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.


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    Title :

    PROCÉDÉ ET AÉRONEF MUNI D'AU MOINS UN MOTEUR À COMBUSTION ET D'UN SYSTÈME D'ENTRAINEMENT À AU MOINS DEUX MACHINES ÉLECTRIQUES


    Additional title:

    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


    Contributors:

    Publication date :

    2024-12-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke