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).


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    Titel :

    HYBRID ELECTRIC AIRCRAFT AND POWERPLANT ARRANGEMENTS


    Weitere Titelangaben:

    ELEKTRISCHES HYBRIDFLUGZEUG UND TRIEBWERKSANORDNUNGEN
    AÉRONEF HYBRIDE ÉLECTRIQUE ET AGENCEMENTS D'INSTALLATION MOTRICE


    Beteiligte:
    SPIERLING TODD A (Autor:in) / THOMASSIN JEAN (Autor:in)

    Erscheinungsdatum :

    2021-03-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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