An example hybrid aircraft propulsion system (2B) includes a plurality of electrical busses (4) comprising a propulsion bus (4A), a critical bus (4B), and a non-critical bus (4C); an electrical energy storage system (34B) coupled to each of the plurality of electrical busses (4); one or more power units (6) configured to generate and output electrical energy via the propulsion bus (4A); one or more electrical machines (14A, 14B) configured to drive respective propulsors (16A, 16B) using electrical energy received via the propulsion bus (4A); one or more hotel loads (50) configured to receive energy via the non-critical bus (4C); and one or more critical loads configured to receive energy via the critical bus (4B).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION


    Weitere Titelangaben:

    ELEKTRISCHE ARCHITEKTUR FÜR HYBRIDANTRIEB
    ARCHITECTURE ÉLECTRIQUE POUR PROPULSION HYBRIDE


    Beteiligte:
    LONG STEPHEN (Autor:in)

    Erscheinungsdatum :

    11.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION

    LONG STEPHEN ANDREW | Europäisches Patentamt | 2020

    Freier Zugriff

    Electrical architecture for hybrid propulsion

    LONG STEPHEN ANDREW | Europäisches Patentamt | 2021

    Freier Zugriff

    ELECTRICAL ARCHITECTURE FOR HYBRID PROPULSION

    LONG STEPHEN ANDREW | Europäisches Patentamt | 2020

    Freier Zugriff

    Electrical propulsion system architecture

    PRASAD RASHMI / NAMUDURI CHANDRA S / GOPALAKRISHNAN SURESH et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    ELECTRICAL PROPULSION SYSTEM ARCHITECTURE

    PRASAD RASHMI / NAMUDURI CHANDRA S / GOPALAKRISHNAN SURESH et al. | Europäisches Patentamt | 2021

    Freier Zugriff