IMPROVED FLYWHEEL ASSEMBLY

The flywheel assembly addresses inefficiencies in energy conservation and kinetic energy absorption by utilizing controlled air flow and resistance management, resulting in enhanced energy storage and reuse, improved stability, and increased compressor efficiency.

NL2040888B1Active Publication Date: 2026-07-14PACA PATENTS & IP BV

Patent Information

Authority / Receiving Office
NL · NL
Patent Type
Patents
Current Assignee / Owner
PACA PATENTS & IP BV
Filing Date
2025-07-25
Publication Date
2026-07-14

AI Technical Summary

Technical Problem

Existing flywheel assemblies fail to efficiently reuse compressed air, experience kinetic energy loss due to incorrect positioning of compression springs, and suffer from inefficiencies in energy conservation and external kinetic energy absorption, leading to delays, collisions, and energy wastage.

Method used

A flywheel assembly with a direct pneumatic connection between the first cylinder space and upper chamber, controlled valves for selective air flow, and additional features like the battery deck, correction deck, and fender deck to manage air flow and resistance, enhancing energy storage and reuse.

Benefits of technology

The flywheel assembly achieves efficient energy storage and reuse, reducing energy loss, improving operational stability, and increasing compressor efficiency by up to 60%, while minimizing noise and component costs.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

The invention relates to an improved flywheel assembly in accordance with the opening of claim 1. Such a flywheel assembly is known in the field, for example from Dutch patent NL2033561, the content of which is included herein by reference. The definitions, components and / or terminology used in this patent application are derived from the content of this patent. In general, in the known flywheel assembly, external energy cannot be conserved because the force of the mass does not fully propel the total mass of the flywheel in the direction of rotation to the desired position. The invention aims to provide a flywheel assembly in accordance with the opening, in which, among other things, the aforementioned disadvantage is eliminated.
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Description

