CZ2010330A3 - Apparatus for carrying out magnetic treatment of liquid and gaseous fuels and reduction of emissions - Google Patents

Abstract

The device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions is formed by a cylinder of the chamber (1) closed by a lid (2) with an axial hole for the inlet (10) of liquid or gaseous hydrocarbon fuels and a lid (3) with an axial opening for drain (11 ) of liquid or gaseous hydrocarbon fuels which, by joining together, form the body of the device chamber (1) in which neodymium axial permanent magnets in the form of cylinders (5) and neodymium axial permanent magnets in the shape of toroid (6). Said first three neodymium axial permanent magnets, in the form of a first cylinder (5 / I), a first toroid (6 / I) and a second cylinder (5 / II) are aligned with each other by identical magnetic poles on the cells of said magnets. From the third neodymium axial permanent magnet in the shape of the second cylinder (5 / II.), All other neodymium axial permanent magnets in the device body (1) are oriented towards each other by opposite magnetic poles on the magnets and are also coincident with the chamber axis. Axial bypass channels (8) are formed between the cylinder (5) and toroid (6) neodymium axial permanent magnet circuits and the chamber cylinder (1). Non-magnetic spacers (4) are located between the individual neodymium axial permanent magnets, which form radial bypass channels (9). For the functionality of the device, the flow direction (10) of liquid or gaseous hydrocarbon fuel is important.

Description

Equipment for magnetic treatment of liquid and gaseous fuels and emission reduction.

Field of technology

The invention relates to a device for performing magnetic treatment of liquid and gaseous fuels based on the principle of strong magnetic field. The passage of fuel through the device leads to its magnetic treatment, the result is a reduction in its consumption and, as a result, reduces emissions from internal combustion engines, turbines, gas burners, thereby reducing environmental air pollution and increasing environmental protection.

State of the art

Fuel saving and its better combustion is one of the current problems of internal combustion engines, both from an economic point of view, because incomplete fuel combustion increases both operating costs and from an environmental point of view, there is considerable air pollution. The better the combustion of the fuel in the engine, the more ecological air pollution is reduced by harmful exhaust gases.

Car manufacturers are trying to solve better combustion and fuel savings by gradually using more complex methods of equipment to reduce fuel consumption, which are in most cases costly and are designed only for a given type of internal combustion engine. Fuel manufacturers also solve the problem of reducing fuel consumption and try to refine the fuel with various additives so that it is used most efficiently and efficiently. In addition to reducing fuel consumption, it also tries to address the issue of environmental pollution by reducing the content of harmful substances in the fuel, such as sulfur, lead, etc.

Manufacturers of various chemical preparations, which produce other substances and additives that are added to the fuel and use these substances to adjust the chemical composition of fuels in order to improve certain properties of fuels, also try to save fuel and improve its combustion.

Given that the fuels supplied are already in a certain balance from the manufacturers, then the manufacturers of chemical preparations must take into account that their manufactured preparations improve certain properties of the fuel at the expense of the deterioration of other properties of the fuel. And by mitigating other deterioration, manufacturers are forced to produce higher quality additives that mitigate or eliminate deterioration, then such substances and additives are costly, making fuel more expensive than conventional higher quality fuels supplied by reputable fuel manufacturers and from an economic point of view does not bring the desired effect.

From the series of patents in class C 02 B of the International Patent Classification, a number of types of equipment used for the treatment of liquids, liquid and gaseous fuels using a magnetic field are known to date. Thus, another possible way of saving fuel and its better combustion using a strong magnetic field is known. Devices for the magnetic treatment of liquids and gases are known from the prior art, which are formed by a housing in which permanent magnets are arranged in pairs against each other, forming a casing surrounding the fuel supply line to the engine in which liquid and gaseous fuels are treated.

The Czech Author's Certificate No. 280 235 discloses a device for the magnetic treatment of liquids and gases, which consists of permanent magnets, the essence of which consists in the fact that two mutually perpendicular pairs of opposite permanent magnets, which are placed on the inner surface of the yoke, forming a sheath of polygonal cross-section, which is provided at both ends with handles for securing the position of the pipe of the medium to be treated in the longitudinal axis of the yoke. Adjacent permanent magnets have opposite magnetic polarity, or adjacent permanent magnets have the same and opposite magnets have opposite magnetic polarity. In the direction of the longitudinal axis of the yoke, protrusions are formed on its inner surface, along the individual permanent magnets. The yoke has a square or octagonal cross section. The yoke is divided into two parts. When applying this device to the car's fuel system, lower consumption can be found with a reduced content of harmful substances in the exhaust gases.

The disadvantage of the described device is the air gaps between the fuel pipe and the permanent magnets, as well as between the planar shapes of the permanent magnets with respect to the circular cross-section of the fuel system pipe, which in both cases reduces the intensity of the magnetic field in the working space and its resulting effect. Other significant disadvantages of this device are the fact that the fuel passing through the fuel line flows only laminarly, so that it does not mix and the magnetic field does not act so intensively on all the passing fuel and the device does not achieve the required efficiency. In addition, each time the engine speed is increased, the fuel passes through the fuel line faster and the magnetic efficiency of the device decreases again because it does not allow the magnetic field to work optimally on all flowing fuel, further reducing the resulting effect of the device.

Other technical solutions and devices for fuel treatment are also known, such as CZ / EP 1 546 541, which discloses an electronic fuel treatment device for improving combustion efficiency and for reducing emissions from an internal combustion engine, such as an internal combustion engine for motor vehicles. , or for heating systems.

The disadvantage of this electronic device is, in addition to the high technical complexity of the individual electrical circuits of the device, the increased possibility of higher failure rates, but mainly its dependence on the power supply, because without input DC voltage the device is inoperative.

