GAS TURBINE PLANT AND OPERATING METHOD THEREFOR

The gas turbine plant is provided with a gas turbine (10), a heating device (60), a decomposition gas line (70), and a decomposition gas compressor (85). The heating device (60) heats ammonia and thermally decomposes the ammonia to convert the ammonia into decomposition gas (PG) including hydrogen g...

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Bibliographic Details
Main Authors TANIMURA Satoshi, NOSE Masakazu, UECHI Hideyuki
Format Patent
LanguageEnglish
French
German
Published 18.09.2019
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION APPARATUS
COMBUSTION ENGINES
COMBUSTION PROCESSES
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
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
STEAM ACCUMULATORS
STEAM ENGINE PLANTS
STEAM ENGINES
WEAPONS
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Summary:The gas turbine plant is provided with a gas turbine (10), a heating device (60), a decomposition gas line (70), and a decomposition gas compressor (85). The heating device (60) heats ammonia and thermally decomposes the ammonia to convert the ammonia into decomposition gas (PG) including hydrogen gas and nitrogen gas. The decomposition gas line (70) sends the decomposition gas PG from the heating device (60) to the gas turbine (10). The decomposition gas compressor (85) increases the pressure of the decomposition gas (PG) to a pressure equal to or higher than a feed pressure at which the decomposition gas (PG) is allowed to be fed to the gas turbine (10).
Bibliography:Application Number: EP20170869962