JP2001221062A - Ultra low power consumption-type gas turbine and mechanical system driven by the same - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a completely clean, compact and inexpensive ultra low power consumption-type gas turbine of high performance and long life capable of preventing the air pollution and global warming, and a mechanical system driven by the same. SOLUTION: The ultralow power consumption gas turbine 10 is adopted as a power system of the mechanical system 14, a plasma reactor 16 is mounted on the gas turbine 10, the hydrogen rich fuel including the water vapor is produced in the presence of plasma arc by reacting the electrolytic water with the hydrocarbon fuel, the hydrogen rich fuel is mixed with the compressed air and burned in a combustor 18 to produce the working fluid of high temperature and high pressure, and an expansion turbine 22 is driven by the working fluid.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a power system using fossil fuel, and more particularly, to a gas turbine used as a power source for vehicles, power plants, large pumps, and the like, and a mechanical system driven by the gas turbine.

[0002]

2. Description of the Related Art Hydrogen-rich energy has recently been used as an effective measure to prevent depletion of petroleum resources, air pollution by harmful gases emitted from various industrial fields such as automobiles, factories and power plants, and global warming due to carbon dioxide emissions. Has attracted attention as an alternative to petroleum energy, and a power system using this has been proposed.

In US Pat. No. 5,176,809, a counter electrode is arranged in a container, and a hydrocarbon such as gasoline or light oil and an electrolyte are introduced, and hydrogen is generated from the hydrocarbon and the electrolyte by an electrolytic action. At the same time, a technique for generating oxygen from an electrolytic solution has been proposed. In this technique, the counter electrode is supplied with low-voltage DC power from a DC power supply, and generates hydrogen oxygen by electrolysis. At this time, since the hydrocarbon is insulative, and even if mixed with the electrolytic solution, the electrolytic action by the counter electrode is insignificant, so that the amount of generated hydrogen is extremely small. During electrolysis, fine bubbles of hydrogen and oxygen adhere to the surface of the counter electrode,
Poor contact between the electrolyte and the electrode occurs, and the electrolytic efficiency is significantly reduced. For the above reasons, it is impossible to supply a sufficient amount of hydrogen oxygen on site, and it has been difficult to put it into practical use as a fuel production apparatus for vehicles.

In US Pat. No. 5,437,250, a corner of a cylindrical plasma anode is arranged so as to be close to the inner wall of an annular plasma cathode, and a water reservoir is provided below an electrode support member to generate steam. This vapor is brought into contact with a plasma arc generated between the counter electrodes to generate a mixed gas of hydrogen and oxygen, and the mixed gas and the hydrocarbon fuel are mixed and supplied to the engine as a hydrogen-rich hydrocarbon fuel. A plasmatron has been proposed. In this device, since a plasma arc is generated only in a locally narrow region due to a localized dielectric breakdown between the opposed electrodes, the hydrogen generation efficiency is extremely low. At this time, local electrode wear is also severe. To prevent this, a magnetic coil is placed around the outer periphery of the cylindrical cathode to change the position where the plasma arc is generated. However, the area where the plasma arc is generated cannot be expanded, so the amount of hydrogen generated increases. I can't let that happen. Furthermore, in this device, the hydrocarbon fuel is not reformed into a clean fuel because it does not have a structure in contact with the plasma arc. Therefore, harmful components such as NOX, CO, HC, and SOX in the exhaust gas of the engine cannot be remarkably reduced, and the fuel efficiency of the engine cannot be improved.

[0005]

SUMMARY OF THE INVENTION In the conventional reformer, the structure of the reformer is complicated and large, and the required amount of hydrogen-rich gas cannot be instantaneously generated on-site. Could not be improved significantly,
Practical application was difficult.

The present invention is compact, high performance and low cost,
Moreover, it is an object of the present invention to provide an ultra-low fuel consumption type gas turbine capable of generating a large amount of hydrogen-rich fuel on site from electrolyzed water and hydrocarbon fuel by a compact structure, and a mechanical system driven thereby.

