发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 <p><P>PROBLEM TO BE SOLVED: To drive out the existing jet airplane to prevent global heating by performing injection output in such a manner that the rotation output of a liquid metal solar engine is increased to 10,000 to 23,000 times the rotation output of the existing steam turbine. <P>SOLUTION: In the liquid metal solar engine, turbines with fitting bolts assembled and including turbine moving blade groups having the same diameter and approximately the same shape with respect to each turbine stage are respectively driven by liquid metal gravity acceleration, partial overheated steam acceleration and partial combustion gas acceleration, liquid meal power having the same speed and the same volume as the atmospheric pressure is set to be 10,000 to 23,000 times the rotation output of the existing steam turbine, most of overheated steam and combustion gas are supplied to a combined engine injection section 78V, fuel is injected and burnt at a four-stage, and superheated steam heating is increased, thereby making pressure of 10 to 100 times, heat quantity injection of 10 times and injection thrust power of 100 to 1,000 times the existing jet airplane reach space in a short time. Consequently, various large airships, various space shuttles and various aircrafts are driven even by torque, fuel economy is reduced, CO2 emissions are reduced, full use of space is achieved, finite resources such as fossil fuel are left to posterity, and also the global heating is prevented. <P>COPYRIGHT: (C)2011,JPO&INPIT</p>
申请公布号 JP2010275863(A) 申请公布日期 2010.12.09
申请号 JP20090114425 申请日期 2009.05.11
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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