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. 17, 2023

Filed:

Jun. 03, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Alston Ilford Scipio, Mableton, 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 ...
F01D 25/00 (2006.01); F23D 14/50 (2006.01); B08B 9/032 (2006.01); B08B 3/08 (2006.01); B08B 3/02 (2006.01); C11D 11/00 (2006.01); C11D 3/00 (2006.01); C11D 3/30 (2006.01); C11D 3/28 (2006.01); F02C 7/30 (2006.01); F23R 3/34 (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 3/0073 (2013.01); C11D 3/28 (2013.01); C11D 3/30 (2013.01); C11D 11/0041 (2013.01); F02C 7/30 (2013.01); F23D 14/50 (2013.01); B08B 2203/027 (2013.01); B08B 2209/032 (2013.01); F05D 2220/32 (2013.01); F05D 2230/72 (2013.01); F05D 2230/90 (2013.01); F23R 3/346 (2013.01);
Abstract

A gas turbine engine system includes a compressor, gas turbine, and combustor including a plurality of late lean fuel injectors supplied with secondary fuel to its interior. The gas turbine engine system includes a wash system in communication with the late lean fuel injectors. The wash system includes a water source; water pump; anti-corrosion agent fluid source with an anti-corrosion agent including a polyamine corrosion inhibitor; anti-corrosion agent supply piping in fluid communication with the anti-corrosion agent fluid source; mixing chamber receiving water and anti-corrosion agent to produce an anti-corrosion mixture in fluid communication with the mixing chamber and the plurality of late lean fuel injectors. Fluid from the mixing chamber including the water, the anti-corrosion agent fluid source, or a mixture thereof is injected, while the gas turbine engine is off-line, into the combustor at at least one of the plurality of late lean fuel injectors.


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