According to the subject-matter of the present disclosure, there is provided an electrically powered fan engine. The fan engine includes: an energiser chamber between an inlet and an exhaust of the electrically powered fan engine; a first rotor within the energiser chamber, the first rotor including a plurality of blades and being configured to receive a fluid from the inlet and configured to rotate at a first velocity; and a second rotor within the energiser chamber, the second rotor including a plurality of blades and being configured to receive the fluid after passing through the first rotor and configured to rotate at a second velocity. The first velocity is different from the second velocity.


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    Titel :

    Electrically powered fan engine


    Beteiligte:

    Erscheinungsdatum :

    18.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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