| IMPROVED FLYWHEEL ASSEMBLY The invention relates to a flywheel assembly according to the introduction of conclusion 1. Such a flywheel assembly is known in the field, for example from the Dutch patent NL2033561, the contents of which are incorporated herein by reference. definitions, components and / or terminology used in this patent application are derived from the content of this patent. The well-known flywheel assembly has the following disadvantages: Firstly, it is not possible with the deposits from the known flywheel assembly sufficient compressed air be reused. Secondly, the first movement (downward) cannot be at the correct position of approximately be activated 90° within the desired speed, whereby external kinetic energy is largely lost. Thirdly, the compression springs of the unloading devices from the well-known flywheel assembly a fixed spring force, which does not over the vertical longitudinal distance, i.e. the length of a displacement of a mass in the vertical direction only, at all positions are desired. This results in delay, collision, and standstill with the used coupled masses. In general, with the known flywheel assembly, the external energy cannot be conserved, because the force of the mass does not fully conserve the total mass of the pushes the flywheel in the direction of rotation to the desired position. In doing so, the compression springs of the barrier devices are not positioned in the desired manner along the entire vertical longitudinal line set. The desired setting of the compression springs can only be selected at one movement speed. be set. The external kinetic energy cannot be absorbed with approximately 48%, because the compressed air pressure is the same during the first and second movement. The invention aims to provide a flywheel assembly according to the introduction, in which the aforementioned disadvantages have been eliminated. To this end, the inventive flywheel assembly has the characteristic that the seat a direct pneumatic second connection comprises between the first cylinder space and a upper chamber of the first cylinder, which second connection by means of a remote operable first valve is breakable; - includes a pneumatic third connection to the ambient air, which third connection is breakable by means of a remotely controlled second valve, and the controls are configured for 1) operating the first valve in such a way that the first valve only during the second movement is opened; 2) operating the second valve in such a way that the second valve only during the First movement is opened. It is noted here that the remark that the residence time of a mass at the descending side, between 0 and 180 degrees, is longer than the residence time of a mass on the ascending side, between 180 and 359 degrees can be explained as that the range of motion of a mass on the descending side, between 0 and 180 degrees, approximately The range of motion of a mass at the ascending side, between 180 and 359 degrees. In a first preferred design of the flywheel assembly according to the the invention comprises the upper chamber of the first cylinder at least a first spring which itself extends from the top of the first cylinder space to the top of the first piston. With the above-mentioned measures, externally introduced energy (compressed air in first cylinder) are stored in a more efficient way, without high and low pressure tanks are no longer needed. The energy is stored with the resistance via the first spring and with the compressed air that moves the first piston towards the upper chamber. This has led to consequence that the pressure point of the cylinder shaft has become much larger than the coupled connection position of the deposit to the flywheel with which the deposit directly connected to the flywheel, i.e. at a greater distance from the center of the flywheel. This pushes the flywheel away in its direction of rotation, thereby increasing the rotational speed. of the flywheel increases. The inventor has chosen to call this part of the barrier the Battery Deck. to be called, since this energy section also stores a part of the kinetic energy in the first spring and stores used compressed air from the lower chamber in the upper chamber. The Accudek thereby creates resistance to the movement on the underside of the first piston during the first movement and creates force on the top side of the first piston during the second movement. This force also ensures that the lower chamber is fully deflated during the second movement if desired. During the first movement, the Accudek ensures, by means of the first spring, additional resistance on the cylinder axis of the depositing agent, causing the attached coupled mass can never be pushed against the direction of rotation of the flywheel. In this process, external kinetic energy (compressed air force) is conserved during the first movement at approximately 80 to 145° of the arc. The vertical movement along the length line, i.e. the residence time of the mass at the desired position. position) on the descending side is extended. The flywheel experiences an acceleration in this process, because from the position of the mass in the direction of rotation is compressed. In a first embodiment of the flywheel assembly according to the invention the upper chamber comprises a filler block that extends from the top of the first cylinder space, such that the total maximum volume available for compressed air in the the upper chamber amounts to approximately 1.3 times the maximum volume of the lower chamber. As a result, it is volume of the upper chamber slightly larger than the volume of the lower chamber. This has as effect that the kinetic energy for the first movement is simple for the second movement with approximately 65% ​​of the compressed air force can be reused. It causes an acceleration of the flywheel, because the first spring with the help of the 65% reused compressed air in the upper chamber the position of the mass with force in pulls the direction of rotation. In a further elaboration of the flywheel assembly according to the invention, it comprises deposit a first leaf, of which a first side is the underside of the first forms a cylinder, in which the thrust device comprises a second leaf spring, which runs parallel to the first leaf spring, multiple spacers are installed between the first leaf spring and the second leaf spring), each of which is perpendicular to both the first leaf spring (15-1) and the second leaf spring, in which a first end of the spacers is fixedly connected to the first leaf spring and the second end of the spacers (5) can be moved by the second leaf spring, in which a second spring is fitted around each spacer. The The inventor has chosen to apply these technical measures to the correction deck to call. The application of the correction deck has the effect of preventing kickback when the second movement. The correction deck corrects or compensates for movements on the downward side for the attached coupled mass at the position of approximately 20° and approximately 145°. In a further elaboration of the flywheel assembly according to the invention, one or multiple first spacer blocks placed between the first leaf spring and the second leaf spring running parallel to the spacers in which a first side of the first spacer blocks are firmly connected to the second leaf spring. With these measures, the free movement distance of the correction deck can be set. In a second preferred design of the flywheel assembly according to the The invention comprises the flywheel assembly a second shaft extending in the extension of the first shaft through the first leaf spring, in which in operation the second shaft through the first leaf slides, in which the second shaft extends through the second leaf, in operation the second axle slides through the second leaf spring, in which a first end of the second shaft is connected to the first piston, in which at least one third feather is placed between one of the sides turned away from the first side second side of the first leaf spring and one in a fixed position on the second shaft installed first spring washer. The inventor has chosen to the above-mentioned technical measures the to be called a mass deck. The mass deck contributes to the correction deck on the vertical descending side can correct the free movement. Preferably, the applied deposit in the flywheel assembly comprises according to the invention a base plate which is permanently attached to a second end of the second shaft and runs parallel to the second leaf spring, such that the second leaf spring is between the first leaf spring and the bottom plate is located, in which on the second leaf spring towards the On the bottom plate turning side, several second spacer blocks have been installed, which are perpendicular. stand on the second leaf. The inventor has chosen to the above-mentioned technical measures the to call a fender deck. The effect of the fender deck is to prevent the at least one first piston strikes against the first cylinder filler block. The push-up deck contributes to this that the crumple zone does not smash the first cylinder chamber upon impact and thereby the Compressed air escapes and a recoil occurs. Preferably, at least the first spring is designed to empty the entire lower chamber. to press. This has the effect that the range of motion of the attached coupled mass position moves optimally forward and the acceleration due to gravity in the free range of motion accelerates on the downward side of the inventive flywheel assembly. This makes a free second movement possible by removing the additional resistance at the upward side of the flywheel assembly (just like the free movement due to the gravitational pull of the Earth). In an alternative embodiment of the flywheel assembly according to the invention the release device comprises a third leaf spring, which with multiple spacers above the the first cylinder top is installed in such a way that the first cylinder top is located between the first and third leaf springs and in which at least a fourth spring is mounted on the first shaft between one of the first cylinder top side turned-away first side of the third leaf spring and one in a fixed position on the first shaft fitted second spring washer. This version constitutes a (partial) alternative for the first spring with identical technical effects. In this version, the first spring can in be wholly or partially omitted. This form of implementation has the advantage that the fourth spring can be dimensioned stiffer than the first spring, whereby approximately 85% of the primary (first movement) kinetic energy force be reused for the second movement. Preferably, the first spring is entirely omitted in this version, with which the practical implementation of the sales instrument has been greatly simplified. Preferably, a sleeve is fitted between the third leaf and the first. cylinder top, which encloses the fourth spring. The casing shields the fourth spring with this. The casing is preferably airtight, with the third leaf spring being equipped with a air duct from the outside of the third leaf spring to the inside of the casing. This creates an opening to the atmosphere, whereby the fourth spring during inward and outward movement no pressure can build up or release in the jacket. The jacket is preferably cylindrical. In an improved alternative embodiment of the flywheel assembly according to the invention comprises the means of sale of one or more pneumatic second cylinders, each second cylinder comprising a second cylinder chamber, one in the second cylinder chamber placed second piston, in which the second cylinder space is sealed off by a second cylinder bottom and a second cylinder top, in which each of the second pistons is connected to the second axis, such that the second axis lies in the extension of the second cylinder space of each of the second cylinders and in which the pneumatic second cylinders lie in line with one another, and in which: - the bottom of the second cylinder includes a third supply connection for supplying compressed air in a lower chamber of the second cylinder space; - the bottom of the second cylinder includes a third drain connection for draining compressed air from the lower chamber of the second cylinder space; - the top of the second cylinder includes a fourth supply connection for supplying compressed air in the upper chamber of the second cylinder space; - the top of the second cylinder includes a fourth drain connection for draining compressed air to ambient air; and in which the flywheel assembly and the control system are designed in such a way that - when extruding the first cylinder, whereby compressed air is introduced into the first lower chamber brought, and compressed air is also brought into the second lower chamber of every second cylinder via the third supply connection; upon expulsion of every second cylinder, in which compressed air is thus in the second lower chamber compressed air is brought in via a fourth discharge connection from the second upper chamber of every second cylinder is vented to the ambient air; - upon pressing the second cylinder, the compressed air present from the second lower chamber discharge is from every second cylinder space via the third drain connection. The effect of these measures is that the operating pressure of the compressed air is reduced. Due to this lower operating pressure, the one or more compressors for delivering the compressed air used has better efficiency, allowing the same force through the deposition agent can be exercised in relation to the other forms of the marketing instrument with lower energy consumption. This results in 40% extra net liters of compressed air production per time unit, improved stability with minimal pressure loss, cost savings on parts for the production of the flywheel assembly and moreover less noise nuisance. A compressor motor for supplying compressed air for the flywheel assembly according to the invention used typically with every increase in working pressure from 1 bar approximately 8% extra electrical power. By using a second cylinder, where the workload is halved, this results in 40% extra per kilowatt of power. capacity of effective compressed air for the force build-up required to overcome a resistance can be due to the pushing away or pulling back of the masses in the flywheel assembly according to the invention. The measures result in a significant improvement in the pressure loss of the system. For comparison: Other versions of the flywheel assembly: - Operates at 13 bar pressure - Has a pressure loss of approximately 2 bar - This means an efficiency loss of approximately 15% Improved alternative design of the flywheel assembly (for application one) second cylinder): - Operates at 6.5 bar pressure - Has only 0.2 bar pressure loss - This means an efficiency loss of approximately 3% The flow rate (the amount of air flowing per unit of time) is moved more efficiently. doon - Multiple compressed air supply ducts operating simultaneously - Doubling of the piston surface area (2 x 804 cm² = 1608 cm²) - Faster filling of the cylinder chambers (within 1.5 seconds) These improvements ensure a much more stable system with minimal pressure loss, which results in a more efficient operation of the entire installation. The cost savings are achieved through the use of cheaper components. for low-pressure compressed air, including: Pressure regulators . Compressed air couplings . Check valves Valves Sensors Pistons cylinder walls Due to lower compressed air pressure, atmospheric escape / venting results in substantial reduction of noise nuisance for the immediate living environment. Preferably, the flywheel assembly comprises a low-pressure tank and is flywheel assembly designed for storing from the first and / or one or more second cylinders discharged compressed air and the flywheel assembly is further configured to the in to reuse the compressed air stored in the low-pressure tank for expelling the first and / or every second cylinder or the pressing of the first and / or every second cylinder. The reuse of compressed air increases the efficiency of the flywheel assembly. further increased. Preferably, the