Czech author's certificate No. 298 708 describes devices for saving fuel and reducing emissions. The fuel saving device consists of a solid non-magnetic support body provided with an opening which delimits a flow channel for the air / fuel mixture and at least three magnets. Each of the magnets has a polar axis oriented substantially parallel to the flow path for the air / fuel mixture and creates a continuous magnetic field through the flow channel in the support body. The at least two magnets being substantially opposite and having a polar axis oriented north-south, the axis of the at least third magnet being oriented south-north. The fuel saving device comprises several embodiments of a support body on which several magnets of opposite polarities are mounted and can be placed in the fuel system of internal combustion engines, thus saving fuel and reducing emissions.

The disadvantage of the described equipment is the high financial demands and labor in its production.

-3 Summary of the Invention

The above-mentioned disadvantages and shortcomings are largely eliminated by the device for performing magnetic treatment of liquid and gaseous fuels. The essence of the invention lies in the construction of the optimal chamber shape of the magnetic treatment device and the suitable internal arrangement of the neodymium axial permanent magnets, which generates a strong magnetic field. In liquid and gaseous fuels flowing through a magnetic chamber, between neodymium axial permanent magnets, turbolent flow and more efficient action of the device on flowing liquid and gaseous hydrocarbon fuels, which change their physical properties, repeatedly occur in the device chamber throughout the fuel treatment in a strong magnetic field. The device is located in the fuel system, in front of the internal combustion engine.

The proposed device according to the invention works on the principle of influencing liquids by a magnetic field. Liquid and gaseous hydrocarbon fuels for internal combustion engines are composed of molecules of carbon and hydrogen compounds, as well as various admixtures and subsequently added air. The fuel molecules try to clump together and act on each other with Laplasian, very weak forces. The fuel molecules may carry an electric charge or have certain magnetic properties. Due to these stated properties of liquid and gaseous hydrocarbon fuels, the magnetic field can act on its treatment. In the equipment chamber, the fuel flows slowly in a turbulent manner. Many admixtures and some hydrocarbon compounds, which are based on a carbon atomic skeleton and various spatially bound hydrogen, form magnetic dipoles, the orientation of which is given by random relationships and intermolecular bonds. If the fuel passes through a strong magnetic field, then the magnetic field with its energy affects the intermolecular bonds and clusters of fuel molecules, which separate from each other. If the magnetic field is strongly inhomogeneous, then the flow of fuel through this magnetic field, its energy, affects the intermolecular bonds and clusters of fuel molecules, which separate from each other and the energy of the magnetic field curves their paths and can rotate with them. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. By arranging the magnets in the device, the flow of fuel in a homogeneous magnetic field results in repeated turbulent flow. This results in better mixing of the fuel at the molecular level and its homogenization. The fuel leaving the plant chamber is thus homogenized and, as a result, more atmospheric oxygen can be added to the mixture during gasification. More oxygen bound in the fuel contributes to a better breakdown of the mixture in the cylinder heads of the internal combustion engine. The result is a reduction in fuel consumption and, as a result, a reduction in internal combustion engine emissions.

The described device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions consists of a chamber cylinder in which neodymium axial permanent magnets are housed. The non-magnetic cylinder of the internally threaded chamber is closed by two non-magnetic externally threaded lids with an axial opening for the inflow and with an axial opening for the outflow of magnetically treated liquid or gaseous fuel. A non-magnetic cylinder with non-magnetic lids forms a chamber body in which, for example, a neodymium axial permanent magnet in the form of a cylinder or a prism, which is separated by non-magnetic spacers from a neodymium axial permanent magnet in

-4shaped toroid shape also aligned with the axis of the chamber. The arrangement of the neodymium axial permanent magnets described in this way in the magnetic chamber of the device is alternating and can be repeated several times. Three, four, five or more neodymium axial permanent magnets in the shape of a cylinder or a prism may be arranged in the non-magnetic cylinder of the device chamber, alternating with two, three, four or more neodymium axial permanent magnets in the shape of a toroid.

It should be emphasized that the following arrangement of magnets must be observed in the chamber of equipment for performing magnetic treatment of liquid and gaseous fuels and reducing emissions:

The first three neodymium axial permanent magnets, for example in the order cylinder, or prism, toroid, cylinder, or prism, are placed in the body of the device chamber with identically oriented poles on the magnet faces to create a highly inhomogeneous field so that the field force pushes molecules from different sides according to their position and, in addition, to rotate the molecules exhibiting magnetic properties. When the fuel flows through a strongly inhomogeneous field, the process of molecular clusters breaks down, separates them, separates the molecules from each other and, thanks to the rotation of the polar molecules, mixes the fuel at the molecular level.

Additional neodymium axial permanent magnets are then placed in the body of the device chamber, for example in the order cylinder, or prism, toroid, cylinder, or prism, toroid, cylinder, or prism, placed with oppositely oriented poles on the magnet faces to create a strong homogeneous field. In a strong homogeneous field, the passing fuel flows due to the arrangement of magnets to repeated turbulent flow, which leads to better mixing at the molecular level. When the above-described neodymium axial permanent magnets are placed in the chamber body, with the opposite poles facing the magnet faces, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field and the fuel is homogenized. The fuel leaving the plant chamber is thus homogenized and, as a result, more atmospheric oxygen can be added to the mixture during gasification. The higher atmospheric oxygen content contributes to a better combustion of the mixture in the cylinder heads of the internal combustion engine, to an increase in engine power and a consequent reduction in fuel consumption and emissions.

Another advantage of the present device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions is the storage of neodymium axial permanent magnets in a chamber, which ensures the formation of turbulent flow in the device. By the described arrangement between the neodymium axial magnets, radial channels are formed in the device chamber by non-magnetic spacers, and axial bypass channels are formed between the circuits of the neodymium toroidal permanent magnets housed in the device and the chamber shell surface. These radial and axial channels cause the chamber to decelerate and accelerate the flow rate of liquid and gaseous hydrocarbon fuels, which is guided through the chamber axially and radially and between the individual neodymium axial permanent magnets in the chamber, acts very strong magnetic field, which has a positive effect on physical properties of liquid and gaseous hydrocarbon fuels, throughout the flow of fuel through the submitted equipment.

