ENGINE COMPONENT

PROBLEM TO BE SOLVED: To provide a turbine component having film holes with improved cooling.SOLUTION: An engine component for a gas turbine engine includes a film-cooled substrate having a hot surface facing a hot combustion gas and a cooling surface facing a cooling fluid flow. The substrate inclu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BUNKER RONALD SCOTT, ROBERT DAVID BRIGGS, FREDERICK ALAN BUCK, KEVIN ROBERT FELDMANN, BRAINCH GULCHARAN SINGH
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS 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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