An aircraft propulsion module (1) comprises a hydrogen storage system (11), an electrochemical converter (7) connected to the hydrogen storage system, wherein the at least one electrochemical converter is adapted to convert hydrogen supplied from the hydrogen storage system into electric energy, and an electric motor (5) electrically connected to the electrochemical converter, wherein the electric motor is adapted to generate thrust; wherein the propulsion module comprises at least one separation means adapted to separate at least one component of the propulsion module from the propulsion module. An aircraft (3) comprises at least one aircraft propulsion module. A method for operating a propulsion module comprises that: during operation of the propulsion module, at least one separation means (22) is actuated, by which actuation at least one component (8) of the propulsion module is separated from the remaining propulsion module (12) and then falls from the remaining propulsion module.


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    Titel :

    AIRCRAFT PROPULSION MODULE AND AIRCRAFT


    Weitere Titelangaben:

    FLUGZEUGANTRIEBSMODUL UND FLUGZEUG
    MODULE DE PROPULSION D'AÉRONEF ET AÉRONEF


    Beteiligte:
    VINCEKOVIC DAVID (Autor:in) / PASQUIET FLORIAN (Autor:in) / SAVIN OLIVIER (Autor:in)

    Erscheinungsdatum :

    2023-11-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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