SYSTEMS AND METHODS FOR DETERMINATION OF GAS TURBINE FUEL SPLIT FOR HEAD END TEMPERATURE CONTROL

To provide methods for controlling a temperature of a first combustion zone of a combustor of a gas turbine engine using a digital simulation.SOLUTION: A method of controlling an operating temperature of a first combustion zone of a combustor of a rotary machine includes determining a current operat...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JOHN ROGERS HUEY, JONATHAN CARL THATCHER, ROBERT JOSEPH LOEVEN II
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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