[0007] Another object of the present invention is to provide 10 to 50% of a hydrocarbon fuel such as natural gas, gasoline, light oil, or kerosene.
It is an object of the present invention to provide an ultra-low fuel consumption gas turbine capable of instantly producing clean hydrogen-rich fuel from 90% electrolyzed water and a mechanical system driven by the gas turbine.

[0008]

Means for Solving the Problems In the first invention of the present application, the ultra-low fuel consumption type gas turbine supplies (a) a hydrocarbon fuel supply means; (b) an electrolyzed water supply means; and (c) supplies compressed air. (D) a plasma reactor that decomposes the hydrocarbon fuel and the electrolyzed water in the presence of the plasma arc to generate a mixed gas of steam and a hydrogen-rich fuel; and (e) communicates with the compressor and the plasma reactor. A combustor for generating a high-temperature and high-pressure combustion gas by burning an air-fuel mixture of the compressed gas and the mixed gas; and (f) an expansion turbine communicating with the combustor to expand the high-temperature and high-pressure combustion gas to obtain power and drive the compressor. And;

In the second invention of the present application, the ultra-low fuel consumption type gas turbine engine includes: (a) a hydrocarbon fuel supply unit; (b) an electrolyzed water supply unit; (c) an engine housing; A plasma reactor disposed in the engine housing to generate a mixed gas of steam and hydrogen-rich fuel by decomposing hydrocarbon fuel and electrolyzed water by a plasma arc; and (e) a compressor disposed in an engine housing to generate compressed air. (F) a combustor arranged in the engine housing to communicate with the plasma reactor and combusting a mixture of the gas mixture and the compressed air to generate a high-temperature, high-pressure combustion gas; and (g) inside the engine housing. An expansion turbine arranged to be coupled to the compressor and driven by the high temperature and high pressure combustion gas to obtain power output; Achieved by providing.

In the third invention of the present application, the mechanical system is disposed in (a) a hydrocarbon fuel supply unit; (b) an electrolyzed water supply unit; (c) an engine housing; and (d) an engine housing. A plasma reactor for decomposing a hydrocarbon fuel and electrolyzed water by a plasma arc to generate a mixed gas of steam and a hydrogen-rich fuel; (e) a compressor disposed in an engine housing to generate compressed air; (f) A combustor arranged in the engine housing to communicate with the plasma reactor and combusting the mixture of the gas mixture and the compressed air to generate a high-temperature, high-pressure combustion gas; and (g) connected to the compressor in the engine housing. (H) an expansion turbine driven by the high-temperature and high-pressure combustion gas to obtain a power output; It is more driven and driven means; is achieved by providing a.

In the fourth invention of the present application, the mechanical system is disposed in (a) a hydrocarbon fuel supply unit; (b) an electrolyzed water supply unit; (c) an engine housing; and (d) an engine housing. A plasma reactor for decomposing a hydrocarbon fuel and electrolyzed water by a plasma arc to generate a mixed gas of steam and a hydrogen-rich fuel; (e) a compressor disposed in an engine housing to generate compressed air; (f) A combustor arranged in the engine housing to communicate with the plasma reactor and combusting the mixture of the gas mixture and the compressed air to generate a high-temperature, high-pressure combustion gas; and (g) connected to the compressor in the engine housing. (H) an expansion turbine driven by the high-temperature and high-pressure combustion gas to obtain a power output; It is accomplished by providing; and more driven generator; (i) motor means driven by the electrical output of the generator; (j) a propulsion means driven by a motor means.

[0012]

In the ultra-low fuel consumption gas turbine of the present invention and the mechanical system driven by the same, the hydrogen-rich fuel is generated by bringing the electrolyzed water and the hydrocarbon fuel into direct contact with the plasma arc, and the hydrogen-rich fuel is generated with the compressed air. Mixing and burning by a combustor generates high-temperature combustion gas and supplies it to the expansion turbine, thereby generating power, thereby achieving compactness, high performance, high efficiency, and low cost. .

