Aircraft electric motor system

AIRCRAFT ELECTRIC MOTOR SYSTEM A method and apparatus for controlling an electric aircraft is presented. An apparatus comprises a controller (400). The controller is configured to identify a state for an electric aircraft (200). The controller is further configured to identify a group of recharging...

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Bibliographische Detailangaben
Hauptverfasser: Quadracci, Leonard J, Cameron, Douglas C, Benson, Christopher Pete
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:AIRCRAFT ELECTRIC MOTOR SYSTEM A method and apparatus for controlling an electric aircraft is presented. An apparatus comprises a controller (400). The controller is configured to identify a state for an electric aircraft (200). The controller is further configured to identify a group of recharging parameters for a group of electric motors (412-418) in an electric propulsion system. The electric propulsion system is configured to move the electric aircraft based on the state for the group of electric motors for the electric aircraft. The controller is still further configured to recharge a power source (402) for the electric aircraft using the group of recharging parameters (420-425) to control recharging of the power source with the group of electric motors when a recharge state (410) is present for the electric aircraft. 'P. CN ~ -. \/ "/ V- ~