An aircraft propulsion system is disclosed that includes at least one hybrid-electric powerplant for delivering power to an air mover for propelling the aircraft, wherein the at least one hybrid-electric powerplant includes a heat engine and an electric motor arranged in a parallel drive configuration or an in-line drive configuration.
DISTRIBUTED PROPULSION CONFIGURATIONS FOR AIRCRAFT HAVING MIXED DRIVE SYSTEMS
03.09.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Distributed propulsion configurations for aircraft having mixed drive systems
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