GENERATION

TECHNICAL FIELD

[001] The present disclosure relates, in general, to engines and more specifically, relates to a non-combustion magnetor engine for electricity generation.

BACKGROUND

[002] Global emissions will need to halve in the next 10 years to keep the world on track to limit earth temperature rise to 1.5C, which is a primary goal of the Paris Agreement. Existing statistics reports shows that global emissions have surpassed 30 gigatons and approximately 27% are emitted from electricity generation through the combustion of fossil fuels like coal, oil, and natural gas to generate the electricity and 28% by fossil fuel-based vehicles, 22% by industries using fossil fuel-based utilities. This results in the issues like carbon dioxide, global warming, greenhouse gas emission, nitrogen and sulphur oxides, environmental impacts, health impacts, air pollution, sound pollution and the likes.

[003] Existing transportation system uses fossil fuel combustion engine and the environmental impact of the transportation system is significant. Since vehicles burn most of the world's fossil fuel, which emits the by-product as C02, nitrous oxides, smoke, heat from millions of engines thereby contributes to environmental temperature rise, sound pollution from millions of engines in operation and particulates and is a significant contributor to global warming through emission of greenhouse gases.

[004] Similarly, the generation of electricity is the largest source of C02 emissions and within the next few years, electricity demand may rise exponentially due to temperature rise, transportation sector growth, pollution growth, industrial sector growth and the likes. Transmission and distribution of electricity would become another environmental disaster and financial disaster to governments around the globe. Mining and chemicals used in battery, waste battery disposal and recycling are a major concern if we are to depend on batteries for the transportation system and household current storage system. However, electricity without emission, an engine without smoke is the solution to overcome the limitations and problems of the existing system. [005] Therefore, there is a need in the art to provide a machine that functions by the power of magnetic repulsion force in combination with mechanical components to generate clean, smart and eco-friendly electricity at an affordable cost. The machine addresses the world’s other most critical problem of electricity demand and distribution. Further, the machine can aid in decentralized electricity generation and distribution to provide easy access to electricity to millions of people to whom electricity is still unaffordable or where providing electricity has not been feasible and a distant dream in many poor countries.

OBJECTS OF THE PRESENT DISCLOSURE

[006] An object of the present disclosure relates, in general, to engines and more specifically, relates to a non-combustion magnetor engine for electricity generation.

[007] Another object of the present disclosure provides an apparatus that enable the transportation system to have smokeless, emission less vehicles and to produce clean, safe, eco-friendly, smart electricity generation without fuel-burning or any type of additional external source of power to produce electricity.

[008] Another object of the present disclosure provides an apparatus that provides decentralized electricity generation and distribution to provide easy access of electricity to millions of people to whom electricity is still unaffordable and a distant dream in many poor countries and to empower and enable the users to meet their own energy demands and provide uninterrupted power supply that can be used always and during the time of natural disasters.

[009] Another object of the present disclosure provides an apparatus that reduces the acquisition of farmlands, wildlife lands, fertile lands for building transmission lines, distribution power stations, power plants, wind farms, solar power farms and the likes.

[0010] Another object of the present disclosure increases the lifting force while utilizing lower input force to operate the mechanism. The torque and force required to operate the machine are reduced based on the size of the levers to operate the mechanism, thereby reduces the size of the motor required to operate the mechanism, consequently time and power required to operate the mechanism is reduced.

[0011] Another object of the present disclosure provides magnets that slide on linear rails using linear bearing base assembly from bottom to top or in any other sliding angles that reduces the force required to bring the repelling magnets to near-contact position. [0012] Another object of the present disclosure provides lock and release mechanism that is used to lock and/or retain the like pole magnets in near-contact position and/or release the magnets in controlled operation to control force and torque building of the magnetic repulsion force within the set of magnetor assemblies to perform the intended action.

[0013] Another object of the present disclosure provides decoupler mechanism for transferring rotational torque between the drive shaft of crankshaft and the driven shaft of the generator assembly, this mechanism enables the shaft of the generator assembly to rotate faster and continue rotating with the accumulated angular moment force of flywheel even when the shaft of the crankshaft is not rotating or in idle condition.

[0014] Another object of the present disclosure produces expected amps, frequency and power at low cost, where the input energy required to rotate the shaft of the electricity generator is less than the total energy produced in each RPM.

[0015] Yet another object of the present disclosure provides an apparatus that has light weight mechanisms, low maintenance, aids in the longevity of mechanical components, reliable power output, and simple design.

SUMMARY

[0016] The present disclosure relates, in general, to engines and more specifically, relates to a non-combustion magnetor engine for electricity generation. The present disclosure does not require fossil fuel, chemicals, gases to function. The engine that does not burn any fuel and/or not emit any kind of toxic substances, the engine that does not depend on natural resources like wind, water, sun and/or any kind of fossil fuel to function. A machine that can be used to generate eco-friendly electricity at an affordable cost. The machine that can aid in decentralized electricity generation and distribution is disclosed in the present disclosure.

[0017] The engine that functions by the power of magnetic repulsion force in combination with mechanical advantages of levers, lock and release mechanism, gear motor, counterweight system, decoupler mechanism, flywheel mechanism and the likes. The force and/or torque produced by the magnetic repulsion force is used to achieve various mechanical motions and/or the achieved mechanical motion is used to rotate the shaft of the electricity generator to generate electricity. By employing mechanical systems such as lever mechanism, counterweight system, gear mechanics and flywheel mechanism, the output force is amplified in contrast to the utilized input force.

