Snecma

Hichem Belghagi

Nicolas Potel

Sylvain Clermonte

Laurence Garin

A method of adjusting a setpoint value of at least one parameter that has an influence on thrust of a gas turbine engine propelling an aircraft during a stage of flight of the aircraft, the method including: obtaining a current value of at least one operating variable of the engine; extracting from a pre-established table a decrement value for the at least one parameter associated with the current value of the at least one operating variable of the engine; and adjusting the setpoint value of the at least one parameter by applying thereto the decrement value extracted from the table.

Method and a device for adjusting a setpoint value of a parameter that influences thrust from a gas turbine engine

The method consists, based on an operating parameter of the turbojet engine, in:

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Garges-les-Gonesse, France

Hichem Belghagi