[0013]

FIG. 1 shows a mechanical system 14 comprising a hybrid mobile body incorporating a next-generation power system 12 employing an ultra-low fuel consumption gas turbine 10 according to a preferred embodiment of the present invention. The gas turbine 10 includes a plasma reactor 16, a combustor 18, a steam control valve 19, an expansion turbine 20, and a flywheel compressor 24. The flywheel compressor 24 is an air cleaner 2
3 Clean air is compressed and the compressed air is converted to a combustor 1
8 The gas turbine 10 includes a hydrocarbon fuel tank 22 such as natural gas, gasoline, light oil, kerosene, heavy oil, and methanol, an electrolyzed water tank 25, and a high-pressure pump 26 for supplying electrolyzed water to the plasma reactor 16 under high pressure.
And a venturi mixing means 27 for mixing the hydrocarbon fuel and the electrolyzed water. Electrolyzed water is tap water, groundwater,
A small amount of an ionizing agent such as seawater, NaOH, or KOH may be mixed with fresh water such as river water or industrial water. The venturi mixing means 27 is composed of 50 to 90% by weight of electrolyzed water and 10 to 50% by weight.
Is designed to obtain a mixing ratio with the hydrocarbon fuel. Preferably, 80 to 90% by weight of electrolyzed water and 10 to 20%
By setting the mixing ratio with the hydrocarbon fuel by weight, ultra low fuel consumption and ultra low pollution can be achieved.

As described later, the plasma reactor 16
Plasma power supply 28 to 50 consisting of three-phase AC inverter
Three-phase AC power of ~ 200 volts and 50 to 400 Hz is supplied as plasma power. At this time, a large amount of small plasma arc of 1800 ° to 3000 ° C. is generated in the plasma reactor 16. In the plasma reactor 16, the electrolyzed water and the hydrocarbon come into contact with a large amount of a small plasma arc and are mostly converted into a hydrogen-rich fuel, and the remainder not in contact with the small plasma arc are converted into water vapor. Recombination is prevented in the presence of Therefore, these mixed gases 17 are injected into the combustor 18 as fuel. Compressed air is injected into the combustor 18 and ignited by the spark plug 30 to generate high-temperature combustion gas. This working fluid is supplied to the expansion turbine 20 via the gas control valve 19, and generates power on the output shaft 34. A rotation sensor 35 is connected to the output shaft 34, and a rotation signal is supplied to the control device 37. The control device 37 stores data corresponding to the reference rotation speed, compares the data with the output signal from the rotation sensor 35, generates an output signal 37a according to the error signal, controls the gas control valve 19, and The expansion turbine 20 is controlled at a constant speed by controlling the supply amount of the working fluid to the expansion turbine 20. The exhaust gas of the expansion turbine 20 is returned to the electrolyzed water tank 25 to be condensed and reused. The exhaust gas component is exhausted from the upper part of the electrolyzed water tank 25 to the atmosphere.
When the present system is used as a cogeneration device, the exhaust gas of the turbine 20 may be supplied to a heating device and a hot water supply device to supply heat and power together, and then returned to the electrolytic water tank 25. Also,
A radiator (not shown) is provided on the moving body 14, and the cooling water is circulated through the condenser (not shown) to condense the steam in the expansion gas of the turbine 20 and circulate through the electrolyzed water tank 25. Is also good.

