RU2449170C1 - Inertial engine by bogdanov - Google Patents

Abstract

FIELD: engines and pumps.

SUBSTANCE: inertial engine comprises at least one system with a propeller and a flywheel with a working medium. Around the flywheel there is a turbine, and the flywheel is made as capable to supply working medium to the inner working surface of the turbine. In another version around the flywheel there is a spiral or a ring with a chute on the inner surface facing the axis of the flywheel rotation, and at the outlet from the spiral or ring there is a hole with the possibility of discharge of the accelerated working medium from the hole.

EFFECT: invention makes it possible to develop thrust in an airless outer space.

25 cl, 12 dwg

Description

The invention relates to the field of jet engines. It can be used in aviation and astronautics to create aircraft.

In addition, the invention can also be used to move an object in any form of transport, including on land, in water and under water.

In addition, the invention can also be used to increase the capabilities of existing modes of transport. For example, the invention can be used to create a flying car or flying submarine.

Known chemical rocket engine [Space engines: state and prospects. Edited by Cavney L., Moscow, Mir, 1988, p. 411], which uses the chemical energy of burning fuel to create rocket thrust.

A disadvantage of a chemical rocket engine is that chemical rocket engines have a low specific energy content per unit weight of fuel, not more than 1.2 · 10 ⁷ J / kg.

The next disadvantage of a chemical rocket engine is the low rate of expiration of the combustion products of chemical rocket fuel, which does not exceed 5.7 km / s (p. 415).

Known Bogdanov’s electromagnetic engine for creating traction on new physical principles [Bogdanov’s electromagnetic engine for creating traction on new physical principles. Patent No. 2200875. Application No. 2001012072. Priority 05.17.2000].

The Bogdanov electromagnetic motor for creating traction on new physical principles contains either a disk or a ring and a disk or ring rotation system configured to rotate the disk or ring, while the ring or disk is made inside the cryostat, and the cryostat is made to rotate together with the ring. In this case, the disk or ring contains a structure containing 50 layers of a superconductor separated by a dielectric with high electrical resistivity (electrical insulator), or more than 50 layers of a superconductor separated by a dielectric with high electrical resistivity.

During rotation of a disk or ring containing 50 layers of a superconductor separated by an insulator, or more than 50 layers of a superconductor separated by an insulator, a weight reduction of 2 percent is observed over each layer of a superconductor. This phenomenon has been experimentally confirmed [Article on the topic "Scientific research". Russian scientists discovered antigravity. © 2008 ScienceArt.Ru,

http: //scienceart.m/researches/rossiyskie_uchenie_otkrili_antigravitaciyu.html].

At the same time, a decrease in weight by 4 percent is observed over two layers of a rotating superconductor, which also found experimental confirmation.

Thus, over all 50 layers of a rotating superconductor, a complete decrease in weight is observed, which makes it possible to reduce energy costs when launching a payload located above rotating structures with superconductor layers into orbit (or when flying to another celestial body).

The disadvantage of Bogdanov’s electromagnetic motor for creating traction on new physical principles is the fact that there is no effective mechanism that removes the effect of reducing gravity over a rotating superconductor without removing it from the superconducting state or without removing it from rotation. This interferes with the use of Bogdanov’s electromagnetic engine during the landing of an aircraft with such an engine.

The next drawback of Bogdanov’s electromagnetic motor for creating traction on new physical principles is the fact that there is no effective mechanism for quickly removing and restoring the reduction of gravity over a rotating superconductor without removing it from the superconducting state or without removing it from rotation with a new creation of a situation when the superconductor rotates in a superconducting state. This makes it difficult to repeat the combinations of takeoff and landing of an aircraft with such an engine.

Known electric propulsion engine Bogdanov [Bogdanov I.G. Electric rocket engine Bogdanov. Patent No. 2046210. Application No. 5064411. Priority of the invention, October 5, 1992], comprising a power system, a magnetic field coil, ionizing radiation sources and an electrode system that accelerates pre-ionized atmospheric gas by generated electric currents and electric fields in generated magnetic fields.

At the same time, Bogdanov’s electric rocket engine works as a powerful plasma engine of a space shuttle (shuttle), which works as a powerful plasma launch vehicle.

Bogdanov’s electric missile engine allows to launch multi-ton aircraft into orbit either due to the energy stored in the coil of the magnetic field, or due to the energy generated by the nuclear or thermonuclear reactor of the on-board power system. In both cases, Bogdanov’s electric rocket engine is able to replace and surpass today's rocket launchers accelerated by a chemical rocket engine.

The disadvantage of the Bogdanov electric rocket engine is the complexity of the design.

The next disadvantage of the Bogdanov electric rocket engine is the low efficiency of the operation, due to the following factors. The conversion efficiency of thermal energy into electrical energy usually does not exceed 40 percent. The best efficiency of electric rocket engines does not exceed 80 percent. Thus, the efficiency of the electric propulsion engine of Bogdanov is not more than 32 percent.

The next disadvantage of the Bogdanov electric rocket engine is significant energy loss when the solenoid is cooled to the temperature of liquid helium during its energy supply.

When the solenoid is cooled to the temperature of liquid helium, the energy loss for feeding its energy ranges from 500 to 1000 times the amount of energy stored in it (but this is without using the author’s patented invention [Bogdanov’s method of changing the amount of energy in a magnetic system and device for its implementation. Patent No. 2295146. The patent was registered on March 10, 2007. Application No. 2005121237. Date of filing of the application July 7, 2005], which solves this problem). Therefore, the creation of this engine becomes relevant after the development of the industry of fast neutron reactors and breeder breeder reactors, which make it possible to obtain about 100 times more energy per unit weight of nuclear fuel than 235 slow neutron reactors from traditional nuclear fuel. This will allow the use of junk uranium 238, which has accumulated a lot in dumps, to produce plutonium. Also, the creation of this engine becomes relevant after the development of thermonuclear energy. Also, the creation of this engine becomes relevant when using a new method for feeding solenoids - the author’s patented invention, which allows energizing the solenoid without energy loss by 500-1000 times, since in this invention the main part of the energy supply is carried out in a magnetic system that is completely in a superconducting state.

Known turbojet engine, which is an aircraft gas turbine engine [Soviet Encyclopedic Dictionary. Publishing house "Soviet Encyclopedia". Moscow, 1980, p. 1374]. A turbojet engine comprises an inlet, a compressor, a turbine, an afterburner, a nozzle, and a combustion chamber.

In a turbojet engine, thrust is created by the direct reaction of a stream of compressed gases flowing out of a nozzle.

The disadvantage of a turbojet engine is the low specific energy content per unit weight of fuel. For example, the specific energy content per unit weight of kerosene is 9.05 · 10 ⁶ J / kg [Burdakov V.P., Danilov Yu.I. Physical problems of space traction energy. Moscow .: Atomizdat. 1969, p. 37].

The prototype of the invention is an inertial engine, which is an energy-powered machine that uses energy stored by a flywheel [Burdakov VP, Danilov Yu.I. Physical problems of space traction energy. Moscow .: Atomizdat. 1969, p. 37]. The inertial engine contains a flywheel.

The inertial engine is known, which is an energy-powered machine using the energy stored by the flywheel [Soviet Encyclopedic Dictionary. Publishing house "Soviet Encyclopedia", Moscow .: 1980, p. 498]. Sometimes used to drive machinery, vehicles. For example, the famous fat globe, gyro globe. Girobus, Girobus [from Italy. giro, Greek gyros - circle, revolution, and Latin omnibus - for everyone], a type of batteryless rail transport moving due to the kinetic energy accumulated in the flywheel [29]. Since 1955, electric globes (EFs) equipped with a flywheel unit consisting of an asynchronous motor - a generator coupled to a flywheel and traction motors have received some practical use. The spinning of the EJ flywheel is carried out by an electric motor. The stored kinetic energy is enough to cover a distance of 4-5 km. EF efficiency no more than 50%; the material consumption of the flywheel unit is 322 kg / kWh (32 times more than modern electrochemical current sources).

In terms of unit operating costs, EF is more expensive than a trolleybus by 5% and a bus by 20%. Experienced ECs were operated, for example, on intercity lines Gent-Merelbeke (Belgium). EZH is an auxiliary passenger transport for short routes, suitable for servicing explosive facilities.

The disadvantage of an inertial engine is that it is not intended to be used for flight in airless space.

The challenge facing the invention is to provide the ability to create traction in the airless space.

This problem is solved by the fact that in the inertial engine containing the flywheel, the flywheel further comprises a working fluid, and at the same time, it is possible to withdraw the working fluid from the flywheel so that at the exit from the engine the working fluid moves in a predetermined direction.

A cavity is made in the flywheel housing, while a working fluid is made in the cavity, and a valve is connected to the flywheel housing or an injector is connected, while the valve is made with the possibility of remote control and with the ability to control the exit of the working fluid flywheel, and the nozzle is made with the possibility of remote control with the ability to control the exit from the flywheel of the working fluid.

The inertial engine is configured to be connected to a thermal power plant, and it is possible to withdraw the working fluid from the flywheel so that the working fluid collides with the fuel of the thermal power plant and heats the fuel of the thermal power plant.

The inertial engine comprises a flywheel rotation drive device, wherein the flywheel rotation drive device comprises a flywheel, a ring and a pipe connecting the flywheel and the ring, wherein an accelerating gap is formed on the top and bottom of the ring, formed by sections of two electrodes located around the ring and facing each other, having the form of hollow half-cylinders, the electrodes being configured to be connected to a generator.

A remotely controlled system with a battery is made on the ring, electrically connected to at least two conductive plates electrically isolated from each other, and the battery of the system with a battery is configured to electrically charge at least two conductive plates with charges of opposite signs.

The inertial engine contains a system with a generator configured to generate electrical energy by rotating the flywheel or ring connected to the flywheel.

The inertial engine comprises a magnetic suspension configured to hold the flywheel on weight during rotation of the flywheel.

The magnetic suspension contains a superconducting magnet.

A turbine is connected to the flywheel, the flywheel being connected to the turbine cooling system and configured to feed the working fluid to the inner working surface of the turbine connected to it through the turbine cooling system.

A turbine is made around the flywheel, and the flywheel is configured to feed a working fluid to the inner working surface of the turbine.

In two flywheels, rocket fuel was made as a working fluid, while in one flywheel combustible fuel was made as a working fluid, and in the other flywheel, a fuel oxidizer was made as a working fluid.

The inertial engine contains a graphite powder atomization system.

A cryostat is made below the flywheel, while inside the cryostat there is a structure containing at least two superconducting layers separated by a dielectric, the structure being made under the flywheel in the form of a ring.

A cryostat is made at the bottom of the flywheel, while inside the cryostat there is a system of structures with superconducting layers separated by a dielectric containing at least two elements, the element containing a structure containing at least two layers of a superconductor separated by a dielectric, and the system is connected with a system for changing the position of elements of a system of structures with superconducting layers separated by a dielectric, and configured to remotely control, while the system for changing the position of elements This system of structures with superconducting layers separated by a dielectric is configured to receive electric power either from a battery or from a generator configured to generate electricity when the flywheel rotates, while a system for changing the position of elements of a system of structures with superconducting layers separated by a dielectric is made with the ability to arrange elements of a system of structures with superconducting layers separated by a dielectric such that the superconducting layers are connected to ltsa disposed below the flywheel and is arranged to locate the elements such that the superconducting layers are connected in a ring.

The flywheel housing is made entirely of synthetic fibers or reinforced with synthetic fibers.

