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:
Jul. 05, 2016

Filed:

Jul. 27, 2012
Applicants:

Benjamin Paul Lacy, Greer, SC (US);

Gregory Allan Crum, Mauldin, SC (US);

James William Vehr, Easley, SC (US);

Inventors:

Benjamin Paul Lacy, Greer, SC (US);

Gregory Allan Crum, Mauldin, SC (US);

James William Vehr, Easley, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/08 (2006.01); F01D 25/12 (2006.01); F01D 9/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 9/065 (2013.01); F05D 2250/14 (2013.01); F05D 2250/75 (2013.01);
Abstract

A system for removing heat from a gas turbine generally includes a plurality of stationary nozzles arranged in an annular array within the gas turbine. Each of the plurality of stationary nozzles may include a radially outer platform and a radially extending cooling passage. The radially extending cooling passage may have an inlet that extends generally axially and circumferentially across a portion of the radially outer platform. A closed loop cooling coil may extend continuously circumferentially around the radially outer platform of two or more of the plurality of stationary nozzles. The closed loop cooling coil may be disposed circumferentially across and outside of the inlet of the radially extending cooling passage of each of the two or more stationary nozzles, and a cooling medium may flow through the cooling coil and out of the gas turbine so as to remove heat from the gas turbine.


Find Patent Forward Citations

Loading…