KR101668592B1 - Amphibious flying car - Google Patents

Abstract

BACKGROUND OF THE INVENTION 1. Field of the Invention [0002] The present invention relates to a submersible vehicle having a metal spherical shape and capable of traveling freely in water or in the air. Such a diving vehicle includes a body 100, which is a metallic sphere; A gas turbine engine 101 installed inside the vehicle body 100 to generate a thrust for forward flight when the vehicle body 100 meets the public airplane; A hydrogen ion engine 200 installed at a lower end of the vehicle body 100 for spraying plasma at a high speed using an ion beam so as to be a propellant in water during flight of the vehicle body 100; At least a pair of magenta permanent magnet sets (300a, 300b) installed at an upper end of the vehicle body (100) and cooled by liquid nitrogen to levitate and rotate the vehicle body (100); At least one pair of electromagnet coil guns 400a to 400d installed at a lower portion of the vehicle body 100 to generate ionized seawater and generate propulsive force using a magnetic force generated by the reaction, Front and rear electromagnet road wheels 500a and 500b fixed to the bottom of the vehicle body 100 and used for landing; A pair of flagpole blades (600a, 600b) formed so as to be hollow like the round bar and maintaining the air flight and level of the vehicle body (100) through upper and lower wings; A self-generating device (700, 700a) for generating electric power using a magnetic field and a sea water flow; And an operation and control unit 800 that maintains a waterproof function in the case of an underwater flight and a driver's seat rising upward to construct a shale during an air flight.

Description

{Amphibious flying car}

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to a submersible vehicle, and more particularly, to a submersible vehicle that can be operated underwater or in the air under the control of a driver.

Many transportation and leisure devices with excellent performance are developed and marketed due to the rapid development of the automobile, ship, and aircraft industries. However, the following problems have been obstructed in the specialization and popularization of leisure culture.

There is no device that generates a plasma acting as a protective film on the surface of a metal sphere which forms a car body of a general automobile or a submarine, and there is no apparatus which uses a high temperature plasma to generate ionic seawater as a conductor, and the existing wing produces a whirlpool whirlwind, And the vibration of the existing brake is dependent on the frictional force between the wheels and rails, the wear of the body is large, and the buoyancy control is carried out by entering and exiting the seawater from outside. There is no device for controlling the buoyancy by being built as a part of the body, Turbines and other rotating devices are needed, and they are heavy inside the bonnet, making them heavy and bulky.

SUMMARY OF THE INVENTION The present invention has been conceived to solve the above problems, and an object of the present invention is to provide a gas turbine engine for traveling, a permanent magnet rotor of a superconducting magnet in front of and behind a head of a vehicle body, It is intended to provide a submersible car capable of vertical launch with propulsion with an integrated ion engine.

It is another object of the present invention to provide an electromagnet rail that is installed on an ion beam of a hydrogen ion engine during an underwater flight and has an electromagnet rail mounted thereon and an electromagnet rudder drive shaft disposed along the electromagnet rail to rotate around the underside of the body, To provide a submersible vehicle capable of underwater flight by rotating 360 degrees.

It is a further object of the present invention to provide a safety device in which the electronic door is lowered into the driver's protective device shelter when the vehicle body is at rest and is shut off by a double door and the lower electrode of the driver's protective device and the upper surface of the electromagnet ejector are arranged at the same pole, The present invention is intended to provide a submersible vehicle in which a shelter is lifted up to the northclick intake port and separated from the vehicle body and can escape.

Yet another object of the present invention is to provide a diving vehicle capable of being charged directly in a vehicle body by generating self-generated electricity using a self-generating device during underwater flight.

In order to accomplish the above objects, the present invention provides a diving vehicle comprising: a vehicle body (100) having a metal spherical shape; A gas turbine engine 101 installed inside the vehicle body 100 to generate a thrust for forward flight when the vehicle body 100 meets the public airplane; A hydrogen ion engine 200 installed at a lower end of the vehicle body 100 for spraying plasma at a high speed using an ion beam so as to be a propellant in water during flight of the vehicle body 100; At least a pair of magenta permanent magnet sets (300a, 300b) installed at an upper end of the vehicle body (100) and cooled by liquid nitrogen to levitate and rotate the vehicle body (100); At least one pair of electromagnet coil guns 400a-400b installed at a lower portion of the vehicle body 100 to generate ionized seawater and to generate propulsive force using a magnetic force generated by the reaction, Front and rear electromagnet road wheels 500a and 500b fixed to the bottom of the vehicle body 100 and used for landing; A pair of flagpole blades (600a, 600b) formed so as to be hollow like the round bar and maintaining the air flight and level of the vehicle body (100) through upper and lower wings; A self-generating device (700, 700a) for generating electric power using a magnetic field and a sea water flow; And an operation and control unit 800 that maintains a waterproof function during underwater flight and a driver seat rising upward to construct a shale during an air flight.

The submersible vehicle according to the present invention has the following effects.

First, the body of the diving airplane is a metal spherical body, a gas turbine engine is used for traveling, a permanent magnet rotor for superconducting magnet is installed at the front and rear of the head of the body, and a propellant Vertical launch is possible.

In addition, in the case of underwater flight, a rotating disk is installed on the hydrogen ion engine ion beam, and an electromagnet rail is installed thereon, and an electromagnet rudder drive shaft is installed along the electromagnet rail to rotate around the bottom water of the vehicle body. I can fly.

In addition, when the vehicle body is at rest, the electronic door is lowered into the driver's protective device shelter and shut off at the double doors, the lower electrode of the driver's protection device and the upper surface of the electromagnet ejector are arranged at the same pole, So that it can separate from the vehicle body and escape.

In addition, self-generated electricity can be generated directly from the vehicle body by using the self-generating device during underwater flight.

FIG. 1 is a perspective view showing the entire outline of a body of a metal sphere of a diving flying vehicle according to a preferred embodiment of the present invention.
2 is a view for explaining generation of plasma on the surface of a body of a metal sphere of a diving flying vehicle according to a preferred embodiment of the present invention.
3 is a view for explaining a structure of a hydrogen ion engine provided in a diving vehicle according to a preferred embodiment of the present invention.
FIG. 4A is a view for explaining the structure of a superconductor marquee permanent magnet provided in a diving vehicle according to a preferred embodiment of the present invention; FIG.
FIG. 4B is a diagram illustrating a detailed structure of a superconducting permanent magnet of a diving flying vehicle according to a preferred embodiment of the present invention; FIG.
FIGS. 4C and 4D are views for explaining a structure of a cylindrical permanent magnet of a superconductor marquee permanent magnet provided in a submersible vehicle according to a preferred embodiment of the present invention.
5 is a view for explaining the structure of an electromagnet coil gun in a diving vehicle according to a preferred embodiment of the present invention.
6A and 6B are views for explaining the operation of an electromagnet road wheel, an electromagnet rail and a rudder provided in a diving vehicle according to a preferred embodiment of the present invention.
FIGS. 7A and 7B are views for explaining the operation of the flagpole wing of the diving flying vehicle according to the preferred embodiment of the present invention when lifting and lowering the flagpole.
FIGS. 8A and 8B are views for explaining a self-power generation apparatus provided in a diving vehicle according to a preferred embodiment of the present invention.
FIG. 9 is a view for explaining the operation of an operator seat protecting apparatus shelter and an electromagnet ejecting apparatus provided in a dive flying vehicle according to a preferred embodiment of the present invention.
10A and 10B are views for explaining the operation of the electromagnet eddy current disk and the permanent magnet eddy current of the diving vehicle according to the preferred embodiment of the present invention.
11 is a view illustrating a process of constructing a driver's seat and a control unit provided in a dive flying vehicle according to a preferred embodiment of the present invention with a shale.

The terms and words used in the present specification and claims should not be construed to be limited to ordinary or dictionary meanings, but the inventor may appropriately define the concept of the term to describe its invention in the best way Can be interpreted as meaning and concept consistent with the technical idea of the present invention.

