Safran Aero Boosters Sa

Techspace Aero S.a.

Benoît Baldewijns

Ghislain Herbaut

Enrique Penalver Castro

The present application relates to a splitter nose of an axial turbomachine configured to separate an annular flow into the turbomachine into a primary flow and a secondary flow, and including: a generally circular leading edge, an annular wall extending from the leading edge and bounding the secondary flow, and at least one duct for a de-icing fluid for the splitter nose extending substantially axially along the wall and opening out into the primary flow. The external surface of the wall is formed by a sheet bounding the de-icing duct.

Splitter nose with a sheet that forms a surface to guide the flow and acts as a de-icing duct

The present invention relates to a method for manufacturing a turbomachine rectifier comprising an outer ring () and a plurality of stator vanes (), said vanes comprising a platform () and a blade (), wherein said method comprises at least the following steps:

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Hannut, Belgium

Benoît Baldewijns