WO2020251392A1

WO2020251392A1 - Hydrodynamic perpetual motion machine

Info

Publication number: WO2020251392A1
Application number: PCT/RU2019/000430
Authority: WO
Inventors: Геннадий Александрович ОЛЕЙНОВ
Original assignee: Геннадий Александрович ОЛЕЙНОВ
Priority date: 2019-06-14
Filing date: 2019-06-14
Publication date: 2020-12-17

Abstract

Proposed is a hydrodynamic perpetual motion machine which generates an unsupported force as a liquid or gas moves in a cavity or channel thereof, in which a special device is installed, the design of which depends on the purpose of the hydrodynamic device. The invention is directed toward producing energy by means of producing an unsupported force during the movement of a liquid or gas in the hydrodynamic device.

Description

ETERNAL ENGINE HYDRODYNAMIC.

This invention makes it possible to obtain energy mainly through obtaining an unsupported force when a liquid or gas moves in a hydrodynamic device. In some embodiments of such a device, additional energy of the flow can be obtained, for example, by converting it into mechanical energy of rotation of the built-in rotor, or by dividing the flow into its component parts by temperature. This invention contradicts the main theoretical postulates of today. They say that the jet thrust is proportional to the amount of motion of the thrown jet, that the lifting force of the wing is formed when a circulation of speed around the wing profile appears, that the mechanical energy of the flow, for example, leaving the pipe, cannot be greater than at the inlet. In the same application, it is said that it is possible to obtain an unsupported force in a variety of hydrodynamic devices, if one adopts other views, namely, that the jet thrust is equal to the resulting from the pressure diagram of the liquid or gas flow on the solid parts of the structure, and the lift of the wing is due to the difference pressures on wing surfaces. In the lower part of the wing, energy arises (there is a higher level of both speed and pressure), and in the upper part it disappears. At the exit from the pipe, if there is a sufficient velocity, the level of static pressure, by special devices, can be close to the level at the inlet, which generally increases the momentum and energy of the flow. Or vice versa - to “extinguish” the energy.

This application includes the main provisions of applications PCT / RU 2012/001051; PCT / RU 2013/000021; PCT / RU 2013/000246 and patent RU Ns 2116223.

Unsupported force and energy is created by special devices installed in any cavity of the hydrodynamic device. If the cavity is intended for rotational, around the axis, and circulation, in the axial plane, movement of the liquid, for example, as in a hydrodynamic transmission, with pump and turbine wheels, then on the transmission housing in the cavity, at radii greater than the radius of the periphery of the impeller blades, on the path of fluid movement from the axis, a special device is installed in the form of one or more channels, for example, interscapular, in the scapula, and the channels have bends with a bulge on the periphery, from the axis. With this design, in addition to obtaining an unsupported force, the hydrodynamic transmission is used as a source of mechanical energy from the turbine wheel, at some cost for rotating the pumping station. If the hydrodynamic device contains a vortex chamber, then the channels bent from the axis can be installed on one of the inner, for example conical, walls of the vortex chamber cavity, on the flow path to the periphery of the chamber in combination with one or more channels, for example, interscapular, on the other wall, on the path of the flow to the axis. The flow is supplied to the vortex chamber at its axis, at smaller radii, and at least one branch is at large, and in the presence of two branches, in particular, one of them is on the axis, the hydrodynamic device is used as a refrigerator or heater. One of the simplest options for obtaining an unsupported force is to place at least three baffles dividing the flow, in the direction of motion, into zones with a certain pressure level, in the flow path from a cavity with a high pressure to a cavity with a lower pressure, in the channel for fluid movement, for example , in the form of grids installed across the flow. A more significant force can be obtained by performing the device in the form of a channel narrowing along the flow, and as a special device to install a cone-shaped or dome-shaped cavity to turn the flow after leaving the converging channel into the return channel for inhibited fluid movement back to the turning section into the narrowing channel ... A special device can be made in the form of walls with the possibility of some displacement channels, which are designed to forcefully influence the flow in the channel, therefore, in the simplest versions, they fence off additional cavities from the channel cavity with a given pressure of the medium, for example, such walls can be made in the form of hinged plates separating additional cavities and the channel cavity with communication between cavities through holes inclined to the direction of flow in the channel.

The drawing illustrates the present invention.

Figure 1 shows a variant of the design of the hydrodynamic transmission as an additional source of mechanical energy.

Figure 2 is a view, along section A-A, of the interscapular channels of the stationary scapular apparatus.

In Fig. 3 - a variant of the vortex chambers also with the function of a temperature flow separator.

Figure 4 is a variant of a hydrodynamic device that creates an unsupported force.

Figure 5 shows a variant of a device with a domed reversal cavity.

