An aircraft that includes a fuselage and wings fixed to the fuselage. The aircraft further includes a shaftless electric fluid-flow device that is coupled to the at least one of the fuselage or a corresponding one of the wings. The shaftless electric fluid-flow device includes a housing and a shaftless hub, which is rotatable within the housing, about a central axis, and defines an open central channel that is open along the central axis. The shaftless electric fluid-flow device also includes a fan blade assembly that is coupled to the shaftless hub, such that the fan blade assembly co-rotates with the shaftless hub. The fan blade assembly includes a plurality of fan blades.


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    Title :

    SHAFTLESS ELECTRIC FLUID-FLOW DEVICE


    Contributors:

    Publication date :

    2024-01-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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