Gas turbine cooling system

A gas turbine plant comprises a gas turbine system provided with a compressor, a gas turbine and a generator which are mounted on a common shaft and operatively connected in series to each other, a gas turbine combustor system including a gas turbine combustor composed of an outer casing and an inne...

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Bibliographic Details
Main Author MAEDA; FUKUO
Format Patent
LanguageEnglish
Published 08.09.1998
Edition6
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION APPARATUS
COMBUSTION ENGINES
COMBUSTION PROCESSES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A gas turbine plant comprises a gas turbine system provided with a compressor, a gas turbine and a generator which are mounted on a common shaft and operatively connected in series to each other, a gas turbine combustor system including a gas turbine combustor composed of an outer casing and an inner cylinder accommodated in the casing, and a cooling air circulation system operatively connected to the gas turbine combustor system for circulating cooling air. A cooling passage structure is disposed along an outer peripheral surface of the inner cylinder and a circulation line is disposed for circulating cooling air in the cooling passage structure and balancing the inner pressure of the casing of the gas turbine combustor. The cooling air circulation system includes an equalizer header unit for supplying the cooling air in the cooling passage structure to the circulation line, a heat exchanger unit for re-cooling the cooling air from the equalizer header unit and a blower unit for returning the cooling air to the cooling passage structure after the re-cooling.
Bibliography:Application Number: US19960756918