Hybrid electric propulsion systems and methods therefore are provided. More particularly, the present disclosure is directed to control systems for hybrid electric propulsion systems for aerial vehicles that are configured for rapidly and automatically taking action in response to rapid electrical load changes on a torque source, such as an engine. Methods for operating hybrid electric propulsion systems for aerial vehicles are also provided.


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    Title :

    FAULT TOLERANT HYBRID ELECTRIC PROPULSION SYSTEM FOR AN AERIAL VEHICLE


    Additional title:

    FEHLERTOLERANTES HYBRIDES ELEKTRISCHES ANTRIEBSSYSTEM FÜR EIN LUFTFAHRZEUG
    SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE À TOLÉRANCE DE PANNES POUR UN VÉHICULE AÉRIEN


    Contributors:
    HON ROBERT (author) / GEMIN PAUL (author)

    Publication date :

    2024-12-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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