Independent pilot fuel control in secondary fuel nozzle

Disclosed herein is a fuel nozzle (36). The fuel nozzle (36) includes a first fuel introduction location, a second fuel introduction location, and fuel passages (50). The first fuel introduction location is located radially about the fuel nozzle (36) and is connected with a fuel passage (50). The se...

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Bibliographische Detailangaben
Hauptverfasser:	VANDALE, DANIEL D, ROMOSER, CAREY, SIMONS, DERRICK, NEGRONI, ALBERTO JOSE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR AIR SUPPLY BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES DRAUGHT-INDUCING GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS WEAPONS
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Beschreibung
Zusammenfassung:	Disclosed herein is a fuel nozzle (36). The fuel nozzle (36) includes a first fuel introduction location, a second fuel introduction location, and fuel passages (50). The first fuel introduction location is located radially about the fuel nozzle (36) and is connected with a fuel passage (50). The second fuel introduction location is located at an end of the fuel nozzle (36) and is connected with another fuel passage (50) such that the fuel passage (50) connected to the first fuel introduction location is separate from the fuel passage (50) connected to the second fuel introduction location.