Turbine nozzle with a flow groove

The present invention provides a turbine nozzle airfoil (230) with a leading edge (240) and a trailing edge (250) and a flow groove (300) extending from the leading edge (240) to the trailing edge (250).

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Bibliographische Detailangaben
1. Verfasser:	BIELEK, CRAIG ALLEN
Format:	Patent
Sprache:	eng ; fre ; ger
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 (230) with a leading edge (240) and a trailing edge (250) and a flow groove (300) extending from the leading edge (240) to the trailing edge (250).