ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION
ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION
- Neue Suche nach: LONG STEPHEN ANDREW
- Neue Suche nach: LONG STEPHEN ANDREW
An example hybrid aircraft propulsion system includes a plurality of electrical busses comprising a propulsion bus, a critical bus, and a non-critical bus; an electrical energy storage system coupled to each of the plurality of electrical busses; one or more power units configured to generate and output electrical energy via the propulsion bus; one or more electrical machines configured to drive respective propulsors using electrical energy received via the propulsion bus; one or more hotel loads configured to receive energy via the non-critical bus; and one or more critical loads configured to receive energy via the critical bus.
Dokumentinformationen
ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION
ARCHITECTURE ELECTRIQUE DE PROPULSION HYBRIDE
2020-05-08
Patent
Elektronische Ressource
Englisch