A hybrid propulsion system for propelling an aircraft (100) comprises a first propulsion system (11) based on fuel cells and a second propulsion (12) system based on one or more combustion engines (15, 16). The first propulsion system (11) is fully providing a base thrust (A). The second propulsion system (12) is providing a peak thrust (B) needed for take-off of the aircraft (100) and/or is assisting the first propulsion system (11) in propelling the aircraft (100) when the peak thrust (B) is needed or in failure conditions.


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    Title :

    HYBRID PROPULSION SYSTEM FOR PROPELLING AN AIRCRAFT, METHOD OF OPERATING SAME, AND HYBRID AIRCRAFT


    Additional title:

    HYBRIDANTRIEBSSYSTEM ZUM ANTREIBEN EINES FLUGZEUGES, VERFAHREN ZU DESSEN BETRIEB UND HYBRIDFAHRZEUG
    SYSTÈME DE PROPULSION HYBRIDE POUR PROPULSER UN AÉRONEF, SON PROCÉDÉ DE FONCTIONNEMENT ET AÉRONEF HYBRIDE



    Publication date :

    2023-05-03


    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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