[0018] The present disclosure provides an apparatus that transforms the inherent re usable potential energy of permanent magnets, preferably magnetic repulsion force is transformed into kinetic energy, the transformed kinetic energy having speed, thrust and/or force is transformed into mechanical energy. The inherent potential energy of magnets is compressed by means of sliding two like poles of the magnets in near contact position, which produces greater potential energy, further the magnetic repulsion force in this mechanism is augmented by holding the repulsive pole magnets in near contact position to a desirable movement of time. Further, when one of the engaged like pole magnet is released in control direction, the release of compressed magnetic repulsion force is converted into potential energy and the movement of the mass on which the potential energy is acting on produces the kinetic energy. The sum of the produced potential energy and the kinetic energy is transformed into mechanical energy. The amplification of produced mechanical energy is achieved by implementing double acting lever mechanism, prime mover mechanism, counter weight system, decoupler mechanism and flywheel mechanism, thus output force is amplified in contrast to the utilized input force by means of the mechanical efficiencies. The mechanism is used to the rotate shaft of the electricity generator to generate clean electricity.

[0019] In an aspect, the present disclosure provides apparatus for generation of electricity, the apparatus includes a doubly acting lever assembly comprising a primary lever beam coupled to a secondary lever beam by an extended lever beam, wherein, on receipt of an input force, motion of an effort arm of the primary lever beam creates reciprocating motion on an effort arm of the secondary lever beam. A vertical lift assembly comprising one or more magnets secured to a first magnetor assembly and a second magnetor assembly respectively, wherein the first magnetor assembly and the second magnetor assembly, upon operation of the lever assembly, configured to slide in an upward direction and/or downward direction along one or more parallel rails. At least two prime mover assemblies comprising one or more magnets secured to a first magnetor assembly and a second magnetor assembly respectively, wherein the first magnetor assembly and the second magnetor assembly operable to move in a forward and/or backward direction horizontally along one or more parallel rails. At least two lock release arms of corresponding prime mover assemblies coupled to corresponding connection apertures of the lift assembly and operatable relative to the movements of corresponding magnetor assemblies. A decoupler configured in a generator assembly of the apparatus to transfer rotational motion of a crankshaft assembly to a generator, the crankshaft assembly interlinked with the corresponding prime mover assemblies.

[0020] According to an embodiment, one or more sensors configured in the lift assembly and in at least two prime mover assemblies, the one or more sensors configured to generate a set of input signals pertaining to motion attributes of said at least two prime mover assemblies and the lift assembly. A motor configured in a drive unit of the apparatus, the motor coupled to the lift assembly through the lever assembly. A controller coupled to the one or more sensors and the motor, the controller configured to operate, on receipt of the set of input signals from the one or more sensors, the motor to activate the lever assembly so as to enable corresponding magnetor assemblies to perform reciprocating motion in conjunction with the lever assembly, wherein the upward motion of the first magnetor of lift assembly and forward motion of the first magnetor of prime mover assembly enables same polarity magnets to face one another to generate a repulsion force, the repulsion force is augmented by engaging the same polarity magnets at a designated position and wherein, upon releasing the first magnetor assembly from the engaged state, the generated repulsion force enables the first magnetor assembly to move backward with torque such that the second magnetor assembly is moved forward based on the reciprocal motion of a crankshaft assembly interlinked with the corresponding prime mover assemblies, the forward and backward motion of the prime move assemblies generates rotational motion in the crankshaft assembly that is transferred to the generator through the decoupler to generate power, the generated output power is amplified in contrast to the input power utilized.

[0021] Various objects, features, aspects, and advantages of the inventive subject matter will become more apparent from the following detailed description of preferred embodiments, along with the accompanying drawing figures in which like numerals represent like components.

BRIEF DESCRIPTION OF THE DRAWINGS

[0022] The following drawings form part of the present specification and are included to further illustrate aspects of the present disclosure. The disclosure may be better understood by reference to the drawings in combination with the detailed description of the specific embodiments presented herein. [0023] FIG. 1A illustrates an exemplary view of double acting lever mechanism, in accordance with an embodiment of the present disclosure.

[0024] FIG. IB illustrates an exemplary up stroke action of double acting lever mechanism, in accordance with an embodiment of the present disclosure. [0025] FIG. 1C illustrates an exemplary down stroke action of double acting lever mechanism, in accordance.

[0026] FIG. 2A illustrates an exemplary front view of lift assembly, in accordance with an embodiment of the present disclosure.

[0027] FIG. 2B illustrates an exemplary side view of lift assembly, in accordance with an embodiment of the present disclosure.

[0028] FIG. 2C illustrates an exemplary top view of lift assembly configured with linear bearings, in accordance with an embodiment of the present disclosure.

[0029] FIG. 2D illustrates an exemplary back view of lift assembly, in accordance with an embodiment of the present disclosure. [0030] FIGs. 3A to 3C illustrate exemplary side view and back view of drive unit, in accordance with an embodiment of the present disclosure.

[0031] FIGs. 4A-4B illustrate exemplary view of double acting lever assembly coupled with the drive unit, in accordance with an embodiment of the present disclosure.

[0032] FIG. 5A illustrates an exemplary back view of upstroke movement of double acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure.

[0033] FIG. 5B illustrates down stroke movement of double acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure.

[0034] FIGs. 5C to 5D illustrate exemplary front view of double acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure.