Due to the formed radial and axial bypass channels, which cause the flow rate of liquid and gaseous fuels to decelerate and accelerate in the chamber, the magnetic treatment device does not consist of any moving parts. For this reason, equipment for performing magnetic treatment of liquid and gaseous fuels and reducing emissions

-5requires no maintenance or power supply and requires no maintenance. The proposed device works in any working position, while still being just as powerful and functional. When installing the device in the fuel system, make sure that the device is mounted in the correct direction and that the drain channel points in the direction of the internal combustion engine.

The present device for performing magnetic treatment of liquids and gases and reducing emissions is designed for four neodymium axial permanent magnets, in the shape of a cylinder, which are placed in the chamber of the device alternately with three neodymium axial permanent magnets, in the shape of a toroid. The device is shown in the attached drawing.

The device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions consists of four neodymium axial permanent magnets, in the shape of a cylinder, alternating with three neodymium axial permanent magnets, in the shape of a toroid. It should be emphasized that the subsequent arrangement and orientation of the neodymium axial permanent magnets with magnetic poles on the faces of said magnets must be observed in the chamber of the device for performing magnetic fuel treatment. Said neodymium axial permanent magnets are housed in a non-magnetic cylinder of an internally threaded chamber. The chamber cylinder is closed by two non-magnetic lids with an external thread with an axial hole for inflow and with an axial hole for outflow of magnetically treated liquid or gaseous fuel. The non-magnetic cylinder with non-magnetic lids forms the chamber body, in which the first neodymium axial permanent magnet in the form of a cylinder is placed in line with the axis of the chamber, which is separated by non-magnetic spacers from the first neodymium axial permanent magnet in the form of said magnets and is mounted coincident with the axis of the chamber. The first neodymium axial permanent toroid is separated by non-magnetic spacers from the second neodymium axial cylindrical permanent magnet. They are oriented towards each other by corresponding magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. The above orientation of the first three neodymium axial permanent magnets creates a strong magnetic field in the resulting radial channels between the neodymium axial permanent magnets, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. The second neodymium axial permanent magnet in the shape of a cylinder is separated in the cylindrical chamber by non-magnetic spacers from the second neodymium axial permanent magnet in the shape of a toroid. Said magnets are oriented to each other by opposite magnetic poles on the faces of said magnets and are also mounted coincident with the axis of the chamber. The second neodymium toroidal axial permanent magnet is separated in the cylindrical chamber by non-magnetic spacers from the third neodymium cylindrical axial permanent magnet. Said neodymium axial permanent magnets are oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. The third neodymium axial permanent magnet in the shape of a cylinder is separated in the cylindrical chamber by spacers from the third neodymium axial permanent magnet in the shape of a

-6toroids oriented by opposite magnetic poles on the faces of said magnets and are mounted identically to the axis of the chamber. The fourth neodymium axial permanent magnet in the shape of a cylinder is separated in the cylindrical chamber from the third neodymium axial permanent magnet in the shape of a toroid, the permanent magnets being oriented towards each other by opposite magnetic poles on the faces of said magnets. Alternatively, the next neodymium axial permanent magnets in the shape of a cylinder or prism are separated from the next neodymium axial permanent magnets in the shape of toroids and all magnets are oriented towards each other by opposite magnetic poles on the faces of said magnets and are also aligned with the axis. chambers. Said orientation of the neodymium axial permanent magnets, which are oriented to each other by opposite magnetic poles on the faces of said magnets, creates a strong homogeneous magnetic field in the resulting radial channels between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level and its homogenization.

Overview of figures in the drawings

The invention will be described and elucidated in more detail with the aid of the drawings, in which Figs. 1-6 show in longitudinal section the technical solution of the internal arrangement of the device for performing magnetic treatment of liquid and gaseous hydrocarbon fuels and reducing emissions.

Giant. 1 Shows the proposed device in which neodymium axial permanent magnets are arranged as follows:

A) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Cylinder - toroid cylinder toroid cylinder toroid cylinder)

B) Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - prismatic neodymium axial permanent magnet.

(Prism - toroid prism toroid - prism toroid - prism)

Fig.2 Has the following arrangement of neodymium axial permanent magnets:

C) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid

-Ίcylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism.

(Cylinder - toroid - cylinder - toroid - cylinder - toroid - prism)

D) Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Prism - toroid - prism - toroid - prism toroid cylinder)

Fig.3 Has neodymium axial permanent magnets arranged as follows:

E) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - prismatic neodymium axial permanent magnet.

(Cylinder - toroid - cylinder - toroid - prism - toroid - prism)

F) Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Prism - toroid - prism - toroid - cylinder toroid - cylinder)

Fig.4 Neodymium axial permanent magnets are arranged as follows:

G) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism, (Cylinder toroid - prism toroid - prism - toroid - prism)

H) Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Prism - toroid - cylinder - toroid - cylinder - toroid - cylinder)

-8Fig.5 Has neodymium axial permanent magnets arranged as follows:

I) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - prismatic neodymium axial permanent magnet.

(Cylinder - toroid - prism - toroid - cylinder - toroid - prism)

J) Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Prism - toroid - cylinder - toroid prism toroid - cylinder)

Fig.6 shows the following arrangement of neodymium axial permanent magnets:

K) Neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder.

(Cylinder - toroid - prism - toroid - prism - toroid - cylinder)

Neodymium axial permanent magnet in the shape of a prism - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a cylinder - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial permanent magnet in the shape of a toroid - neodymium axial prism-shaped permanent magnet.

