TURBINE NOZZLE TRIPLET WITH DIFFERENTIAL VANE COOLING

A turbine nozzle (20) includes a mid vane (24) mounted between a pair of end vanes (26) in outer and inner bands (28,30). The mid vane (24) includes a first pattern of film cooling holes (56,58,60) configured to discharge more cooling air than each of the two end vanes having respective second patte...

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Hauptverfasser: KULYK, MICHAEL PETER, FLODMAN, DAVID ALLEN, SHAPIRO, JASON DAVID
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creator KULYK, MICHAEL PETER
FLODMAN, DAVID ALLEN
SHAPIRO, JASON DAVID
description A turbine nozzle (20) includes a mid vane (24) mounted between a pair of end vanes (26) in outer and inner bands (28,30). The mid vane (24) includes a first pattern of film cooling holes (56,58,60) configured to discharge more cooling air than each of the two end vanes having respective second patterns of film cooling holes (56,58).
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subjects 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
title TURBINE NOZZLE TRIPLET WITH DIFFERENTIAL VANE COOLING
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