A device for de-icing a splitter nose of an aviation turbine engine, the device including a splitter nose having an outer annular wall defining the inside of the bypass stream flow channel and an inner annular wall defining an inlet of the core stream flow channel, and an inner shroud mounted at its upstream end on the inner annular wall of the splitter nose and designed to have inlet guide vanes fastened thereto, the splitter nose and the inner shroud defining an annular volume. The device includes an annular deflector positioned inside the annular volume so as to subdivide the annular volume into a first annular cavity and a second annular cavity, the second annular cavity being defined between the annular deflector and the outer annular wall of the splitter nose.


    Access

    Download


    Export, share and cite



    Title :

    DEVICE FOR DE-ICING A SPLITTER NOSE OF AN AVIATION TURBINE ENGINE



    Publication date :

    2017-11-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    Device for de-icing a splitter nose of an aviation turbine engine

    LOURIT DAMIEN DANIEL SYLVAIN / MARLIN FRANÇOIS MARIE PAUL | European Patent Office | 2019

    Free access

    A device for de-icing a splitter nose of an aviation turbine engine

    DAMIEN DANIEL SYLVAIN LOURIT / FRANCOIS MARLIN | European Patent Office | 2018

    Free access

    Splitter nose with plasma de-icing for axial turbine engine compressor

    HERBAUT GHISLAIN / BOUILLON DAVID | European Patent Office | 2019

    Free access

    De-icing device for a splitter nose of an axial turbine engine compressor

    OGGERO QUENTIN | European Patent Office | 2018

    Free access

    Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine

    SCHOLTES CHRISTOPHE / BRUNET ANTOINE ROBERT ALAIN / AMOEDO SIMON JOSE PIERRE | European Patent Office | 2020

    Free access