| 摘要 |
PROBLEM TO BE SOLVED: To eliminate disadvantage of getting approximate 0 state of speed and output in an existing jet engine and an existing gas turbine through alternative half arrangement of stator blades of zero power and rotor blades while intercepting compressed-air and combustion gas.SOLUTION: There are provided a double inversion engine 2T and a double inversion injection engine 2U having substantial entire rotor blades, in which compressed-air speed and combustion gas expansion speed are made maximum through linear line compression and linear line expansion near a bearing load 0, a high pressure high temperature combustion chamber 5M is provided with a high pressure high temperature water heating pipe 5H to perform heat-recovery and cooling to keep the same compression air volume up to a theoretical air-fuel ratio, cause a fuel combustion amount to become four times of that of the existing jet engine, a calory of 3/4 or more is used in super-heated vapor 50 having pressure of 20 times of that of combustion gas and the like so as to attain injection propulsion output and rotary output of 10 times of the existing jet engine and the existing gas turbine, an existing rocket injection from the ground is considered as the worst operation at a process of airplane driving as one of power generation, an automobile drive, a ship drive and an airplane drive or the like, a rocket injection from the existing maximum high flight altitude is applied so as to enable a day's trip at any locations on the earth such as 16 turning around the earth in one day to be carried out. |
