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US 8,104,288 B2Granted
Effusion cooling techniques for combustors in engine assemblies
AssigneeHoneywell International Inc.
InventorsGregory O. Woodcock, Timothy Ertz, Brian Koch
Life of this patent
Estimating the term…
Abstract
A combustor for an engine assembly includes a cylindrical wall forming a combustion chamber in which an air and fuel mixture is combusted; and a plurality of effusion cooling holes formed in the cylindrical wall, the plurality of effusion cooling holes oriented such that cooling air flowing therethrough cools the cylindrical wall with effusion cooling, convection cooling, and impingement cooling.
Claims15
A combustor for an engine assembly, comprising:
- a cylindrical wall forming a combustion chamber in which an air and fuel mixture is combusted;
- and
- a plurality of effusion cooling holes formed in the cylindrical wall, the plurality of effusion cooling holes oriented such that cooling air flowing therethrough cools the cylindrical wall with effusion cooling, convection cooling, and impingement cooling, wherein each of the plurality of effusion cooling holes is oriented such that the cooling air flowing therethough strikes an inner portion of the cylindrical wall cooling the inner portion as impingement cooling, wherein each of the plurality of effusion cooling holes is oriented at an angle of about 10° to about 30° relative to a tangent line on the cylindrical wall, the tangent line in a plane perpendicular to a centerline of the combustion chamber.
A combustor for an engine assembly, comprising:
- a cylindrical wall forming a combustion chamber in which an air and fuel mixture is combusted;
- and
- a plurality of effusion cooling holes formed in the cylindrical wall, wherein each of the plurality of effusion cooling holes is oriented at an angle of about 60° to about 120° relative to a meridinal line of the combustion chamber and at an angle of about 10° to about 30° relative to a tangent line on the cylindrical wall, the tangent line in a plane perpendicular to a centerline of the combustion chamber, wherein the plurality of effusion cooling holes is oriented such that cooling air flowing therethrough cools the cylindrical wall with convection cooling and cools an inner portion of the cylindrical wall with effusion cooling and impingement cooling.
An engine assembly, comprising:
- a compressor section configured to supply compressed air;
- a combustor section configured to received the compressed air, to mix the compressed air with fuel, and to ignite the air-fuel mixture to produce combustion gases, the combustor section comprising a combustor with a cylindrical wall and a plurality of effusion cooling holes formed in the cylindrical wall, the plurality of effusion cooling holes oriented such that cooling air flowing therethrough cools the cylindrical wall with effusion cooling, convection cooling, and impingement cooling, wherein each of the plurality of effusion cooling holes is oriented such that the cooling air flowing therethough strikes an inner portion of the cylindrical wall cooling the inner portion as impingement cooling;
- wherein each of the plurality of effusion cooling holes is oriented at an angle of about 10° to about 30° relative to a tangent line on the cylindrical wall, the tangent line in a plane perpendicular to a centerline of the combustor;
- a scroll assembly coupled to the combustor section and configured to receive the combustion gases;
- and
- a turbine section coupled to the scroll assembly and configured to receive the combustion gases from the scroll assembly and to extract energy from the combustion gases.
3 more elements
Dependencies are inferred from the claim text.