Methods and systems for operating a hybrid electric aircraft propulsion system (200) mounted to an aircraft. The method comprises driving a first rotating propulsor (206A) from a first electric motor (204A) operatively connected to a generator (202), driving a second rotating propulsor (206B) from a second electric motor (204B) operatively connected to the generator (202), and driving a third rotating propulsor (206C) from a thermal engine (201), the thermal engine (201) operatively connected to the generator (202) and configured to drive the generator (202).
HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION
HYBRIDES ELEKTRISCHES ANTRIEBSSYSTEM UND VERFAHREN ZUM BETRIEB
SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE ET PROCÉDÉ DE FONCTIONNEMENT
2022-12-28
Patent
Electronic Resource
English
Hybrid electric propulsion system and method of operation
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