Methods and systems for operating a hybrid electric aircraft propulsion system mounted to an aircraft. The method comprises driving a first rotating propulsor from a first electric motor operatively connected to a generator, driving a second rotating propulsor from a second electric motor operatively connected to the generator, and driving a third rotating propulsor from a thermal engine, the thermal engine operatively connected to the generator and configured to drive the generator.
HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION
SYSTEME DE PROPULSION HYBRIDE ELECTRIQUE ET SA METHODE DE FONCTIONNEMENT
2020-03-06
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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