GAS TURBINE FOR POWER GENERATION

PROBLEM TO BE SOLVED: To provide a gas turbine capable of suppressing production of excess energy and reducing an increase in the rotating speed of a shaft.SOLUTION: A gas turbine for power generation having a compressor 103 for compressing air, a combustor 112 producing a combustion gas by mixing a...

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Bibliographische Detailangaben
Hauptverfasser:	TAKAHASHI KAZUO, ITO TOMOMICHI, HINO TOKUAKI, KUSUMI HISAHIRO
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a gas turbine capable of suppressing production of excess energy and reducing an increase in the rotating speed of a shaft.SOLUTION: A gas turbine for power generation having a compressor 103 for compressing air, a combustor 112 producing a combustion gas by mixing and burning the air compressed by the compressor 103 and fuel, a turbine 114 driven by the combustion gas, and a power generator 116 generating power by rotational force of the turbine 114, further includes a fuel pipe 111 for supplying the fuel to the combustor 112, a fuel adjustment valve 108 disposed in the fuel pipe 111, a fuel discharge pipe 203 branched from the fuel pipe 111 between the fuel valve 108 and the combustor 112, and a fuel discharge valve 120 disposed in the fuel discharge pipe 203.