HIGH PRESSURE TURBINE VANE COOLING CONFIGURATION

A turbine vane assembly for a gas turbine engine is disclosed herein. The turbine vane assembly includes a turbine vane including a leading edge, a pressure edge, a suction edge, and a trailing edge, a core defined by the turbine vane, an outer platform end wall connected to the turbine vane, the ou...

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Bibliographische Detailangaben
Hauptverfasser: VALERIO, Domenico, PARENT, Christopher, PRENTER, Robin Michael Patrick, MONGILLO JR., Dominic J, SKIDELSKY, Vladimir, FREDETTE, Jeremy B
Format: Patent
Sprache:eng ; fre
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