Propulsion system for an aircraft

A propulsion system for an aircraft can include an electric power source and an electric propulsion assembly having an electric motor and a propulsor. The propulsor can be powered by the electric motor. An electric power bus can electrically connect the electric power source to the electric propulsi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Crabtree, Glenn David, Vondrell, Randy M, Bouvette, Anthony Austin
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A propulsion system for an aircraft can include an electric power source and an electric propulsion assembly having an electric motor and a propulsor. The propulsor can be powered by the electric motor. An electric power bus can electrically connect the electric power source to the electric propulsion assembly. The electric power source can be configured to provide electrical power to the electric power bus. An inverter converter controller can be positioned along the electric power bus and can be electrically connected to the electric power source at a location downstream of the electric power source and upstream of the electric propulsion assembly.