(Prism - toroid - cylinder - toroid - cylinder - toroid - prism)

Examples of embodiments of the invention

The device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions is shown in longitudinal section according to Figs. for the outflow 11 of liquid or gaseous hydrocarbon fuels 3, which form a chamber body by joining with an internal or external thread or by gluing. The device is further formed by non-magnetic spacers 4, neodymium axial permanent magnets 5, 6, 7, according to the proposed arrangement of individual device types, bypass axial channels 8 bypass radial channels 9 and the direction of medium 10 inflow into the device and liquid outflow or gaseous hydrocarbon fuels 11. The body of the device chamber can be made of non-magnetic metal or plastic. In addition to non-magnetic spacers, metal parts of the device, including magnets, can be surface-treated.

In the designed body of the non-magnetic chamber of the device, neodymium axial permanent magnets are placed according to individual pictures in the following composition:

-9Picture No. 1

A) Cylinder 5/1. - toroid 6/1. - cylinder 5/11. - toroid 6 / Π. - cylinder 5 / ΙΠ. - toroid 6 / III. - cylinder 5 / IV.

B) Prism 7/1, - toroid 6 / 1.- prism 7 / II. toroid 6 / 11- prism 7/111, - toroid 6 / IIL- prism 7 / IV.

Figure 2

C) Cylinder 5/1. - toroid 6/1. - cylinder 5/11, toroid 6 / IL - cylinder 5 / III. - toroid 6 / IIL - prism 7/1.

D) Prism 7/1. - toroid 6/1. - prism 7 / II. toroid 6/11. prism 7/111. toroid 6/111, - cylinder 5 / L

Figure 3

E) Cylinder 5 / L - toroid 6/1, - cylinder 5 / IL - toroid 6 / IL - prism 7/1, - toroid 6 / III. - prism 7 / II.

F) Prism 7/1, - toroid 6/1, - prism 7 / II. - toroid 6/11. - cylinder 5 / 1.- toroid 6 / 1II. cylinder 5 / II.

Figure 4

G) Cylinder 5/1. - toroid 6/1. - prism 7/1, - toroid 6 / IL - prism 7 / II. - toroid 6 / 1II. - prism 7 / ΙΠ.

H) Prism 7/1. toroid 6/1. cylinder 5/1. - toroid 6 / IL - cylinder 5 / II. - toroid 6 / IIL - cylinder 5 / ΙΠ.

Figure 5

I) Cylinder 5/1. - toroid 6/1. - prism 7 / L - toroid 6 / IL - cylinder 5 / Π. - toroid 6 / IIL - prism 7 / II.

J) Prism 7 / L - toroid 6/1. - cylinder 5 / L - toroid 6 / IL - prism 7/11. - toroid 6/111. - cylinder 5/11.

Figure 6

K) Cylinder 5 / L - toroid 6/1. - prism 7/1. - toroid 6 / IL - prism 7 / II. - toroid 6 / 1II. - cylinder 5/11.

L) Prism 7/1. - toroid 6/1. - cylinder 5/1. - toroid 6 / IL - cylinder 5 / IL - toroid 6 / IIL - prism 7/11.

The above-mentioned neodymium axial permanent magnets 5, 6, 7 with magnetic poles on the faces of the magnets 5, 6, 7 are placed together by means of non-magnetic spacers 4. The first three neodymium axial permanent magnets (in the direction of fuel flow into the device) are always oriented on on the faces of the magnets 5, 6, 7 with corresponding magnetic poles. Additional neodymium axial permanent magnets 5, 6, 7 are then placed in the body of the device chamber, placed with oppositely oriented poles on the faces of the magnets 5, 6, 7.

In FIG. 1, the placement of the neodymium axial permanent magnets of the shapes shown is alternating and can be repeated several times in succession.

In Figs. 2 to 6, the placement of the neodymium axial permanent magnets of the shapes shown is fixed.

The treated fuel is fed to the device 10 for performing magnetic treatment of liquid and gaseous fuels and reducing emissions through an axial opening in the lid of the chamber body 2 and according to:

In Figure 1, the arrangement of magnets according to A) flows around the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first cylinder 5/1. and further flows through the slit forming the axial bypass channel 8 between the circumference of the first cylinder 5 / L and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. Turbolent flow occurs behind the first 5 / L cylinder as the fuel flows. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the first toroid 6/1. and chamber cylinder 1. Thus

-10 occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 to the second cylinder 5 / II. and further flows through a slit forming an axial bypass channel 8 between the circumference of the second cylinder 5 / Π. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 5 / L, 6/1. and 5/11. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 5 / L, 6/1. and 5 / Π. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5 / L, 6/1. and 5Π. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second cylinder 5 / II. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6 / H. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / Π. and the cylinder of chamber 1. This occurs behind the second toroid 6 / II. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the third cylinder 5 / III through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the third cylinder 5 / III. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third cylinder 5 / ΙΠ. a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the third cylinder 5 / III and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. After the third cylinder 5 / III. turbulent flow occurs again with the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / ΠΙ. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / IIL and the cylinder of the chamber 1. This leads behind the third toroid 6 / ΙΠ. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the fourth cylinder 5 / IV through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the fourth cylinder 5 / IV. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a cylinder 5 / II. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to B) flows around the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder of the chamber 1, whereby

-11decreasing the flow rate of the fuel being treated. Behind the first prism 7/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second prism 7 / IL and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / IL and the cylinder chamber 1, reducing the flow rate of the treated fuel. Said first three neodymium axial permanent magnets 7 / L. 6/1. and 7 / IL are oriented towards each other by corresponding magnetic poles on the faces of said magnets 7 / L, 6/1. and 7/11. Said orientation with the corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / L. 6/1. and 711. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second prism 7 / IL, turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / IL and the cylinder chamber 1, reducing the flow rate of the treated fuel. The treated fuel in the radial bypass channels 9 passes further through the center of the next second toroid 6 / II. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / II. and chamber cylinder L This occurs behind the second toroid 6 / Π. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the third prism 7 / III through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the third prism 7 / III. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third prism 7 / III. a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the third prism 7 / III. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third prism 7 / IIL, the flowing fuel again has a turbolent flow. The treated fuel in the radial bypass channels 9 passes through the center of the next third toroid 6 / IIL and at the same time bypasses it from the sides by an axial channel 8 formed by the circumference of the third toroid 6 / IIL and the cylinder 1. This turbolent flow occurs to increase the flow rate of the treated fuel. The fuel flows through the radial 9 and axial bypass channel 8 a fourth prism 7 / IV. and further flows through the slit forming the axial bypass channel 8 between the circumference of the fourth prism 7 / IV. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7 / IL, all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also arranged in line with the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbulent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of fuel at the molecular level in the plant and its

