GAS TURBINE ENGINE COMBUSTOR WITH A SET OF DILUTION PASSAGES
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United States of America Patent
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Issued Date -
Aug 22, 2024
app pub date -
Apr 5, 2023
filing date -
Feb 20, 2023
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Abstract
A combustor for a gas turbine engine. The combustor having a dome wall, a set of fuel cups, an inner liner, an outer liner, and a set of dilution passages. The dome wall, the inner liner, and the outer liner, together, at least partially defining a combustion chamber. The set of dilution passages terminating in a plurality of dilution holes arranged in a dilution hole arrangement provided in at least one of the inner liner or the outer liner. The dilution hole arrangement having at least a first subset of dilution holes arranged along a first leg and a second subset of dilution holes arranged along a second leg.
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