STRUCTURE OF LATE LEAN INJECTION DEVICE

PROBLEM TO BE SOLVED: To provide a gas turbine engine operating with high efficiency. SOLUTION: The gas turbine engine includes a late lean injection compatible combustor 20 having a first interior 21 in which a first fuel supplied thereto by a fuel circuit 70 is combustible, a turbine 50, a transit...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KARIM HASAN, DAVIS LEWIS BERKELY JR, TERRY JASON CHARLES, VENKATARAMAN KRISHNA K, WASHAM ROY MARSHALL
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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