The flywheel housing is made entirely of carbon nanotubes or reinforced with carbon nanotubes.

The inertial engine comprises a propulsion system comprising a flywheel, a flywheel driving device and a spiral or ring with a groove on the inner surface facing the axis of rotation, wherein the spiral or ring is made around the flywheel, and a hole is made at the outlet of the spiral or ring with the possibility exit from the hole of the accelerated working fluid.

A system with a mover is connected to a rotary device configured to deploy systems with a mover to create the desired direction of the thrust vector.

A steering wheel is connected to the spiral or to the ring in the region of the hole, which is designed to extend and install at an angle along the flight path of the accelerated departing working fluid from the hole.

A modulator is connected to the valve, which is configured to open the working fluid to the valve at strictly calculated time intervals, while the modulator comprises a slotted disk connected to the disk rotation system.

A fluid or fraction is made as a working fluid.

The inertial engine comprises a flywheel rotational drive device comprising a flywheel made around a system of ball bearings embedded in one another such that, in a pair of two adjacent ball bearings, the inner ball bearing is embedded in the outer ball bearing so that the balls or rollers of the outer ball bearing are made to roll along the ring of the inner ball bearing, and at least two such pairs are made.

A system with a propulsion device is connected to a charger configured to charge an accelerated working fluid with an electric charge of a certain sign at the exit of the flywheel, while a device for changing the direction of flow of the accelerated working fluid is connected to a charging device with an electrode system containing at least two electrodes.

A system with a propulsion device is connected to a current source and a device for changing the direction of flow of the accelerated working fluid, containing at least one magnetic coil.

The propulsion system is connected to the vehicle or is made in a submarine, while at least two propulsion systems are connected to the car or are made in the submarine.

Such a technical solution provides the possibility of creating traction in the airless space of space, since it allows the flywheel to eject the working fluid accelerated during rotation in a certain direction, thereby creating reactive traction.

This is due to the fact that the flywheel is accelerated together with the working fluid made in the cavity of the flywheel housing. Then, using the remote control, the valve is opened, and the working fluid accelerated during rotation due to centrifugal forces leaves the cavity, creating a jet thrust. This jet thrust can be used when moving an object in any environment. And in the airless space of outer space, and in water, and on land.

Also, this technical solution makes it possible to increase the specific energy content per unit weight of the inertial engine more than the specific energy content in chemical fuel due to the fact that the stored energy in the working fluid, rotated together with the flywheel, increases with increasing radius with speed faster than increasing centrifugal breaking loads.

Also, this technical solution makes it possible to increase the flow rate of the working fluid in comparison with chemical rocket fuel also due to the fact that in the working fluid, rotated together with the flywheel, the stored energy grows with the speed faster with increasing radius than the centrifugal destructive loads increase .

Due to this, this technical solution will allow, with a steel flywheel radius of 8 m, the velocity of the expiration of the working fluid to increase to a speed of 53.38 km / s.

This exceeds the maximum flow rate of the combustion products of chemical rocket fuel, which does not exceed 5.7 km / s [2], by 9.37 times.

However, for a significant increase in the specific energy content in the flywheels, there are additional possibilities. For this, for example, new materials can be used to manufacture the flywheel: synthetic fibers and, primarily, carbon nanotubes. Kevlar and carbon fiber synthetic fibers can increase the strength of the flywheel up to 20 times per unit of its weight compared to steel, carbon nanofibers can increase this figure hundreds of times, since carbon nanofibres are 78.7 times stronger and much lighter than steel. Information on the manufacture of twisted ropes 10 km long has been published [Popular Mechanics No. 2, 2010, p. 42].

In another case, Kevlar can increase the specific strength of the flywheel per unit of its weight by 20 times compared with steel, carbon fiber in the range from 10 to 20 times, and carbon nanotubes can increase its strength by 78.7 times [Bogdanov K.Yu. How can we calculate the strength of a carbon nanotube, March 20, 2009, http://www.nanometer.ru/2009/03/19/nanotubes_145296.html; http://tarefer.ru/; www.chemnet.ru/rus/jvho/2001-2/56.pdf; http://works.tarefer.ru/94/100071/undex.html; http://e-science.ru/mdex/?id=4630].

Long nanotube manufacturing technologies developed at Cambridge University for the manufacture of a space elevator for NASA. They developed how to make a giant nanoconstruction with a length of 230 thousand kilometers. They developed a new material for the manufacture of nanotubes, and also found a way to combine them repeatedly to form long segments [Nanotubes for a space elevator, RBC daily, Monday January 26, 2009, No. 11 (574), p. 11].

In the manufacture of flywheel housings from carbon nanotubes, flywheels are able to withstand a centrifugal force of 78.7 times more than if they were made of steel.

Due to this, the specific energy content per unit weight can be made orders of magnitude greater than in flywheels made of steel.

This will further increase the specific energy content in the working fluid accelerated by the flywheels, at least up to 78.7 times, compared with chemical rocket fuel. And it will further increase the speed of the expiration of the working fluid up to 8.871 times in comparison with the speed of the expiration of the working fluid of a rocket engine using chemical rocket fuel.

Accordingly, the velocity of the outflow from the flywheels of the working fluid with the help of a magnetic suspension can be increased even up to 8.871 times, and will amount to 473.5 5 km / s.

This exceeds the maximum rate of expiration of chemical rocket fuel combustion products, which does not exceed 5.7 km / s [Space engines: state and prospects. Edited by Cavney L., Moscow, Mir, 1988, p. 415], 83.07 times. Accordingly, in proportion to this value, the flight time to other planets of the solar system will also decrease, compared with the use of known rocket engines using chemical rocket fuel. So if a manned flight to Mars with the return of the astronauts back would have taken earlier than 2 years, now these two years when flying at maximum cruising speed can be reduced to 8.8 days. (Naturally, acceleration time is not taken into account, but only flight at maximum cruising speed.) And given the fact that the gravitational influences of the planets on the calculation of the optimal flight path at such enormous speeds of the expiration of the working fluid do not affect the fuel consumption and flight time , then the total flight time may decrease even further. In this case, the trajectory can be brought as close as possible to a straight line, and the straight line, as you know, is the closest distance between two points.

Accordingly, the specific energy content per unit weight of the accelerated working fluid is proportional to the square of the ratio of the expiration rates of the working fluid, which means that the specific energy content per unit weight of the accelerated working fluid will be 6900.6 times greater.

In addition, this technical solution makes it possible to rotate the fuel in the flywheel and burn it in such a way as to use not only the combustion energy of the fuel, but also its kinetic energy obtained by rotating it in the flywheel to create traction.

In addition, this technical solution makes it possible to fly an aircraft with such an engine in a cloud of volcanic ash, which gives it an advantage over airplanes that cannot fly during volcanic eruptions, since particles of volcanic ash fall inside the aircraft’s engines, melt and turn into glass. This parasitic glassy mass clogs the aircraft engine, cools, hardens and spoils the aircraft engine. In Bogdanov’s inertial engine, this does not happen, since he does not take air inside himself, as happens in airplanes for burning fuel, and therefore does not take volcanic ash inside himself.

No technical solutions were found that fulfill the task with the same technical means.

Figure 1 shows a schematic diagram of an inertial engine Bogdanov.

Figure 2 shows a schematic diagram of a device for bringing the rotation of the flywheel.

Figure 3 shows a schematic diagram of a flywheel with a working fluid and a valve.

Figure 4 shows a schematic diagram of the ring of the device for driving the rotation of the flywheel.

Figure 5 shows a schematic diagram of a system with a propulsion device of the first type.

Figure 6 shows a schematic diagram of a system with a propulsion device of the second type.

Figure 7 shows a top view of a schematic diagram of the inertia engine of Bogdanov.

On Fig shows a top view of a schematic diagram of the inertial engine Bogdanov.

Figure 9 shows a front view of a schematic diagram of the inertial engine of Bogdanov.

Figure 10 shows a rear view of a schematic diagram of the inertial engine of Bogdanov.

11 shows a local section aa.

On Fig shows a local section bB.

The inertial engine of Bogdanov, hereinafter simply the engine of Bogdanov or simply the engine, consists of the following elements.

In the lower part of the engine, on its axis, system 1 is made with a propulsion device of the first type.

System 1 with a propulsion device of the first type comprises devices 2, 3, 4 for driving the flywheel into rotation. Each of the devices 2, 3, 4 for bringing the flywheel into rotation contains a flywheel 5, which accelerates the gap formed by the slices of two electrodes 7, 8 located around the ring 6 and facing each other, partially imitating the shape of hollow half cylinders - duants [Physical Encyclopedia, 1998 , v.5, p.249]. The electrodes are two half rings electrically connected by the inner perimeters of the half conductive pipe. The electrodes are connected to the poles of the high-frequency generator of an external power source through transmission lines, for example, possibly through quarter-wave lines.

The electrodes 7, 8 are connected to the poles of the high-frequency generator of an external power source through transmission lines. The electrodes 7, 8 are made with the possibility of disconnecting from them before the flight of the aircraft or before driving another vehicle with an engine.

On the ring 6, a remotely controlled system 9 with a battery is electrically connected to the conductive plates 10, 11. The battery of the system 9 with a battery is configured to electrically charge conductive plates 10, 11 electrically isolated from each other by charges of opposite signs. The conductive plates 10, 11 with different signs periodically alternate with each other.

For example, the conductive plates 10, 11 with different signs of electric charges are made on opposite sides of the ring 6. The conductive plates 10, 11 are made on the corner segments of the ring 6 with the same alternating period with each other. The conductive plates 10, 11 are arranged to alternately be in the accelerating gap.

Together with the system 9 with a battery or instead of it, systems can be made with an electric generator configured to generate electrical energy when the ring or flywheel is rotated.

Ring 6 and flywheel 5 hold the weight of the elements 12, 13, 14, 15 of the magnetic suspension, for example, containing superconducting magnets.

Elements 12, 13, 14, 15 of the magnetic suspension are made above and below the electrodes 7, 8 of the flywheel driving device with the ability to shield the elements from alternating electric and magnetic fields generated by the electrodes. For example, around the electrodes can be made massive open copper casing, made with the possibility of shielding alternating electric and magnetic fields, made by analogy with a similar casing used for similar purposes in tokamaks.

The fixed elements of the system 1 with the propulsion of the first type are mounted on the housing 18.

Devices 2, 3 to bring the flywheel into rotation are conventionally called upper, and the device 4 to bring the flywheel into rotation is conventionally called lower.

The flywheels of the upper devices 2, 3 for driving the rotation of the flywheel are attached from below along the perimeters of the flywheels of the turbine 16, 17. In this case, the flywheels are made with the possibility of supplying a working fluid to the inner working surfaces of the turbines 16, 17, for example, through the internal cooling channels and pores of the turbines through a turbine cooling system with a flywheel. The turbine cooling system may include remotely controlled valves and nozzles that remotely control the flow of the working fluid to the turbine, for example, by radio.

Bottom of the upper device 3 to bring the rotation of the flywheel made lower device 4 to bring the rotation of the flywheel with the possibility of applying to the turbine 17 an accelerated working fluid. Bottom of the upper flywheel driving device 2, the upper flywheel driving device 3 is made with the possibility of supplying an accelerated working fluid to the turbine 16.

The fixed elements of the system 1 with the propulsion of the first type are mounted on the housing 18.

All flywheels, except for the flywheel of the upper flywheel driving device 2, comprise the following elements.