The flywheel compressor 24 and a generator GE are drivingly connected to an output shaft 34 of the expansion turbine 20. The AC output of the GE is DC-converted by the rectifier 44 and a part is charged to the battery, and the remaining part is a power converter 48
To drive the motor / generator 50 and drive the propulsion means 52 such as rear wheels. Power converter 48
Has a function of both a known inverter and a rectifying function, and has a function of converting AC regenerative electric power generated by the motor / generator 50 during braking of the hybrid vehicle 14 into DC and storing it in the battery 46. At the time of heavy load such as when climbing a hill, the output of the generator GE and the output of the battery 46 are simultaneously supplied to the motor / generator to increase the driving force of the rear wheel 52. The front wheels 56 may be connected to the output shaft 34 via the drive shaft 54, and these may be directly driven.

FIGS. 2 to 5 show a specific structure of the gas turbine 10, and the same components as those in FIG. 1 are denoted by the same reference numerals. The gas turbine 10 includes first to third zones 60, 62,
And a turbine housing 66 having the same. The turbine housing 66 includes an outer cylinder 68, an inner cylinder 70, a front end plate 72, and an insulating rear end plate 7.
4 is provided. The first zone 60 houses the plasma reactor 16 and the combustor 18. Second zone 62
The flywheel compressor 24 is disposed therein, and the expansion turbine 20 is disposed in the third zone 64. As is clear from FIGS. 2 and 3, an arch-shaped insulating casing 78 having an arc-shaped plasma reaction chamber 76 in the first zone 60, the arch-shaped combustor 18, and an insulating casing 78 formed at an intermediate portion between them. Is provided with an air preheating chamber 80 for preheating the compressed air while cooling the air. The first zone 60 is connected to the outer cylinder 68 so as to communicate with the compressor 24.
And the compressed air supply path 82 formed between the inner cylinder 70 and the inner cylinder 70. On the other hand, the combustor 18 is formed between the outer cylinder 68 and the inner cylinder 70 adjacent to the compressed air supply passage 82 and communicates with a jet passage 84 for supplying a high-temperature and high-pressure gas to the expansion turbine 20.

In FIG. 2 and FIG. 3, the plasma reactor 16 includes a fuel injection unit 85 having a fuel injection port 85 a and a small plasma generation unit 86, which are arranged in an arc-shaped plasma reaction chamber 76. The fuel injection means 85 communicates with the venturi 27 shown in FIG. 1, and a mixed liquid of hydrocarbon and electrolyzed water is supplied to the corner of the plasma reaction chamber 76 under pressure. The micro-plasma generating means 86 is provided at a central portion of the plasma reaction chamber 76 at circumferential intervals with three-phase AC plasma electrodes 88, 90, 92 connected to the plasma power supply 28 (see FIG. 1). An arc-shaped neutral electrode 94 fixed to the bottom of the chamber 76 and connected to the neutral point of the plasma power supply 28 via a terminal 93 or grounded. The microplasma generating means 86 further comprises a mixture of a solid electrode body 96 and an insulator 98, and the mixture is filled in a plasma reaction chamber 76 to form plasma electrodes 88, 90, 92 and a neutral electrode 94. A number of gaps 100 are formed between them. In an embodiment,
The mixture is shown as consisting of a ball-shaped electrode body having a diameter of 3 to 20 mm and a ball-shaped insulator having the same diameter as these.
The mixing ratio is selected in the range of 1: 1.5 to 1.5: 1. This mixing ratio has an effect of efficiently generating a small plasma arc in the many gaps 100. As a result, generation of localized plasma arcs in the plasma reaction chamber 76 is prevented, and abnormal wear of the electrodes is prevented. The plasma electrodes 88, 90, 92 and the neutral electrode 94 are selected from refractory metals such as thorium-containing tungsten, hafnium carbide, and hafnium nitride. The above-described clearance 100 also functions as a minute passage for allowing the mixture to pass therethrough, and brings the mixture into contact with a large amount of plasma arc efficiently, thereby significantly improving the decomposition efficiency of the mixture. Water vapor that does not come into contact with the plasma arc also exists in the plasma reaction chamber 76, and thus recombination of hydrogen and oxygen in the plasma reaction chamber 76 is prevented. The plasma reactor 16 is connected to the mixed liquid supply port 1 formed near the corner of the insulating casing 78.
02 and a plurality of compressed air injection ports 106. The mixture of the hydrogen-rich fuel and the compressed air is ignited in the combustor 18 to generate a high-temperature and high-pressure combustion gas.
Moisture inside evaporates instantly upon contact. At this time, the HC component in the mixed liquid A is mixed with the compressed air and burned. In this way, a high-mass, high-pressure working fluid is supplied from the jet passage 84 to the expansion turbine 20.

