Aircraft electric motors are described. The aircraft electric motors include a motor unit having a rotor and a stator, wherein the stator includes a plurality of windings and cooling channels arranged to provide cooling to the plurality of windings, a drive unit configured to drive operation of the motor unit, and a cooling system having at least one directional feature forming a portion of at least one cooling channel, the at least one directional feature configured to prevent backflow of a cooling fluid that passes through the at least one cooling channel.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft electric motor



    Medientyp :

    Patent


    Format :

    Elektronische Ressource



    AIRCRAFT ELECTRIC MOTOR

    TANGUDU JAGADEESH K / COLDWATE JOSEPH K / DU ZHENTAO STEPHEN | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT ELECTRIC MOTOR

    SAVIERS KIMBERLY RAE / ALAHYARI ABBAS A / TANGUDU JAGADEESH KUMAR et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft electric motor

    TANGUDU JAGADEESH KUMAR / ZHANG HUAN / CHAUDHRY ZAFFIR A et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT ELECTRIC MOTOR

    ALAHYARI ABBAS A / TURNEY JOSEPH / TANGUDU JAGADEESH KUMAR et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT ELECTRIC MOTOR

    TANGUDU JAGADEESH KUMAR / ZHANG HUAN / CHAUDHRY ZAFFIR A et al. | Europäisches Patentamt | 2022

    Freier Zugriff