Systems and methods for controlling gas turbines

Embodiments of the disclosure relate to systems and methods for controlling a gas turbine. In one embodiment, a method 300 can be provided. Measurement data associated with the operation of a gas turbine may be received 305 to determine 310 if the current operating state of the gas turbine is associ...

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Bibliographische Detailangaben
Hauptverfasser:	EWENS, DAVID SPENCER, SEELY, WILLIAM FORESTER, JONES, TREVOR V
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 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	Embodiments of the disclosure relate to systems and methods for controlling a gas turbine. In one embodiment, a method 300 can be provided. Measurement data associated with the operation of a gas turbine may be received 305 to determine 310 if the current operating state of the gas turbine is associated with a predefined risk. Thereafter, the measurement data and one or more model operating parameters for operation of the inlet bleed heat system that minimizes the risk may be identified 315 in order to generate 325 one or more control signals operable to adjust the operation of the inlet bleed heat system for the gas turbine to adjust the one or more model operating parameters.