an endwall coupled to a radial end of an airfoil; a chamber positioned within the endwall and radially displaced from a radially outer end of the trailing edge of the airfoil, wherein the chamber includes a pair of opposing chamber walls, one of the pair of opposing chamber walls being positioned proximal to the pressure side surface of the airfoil and the other of the pair of opposing chamber walls being positioned proximal to the suction side surface and the trailing edge of the airfoil, and wherein the cooling fluid in the chamber is in thermal communication with least a portion of the endwall positioned proximal to the pressure side surface and the trailing edge of the airfoil; and a plurality of thermally conductive fixtures positioned within the chamber.


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