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. 27, 2016

Filed:

Mar. 11, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Radu Ioan Danescu, Greer, SC (US);

David Martin Johnson, Simpsonville, SC (US);

Kenneth Damon Black, Greenville, SC (US);

Christopher Paul Cox, Greenville, SC (US);

Ozgur Bozkurt, Greenville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F01D 19/02 (2006.01); F01D 11/24 (2006.01); F01D 25/08 (2006.01);
U.S. Cl.
CPC ...
F01D 19/02 (2013.01); F01D 11/24 (2013.01); F01D 25/08 (2013.01); F05D 2260/20 (2013.01);
Abstract

A turbine casing includes at least one shell adapted to enclose one or more turbine stages in a gas turbine engine; an air inlet in the at least one shell; a flow sleeve secured to an inside surface of the at least one shell, the flow sleeve comprising at least two arcuate segments. Each arcuate segment includes an arcuate base, a pair of sidewalls extending radially outwardly of the base thereby forming a circumferentially-extending flow channel defined by the base, the sidewalls and the inside surface. The air inlet is aligned with the flow channel and the sleeve is configured to distribute air flowing in the channel into spaces proximate the one or more turbine stages in circumferential, radial and axial directions, including along the inside surface of the at least one shell.


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