{
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  "description": "Gas turbine engine system (10) includes a gas turbine (40) engine including a compressor (15), combustor (25) including a plurality of late lean fuel injectors (60); gas turbine, and wash system (100) configured to be attached and in fluid communication with the late lean fuel injectors. The wash…",
  "path": "/patents/1404057",
  "publishedAt": "2024-11-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B08B3/003",
    "GENERAL ELECTRIC TECHNOLOGY GMBH [CH]"
  ],
  "textContent": "Gas turbine engine system (10) includes a gas turbine (40) engine including a compressor (15), combustor (25) including a plurality of late lean fuel injectors (60); gas turbine, and wash system (100) configured to be attached and in fluid communication with the late lean fuel injectors. The wash system includes a water source (110); first fluid source including a first fluid providing vanadium ash and vanadium deposit mitigation and removal from internal gas turbine components; a mixing chamber (170) in communication with the water source and first fluid source; a water pump (220) to pump water (120) 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 is injected into the combustor at the late lean fuel injectors while the gas turbine engine is on-line.",
  "title": "GAS TURBINE ENGINE SYSTEM AND METHOD OF WASHING AN ON-LINE GAS TURBINE ENGINE"
}