An aircraft hybrid electrical propulsion (HEP) system includes an electrical system configured to deliver power to a plurality of electrical loads, a propulsion system configured to generate thrust in response to an input power, and an HEP controller in signal communication with the electrical system and the propulsion system. The HEP controller is configured to monitor a load demand of at least one electrical load among the plurality of electrical loads and to actively control the input power to actively control the thrust in response to changes in the load demand.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION


    Beteiligte:
    BAIG ZUBAIR A (Autor:in) / AMARI MARTIN (Autor:in)

    Erscheinungsdatum :

    12.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION

    BAIG ZUBAIR A / AMARI MARTIN | Europäisches Patentamt | 2024

    Freier Zugriff


    Enabling Electric Propulsion for Flight - Hybrid Electric Aircraft Research at AFRC

    Clarke, Sean / Lin, Yohan / Kloesel, Kurt et al. | NTRS | 2014


    OPERATION OF A HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | Europäisches Patentamt | 2021

    Freier Zugriff

    OPERATION OF A HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff