ASSEMBLY FOR A TURBINE ENGINE

An assembly for a turbine engine is provided. This turbine engine assembly includes a shell (80) and a heat shield (82) attached to the shell with a cooling cavity (84) between the shell and the heat shield. The heat shield defines a plurality of cooling apertures (104) and an indentation (106) in a...

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Bibliographische Detailangaben
Hauptverfasser:	KOSTKA, Jr., Stanislav, CUNHA, Frank J
Format:	Patent
Sprache:	eng ; fre ; ger
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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Beschreibung
Zusammenfassung:	An assembly for a turbine engine is provided. This turbine engine assembly includes a shell (80) and a heat shield (82) attached to the shell with a cooling cavity (84) between the shell and the heat shield. The heat shield defines a plurality of cooling apertures (104) and an indentation (106) in a side of the heat shield opposite the cooling cavity. The cooling apertures are fluidly coupled with the cooling cavity. An outlet (150) of a first of the cooling apertures is located at an edge of the indentation.