bottom and top of the cylinder form of successive second cylinders one component or multi-level mounting plate. This increases the height of the sales means further restricted. Preferably, the flywheel assembly is designed to move the out of the upper chamber of the first cylinder compresses air to the inlet of the air compressor. As a result, the used air is returned to the compressor. In addition, the flywheel assembly is also designed for moving the remaining air forced from the lower chamber of the first cylinder to the inlet of the air compressor after the upper chamber of the first cylinder has been filled. Preferably, the flywheel assembly is designed to achieve a orbital speed of each of the masses exceeding 3 m / s. By means of one or more pneumatic second cylinders (50) and the battery deck the flywheel assembly is able to a speed above 3 m / s the coupled mass object by means of a second movement to move to a position of approximately 320 arc degrees within 0.2 seconds, whereby this movement is followed by the blowing out of the upper chamber of the battery deck of corresponding deposition agent. During tests, the surprising effect was discovered that above a speed of 3 m / s the flywheel assembly also functions as a compressor with compressed air derived from air from the upper and lower chambers cooled by expansion of the battery deck. This low-pressure compressed air (nearly atmospheric pressure) is returned to the compressor, which is used for the initial movement. This cold air is colder than the ambient air. Per unit volume, this cold air has more molecules than warmer air. (ambient) air. As a result, the compressor can compress a larger mass of air per stroke, which increases the compressor capacity. The temperature also rises as a result. less during compression, resulting in a higher isentropic yield. As a result, the energy consumption of the compressor decreases at a rotation speed of 3. m / s of each of the masses decreases drastically. In practice, a decrease in the Energy consumption of the applied compressor of 85% measured. Preferably, the barrier is equipped with a sliding system for support. of a correction deck, in which the correction deck is formed by: - the first leaf; - the support sheet; - the multiple spacers. The sliding system contributes to stability and ensures that there is much less Spacers are needed that slide through the second leaf spring. The sliding system is a important part and has the advantage that it withstands the lateral forces of the removes spacers, so that the spacer only has the function for the setting the free movement length. Preferably, the sliding system is mounted on bearings, so that the resistance in the sliding system is reduced. sliding is reduced. Ball bearings are preferably used for this purpose. In For heavier versions, drum bearings are preferred. Preferably, each barrier is hinged at the first end of a bar. attached to the flywheel near the drive shaft, where a second end of the rod is attached to one of the masses. In the flywheel assembly according to the invention, the air compressor is set to a low pressure (< 4.5 bar) and the first cylinder has an enlarged piston surface area compared to the situation where the air compressor is set to a higher pressure. An air The compressor operates more efficiently at a lower pressure because the pressure difference is smaller, whereby less work is required to compress the gas. As a result, less is also created heat, which limits energy loss. Moreover, the mechanical and thermal losses lower, causing the overall efficiency to increase. To let the flywheel assembly functioning at low pressure; compared to high pressure, the first cylinder has a enlarged piston surface area required. If, for example, one initially assumes a air compressor with a pressure of 12 bar and it is desirable to set the air compressor to 6 for bar to function, the piston surface of the first cylinder will have to double (12:6). If it is subsequently desirable to leave the air compressor at 4 bar for it to function, the piston surface area of ​​the first cylinder will have to triple. (12:4). With these adjustments, an efficiency improvement can be achieved at an air pressure of 4 bar. of the air compressor are achieved higher than 50% relative to an air pressure of 12 bar. In a further improved preferred design of the flywheel assembly according to the invention, the lifting device A comprises operable pre-tensioning devices for the pre-tensioning of the second springs and are the controls configured for the operating the prestressing devices depending on the rotation speed of one or the other multiple masses during use of the flywheel assembly. In practice, it has been shown that the required resilience of the second springs at the starting up of the flywheel assembly needed to be slight, whereas when raising the rotationally fast the required resilience of the second springs must be increasingly higher. Due to the with controllable preload devices, the spring force of the second springs can be dynamic controlled during rotation of the masses of the flywheel assembly. Preferably, the preload devices are designed to preload a second spring. by means of axial displacement of the spring relative to the support blade. This allows the the required resilience of the second springs is set by compression of the second spring. In addition, the preloading devices for each second spring to be preloaded comprise a pin, the support blade includes a pass-through hole for each second spring to be pre-tensioned passage of the pin from one side of the support blade facing away from the first spring leaf, is a side of the second spring lying against the support blade, at least partially over the pin applied and rests on a stop part of the pin near a first end of the pin and includes the preloading devices adjustment devices for setting the relative position of the pin relative to the support blade in the axial direction of the second spring. Preferably, the adjustment means comprise one or more operable hydraulic or pneumatic third cylinders, each mounted on a side facing away from the first leaf the support plate are mounted, in which the third cylinder comprises a third cylinder shaft that is coupled to the pin. This allows, by operating the third cylinder on a advantageous way the prestressing of the second way can be realized. In a highly desirable preferred design of the flywheel assembly according to the invention is the pin formed by one end of the third cylinder shaft, and is it stop part of the pin formed by a third spring ring which is fitted near a end of the third cylinder shaft. Due to the integration of the pin into the cylinder shaft, the operation is of the prestressing devices further simplified. The invention will be further explained by means of the following figures, in which: Figure 1 schematically shows the different positions of the parts. of the flywheel assembly; Figure 2 shows an isometric view of the deposition medium in the flywheel assembly. according to Figure 1; Figure 3 shows a cross-section of the seat according to Figure 2 through a imaginary plane passing through two spacers and the first and second axes; Figure 4 shows an isometric view of the deposition medium in the flywheel assembly. according to Figure 2, in which the second pneumatic connection is shown. Figure 5 shows a cross-section of the seat with multiple first cylinders; Figure 6 shows a cross-section of the alternative implementation of the seat cushion; Figure 7 shows an isometric view of the deposition medium in the flywheel assembly. according to Figure 6. Figure 8 shows an isometric view of the improved alternative form of execution of the marketing agent; Figure 9A shows a side view of an alternative arrangement of 4 consecutive second cylinders that can replace the single cylinder of the deposit agent from Figure 8; Figure 9B shows a cross-section of the setup in Figure 9A. Figure 9C shows an isometric view of the setup in Figure 9A and Figure 9B. Figure 10 shows a cross-section near the underside of the deposit A, in which the second springs are provided with preloading devices. Identical venNijzing figures and / or reference letters in the various figures indicate equal parts to. Figure 1 schematically shows the different positions of the parts. of the flywheel assembly L. The reference letters in the figure indicate the following: A. The medium of sale according to the invention. B. The coupled connection position of the discharge device to the flywheel. C. The line of motion of the cylinder axis of the detaching device. D. The indirect point of contact of the agent against the mass. E. The positions of the coupled suspended masses. F. The lever distance length of line. G. The connecting axes of movement technique. H. The center / pivot point. I. The coupled pivot points of the lever motion technique. J. The orbit of the attached movable mass. K. Direction of rotation. L. Flywheel. The applied movement technique is described in the Dutch patent. NL2033561 and its contents are hereby included as a reference. Upon viewing the flywheel assembly L from the top, one can the latitude distances HL of the mass at positions E at approximately 95°, 315° and 215° Observe carefully with respect to the center H. The masses in the flywheel assembly L rotating in an orbit J in the direction of rotation K without the distance of a mass to the center H changes in the process. In the flywheel assembly L, 3 masses are used and it has 6 dominant masses. resistance points. These are located at positions E of the attached coupled masses at approximately 325°, 25°, 95°, 155°, 205°, and 265°. At these positions, a mass will move towards and remain if there is no energy by means of compressed air or compressed air change (by means of a valve command) between lower chamber 17 and upper chamber 18 of the first cylinder is added to the flywheel assembly L. Rotation of the flywheel assembly can take place by moving a few resistance points, which is realized by moving one of the mass positions E in the flywheel assembly L. To use the gravitational pull of the Earth to make the rotation flywheel assembly L must have the vertical length line VL on the downward side with a larger load downwards, and have one longer length than the vertical length line VL at the upward side. The deposition medium A makes this possible through the mass position E to be corrected twice within the rotation range of approximately 325° to 155°, where the vertical length VL line from position E in orbit J changes. In this process, during the corrective movement of each attached coupled mass the external kinetic energy and absorbed kinetic energy with the released force via the Pressure spring of the deflector preserved in the flywheel. Each coupled suspended mass is therefore twice within a complete rotation of the flywheel propagates by means of the depositing medium A, which deposits indirectly via C against the resistance and indirectly pushes away the built-up force via B, the coupled connection position on the flywheel, in the path of least resistance in the direction of rotation of the flywheel assembly L where simultaneously the distance length of the force of the mass moves back and forth between positions A and D. To eliminate a first resistance point, at position E at 320°, the mass moved by means of the cylindrical axis of the depositing device, which moves over length C, whereby the point of resistance of the mass at position 320° towards the in viewed in the direction of rotation, the next resistance point shifts / rotates by 25°. Upon lifting From a second resistance point at position E, at 90°, mass is also displaced, whereby the center of resistance of the mass at the 90° position towards the direction of rotation seen, the next resistance point shifts by 155°. Thanks to the contact displacement between D, the indirect point of deposition against the mass, and B, the coupled connection position to the flywheel L can the force of the mass within be moved a fraction of a second over a large horizontal distance (HL) with the length between these two points. To move mass in a flywheel, the resistance of the upward mass at positions E, 320°, virtually equal to the resistance of the descending mass position E, 90°. This is because the ascending mass positions E, 320° is indirectly pulled against the direction of rotation by the centrifugal force at its resting point. This force will increase during rotation of the flywheel assembly L. Consequently, without the deposition medium A, no compressed air pressure can be applied according to this invention. can be reused, because the compressed air pressure at both positions (320°, 90°) is virtually the same are. The mass that must be corrected on the downward side has its greatest resistance at position E, 90° of the arc. To convert this external kinetic energy with the In order to preserve flywheel L, the resistance on the deposition medium A, which indirectly is coupled to the mass, be higher than the resistance at the indirect discharge point B with which the deposition agent Azit is coupled to the flywheel. The battery cover of the demountable device as described in the characteristic part of the conclusions contribute to the fact that the attached coupled mass provides extra resistance creates. It is a resistance that will increase when the first piston with more compressed air power creates a larger movement. In summary, due to the applied deposit medium in the well-known flywheel assembly the following is not possible, which is in the inventive flywheel assembly with deposit A dissolved: It is not possible to rotate 360° of the arc with 17% external kinetic energy. realize The external energy cannot be conserved, because the force of the mass is not fully propels the total mass of the flywheel in the direction of rotation to the desired position. The compression springs cannot be positioned over the entire vertical length in the desired manner. set. The desired setting of the compression springs can only be selected at 1 movement speed. (counterforce) be applied. The external kinetic energy can be absorbed. but not used with approximately 48%, because the compressed air pressure during the first and second movement be equal. Figure 2 shows an isometric view of the depositing agent A in the flywheel assembly L according to Figure 1. Figure 3 shows a cross-section of the seat A according to Figure 2 through a imaginary plane passing through two spacers 5 and the axes 11-1;11-2. The Reference figures indicate the following components: 1. Mounting eye. 2. bottom plate 3. Threaded end of cylinder shaft. 4.1. First compressed air supply connection from air compressor to lower chamber for first pneumatic connection. 4.2. Second supply connection for external reused kinetic energy (is compressed air) originating from lower chamber) to upper chamber first cylinder for second pneumatic connection 4.3. First atmospheric exhaust connection from the upper or lower chamber of the first cylinder for third pneumatic connection. 4.4. Second discharge connection used external kinetic energy (= used compressed air) originating from the lower chamber) for second pneumatic connection 4.5 Airflow direction. 5. Spacer 7.1 Second Compression Spring. 7.2 Third Compression Spring. 8-1. First distance block. 8-2. Second distance block. 9. First spring ring. 10. Carrying sheet. 11-1. First axis. 11-2. Second axis. 12. First cylinder above cover. 13. As escort shell. 14. Fixing nut. 14-1 Mounting clamp 15-1. First Leaf. 15-2. Second Leaf. 16. First piston. 17. First cylinder lower chamber. 18. First cylinder upper chamber. 19. filler block 20. First cylinder perimeter jacket. 21. First cylinder mounting thread length. 22. First feather. 23. Sealing ring. 24. Sliding belt first piston 25. Sliding sleeve cylinder shaft. 26. First cylinder under cover. 27. Bumper block. 28. Movement distance of the first cylinder. 29. Free movement distance. 30. Total movement distance. 