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. 14, 2023

Filed:

Jun. 03, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Alston Ilford Scipio, Mableton, GA (US);

Justin Todd Eggart, Marietta, GA (US);

Colin Noel Stevens, Atlanta, GA (US);

Sanji Ekanayake, Mableton, GA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/30 (2006.01); F01D 25/00 (2006.01); B08B 3/02 (2006.01); B08B 3/08 (2006.01); B08B 9/032 (2006.01); C11D 3/04 (2006.01); C11D 11/00 (2006.01); C11D 17/00 (2006.01); F23D 14/50 (2006.01); F23R 3/34 (2006.01); F23D 11/38 (2006.01); F23D 14/64 (2006.01); F23R 3/46 (2006.01); F23K 5/00 (2006.01); F02C 7/228 (2006.01); F23R 3/36 (2006.01);
U.S. Cl.
CPC ...
F01D 25/002 (2013.01); B08B 3/02 (2013.01); B08B 3/08 (2013.01); B08B 9/0325 (2013.01); C11D 3/046 (2013.01); C11D 11/0041 (2013.01); C11D 17/0043 (2013.01); F02C 7/30 (2013.01); F23D 11/386 (2013.01); F23D 14/50 (2013.01); F23D 14/64 (2013.01); F23R 3/346 (2013.01); B08B 2203/027 (2013.01); B08B 2209/032 (2013.01); F02C 7/228 (2013.01); F05D 2220/32 (2013.01); F05D 2230/72 (2013.01); F23K 5/00 (2013.01); F23R 3/36 (2013.01); F23R 3/46 (2013.01); F23R 2900/00019 (2013.01);
Abstract

A system comprises a gas turbine engine including a compressor, combustor, gas turbine, the combustor including a plurality of late lean fuel injectors; and wash system configured to be attached to and in fluid communication with the a plurality of late lean fuel injectors of the combustor. The wash system includes a water source supplying water; a first fluid source supplying a first fluid; a mixing chamber in communication with the water source and first fluid source; a water pump to pump water to the mixing chamber; a first fluid pump to pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and at least one of the plurality of late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at late lean fuel injectors. The wash system is operated with the gas turbine engine off-line.


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