Method and system for operating gas turbine engine system

The invention relates to a method and a system for operating gas turbine engine system. A gas turbine engine system (10) is provided. The gas turbine engine system (10) includes a gas turbine engine including at least one combustor (14) configured to receive a flow of fuel from a flow control device...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	SZEPEK SCOTT WILLIAM, BUCHALTER LAUREN JEANNE, MARIANI MICHAEL JOHN, SWEET BRYAN EDWARD
Format:	Patent
Sprache:	chi ; 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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Beschreibung
Zusammenfassung:	The invention relates to a method and a system for operating gas turbine engine system. A gas turbine engine system (10) is provided. The gas turbine engine system (10) includes a gas turbine engine including at least one combustor (14) configured to receive a flow of fuel from a flow control device (288), and a fuel control system (288) including a piping system configured to channel the flow of fuel from a fuel source to the flow control device, a sensor configured to generate a signal indicative of a property of the flow of fuel wherein the property of the flow of fuel is variable over time, and a controller including a processor programmed to receive the generated signal, using a flow model of the piping system and the received signal, iteratively track the progress of a plurality of discrete volumes flowing through the piping system, and control the flow of fuel using the flow control devices.