Device and a method for regulating a turbine engine, and an aircraft

A regulator device for reducing the risk of a surge phenomenon appearing in a turbine engine, the turbine engine including a gas generator, air extractor communicating with the gas generator and capable of extracting air from the gas generator, and mechanical power take-off means that co-operate mechanically with the gas generator, the turbine engine being controlled by an engine computer;

• wherein the engine computer includes storage that stores a plurality of acceleration regulation relationships, each acceleration regulation relationship corresponding to air extraction performed by the air extractor in an air extraction range, and to mechanical power take-off performed by the mechanical power take-off means in a mechanical power take-off range, the regulator device including first measurement means for measuring current air extraction, and second measurement means for measuring current mechanical power take-off, which first and second means are connected to the engine computer, the engine computer executing stored instructions so as to control acceleration of the turbine engine by implementing the acceleration regulation relationship corresponding to the current air extraction and to the current mechanical power take-off.

A regulator device for reducing the risk of a surge phenomenon appearing in a turbine engine, the turbine engine including a gas generator, an air extractor communicating with the gas generator and capable of extracting air from the gas generator, and a mechanical power take-off device that mechanically co-operates with the gas generator, the turbine engine being controlled by an engine computer, the engine computer including storage that stores a plurality of acceleration regulation relationships, each acceleration regulation relationship corresponding to an air extraction range performed by the air extractor, and to a mechanical power take-off range performed by the mechanical power take-off device, the regulator device including a first measurement device capable of measuring current air extraction, and a second measurement device capable of measuring current mechanical power take-off, the first and second measurement devices being connected to the engine computer, the engine computer executing stored instructions to control acceleration of the turbine engine by implementing the acceleration regulation relationship corresponding to the current air extraction and to the current mechanical power take-off.