It should be noted that the embodiments described in this specification and the configurations shown in the drawings are merely preferred embodiments of the present invention and do not represent all the technical ideas of the present invention, It should be understood that various equivalents and modifications may be present.

FIG. 1 is a perspective view showing a general outline of a body of a metal sphere of a diving flying vehicle according to a preferred embodiment of the present invention. FIG. 2 is a perspective view of a vehicle body of a diving flying vehicle according to a preferred embodiment of the present invention. FIG. 2 is a view for explaining that a plasma is generated in FIG.

1, a diving vehicle according to the present invention includes a body 100, which is a metallic sphere, and a thrust for forward flight when the body 100 is in the airborne state, provided inside the body 100, A hydrogen ion engine 200 installed at a lower end of the vehicle body 100 for injecting plasma at a high speed using an ion beam so as to become a propellant underwater during underwater flight of the vehicle body 100, At least a pair of magenta permanent magnet sets 300a and 300b installed at an upper end of the vehicle body 100 and cooled by liquid nitrogen to levitate and rotate the vehicle body 100 and a pair of permanent magnet sets 300a and 300b installed at a lower portion of the vehicle body 100 At least a pair of electromagnet coil guns 400a-400b for passing through the ionized water and firing at the tail to generate a propulsive force by using magnetic force generated by the reaction, The front and rear electromagnet road wheels 50 A pair of flagpoles (600a, 600b) which are formed so as to be hollow like a whorl and which keep the airplane of the vehicle body (100) and the level thereof horizontal through the upper and lower wings, And an operation and control unit 800 for maintaining a waterproof function during underwater flight and a driver seat rising up to an upper part during an air flight.

As shown in FIG. 1, a rear upper bore 150a and a lower front breeze 150a, which are respectively installed in the rear and bow of the vehicle body 100 so that a predetermined amount of air can be injected or moved, 150b for selectively controlling the air movement path of the baffle line 160, the rear upper baffle 150a and the front lower baffle 150b for connecting the rear upper baffle 150a and the front lower baffle 150b to each other, A valve 170; And a buoyancy-adjusting piston 180 for adjusting the buoyancy by supplying or removing air to or from the rear upper boom 150a or the front lower boom 150b.

Hereinafter, the buoyancy adjusting operation at the time of underwater flight, underwater submersion, and water float will be described.

First, when the underwater flight is performed, the rotational motion of the electric motor is converted into the reciprocating motion of the buoyancy adjusting piston 180 so that the air flows along the inclination of the vehicle body 100 through the bore line 160 to the rear upper breeze or the lower front breeze 150a, 150b so that the buoyant force of the vehicle body 100 can be adjusted to freely move into the water or to maintain the horizontal position.

The buoyancy adjusting piston 180 is pulled backward by the electric motor to draw air in the front lower end bobbin 150b to adjust the check valve 170 to close the front lower end bobbin 150b and to close the rear upper bobbin 150a, The buoyancy adjusting piston 180 is pushed forward and the air is injected into the rear upper baffle 150a so that the front weight of the body 100 is heavy so that the body 100 can be tilted downward to be submerged .

On the other hand, when the water level is raised, the buoyancy adjusting piston 180 is pulled backward by an electric motor to draw air in the rear upper bail 150a, close the rear upper bail 150a using the check valve 170, The buoyancy adjusting piston 180 is pushed forward and the air is injected into the front lower end bobbin 150b so that the front weight of the body 100 is lightened so that the body 100 is lifted in the water surface direction can do.

Therefore, when the driver moves the buoyancy adjusting piston 180 in the forward direction or the backward direction, the buoyancy can be controlled by pushing out or extracting the air contained in the cylinder through the bore line 160.

Here, the breeze has positive buoyancy (float in water), negative buoyancy (sinking in water), and neutral buoyancy (neither float nor sink in water). The wheel can adjust the specific gravity of the body 100 and match the specific gravity of the body 100 with the specific gravity of the surrounding water. The breeze is a thin airbag in the vehicle body 100 and is used as a braking device of the vehicle body 100 to adjust its buoyancy to fly underwater and control diving and injuries. It is a buoyancy regulator that adjusts to where it goes down or where it can go and tells the balance. The driver can adjust the buoyancy control piston (180) to enter deep water or float again.

Here, the size of the body 100 is the size of a medium sized passenger car, the body length is 6 m, the maximum takeoff weight is 600 kg, and the weight of the body 100 in water is reduced to 1/3 of that in water.

The vehicle body 100 further includes a spherical electromagnet ring fixed shaft 110, a spherical electromagnet ring 120 fixed to the outer surface of the electromagnet ring fixed shaft 110, A plurality of protrusions 130 protruding outward from the surface and having an upper end mushroom shape 131 coated with oil and having a plurality of fine holes 133 formed on the surface thereof and a plurality of protrusions 130 formed on an inner surface of the electromagnet fixing shaft 110 And a plurality of pistons 140a and 140b.

The liquid nitrogen 111 compressed through the fine holes 133 formed in the rough and strong waterproof mushroom-shaped oil coating surface 131 formed at the upper end of the protrusion 130 protruding from the surface of the body 100, And it is rotated by the large electromagnet ring 120 to obtain plasma steam without heating as in the prior art.

That is, when the large electromagnet ring 120 is rotated at a high speed while the compressed liquid nitrogen is ejected at a high speed by using the pistons 140a and 140b in the outward direction from the inside of the vehicle body 100, the compressed liquid nitrogen is heated A high-pressure plasma can be generated to generate a vapor cushion. A plurality of fine holes 133 formed in a mushroom-shaped oil coating surface 131 formed on the upper end of a plurality of protrusions 130 protruding from the surface of a vehicle body 100, which is a metal body, The plasma is generated without being heated.

Such a technique is applied by Ivan Bakarelsky, an engineer at the King Abdullah Institute of Clean Burning Research Center in Saudi Arabia, that boils water without bubbles if the surface is treated specially to prevent the steam cushion from collapsing.

The operation of generating such a plasma will be described in detail with reference to FIG.

The liquid nitrogen is compressed as it is pushed into the mushroom-shaped oil-coated surface 131 from the liquid nitrogen source container to compress the liquid nitrogen using the pistons 140a and 140b.

Accordingly, since the internal pressure of the pistons 140a and 140b is increased, the inflow valve of the inflow pipe through which the liquid nitrogen passes is closed to block the inflow of liquid nitrogen, while the outflow valve of the outflow pipe is opened, Can escape outwardly.

On the other hand, when the pistons 140a and 140b return to their original positions, the internal pressures of the pistons 140a and 140b are lowered, so that the opening and closing of the outflow pipe and the inflow pipe are reversed and liquid nitrogen is input again.

On the other hand, when the pistons 140a and 140b are compressed, the pressure inside the pistons 140a and 140b is pushed into the mushroom-shaped oil coating surface 131 to compress the liquid nitrogen. Therefore, the pressure of the liquid nitrogen contained in the pistons 140a and 140b is increased, whereby the liquid nitrogen is poured out to the outlet pipe.

On the other hand, in order for liquid nitrogen pumped into the outflow pipe to be injected into small particles such as mist, the portion where the liquid nitrogen is discharged is formed as a fine-injected snorkel exhaust hole and is blown out like a small bubble (foam, bubble) It can be discharged into water. When the snorkel exhaust hole serving as the nozzle is connected to the outflow pipe, the fine holes 133 obstruct the flow of the liquid nitrogen, so that the liquid nitrogen directed toward the nozzle has to push the pistons 140a and 140b to a large pressure. When the liquid nitrogen pushed at high pressure is pushed into a narrow hole, it can be misty liquid nitrogen because it collides with sea water.

