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:
Jan. 02, 2024

Filed:

Jun. 03, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Alston Ilford Scipio, Mableton, GA (US);

Sanji Ekanayake, Mableton, GA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/34 (2006.01); F02C 3/22 (2006.01); B08B 3/00 (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); F01D 25/00 (2006.01); F23D 14/50 (2006.01); F23R 3/36 (2006.01); F02C 7/30 (2006.01); F23K 5/00 (2006.01); F23D 11/38 (2006.01); F23D 14/64 (2006.01); F02C 7/228 (2006.01);
U.S. Cl.
CPC ...
F02C 3/22 (2013.01); B08B 3/003 (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); F01D 25/002 (2013.01); F02C 7/30 (2013.01); F23D 14/50 (2013.01); F23R 3/346 (2013.01); F23R 3/36 (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); F23D 11/386 (2013.01); F23D 14/64 (2013.01); F23K 5/00 (2013.01);
Abstract

A gas turbine engine system includes a gas turbine engine including a compressor, combustor including a plurality of late lean fuel injectors supplied with secondary fuel; gas turbine, and wash system configured to be attached and in fluid communication with the late lean fuel injectors. The wash system includes a water source including water; first fluid source including a first fluid providing vanadium ash and vanadium deposit mitigation and removal from internal gas turbine components; a mixing chamber in communication with the water source and first fluid source; a water pump to pump the water to the mixing chamber; a first fluid pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at the late lean fuel injectors while the gas turbine engine is on-line.


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