An electrical power system for regenerative loads may include a DC bus and an electrical actuator load, where back-driving the electrical actuator load generates regenerative electrical energy, and where the electrical actuator load is configured to transmit the regenerative electrical energy to the DC bus. The system may also include at least one additional load, where at least a portion of the regenerative electrical energy is transmitted to the at least one additional load.


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    Title :

    Power system architecture for aircraft with electrical actuation


    Contributors:

    Publication date :

    2020-09-22


    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 / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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    EUGENE V SOLODOVNIK / THOMAS F CURRIER / MARK E LIFFRING et al. | European Patent Office | 2019

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    POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION

    SOLODOVNIK EUGENE V / CURRIER THOMAS F / LIFFRING MARK E et al. | European Patent Office | 2020

    Free access

    POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION

    SOLODOVNIK EUGENE V / CURRIER THOMAS F / LIFFRING MARK E et al. | European Patent Office | 2019

    Free access

    POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION

    EUGENE V SOLODOVNIK / THOMAS F CURRIER / MARK E LIFFRING et al. | European Patent Office | 2019

    Free access