Here, liquid nitrogen is a liquid having a high fluidity and flowability, and the reason why the wall surface is rotated longer than ordinary liquids is due to the Raiden Frost effect. In addition, liquid nitrogen is smaller in molecular size than water, allowing water to pass through or through where it does not. If the surface is treated specially so that the steam cushion does not collapse, it can boil the water without bubbles and the key is to make the surface very repulsive to the water. And then sprayed with liquid nitrogen through the fine holes 133, and these super hydrophobic spheres were sprayed on the rotating force of the large electromagnet ring 120 Lt; / RTI >

On the other hand, liquid nitrogen is a material obtained by liquefying nitrogen which occupies 78% of the air. For example, when 2 g of hydrogen gas is burned, a calorific value of 57.72 cal / mo is generated, so that the underwater unit expands. When hydrogen gas comes in contact with air at 1 degree at 0 degree, it explodes by flame. The solid hydrogen density is like a column, and the column shape is burned in the most efficient and constant manner.

3 is a view for explaining a structure of a hydrogen ion engine provided in a diving vehicle according to a preferred embodiment of the present invention.

3, the hydrogen ion engine 200 according to the present invention includes a solid hydrogen fuel cell 210 and a hydrogen-releasing reactor 210 for discharging the solid hydrogen 201 discharged from the solid hydrogen fuel cell 210, An injector-type piston 230 disposed in the middle of the hydrogen-releasing reactor 220 to control the inflow or outflow of the solid fuel by adjusting the internal pressure of the hydrogen-releasing reactor 220, An arc igniter 250 for igniting an arc in the combustion chamber 240; an oxygen supplying nozzle 260 for supplying oxygen to the arc igniter 250; A discharge chamber 270 in which solid hydrogen burned in the combustion chamber 240 performs arc discharge in which strong light and high temperature heat are generated, a compressed air supply unit 280 that supplies compressed air to the discharge chamber 270, , A plasma generated in the arc discharge of the discharge chamber 270 is injected It consists of a small ion engine ion beam (290).

Here, the solid hydrogen used in the hydrogen-ion engine 200 is applied to the hydrogen-releasing reactor continuously by forming the ammonia blanth in the form of a small thumb-sized pill.

Magnesium is attracting attention as a solid reservoir of hydrogen because it has a strong binding force with hydrogen. Magnesium particles are divided into nanometers. Magnesium in the form of nanopowder has a working environment of 200-300 Even hydrogen atoms can be easily inserted and removed. Using this technology, 4 kg of hydrogen can be stored in a solid fuel state.

3, the hydrogen ion engine 200 is configured such that the solid hydrogen 201 is put in the flame arc 251 generated between the electrodes and heated in the combustion chamber 240, (260).

That is, in the preferred embodiment of the present invention, electric energy is converted into kinetic energy without converting it into heat energy and used. The hydrogen gas ejected to the hydrogen ion engine ion beam 290 is similar to a plasma engine because the plasma state is used but the nature of the plasma is not used at the time of acceleration, but the principle is different. Plasma engines use a gas to be used as a propellant by means of an electric method, and a plasma is produced by accelerating the plasma directly to an electromagnet. Solid hydrogen (201) has the disadvantage that it can not stop the reaction once the rocket using solid propellant is ignited, but it is also easy to store and handle. Metallic aluminum powder and magnesium powder are used as the solid fuel.

In the preferred embodiment of the present invention, the hydrogen ion engine 200 does not generate thrust continuously for a long time, but generates a thrust for a short time every time it is needed. This method can be used because it uses very little fuel and reduces engine damage. Solid hydrogen Ammonia Boran is a white solid hydrogen, and hydrogen contained in the amount of a thumb can generate a high capacity electric power. The solid hydrogen ammonia borane is formed in the form of a small pill and continuously supplied to the hydrogen releasing reactor 220. The solid hydrogen 201 applies the principle of the atomizing piston 230 upon injection into the combustion chamber 240. The piston 233 is pushed inward by the electric motor 231 and the compression spring 237 in the cylinder 235 is compressed. As a result, the internal pressure of the pump provided in the hydrogen discharge reactor 220 is increased and the inlet valve 221 of the solid hydrogen is closed to block the hydraulic pressure of the solid hydrogen 201. The outlet valve of the solid hydrogen is opened, The solid hydrogen 201 is discharged.

At this time, when the piston 233 is returned to its original position by the compression spring 237, the pressure in the pump is lowered, so that the open / closed state of the solid hydrogen outflow valve 223 and the inflow valve 221 is reversed. Therefore, as the pressure of the solid hydrogen 201 in the pump becomes higher, the solid hydrogen 201 can be discharged through the outlet valve 223.

3, the nozzle 260 is connected to the outlet valve 233, as shown in FIG. 3, because the nozzle 201 is required to have a narrow hole for injecting the solid hydrogen 201 pumped through the outlet valve 223 into a cylindrical shape. The narrow hole in the solid hydrogen 201 interferes with the flow of the solid hydrogen 201, so that the solid hydrogen 201 directed toward the nozzle 260 must be pushed out to a large pressure by the pump.

At this time, the solid hydrogen pushed through the high pressure is blown outward through the narrow hole of the nozzle 260.

The arc igniter 250 is composed of a power cable through which a direct current flows and a circuit breaker 253 for switching and controlling the power supply. One cable is connected to the negative side of the power source and the other is connected to the positive side Through the circuit breaker 253 to the clamp or ground clamp.

In the embodiment of the present invention, the heat of the arc flame is maintained at 6,000 to 10,000 degrees. The principle of the arc is to convert the electric power into arc and dissolve the solid hydrogen 201 with the heat.

In the embodiment of the present invention, when the two electrodes having an appropriate voltage are brought into contact with each other and then dropped, a spark is generated between the electrodes. At this time, a gas or metal vapor is generated, This is an arc discharge phenomenon in which high temperature heat is generated. The arc is surrounded by a core wire and the material of the part causing discharge in the arc discharge becomes a plasma state. The arc discharge is a state in which a discharge is large while a gaseous state (plasma) with high electric conduction is maintained as a large current discharge state.

In the preferred embodiment of the present invention, the hydrogen ion engine 200 for generating a plasma uses sugar and potassium nitrate solid hydrogen pellets, and the nitrate calmroom serves to transfer oxygen while burning the sugar.

In a preferred embodiment of the present invention, the hydrogen ion engine 200 has the characteristic of generating propulsive force through the momentum conservation law using an ion (charged particle or molecular) beam and accelerating ions in the electric field direction.

The fuel for generating the plasma in the hydrogen ion engine 200 is solid hydrogen 201 which is injected in a solid state into the combustion chamber 240 and then injected into the combustion chamber 240 as solid hydrogen The N + S + N single pole is placed on the inner wall, and the hydrogen gas can easily separate the plasma by the magnetic field.

In a preferred embodiment of the present invention, the solid hydrogen fuel is not corrosive and does not need to be stored at a low temperature, and can be continuously stored in a pre-installed state at the time of manufacture. In addition, since the pump, the control tool, the combustion chamber, and the like are not separately required, the structure is simple, and the propulsion can be provided for a long time.

Further, the driver can control the output by adjusting the amount of combustion by using the piston 233. [

In the state where the hydrogen ion engine 200 generates flame by arc discharge, when the solid hydrogen rushes from the cylindrical fuel tank into the lower portion, the driver uses the piston 233 of the compressed air supply unit 280 to perform fine injection By passing compressed air through the perforated metal plate, the passing speed of the hydrogen ions can be rapidly processed to obtain the driving force.

FIG. 4A is a view for explaining the structure of a superconductor marquee permanent magnet provided in a diving vehicle according to a preferred embodiment of the present invention; FIG. FIG. 4B is a diagram illustrating a detailed structure of a superconducting permanent magnet of a diving flying vehicle according to a preferred embodiment of the present invention; FIG. FIGS. 4C and 4D are views for explaining a structure of a cylindrical permanent magnet of a superconductor marquee permanent magnet provided in a submersible vehicle according to a preferred embodiment of the present invention.

