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:
Nov. 27, 2018

Filed:

Jun. 02, 2015
Applicant:

Alstom Technology Ltd, Baden, CH;

Inventors:

Uwe Rüdel, Baden-Rütihof, CH;

Urs Benz, Gipf-Oberfrick, CH;

Christoph Appel, Umiken, CH;

Ivan Lenuzzi, Karlovac, HR;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F23R 3/50 (2006.01); F23R 3/16 (2006.01); F02C 3/04 (2006.01); F02C 3/14 (2006.01); F02C 7/18 (2006.01); F23R 3/60 (2006.01); F23R 3/00 (2006.01); F23R 3/48 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F23R 3/50 (2013.01); F02C 3/04 (2013.01); F02C 3/14 (2013.01); F02C 7/18 (2013.01); F23R 3/002 (2013.01); F23R 3/16 (2013.01); F23R 3/48 (2013.01); F23R 3/60 (2013.01); F01D 9/023 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/201 (2013.01); F05D 2260/30 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03044 (2013.01); Y02E 20/16 (2013.01);
Abstract

The invention relates to an annular combustion chamber of a gas turbine having a machine axis. The combustion chamber includes at least two zones. A first zone receives the fuel/air mixture of a plurality of burners. A second zone guides the hot gases being produced by the burners from the first zone to an entrance of a turbine section of said gas turbine. An annular transition liner includes a plurality of liner segments located at the transition between said first zone and second zone. Each of the liner segments includes with respect to the axial hot gas flow a leading edge, a trailing edge, and two sidewalls, and is provided with axial mounting means at the leading and trailing edges, such that the liner segment can be installed in axial direction and is axially fixed by respective segments of the neighboring first zone. Local spacer ribs are provided at the leading edge of the liner segments in order to establish a gap of minimum width between the liner segments and the fixing segments of the neighboring first zone.


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