A hybrid electric aircraft powerplant arrangement (100) includes a first wing pair (101a) of powerplants for a first wing (201) of an aircraft (200), the first wing pair (101a) comprising a first electric powerplant (103a) configured to drive a first air mover (105a) and a first heat engine powerplant (107a) configured to drive a second air mover (105b) separate from the first air mover (105a). The arrangement (100) can include a second wing pair of powerplants (101b) for a second wing (203) of the aircraft (200), the second wing pair (101b) comprising a second electric powerplant (103b) configured to drive a third air mover (105c) separate from the first and second air movers (105a, 105b), and a second heat engine powerplant (107b) configured to drive a fourth air mover (105d) separate from the first, second, and third air movers (105a, 105b, 105c).
HYBRID ELECTRIC AIRCRAFT AND POWERPLANT ARRANGEMENTS
ELEKTRISCHES HYBRIDFLUGZEUG UND TRIEBWERKSANORDNUNGEN
AÉRONEF HYBRIDE ÉLECTRIQUE ET AGENCEMENTS D'INSTALLATION MOTRICE
2021-03-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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