Fig. 6 shows embodiments of special devices in the converging channel.

The hydrodynamic device in which the special device according to the present invention is installed becomes a device for obtaining an unsupported force. At the same time, depending on its design, it can be a source of mechanical energy, a refrigerator or a heater. For example, a hydrodynamic transmission with a torus cavity 1 (Fig. 1), which contains a pump blade 2, and a blade 3 of turbine wheels. As a special device in the cavity 1, channels 4 (Fig. 2) are made between the blades of the blades 5 (Fig. 1), which are located at a greater distance from the axis 6 of the cavity 1 than the impeller blade 2 of the pump wheel, and are fixed on the housing 7 hydrodynamic transmission. The interscapular channels 4 of the apparatus 5 have a convex bend from the axis 6 (Fig. 2) of the cavity 1. In particular, the channel 4 can be only one and made in the form of a spiral. In the variant with a vortex chamber 8 (Fig. 3), similar (4 in Fig. 2) curved channels are located between the blades in the blades 9 installed on one of the walls, for example, on the conical wall 10, where the flow moves to large radii vortex chamber 8. In this case (in Fig. 3), instead of the blades 3 of the turbine wheel in Fig. 1, in the cavity of the chamber 8, a blade 11 is installed, located on another, conical, wall 12 (Fig. 3). The interscapular channels of the apparatus 11 have bends that provide a decrease in the tangential component of the flow velocity with an increase in the axial component and the direction of the flow to the concave part 13 for turning, i.e. they are also bent with a bulge from the axis of the chamber 8 and can be of various shapes, composite or singular. To supply the medium flow to the vortex chamber 8, an axial channel 14 is made, and the outlet is divided into, for example, two channels. One (15) is paraxial, and the other (16) is on a larger diameter of the vortex chamber 8. The vane apparatus 17 (Fig. 3) has a tangential direction of the blades, for example, in the form of one spiral blade, to provide preliminary swirling of the flow entering the vortex chamber 8 from channel 14. In another version of the hydrodynamic device having a channel in the housing 18 (Fig. 4), in which between the cavity 19 of higher pressure, with the screw 20 and the cavity 21 of lower pressure, as a special device are installed across the direction flow movement in the housing 18, partitions of various shapes - in the form of grids 22, throttling plates 23, transverse plates 24, enclosing cavities 25, also limited by pliable, for example, rubber surfaces 26, profiles 27 in the form of plates located at an angle to the direction of movement flow, etc. In particular, an embodiment of the partitions is possible in the form of a set of parallel, for example capillary, channels with sufficiently thin walls parallel to the direction of flow. These partitions have a flow area in the direction of movement and divide the channel in the housing 18 into zones with different pressure levels. Additionally, the channel 28 can be made to close the movement of the medium after the baffles again to the screw 19, as well as the channel 29 to maintain the required pressure level along the transverse cavities. Another option assumes the presence of a narrowing, along the flow, channel 30 (Fig. 5), with a screw or auger 31 installed in it. Here, as one of the special devices, a set of inclined profiles 32 connecting the sides of the channel 33 with the sides of the channel 30 is shown Channel 33 is intended for the opposite direction of flow in channel 30, fluid flow and both of them are fixed in front of the dome-shaped cavity 34, designed to turn the flow from channel 30 to channel 33. Special devices can be installed in any channel 35 (Fig. 6) with a moving environment, such as confusing. Such devices can be in the form of pliable, for example, rubber 36 walls or hinged plates 37, separating additional cavities 38 from the channel cavity 35, which can be connected through control devices, such as valve 39, to a source of a certain pressure or connected to the cavity of the channel 35 with holes 40 inclined to the direction of flow. In addition, as a special device, it is possible to install a thin tapered sleeve separating an additional cavity 38 from the channel 35, for example, made of plexiglass. and various stripes of the type of bird feathers, etc.