In FIG. 2 and FIG. 4, the expansion turbine 20
Includes a stator 110 fixedly supported by press fitting or other appropriate means in the inner cylinder 70, and a turbine rotor 112 housed rotatably therein and connected to the output shaft 34. The stator 110 includes an annular stator ring 114 and an arc-shaped stator blade 1 extending radially inward from a central portion thereof.
16. On the other hand, the turbine rotor 112 is first,
Second flywheel rotor disks 118 and 120 are provided. As is apparent from FIG. 4, the stators 110 each have a jet nozzle 122 that communicates with the jet passage 84.
And an outlet 126 communicating with an exhaust chamber 124 formed between the outer cylinder 68 and the inner cylinder 70.
A partition member 128 extends radially inward from the stator ring 114 between the jet nozzle 122 and the outlet 126, and includes a jet stream guide surface 130 facing the jet nozzle 122 and the outlet 126, respectively, and an exhaust guide surface 132. .

In FIG. 2 and FIG. 4, the turbine rotor 1
12 has an annular jet passage 134 formed between the first and second rotor disks 118 and 120 and communicating with the jet nozzle 122 and the outlet 126, in which the arc-shaped stator blade 116 and the partition member 12 are provided.
8 are stored. As is apparent from FIG. 5, the stator blade 116 is adjacent to the jet nozzle 122 and deflects the jet stream S to the first and second rotor disks 118 and 120.
16a, a blade opening / closing section 116b for periodically interrupting the jet flow, and a plurality of auxiliary deflection guide sections 116c formed at intervals in the circumferential direction. The auxiliary guide portion 116c includes first and second rotor disks 118 and 12
With respect to 0, the jet flow passing through the annular jet passage 134 is deflected in the rotational direction to the first and second rotor disks 118 and 120 to collide many times and improve the turbine efficiency. Main deflection guide 1
The stator blade 116a and the auxiliary deflection guide portion 116c may be formed on the independent pieces by dividing the stator blade 116 into a plurality of pieces. Blade opening / closing section 116
b instantaneously shuts off the jet passage periodically, stops the jet flow on the first and second rotor disks 118 and 120 to generate a force due to inertial force and reaction, and causes the rotor disks 118 and 120 to rotate. Then, when the blade opening / closing portion 116b suddenly releases the pressure, the jet flow is accompanied by inertia force from the auxiliary deflection guide portion 116c to the rotor disks 118 and 120 again. The purpose is to increase the output of the turbine 20 by giving a strong impulse.

