Gas turbine nozzle with a flow fence

The present application provides a turbine nozzle airfoil with a leading edge and a trailing edge and a flow fence extending from the leading edge to the trailing edge.

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Bibliographische Detailangaben
1. Verfasser: BIELEK CRAIG ALLE
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The present application provides a turbine nozzle airfoil with a leading edge and a trailing edge and a flow fence extending from the leading edge to the trailing edge.