Method of startup control for a gas turbine system operating in a fired deceleration shutdown process mode

A method of startup control for a gas turbine system that is operating in a fired deceleration shutdown process mode (24) is provided. The method includes determining whether the combustor flame is in a lit state (26). Also included is increasing a fuel flow to the gas turbine system if the combusto...

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Bibliographische Detailangaben
Hauptverfasser:	MORAWSKI, CHRISTOPHER JOHN, POST, EUGENE ARMSTEAD, SNIDER, DAVID AUGUST
Format:	Patent
Sprache:	eng ; fre ; ger
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 INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A method of startup control for a gas turbine system that is operating in a fired deceleration shutdown process mode (24) is provided. The method includes determining whether the combustor flame is in a lit state (26). Also included is increasing a fuel flow to the gas turbine system if the combustor is determined to be in the lit state (26). Further included is initiating (28) a starter system to the gas turbine system.