PROPULSION SYSTEM FOR AN AIRCRAFT

A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or mo...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GANSLER, Michael Thomas, HON, Robert Charles
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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