A HALBACH TUGGING SYSTEM FOR AIRCRAFT

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 wind...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Kumar, G. Dinesh, Gowrishankar, D, N., Niteesh, Chidvilas, N. V, Neeraj, Venkata, Sritha, K, Krishnamoorthy, Vishwajeeth, Suraj, V
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	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_____