发明名称 VARIOUS FULL ROTOR BLADE STEAM GAS TURBINE COMBINED ENGINE
摘要 <p><P>PROBLEM TO BE SOLVED: To provide an various full rotor blade steam turbine combined engine in which a gas turbine exhaust temperature is approached -273°C, moisture is coagulated on a low temperature combustion gas as a nucleus, for differential recovery, combustion gas exhaust, such as CO<SB>2</SB>, etc. is approached zero, and which prevents a global warming from occurring at an electric rate of, for example, 1/10 as small as an ordinary rate. <P>SOLUTION: This various full rotor blade steam turbine combined engine high-pressure combustion heat exchanges without limit by a combustor-cum-heat exchanger of the engine, makes the combustion gas exhaust temperature approach -273°C, and recovers substantially all heat quantity of compressed air of -273°C or higher so that the heat recycling quantity of about twice as large as an existing boiler is set. The step of (amount of combustion gas heat quantity power generation)+(combustion gas mass power generation)=(an increase in the amount of 240-580 times as much as hypothetical power generation of the existing gas turbine) is performed by an electromagnetic heating turbine blade which is annularly cast at each step-down. A frictional loss between high temperature waters, such as 1,700 times as many gravity power as this is remarkably reduced, the structure is simplified and heat consumption is minimized, the moisture is coagulated with the low temperature combustion gas as the nucleus, differentiated as water droplets, and the combustion gas exhaust such as CO<SB>2</SB>, etc. is approached 0. <P>COPYRIGHT: (C)2004,JPO</p>
申请公布号 JP2004100678(A) 申请公布日期 2004.04.02
申请号 JP20020349544 申请日期 2002.12.02
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU
分类号 F02C3/067;F02C3/22;F02C3/30;F02C7/08;(IPC1-7):F02C3/067 主分类号 F02C3/067
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