FIELD: mechanical engineering; gas turbine engine automatic fuel feed control. SUBSTANCE: control system has fuel pump connected with bypass inject or and constant-pressure valve and through jet, with constant pressure differential valve whose outlet is connected to nozzle with shutter of electromagnetic converter; system has metering valve whose control space is connected to line which connects jet and constant pressure differential valve, and spring space is connected to injector and, through metering edge of metering valve, to drain line. EFFECT: enhanced control of fuel feed. 2 dwg