[0035] FIGs. 6A and 6B illustrate exemplary front and back view of prime mover assembly, in accordance with an embodiment of the present disclosure.

[0036] FIG. 6C illustrates an exemplary side view of prime mover assembly, in accordance with an embodiment of the present disclosure. [0037] FIGs. 7A to 7D illustrate exemplary view of lock and release mechanism, in accordance with an embodiment of the present disclosure.

[0038] FIG. 8A illustrates an exemplary view of crank assembly, in accordance with an embodiment of the present disclosure. [0039] FIG. 8B illustrates position of crank rods in accordance with an embodiment of the present disclosure.

[0040] FIG. 8C illustrates a top view of crank assembly coupled with prime mover assembly, in accordance with an embodiment of the present disclosure.

[0041] FIGs. 9A to 9C illustrate exploded exemplary view of non-combustion magnetor engine, in accordance with an embodiment of the present disclosure.

[0042] FIG. 10A illustrates an exemplary view of generator assembly, in accordance with an embodiment of the present disclosure.

[0043] FIG. 10B illustrates coupling of crank assembly with the generator assembly, in accordance with an embodiment of the present disclosure. [0044] FIG. IOC illustrates an exemplary view of decoupled mechanism, in accordance with an embodiment of the present disclosure.

[0045] FIGs. 11A to 11B illustrate exemplary view of non-combustion magnetor engine, in accordance with an embodiment of the present disclosure.

[0046] FIG 12 illustrates an exemplary circuit connection of motor control and sensor system, in accordance with an embodiment of the present disclosure.

DETAILED DESCRIPTION

[0047] The following is a detailed description of embodiments of the disclosure depicted in the accompanying drawings. The embodiments are in such detail as to clearly communicate the disclosure. If the specification states a component or feature “may”, “can”, “could”, or “might” be included or have a characteristic, that particular component or feature is not required to be included or have the characteristic.

[0048] As used in the description herein and throughout the claims that follow, the meaning of “a,” “an,” and “the” includes plural reference unless the context clearly dictates otherwise. Also, as used in the description herein, the meaning of “in” includes “in” and “on” unless the context clearly dictates otherwise.

[0049] In describing the invention, it will be understoood that a number of techniques and steps are disclosed, each of these has individual benefit and each can also be used in conjuction with one or more, or in some cases all, of the other disclosed techniques. Accordingly; for the sake of clarity, this description will refrain from repeating every possible combination of the individual steps in an unnecessary fashion. Nevertheless, the specification and claims should be read with the understanding that such combinations are entirely within the scope of the invention and the claims.

[0050] In the following description, for the purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be evident, however, to one in the skilled in the art that the present invention may be practiced without these specific details. Some embodiments are illustrated by way of example and not limitation in the views of the accompanying drawings. The present disclosure is to be considered as an exemplificiation of the invention, and is not intended to limit the invention to the specific embodiments illustrated by the figures or the description given below.

[0051] The present disclosure relates, in general, to engines and more specifically, relates to a non-combustion magnetor engine for electricity generation. The present disclosure does not require fossil fuel, chemicals, gases to function. The engine that does not burn any fuel and/or not emit any kind of toxic substances, the engine that does not depend on natural resources like wind, water, sun and/or any kind of fossil fuel to function. A machine that can be used to generate eco-friendly electricity at an affordable cost. The machine that can aid in decentralized electricity generation and distribution is disclosed in the present disclosure.

[0052] As the law of conservation of energy states that energy is transformed from one form of energy to another form of energy, mechanism disclosed herein transforms the inherent potential energy of permanent magnets, preferably magnetic repulsion force is transformed into kinetic energy. The transformed kinetic energy having speed, thrust and/or force which acts in conjunction with the intended object and its mass to produce mechanical energy. The amplification of produced mechanical energy is achieved by implementing lever mechanism, counter weight system, gear system and flywheel mechanism. Thus, the output force is amplified in contrast to the utilized input force by means of said mechanical efficiencies.

[0053] The inherent potential energy of magnets is compressed by means of bringing at least two like poles of the magnets in near contact position which produces greater potential energy, further the magnetic repulsion force in this mechanism is augmented by holding the repulsive pole magnets in near contact position to a desirable movement of time, further, when one of the engaged like pole magnet is released in control direction, the release of compressed magnetic repulsion force is converted into potential energy and the movement of the mass on which the potential energy is acting on produces the kinetic energy. The sum of the produced potential energy and the kinetic energy thus transformed into mechanical energy, thus the overall mechanical energy produced is the sum of inherent potential energy of engaged magnets, potential energy of the compressed repulsive force of the magnets, whereas the repulsive force of the magnets depends on the distance between the two engaged like pole magnets, mass of the object on which the intended potential energy is acting on, the efficiency of converting the kinetic energy in motion into mechanical energy.

[0054] The engine that functions by the power of magnetic repulsion force and in combination with mechanical advantages of levers, lock and release mechanism, gear motor, counterweight system, decoupler mechanism, flywheel mechanism and the likes. The force and/or torque produced by the magnetic repulsion force is used to achieve various mechanical motions and/or the achieved mechanical motion is used to rotate the shaft of the electricity generator to generate electricity. By employing mechanical systems such as lever mechanism, counterweight system, gear mechanics and flywheel mechanism, the output force is amplified in contrast to the utilized input force. The present disclosure can be described in enabling detail in the following examples, which may represent more than one embodiment of the present disclosure.

