Dilution Structure for Gas Turbine Engine Combustor
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United States of America
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Issued Date -
Feb 6, 2020
app pub date -
Aug 1, 2018
filing date -
Aug 1, 2018
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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. The liner includes a walled chute disposed at least partially within the opening. The walled chute defines an inner surface at least partially defining a jet destabilizer.
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