A method and system (200) for operating a hybrid electric aircraft propulsion system. The method comprises modulating AC electric power applied to a first electric propulsor (206A) or a second electric propulsor (206B) from at least one motor inverter (208A,208B;308) to synchronize the frequency of the first electric propulsor (206A) or the second electric propulsor (206B) with the frequency of a generator (202).
OPERATION OF A HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM
BETRIEB EINES HYBRIDEN ELEKTRISCHEN FLUGZEUGANTRIEBSSYSTEMS
FONCTIONNEMENT D'UN SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE D'AÉRONEF
27.10.2021
Patent
Elektronische Ressource
Englisch
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