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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    29.06.2017


    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 / F02K JET-PROPULSION PLANTS , Strahltriebwerke






    ENGINE COMPARTMENT VENTILATION STRUCTURE

    MAEDA AKIHIRO / KAWAGUCHI TAKEFUMI / YASUDA TAKASHI | Europäisches Patentamt | 2016

    Freier Zugriff

    Ventilation structure for engine compartment

    TSUTSUMI KATSUHIRO / MIYAMOTO HIROFUMI | Europäisches Patentamt | 2016

    Freier Zugriff