4A, four sets of superconductor permanent magnet sets 300a and 300b according to the present invention are installed in upper, lower, left, and right directions on the upper end of the vehicle body 100. The superconductor permanent magnet sets 300a and 300b The number of blades of the rotary shaft to be installed is preferably twelve.

As shown in FIG. 4B, liquid nitrogen (below -90 degrees Celsius) is poured into the superconductor 330a contained in the liquid nitrogen container 360 to cool the superconductor 330a, When the disc 300 is placed on the undersurface of the permanent magnet 310, the magenta permanent magnet 310 and the superconductor 330a located below the disc 380 repel each other and eventually the disc 380 floats.

The scientific principle in which the disk is lifted in this way is similar to the generation of magnetic force when electricity flows. That is, when a current is passed through a superconductor, the current is generated by the current, which travels around the superconductor as it moves. Therefore, superconducting magnets can be made using the properties of superconductors with quantum anchoring (superconducting magnet binding) and flux spinning (magnetic flux confinement), and moving objects can be made floating by levitation.

4A to 4D, a description will be given in detail of an operation in which the magenta permanent magnet and the superconductor repel each other and become levitation rotation.

In a preferred embodiment of the present invention, as shown in FIG. 4B, the liquid nitrogen container 360 is placed on the superconductor 330a and the superconductor 330a, which is contained in the liquid nitrogen container 360, And then the superconductor 330a is cooled by pouring the superconductor 330a into the superconductor 330a to place the superconductor 330a on the top of the superconductor 330a, And the superconductor 330a repel each other to eventually cause the disk 380 to float.

That is, the superconductor 330a is placed in a liquid nitrogen container 360, a liquid nitrogen container lid 370 or a wooden plate is placed thereon, and finally, a magical permanent magnet 310a is placed on the upper surface of the supercoat 330a. And poured into the nitrogen container 360.

The magnetic force of the magenta permanent magnet 310a penetrates through the superconductor 330a before the liquid nitrogen 361 is poured to form the superconductor 330a. When the superconductor 330a is in a cooled state, the magnetic force of the magic permanent magnet 310a is applied to the superconductor 330a. The superconductor 330a and the magenta permanent magnet 310a pull each other and are pushed against each other by a semi-magnet due to the Meissner effect. Using this principle, it is possible to make a magical permanent magnet rotating at high speed.

At this time, when the superconductor 330a is rotated, a strong magnetic levitation force acts on the direction perpendicular to the rotation direction, so that the superconductor 330a is levitated.

For such levitation, the size and intensity of the permanent magnet must be large, and the permanent magnet should have a ring-shaped symmetrical structure. The disk 380 does not rotate unless it is a ring symmetrical type.

In a preferred embodiment of the present invention, it is desirable to make a piece of permanent magnet to be circular when the magical permanent magnet is formed on the underside of the disk. That is, in order to make an annular disc by attaching a plurality of permanent magnets and to rotate the disc at the top of the superconductor 330a, the magnetic force of the entire magnet ring must be the same pole. To increase the magnetic levitation force between the superconductor and the permanent magnet, The contact area should be wide. That is, many permanent magnets must be attached to the bottom of the disk, and many superconductors should be placed in the cooling vessel.

In a preferred embodiment of the present invention, as shown in FIG. 4D, arranging the twelve magenta permanent magnet rotors 311a-311l to cross at the same pole diagonally makes it possible to produce a magnetic force line distribution in which the superconductor stably floats.

At the initial start, the magenta permanent magnet 310 (310a-310h) arranged at the bottom of the liquid nitrogen container 360 in a regular rule is driven to rotate the electric motor 320a. When the electric current is supplied, magnetism is generated by the electric current , The magnet rotates along with the magnetized permanent magnet (310) as it moves. When the sparking permanent magnet 310 starts to rotate, the sparking permanent magnet 310 can be continuously rotated even when the power of the electric motor 320a is cut off.

The power source is used to initially rotate the superconductor 330a and when the superconductor 330a attached to the upper end does not operate, the power of the electric motor 320a is applied to the sparking permanent magnet 310 located under the superconductor, When the superconductor 330a is cooled by using liquid nitrogen (below minus 190 degrees Celsius) and a current is supplied, magnetism is generated by the current, which moves together with the superconductor 330a.

The superconductor 330a trapped in the permanent magnet ring floats on top of the superconducting annular permanent magnet. This levitation is due to the Meissner effect of the superconductor, and the superconductor 330a can be rotated if a slight force is applied to the superconductor 330a. When the superconductor 330a is positioned at the center of the loop of the permanent magnet and liquid nitrogen is poured thereon, the superconductor 330a is lifted up again, and the superconductor 330a stands in the hollow space of the empty space and floats. This phenomenon is not due to the Meissener's semi-magnetic property but to the magnetic force generated in the penetration into the superconductor 330a. At this time, the magnetic force trapped in the superconductor 330a forms a permanent magnet and a magnetic field, and two objects coupled with a string of a strong magnetic force do not fall off even if they exert an external force. This is called the "string of magnetic force" phenomenon. Although the magnetic attraction is not found in all superconductors, most oxide superconductors, including compound superconductors, are known as type 2 superconductors. Superconductors are semi-magnetic materials and can repel even in weak magnetic fields of permanent magnets, thus allowing levitation without a strong magnetic field. Thus, when the temperature of the liquid nitrogen in the superconductor rises from the outside, the superconductor is stopped and the permanent magnet located on the bottom of the superconductor is rotated by the electric motor power instead of the superconductor in the direction of the corresponding power, So that the superconductor can be rotated.

The core of superconductors is the inverse effect of natural relativity, which can be obtained through mechanical devices. This anti-gravity effect is a side effect of Einstein's general relativity theory that "rotating objects distort gravity" It is estimated.

As shown in FIG. 4C, the superconducting magenta permanent magnet 310 is triple-structured in that the cylindrical permanent magnet 313 is attached to the cylindrical permanent magnet 313 in two layers around the cylindrical permanent magnet 313 to generate a semi-gravity force, Twelve small cylindrical permanent magnets 313b are uniformly adhered to the periphery of the permanent magnets 313 and arranged in the same manner on the outside thereof to form a triple magnet model. At this time, when the middle cylindrical permanent magnet 313b is rotated by the electric motor, twelve cylindrical permanent magnets 313 and cylindrical permanent magnets 313b are rotated together to generate electric power at the outermost side, The liquid nitrogen is cooled in the superconductor 330a contained in the liquid nitrogen container 360 lying on the bottom surface of the permanent magnet 310 so that the sparking permanent magnet 310 and the superconductor 330a repel each other and rotate levitating.

Meanwhile, as shown in FIG. 4C, the arrangement of the superconducting magenta permanent magnets 310 is such that a plurality of permanent magnets 315a-315h are arranged in a square shape so as to be equal to each other in the horizontal, vertical, or diagonal directions.

Pneumatic levitation and rotation can be performed in the state where a superconductor formed by pouring liquid nitrogen into the center of the annular permanent magnet 310 is placed on the center of the permanent magnet. Therefore, magnetic levitation can not occur if the magnets are not matched to each other, because the magnet distribution of the permanent magnets has a constant shape.

The magenta permanent magnet 310 is connected to twelve permanent magnets. When a magnet is constituted, a magnetic force distribution is produced, and the superconductor can be stably contained in the shape.

On the other hand, if you just take the superconductor in liquid nitrogen and take it out and bring it close to the magnet, you can see that the magnetism effect pushes the magnet and superconductor together. This phenomenon is called power-free condition, which is called flux spinning. When a superconductor is cooled, a magnet and a superconductor are brought close to each other (not contacted) The magnetic field of the magnet passes through the superconductor, and if the temperature falls below the critical temperature, the magnetic field may become trapped in the superconductor. In this case, the superconductor and the superconductor are attracted by the trapped magnetic net, The superconductor is cooled in liquid nitrogen (361), the cooled superconductor is placed on the neodymium permanent magnet, and the neodymium permanent magnet is made to cross the n-pole and the s-pole 12. Place the cooled superconductor on a permanent magnet. When raised, it is easy to levitate with a magnet arranged in a certain rule or an annular magnet.

