Turbine nozzle with purge cavity blend

A turbine nozzle for a gas turbine engine includes a nozzle segment having an airfoil-shaped vane with a root, a tip, a leading edge, a trailing edge and opposed curved pressure and suction sides. An arcuate inner band segment is attached to the root of the vane. The inner band segment includes an i...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KLASING KEVIN SAMUEL, CARSON SCOTT MICHAEL
Format: Patent
Sprache:eng
Schlagworte:
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