发明名称 VARIOUS FULL ROTOR BLADE STEAM GAS TURBINE COMBINED- ENGINE
摘要 <p>PROBLEM TO BE SOLVED: To switch to the driving of an internal combustion engine of zero combustion gas exhaust and to prevent the global warming with an electricity bill of 1/3 by allowing a gas turbine exhaust temperature to be close to -273 deg.C, and coagulating the water and the water vapor while using the very low temperature combustion gas as a core for fractional recovery, as the prevention of global warming is urgent need. SOLUTION: The combustion gas exhaust temperature is allowed to be close to -273 deg.C by unlimitedly performing the combustion heat exchange by means of a combustor/heat exchanger of a full rotor blade steam gas turbine combined-engine, the approximately whole amount of heat of the compressed air higher than -273 deg.C is recovered to recover the heat of about two times of that in a conventional boiler, the heating high temperature can be surely and easily achieved by annular-type casting of every stage in a process of increasing the output of a gas turbine by 20-30 times and 4-6 times of an existing gas turbine, and further a vaporization film is formed between a heating high temperature turbine blade and the water of gravitational power of 1700 times and the like to remarkably reduce the heat consumption frictional loss with a simple structure, whereby the full rotor blade steam gas turbine combined-engine of idea output of 24-36 times of the existing gas turbine can be provided, and the thermodynamic brainwashing is excluded.</p>
申请公布号 JP2002303152(A) 申请公布日期 2002.10.18
申请号 JP20010312338 申请日期 2001.10.10
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU
分类号 A01K61/00;F02C3/067;F02C3/113;F02C3/26;F02C3/30;F16H13/04;F16H13/08;F16H13/12;(IPC1-7):F02C3/113 主分类号 A01K61/00
代理机构 代理人
主权项
地址