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
2017-01-17
Patent
Electronic Resource
English
Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit
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