-12homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

In Figure 2, the arrangement of magnets according to C) flows around the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first cylinder 5/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first cylinder 5/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of the chamber 1. This results in a turbolent flow behind the first toroid 6/1, an increase in the flow rate of the fuel to be treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second cylinder 5/11, and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11 and the cylinder chamber 1, thereby reducing the flow rate of the treated fuel. Said first three neodymium axial permanent magnets 5 / L, 6/1. and 5 / 1L are oriented towards each other by corresponding magnetic poles on the faces of said magnets 5 / L, 6/1. and 5 / II. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5 / L, 6/1. and 5II. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second cylinder 5 / Π. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 passes further through the center of the next second toroid 6 / Π. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / II. and the cylinder of chamber 1. This occurs behind the second toroid 6 / II. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the third cylinder 5/111 through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the third cylinder 5 / III, and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third cylinder 5 / IIL, the flowing fuel undergoes turbolent flow and further flows through the slit forming the axial bypass channel 8 between the circumference of the third cylinder 5 / IIL and the cylinder chamber 1, thereby reducing the flow rate of the treated fuel. Behind the third cylinder 5 / IIL, the flowing fuel again has a turbolent flow. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / ΙΠ. and at the same time it flows around it from the sides through an axial channel 8, formed by the circumference of the third toroid 6 / III and the cylinder of the chamber 1. This occurs behind the third toroid 6 / III. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 through the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a cylinder 5/11. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates repeated ones in the resulting radial channels 9

-13turbolent flow and strong homogeneous magnetic field between neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is reduced again, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to D) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the second prism 7 / álními through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 7 / L. 6/1. and 7 / IL are oriented towards each other by corresponding magnetic poles on the faces of said magnets 7 / L, 6/1. and 7 / II. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / L, 6/1. and 71, it creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second prism 7/11. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / Π. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 passes further through the center of the next second toroid 6 / II. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / II. and chamber cylinder 1. This results in a turbolent flow behind the second toroid 6 / Π, and an increase in the flow rate of the fuel to be treated. The fuel flows around the third prism 7 / álními through the radial 9 and axial bypass channel 8. and further flows through the slit forming the axial bypass channel 8 between the circumference of the third prism 7 / III. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third prism 7 / IIL, the flowing fuel undergoes turbolent flow and further flows through a slit forming an axial bypass channel 8 between the circumference of the third prism 7 / L, and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the third prism 7 / III. turbulent flow occurs again with the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the following third toroid 6 / ΠΤ and at the same time flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6/111. and chamber cylinder L This occurs behind the third toroid 6/111. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first cylinder 5/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, whereby the reduction occurs

-14 flow rates of treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7 / II. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. In the interior of neodymium axial permanent magnets in the shape of toroids, it creates a strong scattering magnetic field. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

In Figure 3, the arrangement of magnets according to E) flows around the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first cylinder 5/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Turbolent flow occurs behind the first 5 / L cylinder as the fuel flows. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 to the second cylinder 5 / II. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11, and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 5 / L, 6/1. and 5/11, are mutually oriented by the corresponding magnetic poles on the faces of said magnets 5 / L. 6/1. and 5 / II. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5 / L, 6/1. and 5II. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second cylinder 5 / II. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the axial channel 8 formed by the circumference of the second toroid 6/11. and the chamber chamber 1. This results in a turbolent flow behind the second toroid 6/11, and an increase in the flow rate of the fuel to be treated. The fuel flows through the radial 9 and axial bypass channel 8 of the first prism 7/1, and further flows through the slit forming the axial bypass channel 8 between the circumference of the first prism 7 / L and the cylinder chamber 1, thereby reducing the flow rate of the treated fuel. Behind the first prism 7 / L, the flowing fuel undergoes turbolent flow and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7 / L and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. turbulent flow occurs again with the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / II1. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / III. and the cylinder of chamber 1. This occurs behind the third toroid 6 / ΙΠ. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and the axial bypass channel 8 through the second prism 7 / Π. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a cylinder 5 / II. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to F) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and the axial bypass channel 8 through the second prism 7/11. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / IL and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 7 / L, 6/1. and 7/11. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 7 / L. 6/1. and 7 / IL Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / L. 6/1. and 711. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the second prism 7 / IL, the flowing fuel is re-turbolent and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / IL and the cylinder chamber 1, reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / Π. and the cylinder chamber L This occurs behind the second toroid 6 / II. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first cylinder 5/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first cylinder 5/1. occurs with flowing fuel

to the turbolent flow and further flows through the slit forming the axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first cylinder 5/1. turbulent flow occurs again with the flowing fuel. The treated fuel in the radial bypass channels 9 passes through the center of the next third toroid 6 / III. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / III. and the cylinder of chamber 1. This occurs behind the third toroid 6 / TII. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 of the second cylinder 5/11 · and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5 / II. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7 / II. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

Figure 4 shows the arrangement of magnets according to G) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first cylinder 5/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and a cylinder X, thereby reducing the flow rate of the fuel being treated. Behind the first cylinder 5/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1 and at the same time flows around it through the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first prism 7/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and a cylinder X, thereby reducing the flow rate of the fuel being treated. Said first three neodymium axial permanent magnets 5/1, 6/1. and 7/1. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 5/1., 6/1. and 7/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5/1., 6/1. and 7/1. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first prism 7/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the first prism 7/1. and a cylinder X, thereby reducing the flow rate of the fuel being treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / II. and chamber X chamber

