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_____
A HALBACH TUGGING SYSTEM FOR AIRCRAFT
18.11.2021
Patent
Elektronische Ressource
Englisch
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