On the other hand, if the superconductor deviates from the critical temperature, it loses its superconducting phenomenon and sits down. Because of the spin-spinning effect, superconductors also rise along with the magnet. If the temperature of the semiconductors is suddenly lowered, they become superconductors, and the superconductors are weak enough to push them down. The better the characteristics of the permanent magnet, the greater the magnetic levitation force the closer the distance between the superconductor and the permanent magnet is.

1, the superconductor permanent magnet set 300a and the aft superconductor permanent magnet set 300b rotate in opposite directions to each other, but the superconductor permanent magnet set 300b serving as one of the tandem rotors has an upward direction And the other is turned in the opposite direction, so that it is inclined in the opposite direction so that the lift can be generated in the upward direction.

The front superconducting magic permanent magnet set 300a and the aft superconductor permanent magnet set 300b provided at the upper end of the vehicle body 100 become tandem rotors and rotate in opposite directions to cancel the rotational force but the rotational direction of the tilted tandem rotor Because of the opposite, the flow of airflow can equally float upside down by reaction.

Two superconducting magic permanent magnets installed at the upper end are operated by the setting of the computer provided in the adjustment and control room 800. [ Two superconducting marques are driven at a permanent magnet speed and are rotated clockwise or counterclockwise to the upper rear portion of the vehicle body 100. The superconducting magic permanent magnet set 300a, 300b is cooled by liquid nitrogen and can be adjusted in forward and backward direction at high temperature. When cooled, the speed is fast and stops when the temperature is high. When the speed of the upper end front superconducting magic permanent magnet set 300a is reduced, the speed of the aft superconductor permanent magnet set 300b is increased and the tail is lowered by air floating. When the speed of the upper end aft superconductor permanent magnet set 300b is reduced , The front superconducting magic permanent magnet set 300a increases in speed and lifts forward by air levitation.

5 is a view for explaining the structure of an electromagnet coil gun in a diving vehicle according to a preferred embodiment of the present invention.

5, the solid hydrogen of the hydrogen ion engine 200 is heated and discharged at a high speed to discharge the plasma. The seawater heated by the high temperature is ionized into water (oxygen, hydrogen) and salts, Electromagnets are arranged at a predetermined interval in the pair of electromagnet coil guns 400a and 400b attached to the front and rear sides of the bottom surface of the hydrogen ion engine ion beam 290 at the lower surface of the battery 100, When continuously changing, ionic seawater (oxygen, anode, s pole, hydrogen, cathode, n pole) becomes a conductor, and the current is sequentially supplied to the electromagnet coil guns 400a and 400b arranged at the same pole as the electromagnet coil gun You can accelerate the seawater along the set path.

Therefore, when the electromagnet coil guns 400a and 400b are pulled by the electromagnetic force and the direction of the battery is continuously changed, the electromagnet coil is shaken to each other by using the electromagnetic force of seawater. At this time, the seawater is sprayed backward through the electromagnetic projection device of the strong magnetic field electromagnet coil guns 400a and 400b, and the seawater ions (oxygen, hydrogen, dye) come into contact with each other as the ionized water passing through the electromagnetic projection device returns to the original state The combined force and its reaction result in lift (a force acting at right angles to the direction of motion when an object moves in the liquid) and propulsion.

In this case, the water molecule has a polarity like a magnet having n-pole and s-pole, and the seawater has 96% of water (H2O) and 4% ) Is electrolyzed while flowing between the cathode plates. When the sea water rotates at a high speed, the water molecule rotates rapidly by the force generated by the magnetic force by colliding with the innumerable negative charge (anion) formed in the magnetic field (the tension membrane of the force), and the water molecule is subdivided into hydrogen and oxygen. The forward and backward directions of the electromagnet coil guns 400a and 400b may be simply changed in current flow or the speed may be easily controlled by adjusting the intensity of the current and the magnetic field. Electromagnet coil gun is a magnetism engineering system that generates magnetic force to generate magnetic force, accelerates seawater by the effect of magnetic field, and is a projectile which generates high-speed magnetic propulsion by using electromagnetic coil. Electric current is flowed to the coil sequentially by using a coil for generating an electromagnetic field, thereby accelerating the seawater along the path. In the current-carrying coil, a ring-shaped magnetic field is generated. This magnetic field draws the seawater to one side. The coil-gun uses the ferromagneticity of the circular coil. In other words, after arranging the circular coils in a line in a tunnel form, the ferromagnetic sea water is placed at one end of the tunnel, and current is supplied to the first coil. And the vehicle body 100 is a silent propulsion system equipment for propelling the ionized seawater in the water with a magnetic field coil gun in the rear. It is possible to fly diving with magnetic force and energy in a huge fluid called seawater.

6A and 6B are views for explaining the operation of an electromagnet road wheel, an electromagnet rail and a rudder provided in a diving vehicle according to a preferred embodiment of the present invention.

Referring to FIG. 6A, the front wheel and rear wheel electromagnet road wheels 500a and 500b according to the present invention include an electromagnet motor and a driving device mounted inside the electromagnet road wheel 530, And a decelerator. The electromagnets 550a and 550b are disposed around the electromagnet road wheel drive shaft 520. The electromagnets 550a and 550b are disposed on the electromagnet road wheel 530 with the electromagnets 550a and 550b, Are disposed at regular intervals with N poles and S poles arranged at the same pole as the electromagnet road wheel 530 and current is flowed through the electromagnet road wheel drive shaft 520. The electromagnet wheel wheel 530 The direction of the battery is continuously changed so that the electromagnet road wheel drive shaft 520 and the electromagnet road wheel 530 are engaged with each other and the front wheels and the rear wheel wheels 500a and 500b can rotate respectively.

The front wheels and rear wheel electromotive road wheels 500a and 500b have small turning vibrations and a large number of electromagnets 550a and 550b are placed in the wheel wheel 530 through the rotation of the electromagnet without the electric motor, It is driven by air and runs in the air.

In the preferred embodiment of the present invention, the motor and suspension are integrated into the electromagnet to reduce the need for the main engine, and the bonnet The seawater infinite power generator 700 is housed in the place where the engine is located, so that the weight of the vehicle body 100 can be lightened.

6B, an electromagnet rail 560 is installed above the hydrogen ion engine ion beam 290 installed at the lower end of the central axis of the vehicle body 100. [ The electromagnet rail 560 is provided with a linear motor (in the form of a linear coil of a general motor) and the electromagnet 560 is mounted on the electromagnet rail 560 at the upper part of the electromagnet rail 560 The electromagnet rudder 570 is moved when the bottom of the electromagnet rudder 570 is N pole and the rail located below the electromagnet rudder 570 is also N pole, so that the electromagnet rudder 570 finally floats, Pole and the N-pole of the electromagnet rudder 570, the electromagnet rudder 570 can move forward. At this time, the S pole changes to the N pole at the time of repulsion, so that the electromagnet rudder (570) can continue moving forward.

On the other hand, electromagnets 550a and 550b are arranged at N-poles and S-poles at regular intervals in the electromagnet rail 560, and electromagnets 550a and 550b are arranged in the electromagnet rudder 570 at regular intervals, Are disposed at the same pole as the electromagnet rail 560 and the direction of current flowing to the linear motor is continuously changed, the N pole and the S pole provided in the electromagnet rudder 570 periodically change. Therefore, when the electromagnet rail 560 and the electromagnet rudder 570 begin to shrink each other and the opposite direction of the current is reversed, the attracting force and the repulsive force rapidly appear alternately between the electromagnet rail 560 and the electromagnet rudder 570 Suddenly go back to the electromagnet rudder 570.

