Fuel injectors for gas turbine engines
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United States of America Patent
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Sep 19, 2017
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app pub date -
Jan 30, 2015
filing date -
Jan 30, 2015
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Abstract
A fuel injector for a gas turbine engine includes a monolithic nozzle body that defines within its interior one or more fuel circuits. Each fuel circuit includes an inlet, an outlet orifice, a main passage fluidly coupling the inlet with the outlet orifice, and a branch passage connected to the main passage. The branch passage connects to the main passage downstream of the inlet and upstream of the outlet orifice to form an effective metering flow area that is smaller than the flow area of the outlet orifice.
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