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US 2020/0049349 A1Published application
Dilution Structure for Gas Turbine Engine Combustor
AssigneeGeneral Electric Company
InventorsMayank Krisna Amble, Gurunath Gandikota, Perumallu Vukanti, Ravi Chandra, Karthikeyan Sampath
Life of this patent
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Abstract
The present disclosure is directed to a combustor assembly for a gas turbine engine. The combustor assembly includes a liner defining a combustion chamber therewithin and a pressure plenum surrounding the liner. The liner defines an opening and includes a walled chute disposed at least partially through the opening. A plurality of flow openings is defined through the walled chute.
Claims20
A combustor assembly for a gas turbine engine, the combustor assembly comprising:
- a liner defining a combustion chamber therewithin and a pressure plenum surrounding the liner, wherein the liner comprises an opening, and wherein the liner comprises a walled chute disposed at least partially through the opening, and further wherein a plurality of flow openings is defined through the walled chute, and wherein the walled chute is extended into the pressure plenum surrounding the liner.
A gas turbine engine, the gas turbine engine comprising:
- a combustor assembly comprising a liner defining a combustion chamber therewithin and a pressure plenum surrounding the liner, wherein the liner comprises an opening, and wherein the liner comprises a walled chute disposed at least partially through the opening, and further wherein a plurality of flow openings is defined through the walled chute.
Dependencies are inferred from the claim text.