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).
HYBRID ELECTRIC AIRCRAFT AND METHOD OF OPERATION
HYBRIDES ELEKTRISCHES FLUGZEUG UND VERFAHREN ZUM BETRIEB
AVION HYBRIDE ÉLECTRIQUE ET PROCÉDÉ DE FONCTIONNEMENT
2022-07-06
Patent
Electronic Resource
English
HYBRID-ELECTRIC REGIONAL JET AIRCRAFT OPERATION EFFICIENCY
TIBKAT | 2019
|CONSTRUCTION AND OPERATION OF ELECTRIC OR HYBRID AIRCRAFT
European Patent Office | 2022
|Construction and operation of electric or hybrid aircraft
European Patent Office | 2019
|