An aircraft provided with a power plant provided with at least one combustion engine mechanically connected to a drive system, the drive system comprising two electric machines each connected to the combustion engine by a kinematic chain, the two electric machines being electrically connected to at least one electrical power source. The aircraft comprises a management system controlling at least a mechanical power or an engine torque delivered by each of the two electric machines as a function of a current operating mode, the management system being configured, during a superior operating mode, to control the two electric machines in order for the two electric machines to deliver different and non-zero mechanical powers or engine torques.
PROCÉDÉ ET AÉRONEF MUNI D'AU MOINS UN MOTEUR À COMBUSTION ET D'UN SYSTÈME D'ENTRAINEMENT À AU MOINS DEUX MACHINES ÉLECTRIQUES
METHOD AND AIRCRAFT HAVING AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM HAVING AT LEAST TWO ELECTRIC MACHINES
VERFAHREN UND FLUGZEUG MIT MINDESTENS EINEM VERBRENNUNGSMOTOR UND EINEM ANTRIEBSSYSTEM MIT MINDESTENS ZWEI ELEKTRISCHEN MASCHINEN
18.12.2024
Patent
Elektronische Ressource
Französisch
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