The hydrogen ion engine ion beam 290 is fixed around the seawater while the seawater is brought into contact with the bottom surface of the hydrogen ion engine ion beam 290 during the underwater flight and the electromagnet rudder 570 is controlled to follow the electromagnet rail 560 The vehicle body 100 can be rotated 360 degrees.

Meanwhile, in the method of operating the electromagnet rudder drive shaft, a rotating disk is installed on the hydrogen ion engine ion beam 290 during underwater flight, and an electromagnet rail 560 is provided thereon to provide a rudder drive shaft on the electromagnet rail. The electromagnets 550a and 550b are arranged at regular intervals with N poles and S poles with the hydrogen ion engine ion beam 290 and the electromagnet rail 560 as fixed axes while the bottom surface of the vehicle body 100 is in contact with seawater, The electromagnets 550a and 550b are disposed at the same pitches as the electromagnet rails 560 with the N and S poles being spaced apart from each other with the rudder drive shaft 520 as a center and the current is supplied to the electromagnet rudder 570, The electromagnet rail 560 is pulled and the direction of the battery is continuously changed so that the electromagnet rudder 570 and the electromagnet rail 560 are engaged with each other and the electromagnet rudder 570 is rotated.

7 is a view for explaining the operation of the flag pin wing of the dive flying vehicle according to the preferred embodiment of the present invention.

7, a cable 612, a rocker arm 613 and a crankshaft 614 are connected to the inside of each of the calvuit blades 620 and 630, and the cable 612 is wound on the winding surface 611 by an electric motor 611 As each of the calvic vanes 620 and 630 is folded inwardly so that the calvic vanes 620 and 630 are bent upward and the cable 612 is released by the electric motor 611, It is bent down.

Here, the rotary motion of the calvibs 620 and 630 is converted into a vertical reciprocating motion by a scotch yoke 640, and the electric motor 641 is rotated in one direction, so that the calvet blades 620 and 630 are reciprocated in the vertical direction And the calvic vanes 620 and 630 rotate 180 degrees so that the calvic vanes 620 and 630 can flap from top to bottom and vice versa.

The scotch yoke 640 is mounted on the right and left sides of the calvary wings 620 and 630, respectively, when flying.

The scoop yoke 640 is a type of double slider crank mechanism that converts rotational motion into reciprocating motion or reciprocating motion into rotational motion and includes an electric motor 641, a belt 642, a drive shaft 643, The piston 642 is connected to the piston 642 via the belt 642 and the piston 642 is connected to the piston 642 via the belt 642. When the electric motor 641 is driven by the half- 644, and consequently converts the rotational motion of the electric motor 641 into a vertical reciprocating motion.

Meanwhile, the cable 612 is connected to the pulley 620 and 630 by the electric motor 611 by connecting the pulley and the cable to the feather made of hollow blades, When the knife blade 620 and 630 are lifted up, the knife blade 620 and 630 are lifted up by the electric motor 611 and the cable 612 is wound The feather shell wraps around and rotates to make the wings fly through the feathers.

It is very scalable in terms of range and speed to control the calvibs 620 and 630, and is a technique for controlling the special wings that appear when the calvibs 620 and 630 are moved up and down.

The general wings are noisy because they generate a whirlpool whirlwind, but the operation of the flagwheel according to the embodiment of the present invention is operated by the electric motor 611 and the noise is very low.

On the other hand, the feature of the calvic wings 620 and 630 is a stiff calvitic shape formed along the leading edge of the wing. It is preferred that the operation of the calvic vanes 620 and 630 be made using a thin shell that is deformable since the calvic vanes 620 and 630 are made up of a plurality of shells and the calvic vanes 620 and 630 are essential elements in flight . In this case, although the operation is symmetrical with the use of the calvet's wings 620 and 630, the balance of the wings can be lost due to the characteristics of the flagpole wings moving during the air flight, A set of superconducting permanent magnet sets 300a is provided on the upper portion of the vehicle body 100 and a set of superconducting permanent magnet sets 300b is installed on the upper end of the upper portion of the vehicle body 100 to maintain balance during aerial flight.

In the above-described embodiment of the present invention, the bristle wings 620 and 630 are provided with a knife comb part of the flagpole wing for obtaining a lift force and for receiving resistance when the wing is up and down, 651 so as to float the upper and lower sides of the calvet blades 620, 630, thereby obtaining a driving force to overcome the resistance.

In addition, the calvic wings (620, 630) are made of hollow aluminum and have no sound when winged, all of which are covered with feathers and are formed such that the tip of the flagpole is split like a comb. Here, the feathers serve as a buffer for dispersing the frictional force upon contact with the air due to the contact with the air, and the knives of the knives 620 and 630 are split like a comb, so that the feather shell rotates with each other and rotates to friction with the knives 620 and 630 So that the generation of the fricative can be minimized, thereby reducing the noise.

Also, the hollow aluminum flagpole of the calvic wings (620, 630) is less flexible, but it is lighter and stabilizes the movement of the wing, allowing better flight, and the inside of the flagpole is empty.

Accordingly, a driving force is generated in the horizontal axis which is generated by moving the calvibs 620 and 630 to the left and right, and an electric motor 651 is mounted on the rotary disk at the center mounted in the calvibs 620 and 630. The calvet blades 620 and 630 protrude outward from the inside of the left side of the vehicle body 100 and are housed and stored therein. Here, the secret to making movement with simple flaps is that the springs 621 and 631 are respectively attached to the lower ends of the bladed wings 620 and 630 to impart elasticity and move at a lower speed through the propellant method rotating left and right with the knife blades 620 and 630, Can be reduced.

Referring to FIGS. 8A and 8B, a process for generating electricity by rotating a seawater infinite power generator and an iron ball wheel in order to reduce a fuel cost of a propulsion device in a vertical floating state of a diving vehicle according to a preferred embodiment of the present invention will be described Fig.

The self-generating device shown in FIG. 8A generates electricity by itself using the seawater infinite power generator 700 or the bead wheel 700a, directly charges and stores the vehicle body 100, and charges the fuel while the vehicle is flying underwater . The seawater 701 in the seawater tank 710 descends from the top to the bottom and passes through the electromagnet 730 in the seawater induction pipe 720 while being driven by the electromagnet 730 by the electromagnet 730, A magnetic field flows between the two electrodes 740a and 740b and a current is generated by crossing the two electrodes 740a and 740b installed at the right and left ends of the end portion of the sea water induction pipe 720 at right angles. At this time, current starts flowing in a direction orthogonal to each of the magnetic field and the sea water flow, and a self-generated power is generated without loss of energy since a rotating device such as a turbine is not necessary.

In the preferred embodiment of the present invention, the generated current is stored in a cell inside the vehicle body 100, and the fuel can be charged while flying under water using the collected battery.

The seawater in the seawater tank 710 pushes the seawater from the top to the bottom and the seawater 701 in the seawater induction pipe 720 rises from the bottom to the top by the water pressure and becomes a circulating loop into the seawater tank 710, do. When the seawater 701 is backwashed, the seawater induction pipe 720 is closed by the breech 711, so that the seawater 701 is introduced into the sea water tank 710, Do not backflow.

As shown in FIG. 8B, when electricity is generated by infinite power using the wheel 700a in the underwater flight, the generated electricity is stored in the cell in the vehicle body 100, The fuel can be charged.

The wheel spindle wheel 700a includes a drive shaft 750, a wheel wheel 760 spaced a predetermined distance from the drive shaft 750, and a bead 770 inserted into the wheel wheel 760, And a steel ball door 780 formed on the outer ring of the wheel wheel 760, respectively.

9, when the iron ball 770 is inserted into the iron ball door 780 and rotated once, the electricity generated by the rotation of the iron ball 730 at the same speed as the infinite power is stored in the cell (battery) And the battery can be charged with fuel.