[0055] FIG. 1A illustrates an exemplary view of double acting lever mechanism, in accordance with an embodiment of the present disclosure.

[0056] Referring to FIG. 1A, non-combustion magnetor engine 100 (also referred to as apparatus 100, hcrcinjcan be configured to generate electricity and can be operated by the power of magnetic repulsion force in combination with mechanical advantages of double acting lever mechanism 102, lift assembly 200, drive unit 300, at least two prime mover assemblies (400-1, 400-2) (also referred to as prime mover assemblies, herein), crankshaft assembly 800 and generator assembly 900 (as illustrated in FIG. 11A and FIG. 11B respectively). The force and/or torque produced by the magnetic repulsion force used to achieve various mechanical motions and/or the achieved mechanical motion is used to rotate the shaft of the generator to generate electricity, wherein the generated output power is greater than the applied input power. The present disclosure can be employed in a wide range of applications such as vehicles/transportation sector, industrial sector, household appliances and the likes. Significant contribution can be made to educational field and health care system where there is disruption due to electricity shortage.

[0057] In an exemplary embodiment, double-acting lever mechanism 102(also interchangeably referred to as lever assembly 102, herein) can include a primary lever beam 104 and a secondary lever beam 106. The primary lever beam 104 can include an effort arm 108 at a first end of the primary lever beam 104 and a load arm 110 at a second end of primary lever beam 104, where the load arm 110 is affixed with bearing 112 at a top portion. The effort arm 108 can include a shaft hole and studded with flange bearing on both sides of the effort arm 108. A crank arm 114having a first end and a second end 116, where the second end 116 of the crank arm 114 pivotally coupled to the effort arm 108 using a connecting rod. The primary lever beam 104 is pivotally coupled to a first fulcrum point 118 and pivotally coupled to an extended lever beam 120.

[0058] The extended lever beam 120 having a curved channel is pivotally connected to an effort arm 122 of the secondary lever beam 106 using a connecting rod at a first end of the secondary lever beam 106 and a load arm 124 at a second end studded with bearing 126 on top of the second end. The secondary lever beam lever 106 is pivotally fixed at a second fulcrum point 128. The lever mechanism 102 configured to increase the lifting force while utilizing lower input force to perform the intended action.

[0059] The double-acting lever mechanism 102 can operate in unison means any action/input force performed on the effort arm 108 of the primary lever beam 104 creates retro action on the effort arm 122 of the secondary lever beam 106. Thus, providing the advantage of lower input force, efficient time utilization and minimizes mechanical components required to operate, by implementing the mechanisms, where the output force is amplified in contrast to the utilized input force by means of the mechanical efficiencies.

[0060] FIG. IB illustrates an exemplary upstroke action of double-acting lever mechanism, in accordance with an embodiment of the present disclosure. The lever mechanism 102 increases the lifting force while utilizing lower input force to perform the above disclosed mechanism.

[0061] FIG. 1C illustrates an exemplary down stroke action of double-acting lever mechanism, in accordance with an embodiment of the present disclosure. By implementing the mechanisms, output force is amplified in contrast to the utilized input force by means of the mechanical efficiencies. Thus, the required torque and force required to operate the mechanism is reduced based on the size of the levers to operate the mechanism, thereby reduces the size of the motor required to operate the mechanism, consequently power consumption of the motor is reduced. Further, double-acting lever mechanism 102 reduces the time required to operate the mechanism by half since two actions are performed in a single stroke.

[0062] FIG. 2A illustrates an exemplary front view of lift assembly, in accordance with an embodiment of the present disclosure.

[0063] Referring to FIG. 2A, lift assembly 200as presented in the example can be in vertical configuration and can include one or more vertical rails(202-l to 202-4)(also referred to as rails, herein) assembled in two sets of parallel rail tracks. The lift assembly 200 can include a first magnetor assembly 204-1, a second magnetor assembly 204-2, one or more sensors (208-1, 208-2) (also referred to as sensors herein), motor controller 210, one or more magnets (206-1, 206-2), a first release arm connection aperture 212-1 and a second release arm connection aperture 212-2. The sensors may include a first position sensor 208-1, a second position sensor 208-2, and one or more magnets can include a first magnet 206-1 and a second magnet 206-2. As can be appreciated, the present disclosure may not be limited to this configuration but may be extended to other configurations.

[0064] The first release arm connection aperture 212-1 can include a first end 214-1 coupled to the first magnetor assembly 204-1 and second end 216-1 can include a slot. Similarly, the second release arm connection aperture 212-2 can include a first end 214-2 coupled to the second magnetor assembly 204-2 and a second end 216-2 can include a slot.

[0065] Magnets have enormous re-usable, almost inherent permanent energy in the form of magnetic attraction force and magnetic repulsion force which can be used and reused whenever needed, thus magnetic repulsion force is transformed into mechanical motion. However, an extremely strong magnetic repulsion force is required to operate a mechanism that can yield profitable, useable mechanism that can yield excessive mechanical power than power utilized to produce such a working mechanism i.e., more output power is required than the utilized input power. Further, bringing two extremely strong powerful magnets of the like poles to near contact position directly by forcing or pushing the magnets in front of each other is nearly impossible, or may require enormous energy to achieve this task.

