Gas turbine combustion system cooling arrangement

Cooling is provided for a gas turbine combustion system (10) that includes a first member (13), such as a liner, having exterior (26) and interior (28) surfaces that define a wall (30) therebetween and a central area. A second member (40), such as a cap, is located adjacent that interior surface (28...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Berkman, Mert, Chillar, David, Byrne, William
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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