An assembly for use in an aircraft includes a housing (40) having an inlet and an outlet and a flow path for an airflow extends between the inlet and the outlet. The assembly additionally includes a rotatable portion (85) including a rotor mounted within the housing (40) between the inlet and the outlet along the flow path. The rotor has a body including a first side facing the inlet, a second opposite side, and a plurality of impeller blades protruding from the first side. An axial flux electric motor (26) includes a motor rotor having at least one first flux element and a motor stator. The at least one first flux element is integrated into the rotatable portion (85) and the motor stator is remote from the flow path.


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    Titel :

    ROTOR INTEGRATED AXIAL FLUX ELECTRIC MOTOR


    Weitere Titelangaben:

    ROTORINTEGRIERTER AXIALFLUSSELEKTROMOTOR
    MOTEUR ÉLECTRIQUE À FLUX AXIAL INTÉGRÉ AU ROTOR


    Beteiligte:
    KILCHYK VIKTOR (Autor:in) / MERRITT BRENT J (Autor:in)

    Erscheinungsdatum :

    2024-02-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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