ANNULAR COMBUSTOR DILUTION WITH SWIRL VANES FOR LOWER EMISSIONS
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United States of America Patent
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Issued Date -
Mar 30, 2023
app pub date -
Jan 28, 2022
filing date -
Jan 28, 2022
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Abstract
A combustor liner for a combustor of a gas turbine includes an outer liner and an inner liner. The outer liner has an annular outer liner slot dilution opening, with a plurality of outer liner swirl vanes disposed within the annular outer liner slot dilution opening. The inner liner of the combustor liner includes an annular inner liner slot dilution opening, and also includes a plurality of inner liner swirl vanes disposed within the annular inner liner slot dilution opening.
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