A hybrid electric aircraft powerplant controller (101) for controlling an engine (103) and an electric motor-generator (105) can include an engine recharging module (107). The engine recharging module can be configured to operate the engine to produce a desired output power to a propulsor (109) and to produce additional power to drive the electric motor-generator to produce electrical output from the electric motor-generator to recharge an electrical storage device (117) during at least one power setting and/or flight phase where the electric motor-generator is not driving the propulsor.


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    Title :

    HYBRID ELECTRIC AIRCRAFT ENERGY REGENERATION


    Additional title:

    HYBRIDE ELEKTRISCHE FLUGZEUGENERGIE-RÜCKGEWINNUNG
    RÉGÉNÉRATION D'ÉNERGIE D'AÉRONEF ÉLECTRIQUE HYBRIDE


    Contributors:

    Publication date :

    2021-02-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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