COMBUSTOR FUEL NOZZLE ASSEMBLY
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United States of America Patent
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Issued Date -
Aug 22, 2024
app pub date -
Aug 21, 2023
filing date -
Jan 14, 2022
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Abstract
A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.
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