CO-GENERATION SYSTEM

PURPOSE:To contrive the saving of fuel consumption by providing a water cooling wall converting feed water into vapour for the combustor of a gas turbine. CONSTITUTION:A water cooling wall converting feed water 59 into vapour for the combustor (pressurized combustion boiler) 50 is provided for a gas...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	KAWANO SHIGEHIRO, ISHIDA TETSUYOSHI, ARISAKI KENJI, FUJIWARA TADAYUKI
Format:	Patent
Sprache:	eng
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:	PURPOSE:To contrive the saving of fuel consumption by providing a water cooling wall converting feed water into vapour for the combustor of a gas turbine. CONSTITUTION:A water cooling wall converting feed water 59 into vapour for the combustor (pressurized combustion boiler) 50 is provided for a gas turbine generating system. High pressure saturated vapour 53 generated within an exhaust heat boiler 16 and vapour generated by the combustor 50 are led to a super heater 51 so as to be fed to a high pressure steam turbine 45. Thus, since the water cooling wall is provided in the combustor 50, combustion gas can be lowered in temperature down to the heat proof limit of a gas turbine, the quantity of air to be fed to the combustor can thereby be reduced. This constitution thereby enables the saving of fuel consumption.