FIELD: engines and pumps.
SUBSTANCE: system of a gas turbine engine combustion chamber fuel supply refers to the automatic adjustment of fuel supply to the combustion chamber (CC) of the gas turbine engine (GTE). The system additionally introduced a bypass valve and solenoid. The bypass valve closure member arranged to yield a compound I channel from the output channel header II in the collector, and the bypass valve control chamber is connected to the solenoid valve and through the orifice to the source of constant pressure.
EFFECT: improved combustion chamber works gas turbine engine, increasing fuel consumption range in the COP and the improvement of reliability and system resource.
2 dwg
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Authors
Dates
2017-04-14—Published
2016-06-14—Filed