A system includes a low pressure machine (206), a high pressure machine (202), a motor controller device, a first set of switches configured to selectively couple the low pressure machine (206) to an inverter or a rectifier included in the motor controller device, based on a control signal, and a second set of switches configured to selectively couple the high pressure machine (202) to the inverter or the rectifier, based on the control signal.


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    Title :

    MULTIPLEXED BI DIRECTIONAL CONVERTERS FOR HYBRID ELECTRIC AIRCRAFT PROPULSION


    Additional title:

    MULTIPLEXIERTE BIDIREKTIONALE WANDLER FÜR HYBRIDEN ELEKTRISCHEN FLUGZEUGANTRIEB
    CONVERTISSEURS BIDIRECTIONNELS MULTIPLEXÉS POUR PROPULSION ÉLECTRIQUE HYBRIDE D'AÉRONEF


    Contributors:

    Publication date :

    2025-05-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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