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.
SPLITTER NOSE OF A LOW-PRESSURE COMPRESSOR OF AN AXIAL TURBOMACHINE WITH ANNULAR DEICING CONDUIT
NEZ DE SEPARATEUR D'UN COMPRESSEUR BASSE PRESSION D'UNE TURBOMACHINE AXIALE DOTE D'UN CONDUIT DE DEGIVRAGE TUBULAIRE
17.01.2017
Patent
Elektronische Ressource
Englisch
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