Machining process for a multi-vane nozzle

A method of machine finishing a blank casting of a multi-vane or bi-vane nozzle of turbine engine. The nozzle comprises a first vane 1 and a second vane 2 extending radially between inner ring sector 3 and inner ring sector 4 as shown in figure 1. A duct is defined between vanes 1 and 2 shown in fig...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Thibault Dalon, Gabriela Mihaila, Christian Bariaud, Florian Le Merdi
Format: Patent
Sprache:eng
Schlagworte:
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