[0066] To overcome limitations, the lift assembly 200 can be configured to bring the like poles of the magnets to desired near contact position to create magnetic repulsion force by the operation of the lever assembly 102. Instead of bringing the two same poles of magnets directly face to face and force each other to near contact position, the magnets (206-1, 206-2) in the present disclosure are slide through any or a combination of the bottom to top, top to bottom, left to right, right to left or in any other sliding angles, this sliding method/angles exponentially reduces the force required to bring the repelling magnets to near contact position, while utilizing lower input force to perform the intended action.

[0067] The lift assembly 200 can operate in unison means such that any action performed on the first magnetor assembly 204-1 and/or on second magnetor assembly 204-2 creates retro action on either of the aforesaid assemblies (204-1, 204-2), thus providing the advantage of counterweight balance mechanism that lowers the input force requirement, aids efficient time utilization and minimizes mechanical components required to operate the mechanism each separately, particularly electricity input required to operate the mechanism and time consumption required to complete the operation cycle, thus providing robust mechanical advantage and operational efficiency.

[0068] FIG. 2B illustrates an exemplary side view of lift assembly, in accordance with an embodiment of the present disclosure. The end position of the second magnetor assembly 204-2 and start position of the first magnetor assembly 204-1 is illustrated in FIG. 2B. The first magnetor assembly 204-1 is placed at the load arm 110 and/or the second magnetor assembly 204-2 is placed at the load arm 124, each aforesaid components aligned and assembled at a desired connecting point to enable efficient, smooth functioning of the mechanism. The magnetor assemblies (204-1, 204-2) are aligned and/or positioned to function in conjunction with the load arms(110, 124) of the lever mechanism 102, each aforesaid components aligned and positioned at desired connecting points to enable efficient, smooth functioning of the mechanism.

[0069] FIG. 2C illustrates an exemplary top view of lift assembly configured with linear bearings, in accordance with an embodiment of the present disclosure. As shown in FIG 2C, the first magnetor assembly204-l is fitted with linear bearings(218-l, 218-2) at the backside of the first magnetor assembly 204-1, where the linear bearings (218-1, 218-2) are inserted into the rails (202-1,202-2) through bearing aperture. The linear bearing (218-1, 218- 2) enables the first magnetor assembly 204-1 to travel along the rails (202-1, 202-2) smoothly, faster and lowers the friction along the rails, where the first magnet 206-1 is secured to the first magnetor assembly 204-1. The first release arm 212-1 having a first end 214-1 and a second end 216-1, where the first end 214-1 is attached to the first magnetor assembly 204-1 and the second end 216-1 has the slot to couple with a lock release arm 416-1 as illustrated in FIG. 6C. The first position sensor 208-1 with on/off state is fitted at an appropriate place, where the travel end position of the first magnetor assembly 204-1 expected to end, once the first magnetor assembly 204-1 hits the travel end position or start position of the rails (202-1,202-2), the signal from the sensor 208-1 is sent to the motor 302 (illustrated and described in FIG 3A) which controls the start and stop action of the shaft 312.

[0070] Similarly, the second magnetor assemblies 204-2 is fitted with second linear bearings(218-3, 218-4) at the backside of the second magnetor assemblies 204-2. The second linear bearing (218-3, 218-4) is inserted into the rails (202-3,202-4) through bearing aperture, where the second linear bearing (218-3, 218-4) enables the second magnetor assembly 204-2 to travel along the rails(202-3, 202-4) smoothly, faster and lowers the friction along the rails. The second magnet 206-2 is secured to the second magnetor assemblies 204-2. The second release arm 212-2 having a first end 214-2 and a second end 216-2, where the first end 214-2 is attached to second magnetor assembly 204-2 and the second end 216-2 has the slot for lock release arm 416-2 (as illustrated in FIG. 6C). The second position sensor 208-2 with on/off state is fitted at an appropriate place, where the travel end position of the second magnetor assembly 204-2 is expected to end. Once the second magnetor assembly 204-2 hits the travel end position or start position of the rails (202-3,202-4), the signal from the sensor 208-2 is sent to the motor 302 which controls the start and stop action of the shaft 312. The rotation direction of the motor shaft 312 is controlled by the motor controller/switch 210.

[0071] FIG. 2D illustrates an exemplary back view of lift assembly, in accordance with an embodiment of the present disclosure. The lift assembly 200 can further include vertical lift end blocks (220-1,220-2), first prime lifter 222-1 and second prime lifter 222-2. The lift end block 220-1 acts as a stop point for the first magnetor assembly 204-1 and the first prime lifter 222-1 act as a prime lifter for the first magnetor assembly 204-1. Similarly, the second lift end block 220-2 acts as a stop point for the second magnetor assembly 204-2 and the second prime lifter 222-2 act as a prime lifter for the second magnetor assembly 204-2. The first prime lifter 222- lis enjoined with the first magnetor assembly 204-1, which enables the first magnetor assembly 204-1 to perform up and down motion when the first prime lifter 222-1 is lifted upward or downward. Similarly, the second prime lifter 222-2 is enjoined with the second magnetor assembly 204-2 enables the second magnetor assembly 204-2 to perform upward and downward motion when the second prime lifter 222-2 is lifted upward or downward.

[0072] The load arm 110 of the primary lever beam 104 is assembled beneath the first prime lifter 222-1 of the first magnetor assembly 204-1 and the load arm 124 of the secondary lever beam 106 is assembled beneath the second prime lifter 222-2 of the second magnetor assembly 204-2. Upon operation of the motor 302, the first prime lifter 222-1 and the second prime lifter 222-2 enables corresponding magnetor assemblies (204-1, 204-2) to perform upward motion and downward motion in conjunction with the motion of corresponding load arms (110, 124) to travel along corresponding rails (202-1 - 202-4).

