ELECTRIC PROPULSION SYSTEM

An electric propulsion system (16) for an aircraft (10) comprises a plurality of propulsion modules (16). Each propulsion module (16) comprises a motor (22), an energy store (30) configured to supply electrical energy to the motor (22), and a controller (50) configured to control the motor (22) and...

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Bibliographische Detailangaben
Hauptverfasser:	BALACHANDRAN, Ajith, MENON, Kalyani Govindankutty
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	An electric propulsion system (16) for an aircraft (10) comprises a plurality of propulsion modules (16). Each propulsion module (16) comprises a motor (22), an energy store (30) configured to supply electrical energy to the motor (22), and a controller (50) configured to control the motor (22) and the energy store (30). Each propulsion module (16) is configured such that the motor (22) of the propulsion module (16) receives electrical energy only from the energy store (30) of the propulsion module (16).