AIRCRAFT TURBINE ENGINE COMPRISING AN ELECTRIC MOTOR COMPRISING A DEVICE FOR CORRECTING A PRECESSION MOVEMENT AND ASSOCIATED METHOD

The invention relates to an aircraft turbine engine including at least a propulsion shaft and an electric motor (1), the rotor (3) of which is rigidly connected to the propulsion shaft, the electric motor (1) comprising at least three power channels (C1-C4), a control device (4) designed to determin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	TAN-KIM, Alexandre Jean-Marie, MONTIN, Frédéric, TRUCO, Romain, REIGNER, Pierre-Alain Jean Philippe
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION
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