[0073] FIGs. 3 A to 3C illustrates an exemplary side view and back view of drive unit, in accordance with an embodiment of the present disclosure.

[0074] Referring to FIGs. 3A to 3C, the drive unit 300 is configured in apparatus 100, where the drive unit 300 can include gear motor 302 (also referred to as motor 302, herein), gear unit 304, motor break 306, crank bar 308 and counterweight 314. The crank bar 308 having a first end 310-1, midpoint 310-3, and a second end 310-2, where the midpoint 310-3 of the crank bar 308 is coupled to a motor shaft 312 and the first end of the crank arm 114 of the double-acting lever mechanism 102 is pivotally connected to the first end 310-1 of the crank bar 308 of the drive unit 300 as shown in FIG.4A and 4B respectively.

[0075] In an implementation, the motor 302 coupled to the lift assembly 200through the lever assembly 102. The motor controller 210 (also referred to as controller, herein) coupled to the sensors and the motor 302, where the controller 210, on receipt of the set of input signals from the one or more sensors, configured to operate the motor to activate the lever assembly 102 such that the reciprocating movements of the lever assembly 102 enables the corresponding magnetor assemblies (204-1, 204-2) to move in conjunction with the lever assembly 102.

[0076] The gear motor shaft 312 does not make full rotation at any moment of time, the crank that connects gear motor 302 and lever arm makes only semicircle rotations, either in clockwise or anti-clockwise direction, which makes the flange attached to the shaft to move either in upward or downward direction, which is the optimal requirement for operation of lever mechanism 102. This reduces the time required to make full revolution as well as reduces power consumption of motor 302 by half in every single revolution. Thus, reducing the overall power requirements of motor per revolution and as well as time required to make full revolution. This mechanism enhances the overall performance of the machine.

[0077] FIG. 5A illustrates an exemplary back view of upstroke movement of double acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure.

[0078] Referring to FIG. 5A the first magnetor assembly 204-1 and the second magnetor assembly 204-2 are aligned and/or positioned to function in conjunction with the load arm 110 and/or load arm 124 of lever mechanism 102, each aforesaid components aligned and positioned at desired connecting points so as to enable efficient, smooth functioning of the mechanism.

[0079] The load arm 110 of the primary lever beam 104 is assembled beneath the first prime lifter 222-1 and the load arm 124 of the secondary lever beam 106 is assembled beneath the second prime lifter 222-2, where the first fulcrum 118 and the second fulcrum 128 are placed at appropriate location and position so to enable efficient and smooth functioning of the mechanisms according to the present disclosure. The upstroke and down stroke action of the levers (104, 106) is controlled and performed by the drive unit 300, where the crank bar 308 is driven by the motor 302 via motor shaft 312. The rotational direction of the motor 302 is controlled by the sensors (206-1, 206-2) and the motor controller 210.

[0080] Upstroke Movement of double acting lever assembly coupled with lift assembly:

[0081] In an example implementation, the effort arm 108 of the primary lever arm 104 perform upstroke action by the motor 302, where the load arm 110 moves downward which initiates the down stroke movement of the first prime lifter 222-1 and a reciprocating action of double action lever extended to the secondary lever beam 106 which initiates the down stroke action of effort arm 122 and the load arm 124 of the secondary lever beam 106 initiates the upstroke action of the second prime lifter 222-2. The upstroke action of the effort arm 108 initiates the down stroke action of the first prime lifter 222-1, since the first prime lifter 222- lis conjoined with the first magnetor assembly204-l, the first magnetor assembly204-l also moves downward with the first prime lifter 222-1. The effort arm 108 upstroke stroke movement also initiates effort arm 122 down stroke movement and the load arm 124 of the secondary lever beam 124 initiates the upstroke action of the second prime lifter 222-2, where the second prime lifter 222-2is conjoined with the second magnetor assembly204-2, the second magnetor assembly 204-2moves upward with the second prime lifter 222-2.

[0082] FIG. 5B illustrates down stroke movement of double acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure.

[0083] Down stroke movement of double acting lever assembly coupled with lift assembly:

[0084] In an example implementation, as shown in FIG. 5B, when the effort arm 108 down stroke action is performed by the motor302, the load arm 110 moves upward which initiates the upstroke movement of the first prime lifter 222-1 and a reciprocating action of the double-action lever extended lever beam 120initiates the upstroke action of the effort arm 122 and the load arm 124 of the secondary lever beam 106 initiates the down stroke action of the second prime lifter 222-2. The down stroke action of the effort arm 108 initiates upstroke action of the first prime lifter 222-1, where the first prime lifter 222-1 is conjoined with the first magnetor assembly204-l, the first magnetor assembly 204-lmoves upward with the first prime lifter 222-1. The effort arm 108 down stroke movement also initiates effort arm 122 upstroke movement and the load arm 124 of the secondary lever beam 106 initiates the down stroke action of the second prime lifter 222-2, where the second prime lifter 222-2is conjoined with the second magnetor assembly204-2, the second magnetor assembly 204-2 also moves downward with the second prime lifter 222-2. This action creates double acting reciprocating efficient lever mechanism, which reduces the time consumed by mechanism cycles and power consumption of the drive motor 302.

