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

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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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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creator MORAWSKI, CHRISTOPHER JOHN
POST, EUGENE ARMSTEAD
SNIDER, DAVID AUGUST
description 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.
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subjects 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
title Method of startup control for a gas turbine system operating in a fired deceleration shutdown process mode
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