发明名称 VARIOUS ENERGY CONSERVATION CYCLE COMBINED ENGINE
摘要 <p>PROBLEM TO BE SOLVED: To solve a problem of existing jet engines and gas turbines that compressed air and fuel gas are intercepted to make speed and output closer to 0 by alternately, fifty-fifty providing stationary blades and moving blades without power.SOLUTION: In comparison with extremely undesirable, existing most advanced science and technology, in a double inversion engine 12B or the like, compression blades 8q and 8r and output blades 8s and 8t out of all moving blades achieve an air compression speed or a combustion gas expansion speed by means of linear compression or linear expansion that is intended to be 10 times as high as that of the existing most advanced science and technology, a compressed-air heat exchanger 2Y that exchanges heat with a fuel injection/combustion pipe at a compression ratio of 40 or higher produces superheated steam 5H such that a production amount of the superheated steam 5H is intended to be 20 times or more as large as that produced by an existing thermal power plant boiler with the same fuel amount, a power generation amount that is intended to be 1000 times as large as that of an existing thermal power plant with the same fuel amount is achieved, injection propulsion power and rotational power intended to be 1000 times as high as those by an existing jet engine or the like are achieved. The double inversion engine 12B or the like is used for driving an automobile, a ship, an airplane or the like, and also used for superheated steam rocket injection at an existing highest flight altitude such that space launch cost can be reduced to one-500 thousandth or the like.</p>
申请公布号 JP2014185531(A) 申请公布日期 2014.10.02
申请号 JP20130059199 申请日期 2013.03.22
申请人 TANIGAWA HIROYASU;TANIGAWA KAZUNAGA 发明人 TANIGAWA HIROYASU ; TANIGAWA KAZUNAGA
分类号 F01K7/02;F01D15/02;F01D15/04;F02C3/067 主分类号 F01K7/02
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