Combustor assembly with moveable interface dilution opening
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United States of America Patent
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Aug 15, 2023
Grant Date -
Jan 5, 2023
app pub date -
Jun 30, 2021
filing date -
Jun 30, 2021
priority date (Note) -
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Abstract
A gas turbine engine and combustor assembly are provided, the combustor assembly including a first liner and a second liner together defining at least in part a combustion chamber, wherein the first liner and the second liner are separated by a gap along the longitudinal direction, and wherein the first liner is forward of the second liner relative to a flow of fluid through the combustion chamber along the longitudinal direction, and wherein the gap is extended along the circumferential direction.
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