WO2019078752A1

WO2019078752A1 - Hydrodynamic perpetual motion machine

Info

Publication number: WO2019078752A1
Application number: PCT/RU2017/000767
Authority: WO
Inventors: Геннадий Александрович ОЛЕЙНОВ
Original assignee: Геннадий Александрович ОЛЕЙНОВ
Priority date: 2017-10-20
Filing date: 2017-10-20
Publication date: 2019-04-25

Abstract

Proposed is a hydrodynamic perpetual motion machine which generates a non-support force as a liquid or gas moves in a cavity or channel thereof, wherein a special device is installed, the design of which depends on the purpose of said hydrodynamic device.

Description

ETERNAL ENGINE HYDRODYNAMIC.

This invention allows to obtain energy, mainly through the means of obtaining unsupported force during the movement of a liquid or gas in a hydrodynamic device. In some embodiments, the execution of such a device can receive additional energy flow, for example, with its translation into mechanical energy of rotation of the built-in rotor or to divide the flow into its component parts according to temperature. This invention contradicts the basic theoretical modern tenets. Which state that the jet thrust is proportional to the amount of movement of the jet thrown, that the wing lift force is formed when the circulation speed appears around the wing profile, that the mechanical energy of the flow, for example, coming out of the pipe, cannot be greater than at the entrance. In this application, it is said that it is possible to obtain unsupported force in various hydrodynamic devices, if it is established in other views, namely that jet thrust is equal to the pressure of the flow of a fluid or gas flow to the solid parts of the structure resulting from the plot, and the lifting force of the wing is due to the drop pressure on the surfaces of the wing. In the lower part of the wing, energy arises (there is a higher level and speed and pressure), and in the upper part it disappears. At the outlet of the pipe, if there is a sufficiently large velocity, the level of static pressure, by special devices, can be brought closer to the level at the inlet, which generally increases the amount of movement and energy of the flow. And it is possible and vice versa - to “redeem” energy.

This application includes the main provisions of applications PCT / RU 2012/001051; PCT / RU 2013/000021; PCT / RU 2013/000246 and RU JV2 2116223 patent.

Reliable power and energy is created by special devices installed in any cavity of a hydrodynamic device. If a The U2017 / 000767 cavity is designed for rotational, around an axis, and circulating, in an axial plane, fluid motion, for example, as in a hydrodynamic transmission, with pumping and turbine wheels, then on the transfer housing in the cavity, on radii greater than the radius of the periphery of the pumping blades wheels, on the path of the fluid from the axis, a special device is installed in the form of one or several channels, for example, interscapular, in the blade apparatus, and the channels have bends with convexity to the periphery, from the axis. With this implementation, in addition to obtaining unsupported force, the hydrodynamic transmission is used as a source of mechanical energy from the turbine wheel, with some costs for rotating the pumping wheel. If the hydrodynamic device contains a vortex chamber, the channels bent from the axis can be installed on one of the inner, for example conical, walls of the cavity of the vortex chamber, along 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 flow to the axis. The flow into the vortex chamber is carried out at its axis, at smaller radii, and, at least one, at large, and if there are two branches, in particular, one of them - at the axis, the hydrodynamic device is used as a refrigerator or heater. One of the simplest options for obtaining unsupported force is to set up in the channel for the movement of fluid, on the path of flow from the cavity with greater pressure to the cavity with less pressure, at least three partitions dividing the flow, in the direction of movement, into zones with a certain pressure level, for example , in the form of grids installed across the stream. A more significant force can be obtained by performing the device in the form of a narrowing downstream channel, and as a special device, install a cone-shaped or dome-shaped cavity to turn the flow after leaving the narrowing channel into the reverse channel for the inhibited movement of fluid back to the turning section into the narrowing channel . A special device can be made in the form of having the possibility of a certain displacement of the walls. channels that are intended to force the flow in the channel; therefore, in the simplest cases, they isolate additional cavities from the cavity of the channel 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 inclined to the flow direction in the channel holes.

The drawing explains the invention.

Figure 1 shows a variant of the design of hydrodynamic transmission in the additional quality of a source of mechanical energy.

Figure 2 is a view, along the section A-A, on the interscapular channels of stationary shoulder blades.

In FIG. 3, a variant of the vortex chambers is also with a function as a temperature separator for the flow.