-17, after the second toroid 6/11, there is again a turbolent flow and an increase in the flow rate of the treated fuel. The fuel flows around the radial 9 and the axial bypass channel 8 through the second prism 7 / II. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7/11. a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7 / II. turbolent flow occurs again with the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / ΙΠ. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / III. and the cylinder of chamber 1. This occurs behind the third toroid 6 / III. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and the axial bypass channel 8 through the third prism 7 / III. and further flows through the slit forming the axial bypass channel 8 between the circumference of the third prism 7 / ΙΠ. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7/1. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to H) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first cylinder 5/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 7 / L, 6/1. and 5/1. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 7 / L. 6/1. and 5/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / L, 6 / L and 5/1. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first cylinder 5/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between

-18 circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The fuel to be treated in the radial bypass channels 9 then passes through the center of the next second toroid 6 / IL and at the same time flows around it through an axial channel 8 formed by the circumference of the second toroid 6 / IL and the cylinder chamber 1. This follows the second toroid 6/11. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second cylinder 5 / IL and further flows through the gap forming the axial bypass channel 8 between the circumference of the second cylinder 5 / IL and the cylinder chamber 1, reducing the flow rate of the treated fuel. Behind the second cylinder 5 / IL, a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second 5 / IL cylinder, turbolent flow recurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / IIL and at the same time flows around it through an axial channel 8 formed by the circumference of the third toroid 6 / IIL and the cylinder chamber 1. This occurs behind the third toroid 6/111. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the third cylinder 5 / IIL and further flows through the slit forming the axial bypass channel 8 between the circumference of the third cylinder 5 / L. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 5/1. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

Figure 5 shows the arrangement of magnets according to I) bypassing the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first cylinder 5/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first cylinder 5/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first prism 7/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 5 / L, 6/1. and 7/1. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 5 / L. 6/1. and 7/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5 / L, 6/1. and 7/1. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high gradient

-19 magnetic field, which increases the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first prism 7/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11, and at the same time it flows around it through the axial channel 8 formed by the circumference of the second toroid 6/11. and the chamber chamber 1. This occurs behind the second toroid 6/11. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second cylinder 5/11, and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5/11. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second cylinder 5/11. at the flowing fuel for turbolent flow and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second 5 / IL cylinder, turbolent flow recurs in the flowing fuel. The treated fuel in the radial bypass channels 9 passes through the center of the next third toroid 6 / III. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / 1II. and the chamber cylinder This occurs behind the third toroid 6 / ΙΠ. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 through the second prism 7/11, and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7/1. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to J) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first cylinder 5/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 7 / L, 6/1. and 5/1. they are mutually agreed

-20magnetic poles on the faces of said magnets 7 / L. 6/1. and 5/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / L, 6/1. and 5/1. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first cylinder 5/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the first cylinder 5/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the axial channel 8 formed by the circumference of the second toroid 6/11. and the chamber chamber 1. This occurs behind the second toroid 6/11. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 through the second prism 7 / IL and further flows through the slot forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7 / IL, the flowing fuel undergoes turbolent flow and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / IL and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7 / IL, the flowing fuel again has a turbolent flow. The treated fuel in the radial bypass channels 9 passes through the center of the next third toroid 6 / 1II. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / ΙΠ. and the cylinder of chamber 1. This occurs behind the third toroid 6 / III. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 to the second cylinder 5 / II. and further flows through a slit forming an axial bypass channel 8 between the circumference of the second cylinder 5 / Π. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a 5 / L prism, all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

Figure 6 shows the arrangement of magnets according to K.), the treated liquid or gaseous hydrocarbon fuel flows through the radial bypass channels 9, the first cylinder 5 / L and further flows through the slit forming the axial bypass channel 8 between the circumference of the first cylinder 5 / L and the cylinder 1 chamber. to reduce the flow rate of the fuel being treated. Behind the first cylinder 5/1. turbolent flow occurs in the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the first toroid 6/1. and the cylinder of chamber 1. This occurs behind the first toroid 6/1. to turbolent flow and to increase

-21 flow rate of the treated fuel. The fuel flows around the first prism 7/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Said first three neodymium axial permanent magnets 5 / L, 6/1. and 7/1. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 5 / L. 6/1. and 7/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 5 / L, 6/1. and 7 / L creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of flowing fuel molecules are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first prism 7/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the first prism 7/1. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the second toroid 6 / II. and the chamber chamber 1. This occurs behind the second toroid 6/11. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and the axial bypass channel 8 through the second prism 7/11. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7 / II. a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7 / II. and the cylinder chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the second prism 7 / II. turbulent flow occurs again with the flowing fuel. The fuel to be treated in the radial bypass channels 9 passes through the center of the next third toroid 6 / I1I. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / III. and the cylinder of chamber 1. This occurs behind the third toroid 6 / 1II. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows through the radial 9 and axial bypass channel 8 through the second cylinder 5 / II. and further flows through a slit forming an axial bypass channel 8 between the circumference of the second cylinder 5 / Π. and the cylinder chamber 1, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 7 / L, all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate in the opposite direction to the homogeneous magnetic field. This results in better mixing of the fuel at the molecular level in the device and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

the bearing of the magnets according to L) bypasses the treated liquid or gaseous hydrocarbon fuel through radial bypass channels 9, the first prism 7/1. and further flows through the slit forming the axial bypass channel 8 between the circumference of the first prism 7 / L and the cylinder of the chamber 1, thereby reducing the flow rate of the fuel to be treated. Behind the first prism 7/1. occurs at