In order to meet the above-mentioned purpose, the first and second rotor disks 118 and 120 are provided with flywheel disks 136 and 138 which are arranged at intervals in the axial direction, respectively.
Is provided. The flywheel disks 136 and 138 respectively have cylindrical bases 140 and 142 mounted on the output shaft 34.
, And the connection bolt 144 penetrates these. The bolt 144 extends between the flange 146 of the output shaft 34 and the holding flange 148 and
And the expansion turbine 20 are held at predetermined positions. FIG.
4 and 5, the flywheel disk 136,
138 are a plurality of turbine blades 15 having a plurality of arc-shaped cross sections which are arranged at intervals in the circumferential direction and extend in the axial direction.
0, 152. Turbine blades 150, 152
Each have an arcuate blade surface and an arcuate back surface against which the jet stream impinges, and adjacent radial or valve surfaces 150a, 150a, 150a along the annular jet passage 136.
52a. As described above, the rotor disk 11
8, 120 with respect to the blade opening / closing portion 116b of the stator blade 116, the turbine blades 150, 1
When the valve surfaces 150a and 152a of the 52 periodically engage or overlap with each other, the jet flow is suddenly cut off, and the pressure of the jet flow in the blades 150 and 152 rises sharply to transfer rotational energy to the flywheel disks 136 and 138. accumulate. When the valve surfaces 150a, 152a are opened from the blade opening / closing portion 116b, the high-pressure jet flow accumulated in the blades 150, 152 is released at a stretch and is guided by the auxiliary deflection guide 116c, so that the next stage blade 150 , 152. In this way, the jet stream gives a strong torque to the turbine blades 150, 152 sequentially while passing through the annular jet passage 134, and this rotational energy is stored in the flywheel disks 136, 138. in this way,
The energy conversion efficiency of the jet stream is extremely high, and the turbine efficiency is significantly increased. In this manner, the jet stream expands and extends from outlet 126 to exhaust chamber 124.
The expansion gas 36 is discharged from the exhaust port 160 in FIG.
To a condensate 22, where it is cooled to produce a mixed fluid 38 of condensed water and helium gas. The mixed fluid 38 is introduced into the high-pressure pump 24 through an introduction port 162 formed in the engine housing 66.

In FIG. 2, FIG. 4, and FIG. 6, a flywheel compressor 24 includes a stator 164 press-fitted concentrically with the stator 110 in an inner cylinder 70, and a pair of rotor disks 166 rotatably housed therein. , 168. The stator 164 includes an annular stator ring 172, an arc-shaped stator guide 174 and a partition member 176 extending radially inward from a central portion thereof. The stator 164 includes a suction port 178 adjacent to the arch-shaped guide surface 176a of the partition member 176, and a discharge port 180 adjacent to the arch-shaped guide surface 176b. The discharge port 180 is the air preheating chamber 8
0 and communicates with the above-mentioned combustor 18. 4 and 6, the stator guide 174 extends between the suction port 178 and the discharge port 180, is adjacent to the suction port 178, and sends air from the air filter 23 (see FIG. 1) to the rotor disks 166, 168. A deflection guide portion 174a for deflecting to the side, a plurality of bucket opening / closing portions 174b, and a plurality of arch-shaped bypass passages 174c are provided. The rotor disks 166 and 168 are fixedly supported on the output shaft 34 by bolts 144 and have an annular groove 182 in which the stator guide 174 is housed. Rotor disk 1
66 and 168 are flywheel disks 18 respectively
4, 186 and flywheel disks 184, 186
A plurality of arc-shaped rotor blades 184a and 186a are formed at intervals in the circumferential direction and extend in the axial direction. The concave portions of the rotor blades 184a and 186a face in the rotation direction. Rotor blades 184a, 18
The axial end of 6a extends radially along the annular groove 182 and periodically engages or overlaps the bucket opening and closing section 174b to prevent fluid from returning. Rotor 1
When the 70 rotates, the air at the inlet 178 is
a, 186a, and are directed from the guide portion 174a to the rotor blades 184a, 186a at the subsequent stage, flow into the rotor blades 184a, and are trapped. That is, the air is forcibly supplied to the space between the adjacent rotor blades by the interaction between the guide portion 174a and the rotor blades 184 and 186a, and from there to the downstream rotor blade via the bypass passage 174c. Can be In this manner, the air is continuously pumped at a high pressure to the discharge port 180.
The compressor 24 has a flywheel effect for storing rotational energy of the expansion turbine 20 in addition to the compression action.

[0022]

As is clear from the above, according to the ultra-low fuel consumption type gas turbine of the present invention and the mechanical system driven by the same, air pollution and global warming can be effectively reduced and oil resources are depleted. Contribution as a petroleum alternative energy system that can solve the gasification problem.

