VARIABLE RESTRICTION OF A FUEL CIRCUIT OF A FUEL NOZZLE

A fuel injector for a turbine engine includes a fuel scheduling valve configured for regulation of fuel flow from a fuel inlet in response to fuel pressure received at the fuel inlet. Primary and secondary fuel circuits receive fuel from the scheduling valve, and an electrically-controlled valve is...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Williams, Brandon P, Kokas, Jay W, Reuter, Charles E, Ferrarotti, Michael, Versailles, Richard E, Rourke, JR., Russell P, Lokhandwalla, Murtuza, Haugsjaahabink, Todd, Ryon, Jason A
Format:	Patent
Sprache:	eng
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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