Patent ID: 11898753
Assignee: GE INFRASTRUCTURE TECHNOLOGY LLC
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 9:
10. The system of claim 1, wherein the combustor comprises a combustor portion and a head end portion; wherein the combustor portion comprises the combustion chamber, the liner, the flow sleeve, and the passage; wherein the head end portion comprises a plurality of primary fuel nozzles in a head end chamber; wherein the combustor comprises a cap plate disposed between the head end chamber and the combustion chamber; wherein an air flow path extends from the compressor discharge chamber, through openings in the flow sleeve into the passage, along the passage to the head end chamber, and through the plurality of primary fuel nozzles into the combustion chamber, wherein the first fuel sweep louver extends from the flow sleeve into the passage toward the head end chamber.