In the cavity in the housing 19 of each flywheel, a working fluid 20 is made. In the cavity in the housing 19 of each flywheel, in addition to the flywheel of the upper flywheel driving device 2, a valve 21 is made, which is able to open and close by remote control, for example, by means of a radio . At the same time, it is possible that, when the valve 21 is open, from the inner cavity of the flywheel housing 19 during its rotation, the working fluid 20 flows out under the action of centrifugal force. The lateral surface of the flywheel housing 19 is made inclined with an inclination towards the valve with the possibility of directing the working fluid towards the valve by centrifugal force.

The flywheel of the upper device 2 for driving the rotation of the flywheel is connected to the turbine cooling system and is configured to feed its working fluid to the inner working surface of the turbine 16 connected to it through the turbine cooling system.

The turbine cooling system is configured to create a kind of protective film from the working fluid on the inner working surface of the turbine.

The flywheel of the upper flywheel driving device 3 is connected to the turbine cooling system and is configured to feed its working fluid to the inner working surface of the turbine 17 connected to it through the turbine cooling system.

The flywheels of the devices 2, 3, 4 of bringing the flywheel into rotation are configured to feed the accelerated working fluid to the turbines 16, 17. The turbines 16, 17 are configured to direct the working fluid incident on them with their blades downward with the ability to create reactive thrust.

The first models of the Bogdanov inertia engine, in which a very high speed of rotation of the flywheels may not yet be achieved, can be made with the possibility of using additional thrust arising from the combustion of chemical rocket fuel in their work.

For this purpose, fuel fuel is made in one or two devices 2, 3, 4 of turning the flywheel in the flywheel as the working fluid, and in the other or in the other devices 2, 3, 4 of turning the flywheel in the flywheel as the working fluid made oxidizer fuel.

It is better to place the fuel oxidizing agent in the flywheel of the upper flywheel driving device 2, and the fuel fuel is better located in the flywheel of the lower flywheel driving device 4 and in the flywheel of the upper flywheel driving device 3.

Bottom of the devices 2, 3, 4 of bringing into rotation of the flywheel made nozzle 22.

At the bottom of the flywheel is a double cryostat 23, which consists of two parts. The inner part contains a cryostat with liquid helium, placed in the outer part containing a cryostat with liquid nitrogen. Inside the cryostat 23, a system 24 for changing the position of elements of a system of 25 structures with superconducting layers separated by a dielectric with a high electrical resistivity is made.

In this case, the system 24 of changing the position of elements of the system 25 of structures with superconducting layers separated by a dielectric with high electrical resistivity is configured to be remotely controlled, for example, by radio, and electrically powered either by a battery connected to it or a generator connected to it and generating electricity when the flywheel rotates.

Moreover, the system 24 of changing the position of the elements of the system 25 of structures with superconducting layers separated by a dielectric with high electrical resistivity is configured to arrange the elements of the system of 25 structures with superconducting layers separated by a dielectric with high electrical resistivity, so that the superconducting layers are in the same position are connected in rings located below the flywheel, and in another position the elements are disconnected and the rings are not formed.

In this case, the disk or ring contains a structure containing 50 layers of a superconductor separated by a dielectric with high electrical resistivity (electrical insulator), or more than 50 layers of a superconductor separated by a dielectric with high electrical resistivity.

Such a system of 25 structures with superconducting layers can be taken as an element from Bogdanov’s electromagnetic motor to create traction on new physical principles [Bogdanov’s electromagnetic motor to create traction on new physical principles. Patent No. 2200875. Application No. 2001012072. Priority 05/17/2000], which contains either a disk or a ring and a disk or ring rotation system configured to rotate the disk or ring, wherein the ring or disk is made inside the cryostat, the cryostat being able to rotate together with the ring.

For example, with the ability to stack the elements of the system - the structure in the form of an accordion or to install them in the form of a stack one above the other.

Around the system 1 with the propulsion device of the first engine type, the upper systems 26, 27 with the propulsion device of the second type and the lower systems 28, 29 with the propulsion device of the second type are made.

In these systems, it may be possible to create a vacuum and maintain a vacuum on Earth with the ability to create traction only in outer airless space.

In each system with a propulsion device of the second type, a device 30 for rotating the flywheel into rotation is made, around which a spiral 31 is made with a groove on the inner surface facing the axis of rotation. (Instead of a spiral, a ring with a similar trough can be made.) At the exit from the spiral, a hole is made that can allow the working fluid to exit through it.

In some systems with a propeller of the second type, it is intended to rotate the flywheels in one direction, and in others - in the opposite direction, and their spirals are twisted in the same directions.

In the flywheels of the upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion, a modulator 32 is made with the ability to open the access of the working fluid to the valve at strictly calculated time intervals, when the accelerated working fluid departing from the valve will be directed according to preliminary calculation strictly in the direction of the spiral hole. The modulator 32 comprises a slotted disk connected to a disk rotation system configured to rotate the disk so that the slot is opposite the valve at pre-calculated times when the valve is opposite the spiral hole.

Any liquid, such as water, or balls, such as shot or buckshot, can be used as a working fluid.

The upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion are connected to rotary devices 33, 34, 35, configured to deploy the systems with the second type of propulsion relative to each other to create the desired direction of the thrust vector.

Depending on the velocity of the expiration of the accelerated working fluid, various versions of the upper systems 26, 27 with the propulsion device of the second type and the lower systems 28, 29 with the propulsion device of the second type are possible.

Options can be successfully implemented in a single engine.

To work with a relatively low velocity of the expiration of the accelerated working fluid, the following version of their execution is performed.

At the exit from the spiral 31, rudders 36, 37 are made, with the possibility of alternately extending and installing at an angle on the path of departure from the hole of the accelerated departing working fluid.

Steering wheels and spirals can be made with the possibility of supplying to their working surfaces a cooling system of the steering wheels and spirals of coolant, for example, through cooling channels and through pores with the possibility of creating a protective film on their surface. As a cooling liquid, a substance of the working fluid, for example, water, can be used. To increase the cooling power can use liquid metal, for example, aluminum. In this case, known cooling devices for turbine turbine engine turbines and the first wall of a thermonuclear reactor can be copied.

Graphite powder spraying systems 38, 39, 40 are connected to the spiral 31 and to the rudders 36, 37, made with the possibility of spraying graphite powder on the inner working surfaces of the spiral 31 and rudders 36, 37 with the ability to protect the spiral 31 and rudders 36, 37 from destruction fall time on them with a high speed of the working fluid. Steering wheels 36, 37 can be made either in the form of blades of a blade, or in the form of plates of metal, or of cermet with the possibility of cooling, for example, water entering through the pores, or liquid metal entering through the pores.

To operate at a relatively high velocity of the expiration of the accelerated working fluid for low-thrust flights, the following embodiment can be added to the first option.

To operate at a high velocity of the expiration of the accelerated working fluid for flights with low thrust instead of rudders, and possibly with them, devices made of electronic, ionic and plasma optics can be made. In this case, a conductive fluid, such as sea water, or conductive balls, such as metal shot or buckshot, are used as the accelerated working fluid.

In this case, at the exit from the spiral 25, a charger is configured to charge the accelerated working fluid with an electric charge of a certain sign. With the exit from the spiral 25, the electrodes of the device for changing the direction of flow of the accelerated working fluid are connected.

Also, instead of electrodes, magnetic coils and a starting device can be used along two streams of an accelerated working fluid of electric current. Coils can be superconducting.

Also, at the exit of spiral 25, a plasma-optical system with crossed electric and magnetic fields can be made.

The operation of all elements is coordinated and controlled by the on-board computer.

Compartment 41 for the payload of the system 1 with the propulsion device of the first type inside may contain various rooms. Inside the compartment 41 for the payload, the control cabin, the living compartment of the aircraft crew, the payload, and the retractable ladder or elevator for lowering and raising the crew can be made.

Around each of the upper systems 26, 27 with the propulsion device of the second type and the lower systems 28, 29 with the propulsion device of the second type, a device 42 for bringing the atmosphere into rotation is made. The atmospheric gas rotation device 42 is made on the basis of elements of Bogdanov’s patented electric rocket engine [I. Bogdanov Electric rocket engine Bogdanov. Patent No. 2046210. Application No. 5064411. The priority of the invention on October 5, 1992]. Atmospheric gas rotation device 42 is configured to ionize atmospheric gas and bring gas into rotation either in one direction around the axis or rotate in opposite directions relative to the plane of symmetry of the device so that the gas flies behind the device and creates additional reactive thrust. The device 42 comprises an external housing on which ionizers and a system of sectioned electrodes are made, connected to a coil of an external magnetic field, configured to create crossed electric and magnetic fields with the possibility of ionizing atmospheric gas and bringing it into rotation in crossed electric and magnetic fields. The external magnetic field coil can be made in the form of a Bogdanov’s patented magnetic coil with the possibility of feeding currents in opposite directions so that an optimal magnetic field configuration is formed to bring the atmosphere into rotation. The coil can be multi-turn. Also, the coil of the external magnetic field can be made in the form of a curved restriction coil. The atmospheric gas driving devices of various upper systems 26, 27 with a second type propulsion device and lower systems 28, 29 with a second type of propulsion system are matched to each other. These devices are configured to ionize atmospheric gas and bring it into rotation in crossed electric and magnetic fields and around rotary devices 33, 34, 35.

Atmospheric gas rotation device 42 is electrically connected to a generator connected to the flywheel with the possibility of generating electricity from the rotation of the flywheel. The outer casing of the atmosphere gas actuator 42 is streamlined.

Inertial engine Bogdanov works as follows.

At start, system 1 works with the first type of propulsion.

System 1 with a propeller of the first type rotates the flywheels in devices 2, 3, 4 of bringing the flywheel into rotation. Each of the devices 2, 3, 4 bringing in rotation of the flywheel operates as follows. First comes the process of energy storage in the device.

The flywheel 5 rotate the elements of the device to bring the flywheel into rotation. This device is made by analogy with the charged particle accelerator cyclotron and works by analogy with it.

It is known that the cyclotron periodically delivers a high-frequency alternating electric field to the accelerating gap formed by sections of two electrodes located around the flywheel and facing each other, having the form of hollow half-cylinders - duants [Physical Encyclopedia, 1998, v.5, p.249]. Duants are connected to the poles of a high-frequency generator through transmission lines, for example, possibly through quarter-wave lines.

In more detail, the flywheel rotation drive device operates as follows.

An external power source, such as a nuclear or thermonuclear power plant, periodically supplies a high-frequency alternating electric field to an accelerating gap formed by slices of two electrodes 7, 8 located around the ring 6 and facing each other, partially imitating the shape of hollow half-cylinders - duants [Physical Encyclopedia, 1998 ., t.5, p.249]. The electrodes are two half rings electrically connected by the inner perimeters of the half conductive pipe. The electrodes are connected to the poles of the high-frequency generator of an external power source through transmission lines, for example, possibly through quarter-wave lines. It is advisable to use a nuclear power plant with fast neutron reactors as an external power source, the development of which has become a priority for Rosatom, since it allows you to get 100 times more energy per unit of nuclear fuel and allows you to use junk uranium 238, which is very much in dumps. In addition, it is advisable to use a hybrid fusion reactor - a hybrid - as an external energy source. Demonstration thermonuclear reactors with an energy output of 1-2 have already been created. The energy yield in such a reactor can be increased by using waste uranium 238 or thorium 233 to produce additional energy, which in the fusion reactor will produce new fissile materials for a nuclear power plant.

The electrodes 7, 8 are disconnected from an external power source before the flight of the aircraft or before driving another vehicle with an engine.

