An example hybrid aircraft propulsion system includes a plurality of power units configured to output electrical energy onto one or more electrical busses; one or more propulsors; and one or more electrical machines, each respective electrical machine configured to drive a respective propulsor of the one or more propulsors using electrical energy received from at least one of the one or more electrical busses.
HYBRID PROPULSION SYSTEMS
SYSTEMES DE PROPULSION HYBRIDE
2020-05-08
Patent
Electronic Resource
English