SYSTEM AND METHOD FOR SUPPLYING FUEL TO GAS TURBINE

PROBLEM TO BE SOLVED: To provide a system (300) and method (600) for supplying fuel to a gas turbine (315).SOLUTION: A fuel may be received, and one or more parameters associated with the received fuel may be determined. Based at least in part upon the determined one or more parameters, a desired pr...

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Bibliographische Detailangaben
Hauptverfasser:	MOSS DANIEL MARTIN, BILTON TIMOTHY RUSSELL, RENDO KOREY FREDERIC, WILKES COLIN
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a system (300) and method (600) for supplying fuel to a gas turbine (315).SOLUTION: A fuel may be received, and one or more parameters associated with the received fuel may be determined. Based at least in part upon the determined one or more parameters, a desired pressure for removing one or more liquids from the fuel utilizing a separator (310) may be calculated. The operation of a pressure changing device (305) may then be controlled in order to achieve the desired pressure. In certain embodiments, the operations of the method may be performed by a controller (320) that includes one or more computers.