PROPORTIONAL RESTRICTION OF FUEL NOZZLE WITH AN AUXILIARY CIRCUIT

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, secondary and auxiliary fuel circuits receive fuel from the scheduling valve, and an electrically-controll...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Williams, Brandon P, Kokas, Jay W, Ferrarotti, Michael, Versailles, Richard E, Rourke, JR., Russell P, Lokhandwalla, Murtuza, Haugsjaahabink, Todd
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING 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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