FIG. 9 is a view for explaining the operation of an operator seat protecting apparatus shelter and an electromagnet ejecting apparatus provided in a dive flying vehicle according to a preferred embodiment of the present invention.

9, when the driver pulls the cable 811b connected to the electromagnet injector 860, the connection ring of the spring 850, which contacts the bottom surface of the driver protection device shelter 810 and the top surface of the electromagnet injection device 860, The spring 862 embedded in the electromagnet injector 860 protrudes upward and pushes up the driver's protective device shelter 810 which lies on top of the electromagnet extruder 860 by the force of the spring 862, The driver's protection device shelter 810 can float in the vertical direction through the snorkel absorbing port 870 and can be separated from the vehicle body 100. At the same time, a driver protection device shelter 810 is mounted on the rails 864 of an electromagnet catapult (injection device: an apparatus for oscillating an airplane in a narrow space) 860 provided as a support for the driver protection device shelter 810, The upper surface of the electromagnet extruder 860 and the bottom of the driver's protection device shelter 810 are arranged at the same pole so that the electromagnet injector 860 keeps flowing the current continuously as the electromagnet injector 860 advances, The same polarity as that of the bottom electrodes 740a and 740b of the driver protection device shelter 810 pushes them together and becomes the power for lifting the driver protection device shelter 810 to the snorkel absorption port 870.

Meanwhile, when the vehicle body 100 is submerged in water, an electric current is automatically supplied so that the electric stone gate 813 attached to the door 815 of the driver's protection device shelter 810 is unfolded according to the operation means, Thereby protecting the driver's protective device shelter. At this time, it is important to maintain the level for forming air pockets and the weight center weight 840 is laid down on the outside of the bottom of the driver's protection device shelter 810 to keep it horizontal, The screw propellers 830a and 830b are installed to operate as a battery and can escape.

The operator protector shelter 810 connected to the driver's seat can be escaped from the snorkel inlet 870 by the electromagnet injector 860 by the electromagnet injector 860 when the body 100 is in an emergency, (870) and can be separated from the driver's seat.

10A and 10B are views for explaining the operation of the electromagnet eddy current disk and the permanent magnet eddy current of the diving vehicle according to the preferred embodiment of the present invention.

10A, in an electromagnet and eddy current brake 920, an electromagnet eddy current disc 910 fixed to an axle as a kind of electric braking of a vehicle, and an electromagnet 930 installed with a proper gap therebetween The braking force generated by the eddy current induced on the surface of the brake disk 910 is used according to the relative motion.

Two electromagnetic electromagnet eddy current discs 910 carrying an electromagnet 930 at the center of the axle of the electromagnet eddy current magnetic substance are provided and four coils 940 are installed on both sides of the electromagnet eddy current disc to form coils 940 An eddy current can be generated in the electromagnet eddy current disk 910 and converted into heat.

On the other hand, braking is used in an electromagnet and eddy current braking device that generates a rotating magnetic field from the electromagnet 930 to generate an electromotive force due to the Fleming's left-hand rule and interfere with the rotation of the superconductor sparking permanent magnet. So as to stop the rotation.

At this time, the electromagnet 930 is mounted at a position very close to the rails, and the electromagnet and eddy current brake 920 is driven by passing an electric current through the electromagnet 930 and the electromagnet and eddy current brake 920 by the eddy current generated in the rail. And the braking force acts directly between the electromagnet 930 of the wheel and the rail.

The eddy-current braking device is provided with respective passages. Eddy current is generated in the magnetic body when the magnetic flux changes in the magnetic body, and the electromotive force A swirling current flows through the magnetic body. Eddy currents are created in the conductor to create a magnetic field in the same direction as the external magnetic field to prevent the magnetic field from weakening as the object moves away from the magnetic field, do. In electricity, eddy current (eddy current) refers to the current flowing in a vortex shape through numerous paths on a conductor surface or inside a conductor.

Referring to FIG. 10B, since copper is not a ferromagnetic substance in the permanent magnet eddy current (980), there is no reaction even when it is attached to the permanent magnet, and the attraction is not generated.

For example, if a permanent magnet is dropped into a copper pipe 950, it will fall as if it were caught in a pipe. This phenomenon is described by electric theory. Since a moving permanent magnet makes a magnetic field (magnetic flux) which changes around it and the copper pipe 950 is linked to the changing magnetic flux, the electromotive force . Copper conductors have a number of fine electrical circuits inside them, which produce eddy currents (eddy currents) through the generated electromotive force in a number of paths.

Here, the direction of the induced electromotive force (direction of the pole, eddy current) is a direction that can interfere with the change of the magnetic field of the permanent magnet by using the magnetic field generated by the current flowing by the electromotive force.

The reason why the induced electromotive force takes such a polarity that it interferes with the flux change of the principle that made this electromotive force is because it follows the Law of Lorentz which is one kind of energy conservation law.

Therefore, a repulsive force is generated with the copper pipe 950 that approaches the permanent magnet when the permanent magnet falls, and attraction occurs with the copper pipe 950 away from the magnet. As a result, the speed at which the permanent magnet moves away is slower than the speed at which it falls in free space. However, no matter how strong the permanent magnet is, there is not a large attraction to stop the magnet in the copper pipe 950. When the magnet stops, the magnetic field does not change, and the electromotive force is not generated in the copper conductor 951, so that the eddy current does not flow.

When the copper pipe 950 is cooled to a very low temperature by using a cryogenic material such as liquid nitrogen, the conductivity of the copper becomes extremely high at a very low temperature. As a result, the electromotive force is increased and the eddy current flows immediately. It becomes slow.

If you place a permanent magnet on a superconductor instead of a copper pipe (950), the superconductor and the permanent magnet will stay at a constant distance from one another and will be farther away. The reason for this is that a very large eddy current flows through the surface of the superconductor as the n-pole of the permanent magnet moves closer to the superconductor as the magnetic field changes as the n-pole approaches the superconductor (the superconductor has zero resistance so that infinite current flows through a small electromotive force) This is because the direction of the magnetic flux of the permanent magnet is suppressed by Lorentz's law, which is a kind of the law, so that the n-pole is formed on the surface of the superconductor, which hinders the increase of the magnetic flux. On the contrary, when the n pole of the permanent magnet tries to move away from the superconductor, the magnetic flux decreases, and the eddy current flows on the surface of the superconductor in the direction opposite to the first direction, thereby forming the s pole and pulling the permanent magnet n pole. Since the attracting force and the repulsive force are generated almost simultaneously, the permanent magnet 330 can not move away from the superconductor. These eddy currents are hidden under the magnetic levitation phenomenon of superconductors. Smooth deceleration is possible because the faster the speed, the larger the eddy current induced and the greater the braking force. The slower the speed, the less the braking force will be with the eddy current. Unlike friction braking, noise and wear are also advantages of eddy current braking. Because of the relative motion between neodymium (rare earth) permanent magnets and pure copper, eddy current braking occurs, so no artificial power supply for braking is required and no failure can occur. As the magnetic bar code line penetrates and bridges the surface vertically within the copper pipe 950, the copper pipe 950 flows as if it were circumferentially along a circular line when it was surfaced by stacking a number of copper rings. In addition, the upper and lower parts of the permanent magnet have opposite current directions. The superficial elevation is due to Meissner effect and eddy currents levitating the permanent magnet. Only the magnetic force of the superconductor and the permanent magnet causes circular movement along the orbit.

11 is a view illustrating a process of constructing a driver's seat and a control unit provided in a dive flying vehicle according to a preferred embodiment of the present invention with a shale.

11, the driver controls the vehicle body 100 from the driver's seat 800 to the telescope during the underwater flight, and the driver's seat 800 is operated by the lift valve 872, the rocker arm 876, The lift weight 873 is lowered and the glass film 880 rises along the rail to the shale so that the driver's view can be secured.