31. Induction loop 32. valve 67. pass-through hole 68. Third spring ring 69. Third cylinder Figure 4 shows an isometric view of the depositing agent A in the flywheel assembly L according to Figure 2, in which the second pneumatic connection is 31 shown. The second pneumatic connection 31 connects the second drain connection 4.4 with the second supply connection 4.2. This connection is to be interrupted remotely through an operable valve 32. The compressed air from the lower chamber 17 flows into the direction 4.5 via the operable valve 32 to the upper chamber 18. The battery cover of sprayer A includes: - the direct pneumatic second connection 31 (shown only in Figure 4) between the lower chamber 17 and the upper chamber 18 of the first cylinder via the second drain connection 4.4 and second supply connection 4.4, which second connection 31 is breakable by means of a remotely controlled first valve 32; - a pneumatic third connection to the ambient air via first drain connection 4.3, which third connection by means of a remotely controllable second valve is breakable, - at least one first spring 22 which is enclosed in the upper chamber 18 of the first cylinder 16 which extends from the top of the first cylinder space to the top of the first cylinder 16. Additionally, the controls on the battery deck are configured for 1) operating the first valve 32, such that the first valve 32 at the position of The corresponding mass of approximately 325 degrees is open and is closed at 90 to 325 degrees; 2) operating the second valve in such a way that the second valve at a position of the corresponding mass of approximately 90 degrees is opened for the transition to atmospheric pressure bringing the upper chamber 18 of the first cylinder and is closed from 110 degrees. At filling the lower chamber 17 therefore opens the second valve to atmosphere. When the stopping the filling of the lower chamber 17 simultaneously closes the second valve to atmosphere. When filling the lower chamber, the valve attached to the first is Supply connection 4.1 open. In the upper chamber, the second valve to atmosphere is located. open, whereby valve 32 in the ring main 31 to the upper chamber is closed. When the upper chamber is filled, valve 32 is open and the second valve is (direction atmosphere) closed. The valve for filling the lower chamber is then closed. The battery deck provides additional resistance upon the first movement via the lower chamber 17 against the first piston 16 direction at the discharge point 3 of the discharge device A, so that the attached coupled mass never operates against the direction of rotation of the flywheel can be pushed away. The battery cover retains the external at the first movement. kinetic energy (compressed air force) during the first movement at approximately 80 to 145° from the bow. The battery deck ensures the extension of the vertical movement upon the first movement. The longitudinal line VL is on the downward slope, which corresponds to an extension of the duration of stay. of the mass at the desired position). The battery deck accelerates the flywheel upon the first movement, because the flywheel is pressed from the position of the mass in the direction of rotation. The battery deck ensures, through the use of filler block 19, that the kinetic energy from the first movement simply via the second pneumatic connection 31 also for the second movement with approximately 65% ​​of the compressed air force together with the pushing force of the conserved kinetic energy via the compression spring 22 can be reused. The battery deck also accelerates the flywheel during the second movement, because the flywheel is pressed in the direction of rotation from the position of the mass. The mass deck of the demountable vehicle A comprises a second axle 11-2 that extends into the extension of the first shaft 11-1 through the first leaf spring 15-1. In operation, the second slides shaft 11-2 through the first leaf spring 15-1. The second shaft 11-2 extends through the second leaf spring 15-2, in which, during operation, the second shaft 11-2 slides through the second leaf spring 15-2. A first end of the second shaft 11-2 is connected to the first piston 16. At least one third spring 7-2 is fitted to the second axis 11-2 between one of the first sides turned-away second side of the first leaf spring 15-1 and one at a fixed position on the second shaft 11-2 fitted first spring washer 9. The mass-deck compression spring 7-2 is tensioned via a fixed connection to the first spring ring 9 on the cylinder shaft 11-2 that the compression spring 7-2 against the upper first cylinder presses leaf spring 15-1. The Mass deck has a different function than the Battery deck. It must contribute to the Correction deck on the vertical descending side having the free can correct the movement again. The attached coupled masses at positions E must be able to move up and down in a curved motion on orbit J. The mass deck and the correction deck ensure that the free movement distance 29 the attached coupled mass via F at its position E is not hindered and can take place around 20°, whereby the force of the mass the battery deck via the First cylinder leaf spring 15-1 presses against the spacer blocks 8-1 and is corrected around the 145° collision without recoil. For this, it is important that the force of the attached coupled mass at position E is equal to the force of the compression springs 7-1 of the Correction deck, where the compression springs 7-1 between the bottom and top First cylinder leaf springs 15-1 and 15-2 are clamped in place. The Spacers 5 slide through the lower First cylinder. leaf spring 15-2 and are fixedly mounted to the upper first cylinder leaf spring 15-1, with which the free movement distance is determined. The Cylinder Shaft 11-1 has an indirect fixed hinge connection with the attached coupled mass at position E. Cylinder shaft 11 has at the position of the first cylinder a fixed connection to the First piston 16. The correction deck of deposit A ​​comprises: - a first leaf spring 15-1, of which a first side is the underside of the first cylinder forms - a second leaf spring 15-2, running parallel to the first leaf spring 15-1, and - multiple spacers 5 fitted between the first leaf spring 15-1 and the second leaf spring 15-2, each perpendicular to both the first leaf spring 15-1 and the second leaf spring 15-2. A first end of the spacers 5 is firmly connected to the first leaf spring 15-1 and the second end of the spacers 5 are sliding through the second leaf spring 15-2. Around each spacer 5 is a second spring 7-1 applied The correction deck ensures that no kickback occurs on the second movement. The mass is sandwiched between two resistors. The cylinder shaft 11-1 and the The resistance force of the correction deck ensures that the force is in the direction of the rotation is pressed. At approximately 325 degrees, approximately 65% ​​of the compressed air force in the upper chamber of the first cylinder be accommodated. This is because the volume of the upper chamber is larger is then the lower chamber of the first cylinder. The resilience of the battery deck and the mass deck compress by means of compressed air force from the first cylinder upper chamber 18 the entire contents from the first cylinder lower chamber 17. Because the force of the mass presses against the correction deck in this process, the kinetic energy is also conserved here in the direction of rotation of the composite flywheel. Because the mass force on the downward side has increased in this process, it presses this force pushes the correction deck completely into the spacer blocks 8-1 with a build-up power from approximately 20 degrees. Because the attached coupled mass is clamped between the first cylinder compressive forces the counterforce of the correction deck means no kickback is possible. The mass deck makes it possible that during the first and second forced movement the correction deck offers resistance differences for the movements on the downward side for the attached coupled mass at the position of approximately 20° with a lower resistance and the position of approximately 145° for a corrective movement. The mass deck offers a higher correction force than the 7-1 compression springs of the correction deck. It Mass deck takes the higher downward correction during the first forced movement force partially removed and helps the push-up springs 7-1 of the correction deck the free movement 29 to correct. The compound flywheel L has one for every mass at positions E. Movement length required with a crumple zone without recoil. This movement length comes established with the selling medium A. It has an indirect connection with the coupled attached masses at the positions on the end of the cylinder shaft (11-1) against the indirect point of attachment to the mass (D) and with the mounting eyes (1) to the frame of the compound flywheel at position (B). The range of motion consists of three parts. The first and second forced movements that are indirectly via the cylinder axis 11-1 achieved and the free movement that takes place between take-off blocks 8-1) and the first leaf spring (15-1). The free motion length is the motion that is performed solely with the force of the coupled mass takes place. Both movements take place on the downward side. The reason for the mutual movements via F with the attached coupled mass is to create imbalance, where the resistance force on the upward vertical side is lower than the descending side. The greater the distances between them, the the more imbalance, like on a seesaw, the smaller the distance from the center and how smaller the horizontal resistance at the center. The free movement is a free extra imbalance position difference with extra force on the downward side of the flywheel assembly L that was created by the gravitational force on the mass. The falling / downward movement of the attached coupled mass at position E takes place at the top. Correction (or repositioning) only takes place at the bottom side on the downward side, where the correction must be realized for the position of 165° of the arc. The correction to this movement will the contact displacement bring about within a fraction of a second at approximately 325° from the arc, because the force of the attached coupled mass position at approximately 170° from the arc on will be corrected in a natural way with an enormous collision (damage and energy) loss), when the position of the force of the mass on B and D become horizontally equal to lie. The bumper deck of the discharge device in the inventive flywheel assembly comprises: - comprises a base plate 2 which is fixedly attached to a second end of the second shaft 11-2 and runs parallel to the second leaf spring 15-2, such that the second leaf spring 15- 2 is situated between the first leaf spring 15-1 and the bottom plate 2, in which on the second leaf spring 15-2 on the side facing the bottom plate 2 multiple second spacer blocks 8-2 are fitted, which are perpendicular to the second leaf spring 15-2. The function of the thrust deck is to ensure that the first piston 16 the does not touch filler block 19. To this end, the height of spacer blocks 8-2 has been configured as follows that this is not possible. Figure 5 shows a cross-section of a deposit A ​​with multiple first cylinders. Deposit medium A can be used in a flywheel assembly in which the masses have a high weight. The deflector A preferably has a first leaf spring 15-1 and one second leaf spring 15-2. The action of the deposition agent A is otherwise the same as the action of the deposit A ​​from the previous figures, but is especially suitable for heavier flywheel assembly. By placing the first cylinders in a row, the free movement length 30 (sum of movement lengths 28 and 29) of the barrier A not greater than the length of the composite cylinder axis of the depositing agent A at equal dimensioning of cylinder axes 11-1 and 11-2. Without the discharge medium in the inventive flywheel assembly L, the following can points are not realized: 1. Conserving external energy during rotation between approximately 75 and 145° degrees of the arc. 2. Capturing and reusing the used external energy (compressed air pressure) with 65% at 325 degrees. 3. The indirect transformation of energy forms by the gravitational pull of the Earth in kinetic energy. The second movement is now only possible with the mass object at position E at approximately 325°. the flywheel assembly L can be realized. In doing so, the captured compressed air is utilized from the lower chamber 17 and the compressive force of the first spring in the upper chamber 18 without using additional external kinetic energy. 5. With the application of the mass deck, the resistance force of the total can the mass present of the flywheel assembly constant over 360 degrees of the arc become resist 6. With the application of the battery deck, the resistance force of its own mass can of the flywheel assembly L and the third resistor applied to the drive shaft constant be withstood over 360 degrees of the arc. Figure 6 shows a cross-section of the alternative implementation of the seat aid A. The additional venNijzings figures indicate the following components: 6. Sliding system 6.1 Notch for sliding system 6.2 Mounting holes for sliding system 40. Third leaf 41. spacer 42. fourth spring 43. second spring ring 44. Coat. 45. Air duct 3-1. Threaded spacer (for tensioning the fourth spring) In this version of the barrier A, the first spring 22 has been completely replaced. by fourth spring 42. Because the space in which the fourth spring 42 is not under pressure set, as is the case with the first spring 22, the fourth spring can optimally be dimensioned. This means that the fourth spring can be stiffer than the first spring, whereby more energy can be stored in the fourth spring. Compared to preservative A, this allows up to approximately 85% of the primary (first movement) kinetic energy force be reused for the second movement. Figure 7 shows an isometric view of the depositing agent A in the flywheel assembly L according to Figure 6, in which the positions of the first feed connection 4.1, second supply connection 4.2, first drain connection 4.3 and second drain connection 4.4 is shown. The position of air duct 45 is also shown in 2O the third leaf spring 40. The air channel 45 ensures that the space in the casing 44 in which the fourth spring 42 moves under atmospheric pressure remains stationary. The sliding system 6 contributes to stability and ensures that much less Spacers are needed that slide through 15-2. By using demarcation agent A, the following points can be achieved become: 1) By applying the combination of the battery deck combined with the first The cylinder can counteract the resistance of the flywheel together with one coupled to the drive shaft. resistance (such as a generator, for example) now with the primary first movement on the the downward side is pressed via position B in the direction of rotation. 2) The compressed air power is maintained. 3) The compressed air power (external energy) can be reused for approximately 85%. 