FIELD: engines and pumps.
SUBSTANCE: invention relates to aircraft engine production and can be used in ACS of gas turbine engine with afterburner. In compliance with the proposed invention, additionally mismatch between preset and measured positions of PC flaps is controlled. If said mismatch exceeds preset value defined from the results of engine acceptance tests, fuel flow rate variation in combustion chamber with after burner if limited.
EFFECT: higher quality of ACS operation, hence, higher engine efficiency and reliability.
1 dwg
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