MACHINING PROCESS FOR MULTI-VANE NOZZLE

The present invention relates to a method for machine finishing the shape of a blank casting for a multi-vane, in particular bi-vane, nozzle of a turbine engine, comprising a first vane and a second vane extending substantially in a radial direction between two walls that are radially inner and radi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BARIAUD Christian, LE MERDI Florian, MIHAILA Gabriela, DALON Thibault
Format: Patent
Sprache:eng
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