A method and system (200) for operating a hybrid electric aircraft propulsion system. The method comprises modulating AC electric power applied to a first electric propulsor (206A) or a second electric propulsor (206B) from at least one motor inverter (208A,208B;308) to synchronize the frequency of the first electric propulsor (206A) or the second electric propulsor (206B) with the frequency of a generator (202).


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    Title :

    OPERATION OF A HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM


    Additional title:

    BETRIEB EINES HYBRIDEN ELEKTRISCHEN FLUGZEUGANTRIEBSSYSTEMS
    FONCTIONNEMENT D'UN SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE D'AÉRONEF


    Contributors:

    Publication date :

    2021-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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