[Brief description of the drawings]

FIG. 1 is a block diagram of an ultra-low fuel consumption gas turbine and mechanical system according to a preferred embodiment of the present invention.

FIG. 2 is a partial cross-sectional view of the gas turbine of FIG.

FIG. 3 is a sectional view taken along line III-III in FIG. 2;

FIG. 4 is a sectional view taken along the line IV-IV in FIG. 2;

FIG. 5 is a relationship diagram between a stator and a turbine rotor of the expansion turbine of FIG. 2;

FIG. 6 is a diagram showing a relationship between a stator and a rotor of the high-pressure pump of FIG. 2;

[Explanation of symbols]

10 gas turbine, 12 power system, 14
Mechanical system, 16 plasma reactor, 18 combustor, 20 expansion turbine, 24 flywheel compressor, 28 plasma power, 30 spark plug, 44 rectifier, 46 battery, 48 power converter, 50 motor generator, 52 rear wheel, 5
4 drive shafts, 56 front wheels

──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. ⁷ Identification symbol FI Theme coat ゛ (Reference) F02C 3/30 F02C 7/08 Z 7/08 F04D 29/26 F04D 29/26 H05H 1/24 // H05H 1/24 B60K 9/00 C

Claims (18)

[Claims] (A) hydrocarbon fuel supply means; (b) electrolyzed water supply means; (c) a compressor for supplying compressed air; and (d) hydrocarbon fuel and electrolyzed water in the presence of a plasma arc. A plasma reactor that decomposes gas to generate a mixed gas of steam and hydrogen-rich fuel; and (e) communicates with the compressor and the plasma reactor and burns the mixture of the compressed gas and the mixed gas to produce a high-temperature, high-pressure combustion gas. And (f) an expansion turbine that communicates with the combustor and expands the high-temperature and high-pressure combustion gas to obtain power and drives a compressor. 2. The air preheating chamber according to claim 1, further comprising: an air preheating chamber formed between the plasma reactor and the combustor.
An ultra-low fuel consumption type gas turbine comprising a plurality of injection nozzles extending between an air preheating chamber and a combustor, wherein compressed air is preheated in the air preheating chamber and supplied to the combustor via the injection nozzle. 3. An ultra-low fuel consumption gas turbine according to claim 2, further comprising means for supplying electrolytic water to the injection nozzle. 4. The plasma reactor according to claim 2, wherein the plasma reactor includes a plasma reaction chamber, and a microplasma generating unit disposed therein, and the plasma reaction chamber includes a plurality of mixed gas injection ports that open to the combustor. Super low fuel consumption gas turbine. 5. The gas turbine according to claim 1, wherein the expansion turbine includes a stator and a flywheel turbine rotatably housed in the stator. 6. The gas turbine according to claim 5, wherein the compressor comprises a stator and a flywheel impeller rotatably housed in the stator. 7. The method according to claim 4, wherein the microplasma generating means comprises a plasma electrode disposed in the plasma reaction chamber, and a mixture of a solid electrode body and a solid insulator filled in the plasma reaction chamber. The mixing ratio is 1: 1.5-1.
An ultra-low fuel consumption gas turbine defined in the range of 5: 1. 8. A hydrocarbon fuel supply means; (b) electrolyzed water supply means; (c) an engine housing; and (d) a hydrocarbon fuel and electrolysis disposed in the engine housing by plasma arc. A plasma reactor that decomposes water to generate a mixed gas of steam and a hydrogen-rich fuel; (e) a compressor that is disposed in an engine housing to generate compressed air; and (f) a plasma reactor in the engine housing. A combustor arranged to communicate and combust the mixture of the gas mixture and the compressed air to generate a high temperature and high pressure combustion gas; and (g) a high temperature and high pressure combustion gas arranged to be connected to the compressor in the engine housing. And an expansion turbine driven by the engine to obtain a power output. 9. The engine housing according to claim 8, wherein the engine housing includes first to third zones, a first zone houses a plasma reactor and a combustor, a second zone houses a compressor, and a third zone houses an expansion turbine. Ultra low fuel consumption type gas turbine housed. 