Gas turbine nozzle segment and process therefor

A gas turbine engine nozzle segment and process for producing such a nozzle segment to exhibit improved durability and aerodynamic performance. The process produces a nozzle segment having at least one vane between and interconnecting a pair of platforms. The nozzle segment is cast from a gamma prim...

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Bibliographische Detailangaben

Hauptverfasser:	Farmer, Andrew David, Nagaraj, Bangalore Aswatha, Lu, Wenfeng, Lee, Ching-Pang, Guentert, Joseph Michael
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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