COOLING SYSTEM FOR TURBOMACHINE

PROBLEM TO BE SOLVED: To provide a cooling system improving combined cycle efficiency and an increase in power output by reducing exhaust dilution losses and reducing the parasitic load by requiring fewer air circulation devices, and reducing the installation and start-up costs by requiring fewer ai...

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Bibliographische Detailangaben
Hauptverfasser:	SMITH RAUB W, CHILLAR RAHUL J
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 HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ACCUMULATORS STEAM ENGINE PLANTS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a cooling system improving combined cycle efficiency and an increase in power output by reducing exhaust dilution losses and reducing the parasitic load by requiring fewer air circulation devices, and reducing the installation and start-up costs by requiring fewer air circulation devices and integrating the systems. SOLUTION: Fluid communication of integrated cooling circuits cooling each of a plurality of compartments 105, 110 of a gas turbine device constituting a turbomachine 100 is established, and a cooling fluid comprising compartment air is circulated between the circuits. COPYRIGHT: (C)2010,JPO&INPIT