Cooling aft end of a combustion liner

A liner ( 18 ) installed in a transition region ( 16 ) between a combustion section ( 12 ) of a gas turbine engine ( 10 ) and an air discharge section ( 14 ) of the turbine. The liner has an air inlet ( 26 ) for admitting air into the liner, and an air outlet ( 28 ) by which air is discharged from t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	FARRELL THOMAS R, INTILE JOHN C
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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