System and method for supplying fuel to a gas turbine

The invention relates to a system and a method for supplying fuel to a gas turbine. The system for supplying fuel to the gas turbine includes piping containing fuel at a pressure greater than approximately 500 psi. A pressure reducing valve connected downstream of the piping reduces the pressure of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MOSS DANIEL MARTIN, BILTON TIMOTHY RUSSELL, RENDO KOREY FREDERIC, WILKES COLIN
Format:	Patent
Sprache:	chi ; 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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