Durable turbine vane

A durable nozzle vane includes a leading edge where hot combustion gas impinges on the vane, a pressure side extending from the leading edge to a trailing edge and a suction side extending from the leading edge to the trailing edge, a blunt region along the suction side between the leading edge and...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Demers Daniel Edward, Molleson Sean Michael, Bubnick Joseph Steven, Heffron Todd Stephen, Frederick Robert Alan, Bartz Robert Joseph
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A durable nozzle vane includes a leading edge where hot combustion gas impinges on the vane, a pressure side extending from the leading edge to a trailing edge and a suction side extending from the leading edge to the trailing edge, a blunt region along the suction side between the leading edge and a high curvature region, the blunt region having small curvature in the length between the leading edge and the high curvature region allowing for at least two rows of cooling apertures.