-22 flowing fuel for turbolent flow. The fuel to be treated in the radial bypass channels 9 passes through the center of the next first toroid 6/1. and at the same time it flows around it from the axial channel 8 formed by the circumference of the first toroid 6/1. and the chamber chamber 1- This occurs behind the first toroid 6/1. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the first cylinder 5/1 through the radial 9 and axial bypass channel 8. and further flows through a slit forming an axial bypass channel 8 between the circumference of the first cylinder 5/1. and a cylinder X, thereby reducing the flow rate of the fuel being treated. Said first three neodymium axial permanent magnets 7 / L, 6/1. and 5/1. they are oriented towards each other by corresponding magnetic poles on the faces of said magnets 7 / L, 6/1. and 5/1. Said orientation with corresponding magnetic poles on the faces of said neodymium axial permanent magnets 7 / χ., 6/1. and 5/1. creates a strong magnetic field between the magnets in the resulting radial channels 9, which is inhomogeneous with a high magnetic field gradient, thus increasing the efficiency of the described device. In this part of the device, intermolecular bonds and clusters of molecules of flowing fuel are affected, which separate from each other and the energy of the magnetic field curves the paths of their movements and can even rotate with them. Behind the first cylinder 5/1. turbolent flow occurs again in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the first cylinder 5/1. and a cylinder X, thereby reducing the flow rate of the fuel being treated. The treated fuel in the radial bypass channels 9 further passes through the center of the next second toroid 6/11. and at the same time it flows around it from the axial channel 8 formed by the circumference of the second toroid 6/11. and the cylinder of chamber X. This occurs behind the second toroid 6/11. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second cylinder 5/11. and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5 / 1L and the cylinder of the chamber X, thereby reducing the flow rate of the fuel to be treated. Behind the second cylinder 5 / II. a turbolent flow occurs in the flowing fuel and further flows through the slit forming the axial bypass channel 8 between the circumference of the second cylinder 5 / Π. and a cylinder X, thereby reducing the flow rate of the fuel being treated. Behind the second cylinder 5 / II. turbulent flow occurs again with the flowing fuel. The treated fuel in the radial bypass channels 9 passes through the center of the next third toroid 6 / III. and at the same time it flows around it from the sides through an axial channel 8 formed by the circumference of the third toroid 6 / ΠΙ. and chamber cylinder χ. This occurs behind the third toroid 6 / III. to turbolent flow and to increase the flow rate of the fuel being treated. The fuel flows around the radial 9 and axial bypass channel 8 of the second prism 7 / IL and further flows through the slit forming the axial bypass channel 8 between the circumference of the second prism 7/11. and a cylinder X, thereby reducing the flow rate of the treated, homogenized fuel. From the third neodymium axial permanent magnet in the shape of a prism 5/1. all the magnets are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also mounted identically to the axis of the chamber. Such an orientation of the neodymium axial permanent magnets creates a repeated turbolent flow in the resulting radial channels 9 and a strong homogeneous magnetic field between the neodymium axial permanent magnets. It creates a strong scattering magnetic field in the interior of neodymium toroidal axial permanent magnets. In a strong homogeneous magnetic field, the individual molecular dipoles of the fuel rotate, in the opposite direction to the action of the homogeneous magnetic field, in the device there is a better mixing of the fuel at the molecular level and its homogenization. During the outflow from the device, the flow of the treated homogenized fuel is again reduced, which flows out through the axial opening in the lid of the chamber body 3.

The advantage of the described combinations of the arrangement of neodymium axial permanent magnets in a device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, in Figs. 1-6, is to achieve optimal repeated turbolent flow with changes in flow rate of treated liquid or gaseous fuel. Strong magnetic fields act on the fuel with their energy, in the radial channels 9, which are purposefully created in the device. The strong magnetic field with its energy affects the intermolecular bonds and clusters of fuel molecules. Therefore, in order for the magnetic field to be strongly inhomogeneous in the first part of the device, then the first three neodymium axial permanent magnets must be placed in the body of the device chamber 1 with identically oriented poles on the faces of the first three magnets. The flow of fuel through this inhomogeneous magnetic field causes its energies to affect intermolecular bonds and clusters of fuel molecules, which separate from each other, and the energy of the magnetic field curves the paths of motion of fuel molecules and can rotate with them. Additional neodymium axial permanent magnets are then placed in the chamber body of the device 1, which are placed with oppositely oriented poles on the faces of the magnets in order to create a strong homogeneous field. In a strong homogeneous field, the fuel flows turbulently and repeatedly in the intentionally formed radial channels 9, which results in better mixing at the molecular level. When the above-described neodymium axial permanent magnets are placed in the body of the chamber, with the opposite poles facing the magnet faces, the individual molecular dipoles of the fuel rotate, and the fuel is homogenized repeatedly. The fuel flowing out 11 from the chamber of the device 1 is homogenized and during its gasification more atmospheric oxygen can be added to the mixture. Higher atmospheric oxygen content contributes to better combustion of the mixture in the cylinder heads of the internal combustion engine, turbine, gas boilers, etc. Improved fuel combustion increases the performance of the internal combustion engine, turbine, gas boiler, etc. with the same fuel consumption and significantly reduces the amount of emissions released into the atmosphere.

Industrial applicability

The proposed device for performing magnetic treatment of liquid and gaseous and reducing emissions, according to the proposed patent, is applicable to all petrol or diesel engines for liquid or gaseous fuels. The device can be used not only in the automotive industry to reduce fuel consumption and emissions, but it can also be used in other motor vehicles, such as truck and bus transport, agriculture, shipping, rail and air transport, etc. It can also be used in urban public transport buses, where fuel treatment will result in greener operation and environmental protection in cities and conurbations. The device can also be suitably used in mechanical engineering, construction and other machines that are powered by internal combustion engines for liquid and gaseous fuels. It can also be used in the gas system for heating buildings, where heating becomes more economical and environmentally friendly. The proposed device can be used in the modification of already manufactured engines, or it can be installed in older motor vehicles. The present invention can also be used to perform magnetic gas treatment, which can be further used more efficiently in internal combustion engines, in gas burners, or in the chemical industry and other fields of possible use.