Each of the devices 2, 3, 4 bringing the rotation of the flywheel rotates the flywheel 5 using the ring 6. Ring 6 rotate the electrodes 7, 8 of the device for bringing the rotation of the flywheel as follows.

On the ring 6 there is a remotely controlled system 9 with a battery connected to the conductive plates 10, 11. The battery of the system 9 with a battery electrically charges the conductive plates 10, 11 electrically isolated from each other by charges of opposite signs. The conductive plates 10, 11 with different signs periodically alternate with each other.

For example, conductive plates 10, 11 with different signs of electric charges are made on opposite sides of ring 34. In this case, plates with one sign of electric charge and plates with opposite signs of electric charge in the gap by an electric field are accelerated in opposite directions, increasing the torque of the ring or flywheel .

The conductive plates 10, 11 are made on the angular segments of the ring 6 with the same periods of alternation with each other, which are correlated with the frequency of the alternating voltage supplied to the electrodes. With an increase in the rotational speed of the ring 6, the frequency of the alternating voltage supplied to the electrodes 7, 8 of the flywheel driving device increases synchronously.

The conductive plates 10, 11 are located in an accelerating gap, to which an alternating electric field is applied, which accelerates the plates together with the ring 6 and the flywheel 5 and makes them rotate with acceleration. An alternating electric field is changed synchronously with a change in rotational speed.

The rotation speed is increased to a certain critical value, limited from above by the strength of the material of the rings and the flywheel.

Together with systems with a battery, systems with electric generators can be made that generate electrical energy when the rings or flywheels rotate.

Ring 6 and flywheel 5 hold the weight of the elements 12, 13, 14, 15 of the magnetic suspension, for example, containing superconducting magnets, ring rails and electrodes.

The elements of the magnetic suspension 12, 13, 14, 15 can use not only magnetic fields, but also electric fields to keep the flywheel 5 and the ring 6. The sensors can also use a feedback system that controls the position of the flywheel 5 and the ring 6 and giving signals to the adjustment system of the magnetic suspension. They can also use in their work the well-known effect of freezing of a superconductor over a magnet - the so-called “Coffin of Magomed" effect.

It is necessary to use a magnetic suspension above and below the electrodes 7, 8 of the flywheel driving device for the reason that the alternating electric and magnetic fields heat the superconducting magnets of the magnetic suspension until the destruction of superconductivity. Therefore, the electrodes 7, 8 of the flywheel driving device must be made outside of the magnetic suspensions. And the best arrangement of the electrodes 7, 8 of the device for bringing the flywheel into rotation and, accordingly, the ring 6 is the location between the elements of the magnetic suspension 12, 13, 14, 15 at a distance from them.

Elements 12, 13, 14, 15 of the magnetic suspension are made above and below the electrodes 7, 8 of the flywheel driving device with the ability to shield the elements from alternating electric and magnetic fields generated by the electrodes. For example, around the electrodes can be made massive open copper casing, made with the possibility of shielding alternating electric and magnetic fields, made by analogy with a similar casing used for similar purposes in tokamaks. In elements containing ring rails, a current is introduced along the ring rails and the flywheel is suspended by the repulsive force between currents of opposite directions. In the elements containing the electrodes, electric fields are created between the electrodes so that the emerging electric force of repulsion or attraction maintains the necessary gap between the elements of the magnetic suspension.

Since the cyclotron is capable of accelerating charged particles to relativistic speeds, the speeds to which the proposed flywheel drive device can accelerate the flywheel are limited from above only by the strength of the materials of the flywheel and rings.

In adjacent devices 2, 3, 4 of bringing the flywheel into rotation, the flywheels rotate in opposite directions.

Together with the flywheel, the upper flywheel driving devices 2, 3 rotate the turbines 16, 17 attached to their flywheels from below along their perimeters and supply a working fluid to their inner surfaces. In this case, the supply of the working fluid to the turbines can be carried out through the internal cooling channels and pores of the turbines connected through the cooling system of the turbines to the flywheel. The turbine cooling system may include remotely controlled valves and nozzles that remotely control the flow of the working fluid to the turbine, for example, by radio.

Bottom of the upper flywheel driving device 3, the accelerated working fluid feeds the lower flywheel driving drive device 4 to the turbine 16. Bottom of the upper flywheel driving device 2, the accelerated working medium is supplied to the turbine 17 by the upper flywheel driving driving device 3.

The fixed elements of the system 1 with the propulsion of the first type are mounted on the housing 18.

All flywheels, except the flywheel of the upper device 2 to bring the rotation of the flywheel, work as follows.

From the cavity in the housing 19 of each flywheel, the working fluid 20 is released by a valve 21, which is opened and closed by remote control. With the valve 21 open, the working medium 20 flows out from the inner cavity of the flywheel housing 19 by centrifugal force. The lateral surface of the flywheel housing 19 is made inclined with an inclination towards the valve with the possibility of directing the working fluid towards the valve by centrifugal force.

The flywheel of the upper device 2 for driving the rotation of the flywheel instead of the valve 21 delivers its working fluid to the inner working surface of the turbine connected to it through the cooling system of the turbine.

The turbine cooling system creates a semblance of a protective film from the working fluid on the inner working surface of the turbine, which protects its blades from another working fluid flying at high speed.

The flywheels of the devices 2, 3, 4 for bringing the flywheel into rotation supply the accelerated working fluid to the turbines 16, 17. The turbines 16, 17 direct the working fluid falling on them with their blades, creating a jet thrust.

The first models of the Bogdanov inertia engine, in which a very high rotation speed of the flywheels may not yet be achieved, can use additional thrust in their work arising from the combustion of chemical rocket fuel.

For this purpose, fuel oil was used in one or two devices 2, 3, 4 of turning the flywheel in the flywheel as a working fluid, and in the other or in other devices 2, 3, 4 of turning the flywheel in the flywheel as a working fluid used oxidizer fuel.

It is better to place the fuel oxidizing agent in the flywheel of the upper flywheel driving device 2, and the fuel fuel is better located in the flywheel of the lower flywheel driving device 4 and in the flywheel of the upper flywheel driving device 3.

The rotation of the flywheels with the working fluid gives the working fluid additional kinetic energy. The working fluid 11 emitted from the flywheels of the devices 2, 3, 4 for driving the rotation of the flywheel enters the turbines 16, 17. The turbines drop the working fluid that has fallen onto them so that the impulse component appears along the axis of the working fluid. This component of the pulse creates reactive thrust. Since the working fuel directed from different flywheels contains fuel fuel and a fuel oxidizer, the oxidizer and fuel mix, burn and create additional rocket propulsion. Thus, the thrust impulses obtained due to the rotation of the flywheels and the combustion of the fuel add up and the thrust increases.

The flame of the burning fuel formed by mixing the fuel and the oxidizing agent enters the nozzle 22 and creates a reactive thrust with a separate direction of release of the products of fuel combustion.

At the bottom of the flywheel is a double cryostat 23, which consists of two parts. The inner part contains a cryostat with liquid helium, placed in the outer part containing a cryostat with liquid nitrogen. Inside the cryostat 23, a system 24 for changing the position of elements of a system of 25 structures with superconducting layers separated by a dielectric with a high electrical resistivity (electrical insulator) is made.

In this case, the system 24 of changing the position of elements of the system 25 of structures with superconducting layers separated by a dielectric with a high electrical resistivity is remotely controlled, for example, by radio, and is electrically powered either by a battery connected to it or a generator connected to it and generating electricity when rotating the flywheel.

At the same time, the system 24 of changing the position of the elements of the system of 25 structures with superconducting layers separated by a dielectric with high electrical resistivity, when taking off and flying near the surface of the celestial body, has elements of the system 25 of structures with superconducting layers so that the superconducting layers are connected into rings located below flywheel.

In this case, the disk or ring contains a structure containing 50 layers of a superconductor separated by a dielectric with high electrical resistivity (electrical insulator), or more than 50 layers of a superconductor separated by a dielectric with high electrical resistivity.

During rotation of a disk or ring containing 50 layers of a superconductor separated by an insulator, or more than 50 layers of a superconductor separated by an insulator, a weight reduction of 2 percent is observed over each layer of a superconductor. This phenomenon has been experimentally confirmed [Article on the topic "Scientific research". Russian scientists discovered antigravity. © 2008 ScienceArt.Ru

http: //scienceart.m/researches/rossiyskie_ucheme_otkrili_antigravitaciyu.html.

At the same time, a decrease in weight by 4 percent is observed over two layers of a rotating superconductor, which also found experimental confirmation.

Thus, over all 50 layers of a rotating superconductor, a complete decrease in weight is observed, which makes it possible to reduce energy costs when launching a payload located above rotating structures with superconductor layers into orbit (or when flying to another celestial body).

This effect of reducing weight over a rotating structure with superconducting layers separated by a dielectric with high electrical resistance is an additional effect in the operation of an inertial motor, which can be used in its work, but may not be used in its work.

Such a system of 25 structures with superconducting layers can be taken as an element from Bogdanov’s electromagnetic motor to create traction on new physical principles [Bogdanov’s electromagnetic motor to create traction on new physical principles. Patent No. 2200875. Application No. 2001012072. Priority 05/17/2000], which contains either a disk or a ring and a disk or ring rotation system configured to rotate the disk or ring, wherein the ring or disk is made inside the cryostat, the cryostat being able to rotate together with the ring.

When landing, on the contrary, the system 24 of changing the position of the elements of the system of 25 structures with superconducting layers separated by a dielectric with high electrical resistivity changes the position of the elements so that rings from the connected superconducting layers of structures are not formed. For example, it adds up the elements of the system - the structure in the form of an accordion or sets them in the form of a stack one above the other. In this case, the effect of weight reduction over a rotating structure with superconducting layers separated by a dielectric with high electrical resistance is not formed and landing is carried out without counteracting this effect.

This eliminates the above drawback of the Bogdanov electromagnetic motor for creating traction on new physical principles [The Bogdanov electromagnetic motor for creating traction on new physical principles. Patent No. 2200875. Application No. 2001012072. Priority 05.17.2000], which is the fact that an effective mechanism is not provided that removes the effect of reducing gravity over a rotating superconductor without removing it from the superconducting state or without removing it from rotation. Elimination of the drawback allows landing without counteracting this effect during landing of an aircraft with an engine bearing such a rotating structure.

This eliminates the other drawback of the Bogdanov electromagnetic motor for creating traction on new physical principles, which is the fact that there is no effective mechanism for quickly removing and restoring the decrease in gravity over a rotating superconductor without removing it from the superconducting state or without removing it from rotation with a new creating a situation where a superconductor rotates in a superconducting state. Elimination of the deficiency allows multiple repetition of combinations of takeoff and landing of an aircraft with such an engine.

In the work [Burdakov V.P., Danilov Yu.I. Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 37] it is reported that very large energy can be stored in rotating flywheels. For example, in rotating steel flywheels with a diameter of 1.6 cm and a speed of 211,000 rpm, accelerated to such a speed of rotation in a vacuum by electromagnetic fields, an energy of 1.2 · 10 ⁷ J / kg was stored, that is, the same as the top energy limit in chemical rocket fuel. Rotating in a vacuum, the steel flywheels did not experience resistance and retained the stored energy for a long time so that only 19 percent of the stored energy was lost during the year.

Since the speeds to which the proposed flywheel driving device is capable of accelerating the flywheel are limited from above only by the strength of the materials, it means that it is fundamentally possible for these devices to accelerate to those achieved in the work [Burdakov VP, Danilov Yu.I., Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 37] rotation speeds of 211,000 rpm and larger flywheels with the same centrifugal forces.

