Patent ID: 11859533
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B  C | IPC B  C  F

Claim 1:
2. The gas turbine engine system of claim 1, wherein the first fluid source includes a mixture of demineralized/deionized water and at least one of magnesium (Mg), yttrium (Y), or detergent as vanadium ash formation mitigant, the mixture of demineralized/deionized water and at least one of magnesium (Mg), yttrium (Y), or detergent as vanadium ash formation mitigant is configured to be injected into the combustor at at least one of the plurality of late lean fuel injectors; and the mixture of demineralized/deionized water and at least one of magnesium (Mg), yttrium (Y), or detergent as vanadium ash formation mitigant is delivered to the at least one of the plurality of late lean fuel injectors and then conveyed to internal components of gas turbine with a flow of combustion gases from the combustor to the gas turbine.