During the operation of the presented variants of the hydrodynamic device, that is, when a liquid or gas flows in its channels, an unsupported force arises in the direction B (Figs. 1, 3, 4, 5, 6). In the hydrodynamic transmission (Fig. 1), the rotation begins with the pumping wheel with the blade apparatus 2, after which the liquid enters the channels 4 (Fig. 2) of the blade apparatus 5, where it receives an additional moment of momentum around the axis 6. In this case, the static pressure of the moving to the periphery flow of liquid rotating around the axis 6, due to the action centrifugal forces, does not fall, but grows. Those. with an increase in the angular momentum and kinetic energy of the flow, the pressure increases due to the increase in the radius of rotational motion. The received energy is transferred to the blades 3 of the turbine wheel with the return of the flow to the axis of the cavity 1 and the braking of the rotational movement around the axis 6. The energy received by the turbine wheel is greater than the costs of the impeller, which, after starting, can be connected to the turbine wheel. The liquid rotating around the axis 6 is aligned along the radius of the cavity 1 strictly in accordance with the level of mechanical rotation energy - the streams that acquire energy, in the apparatus 5, go to the periphery, and those that lose energy, in the apparatus 3, go to the axis. At the same distance from the axis 6 or radius, the pressure on the walls of the cavity 1 near the blade apparatus 5 is less (the flow accelerates) than near the apparatus 3 (the flow is inhibited). Which creates the resulting force in the direction B. In the same way, a force arises in the direction B, when the flow moves in the vortex cavity 8 (Fig. 3), - the general acceleration of the flow in the blade apparatus 9 (plus the action of centrifugal forces on the inner surface of the conical wall 10 ) and the deceleration of the flow in the blade apparatus 11. And in this case, the flow jets rotating around the axis 6 are aligned according to the mechanical energies of rotation - the jets with greater energy occupy large radii, which leads to laminarization of the rotational motion and the stratification of the flow by temperature - the peripheral jets get large temperature than those closest to the axis 6. The same as in the Rank-Hilsch vortex tube. Therefore, a cooled flow comes from channel 15, and a heated one from channel 16. But in this invention, if the gas flow, in contrast to the Ranque-Hilsch tube, appears, like the Natural Tornado (Tornado), additional energy due to the removal, by the guide vane 11, of the momentum of the jet into the axial vortex zone, into the low pressure, where this jet of expanded gas is cooled, and then heated with compression at the periphery (i.e., a thermodynamic cycle with the release of mechanical energy). This eliminates the need for an energy source, pump or compressor, for pumping the medium through the vortex chamber. When a hydrodynamic device with a housing 18 (Fig. 4) is operating, in the cavity 19, for example, by the screw 20, an increased level of fluid pressure is created, which creates a force in the direction B, and it moves to the cavity of reduced pressure 21. In this case, a special device in the form transverse partitions (22,23,24,25,26,27 in Fig. 4), creates flow conditions with alternating accelerations and decelerations, which breaks down the total pressure drop along the length of the flow in the body cavity 18 into a certain number of drops, and the total speed flow is determined only by the total flow area of one partition and the difference on it. Therefore, the total flow rate of the fluid flow is less, when compared with a flow without baffles, per root of the number of baffles (according to the Bernoulli equation). This makes it possible not to eject the flow, as in a jet propulsion unit, outward, but to return it again to the cavity 19 through channel 26, in which a pump can be installed, replacing the screw 20. In the embodiment in Fig. 5, the flow accelerates in channel 30 with high pressure, than in the same confuser with solid and smooth walls (thanks to 32 profiles), acquiring kinetic energy and momentum. After leaving the channel 30, the flow enters the dome-shaped cavity 34, creating in it an increased pressure level and force in the direction B, with a turn in the opposite direction, into the channel 33 and decelerating the flow. From channel 33, the decelerated flow again enters the entrance to channel 30. In the converging channel 35 (Fig. 6), when a liquid or gas moves, an unsupported force is also created in the direction B, i.e. in the direction of flow. Here, the surfaces 36 and 37, due to the force acting from the pressure of the medium in the cavities 38, create an increased level of static pressure of the flow in the cavity of the channel 35 in the same way as it happens under the wing of an aircraft. But the unsupported force in the latter case can also be obtained in the direction opposite to B shown in Fig. 6. When the pressure in the cavities 38 is less than the static pressure of the flow. The operability of this invention is confirmed by both experiments and a simple overview of modern technology. For example, when a motor with a propeller is placed from a child's toy into a closed cavity, its weight changes during and without operation (by about 5 grams). If a closed cavity with a nozzle injecting liquid into it is pivotally suspended on links, then an unsupported force can also be detected. It has long been noted that a tube with a cyclically variable flow area in the direction of flow has a much higher resistance than an even tube with a constant flow rate smaller than that of the first flow area. Confuser with a coaxial conical movable wall (for example, made of plexiglass), separating a cavity with an increased pressure level from the flow, gives an addition of jet energy such that the total energy of the jet becomes greater than at the inlet. The article "Useful tornado" (magazine "Inventor and Rationalizator", Nsl l, 1982, Moscow) describes an increase in the range of a jet from a fire hose by 30% with a special tube attached. The appearance of "Unexplained" energy and momentum of the jet of a commutative explosion piercing the armor can be explained by its acceleration at constant (and even growing) external pressure (as in Figs. 5 and 6). In the 1950s, jet engines threw out jets with tremendous speed and strong sound. At present, the sound has become quieter, but the speed of the jet stream has dropped, and the thrust of the engines has increased significantly! The greater the thrust, the larger the cross-section of the engine, which means that the matter is still not in the speed of the thrown jet, but in the pressure diagram on the solid parts of the structure. Aircraft are braked by reverse thrust, but the jets do not hit forward, but to the sides! This means that this is not a reaction of the thrown jet. Can you turn the engines in the opposite direction, and take off? (See Fig. 5). When leaving, in the hydrodynamic device according to figure 1, only one wheel with the location of the blades 2 on a larger diameter than the blades 5, the power of rotation of the wheel is sufficient (on water) only to maintain this rotation in bearings without load. Those. Fig. 1 shows a significantly more efficient option with obtaining both an unsupported forces and energy of rotation. The aircraft is kept in the air due to the fact that the pressure under the wing is greater than the pressure of the surrounding stationary air, and above the wing it is less. Therefore, a person does not feel the weight of a heavy transport aircraft, even flying 8 meters above it. Just like a water skier "pressing down" the water with a small hole.

