Patent ID: 11920790
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 1:
2. The combustor liner according to claim 1, wherein the combustor liner defines an axial direction along the combustor centerline, a radial direction extending from the combustor centerline, and the circumferential direction extending circumferentially about the combustor centerline,
the each segment of the plurality of outer liner segments having an outer liner cold surface side and an outer liner hot surface side, and defining an outer flow direction extending in the axial direction from an outer liner upstream end to an outer liner downstream end, the outer liner dilution zone being between the outer liner upstream end and the outer liner downstream end, and the outer liner deflector wall extending in the radial direction radially inward from the outer liner hot surface side, and
the each segment of the plurality of inner liner segments having an inner liner cold surface side and an inner liner hot surface side, and defining an inner liner flow direction extending in the axial direction from an inner liner upstream end to an inner liner downstream end, the inner liner dilution zone being between the inner liner upstream end and the inner liner downstream end, and each inner liner deflector wall extending in the radial direction radially outward from the inner liner hot surface side.