Claims (18)

PATENT CLAIMS Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, characterized in that it consists of a cylinder chamber (1) closed by a lid (2) with an axial opening for the inflow (10) of liquid or gaseous hydrocarbon fuels and a lid (3) with an axial opening for the outflow (11) of liquid or gaseous fuels, which forms a chamber body by connecting with an internal or external thread or by gluing. According to Fig. 1, letters A), neodymium axial permanent magnets in the shape of a cylinder (5) and neodymium axial permanent magnets in the shape of a toroid (6) are placed alternately or repeatedly in the cylinder axis of the chamber (1) in the cylindrical body thus formed. . According to FIG. 1, the neodymium axial permanent magnets in the shape of a prism (7) and the neodymium axial permanent magnets in the shape of a toroid (6) are mounted alternately or repeatedly in the direction of the cylinder axis of the chamber (1). Said first three neodymium axial permanent magnets, according to Fig. 1, letter A) in the form of a first cylinder (5 / L), a first toroid (6/1.) And a second cylinder (5 / II.) And according to Fig. 1, letters B) in the form of a first prism (7/1), a first toroid (6/1) and a second prism (7 / IL) are oriented towards each other by corresponding magnetic poles on the faces of said magnets. From the third neodymium axial permanent magnet according to Fig. 1, letter A) in the shape of a second cylinder (5 / II.) And according to Fig. 1, letter B) in the shape of a second prism (7 / II.), All neodymium axial permanent magnets are in the chamber of the body of the device oriented to each other by opposite magnetic poles on the faces of said magnets and are also mounted coincident with the axis of the chamber. According to Figs. in the given basic set, in order, according to the given picture. Even in these chambers, the first three neodymium axial permanent magnets are oriented towards each other by matching magnetic poles on the faces of said magnets. From the third neodymium axial permanent magnet, all the neodymium axial permanent magnets in the device body chamber are then oriented towards each other by opposite magnetic poles on the faces of said magnets and are also arranged in line with the chamber axis. According to Figs. the magnets are located non-magnetic spacers (4), which form radial bypass channels (9) and the direction of inflow of liquid or gaseous hydrocarbon fuel (10) is important for the functionality of the device. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claim 1, characterized in that all used magnets stored in the non-magnetic cylinder of the device chamber (1) are only neodymium axial permanent magnets, with surface treatment. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 2, characterized in that all used magnets stored in the non-magnetic cylinder of the device chamber (1) are only neodymium axial permanent magnets with surface treatment, anisotropic direction of magnetization and are placed identically with the axis of the chamber. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 3, characterized in that neodymium axial permanent magnets arranged in the non-magnetic cylinder of the device chamber (1) are arranged so that they part -25 created a strong inhomogeneous magnetic field and a strong homogeneous magnetic field in the following part of the chamber of the device. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 4, characterized in that individual neodymium axial permanent magnets with surface treatment and anisotropic magnetization direction with magnetic poles on the magnet faces are in the cylinder chamber (1). The devices are arranged so that the first three neodymium axial permanent magnets are oriented towards each other by corresponding magnetic poles on the faces of said magnets. From the third neodymium axial permanent magnet, all subsequent neodymium axial permanent magnets mounted in the body chamber (1) of the device are oriented to each other by opposite magnetic poles on the faces of said magnets and are mounted coincident with the chamber axis. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 5, characterized in that the outer diameter of the non-magnetic cylinder of the device chamber (1) is given by dimensions ranging from 20 mm up to 250 mm. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1). ) - toroid (6/1.) cylinder (5 / II.) - toroid (6/11.) - cylinder (5 / ΙΠ.) - toroid (6 / ΙΠ.) - cylinder (5 / IV.), or repeatedly. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder chamber (1) in the order: prism (7 / L) - toroid (6/1.) - prism (7 / Π.) - toroid (6/11.) prism (7 / IIL) - toroid (6 / IIL) - prism (7 / IV.), or repeatedly. Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1). ) - toroid (6/1.) cylinder (5/11.) - toroid (6 / II.) - cylinder (5 / III.) - toroid (6 / IIL) - prism (7 / L). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: prism (7/1). ) toroid (6/1.) - prism (7 / IL) - toroid (6 / IL) prism (7 / IIL) - toroid (6 / IIL) - cylinder (5/1.). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1.) - toroid (6/1.) cylinder (5 / II.) - toroid (6 / IL) - prism (7 / L) - toroid (6/111.) - prism (7 / IL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial -26permanent magnets are stored in the cylinder chamber (1) in the following order: prism (7/1.) - toroid (6/1.) - prism (7 / II.) - toroid (6 / II.) - cylinder (5 / 1.) - toroid (6 / IIT.) - cylinder (5 / IL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1). ) - toroid (6/1.) prism (7/1.) - toroid (6 / IL) - prism (7/11.) - toroid (6 / III.) - prism (7 / IIL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: prism (7/1). ) - toroid (6/1.) - cylinder (5/1.) toroid (6 / II.) - cylinder (5 / IL) - toroid (6 / IIL) - cylinder (5 / IIL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1). ) toroid (6/1.) prism (7 / L) - toroid (6 / IL) - cylinder (5 / II.) - toroid (6 / III.) - prism (7 / IL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder chamber (1) in the order: prism (7/1) toroid ( 6/1.) - cylinder (5/1.) - toroid (6 / IL) - prism (7 / IL) - toroid (6 / IIL) - cylinder (5 / IL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder of the chamber (1) in the order: cylinder (5/1). ) - toroid (6/1.) prism (7/1.) - toroid (6 / IL) - prism (7 / IL) toroid (6 / III.) - cylinder (5 / IL). Device for performing magnetic treatment of liquid and gaseous fuels and reducing emissions, according to claims 1 to 6, characterized in that the individual neodymium axial permanent magnets are arranged in the cylinder chamber (1) in the order: (prism (7 / L) - toroid ( 6/1.) - cylinder (5/1.) - toroid (6 / II.) - cylinder (5 / II.) Toroid (6 / IIL) - prism (7 / IL).