[0085] FIGs. 5C to 5D illustrate exemplary front view of double-acting lever assembly coupled with lift assembly, in accordance with an embodiment of the present disclosure. The lift mechanism 200 is used to bring the like poles of the magnets to desired near-contact position to create magnetic repulsion force. Instead of bringing the two same poles of magnets directly face to face and force each other to near contact position, in the present disclosure, preferably the magnets are slid from bottom to top through other possibilities like top to bottom and/or left to right and/or right to left or in any other sliding angles, this sliding method exponentially reduces the force required to bring the repelling magnets to near contact position, while utilizing lower input force to perform the intended action disclosed in this disclosure.

[0086] FIGs. 6 A to 6B illustrate exemplary front and back view of prime mover assembly, in accordance with an embodiment of the present disclosure.

[0087] Referring to FIGs. 6A and 6B, the apparatus 100 as illustrated in the example can include at least two prime mover assemblies (400-1, 400-2) (also referred to as prime mover assemblies, herein). The prime mover assemblies (400-1, 400-2)can include a first magnetor assembly 402-1, a second magnetor assembly 402-2, a first prime mover 404-1, a second prime mover 404-2, which are configured in parallel arrangements to create reciprocating mechanism interconnected with the crank assembly 800 (as illustrated in FIG. 8A).One or more linear drive rails (406-1 to 406-4) (also referred to as rails, herein) assembled in parallel positions on top of the first and second prime movers (404-1, 404-2) respectively. The first magnetor assembly 402 -1 and the second magnetor assembly 402-2 configured to operate on the rails (406-1 to 406-4), where the first magnetor assembly 402-1 and second magnetor assembly 402-2 is inserted onto to the rails (406-1 to 406-4) through the linear bearing apertures. The prime movers (404-1, 404-2) configured to facilitate the operation of the corresponding magnetor assemblies (402-1, 402-2) to be secured on the base platform. As can be appreciated, the present disclosure may not be limited to this configuration but may be extended to other configurations.

[0088] The first and the second magnetor assemblies (402-1, 402-2) is made of solid material suitable to be drilled, holed, screwed, attach components rigidly, durable, withstand shock, vibrations, stress-resistant and/or does not break easily. The first and the second magnetor assemblies (402-1, 402-2) can include 6 sides namely, top side, bottom side, front side, backside, right side, and left side.

[0089] In another embodiment, one or more magnets (408-1, 408-2) and one or more sensors (410-1, 410-2, 426-1, 426-2) are configured in the prime mover assemblies (400-1, 400-2). The one or more magnets can include a first magnet 408-1 and second magnet 408-2 are securely attached to the front side of the corresponding magnetor assemblies (402-1, 402- 2). The sensors can include a first position sensor 410-1 and a second position sensor 410-2 is preferably attached to right side of the first and second magnetor assemblies(402-l, 402-2) in an appropriate position so that the sensors (410-1, 410-2) can be triggered when required. The prime mover assemblies (400-1, 400-2)can include a first magnetor lock plate 412-1 and a second magnetor lock plate 412-2 that is assembled in an appropriate position at bottom side of the first and second magnetor assemblies (402-1, 402-2) so that it can be engaged and/or disengaged and/or locked in position and/or released from lock state by a first lock arm 414-1 and second lock arm 414-2 as and when required. The lock arms (414-1, 414-2) located on the front portion of the prime movers (404-1, 404-2)

[0090] The first and second lock arms (414-1, 414-2) can include a spring action lock mechanism. The lock arm mechanism has two state action mode to engage and disengaged state, where dis-engagement is performed by a first lock release arm 416-1 and second lock release arm 416-2 (as illustrated in FIG. 6C) by lifting the respective lock release arms(416-l, 416-2) in upstroke motion. The first and second lock arms (414-1, 414-2) coupled to lock release arms (416-1, 416-2). The lock release arms (416-1, 416-2) coupled to the slots configured in the release arm connection apertures (216-1, 216-2) of the lift assembly 200. The engagement mechanism engages a portion of the first and second lock arms (414-1, 414- 2) when the first magnetor assembly 402-1 and the second magnetor assembly 402-2 moves into the lock position.

[0091] For example, the lock release arm 416-1 which is connected to release arm connection aperture 216-1 and operatable relative to the movements of the first magnetor assembly 204-1. The engagement mechanism engages a portion of the magnetor lock arm 414-1 when the first magnetor assembly 402-1 move into the lock position. When the lock arm 414-1 is in a disengaged state, the magnetor assembly 402-1 can be free to retreat and move along the rails (406-1, 406-2) from a start point (418-1, 418-2) to end points (418-3, 418-4) and vice versa as shown in FIG. 6C.

[0092] In another embodiment, a twin linear bearing set (420-1 to 420-4) as illustrated in FIG. 6B configured in parallel order spaced in between each set to match accurately in measurements and angles with the measurements and angles of the rails (406-1 to 406-4) assembled in parallel positions on top of the prime movers (404-1, 404-2) attached at the bottom side of the magnetor assemblies (402-1, 402-2). The first magnetor assembly 402-1 and the second magnetor assembly 402-2 inserted onto the rails (406-1 to 406-4) through the linear bearing apertures, where the linear bearing mechanism enables the magnetor assemblies (402-1, 402-2) to move smoothly and efficiently on the respective rails (406-1 to 406-4) with less friction, while the prime movers (404-1, 404-2) are fixed on the base platform.

