Remote tuning for gas turbines

A system and method for tuning a gas turbine (200) comprises a turbine controller (210) coupled to the gas turbine (200), a first computer system coupled to the turbine controller (210) and located locally to the gas turbine (200), and a second computer system (240) for exchanging data with the firs...

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Bibliographische Detailangaben
Hauptverfasser:	WILLIAMS, GEORGE EDWARD, BUTTERFIELD, ERIC GARDNER, MCCARTHY, JOHN PATRICK, RUSSO, VICTOR FRANZ, SHAPIRO, ANDREW PHILIP, MATTISON, SCOTT CAMPBELL, GRANT III, MILTON LEWISTON
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CALCULATING COMBUSTION ENGINES COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING CONTROLLING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COUNTING ELECTRIC DIGITAL DATA PROCESSING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING WEAPONS
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Beschreibung
Zusammenfassung:	A system and method for tuning a gas turbine (200) comprises a turbine controller (210) coupled to the gas turbine (200), a first computer system coupled to the turbine controller (210) and located locally to the gas turbine (200), and a second computer system (240) for exchanging data with the first computer system. The second computer system (240) is located remotely from the gas turbine (200) and exchanges data with the first computer system via a network connection such as the internet, an intranet or a virtual private network (VPN). Data relating to a characteristic such as turbine combustion dynamics and/or emissions is transmitted by the first computer system to the second computer system (240). The second computer system (240) transmits control data over the network connection to the first computer to tune the gas turbine (200).