An example hybrid aircraft propulsion system (2) includes a plurality of power units (6A-6N) configured to output electrical energy onto one or more electrical busses (4); one or more propulsors (16); and one or more electrical machines (14), each respective electrical machine configured to drive a respective propulsor of the one or more propulsors (16) using electrical energy received from at least one of the one or more electrical busses (4).
HYBRID PROPULSION SYSTEMS
HYBRIDANTRIEBSSYSTEM
SYSTÈMES DE PROPULSION HYBRIDE
2022-06-29
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |