ELECTRIC AIRCRAFT PROPULSION ASSEMBLY AND METHOD

The disclosure relates to an electric aircraft propulsion assembly (300) comprising: an electric storage unit (302); a first electric motor (303) connected to power a first propulsor (305); a first converter (307) configured as a DC:AC converter having input connections connectable to the electric s...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Trainer, David, Chivite Zabalza, Francisco Javier, Chong, Ellis
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The disclosure relates to an electric aircraft propulsion assembly (300) comprising: an electric storage unit (302); a first electric motor (303) connected to power a first propulsor (305); a first converter (307) configured as a DC:AC converter having input connections connectable to the electric storage unit (302) and output connections connected across the first electric motor (303), the first converter (307) configured as a DC:AC converter; a second electric motor (304) connected to power a second propulsor (306); a second converter (308) connected between the first converter input connections and the second electric motor (304); and a controller (309) configured to control operation of the first and second converters (307, 308), wherein the second converter (308) is operable as a DC:AC converter to convert the DC supply from the electric storage unit (302) to an AC supply across the second electric motor (304) and as a DC: DC converter to convert the DC supply from the electric storage unit (302) at a first DC level to a DC supply at the input connections of the first converter (307) at a second DC level.