A core compartment ventilation device is provided. The core compartment ventilation device comprises a fireproof sealing member (202) for substantially sealing a core compartment (66) in a nacelle (34) for a gas turbine engine (20) and a chimney (204) configured to be in fluid communication with the fireproof sealing member (202) for conducting hot air from the core compartment (66) to the external atmosphere via the fireproof sealing member (202). A gas turbine engine (20) and nacelle (34) including the core compartment ventilation device are also provided.


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    Titel :

    CORE COMPARTMENT VENTILATION DEVICES FOR NACELLES OF GAS TURBINE ENGINES FOR COOLING A CORE COMPARTMENT OF A GAS TURBINE ENGINE


    Weitere Titelangaben:

    KERNFACHBELÜFTUNGSVORRICHTUNGEN FÜR GONDELN VON GASTURBINENMOTOREN ZUM KÜHLEN EINES KERNFACHS EINES GASTURBINENMOTORS
    DISPOSITIFS DE VENTILATION DU COMPARTIMENT CENTRAL DE NACELLES DE TURBINE À GAZ POUR REFROIDIR LE COMPARTIMENT CENTRAL D'UNE TURBINE À GAZ


    Beteiligte:

    Erscheinungsdatum :

    07.08.2019


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES






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