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公开(公告)号:US20230115387A1
公开(公告)日:2023-04-13
申请号:US18080809
申请日:2022-12-14
Applicant: General Electric Company
Inventor: Alston Ilford Scipio , Colin Noel Stevens , Sanji Ekanayake
IPC: F01D25/00 , B08B3/02 , B08B3/08 , B08B9/032 , C11D3/00 , C11D3/28 , C11D3/30 , C11D11/00 , F02C7/30 , F23D14/50
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 amine 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 and at least one of the plurality of late lean fuel injectors.
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公开(公告)号:US11814972B2
公开(公告)日:2023-11-14
申请号:US17338010
申请日:2021-06-03
Applicant: General Electric Company
Inventor: Alston Ilford Scipio , Justin Todd Eggart , Colin Noel Stevens , Sanji Ekanayake
IPC: F02C7/30 , F01D25/00 , B08B3/02 , B08B3/08 , B08B9/032 , C11D3/04 , C11D11/00 , C11D17/00 , F23D14/50 , F23R3/34 , F23D11/38 , F23D14/64 , F23R3/46 , F23K5/00 , F02C7/228 , F23R3/36
CPC classification number: F01D25/002 , B08B3/02 , B08B3/08 , B08B9/0325 , C11D3/046 , C11D11/0041 , C11D17/0043 , F02C7/30 , F23D11/386 , F23D14/50 , F23D14/64 , F23R3/346 , B08B2203/027 , B08B2209/032 , F02C7/228 , F05D2220/32 , F05D2230/72 , F23K5/00 , F23R3/36 , F23R3/46 , F23R2900/00019
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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公开(公告)号:US20220389832A1
公开(公告)日:2022-12-08
申请号:US17338010
申请日:2021-06-03
Applicant: General Electric Company
Inventor: Alston Ilford Scipio , Justin Todd Eggart , Colin Noel Stevens , Sanji Ekanayake
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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公开(公告)号:US11555415B2
公开(公告)日:2023-01-17
申请号:US17338020
申请日:2021-06-03
Applicant: General Electric Company
Inventor: Alston Ilford Scipio , Colin Noel Stevens , Sanji Ekanayake
IPC: F01D25/00 , F23D14/50 , B08B9/032 , B08B3/08 , B08B3/02 , C11D11/00 , C11D3/00 , C11D3/30 , C11D3/28 , F02C7/30 , F23R3/34
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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公开(公告)号:US20220389833A1
公开(公告)日:2022-12-08
申请号:US17338020
申请日:2021-06-03
Applicant: General Electric Company
Inventor: Alston Ilford Scipio , Colin Noel Stevens , Sanji Ekanayake
IPC: F01D25/00 , F02C7/30 , F23D14/50 , B08B9/032 , B08B3/08 , B08B3/02 , C11D11/00 , C11D3/00 , C11D3/30 , C11D3/28
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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