Gas turbine nozzle with a flow groove

The present invention provides a turbine nozzle airfoil with a leading edge and a trailing edge and a flow groove 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:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The present invention provides a turbine nozzle airfoil with a leading edge and a trailing edge and a flow groove extending from the leading edge to the trailing edge.