Cooled turbine engine components

A combustor heat shield panel (74) has interior (102) and exterior (100) surfaces with a number of circuitous non-interconnected cooling gas passageways having inlets (116) on the exterior surface (100) and outlets (118) on the interior surface (102).

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Bibliographische Detailangaben
Hauptverfasser:	NAPOLI, NIKOLAOS, SEGALMAN, IRVING, CHEUNG, ALBERT K
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A combustor heat shield panel (74) has interior (102) and exterior (100) surfaces with a number of circuitous non-interconnected cooling gas passageways having inlets (116) on the exterior surface (100) and outlets (118) on the interior surface (102).