Hybrid electric propulsion system for aircraft and method of operation thereof

A hybrid electric propulsion system for an aircraft includes a gas turbine engine and an electric machine coupled to the gas turbine engine, and a method of operating the hybrid electric propulsion system. A method of operating the propulsion system includes determining, by one or more computing dev...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GUTZ DAVID ALLEN, NICHOLAS ADAM WAGNER, DAVID EUGENE BERGSTEN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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