TURBINE ENGINE HAVING ACOUSTICALLY TUNED FUEL NOZZLE

A fuel nozzle (26) for a turbine engine (10) having a combustion chamber (28) is disclosed. The fuel nozzle has a common axis (42), a body member (36), and a barrel member (34). The fuel nozzle also has a mixing duct (37) and an air inlet duct (35), each with predetermined lengths. The fuel nozzle a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BLUST, JAMES, W, CRAMB, DONALD, J, ABREU, MARIO, E, TWARDOCHLEB, CHRISTOPHER, Z, ROGERS, THOMAS, J.C
Format:	Patent
Sprache:	eng ; fre
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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