PILOTED AIRBLAST LEAN DIRECT FUEL INJECTOR

A gas turbine fuel injection system of the lean direction injector type to reduce NOx emissions is provided. The configuration includes a pilot fuel injector (66), a pilot swirler (28), a main injector (68), and inner (22) and outer (24) main swirlers. An air splitter (26) between the pilot (28) and...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	NICKOLAUS, DANIEL, A, SMITH, CLIFFORD, E, CROCKER, DAVID, S
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING BURNERS 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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