A method includes controlling an electric motor (104) of a hybrid-electric powerplant (106) for an aircraft using an EPC (electric powertrain controller) (120) and controlling a heat engine (102) of the hybrid-electric powerplant using an ECU (engine control unit) (114). The method includes protecting the hybrid-electric powerplant using the ECU to power down the electric motor, and/or using the EPC to power down the heat engine.


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    Title :

    PROTECTION FUNCTIONS


    Additional title:

    SCHUTZFUNKTIONEN
    FONCTIONS DE PROTECTION


    Contributors:

    Publication date :

    2024-01-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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