Moreover, in the work [Burdakov V.P., Danilov Yu.I. Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 36], it is reported that with increasing diameter of a rotating flywheel, the stored energy grows faster than centripetal forces that tend to destroy it with increasing diameter and speed. However, used in the work [Burdakov V.P., Danilov Yu.I. Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 37] The kinetic energy of rotation has a low specific energy per unit weight of the entire battery due to the small size of the steel flywheels. This disadvantage is eliminated by increasing the size of the flywheels. Also, the specific energy content in such energy accumulators with flywheels is reduced by the power supply systems for the device for driving the flywheel into rotation, which use external energy sources in the engine. This disadvantage is eliminated due to the fact that power supply systems do not participate either in the flight of an object (for example, an aircraft) with an engine, or in other movement of an object (for example, an automobile) with an engine or a submarine with an engine.

Therefore, the weight of external power sources does not affect the relative energy content per unit weight of the object with the engine.

Around the system 1 with the first type of propulsion, the flywheels rotate the upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion.

In these systems, it is possible to maintain a vacuum on the Earth and turn them on only in outer airless space and thereby achieve a higher flywheel rotation speed than in the central devices 2, 3, 4 of turning the flywheel into rotation.

In each system with a propulsion device of the second type, the flywheel rotational drive device 30 rotates the flywheel, from which centrifugal forces eject the accelerated working fluid onto the spiral 31 with a groove on the inner surface facing the axis of rotation. (Instead of a spiral, a ring with a similar trench can be made.) Then, the accelerated working fluid moves due to inertia in a spiral and is discharged through an opening made at the exit from the spiral.

In some systems with a propeller of the second type, the flywheels rotate in one direction, and in others in the opposite direction and in the same directions their spirals are twisted.

In the flywheels of the upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion, the modulator 32 allows the working fluid to enter the valve 21 at strictly calculated time intervals, when the accelerated working fluid departing from the valve, according to preliminary calculation, will be sent strictly to direction to the spiral hole. To do this, in the modulator 32, in parallel with the rotation of the flywheel, the slotted disk is rotated using the disk rotation system so that the slot is opposite the valve at pre-calculated times when the valve is opposite the spiral hole.

Any liquid, such as water, or balls, such as shot or buckshot, can be used as a working fluid.

The upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion are rotated relative to each other by the rotary devices 33, 34, 35. The rotary devices rotate the systems with the second type of propulsion relative to each other to create the desired direction of the thrust vector. Thus, a rotation in the horizontal plane can be carried out.

Depending on the flow rate of the accelerated working fluid, different methods of deviating its flow are used.

With a relatively low velocity of the expiration of the accelerated working fluid, the following method is used.

At the exit from the spirals, the accelerated working fluid is directed to the rudders 36, 37, made with the possibility of alternately extending and installing at an angle on the flight path from the opening of the accelerated departing working fluid.

The rudders and spirals can be protected from destruction by supplying coolants and spirals of coolant to their working surfaces, for example, through cooling channels and through pores. The coolant in this case creates a protective film. As a coolant, a working fluid substance, for example water, can be used. To increase the cooling power can use liquid metal, for example, aluminum. In this case, known methods of cooling turbines of turbojet engines and the first wall of a thermonuclear reactor can be copied.

Graphite powder spraying systems 38, 39, 40 spray graphite powder onto the inner working surfaces of the spiral 31 and the rudders 36, 37. The spraying of the graphite powder protects the spiral 31 and the rudders 36, 37 from destruction when the working fluid falls on them. This fact was used in the development of the Orion Project to accelerate a steel plate with low-power nuclear explosions, carried out under the plate. As soon as the sprayed graphite powder protects the steel plate from the products of low-power nuclear explosions incident on it, it will certainly be able to protect the turbine from the working fluid incident on it.

To perform the rotation in the vertical plane, the rudders 36, 37 are extended, installed on the path of the outgoing working fluid. For example, rudders can be made either in the form of blades of a blade, or in the form of plates of metal, or of cermets. At the same time, for rotation in the vertical plane, the upper and lower systems with a propulsion unit of the second type are deployed on opposite sides of the axis of rotation of the flywheels, and the rudders are extended so that the accelerated working fluid that moves away from the upper and lower systems in opposite directions.

To create additional traction along the axis of rotation of the flywheels, the outlet openings of the elements of the lower flywheel systems are installed symmetrically on opposite sides of the axis of rotation, extend the rudders and direct the working fluid reflected from them down from the engine, for example, during takeoff and landing.

Similarly, the upper flywheel systems can create traction, reflecting the rudders falling from them, the working fluid up from the engine, for example, when braking.

This method is used at such velocities of the expiration of the accelerated working fluid at which the rudder material does not collapse upon contact with the flow of the accelerated working fluid.

At a high velocity of the expiration of the accelerated working fluid, as well as for flights with low thrust, methods from electronic and ion optics are used. In this case, the change in the direction of flow of the accelerated working fluid is as follows.

As the accelerated working fluid, a conductive liquid, for example, sea water, or conductive balls, for example, metal shot or buckshot, are used.

In this case, the charger at the exit of the flywheel charges the accelerated working fluid with an electric charge of a certain sign. Then, the accelerated working fluid is sent to the gap between the two electrodes of the device for changing the direction of flow of the accelerated working fluid, the voltage is applied to the electrodes, and the accelerated working fluid having a certain electric charge is rejected in the desired direction. In this case, a pair of flywheels is used, the accelerated working body of which is electrically charged with electric charges of different signs. They create two approximately parallel jets of the accelerated working fluid, which are charged with electric charges of opposite signs, are attracted to each other after exiting the engine, collide with each other and are electrically neutralized. In this method, a pulsed mode of operation is needed, since an electric current will flow when the streams meet and the charges are neutralized.

In another method, instead of electrodes, magnetic coils may be used. Along two streams of the accelerated working fluid, an electric current is released, which is deflected by the magnetic field of the coils, letting the flows in the desired direction. Coils can be superconducting.

In the third method, the flow of the working fluid is rejected by crossed electric and magnetic fields.

The operation of all elements is coordinated and controlled by the on-board computer.

Compartment 41 for the payload of the system 1 with the propulsion device of the first type inside may contain various rooms. Inside the compartment 41 for the payload, the control cabin, the living compartment of the aircraft crew, the payload, and the retractable ladder or elevator for lowering and raising the crew can be made.

Around each of the upper systems 26, 27 with the second type of propulsion and the lower systems 28, 29 with the second type of propulsion, the atmosphere gas driving device 42 rotates the atmosphere gas. Atmospheric gas rotation device 42 is made on the basis of elements of Bogdanov’s patented electric rocket engine [5]. Atmospheric gas driving device 42 ionizes the atmospheric gas with ionizers. Then, around the outer casing on which the ionizers are made, a system of sectioned electrodes creates electric fields. A coil of an external magnetic field creates magnetic fields. This creates crossed electric and magnetic fields so that the gas comes into rotation in crossed electric and magnetic fields.

In this case, the gas is rotated either in one direction around the axis so that the rotation decreases the resistance of the leaking masses of gas, or the gas is rotated in different directions relative to the plane of symmetry of the device so that the gas flies behind the device and creates additional reactive thrust while reducing the resistance of the leaking atmospheric gas masses. Similarly, these devices can create traction in any conductive fluid, such as sea water. Thus, the engine can create traction both as the engine of a submarine, including a flying one, and as the engine of a surface ship. Also, the engine, accelerating atmospheric gas, can create traction for an hovercraft and for an ekranoplan.

The external magnetic field coil can be made in the form of a Bogdanov’s patented magnetic coil and can be powered by currents of opposite directions so that an optimal magnetic field configuration is formed to bring the atmosphere into rotation. The coil can be multi-turn. Also, the coil of the external magnetic field can be made in the form of a curved restriction coil. The operation of atmospheric gas driving devices of various upper systems 26, 27 with a second type propulsion and lower systems 28, 29 with a second type of propulsion is coordinated between various devices and optimized using a computer. These devices ionize atmospheric gas and cause it to rotate in crossed electric and magnetic fields and around rotary devices 33, 34, 35.

Similarly, these devices can create traction in any conductive fluid, such as sea water.

Electric energy for the operation of the device for bringing the atmospheric gas into rotation is provided by a generator connected to the flywheel, which receives it from the rotation of the flywheel.

The use of the inertial engine of Bogdanov in the country's energy system

The engine can be used to transfer energy accumulated in rotating flywheels from power plants made near energy sources, or from energy sources themselves to power plants made near energy consumers, or to energy consumers themselves. Sources of energy can be gas, oil, coal, geothermal sources, as well as volcanoes.

In this case, the flywheels of the engine can be powered by power from power plants made near energy sources, or from the energy sources themselves.

For example, they build power plants where there are deposits of gas, oil, coal, geothermal springs or volcanoes.

In another embodiment, power plants can transport aircraft with the inertial engine of Bogdanov. For this, in the simplest version, the power plant contains a boiler with a generator mounted on top. The boiler is mounted on a tripod, the height of which is slightly higher than the height of the pipe on which the associated gas is burned. A tripod with a boiler is installed over a pipe in which associated gas is burned. Burning gas heats the boiler, water boils, rotates the generator turbine, and the power plant generates electricity. Water is sent to the boiler by a pump through a hose from the nearest body of water.

In another embodiment, a boiler with a generator mounted on top is lowered into the mouth of a volcano. The volcano heats the boiler, the water boils, rotates the generator turbine, and the power plant generates electricity. Water is also sent to the boiler by a pump through a heat-resistant hose made of fire-resistant materials from the nearest body of water. Moreover, if the lava level is lower than the water level in the nearest body of water, then the water is only sent by the pump first, and then flows into the boiler itself according to the law of communicating vessels.

They generate cheap electrical energy. This flywheel is powered by the flywheels of the inertial engine of Bogdanov and transferred by the aircraft with this engine the stored energy to the energy consumers. There, the stored energy is redistributed. For example, water, air or natural gas can be passed through a Bogdanov’s inertial engine installed in a power plant and heated by a working fluid that leaves the flywheel at high speed.

Water heats up, boils, steam forms, steam rotates the turbine of the power plant, the power plant generates electricity. In another case, heated air or natural gas increases the combustion temperature of the fuel and provides additional heat to generate electricity. In addition, heated water can be used in steam or water heating systems in cities.

The resulting electric power can be powered by other inertial engines of Bogdanov to repeat the process.

Such a method of energy transfer for Russia will give a significant profit due to the following factors.

1. It will save energy due to transport energy losses during its transmission by wire over a considerable distance.

2. Accelerate energy transfer due to the fact that you do not need to build a long power line for a long time, but you can quickly transfer a significant amount of energy to aircraft with Bogdanov's inertial engine.

In addition, tankers for transporting liquefied gas and oil can be built on the basis of the inertial engine of Bogdanov. Tankers can be floating, underwater, flying, hovercraft and ekranoplans.

In addition, if we consider the entire set of technical and economic parameters of this method of energy transfer and distribution based on the inertial engine of Bogdanov, then we can say the following.

On its basis, a grandiose project to change the entire energy system of the country can be created, which will bring benefits and will have advantages in the following respects.

1. The country - a huge profit from the development of remote oil and gas fields, including the Arctic. Agree, the development of the Arctic shelf is already a priority state task, which means - this is another reason to give carte blanche to my Project !!!

