Gas turbine fuel nozzle having a lip extending from the vanes of a swirler

An engine can utilize a combustor to combust fuel to drive the engine. A fuel nozzle assembly can supply fuel to the combustor for combustion or ignition of the fuel. The fuel nozzle assembly can include a swirler and a fuel nozzle to supply a mixture of fuel and air for combustion. Increasing effic...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Naik, Pradeep, Cooper, Clayton S, Vukanti, Perumallu, Chiranthan, R Narasimha, Patra, Ajoy, Bucaro, Michael T, Pachaiappan, Dharmaraj, Giridharan, Manampathy G, Vise, Steven C, Benjamin, Michael A
Format:	Patent
Sprache:	eng
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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