Pressure control method and system to reduce gas turbine fuel supply pressure requirements

A system and method to reduce the gas fuel supply pressure requirements of a gas turbine, which results in an increased operability range and a reduction in gas turbine trips. According to the method, the gas turbine is allowed to start and operate at supply pressures determined as a function of amb...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	THATCHER JONATHAN CARL, ELURIPATI RAVI PRAVEEN S, CHILDERS PRISCILLA, GALLAGHER BRIAN, SWEET BRYAN EDWARD
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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