Turbine inlet air heat pump-type system

A heating and cooling system (100) for inlet air of a turbine compressor (20). The heating and cooling system (100) may include a thermal energy storage tank charging loop (190), a cooling loop (200) in communication with the thermal energy storage charging loop (190), and a heating loop (210) in co...

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Bibliographische Detailangaben
Hauptverfasser:	MOTAKEF, ABBAS, FEHER, PETER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL ENGINE PLANTS NOT OTHERWISE PROVIDED FOR ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION STEAM ACCUMULATORS STEAM ENGINE PLANTS STEAM ENGINES 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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Beschreibung
Zusammenfassung:	A heating and cooling system (100) for inlet air of a turbine compressor (20). The heating and cooling system (100) may include a thermal energy storage tank charging loop (190), a cooling loop (200) in communication with the thermal energy storage charging loop (190), and a heating loop (210) in communication with the cooling loop (200) and the inlet air of the turbine compressor (20).