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:
Oct. 08, 2019

Filed:

Mar. 18, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Christopher Paul Willis, Liberty, SC (US);

Richard Martin DiCintio, Simpsonville, SC (US);

Patrick Benedict Melton, Horse Shoe, NC (US);

Lucas John Stoia, Taylors, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F23R 3/60 (2006.01); F23R 3/00 (2006.01); F01D 11/18 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F01D 9/023 (2013.01); F01D 11/18 (2013.01); F01D 25/24 (2013.01); F23R 3/005 (2013.01); F23R 3/60 (2013.01); F05D 2230/642 (2013.01); F05D 2300/50212 (2013.01); F23R 2900/00012 (2013.01);
Abstract

An assembly for controlling a gap between a liner and a stationary nozzle within a gas turbine includes an annular liner having an aft frame that is disposed at an aft end of the liner, and a mounting bracket that is coupled to the aft frame. The assembly further includes a turbine having an outer turbine shell and an inner turbine shell that at least partially defines an inlet to the turbine. A stationary nozzle is disposed between the aft frame and the inlet. The stationary nozzle includes a top platform portion having a leading edge that extends towards the aft frame and a bottom platform portion. A gap is defined between the aft end of the aft frame and the leading edge of the top platform portion. The mounting bracket is coupled to the outer turbine shell, and stationary nozzle is coupled to the inner turbine shell.


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