A splitter nose of an axial turbomachine, in particular a compressor, has: an annular casing, and an annular conduit for deicing a separation edge of the splitter nose. The conduit is connected to the casing only in a first zone in the region of a hot air inlet and in a second zone located in a position diametrically opposite the inlet, or forming relative to the axis of the turbomachine an angle (a) less than 30° with respect to the position so as to allow expansion deformations of the conduit. The splitter nose can be used in a compressor and a turbomachine.


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    Titel :

    SPLITTER NOSE OF A LOW-PRESSURE COMPRESSOR OF AN AXIAL TURBOMACHINE WITH ANNULAR DEICING CONDUIT


    Weitere Titelangaben:

    NEZ DE SEPARATEUR D'UN COMPRESSEUR BASSE PRESSION D'UNE TURBOMACHINE AXIALE DOTE D'UN CONDUIT DE DEGIVRAGE TUBULAIRE


    Beteiligte:

    Erscheinungsdatum :

    17.01.2017


    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



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