4) Free movement creates the possibility that the Earth's gravity is converted into kinetic energy. The free range of motion can be larger than the forced range of motion with the first cylinder (compressed air). This space (more imbalance) creates the energy by means of attraction. The free movement makes production of kinetic energy possible. The bottom plate 10 and the second leaf spring 15-2 can be identical parts. The advantage of the combination of the assembled cylinder shaft 11, which consists of shaft 11-1 and as 11-2, of the deposit medium A with, for example, a diameter of approximately 20 mm to 120mm that keeps barrier A straight during stable, large ranges of motion. With this does the forced and free movement together exceed 400mm without recoil is. This ensures the movement, whereby the cylinder shaft 11 (A) is stable in one maintains a straight line and the spacers through relatively short sliding sleeves through the second leaf spring 15-2 can slide and not bind. Figure 8 shows an isometric view of an improved alternative deposit A. The marketing agent A is an improvement on the marketing agent A according to Figures 6 and 7. The In this example, deposition device A comprises one pneumatic second cylinder 50, but can can be expanded with multiple second cylinders 50. This is explained in the discussion of Figures 9A, 9B and 9C. Each of the second cylinders 50 comprises: - a second cylinder space; - a second piston 56 placed in the second cylinder space, in which the second cylinder space is closed off by a second cylinder bottom 51;54 and a second cylinder top53;54; Each second piston 56 is coupled to the second shaft 11-2, such that the the second shaft 11-2 lies in line with the second cylinder spaces. As a result, the pneumatic second cylinders aligned with one another. In every second cylinder bottom 51 ;54 of a second cylinder 50 is a third supply connection 58 installed for supplying compressed air into a second lower chamber 63 of the second cylinder space; In every second cylinder bottom 51 ;54 of a second cylinder 50 there is also a third discharge connection installed for discharging compressed air from the second Lower chamber 63 of the second cylinder space. This is not shown in the figure. In addition, every second cylinder top comprises 53;54 of a second cylinder 50 a fourth discharge connection 58 for discharging compressed air from the second upper room 64 to the ambient air. The flywheel assembly and in particular the operating device are in this embodiment designed in such a way that when the first cylinder is pressed out, whereby compressed air is introduced into the first lower chamber, and compressed air is also introduced into the second lower chamber 63 of every second cylinder 50 via the third supply connection 58. Upon extruding every second cylinder 50, in which compressed air is therefore in the second compressed air is supplied via a fourth discharge connection 58 to lower chamber 63. from the second upper chamber 64 of every second cylinder 50 to the ambient air discharged. When the second cylinder 50 is pressed, the available compressed air is also expelled. the second lower chamber 63 of every second cylinder space via the third drain connection 58 discharged. Preferably, the extracted compressed air is stored in a low-pressure tank. The flywheel assembly is then preferably designed to the in the low-pressure tank to reuse stored compressed air for expelling the first and / or every second cylinder 50 or pressing the first and / or every second cylinder 50. The second cylinder top 53;54 of every second cylinder 50 can a fourth supply connection 58 include for supplying compressed air in a second upper chamber 64 of the second cylinder space for pressing in the second cylinder 50. The working pressure of the compressed air is supplied by a compressor system by means of compressed ambient air. By using one second cylinder 50, the The usual working pressure will be halved. So, for example, 12 bar compressed air becomes 2 times 6 bar compressed air. The piston surface with the application of a second cylinder 50 with equal piston surface area as the first cylinder is now doubled, for example from 350 cm2 to 2 times 350 cm² = 700 cm². By using 3 second cylinders, the working pressure becomes reduced from 12 bar to 4 bar. By using 4 second cylinders, the working pressure is reduced from 12 bar to 3 bar. It is therefore of great advantage that by using multiple second cylinders 50 the operating pressure is further reduced while the piston surface of the first and remains constant second pistons 56. By lowering the operating pressure, the one or more produce compressors coupled to the flywheel assembly more liters of air per kW (gross efficiency) with additional amount of liters of compressed air per kW (net efficiency compressor). In a year, during the operation of the flywheel assembly, this extra The amount of compressed air varies between 15.5 million liters and more than 31 million. liters of compressed air. By applying the flywheel assembly with this embodiment of the deposit medium can the flywheel assembly indirectly the with the one or more industrial compressors the extra amount of compressed air with equal electricity consumption in equal convert mechanical pressure and tensile stress per kW because the summed piston surfaces in the first cylinder and in the one or more second cylinders in ratio has been increased. The performance of the flywheel assembly with this embodiment of the deflection medium relative to the flywheel assembly of the flywheel assembly with the for other forms of the liquid product, however, remains equal to the liters used compressed air, because the amount of liters of compressed air to move the resistance is equal remains. The supply velocity of the compressed air of the flywheel assembly with this The implementation form is, however, better. In addition, the major advantage is that due to the lower working pressure the output of compressed air is much higher per kW in the same duration with the same one or more industrial compressors. The application of the flywheel assembly with this embodiment of the sales agent, whereby the workload is reduced, results in an increase of output of compressed air by one or more industrial compressors between approximately 19% and more than 38% per kW per year. As an additional example, 115,775 liters of compressed air are used per pass by 3 depositing agents with pistons of 320 mm diameter. That amounts to 1,447.2 liters per minute at 12.5 rpm and results in an electricity consumption of the compressor of approximately 0.134 kW. In the other versions of the flywheel assembly, the electricity consumption of the compressor 0.242 kW. Figure 9A shows a side view of an alternative arrangement of 4 consecutive second cylinders 50 that can replace the outstanding cylinder 50 of Figure 8. Figure 9B shows a cross-section of the setup in Figure 9A. To keep the setup as compact as possible, the bottom of the second cylinder and second cylinder top of intermediate cylinders 50 formed from a single part that is designated by the inventor as floor construction plate 56. The supply and discharge connections 58 for compressed air have been installed in the multi-level building slab 56. The additional Reference figures indicate the following components: 50. Second cylinder 51. Lower second cylinder bottom 53. Top of the top of the upper second cylinder. 54. Floor plan. 55. Spacer. 65. Coat. 66. Mounting holes 58. Compressed air pass-through holes. 59. Bronze sliding sleeve for displacement seam. 60. Sealing ring. 56. Second piston. 57. Piston sliding seal. 61 Screw thread. 62. Fixing nut. 63. Second lower chamber second cylinder. 64. Second upper chamber second cylinder. The lower second cylinder bottom 51, upper second cylinder top 53 and the level assembly plate 54 are equipped with a sliding sleeve 59 for the second axis 11-2 and a sealing ring 60. As with the floor construction plates 54, the bottom second cylinder bottom 51 and upper second cylinder top 53 equipped with compressed air pass-through holes 58 and mounting holes for the spacers 55. The height distribution of the sheath 65 is interrupted by the floor build-up plates 54, which indirectly the maximum The range of motion for the second pistons 56 determines which second pistons 56 are coupled are on the second axis 11-2. The second cylinder bottom 51, upper second cylinder top 53 and the Floor extension plates 54 are connected to each other by spacers 55. These Spacers 55 are preferably threaded on both sides, with which they can be attached to the bottom of the second cylinder 51, which is also provided of screw thread. On the other side, the spacers 55 are secured to the upper second cylinder top 53 with a mounting nut 62. The compressed air pass-through holes 58 are preferably threaded for direct connection to the compressed air systems. The divided floors, which by the floor build-up plates 54 and casing 65 are formed, are all equipped with a on the second shaft 11-2 coupled piston 56. The divided levels are equipped with a sealing ring 60 and a bronze sliding sleeve 59 for passage of the second shaft 11-2. The movement space of the piston 56 in the jacket 65 creates a lower chamber for each stage 63 and an upper chamber 64, in which the compressed air pressure can come directly against the piston surface work. Figure 9C shows an isometric view of the setup in Figure 9A and Figure 9B. Figure 10 shows a cross-section near the underside of the deposit A, in which the second springs (7-1) are fitted with preloading devices. The preloading devices are formed by the third operable cylinders 69 and the third spring ring 68. The operable cylinders 69 are mounted on one side of the 15-1 facing away from the first spring leaf support sheet 10. For economic reasons, use has been made in Figure 10 of the Cylinder arrangement as described in Figures 9A and 9B, but with two pistons instead of four. The shown parts of the 69 cylinders are therefore identical to the shown parts in Figures 9A and 9B. The number of pistons can be adjusted to the dimensions of the flywheel assembly. The cylinders 69 are pneumatically coupled to the pneumatic provisions of the flywheel assembly. The third cylinder shaft of cylinders 69 is formed by the second shaft 11-2 and protrudes through a pass-through hole 67 in the support plate 10. Near the top of the third cylinder axis is a third spring ring 68 installed. The second spring 7-1 is over the third cylinder shaft applied. As a result, one side of the second spring 7-1 rests on the third spring ring 68 and lies another side of the second spring 7-1 against the first spring leaf 15-1, preferably in a recess in the first leaf spring 15-1. By operating the cylinders 69, the relative position of the third spring ring 68 can be adjusted. be adjusted relative to the support tray 10. By adjusting this position the preload of the second spring 7-1 is determined. Alternatively, hydraulic cylinders can also be used for the compressed air cylinders 69. used, particularly for systems with heavy masses, or a combination of compressed air and hydraulic cylinders. The free range of motion creates controlled range of motion for the force of the mass, without the use of external energy, whereby more than 50% of the Imbalance is realized within the 360 ​​degrees of rotation. The free range of motion in the lifting device A is controlled by the pushing force. (resistance) of the second compression spring 7-1. By means of the adjustable preload on the second compression springs 7-1 the desired operational alternating resistances are realized, for the forces of the attached, coupled, movable mass objects during the absorption (acceleration) and correction (movement) on the downward side of the flywheel assembly L. The free range of motion is located between the support tray 10 and the first leaf 15-1. To make a flywheel assembly L rotate by means of imbalance, it must be done via the coupled connection position B of the deflector to the flywheel L the forces of the attached, coupled moving masses inside the flywheel indirectly successively pushing off above the imaginary horizontal line. The greater part of the The total rotating mass in the compound flywheel system L lies above the imaginary horizontal line. The imaginary horizontal line is indicated by a dotted line that runs from position 270 to 90 arc degrees and crosses the pivot point H of the flywheel. The largest part of the total mass is located during rotation due to imbalance. of the flywheel is therefore not below this imaginary horizontal line and is the realized imbalance with driving force on the downward side not only greater, but the range of motion is also longer. To achieve an optimal imbalance, it is essential to fully utilize the available range of motion. This freedom of movement fulfills three functions: First, it creates controlled freedom of movement without the use of external energy, with which more than 50% of the imbalance is realized within the 360 degrees of rotation which controlled range of motion is greater than the forced room for maneuver. Secondly, it creates fluid movements, because together with the others segments of the demountable material eliminate three collision possibilities on the descending side. These possibilities arise because the attached, coupled, movable mass against the direction of rotation of the compound flywheel L becomes pushed. Thirdly, it corrects with the remaining segments of the drive unit of the composite barrier A the position of the attached, coupled, movable mass E on the downward side in its orbit J, equal to that position which for the an upward side is necessary, whereby the thrust part that is predominant on the The downward side in the direction of rotation K is realized. The need for this upward resistance force with the second compression spring 7-1 During free motion, the rotation of the masses is very small at the start. However, this The upward resistance force with the second compression spring 7-1 must be very strong at rotational speeds increasing to 3 m / s and faster. The second compression springs 7-1 have been installed. between the support leaf 10 and the first spring leaf 15-1. Because the resistance against the second compression spring 7-1 during absorption and correction movements during rotational acceleration of the flywheel must become increasingly stronger, due to the increase in potential energy of the attached coupled movable masses at position E, the support sheet is 10 equipped with the operable preloading devices. The composite flywheel L receives in the Compressed air rotary coupling for this, next to the return compressed air transfer and supply compressed air. with working pressure one-third compressed air throughput for the supply line within the infrastructure with its own pressure regulator. At each individual rpm (speed), for example from 0 to 20 rpm, the desired compressed air force is determined via the computer-controlled pressure regulator under the second compression spring 7-1, and thereby indirectly the desired resistance forces with the cylinders and directly the resistance via length of movement in which the second compression springs are located sandwiched between the third spring ring 68 and the first spring leaf 15-1. Through these measures, the desired operational resistance to the forces can be achieved. of the attached, coupled, movable mass objects during capture (acceleration) and correction (movement) are realized within the range of motion of the free range of motion, both during the start with low resistance and during rotational speeds with high resistance within this free range of motion. In the flywheel assembly according to the invention, operation arises from the state of motion of the mass, with a primary action a motion reaction (mass- inertia) and an initial velocity. The state of motion of a mass object (weight or potential energy of an object) that is indirectly coupled to a deposit is depending on the combined position and speed. It has been shown that: ° Metal objects of varying weight within a length of one meter able to move back and forth almost identically. ° At every increase in speed, the potential energy and the centrifugal force increase on the rotating mass objects and are only usable via the correct imprint and resistance length within the available time. It is important that for a flywheel motor, the correct composition with resistance and pressure forces are composed with the bonding agent technique and the ratio of for example approximately 15%, 20% or 25% external kinetic energy (circulation speed) for the desired goal. The test setup shows that the higher the speed, the lower the external energy consumption is, whereby 100% internal energy yield is achieved. The deposition technique is a unique mechanical resistance and imprinting technique. Research has shown that the flywheel motor with an increase in potential force due to acceleration of mass objects directly via the "Depositors" the compressed air infrastructure positively influenced. The consumption of compressed air (number of liters of air per minute) is proportionally much less as speed increases. In this scenario, the dominant potential action force is from the acceleration of the mass object pushing on the reaction force via the existing resistances, combined with compression springs and the compressive air pressure present inside cylinder chambers via an open connection towards the composite piping structure. In this context, the