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:
Aug. 23, 2016

Filed:

Oct. 18, 2012
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Matthew Stephen Casavant, Greenville, SC (US);

Kenneth Damon Black, Travelers Rest, SC (US);

David Martin Johnson, Simpsonville, SC (US);

Radu Ioan Danescu, Greer, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/24 (2006.01); F01D 11/16 (2006.01); F01D 11/02 (2006.01); F01D 11/18 (2006.01); F01D 11/20 (2006.01); F01D 11/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 11/025 (2013.01); F01D 11/14 (2013.01); F01D 11/16 (2013.01); F01D 11/18 (2013.01); F01D 11/20 (2013.01);
Abstract

Thermal control is provided for a gas turbine casing by supplying thermal control gas from a compressor to a space between an outer casing and an inner casing, and transferring the thermal control gas from the space through the opening in the inner casing via a plurality of holes defined through a plate attached to an outer surface of the inner casing. The holes are arranged with a predetermined non-uniform distribution corresponding to a desired preferential impingement pattern for providing non-uniform heat transfer. A gas turbine thermal control assembly includes structure providing preferential heat transfer from the inner casing during operation of the gas turbine via a thermal control gas flow path from radially outside of the inner casing into the interior of the gas turbine.


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