| 摘要 |
<p>PROBLEM TO BE SOLVED: To attain solutions overcoming defaults found in the existing jet engines or gas turbines that half of the stationary blades having no power and half of the rotary blades are alternatively arranged to reserve compressed air or combustion gas to cause their speed or output to approach to a value of 0.SOLUTION: In order to eliminate too incoherent defaults found in the existing most-advanced scientific technologies, 10 times-speed compression and expansion are attained through super-speed double inversion linear compression and linear expansion of compression blades 8q, compression blades 8r, output blades 8s and output blades 8t for use in cooling and compression of compressed air with water-cooled compression blades of a double inversion engine 12G and the like having full rotary blades; super-heated steam 5H is manufactured by a compression air heat exchanger 2Y with fuel injection, combustion and heat exchanging operation with a compression ratio being about 100; 130 times super-heated steam 5H of the existing fire power generation boiler with the same amount of fuel is manufactured; 1000 times injection propulsion output of the existing jet engine with the same amount of fuel or rotary output is attained; in an automobile driving or ship driving or airplane driving, the case of the airplanes is rocket injection with super-heated steam from near the existing highest altitude and expenditure of the existing rocket reaching the space is its 1/5,00,000.</p> |
