SYSTEMS AND METHODS FOR TURBINE SYSTEM OPERATION IN LOW AMBIENT TEMPERATURES

A system includes a controller communicatively coupled to a compressor (26). The controller is configured to sense an exhaust temperature of a gas turbine system (24) fluidly coupled to the compressor (26) and derive a setpoint based on the sensed exhaust temperature. The controller is also configur...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MESTRONI, JULIO ENRIQUE, COCCA, MICHAEL ANTHONY, SCIPIO, ALSTON ILFORD, MATHAI, GEORGE VARGESE, EKANAYAKE, SANJI, KLOSINSKI, JOSEPH PHILIP
Format:	Patent
Sprache:	eng ; pol
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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