The invention relates to a fluid duct system for thermal management and/or ventilation in a compartment containing at least one temperature sensitive target within a turbo engine, said turbo engine comprising a first spatial area within the turbo engine through which a fluid flows during operation of the turbo engine, characterized by a fluid duct device (3) connecting the first spatial area (1) with a second spatial area (2) having a lower pressure than the first spatial area (1) during operation of the turbo engine (7), so that a pressure gradient is present in the fluid duct device (3) and a flow of fluid from the first spatial area (1) towards the second spatial area (2) is generated resulting in a pressure gradient in the compartment (11) and therefore in a flow of fluid for thermal management and/or ventilation of the compartment (11).


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    Titel :

    TURBO ENGINE WITH A FLUID DUCT SYSTEM


    Weitere Titelangaben:

    TURBOMASCHINE MIT EINEM FLUIDLEITUNGSSYSTEM
    TURBOMACHINE ÉQUIPÉE D'UN SYSTÈME DE CONDUIT DE FLUIDE



    Erscheinungsdatum :

    07.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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