Figure 4 is a variant of the hydrodynamic device that creates a supportless force.

Figure 5 is a variant of the device with a dome-shaped reversal cavity.

Figure 6 - embodiments of special devices in the confused channel.

A hydrodynamic device into which a special device is installed, according to this invention, becomes a device for obtaining 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), in which there are a pumping unit 2 of the pumping unit, and a blade unit of the turbine wheel 3. As a special device in the cavity 1, the channels 4 (FIG. 2) between the blades of the blade apparatus 5 (FIG. 1) are made, which are located at a greater distance from the axis 6 of the cavity 1 than the blade blade 2 of the impeller, and are fixed to the housing 7 hydrodynamic transmission. Interscapular channels 4 of the apparatus 5 have a bend convexity 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 the vortex chamber 8 (FIG. 3), similar (4 in FIG. 2) curved channels are located between the blades in the blade apparatus 9 mounted 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 blade apparatus 3 of the turbine wheel in FIG. 1, a blade apparatus 11 located on another conical wall 12 (FIG. 3) is installed in the cavity of chamber 8. 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 flow to the concave part 13 for turning, i.e. they are also curved with a bulge from the axis of the chamber 8 and can be of various shapes, composite or singular. To supply the flow of the medium into the vortex chamber 8, the 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 blade apparatus 17 (FIG. 3) has a tangential direction of the blades, for example, in the form of one spiral blade, to provide a preliminary swirl of the flow entering the vortex chamber 8 from channel 14. In another embodiment of a hydrodynamic device having a channel in housing 18 (FIG. 4), in which between cavity 19 there is more pressure, with screw 20 and cavity 21 less pressure, as a special device installed across the direction flow in the body e 18, partitions of various shapes — in the form of grids 22, throttling plates 23, transverse plates 24, fencing off cavities 25, which are also limited by compliant, for example, rubber surfaces 26, profiles 27 in the form of plates arranged at an angle to the direction of flow, and 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 motion and divide the channel in the housing 18 into zones with different pressure levels. Additionally, channel 28 can be made to close the movement of the medium after the partitions again onto screw 19, as well as channel 29 to maintain the required level of pressure along transverse cavities. Another option involves the presence of a tapering, downstream, channel 30 (figure 5), with a screw or screw 31 installed in it. Here, as one of the special devices, a set of inclined profiles 32 connecting the sides of the channel 33 is shown, with the sides of the channel 30 Channel 33 is designed to reverse the direction of flow in channel 30, the flow of fluid and both 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 (6) with a moving Wednesday th, for example confused. Such devices can be in the form of flexible, for example, rubber 36 walls or hinged plates 37, which separate additional cavities 38 from the cavity of the channel 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 is inclined to the direction of flow of the holes 40. In addition, as a special device, you can install a thin conical sleeve that separates from the channel 35 an additional cavity 38, for example, from eksiglasa. Or different stripes like bird feathers, etc.

