| 摘要 |
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. |
