Helicopter main rotor powering procedure during one engine inoperative simulation

摘要

the present invention is directed to a process of training in rotation of a rotor of a rotorcraft main implementing a simulation mode in the flight of a failure of one of the engines of the aircraft.in simulation mode, and in the case where a current rotational speed of the main rotor (nr) is detected as less than a threshold value (s) to a predetermined rotational speed.the simulation mode is maintained, and an active control is generated to cause a gradual increase in (a) controlled the power provided by the engine by providing a crossing the limit imposed by a locker (ied / 2) for control of the operation the engine simulation mode.