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:
Apr. 20, 2021

Filed:

Feb. 20, 2019
Applicant:

Siemens Energy, Inc., Orlando, FL (US);

Inventors:

Charalambos Polyzopoulos, Orlando, FL (US);

Richard L. Thackway, Oviedo, FL (US);

Stephen A. Ramier, Fredericton, CA;

Vinayak V. Barve, Cumming, GA (US);

Khalil Farid Abou-Jaoude, Winter Springs, FL (US);

Daniel W. Garan, Chuluota, FL (US);

David P. Holzapfel, Charlotte, NC (US);

Kevin J. Spence, Jupiter, FL (US);

Joseph Scott Markovitz, Sanford, FL (US);

Blake R. Cotten, Orlando, FL (US);

Urmi B. Dave, Oviedo, FL (US);

Vaidyanathan Krishnan, Charlotte, NC (US);

Michael C. Escandon, Oviedo, FL (US);

Assignee:

SIEMENS ENERGY, INC., Orlando, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/00 (2006.01); F01D 9/02 (2006.01); F23R 3/16 (2006.01); F23R 3/28 (2006.01); F23R 3/36 (2006.01); F23R 3/48 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F01D 9/023 (2013.01); F02C 3/04 (2013.01); F23R 3/06 (2013.01); F23R 3/16 (2013.01); F23R 3/28 (2013.01); F23R 3/36 (2013.01); F23R 3/48 (2013.01); F05B 2240/40 (2013.01); F05D 2240/35 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03043 (2013.01); Y02T 50/60 (2013.01);
Abstract

An improved combustion section for a gas turbine engine is disclosed. A fuel nozzle includes new features which provide improved injection patterns of oil fuel and cooling water, resulting in better control of combustion gas temperature and NOx emissions, and eliminated impingement of cooling water on walls of the combustor. A new combustor includes a plate-fin design which provides improved cooling, while the combustor also makes more efficient use of available cooling air and has an improved component life. A new transition component has a smoother shape which reduces stagnation of combustion gas flow and impingement of combustion gas on transition component walls, improved materials and localized thickness increases for better durability, and improved cooling features for more efficient usage of cooling air.


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