Aircraft electric machines are described. The aircraft electric machines include a laminated rotor operably connected to a shaft, the laminated rotor comprising a plurality of rotor teeth and air gaps defined between adjacent rotor teeth about a circumference of the laminated rotor, a modular stator assembly comprising at least one stator segment having a winding wrapped about a center body of the at least one stator segment, a cooling element arranged at least one of adjacent to or within the winding, and at least one power module system comprising an active rectifier and wherein the laminated rotor and modular stator are arranged as a switched reluctance rotor-stator assembly.


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    Titel :

    SWITCHED RELUCTANCE ELECTRIC MACHINE


    Beteiligte:
    TANGUDU JAGADEESH K (Autor:in) / KOENIG ANDREAS C (Autor:in) / DWARI SUMAN (Autor:in) / SPIERLING TODD A (Autor:in)

    Erscheinungsdatum :

    06.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    SWITCHED RELUCTANCE MOTOR AND ELECTRIC CART

    UEDA HATSUHISA | Europäisches Patentamt | 2017

    Freier Zugriff

    Switched reluctance drives for electric vehicles

    Gao, Chao / Zhang, Zhixue | Tema Archiv | 2010



    A Novel Unidirectional Switched Reluctance Machine

    Cathey, J. J. / Bhuiya, R. R. / Chickamenahalli, S. A. | SAE Technical Papers | 1993


    Switched Reluctance Drive for Electric Light Evs

    Ilinski, N. F. / Bitchkov, M. G. / Japan Electric Vehicle Association et al. | British Library Conference Proceedings | 1999