During the operation of the presented variants of a hydrodynamic device, i.e., with the flow of a liquid or gas in its channels, a supportless force in direction B arises (Fig. 1, 3, 4, 5, 6). In the hydrodynamic transmission (Fig. 1), the pumping wheel starts with a blade unit 2, after which the liquid enters the channels 4 (Fig. 2) of the blade apparatus 5, where it receives an additional amount of momentum around the axis 6. At the same time, the static pressure moving to the periphery flow rotating around the axis 6 of the fluid, due to the action centrifugal force does not fall, but grows. Those. with the growth of the angular momentum and the kinetic energy of the flow, the pressure increases, due to the increase in the radius of the rotational motion. The resulting energy is transferred to the blade unit 3 of the turbine wheel with the return of the flow to the axis of the cavity 1 and the braking of the rotary around the axis of motion 6. The energy received by the turbine wheel is greater than the cost of the pump wheel, which, after starting, can be connected to the turbine wheel. The fluid rotating around the axis 6 is aligned along the radius of cavity 1 strictly in accordance with the level of mechanical energy of rotation — energy acquiring, in device 5, trickles go to the periphery, and energy-losing, in device 3, to the axis. At the same distance from axis 6 or radius, the pressure on the walls of cavity 1 near the blade unit 5 is less (the flow accelerates) than near apparatus 3 (the flow is inhibited). This creates a resultant force in direction B. In the same way, a force arises in direction B, when the flow moves in the vortex cavity 8 (Fig. 3), the total acceleration of flow in the blade apparatus 9 (plus the effect of centrifugal forces on the inner surface of the conical wall 10 ) and deceleration of the flow in the blade apparatus 11. And in this case alignment of the flow streams rotating around the axis 6 along the mechanical rotational energies occurs — the trickles with greater energy occupy large radii, which leads to laminarization of the rotational motion and stratification iju temperature flow - peripheral streams obtained a higher temperature than the proximal to the axis 6. Just as in the vortex tube Ranque-Hilsch. Therefore from the channel 15 there is a cooled stream, and from the channel 16 - heated. But in this invention, if the gas flow, in contrast to the Ranka-Hilsch tube, appears, like the Natural Smerch (Tornado), additional energy due to removal, by the guiding device 11, the amount of jet movement in the axial zone of the vortex, in the zone of pressure, where cooling of the expanded gas occurs, and then heating with compression at the periphery (i.e., thermodynamic cycle with release of mechanical energy). This eliminates the need for a power source, pump or compressor for pumping medium through the vortex chamber. When the hydrodynamic device works with the housing 18 (FIG. 4), an increased level of fluid pressure is created in the cavity 19, for example, a screw 20, which creates a force in the direction B, and it moves to the cavity of the reduced pressure 21. At the same time, a special device, in the form transverse partitions (22,23,24,25,26,27 figure 4), creates flow conditions with alternating acceleration and braking, which breaks the total pressure drop along the length of the flow in the cavity of the housing 18 into a number of drops, and the total speed currents are determined only by the total races odnym section of one wall and drop on it. Therefore, the overall flow rate of the fluid flow is less when compared with the flow without partitions, to the root of the number of partitions (according to the Bernoulli equation). This allows you not to throw out the flow, as in a water-jet propulsion, outside, and return it back to cavity 19 through channel 26, in which a pump can be installed, replacing screw 20. In the embodiment of figure 5, the flow accelerates in channel 30 with high pressure, than in the same confuser with hard and smooth walls (thanks to profiles 32), acquiring kinetic energy and momentum. After exiting the channel 30, the flow enters the dome-shaped cavity 34, creating in it an increased level of pressure and force in the direction B, with a turn in the opposite direction, into channel 33 and deceleration of the flow. From the channel 33, the inhibited flow again enters the entrance to the channel 30. In the converging channel 35 (FIG. 6), as the fluid or gas moves, there is also a supportless force in the direction B, i.e. in the direction of flow. Here, the surfaces 36 and 37, due to the force acting on 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, just as it does under the wing of an airplane. But the unsupported force in the latter case can be obtained in the direction opposite to B shown in Fig.6. With a pressure in the cavities of 38 less than the static pressure of the flow. The performance of this invention is confirmed by experiments and a simple review of modern technology. For example, at the conclusion of a motor with a propeller from a children's toy in a closed cavity, its weight changes during operation and without (approximately 5 grams). If a closed cavity with a nozzle injecting fluid into it is pivotally suspended on the links, then it is also possible to detect unsupported force. It has long been observed that a tube that has a cyclically variable, along the flow, the flow section, has a much greater resistance than a flat tube with a constant and smallest than the first flow section. A confuser with a coaxially conical movable wall (for example, made of plexiglass), fencing off a cavity with an elevated pressure level from the flow, gives an increase in jet energy such that the total jet energy becomes larger than at the inlet. The article “Useful Tornado” (the journal “Inventor and Rationalizer”, Nel l, 1982, Moscow) describes an increase in the range of a jet from a fire engine by 30% with a special tube attached. The appearance of the “Unexplained” energy and the amount of movement of the jet of a cumulative explosion, penetrating the armor, can be explained by its acceleration at constant (and even increasing) external pressure (as in FIGS. 5 and 6). In the 50s jet engines threw jets with great speed and strong sound. At the present time, the sound has become quieter, but then the speed of the jet has dropped, and the thrust of the engines has increased significantly! The greater the thrust — the greater the cross section of the engine, so the matter is not in the speed of the jet being thrown, but in the plot of pressures on the hard parts of the structure. The braking of the aircraft occurs by reversing the thrust, but the jets are not beating forward, but to the sides! So this is not the reaction of the jet being thrown. You can turn the engines in the opposite direction, and take off? (See figure 5). When left, in the hydrodynamic device of FIG. 1, only one wheel with blades 2 on a larger diameter than blades 5, the wheel's rotational power is enough (on water) only to maintain this rotation in bearings without load. Those. figure 1 shows a significantly more efficient option with getting as unsupported force and rotational energy. The plane is kept in the air due to the fact that under the wing the pressure is greater than the pressure of the surrounding still air, and above the wing - less. Therefore, a person does not feel the gravity of a heavy transport aircraft, even flying 8 meters above it. As well as the water skier, "pressing down" the water with a small hole.