dominant action force generates on the reaction force pressure differences in a ring main, which in this combination are effectively managed in a Enclosed space against pressure loss in case of overpressure. This built-up overpressure can remain and be used simultaneously elsewhere at a desired position. The composite cylinder set / deck works in combination against resistance build-up. of the underlying spring set / deck of the deposit technology and works at higher circulation speeds like a compressor system. It increases the available compressed air pressure. within a composite pipeline infrastructure. The increase in driving force arises from acceleration at the position from approximately 30 arc degrees at the top on the descending side of the compound flywheel motor. When returning the coupled mass object after the set assumed rotation speed pressure builds up over a length of approximately 50 degrees of rotation, whereby simultaneously the force from acceleration is removed on the central drive shaft. Research shows that during a rotational speed of approximately 3 m / s (distance of movement per second) with the mass object in its orbit, there is an increase is of constant compressed air pressure build-up (absorption per second). This force on the position of approximately 320 arc degrees is achieved with the unique combination of the barrier used sequentially. After the overlying spring set / deck of the deflector technique initiating a rapid movement above the cylinder set / deck within a fraction of approximately 0.2 seconds with the coupled mass object, this movement follows in the cylinder upper chamber with extra compressed air pressure force. The assumed rotational speed (at 3 m / s) of the mass object accelerates additionally by approximately 2 m / s within a virtually horizontal longitudinal distance in approximately 70 degrees of arc in approximately 0.5 seconds at the top of the system, without the assumed rotational speed of the flywheel assembly becomes negative from approximately 3 meters per second influenced by, for example, a collision. Collisions that are removed with the current barrier technique cause by coupled mass objects are: ° First, acceleration against the resistance of the application technique (reducing rotational speed). This resistance is then too high in relation to the absorbing force via the mass object. The mass object is then by the velocity of overtaken the flywheel motor. ° Secondly, after the mass object is in the opposite direction of rotation pushed away (too low resistance). The correction force via the propulsion technique against the mass object pressing past or before the 90-degree position becomes too small or too large. The mass object is then overtaken by the speed of the flywheel motor. ° Thirdly, when the mass object its Length (total distance of movement of the deposition technique) has not traveled in the direction of rotation of the flywheel assembly and not via the second mounting point in the driveshaft of the flywheel assembly has been moved within the correct time. The mass object is then by the speed of the flywheel assembly overtaken. The combination of the first and second spring in the barrier is indispensable for the exceptional push-off for acceleration (fraction of approximately 0.25 seconds) onto the side position of 320 arc degrees of the flywheel assembly in operation according to the invention. In addition, in combination with the weight of the mass object, it increases the resistance. on the cylinder axis, so that the mass object is not against the direction of rotation of the flywheel assembly in operation is pushed away during the correction back to the rotational speed of the flywheel assembly within a time span of approximately 0.5 seconds on the downward side. Alternatively, the first and second springs of the propulsion device can instead of on top of the cylinder set, positioned behind the lever (F), in which the deflector opposes the construction of the composite flywheel. Here, the the force position is on the upward side of the flywheel and now on the downward side side at the top. To achieve the objective, safety and sustainability in the flywheel assembly according to the To guarantee the invention, it is important that the movement technique for the desired the state of motion of the applied mass objects is optimal. To prevent: ° Metal fatigue and wear. ° Ground vibrations. ° Noise nuisance. ° Loss of external kinetic energy. A mass object that is pushed against the direction of rotation on the downward side side, successively creates a collision and thereby takes, apart from the possible damage, the positive thrust kinetic energy out of the system. By means of the medium according to the invention, during the operation of the flywheel assembly: the Earth's gravitational pull converted into thrust energy. In the application of the deposition medium in a flywheel assembly according to the invention three equal coupled movable mass objects are used that only is movable on their orbit in the flywheel assembly. To use a weight to gain dominance over the combined potential resistances by means of a mass object during rotation, the flywheel assembly must operate at a speed according to the invention. assuming a speed of approximately 3 meters per second without the state of motion of the mass- object during the enormous rapid displacement in the direction of this assumed rotational speed does not slow down or hinder the speed. The displace resource is a mechanical, unique composite. movement technique. It is a tool with which, indirectly and in an optimal manner, the centrifugal force the state of motion of the mass object in its direction with deflects force and converts it together with the gravitational pull of the earth and compressed air force in motion. These combined forces indirectly and directly control the State of motion of the mass object with a weight ranging from a few kilos to thousands kilos, by means of the mentioned speed. The main goal is the potential energy of the mass- objects in the free space of motion in the flywheel assembly according to the invention in to incorporate company and expand by means of the earth's gravitational pull with a oven / moisture on all present and connected resistors. The free movement space in the lifting device on the vertical downward side, where no external energy is used, has a longer length than the forced (cylinder shaft) range of motion. It is a calculated interplay of action forces and reaction forces. The rotating speed of the mass objects above 3 meters per seconds and higher completes the application of the depositant and reduces the use of external energy. In this regard, the first spring pack (formed by the first and second spring of the release agent), which is placed on top of the cylinder pack, the gears at the top of the flywheel assembly according to the invention, at the position between approximately 320 to 30 arc degrees, virtually horizontal, strong onset of displacement with a speed of movement in the direction of rotation. In doing so, the potential force increases and becomes supplemented by the gravitational pull of the Earth within the free successive space of motion for the mass object in its orbit, where the mass object via kinetic energy and the force of the deflecting centrifugal force is transferred into the flywheel assembly during the position between approximately 30 to 150 arc degrees on the downward side. The mass object is thereby moved with a fluid motion reduced to the rotational speed of the flywheel assembly via the upward side back to the position of 320 arc degrees. The combination with the first spring package is indispensable for exceptional sales. for acceleration (fraction of approximately 0.25 seconds) top side at position of 320 arc degrees of the flywheel assembly in operation. Additionally, in combination with the weight, it increases of the mass object the resistance on the cylinder axis, so that the mass object does not against the rotation direction of the flywheel assembly in operation is pushed away. During the correction back to the rotational speed of the flywheel assembly according to the invention in company within a time span of approximately 0.5 seconds on the downward side. The barrier agent is therefore a unique composition to withstand heavy action forces in to form functional reaction forces within a short period of time and where over approximately 120 degrees of arc simultaneously the centrifugal force has changed direction, that influence has on the state of motion of the rotating mass objects. During this Changes keep the mentioned functional reaction forces away from the negative influence on the potential energy of the flywheel assembly in operation. The primary sequential acting force for the flywheel assembly according to the invention is supplied in operation by means of kinetic energy (compressed air). The barrier preferably has two composite spring packages (combination first and second spring and separate third spring) and between the two is one cylinder pack combined. The deposition medium that is combined with a mass object has two attachment points, with which the deposit is secured in the flywheel assembly. The The first attachment point is indirectly coupled to the movable suspended mass. object and combined via the first spring package and thus subject to greater coupled resistors. The second mounting point is closer to the center of the flywheel assembly mounted and is the position where the increasing forces (greater than on the first mounting point) on the central drive shaft of the flywheel assembly press down and pushes the range of motion of the barrier against the central drive shaft The flywheel assembly obtains its basic rotation through imbalance with the combined coupled attached mass objects. This is created with approximately 15% constant external compressed air power (primary kinetic energy) derived from the 100% output consumed. Upon the generation of the set desired rotational acceleration from approximately 2 m / s The thrust of the mass objects is replenished and can rise to approximately 85%. by means of the techniques of this sales agent. To dampen the noise of the flywheel assembly in operation in accordance with the invention, all used compressed air is returned to the inlet of the compressors with the advantage that it: ° It dampens the sound. ° The cool return air cools the compressor. ° Minimal amount of pollution and moisture from the atmosphere / environment in the ends up in infrastructure. ° The compressed air supplied at the inlet is equal to the quantity used and the pressure of the return air remains virtually equal to atmospheric pressure. In the cooled return air, the air molecules present are closer together than in the warmer air. ambient air. This contributes to the compressed air efficiency (number of liters of air per minute) of the compressor systems can be as much as 30% higher in a warm environment spaces The outlet makes it revolutionary possible to small household and to realize large industrial engines for the production of, for example, electricity combined with a generator. The primary movement is achieved by means of the cylinder pack and is braked by means of the overhead first spring pack when there speed is created. This is because the enormous impact of the mass force within a time unit of approximately 0.25 seconds slows down the combined resistance and prevents the mass object with the required displacement force against the in a short period of time is pushed away in the direction of rotation. To be able to move a movable propellant (mass) in a controlled manner in a rotating flywheel assembly, implies that controlled: ° that the mass object rotates at least along with the obtained rotation speed of the flywheel assembly in operation and does not decelerate. And that a collision will occur successively. cause, because the state of motion of the mass object is in the wrong direction moves ° that the mass that has accelerated from the position of approximately 320 arc degrees and caused no collisions due to blockage outside the barrier but the kinetic converts energy into a fluid propulsive motion. Free motion as discussed is a theory based on facts: An object with mass (mass object) rotating on its length from the center on its orbit, is influenced by the centrifugal force, whereby it from the pulls the center outwards. At the moment the moving object the mass object slows down, bends the direction of the centrifugal force. The means of pressure slows down the mass over a length of approximately 50 degrees of rotation depending on the potential force. It presses subsequently this incorporated thrust force in the second spring pack and the content of remove the cylinder set via the second mounting point in the driveshaft of the Flywheel assembly in operation. In the time interval between the absorption of the acceleration in the third spring pack and changing the content of the cylinder set (compressing the quantity the centrifugal force changes direction. An object with mass rotating on length from the center, is influenced by the gravitational pull of the Earth. Although the force on the object always remains the same, this force on the horizontal width in the flywheel system not equal, measured from through the vertical line drawn from the center of the flywheel assembly. The further the mass from The further this line is drawn, the greater the force on the connection point of the arm (lever). The greatest force on the lever arm relative to the center is at the position of 90 and 270 degrees. The position of 180 degrees, where the centrifugal and the the Earth's gravitational pull assuming the same direction has no negative here influence because the mass object has already been corrected in speed and in its current The state of motion remains in this position. Because the correction length is between approximately 30 and 80 and takes place between approximately 100 and 150 arc degrees, is within the time duration per rpm 3 times approximately 15 degrees of rotation on the orbit with force Longer present within equal duration. The thrust length of the mass object on the descending side is approximately 120 degrees of rotation and the vertical distance is longer than on the upward side. In short, it comes down to the fact that due to the enormous speed (> 5 m / s) where the acceleration of the mass object acceleration is absorbed there: - when deflected, an additional force arises via the mass object through the apparent centrifugal force. - twice an additional force absorption occurs on the central drive shaft in a smooth movement, because the third spring pack / set absorbs the movement and pushes it away from the position of approximately 35 and subsequent during correction with primary movement at 90 degrees of arc. This overpressure on the third spring is increased once by the acceleration of the mass created and once during correction with resistance build-up with the first spring. A compressor is inherently an inefficient machine. Typically, with heavy Compressors convert 90 to 95% of the energy used into heat, and only 5 to 10% in high-pressure compressed air. However, the efficiency of a compressor increases if the compressor is set to low-pressure compressed air (for example, approximately 4 bar). The increase in efficiency at a lower compressed air outlet pressure can increase to up to 60%. The The flywheel assembly according to the invention is therefore designed to function with a compressor that generates low-pressure compressed air of, for example, approximately 4 bar. The The cylinders used are dimensioned for this, which means that the piston surface is enlarged. In the flywheel assembly according to the invention, virtually 100% of the by The compressor generated air returned to the compressor inlet. Because the returned air, which has also been cooled by expansion, is economically further immediately increases the efficiency of the compressor by an additional 30%. Increasing the efficiency of the compressor through the above-mentioned measures mean that the compressor delivers more liters of air per unit of time and can produce with equal energy consumption.

