A system for supplying pressurised air installed in an aircraft turbine engine, configured to supply pressurisation air to a portion of the aircraft for using compressed air from pressurisation air collected from a portion for collecting compressed air, characterised in that it comprises a collection port formed on a casing of the compressed air collection portion, a collection member coupled to the collection port, a through port of the collection member formed on a casing of a compartment of the turbine engine, said casing being subjected to small movements relative to the casing of the compressed air portion, the collection member crossing the through port with a freedom of movement relative to the latter during said small movements, a high-pressure space crossed by the collection member, located between the casing of the compressed air collection portion and the casing of the compartment.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEM FOR SUPPLYING PRESSURISED AIR INSTALLED IN AN AIRCRAFT TURBINE ENGINE INCLUDING SEALING MEANS


    Beteiligte:

    Erscheinungsdatum :

    2017-07-20


    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




    Pressurised void aircraft

    ROBERT WILLIAM CHIDSEY | Europäisches Patentamt | 2023

    Freier Zugriff

    Pressurised void aircraft

    Europäisches Patentamt | 2022

    Freier Zugriff

    System and method for controlling a gas turbine engine supplying power to an aircraft

    CHEN BRYAN / CHMIEL DARIUSZ / BEAUCHESNE-MARTEL PHILLIPPE et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Pitch change system equipped with means for supplying fluid to a control means and corresponding turbine engine

    TAJAN SÉBASTIEN EMILE PHILIPPE / FABRE ADRIEN JACQUES PHILIPPE / FORESTO PAUL ANTOINE et al. | Europäisches Patentamt | 2020

    Freier Zugriff