2. The solution to the problem of associated gas at all oil fields - if it cannot be transported, it can simply be burned in the furnaces of gas power plants.

3. The solution to the problem of deterioration of power lines. Energy is not transferred through them, but in superconducting second magnetic coils reinforced with carbon nanotubes.

4. The obvious benefit and direct benefit is that, firstly, there are no energy losses in power lines. Secondly, it is not necessary to make clearings in the dense taiga, it is not necessary to drain swamps in Siberia and the tundra on the path of power lines, and it is not necessary to pull power lines through wide rivers and taiga mountain ranges.

5. There is no alienation of the territory under power lines in the case when they pass through fields and cities - through territories that are somehow involved in the national economy.

6. It is possible to dismantle worn-out power lines, and build elite villages on their territory. Land from worn out power lines can be sold and made a profit.

7. There is an opportunity to get additional profit from unprofitable deposits today, for example, from offshore fields, and make them profitable due to this.

8. It is possible to use decommissioned submarines as tankers for liquefied natural gas and oil, which will transport surface or submarines with the Bogdanov inertia engine.

9. All of the listed transport resources are possible for the development of the Arctic, which will give Russia advantages in this matter.

10. In the context of the global crisis, the project will provide Russia with the creation of new jobs and will not allow the development of mass unemployment.

11. Allows you to use the huge potential of military factories for the construction of nuclear submarines with the aim of building a peaceful version of underwater (surface) supertankers based on the Bogdanov inertial engine with the possibility of transporting both liquefied gas and oil, and superconducting magnetic coils, as well as platforms for developing offshore oil fields and gas. In this case, it is possible to create underwater caravans from a variety of submarine tankers filled with liquefied gas or oil, driven by two nuclear submarines in which missile hatches are replaced by tanks for storing liquefied gas or oil.

12. It is known that in flywheels the specific density of accumulated energy increases with increasing size. This means that with an increase in the size of the system, the specific energy density will be several orders of magnitude higher than the specific energy density in both oil and liquefied gas. Even by many orders of magnitude !!! And this is a direct benefit in transporting energy.

Calculations and additions

Discussion about the size, rotation speed and strength of materials

The calculations are made both for the general case and for the special case of a system of ball bearings embedded in each other. The calculation results can also be used for systems with magnetic suspensions.

To increase the ratio of the weight of the flywheels to the weight of the energy accumulator itself, the following technical solutions should be implemented.

The flywheel is rotated on ball bearings. However, when the flywheel rotates around the shaft on ball bearing rollers, a limitation of the angular speed of rotation for steel rollers 1174 radians per second occurs [Energy storage and switching of high densities, Moscow, Mir, 1979, p. 303]. To increase this restriction, the author uses systems of ball bearings embedded in each other to rotate the entire flywheel. In each such system, the rollers or balls of each subsequent outer ball bearing roll on the outside of the outer ring of the previous inner ball bearing, using it as a shaft. Thus, using 1000 pairs of such ball bearings, the angular velocity of rotation can be increased 1000 times. Moreover, in the center-of-mass system of each inner ball bearing ring of each pair of roller loads, they will be the same as if this ring was a fixed shaft.

For calculations, it is enough to take either 211 pairs of ball bearings, or 1000 and take steel rollers with a diameter of steel flywheels of 1.6 cm as rollers from the version of the work [Burdakov VP, Danilov Yu.I. Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 37]. If we take the thickness of the rings equal to the radii of the rollers, then the thickness of the entire system is equal to its radius without the radius of the shaft

Accordingly, for 1000 pairs of ball bearings we get

1000 × 1.6 × 2 cm = 1000 × 3.2 cm = 3200 cm = 32 m.

The energy stored in the flywheel is proportional to the product of the mass of the flywheel, the second degree of the radius of the flywheel and the second degree of the angular velocity of rotation [Energy storage and switching of high densities, Moscow, Mir, 1979, p. 302; Yavorsky B.M., A.A. Detlaf. Handbook of Physics. Moscow, Science, Fizmatlit, 1996, p. 50].

m is the mass of the flywheel,

R is the radius of the flywheel,

ω is the angular velocity of rotation.

Centrifugal forces are proportional to the first degree of the radius of the flywheel and also the second degree of the angular velocity of rotation

Thus, in order to prevent the flywheel from being destroyed by centrifugal forces, with increasing radius, the angular velocity of rotation should be reduced in proportion to the square root of the increase in radius. But with this decrease in angular velocity, the energy stored in the flywheel will still grow at a faster rate in proportion to the first degree of increase in radius.

Linear speed during rotation of the flywheel is

Thus, with increasing radius with a constant centrifugal force, the linear speed of the flywheel should increase in proportion to the square root of its radius.

Thus, the system of ball bearings embedded in each other allows for steel flywheels from the material of the work option [Burdakov VP, Danilov Yu.I. Physical problems of space traction energy, Moscow, Atomizdat, 1969, p. 37] with an increase in their diameters over 1.6 cm, increase the stored energy in the range from 211 to 1000 times. They will also allow to increase the linear rotation speed of steel flywheels in the range from the root of 211 to the root of 1000 times with a radius of a system of ball bearings embedded in each other without a shaft radius of 6.752 m to 32 m.

In this case, they will also allow to increase the linear rotation speed of steel flywheels in the range from the root of 211 to the root of 1000 times.

If we now consider that the working fluid is flowing out of the side surface of the flywheels, then, accordingly, the velocity of the outflow from the flywheels of the working fluid will increase in the range from the root of 211 to the root of 1000 times, that is, in the range from 14.5258 to 31.6228 times .

For a flywheel with a radius of 0.8 cm, rotating at a speed of 211,000 rpm, the linear rotation speed is

Accordingly, the velocity of the outflow from the flywheels of the working fluid using systems of ball bearings embedded in each other will increase in the range from 14.5258 to 31.6228 times and will be

14.5258 × 1688 m / s≤v≤31.6228 × 1688 m / s

24519.6 m / s≤v≤53379.3 m / s

Or, if you convert meters to kilometers,

24.5 km / s≤v≤53.4 km / s

This exceeds the maximum rate of expiration of the products of combustion of chemical rocket fuel, which does not exceed 5.7 km / s [2], in the range of times from 4.30 to 9.37 times.

However, for a significant increase in the specific energy content in the flywheels, there are additional possibilities. For this, for example, new materials can be used to manufacture the flywheel: synthetic fibers and, primarily, carbon nanotubes. Kevlar and carbon fiber synthetic fibers can increase the strength of the flywheel up to 20 times per unit of its weight compared to steel, carbon nanofibers can increase this figure hundreds of times, since carbon nanofibres are 78.7 times stronger and much lighter than steel. Information on the manufacture of twisted ropes 10 km long has been published [Popular Mechanics No. 2, 2010, p. 42].

For example, Kevlar can increase the specific strength of a flywheel per unit of its weight by 20 times compared with steel, carbon fiber in the range from 10 to 20 times, and carbon nanotubes can increase its strength by 78.7 times [Bogdanov K.Yu. How can we calculate the strength of a carbon nanotube. March 20, 2009, http://www.nanometer.ru/2009/03/19/nanotubes_145296.html; http://tarefer.ru/; www.chemnet.ru/rus/jvho/2001-2/56.pdf; http://works.tarefer.ru/94/100071/index.html; http://e-science.ru/mdex/?id=4630].

Long nanotube manufacturing technologies developed at Cambridge University for the manufacture of a space elevator for NASA. To do this, you need a giant nanoconstruction with a length of 230 thousand kilometers. They developed a new material for the manufacture of nanotubes, and also found a way to combine them repeatedly to form long segments [Nanotubes for a space elevator, RBC daily, Monday January 26, 2009, No. 11 (574), p. 11].

In the following, we give a calculation by which the rotation speed can be increased by manufacturing all the necessary components from carbon nanotubes, for example, components on which the structural strength, the strength of flywheels and ball bearings depend. And for this we make them from carbon nanotubes.

So, in the manufacture of the necessary elements from carbon nanotubes, the flywheels are able to withstand a centrifugal force of 78.7 times more than if they were made of steel.

Due to this, the specific energy content per unit of their weight can be made orders of magnitude greater than in flywheels made of steel.

раз по сравнению со скоростью истечения рабочего тела ракетного двигателя на химическом ракетном топливе.This will make it possible to further increase the specific energy content in the working fluid accelerated by the flywheels by at least another 78.7 times, in comparison with chemical rocket fuel. And it will further increase the flow rate of the working fluid back in

times compared with the rate of expiration of the working fluid of a rocket engine using chemical rocket fuel.

Accordingly, the velocity of the outflow from the flywheels of the working fluid using a system of ball bearings embedded in each other, increased in the range from 14.5258 to 31.6228 times, can be increased up to 10 times, and will be

245 km / s≤v≤473.55 km / s

This exceeds the maximum rate of expiration of chemical rocket fuel combustion products, which does not exceed 5.7 km / s [Space engines: state and prospects. Edited by Cavney L., Moscow, Mir, 1988, p. 415], in the range of times from 43.0 to 83.07 times.

Accordingly, the specific energy content per unit weight of the accelerated working fluid is proportional to the square of this value, which means that the specific energy content per unit weight of the accelerated working fluid will be greater in the range from 1849 to 6900 times.

Calculations for magnetic suspension

For magnetic suspension, everything is simpler.

For a steel flywheel with a radius of 0.8 cm, rotating at a speed of 211,000 rpm, the linear rotation speed is

Without the threat of destruction by centrifugal forces, the speed can increase in proportion to the square root of the radius. This means that with a radius of the steel flywheel 100 times greater than 0.8 m, the linear rotation speed and the velocity of the expiration of the working fluid can be increased 10 times. Namely, up to a speed of 16.88 km / s.

With an increase in the radius of the steel flywheel by a factor of 1000, namely, up to 8 m, the linear rotational speed and the velocity of the expiration of the working fluid can be increased by a factor of 1000, i.e., 31.622776 times. Namely, up to a speed of 53.38 km / s.

This exceeds the maximum rate of expiration of chemical rocket fuel combustion products, which does not exceed 5.7 km / s [Space engines: state and prospects. Edited by Cavney L., Moscow, Mir, 1988, p. 415], 9.37 times.

However, for a significant increase in the specific energy content in the flywheels, there are additional possibilities. For this, for example, new materials can be used to manufacture the flywheel: synthetic fibers and, primarily, carbon nanotubes. Kevlar and carbon fiber synthetic fibers can increase the strength of the flywheel up to 20 times per unit of its weight compared to steel, carbon nanofibers can increase this figure hundreds of times, since carbon nanofibres are 78.7 times stronger and much lighter than steel. Information on the manufacture of twisted ropes 10 km long has been published [K. Bogdanov, How can I calculate the strength of a carbon nanotube, March 20, 2009, http://www.nanometer.ru/2009/03/19/nanotubes_145296.html].

For example, Kevlar can increase the specific strength of a flywheel per unit of its weight by 20 times compared with steel, carbon fiber in the range from 10 to 20 times, and carbon nanotubes can increase its strength by 78.7 times [Bogdanov K.Yu. How can we calculate the strength of a carbon nanotube. March 20, 2009, http://www.nanometer.ru/2009/03/19/nanotubes_145296.html; http://tarefer.ru/; www.chemnet.ru/rus/jvho/2001-2/56.pdf; http://works.tarefer.ru/94/100071/index.html; http://e-science.ru/mdex/?id=4630].