If you compare the device in figure 4 with a water jet propulsion of the same thrust, then when placed in a device, for example, 100 partitions, the flow rate in it is 10 times less, which means the power consumption is less almost 100 times less, and screw 20 has, for the same rotational speed is a much smaller step; and you can just put a low-power pump in the channel 28. Effective will be the installation of partitions from tubes of small cross section, for example, capillary. The variant in FIG. 3 can, in addition to obtaining unsupported force, be used for heating or cooling rooms, and even as a source of water, when it condenses from the atmosphere. Option 6 can be used as a device for reducing the resistance of pipes, such as trunk. If the variant of FIG. 3 is intended mainly for receiving flows with different temperatures, then it is preferable to make the wall 10 or at a right angle to the axis of the chamber, or at an acute angle, inside the chamber 8, to the axis. Both walls, 11 and 12, can be made flat, at right angles to axis 6, and it is possible to start the flow in the vortex chamber 8 (Fig. 3) in the opposite direction — from channel 15 to channel 14 (with transfer of installation location of the device 17 ).

Thus, the scope of this invention is very wide. It is driving and braking any vehicles; heating and cooling of the room; getting water from the atmosphere by freezing the air; significant reduction in the cost of pumping liquids and gases in pipelines, etc ..

Claims

CLAIM.

1. The perpetual hydrodynamic engine with obtaining unsupported force during the movement of a liquid or gas in its cavity or channel, a special device has been installed, the design of which depends on the purpose of the hydrodynamic device.

2. Perpetuum mobile hydrodynamic pop. 1, characterized in that when a hydrodynamic device has an axisymmetric cavity, as in a hydrodynamic transmission, with pumping and turbine wheel blades, a special device is made as a channel or channels, for example, interscapular in a guide vane installed inside the cavity on case, and these channels are installed at a distance from the axis of the cavity greater than the blade unit of the impeller so that the flow moves to the periphery through them and these channels have bends convex with the cavity axis, and the hydrodynamic device itself, with this design, can be used both as a source of mechanical energy of rotation of the turbine wheel and as a supportless propulsion unit.

3. Perpetuum mobile hydrodynamic pop. 1, characterized in that, if a vortex chamber is present in the structure, the special device is made in the form of one or several channels, for example, interscapular in a blade apparatus installed on one of the inner walls, for example conical, where the flow moves on the periphery of the chamber, and these channels have bends with convexity directed from the axis of the chamber, moreover, similar channels with convexity from the axis are also made at the point of flow to the axis of the chamber, for example, on the opposite conical which wall, in particular, when using a hydrodynamic device for separating the flow according to temperature, the channel for supplying the medium 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. Perpetuum mobile hydrodynamic pop. 1, characterized in that if there is a channel in it that connects cavities with higher and lower pressures, where the surrounding space may be a cavity with lower pressure, at least three partitions are used as a special device, for example transversely to the flow of installed grids having a flow section in the direction of flow and separating the channel in series, in the direction of flow, areas with certain pressure levels, which allow get the source unsupported force.

5. Perpetuum mobile hydrodynamic pop. 1, characterized in that the device for receiving a support-free propeller contains an accelerating section in the form of a converging channel, a channel for the reverse movement of a liquid or gas and a dome-shaped cavity for turning the flow that connects these channels.

6. Perpetuum mobile hydrodynamic pop. 1, characterized in that in the channel for the movement of fluid, displaceable or pliable walls are installed as devices, for example, in the form of hinged plates, which, to create a certain level of static pressure, are separated from the cavity channel additional cavities with predetermined pressure levels, obtained mainly by connecting them with the cavity of the channel holes.