METHOD FOR REGULATING THE ACCELERATION OF A TURBOMACHINE

The invention relates to a method for regulating an acceleration of a turbomachine, the turbomachine comprising a combustion chamber, a high-pressure turbine located downstream of the combustion chamber and which drives a high-pressure shaft in rotation, and a low-pressure turbine located downstream...

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Hauptverfasser: CUVILLIER, Romain, Guillaume, CABRERA, Pierre
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Sprache:eng ; fre ; ger
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creator CUVILLIER, Romain, Guillaume
CABRERA, Pierre
description The invention relates to a method for regulating an acceleration of a turbomachine, the turbomachine comprising a combustion chamber, a high-pressure turbine located downstream of the combustion chamber and which drives a high-pressure shaft in rotation, and a low-pressure turbine located downstream of the high-pressure turbine and which drives a low-pressure shaft in rotation, characterized in that the method comprises the following steps:Injecting (100) mechanical power onto the high-pressure shaft until a speed of the high-pressure shaft attains a target value, thenExtracting (200) mechanical power from the high-pressure shaft so as to maintain the speed at the target value.
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language eng ; fre ; ger
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title METHOD FOR REGULATING THE ACCELERATION OF A TURBOMACHINE
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