Claims

1. Flywheel assembly (L), which is driveable by means of compressed air combined with gravitational pull of the earth, comprising a flywheel with a drive shaft, which is mounted at the center of the flywheel; a support device in which the flywheel is mounted vertically; an odd number of at least 1 articulating mass, preferably 3 masses, each are mounted by means of a rod at a distance from the drive shaft and radially evenly distributed are about the flywheel, in which a first end of the rod is hinged to the flywheel near the drive shaft and a second end of the rod is attached to the mass; in which near each bar a pneumatically operated barrier (A) comprising at least one pneumatic first cylinder is installed, comprising a first cylinder space, a first piston placed in the first cylinder space (16) and an on the first piston (16) coupled first cylinder shaft (11-1 ), which first cylinder shaft (11-1) lies in the extension of the first cylinder space, in which the first cylinder space is closed by a first bottom cylinder and a first top cylinder, which is formed by a first cylinder top cover (12), in which each outlet (A) has an indirect connection with the coupled attached mass (D) has at a position on the end of the cylinder shaft (11-1) and by means of screw thread (3) against an indirect point of contact with the mass and on a coupled position (B) is attached to the flywheel, in which the outlet (A) is designed to create an imbalance in operation in the flywheel, such that the residence time of a mass on the downward side, between 0 and 180 degrees, is longer than the residence time of a mass on the ascending side, between 180 and 359 degrees, in which the flywheel assembly comprises a control device for operating the outlets (A) in which compressed air is supplied under the pneumatic first connection first piston (16) is introduced, into which the compressed air comes from a air compressor; in which the control device is also configured for: - creating an initial movement via a lower chamber (17) of the first cylinder, in which at least one first piston (16) of a deposit (A) is expressed as a corresponding mass is located between approximately 70 arc degrees and 145 degrees of arc, in particular at 110 degrees of arc; - creating a second movement, in which at least one first piston (16) a deposition agent (A) is pressed in via an upper chamber (18) of the first cylinder if a corresponding mass is located between approximately 300 and 10 arc degrees, with the characteristic that the selling medium (A): - a direct pneumatic second connection (31) includes between the lower chamber (17) and an upper chamber (18) of the first cylinder via a second drain connection (4.4) and a second supply connection (4.4), which second connection (31) by means of a remote-operated first valve (32) is breakable; - includes a pneumatic third connection to the ambient air by means of a first drain connection (4.3), which third connection by means of a remote operable second valve is breakable, and the controls are configured for 1) operating the first valve (32), such that the first valve (32) only is opened during the second movement; 2) operating the second valve in such a way that the second valve only during the First movement is opened.

