COMBUSTOR WITH BAFFLE
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United States of America Patent
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Issued Date -
Jun 27, 2024
app pub date -
Mar 6, 2024
filing date -
Jan 12, 2022
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Abstract
A turbine engine and associated methods for a combustor as shown and described. The turbine engine including a combustor with a combustor liner having dilution openings and a geometry that changes along an axial direction. The combustor further having a baffle surrounding a combustor liner defining a combustion chamber of the combustor. A method for controlling nitrogen oxides within the combustor, including injecting compressed air into the annular combustion chamber through any of the dilution openings described herein.
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