System and method of using a compressed air storage system with a gas turbine

SYSTEM AND METHOD OF USING A COMPRESSED AIR STORAGE SYSTEM WITH A GAS TURBINE A power generation system (200) includes a first compressor (202), a second compressor (206), a combustor (232) configured to receive compressed air from the second compressor (206) to produce an exhaust stream, a first tu...

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Bibliographische Detailangaben
Hauptverfasser:	HOFFMANN, STEPHANIE MARIE-NOELLE, FREUND, SEBASTIAN WALTER, FINKENRATH, MATTHIAS, FERGUSON, GARLAND, NAIDU, BALACHANDAR, BOOTH, CHARLES MICHAEL
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GENERATION HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION SYSTEMS FOR STORING ELECTRIC ENERGY TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Zusammenfassung:	SYSTEM AND METHOD OF USING A COMPRESSED AIR STORAGE SYSTEM WITH A GAS TURBINE A power generation system (200) includes a first compressor (202), a second compressor (206), a combustor (232) configured to receive compressed air from the second compressor (206) to produce an exhaust stream, a first turbine (238), and a power turbine (244). The first turbine (238) is configured to receive the exhaust stream, generate a rotational power from the exhaust stream, output the rotational power to a second compressor (206), and output the exhaust stream. The system (200) includes a coupling device (212) configured to couple and decouple the first compressor (202) to/from a second turbine (242), an electrical generator (210) coupled to an output of the power turbine (244) and configured to output electrical power, and a controller (256) configured to cause the coupling device (212) to mechanically decouple the second turbine (242) from the first compressor (202), and cause the coupling device (212) to direct compressed air from an air storage cavern (224) to an inlet (208) of the second compressor (206). 218 28 20 222 204 220 236 232 252 26234 248 250 254 212 206 238 210 202 242 244- 246