The lift weight 873 is lifted while being lowered by the lift valve 872, the rocker arm 876 and the crank shaft 875 during the underwater flight so that the glass film 880 is lowered below the rail and stored in the driver's seat.

Here, the lift valve 872 and the glass film 880 are connected to each other, and the glass film 880 can survive for at least 5 hours without supplying external air. When the glass film 880 floats on the surface of the water, And the driver can open the upper vent valve 871 if necessary.

Air is left from the bottom surface to the inner surface of the glass film 880 during the underwater flight to form a kind of air pockets (air bladder) so that the inside of the vehicle does not get wet even if the vehicle body 100 falls into the water.

According to the above-described invention, the scooter yoke, which is made to reciprocate up and down while the electric motor rotates in one direction, is provided with left and right hollow flagpoles, And when they climb up, the flagpole wings are wobbled to rotate, and the wing flapping out of the air is a source technology to fly the air. The plasma is generated by the high-speed injection of the compressed liquid nitrogen of the piston through the fine holes by the mushroom-shaped oil coating on the surface of the metal body of the body 100, and the plasma is rapidly ejected by the ion beam of the hydrogen ion engine 200, And it is a source technology to fly underwater. When it is commercialized, it will be applied firstly for leisure and military purpose, and there is no case of commercialization in the world, so it is a promising field of superpower that can preempt the market with differentiation. It is a new type of water sports that can fly underwater and run freely on the water surface. Recently, demand for personal helicopters and yachts has been increasing mainly in the affluent.

The embodiments of the present invention disclosed in the present specification and drawings are merely illustrative of specific examples for the purpose of understanding and are not intended to limit the scope of the present invention. It will be apparent to those skilled in the art that other modifications based on the technical idea of the present invention are possible in addition to the embodiments disclosed herein.

100: Body 101: Gas turbine engine
110: electromagnet ring fixing shaft 120: electromagnet ring
130: projection 131: mushroom shape
111, 133: fine holes 140a, 140b: piston
150a: Upper upper bore 150b: Lower lower breeze
160: Bure line 170: Check valve
180: Buoyancy control piston 200: Hydrogen ion engine
201: solid hydrogen 210: fuel cell
220: hydrogen release reactor 221: inlet valve
223: Outflow valve 230: Spray type piston
231, 611, 641, 651, 320a, 320b, 281, 877:
233,283: Piston 235,285: Cylinder
237: Compression spring 240: Combustion chamber
250: arc igniter 251: arc
253: circuit breaker 260: nozzle
270: discharge chamber 280: compressed air supply unit
287: compressed air inlet 290: hydrogen ion engine ion beam
300a, 300b: a set of sparking permanent magnets 310, 310a to 310h: a sparking permanent magnet
330, 330a, 330b: Superconductors 311, 311a to 311l: Sparking permanent magnet rotors
313: Cylindrical permanent magnet 313a: Cylinder
313b: Cylindrical permanent magnet
340a, 340b, 613, 645, 876, 655a, 655b:
350a, 350b, 614, 635, 646, 653a, 653b, 875,
360: liquid nitrogen container 111,361: liquid nitrogen
370: liquid nitrogen container cover 380,625,635: disk
381, 383: rotor 400a, 400b: electromagnet coil gun
410: Electromagnet coil 500a, 500b: Front and rear road wheels
510: Shoba 520: Electromagnet road wheel drive shaft
530: Electromagnet road wheel wheel 540: Electromagnet front wheel road wheel
550a, 550b: electromagnet 560: electromagnet rail
570: Electromagnet rudder 600a, 600b: Flag pole wing
610: Flagpole wing power section 620,630,621,631: Calvin wing
640: scotch yoke 642: belt
643: drive shaft 644: piston disc
700: Seawater Infinite Power Generator 701: Seawater
710: Seawater tank 711: Breeze
720: Seawater induction pipe 730: Electromagnet
740a, 740b: Electrode 800: Operation and control device
810: Driver protection device Selter 811a, 811b: Cable
813: Electronic door 815: Driver's protective device Selter door
817, 862: spring 820: telescope
830a, 830b: screw propeller 840: center of gravity weight
850, 850, 862, 621, 633: Spring 860:
864: electromagnet injector rail 870: snorkel inlet
871: Vent valve 872: Lift valve
873: Lift weight 880: Glass sheet
901: electromagnet eddy current center axis 910: electromagnet eddy current disk
920: electromagnet eddy current brake 930: electromagnet
940: electromagnet eddy current coils 950: copper pipe
951: copper conductor 960: liquid nitrogen container
970: Electric circuit 980: Permanent magnet eddy current

Claims (4)

A vehicle body (100) having a metal spherical shape;
A gas turbine engine 101 installed inside the vehicle body 100 to generate a thrust for forward flight when the vehicle body 100 meets the public airplane;
A hydrogen ion engine 200 installed at a lower end of the vehicle body 100 for spraying plasma at a high speed using an ion beam so as to be a propellant in water during flight of the vehicle body 100;
At least a pair of magenta permanent magnet sets (300a, 300b) installed at an upper end of the vehicle body (100) and cooled by liquid nitrogen to levitate and rotate the vehicle body (100);
At least a pair of electromagnet coil guns (400a, 400b) installed at a lower portion of the vehicle body (100) for generating ion propulsion through the ionized seawater to generate a propulsion force by using a magnetic force generated by the reaction;
Front and rear electromagnet road wheels 500a and 500b fixed to the bottom of the vehicle body 100 and used for landing;
A pair of flagpole blades (600a, 600b) which are formed to be hollow like a whorl and which maintain the air flight and level of the vehicle body (100) through upper and lower wings;
A self-generating device (700, 700a) for generating electric power using a magnetic field and a sea water flow;
And an operation and control unit (800) that maintains a waterproof function during underwater flight and a driver seat rising upwards to construct a shale during an air flight;
The vehicle body (100)
A spherical electromagnet ring fixing shaft 110;
A spherical electromagnet ring (120) fixed to an outer surface of the electromagnet ring fixing shaft (110);
A plurality of protrusions 130 projecting outward from the outer surface of the spherical electromagnet ring 120 and having an upper end coated with oil as a mushroom shape 131 and having a plurality of fine holes 133 formed on the surface thereof;
And a plurality of pistons (140a, 140b) provided on an inner surface of the electromagnet ring fixing shaft (110). The method according to claim 1,
A rear end upper boss 150a and a front lower end bobbin 150b respectively installed at a rear end and a bow of the vehicle body 100 so that a predetermined amount of air can be injected or moved, A check valve 170 for selectively controlling the air movement path of the baffle line 160, the aft upper baffle 150a and the front lower baffle 150b, which connect the lower baffle 150a and the lower baffle 150b to each other; Further comprising a buoyancy regulating part comprising a buoyancy adjusting piston (180) for regulating the buoyancy by supplying or removing air to or from the rear upper boom (150a) or the front lower end boom (150b). delete The method according to claim 1,
The hydrogen ion engine (200)
A hydrogen discharge reactor 220 for discharging the solid hydrogen discharged from the solid hydrogen fuel cell 210 by a predetermined amount;
A spray-type piston (230) installed in the hydrogen-releasing reactor (220) for regulating the internal pressure of the hydrogen-releasing reactor (220) to control the inflow or outflow of the solid fuel;
A combustion chamber 240 for burning solid hydrogen discharged from the hydrogen discharge reactor 220;
An arc igniter 250 for igniting the arc in the combustion chamber 240;
An oxygen supply nozzle 260 for supplying oxygen to the arc igniter 250;
A discharge chamber 270 in which the solid hydrogen burned in the combustion chamber 240 performs arc discharge in which strong light and high temperature heat are generated;
A compressed air supply unit 280 for supplying compressed air to the discharge chamber 270;
And a hydrogen ion engine ion beam (290) for injecting plasma generated in the arc discharge of the discharge chamber (270).

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