10. The ultra low fuel consumption gas turbine according to claim 9, further comprising an air preheating chamber formed between the plasma reactor and the combustor in the first zone to preheat compressed air supplied from the compressor. . 11. The plasma reactor according to claim 8 or 9, wherein the plasma reactor communicates with the hydrocarbon fuel supply means and the electrolyzed water supply means, the minute plasma generation means arranged in the plasma reaction chamber, and the mixed gas. An ultra-low fuel consumption gas turbine having a fuel injection port for injecting into a combustor. 12. The flywheel turbine according to claim 9 or 10, wherein the expansion turbine comprises a flywheel turbine, wherein the flywheel turbine is disposed in the third zone, and a flywheel turbine rotor rotatably housed in the stator. Wherein the stator comprises guide means for deflecting the jet flow of the combustion gas, and blade opening / closing means for periodically interrupting the jet flow to increase the pressure thereof, wherein the flywheel turbine rotor is provided with guide means for the stator. And a turbine blade moving along the blade opening / closing means. 13. The turbine rotor according to claim 12, wherein the turbine rotor has an annular jet passage communicating with the combustor, the stator has guide means and blade opening / closing means, and has a stator blade arranged in the annular jet passage. An ultra-low fuel consumption gas turbine comprising turbine blades circumferentially spaced along an annular jet passage. (A) a hydrocarbon fuel supply means; (b) electrolyzed water supply means; (c) an engine housing; and (d) a hydrocarbon fuel and an electrolysis which are arranged in the engine housing and are plasma-arced. A plasma reactor that decomposes water to generate a mixed gas of steam and a hydrogen-rich fuel; (e) a compressor that is disposed in an engine housing to generate compressed air; and (f) a plasma reactor in the engine housing. A combustor arranged to communicate and combust the mixture of the gas mixture and the compressed air to generate a high temperature and high pressure combustion gas; and (g) a high temperature and high pressure combustion gas arranged to be connected to the compressor in the engine housing. (H) driven means driven by the expansion turbine to obtain a power output. Mechanical system. 15. The mechanical system according to claim 14, wherein the mechanical system comprises a moving body, and the driven means comprises a propulsion means. 16. The method according to claim 14, further comprising: (i) a generator driven by an expansion turbine;
(J) a mechanical system comprising: a plasma power supply connected to the generator for supplying plasma power to the plasma reactor. 17. A hydrocarbon fuel supply means; (b) electrolyzed water supply means; (c) an engine housing; and (d) an electrolysis of hydrocarbon fuel and plasma electrolysis by being arranged in the engine housing. A plasma reactor that decomposes water to generate a mixed gas of steam and a hydrogen-rich fuel; (e) a compressor that is disposed in an engine housing to generate compressed air; and (f) a plasma reactor in the engine housing. A combustor arranged to communicate and combust the mixture of the gas mixture and the compressed air to generate a high temperature and high pressure combustion gas; and (g) a high temperature and high pressure combustion gas arranged to be connected to the compressor in the engine housing. (H) a power generator driven by the expansion turbine to obtain a power output; (h) a power generator driven by the expansion turbine; Mechanical system comprising; a propulsion means driven by a (j) motor means; motor means and driven by the electrical output. 18. The rectifier according to claim 17, wherein the mechanical system comprises a moving body, the motor means comprises a motor / generator, and (k) a rectifier for converting an AC output of the generator into a DC output; A mechanical system comprising: a power converter connected between the rectifier and the motor means; and (m) a battery connected to the rectifier and the power converter for storing brake regenerative power of the moving object.