Long nanotube manufacturing technologies developed at Cambridge University for the manufacture of a space elevator for NASA. To do this, you need a giant nanoconstruction with a length of 230 thousand kilometers. They developed a new material for the manufacture of nanotubes, and also found a way to combine them repeatedly to form long segments [Nanotubes for a space elevator, RBC daily, Monday January 26, 2009, No. 11 (574), p. 11].

In the following, we give a calculation by which the rotation speed can be increased by manufacturing all the necessary components from carbon nanotubes, for example, components on which the structural strength, the strength of flywheels and ball bearings depend. And for this we make them from carbon nanotubes.

So, in the manufacture of the necessary elements from carbon nanotubes, the flywheels are able to withstand a centrifugal force of 78.7 times more than if they were made of steel.

Due to this, the specific energy content per unit of their weight can be made orders of magnitude greater than in flywheels made of steel.

раз по сравнению со скоростью истечения рабочего тела ракетного двигателя на химическом ракетном топливе.This will make it possible to further increase the specific energy content in the working fluid accelerated by the flywheels by at least another 78.7 times, in comparison with chemical rocket fuel. And it will further increase the flow rate of the working fluid back in

times compared with the rate of expiration of the working fluid of a rocket engine using chemical rocket fuel.

Accordingly, the velocity of the outflow from the flywheels of the working fluid with the help of a magnetic suspension can be increased by another 8.871 times, and will be

This exceeds the maximum rate of expiration of the products of combustion of chemical rocket fuel, which does not exceed 5.7 km / s [Patent No. 2200875], by 83.07 times.

Accordingly, the specific energy content per unit weight of the accelerated working fluid is proportional to the square of this quantity, which means that the specific energy content per unit weight of the accelerated working fluid will be 6900.6 times greater.

Next option

In devices 2, 3, 4, 30 of driving the flywheel into rotation, electric generators generate electrical energy by rotating the rings or the flywheels. This electrical energy is used for various tasks of the engine and the entire aircraft, for example, for the operation of rotary devices, for moving rudders, for ensuring the operation of the charger, electrodes, power supply for the on-board computer and maintaining the conditions necessary for the crew’s vital functions.

In this embodiment, the engine may contain additional electric rocket engines, for example ionic, in which the highest efficiency of all electric rocket engines, for example, is greater than that of plasma.

In this case, the received electricity is used to power the power system of additional electric rocket engines, if the engine contains them.

Next option

In this embodiment, systems with a propulsion device of the second type are connected to the car and installed on or on the roof of it. The flows of the accelerated working fluid of some systems with a propulsion unit of the second type are directed by the rudders down from the car, creating a lifting jet thrust. To do this, you need four systems with a propeller of the second type and four steering wheels. Two systems with a propeller of the second type rotate the flywheels and the working fluid in the same direction. Two other systems with a propulsion device of the second type rotate the flywheels and the working fluid in the opposite direction.

Also, the flows of the accelerated working fluid of two more systems with a second type propulsion system are directed in the horizontal direction, creating a horizontal jet thrust. In this case, two systems with a propeller of the second type rotate the flywheels and the working fluid in opposite directions.

The operation of all elements is coordinated and controlled by a computer.

The car can be either hybrid, or the car can have an electric motor and be an electric car.

In this case, systems with a propulsion device of the second type may contain generators for generating electricity. Preliminarily, systems with a propulsion device of the second type are driven into rotation, using energy from an external source of electricity, for example, from a network. And then the generators can generate electrical energy from the stored mechanical energy of rotation and direct it to the operation of the electric motor of a car or electric vehicle.

Next option

At least two propulsion systems are implemented in a submarine or in a ship. In this case, they just work like water cannons. They throw away a rotational accelerated working fluid, for example water, fresh or marine, and thereby create a jet propulsion.

This can be done when swimming under water, and in water, and above water by creating an air cushion.

Next option

In the engine for creating horizontal thrust, the flywheels are made in volumes limited by turbines made in the form of spirals. The exits from the spirals are parallel.

Next option

Around the axis of the engine, the flywheel rotational drive device rotates the flywheel around a system of ball bearings embedded in one another. Moreover, in a pair of two adjacent ball bearings around the inner ball bearing rotate the outer ball bearing so that the balls or rollers of the outer ball bearing roll along the ring of the inner ball bearing, and such pairs are made as many as possible, for example, from 211 to 1000. In other words, each previous ball bearing is shaft for subsequent ball bearing.

This makes it possible to increase the speed of rotation of the outer pair of ball bearings in relation to the inner pair of ball bearings and in relation to the fixed shaft, around which they all rotate.

Since the cyclotron is capable of accelerating charged particles to relativistic speeds, the speeds to which the proposed flywheel rotation drive is able to accelerate the flywheel are limited from above only by the strength of the materials of the flywheel and elements of the system of ball bearings embedded in each other.

In the rings of the system of ball bearings embedded in each other and in the flywheels, remotely controlled systems with a battery are connected, connected to conductive plates. Batteries electrically charge conductive plates electrically isolated from each other by charges of opposite signs. Plates with different signs periodically alternate with each other.

For example, plates with different signs of electric charges are made on opposite sides of the rings and flywheels. In this case, plates with one sign of electric charge and plates with opposite sign of electric charge in the gap by an electric field are accelerated in opposite directions, increasing the torque of the ring or flywheel.

The conductive plates are made on the angular segments of the rings and flywheels with the same periods of alternation with each other, which are correlated with the frequency of the alternating voltage supplied to the electrodes. With increasing rotation of the rings and the flywheel, the frequency of the alternating voltage supplied to the electrodes increases simultaneously.

The plates are located in the accelerating gap, which serves an alternating electric field, which accelerates the plates together with the rings and flywheels and makes them rotate with acceleration. An alternating electric field is changed synchronously with a change in rotational speed. As soon as the frequency of rotation of the rollers or balls of the ball bearing relative to the selected ring, starting in order of priority from the shaft, reaches a dangerous 1000 revolutions per second, a signal is remotely applied to the system with the battery, causing them to discharge the plates of this ring so that the ring stops accelerating. Thus, the relative speed of the rings from the shaft is increased by 1000 revolutions per second for each ring and no more so that the rings do not break. This is repeated until the flywheel itself, the rotation speed of which becomes approximately equal to the number of rings of the system of ball bearings embedded in each other, multiplied by 1000 revolutions per second.

In the event that the rings begin to accelerate due to friction more than the specified critical relative angular velocity of rotation of about 1000 revolutions per second, braking combinations of signs of electric charges are applied to the conductive plates of the overly accelerated ring of the system with the battery.

Together with systems with a battery, systems with electric generators can be made that generate electrical energy when the rings or flywheels rotate.

The following options and additions

Instead of a system of ball bearings embedded in each other, a gearbox can be made to increase the speed of rotation.

Instead of the valve or together with the valve can use a nozzle. In this case, the nozzle is connected to the flywheel housing, made with the possibility of remote control and with the ability to control the exit of the working fluid from the flywheel. The nozzle releases the working fluid from the flywheel by orders of remote control, for example, radio control.

As elements of a magnetic suspension, superconducting magnets mounted on top of one another, powered by opposite currents, can be made, the upper superconducting magnet connected to the flywheel and made in a vacuum chamber, while a quadrupole focusing system is made around the magnet.

In this case, the flywheel rotates and hangs in vacuum together with the upper magnet above the lower magnet and does not experience friction.

This continues until the spacewalk, in which the accelerated working fluid begins to exit the flywheel and creates traction.

A cryostat is made at the bottom of the flywheel, while inside the cryostat there is a structure containing 50 layers separated by a dielectric, the structure being made under the flywheel in the form of a ring. The rotation of such a structure at startup reduces the weight of the flywheel.

Next option

Instead of dints, the flywheel rotational drive device contains an accelerating gap formed by slices of two pairs located above and below the flywheel and facing each other in the form of semicircles.

By analogy with the cyclotron, the flywheel rotational drive device periodically supplies a high-frequency alternating electric field with a high-frequency generator to the accelerating gap formed by slices of two pairs of electrodes in the form of semicircles located around the flywheel and facing each other. At the same time, it supplies an accelerating potential difference to the accelerating gap formed by sections of two pairs of electrodes in the form of semicircles located around the flywheel and facing each other.

Energy is supplied to a high-frequency generator either by a network or a nuclear reactor, for example, fast neutrons, or a thermonuclear reactor, such as a hybrid.

Next option

One or both of the turbines 16, 17 may be stationary. If the turbine is stationary, then it can also direct the working fluid moving along the tangent to it downward.

For example, the working fluid coming from the upper central device 3 for bringing the flywheel into rotation to the turbine 16 moves down in the gap between the turbine 17 and the engine body 18.

To explain how a stationary turbine can throw down the working fluid coming into it, we carry out the following reasoning. In the reference system of the central flywheel driving device 3, the turbine rotates, and therefore, in this reference system, the working fluid coming to the turbine 16 is thrown off by the turbine 16 as if it were rotating.

Next option

In the flywheel drive devices, the conductive plates 10, 11 can charge the high voltage generator with the aid of corona electrodes. Using a high-voltage generator, an electric discharge is applied to the corona electrodes, and electronic emission begins with them. A positive charge on the conductive plate is created if the corona electrodes are made on the conductive plate, and the voltage is applied so that electron emission is caused from the corona electrodes and the plate is charged with the same positive charge. A negative charge on the plate is created if the corona electrodes are made outside the conductive plate opposite it on the other side of the interelectrode gap. A potential difference is applied to the gap, electron emission is from the corona electrodes, electrons fly out from the corona electrodes and enter the conductive plate. And, thereby, they charge the plate with a negative charge.

A high-voltage generator can also supply high voltage to the electrodes 7, 8 of the flywheel driving device with a high frequency due to a modulator containing a rotatable disk with alternating conductive plates electrically isolated from each other, some of which have corona electrodes, but not others. In this case, the rotatable disk is rotated between two stationary disks also with conductive plates electrically isolated from each other, on some of which there are corona electrodes, and on the other there are not. High voltage is applied to the conductive plates of the fixed disks, electronic emission is caused, and electric charges are created on the plates of the rotatable disk, which are supplied from it to the conductive plates 10, 11 and with their help they rotate the ring 34 connected to the flywheel, as described above.

Next option

In the flywheel driving devices, the conductive plates 10, 11 can charge a high voltage generator inside the ring, for example a Wad der Graf generator. This generator rotates the tape between two conductive plates. Moreover, the tape removes a negative charge from one plate and creates an excess positive charge on it. On the other hand, the tape, on the contrary, applies a negative charge to and creates an excess negative charge on it.

The energy for moving the tape and for the operation of other elements of the high-voltage generator is provided either by a system with a battery, or a system with a generator that generates electricity when the flywheel or the ring is connected to the flywheel.

Next option

Graphite powder spraying systems spray graphite powder onto the inner working surfaces of the turbines 16, 17. The spraying of the graphite powder prevents the turbines from collapsing when they fall on them at a high speed of the working fluid. This fact was used in the development of the Orion Project to accelerate a steel plate with low-power nuclear explosions, carried out under the plate. As soon as the sprayed graphite powder protects the steel plate from the products of low-power nuclear explosions incident on it, it will certainly be able to protect the turbine from the working fluid incident on it.

Next option

The ring and pipe connected to the flywheel are made entirely of synthetic fibers or reinforced with synthetic fibers.

The ring and pipe connected to the flywheel are made entirely of carbon nanotubes or reinforced with carbon nanotubes.

This strengthens the elements of the engine.