If we compare the device according to Fig. 4 with a jet propulsion device of the same thrust, then when setting into the device, for example, 100 partitions, the flow rate in it is 10 times less, which means that the power consumption is almost 100 times less, and the screw 20 has, at the same speed of rotation is much smaller step; and you can simply put a low-power pump in channel 28. It will be efficient to install partitions from small-section tubes, for example, capillary ones. The variant in Fig. 3 can, in addition to obtaining an unsupported force, be used for heating or cooling rooms, and even as a source of water, when it condenses from the atmosphere. The variant in Fig. 6 can be used as a device for reducing the resistance of pipes, for example, main pipes. If the variant according to Fig. 3 is intended mainly to obtain flows with different temperatures, then it is preferable to make the wall 10 either at right angles to the axis of the chamber, or at an acute angle, inside the chamber 8, to the axis. You can make both walls 11 and 12 flat, at right angles to the axis 6, or you can run the flow in the vortex chamber 8 (Fig. 3) in the opposite direction - from channel 15 to channel 14 (with the transfer of the installation site of the apparatus 17 ).

Thus, the scope of the present invention is very broad. This is the drive and braking of any vehicles; heating and cooling the room; obtaining water from the atmosphere by freezing air; significant reduction in the cost of pumping liquids and gases in pipelines, etc.

Claims

CLAIM.

1. The perpetual motion machine is hydrodynamic with the receipt of an unsupported force when a liquid or gas moves in its cavity or channel; a special device is installed, the design of which depends on the purpose of the hydrodynamic device.

2. Perpetual motion machine hydrodynamic p. 1, characterized in that if the hydrodynamic device has an axisymmetric cavity, as in a hydrodynamic transmission, with the blades of the pump and turbine wheels, a special device is made as a channel or channels, for example, inter-blade channels in a guide vane installed inside the cavity on housing, and these channels are installed at a distance from the cavity axis greater than the impeller blade so that the flow moves to the periphery through them and these channels have convex bends from the cavity axis, and the hydrodynamic device itself, with this design, can be used and as a source of mechanical energy of rotation of the turbine wheel and as an unsupported propulsor.

3. Perpetual motion machine hydrodynamic p. 1, characterized in that, if the structure has a vortex chamber, a special device is made in the form of one or more channels, for example, interscapular in a blade apparatus, installed on one of the inner walls, for example, a conical one, where the flow moves to the periphery of the chamber, and these channels have bends with a convexity directed from the axis of the chamber, in addition, similar channels, with a bulge from the axis, are also made in the place of flow movement to the axis of the chamber, for example, on the opposite conical wall, in particular, when using a hydrodynamic device for flow separation by temperature, medium supply channel to the vortex chamber is located on the axis of the chamber, and the outlets are divided at least into two, peripheral and paraxial.

4. Perpetual motion machine hydrodynamic pri. 1, characterized in that if there is a channel in it connecting cavities with higher and lower pressures, where the surrounding space can be a cavity with lower pressure, at least three partitions are used as a special device, for example, in in the form of installed grids transversely to the flow, having a flow section in the direction of flow and dividing the channel into sequentially, in the direction of flow, located zones with certain pressure levels, which makes it possible to obtain a source of unsupported force.

5. Perpetual motion machine hydrodynamic p. 1, characterized in that the device for obtaining an unsupported propulsive device contains an accelerating section in the form of a converging channel, a channel for the reverse movement of liquid or gas and a dome-shaped cavity for flow reversal, which connects these channels.

6. Perpetual motion machine hydrodynamic p. 1, characterized in that in the channel for the movement of liquid as a device, displaceable or flexible walls are installed, for example, in the form of hinged plates, which, to create a certain level of static pressure of the flow, are separated from the cavity channel additional cavities with predetermined pressure levels obtained mainly by connecting them to the channel cavity with openings.