The present invention relates to a thermal management system (10) for a hybrid electric aircraft (100), wherein the system comprises: at least one aircraft unit (12) configured to be used in electric propulsion of the aircraft; a first fluid circuit (18) arranged to cool the at least one aircraft unit; an internal combustion engine (28); a second fluid circuit (30) for the internal combustion engine; and a heat exchanger (20), wherein the first fluid circuit is arranged to provide heating to the second fluid circuit via said heat exchanger.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AEROSPACE THERMAL MANAGEMENT SYSTEM


    Beteiligte:
    FRANSSON JOEL (Autor:in) / MARTINS FRANCISCO (Autor:in) / CARLSON NILS (Autor:in) / DÕNMEZ ENIS (Autor:in)

    Erscheinungsdatum :

    31.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AEROSPACE THERMAL MANAGEMENT SYSTEM

    FRANSSON JOEL / MARTINS FRANCISCO / CARLSON NILS et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    AEROSPACE ELECTRIC PROPULSION THERMAL MANAGEMENT SYSTEM

    CARLSON NILS / CUENCA ALAIN / HELLSING JOHAN et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    AEROSPACE ELECTRIC PROPULSION THERMAL MANAGEMENT SYSTEM

    CARLSON NILS / CUENCA ALAIN / HELLSING JOHAN et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    STRUCTURALLY INTEGRATED THERMAL MANAGEMENT SYSTEM FOR AEROSPACE VEHICLES

    DAVID E BLANDING / ARUN MULEY / JEFFREY C COFFMAN et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Structurally integrated thermal management system for aerospace vehicles

    BLANDING DAVID E / MULEY ARUN / COFFMAN JEFFREY C et al. | Europäisches Patentamt | 2018

    Freier Zugriff