CONTROL METHOD OF AIRCRAFT JET TURBINE ENGINE Russian patent published in 2012 - IPC F02C9/00 

FIELD: engines and pumps.

SUBSTANCE: control method of aircraft jet turbine engine involves maintenance of the specified rotor speeds and gas temperature after turbine by means of engine rotor speed controls and gas temperature after axial turbine depending on air temperature at engine inlet; engine warm-up time is pre-determined in it; at the aircraft takeoff without engine pre-warming, when engine throttle lever is set to position of maximum or afterburning modes, there instantaneously changed is setting of engine rotor speed controls for higher values for the time which is less than the engine warm-up time.

EFFECT: method allows increasing the aircraft thrust instantaneously for the time which is not less than travel time of aircraft along aircraft carrier deck.