The spiral and turbine are made entirely of synthetic fibers or reinforced with synthetic fibers.

The spiral and turbine are made entirely of carbon nanotubes or reinforced with carbon nanotubes.

This strengthens the elements of the engine.

Next option

The inertial engine of Bogdanov can be made in the form of a cylinder, along the lateral surface of which movers of the second type are made. Inside the cylinder, a hangar can be made for receiving and moving aircraft with the Bogdanov engine, made according to the first embodiment of the invention.

In this case, from the propulsors of the second type, made along the lateral surface of the cylinder, a working fluid accelerated during rotation in the flywheels is thrown out in a specific distinguished direction perpendicular to the axis of the cylinder and, thereby, reactive thrust is created perpendicular to the axis of the cylinder. To rotate an aircraft with such an inertial engine, Bogdanov’s working fluid can be thrown from different ends of the lateral surface of the cylinder in different directions, thereby creating a torque.

An aircraft with such an inertial engine of Bogdanov, made in the form of a large cylinder, can transfer other smaller aircraft, made in the form of aircraft with the Bogdanov engine according to the first embodiment of the invention, when flying to other celestial bodies in its hangar. Thus, an aircraft with a Bogdanov inertial engine in the form of a cylinder becomes a womb for smaller aircraft with a Bogdanov engine according to the first embodiment of the invention.

When the diameter of the inertial engine of Bogdanov, made in the form of a cylinder, increases, the amount of energy stored in it increases with the diameter of the flywheels of the second type propulsors, made along its side surface.

The Bogdanov inertial engine, made in the form of a large cylinder, can create the greatest thrust of all the options, since along the lateral surface of the cylinder you can place the largest number of propulsors of the second type per unit surface of the aircraft.

Thus, the inertial engine of Bogdanov, made in the form of a large cylinder, becomes an ideal version of the engine of the uterine ship, adapted for transferring smaller aircraft with the Bogdanov engine to other celestial bodies, made according to the first embodiment of the invention.

Next option

The inertial engine of Bogdanov can use their traction to turn the propulsors of the second type. In this case, the propeller of the second type ejects the rotating working fluid, creates a torque and rotates itself with the help of this torque relative to the rotary device, which then only fix it in the desired position.

Next option

Systems with propellers of the first and second type can be sealed. Systems with propulsors of the first and second type may contain vacuum chambers. In this case, a vacuum is created in them before starting. In this case, there may be several vacuum chambers. Vacuum in each of the systems with propellers of the first and second type is needed to reduce friction losses. Vacuum can break directly at the moment of creation of draft. In this case, the systems can turn on one after another.

Systems with propulsors of the first and second type may contain several propulsors, each made in its own separate vacuum chamber.

Following options

Inside the flywheel, a tape drive mechanism can be made comprising a tape, while cells with fuel are made inside the tape. Moreover, it is possible to separately burn individual cells with fuel at the moment the cell is in the desired position, in which the cell velocity vector approximately coincides with the direction of the selected thrust vector. For example, an inertial engine may comprise a synchronous heating system, for example, a synchronous laser ignition system.

At the right time, the synchronous laser ignition system delivers a short powerful laser beam, the cell with fuel burns up, combustion products burn up in a short time, fly out in the right direction, and the speed of rotation of the cell with fuel is added to the thermal speed of the burning fuel along with the flywheel. Due to this, traction is created in a short period of time in the right direction.

The tape drive mechanism moves a new cell with fuel to the right place, and at the right time, the synchronous laser ignition system with a fast powerful short pulse again sets fire to a new cell with fuel. And so on.

In the tape drive mechanism, the use of a stepper motor is possible.

Similarly, the tape drive mechanism can move the tape from refractory filaments, for example, from tungsten, between which a fusible substance, such as lead, in which refractory shots are made. The synchronous heating system at the right time synchronously with the movement of the tape heats the tape, the fusible substance in a small volume of heating quickly melts, releases the pellet, and the pellet with the melted substance at the right time due to rotation fly out, creating traction. All this can be done without pellets.

In another embodiment, a nozzle may be formed on the outside of the flywheel to which a fast synchronous fuel injection system inside the nozzle and a synchronous fuel ignition system inside the nozzle are connected, configured to simultaneously introduce fuel into the nozzle and simultaneously burn fuel inside the nozzle at a time when the speed fuel rotation approximately coincides with the direction of the selected thrust vector.

The synchronous quick fuel injection system inside the nozzle synchronously injects fuel into the nozzle and the synchronous ignition system synchronously ignites the fuel inside the nozzle at a time when the fuel rotation speed approximately coincides with the direction of the selected thrust vector.

For example, it is possible to quickly simultaneously inject fuel into the nozzle, for example, combustible fuel and a fuel oxidizer, and then synchronize with this at the right time by firing with a laser. Instead of a laser, an electron beam, a charged particle beam, or microwave radiation can be used.

This method of creation can be used in outer space, so that friction against atmospheric gas does not inhibit the flywheel. At the same time, the rotating flywheel can be delivered into space inside the vacuum chamber. Then, an exit window is opened in the wall of the vacuum chamber to create traction, and combustion products are thrown into space through the exit window.

It is advisable to use two flywheels rotating in opposite directions to extinguish the arising moment of rotation. You can use either one pair of flywheels or several pairs of flywheels.

Claims (25)

1. An inertia engine comprising a flywheel, characterized in that it comprises at least one system with a propulsion device, wherein the flywheel is made in the system, the flywheel comprising a working fluid, or a turbine is made around the flywheel, the flywheel being adapted to feed the working fluid on the inner working surface of the turbine, or the system contains a spiral or ring with a groove on the inner surface facing the axis of rotation of the flywheel, while the spiral or ring is made around the flywheel, and at the exit of the spiral and or a ring is made a hole with the possibility of exit from the hole of the accelerated working fluid. 2. The inertial engine according to claim 1, characterized in that the flywheel comprises a valve or nozzle, while in the housing of the flywheel a cavity is made and a working fluid is located in the cavity, the valve being made with remote control and with the ability to control the exit of the working fluid from the flywheel, and the nozzle is made with the possibility of remote control and with the ability to control the exit from the flywheel of the working fluid. 3. The inertial engine according to claim 1, characterized in that it is configured to connect to a thermal power plant, and it is possible to withdraw the working fluid from the flywheel so that the working fluid collides with the fuel of the thermal power plant and heats the fuel of the thermal power plant. 4. The inertial engine according to claim 1, characterized in that it comprises a flywheel rotation drive device, wherein the flywheel rotation drive device comprises a ring and a pipe connecting the flywheel and the ring, wherein an accelerating gap formed by slices of two located at the top and bottom of the ring around the ring and facing each other electrodes having the form of hollow half-cylinders, the electrodes being configured to be connected to a generator. 5. The inertial engine according to claim 1 or 4, characterized in that the ring is made remotely controlled system with a battery, electrically connected to at least two conductive plates electrically isolated from each other, while the battery of the system with the battery is configured to electrically charge at least two conductive plates with charges of opposite signs. 6. The inertial engine according to claim 1, characterized in that it comprises a system with a generator configured to generate electrical energy by rotating the flywheel or ring connected to the flywheel. 7. The inertial engine according to claim 1, characterized in that it contains a magnetic suspension configured to hold the flywheel in weight during rotation of the flywheel. 8. The inertial engine according to claim 1 or 7, characterized in that it contains a magnetic suspension configured to hold the flywheel in weight during rotation of the flywheel, while the magnetic suspension contains a superconducting magnet. 9. The inertial engine according to claim 1, characterized in that the turbine is connected to the flywheel, the flywheel being connected to the turbine cooling system and configured to feed the working fluid to the inner working surface of the turbine connected to it through the turbine cooling system. 10. The inertial engine according to claim 1, characterized in that a turbine is made around the flywheel, and the flywheel is configured to feed the working fluid to the inner working surface of the turbine, and the turbine is configured to direct the working fluid incident on the turbine with the ability to create reactive thrust. 11. The inertia engine according to claim 1, characterized in that it contains two flywheels, and rocket fuel is made in two flywheels as a working fluid, while in one flywheel combustible fuel is made as a working fluid, and in the other flywheel as a working fluid made oxidizer fuel. 12. The inertial engine according to claim 1 or 10, characterized in that it contains a spray system of graphite powder. 13. The inertial engine according to claim 1 or 10, characterized in that a cryostat is made below the flywheel, while inside the cryostat there is a structure containing at least two superconducting layers separated by a dielectric, the structure being made under the flywheel in the form of a ring. 14. The inertial engine according to claim 1, characterized in that a cryostat is made below the flywheel, while inside the cryostat there is a system of structures with superconducting layers separated by a dielectric containing at least two elements, the element containing a structure containing at least at least two layers of a superconductor separated by a dielectric, the system being connected to a system for changing the position of elements of a system of structures with superconducting layers separated by a dielectric and configured to remotely control However, the system of changing the position of elements of a system of structures with superconducting layers separated by a dielectric is configured to receive electric power either from a battery or from a generator configured to generate electricity when the flywheel rotates, while the system of changing the position of elements of a system of structures with superconducting layers separated by a dielectric, configured to arrange elements of a system of structures with superconducting layers separated by a dielectric trick so that the superconducting layers are connected in a ring disposed below the flywheel and is arranged to locate the elements such that the superconducting layers are connected in a ring. 15. The inertial engine according to claim 1, characterized in that the flywheel housing is made entirely of synthetic fibers or reinforced with synthetic fibers. 16. The inertial engine according to claim 1, characterized in that the flywheel housing is made entirely of carbon nanotubes or reinforced with carbon nanotubes. 17. The inertial engine according to claim 1, characterized in that the flywheel is connected to the turbine cooling system and is configured to feed its working fluid to the inner working surface of the turbine connected to it through the turbine cooling system, and the turbine cooling system is configured to create a protective film from the working fluid on the inner working surface of the turbine. 18. The inertial engine according to claim 1 or 17, characterized in that the system with the propulsion device is connected to a rotary device configured to deploy the system with the propulsion device to create the desired direction of the thrust vector. 19. The inertial engine according to claim 1 or 17, characterized in that a steering wheel is connected to the helix or ring in the region of the hole, which is designed to extend and install at an angle along the escape path from the hole of the accelerated departing working fluid. 20. The inertial engine according to claim 1 or 2, characterized in that a modulator is connected to the valve, configured to allow access of the working fluid to the valve at strictly calculated time intervals, while the modulator comprises a slotted disk connected to the disk rotation system. 21. The inertial engine according to claim 1, characterized in that the fluid or fraction is made as a working fluid. 22. The inertial motor according to claim 1, characterized in that it comprises a flywheel driving device comprising a system of ball bearings embedded in each other, made in such a way that, in a pair of two adjacent ball bearings, the inner ball bearing is embedded in the outer ball bearing so that the balls or the rollers of the outer ball bearing are configured to roll along the ring of the inner ball bearing, and at least two such pairs are made. 23. The inertial engine according to claim 1 or 17, characterized in that a charger is connected to the system with the propulsion device, configured to charge an accelerated working fluid with an electric charge of a certain sign at the exit of the flywheel, while a device for changing the direction of accelerated flow is connected to the charger a working fluid with an electrode system containing at least two electrodes. 24. The inertial engine according to claim 1 or 17, characterized in that a current source and a device for changing the direction of flow of the accelerated working fluid containing at least one magnetic coil are connected to the system with a propulsion device. 25. The inertial engine according to claim 1 or 17, characterized in that the propulsion system is connected to the car or is made in a submarine.

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