Aircraft air cycle machines include a housing (302), a shaft (304) arranged within the housing, and a first wheel assembly (606) operably coupled to the shaft and arranged within the housing. The first wheel assembly is configured to rotationally drive the shaft. A second wheel assembly (608) is operably coupled to the shaft and configured to be rotationally driven by the shaft. A magnetic assembly (618) is arranged within the housing and along the shaft. The magnetic assembly includes a stator assembly (622) fixedly connected to the housing and a rotor assembly (620) rotationally coupled to the shaft. The magnetic assembly is arranged along the shaft to provide a gear ratio between the first wheel assembly and the second wheel assembly.


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    Titel :

    GEARED AIR CYCLE MACHINE FAN FOR AIRCRAFT SYSTEMS


    Weitere Titelangaben:

    GEBLÄSE EINER LUFTKREISLAUFMASCHINE MIT GETRIEBE FÜR LUFTFAHRZEUGSYSTEME
    VENTILATEUR DE MACHINE À CYCLE D'AIR À ENGRENAGES POUR SYSTÈMES D'AÉRONEF


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

    Erscheinungsdatum :

    21.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / F16C SHAFTS , Wellen / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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