发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 PROBLEM TO BE SOLVED: To increase the injection output of a liquid metal solar heat engine with 10,000-23,000 times of the rotational output of an existing steam turbine.SOLUTION: The moving blade group of a plurality of turbines are formed in a same diameter and generally same shape for each stage, and the turbines assembled with fitting bolts are driven by gravity acceleration of liquid metal, partly acceleration of superheated steam, and partly acceleration of combustion gas, respectively, in the liquid metal solar heat engine. The atmospheric pressure, same speed, same volume liquid metal power becomes 10,000-23,000 times of the rotational output of the existing steam turbine. Most of the superheated steam and combustion gas are supplied to a combined engine injection part 78V and fuel is injected and burned in four stages to enhance the heating of the superheated steam to target, in a short time, to arrive at a space with 10-100 times of pressure, 10 times of heat quantity injection, and 100-1,000 times of injection propulsion output of an existing jet plane. Therefore, large-sized various airships, various airplanes, and various aircraft can be driven. Since fuel consumption is reduced, exhaust of CO2 is reduced, and the use thereof in a space is in heyday, limited resources such as fossil fuel can be left to descendants, and global warming can be prevented from advancing.
申请公布号 JP2011007043(A) 申请公布日期 2011.01.13
申请号 JP20090143024 申请日期 2009.06.16
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA
分类号 F03G3/00 主分类号 F03G3/00
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