FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engines control. Method of aircraft engines synchronization by means of activation logic, intended for checking safety conditions and/or activation for use of synchronization, where activation logic detects deactivated state, readiness and activated states. Method further includes synchronization transition from deactivated state into readiness state, when command for activation is given by aircraft pilot; synchronization transition from readiness state into activated state, when certain safety and/or activation conditions are met and synchronization transition from activated state or readiness state into deactivated state, when command for deactivation is given by pilot or when safety conditions are not met.
EFFECT: reduced risk for engines.
10 cl, 4 dwg
