The present invention generally relates to a Halbach tugging system for aircraft comprises a step-down transformer coupled for stepping down AC power received from an auxiliary power unit to required voltage; an electronic speed controller for controlling amount of voltage to be fed into stator winding; and a Halbach array arrangement mechanically coupled to a rotor configured to rotate the rotor thereby providing required torque for tugging the aircraft at a lower RPM. (I_____


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    Title :

    A HALBACH TUGGING SYSTEM FOR AIRCRAFT


    Contributors:

    Publication date :

    2021-11-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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