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

Claim 13:
14. The system of claim 1, comprising a second fuel conduit disposed in the compressor discharge chamber along the flow sleeve, wherein the second fuel conduit is offset from the exterior surface of the flow sleeve in the radial direction relative to the longitudinal axis of the combustor, the fuel sweep system comprises a second fuel sweep opening in the flow sleeve and a second fuel sweep louver coupled to the flow sleeve adjacent the second fuel sweep opening, the second fuel sweep opening and the second fuel sweep louver are disposed radially inward relative to the second fuel conduit, and the second fuel conduit overlaps with the second fuel sweep opening and the second fuel sweep louver in the axial direction and the circumferential direction relative to the longitudinal axis of the combustor.