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).


    Access

    Download


    Export, share and cite



    Title :

    HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION


    Additional title:

    HYBRIDES ELEKTRISCHES ANTRIEBSSYSTEM UND VERFAHREN ZUM BETRIEB
    SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE ET PROCÉDÉ DE FONCTIONNEMENT


    Contributors:

    Publication date :

    2022-10-26


    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



    Hybrid electric propulsion system and method of operation

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2022

    Free access

    Hybrid electric propulsion system and method of operation

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2023

    Free access

    HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2022

    Free access

    HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2020

    Free access

    HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2020

    Free access