GAS TURBINE FACILITY AND ITS CONTROL METHOD
PROBLEM TO BE SOLVED: To increase quantity of heat when supplying the heat, by highly maintaining efficiency of a compressor and a turbine, regardless of an increase-decrease in quantity of steam included in combustion gas passing through the turbine, in a moisture using type gas turbine for injecti...
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| creator | SHIBATA TAKANORI HATAMIYA SHIGEO SEIKI NOBUHIRO |
| description | PROBLEM TO BE SOLVED: To increase quantity of heat when supplying the heat, by highly maintaining efficiency of a compressor and a turbine, regardless of an increase-decrease in quantity of steam included in combustion gas passing through the turbine, in a moisture using type gas turbine for injecting moisture into delivery of the compressor and a combustor. SOLUTION: This gas turbine facility has the compressor 10 for compressing air, the combustor 12 for generating the combustion gas by burning fuel and compressed air provided by being compressed by the compressor, the turbine 14 driven by the combustion gas generated by the combustor, a means 42 for supplying the moisture to the compressed air or the combustion gas, and a measuring device for directly or indirectly measuring the quantity of supplied moisture. The gas turbine facility is provided with a control means for raising the combustor outlet gas temperature in response to reduction in moisture quantity. COPYRIGHT: (C)2005,JPO&NCIPI |
| format | Patent |
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SOLUTION: This gas turbine facility has the compressor 10 for compressing air, the combustor 12 for generating the combustion gas by burning fuel and compressed air provided by being compressed by the compressor, the turbine 14 driven by the combustion gas generated by the combustor, a means 42 for supplying the moisture to the compressed air or the combustion gas, and a measuring device for directly or indirectly measuring the quantity of supplied moisture. The gas turbine facility is provided with a control means for raising the combustor outlet gas temperature in response to reduction in moisture quantity. 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SOLUTION: This gas turbine facility has the compressor 10 for compressing air, the combustor 12 for generating the combustion gas by burning fuel and compressed air provided by being compressed by the compressor, the turbine 14 driven by the combustion gas generated by the combustor, a means 42 for supplying the moisture to the compressed air or the combustion gas, and a measuring device for directly or indirectly measuring the quantity of supplied moisture. The gas turbine facility is provided with a control means for raising the combustor outlet gas temperature in response to reduction in moisture quantity. 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SOLUTION: This gas turbine facility has the compressor 10 for compressing air, the combustor 12 for generating the combustion gas by burning fuel and compressed air provided by being compressed by the compressor, the turbine 14 driven by the combustion gas generated by the combustor, a means 42 for supplying the moisture to the compressed air or the combustion gas, and a measuring device for directly or indirectly measuring the quantity of supplied moisture. The gas turbine facility is provided with a control means for raising the combustor outlet gas temperature in response to reduction in moisture quantity. COPYRIGHT: (C)2005,JPO&NCIPI</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL 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 ENGINES WEAPONS |
| title | GAS TURBINE FACILITY AND ITS CONTROL METHOD |
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