PROPULSION SYSTEM FOR AN AIRCRAFT

PROPULSION SYSTEM FOR AN AIRCRAFT

A propulsion system 50, 350 for an aircraft 10 includes an electric generator 56, 356 mechanically driven by a combustion engine, with the electric generator 56, 356 configured to generate alternating current electrical power. The propulsion system 50, 350 additionally includes a power bus 58, 356 e...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GEMIN, Paul Robert, BARONE, Dominic
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:A propulsion system 50, 350 for an aircraft 10 includes an electric generator 56, 356 mechanically driven by a combustion engine, with the electric generator 56, 356 configured to generate alternating current electrical power. The propulsion system 50, 350 additionally includes a power bus 58, 356 electrically connected to the electric generator 56, 356 and configured to receive and transmit the alternating current electrical power generated by the electric generator 56, 356. Additionally, the propulsion system 50, 350 includes, an electric propulsor assembly comprising an electric motor 360 and a propulsor drivingly connected to the electric motor 360, the electric motor 360 electrically coupled to the power bus 58, 356 for the receiving alternating current electrical power from the power bus 58, 356.