Integrazione booster di gas combustibile-turbina a gas per risparmio energetico e operatività ottimizzata

A fuel gas booster-gas turbine integration for energy saving & optimized operability is disclosed. The fuel gas booster-gas turbine integration comprises an integrated system comprising a reciprocating compressor based fuel gas booster (10) and a gas turbine (11) wherein the gas turbine flow and...

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Bibliographische Detailangaben
Hauptverfasser:	Petruzzi, Luca, Carnieri, Andrea, Fadlun, Ever Avriel
Format:	Patent
Sprache:	ita
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:	A fuel gas booster-gas turbine integration for energy saving & optimized operability is disclosed. The fuel gas booster-gas turbine integration comprises an integrated system comprising a reciprocating compressor based fuel gas booster (10) and a gas turbine (11) wherein the gas turbine flow and pressure control system (15) and the fuel gas booster pressure and capacity control system (20) are synchronized to optimize the fuel gas booster power consumption or the fuel gas booster and gas turbine package power consumption, and wherein the gas turbine flow and pressure control system (15) comprises at least one gas turbine fuel gas input control valve (14) and the fuel gas booster control system (20) comprises a gas turbine fuel gas input control valve position controller, associated to said at least one gas turbine fuel gas input control valve (14), and fuel gas booster capacity control devices, associated to said reciprocating compressor based fuel gas booster (10).