2. Flywheel assembly according to claim 1, in which the upper chamber (18) of the first cylinder includes at least one first spring (22) which extends from a top side from the first cylinder space to the top of the first piston (16); 3. Flywheel assembly according to claim 2, in which the upper chamber (18) a filler block (19) includes that extends from the top of the first cylinder space towards the top of the first piston (16), such that the total available for compressed air maximum volume in the upper chamber (18) approximately 1.3x the maximum volume of the lower room (17) amounts to.

4. Flywheel assembly according to one of the previous claims, in which the deposit medium (A) a first leaf spring (15-1) includes, which forms the bottom of the first cylinder, in which the thrust device (A) includes a second leaf spring (15-2), which runs parallel to the first leaf (15-1 ), several spacers (5) have been placed between the first leaf spring (15-1) and the second leaf spring (15-2), each of which is perpendicular to both the first leaf spring (15-1) and the second leaf (15-2), in which a first end of the spacers (5) is attached to the first spring leaf (15-1) and the second end of the spacers (5) are adjustable by the second leaf (15-2), in which a second spring (7-1) is fitted around each spacer (5).

5. Flywheel assembly within the meaning of claim 4, in which one or more first Spacer blocks (8-1) are placed between the first leaf spring (15-1) and the second leaf spring (15-2) running parallel to the spacers (5) in which a first side the first spacer blocks (8-1) is firmly connected to the second leaf spring (15-2).

6. Flywheel assembly according to claim 4 or 5, comprising a second shaft (11-2) which extends in line with the first shaft (11-1) through the first leaf spring (15-1 ), in which in operation the second shaft (11-2) slides through the first leaf spring (15-1), in which the second shaft (11-2) extends through the second leaf spring (15-2), in which in the second shaft (11-2) slides through the second leaf spring (15-2), in which a first end of the second shaft (11-2) is connected to the first piston (16), in which at least one third spring (7-2) is fitted to the second shaft (11-2) between one second side of the first leaf facing away from the first side (15-1) and a the first spring washer (9) fitted in a fixed position on the second shaft (11-2).

7. Flywheel assembly according to one of the previous claims, in which the deposit medium (A) a base plate 2 comprises, which is fixedly attached to a second end of the second shaft (11-2) and runs parallel to the second leaf spring (15-2), such that the second spring leaf (15-2) is located between the first spring leaf (15-1) and the bottom plate (2), in which on the second leaf spring (15-2) on the side facing the bottom plate (2) several second spacer blocks (8-2) have been installed, which are perpendicular to the second leaf (15-2).

8. Flywheel assembly according to one of the previous claims 2-7, in which the at least the first spring (22) is designed to press the entire lower chamber 17 into a void.

9. Flywheel assembly according to one of the previous claims, in which the deposit medium (A) a third leaf spring (40) includes, which with multiple spacers (41) above the first cylinder top (12) is fitted in such a way that the first cylinder top (12) is located between the first leaf spring (15-1) and the third leaf spring (40) and in which at least one fourth spring (42) is fitted to the first shaft (11-1) between one of the first cylinder top turned away first side of the third leaf spring (40) and a a second spring washer (43) fitted in a fixed position on the first shaft (11-1).

10. Flywheel assembly according to claim 9, in which between the third leaf spring (40) and the first cylinder top (12) a casing (44) is fitted, which the fourth spring (42) includes.

11. Flywheel assembly according to claim 10, in which the casing (44) is airtight and the third leaf spring (40) is equipped with an air duct (45) from the outside of the third leaf (40) to the inside of the casing.

12. Flywheel assembly within the meaning of claim 9, 10 or 11, in which the deposition medium (A) one or includes multiple pneumatic second cylinders (50), each second cylinder (50) comprising a second cylinder space, a placed in the second cylinder space second piston (56), in which the second cylinder space is closed off by a second cylinder bottom (51;54) and a second cylinder top (53;54), in which each of the second piston (56) is coupled to the second shaft (11-2), such that the second shaft (11-2) lies in line with the second cylinder space of each of the second cylinders (50) and in which the pneumatic second cylinders (50) extended into one another lie, and in which: - the second cylinder bottom (51;54) includes a third supply connection (58) for the supplying compressed air to a second lower chamber (63) of the second cylinder room; - the second cylinder bottom (51;54) includes a third drain connection (58) for the discharge of compressed air from the second lower chamber (63) of the second cylinder room; - the second cylinder top (53;54) includes a fourth supply connection (58) for supplying compressed air to the second upper chamber (64) of the second cylinder space; - the second cylinder top (53;54) includes a fourth drain connection (58) for the discharge compressed air from the second upper chamber (64) to the ambient air; and in which the flywheel assembly and the control system are designed in such a way that - upon extruding the first cylinder, whereby compressed air enters the first lower chamber is introduced, and compressed air is also introduced into the second lower chamber (63) of each second cylinder (50) via the third supply connection (58); when expelling every second cylinder (50), in which compressed air in the second compressed air from the lower chamber (63) is brought in via a fourth discharge connection (58) from the second upper chamber (64) from every second cylinder (50) to the ambient air is disposed of; - when pressing the second cylinder (50) the compressed air present from the first lower chamber (63) of every second cylinder space via the third drain connection (58) is being disposed of.

13. Flywheel assembly according to claim 12, in which the flywheel assembly has a low includes pressure tank and the flywheel assembly is designed for storing from the first and / or one or more second cylinders (50) discharged compressed air and the The flywheel assembly is further configured to the compressed air stored in the low-pressure tank to be reused for pressing out the first and / or every second cylinder (50) or by pressing the first and / or every second cylinder (50).

14. Flywheel assembly within the meaning of claim 12 or 13, in which the lower end of the cylinder and cylinder top of successive second cylinders (50) one part or level form a mounting plate.

15. Flywheel assembly according to one of the previous claims, in which the flywheel assembly is designed for moving the printed from the upper chamber of the first cylinder air to the inlet of the air compressor.

16. Flywheel assembly according to one of the previous claims, in which the flywheel assembly is equipped for moving the remaining ones from the lower chamber of the first cylinder compressed air to the inlet of the air compressor after first the The upper chamber of the first cylinder is filled.

17. Flywheel assembly according to one of the previous claims, in which the flywheel assembly is designed to achieve a rotational speed of each of the masses that is higher than 3 m / s.

18. Flywheel assembly according to one of claims 4-17, in which the discharge device is provided of a sliding system (6) for optimal alignment of a correction deck, in which the correction deck is formed by: - the first leaf (15-1 ); - the support sheet (10); - the multiple spacers (5).

19. Flywheel assembly according to claim 18, in which the sliding system 6 is bearing-mounted.

20. Flywheel assembly according to one of the previous claims, in which the air compressor on a low pressure (< 4.5 bar) is set and the first cylinder has an enlarged piston surface area has.

21. Flywheel assembly according to one of claims 4-20, in which the deposition medium A operable preloading devices include for preloading the second springs (7-1) and the controls are configured for operating the prestressing devices depending on the rotational speed of one or more masses during use of the flywheel assembly.

22. Flywheel assembly within the meaning of claim 21, in which the preloading devices are arranged to to pre-tension a second spring (7-1) by axial displacement of the spring (7-1) at relative to the support sheet (10).

23. Flywheel assembly according to claim 22, in which the preloading devices for each to tension second spring (7-1) encloses a pin, and the support plate (10) at each second spring to be pre-tensioned (7-1) a pass-through hole (67) includes for passage of the pin from one of the first spring leaf (15-1) turned away side of the support sheet (10), a side of the second spring (7-1) lying against the support sheet (10) at least in part is applied over the pin and rests on a stop part of the pin near a first end of the pen and The preloading devices include adjustment devices for setting the relative position. of the pin relative to the support blade (10) in the axial direction of the second spring (7- 1).

24. Flywheel assembly within the meaning of claim 23, in which the adjustment means one or more comprise operable hydraulic or pneumatic third cylinders, each on one of the first leaf spring (15-1) facing side of the support leaf (10) are fitted, in which the third cylinder comprises a third cylinder shaft that is coupled to the pin.

25. Flywheel assembly within the meaning of claim 24, in which the pin is formed by an end of the third cylinder axis, and the stop part of the pin is formed by a third spring washer (68) fitted near one end of the third cylinder shaft.