FIELD: gas turbine engines.
SUBSTANCE: method for controlling the temperature of the exhaust gases of gas turbine engine (1), including the following steps: regulation of fuel injection into combustion chamber (5) of gas turbine engine (1) to create a target thrust by gas turbine engine (1); regulation of supply of mechanical power from electric motor (10) to shaft (8, 9) driven by turbine (6, 7), while electric motor (10) is activated when the gap between casing (62) and blades (61) of turbine (6, 7) exceeds the threshold value. In addition, a gas turbine engine and an aircraft are also presented.
EFFECT: reduction or even elimination of the temperature peak of the gas turbine engine exhaust gases during the first take-off of an aircraft.
12 cl, 2 dwg
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