COMBUSTOR WITH A FUEL INJECTOR
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United States of America Patent
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Issued Date -
Jun 22, 2023
app pub date -
Feb 22, 2022
filing date -
Dec 21, 2021
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Abstract
A turbine engine having a compressor section, a combustion section and a turbine section in serial flow arrangement. The turbine engine further having a combustor, provided within the combustion section, defining a combustion chamber and having at least one fuel injector. The fuel injector having a fuel channel, a first set of fuel orifices, and a flow restrictor located within the fuel channel and having a second set of fuel orifices.
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