[0093] In another embodiment, magnetor stoppers (422-1 to 422-4) which is fixed on the front side of the first and second prime movers (404-1, 404-2) as illustrated in FIG. 6C. The first and second position sensors(410-l, 410-2) are assembled at the appropriate position so that position sensors(410-l, 410-2) can be triggered when the first and second magnetor assemblies (402-1, 402-2) move on the rails (406-1 to 406-4) from the start point (418-1, 418-2) to endpoints (418-3, 418-4) and vice versa. The motor controller 210, on receipt of the signals received from the sensors (426-1, 426-2), controls the gear motor shaft 312 to rotate either in the clockwise or anti-clockwise direction.

[0094] Crank lock pins (424-1,424-2) is assembled at the backside of magnetor assemblies (402-1, 402-2) as depicted in FIG. 6B. The double-wall crank links (428-1 to 428- 4) with axial holes having inner diameter size that of outer diameter size of the crank pins (424-1,424-2), the crank pins(424- 1,424-2) is inserted from one end of the double-wall crank link through axial hole. Further, second ends (802-la, 802-2a) of crank rods (802-1, 802-2) is introduced in between the two double-wall crank links (428-1 to 428-4) and crank pins(424- 1, 424-2) is inserted through the axial hole of second ends(802-la, 802- lb) of the crank rods (802-1, 802-2) through the other end of the double-wall crank links, where the crank pin is secured therein.

[0095] In an implementation, the sensors (208-1, 208-2, 410-1, 410-2, 426-1, 426-2) configured in the lift assembly 200 and in at least two prime mover assemblies (400-1, 400- 2), the sensors configured to generate a set of input signals pertaining to motion attributes of the at least two prime mover assemblies (400-1, 400-2) and the lift assembly 200. The controller 210 coupled to the one or more sensors and the motor 302, the controller 210 configured to operate, on receipt of the set of input signals, the motor 302 to activate the lever assembly 102 such that the reciprocating movements of the lever assembly 102 enables corresponding magnetor assemblies (204-1, 204-2) to move in conjunction with the lever assembly 102. The upward motion of the first magnetor assembly 204-1 enables same polarity magnets (206-1, 408-1) of the first magnetor assembly 402-1 to face one another to generate a repulsion force, the repulsion force is increased by engaging the same polarity magnets (206-1, 408-1) at a designated position. [0096] Lock arms (414-1, 414-2) engages the corresponding magnetor assemblies (402- 1, 402-2) in designated position during forward motion of the corresponding magnetor assemblies (402-1, 402-2) and released by at least two lock release arms (416-1, 416-2) (also referred to as lock release arms, herein) relative to the motion of the corresponding magnetor assemblies (204-1, 204-2). The lock arms (414-1, 414-2) having the spring action lock mechanism is securely fixed to front portion of the corresponding prime movers (404-1, 404- 2) to engage corresponding lock plates (412-1, 412-2) located at the bottom side of the corresponding magnetor assemblies (402-1, 402-2), where the dis-engagement is performed by the lock release arms (416-1, 416-2) as illustrated and described in FIGs. 7A to 7D respectively.

[0097] On releasing the first magnetor assembly 402-1 from the engaged state, the generated repulsion force enables the first magnetor assembly 402-1 to move backward with torque such that the second magnetor assembly 402-2 is moved forward based on the reciprocal motion of a crankshaft assembly 800 interlinked with the corresponding prime mover assemblies (400-1, 400-2), where the forward and backward motion of the prime mover assemblies (400-1, 4002) generates rotational motion in the crankshaft assembly 800 that is transferred to a generator 906 (as illustrated in FIG. 10A) through a decoupler 902 to generate power.

[0098] FIGs. 7 A to 7Dillustrate exemplary view of lock and release mechanism, in accordance with an embodiment of the present disclosure.

[0099] The lock release arms(416-l, 416-2) also interchangeably referred to as leversof the first and second prime movers (404-1, 404-2) is connected to the connection apertures(216-l, 216-2) of the release arms (212-1, 212-2) respectively. The lock and release mechanism used to lock and/or retain the magnetor assemblies (402-1, 204-1) comprising like pole magnets in near-contact position and/or release the first magnetor assembly 402-1 in controlled operation to control force and torque building of the magnetic repulsion force within the set of magnetor assemblies (402-1, 204-1) to perform the intended action.

[00100] For example, as shown in FIG. 7B, when the first magnetor assembly 204-1 moves upward in the rail (202-1, 202-2) and reaches designated stop point, the release arm 212-1 moves upward relative to the first magnetor assembly 204-1 stop position and lifts the lock release arm 416-1 relative to the release arm 212-1 position, as the lock release arm 416- 1 is lifted upward, the lock arm 414-1 gets disengaged and the first magnetor assembly 402-1 moves to the released position. As shown in FIG. 7A, when the first magnetor assembly 204- 1 moves down in the rails (202-1, 202-2) and reaches designated start point, release arm 212-

1 moves downward relative to the first magnetor assembly 204-1 start position and disengages the lock release arm 416-1 relative to the release arm 212-1 start position, as the lock release arm 416-1 is moved down, the lock arm 414-1 become ready again to engage due to inbuilt spring action.

[00101] For example, the spring-loaded lock arm 702 holds the first magnetor assembly 402-1 in designated place while like pole magnet 408-1 in the prime mover assembly 400-1 and magnet 206-1 in the lift assembly 200 in opposite direction is brought to near-contact position by the action of double-acting lever mechanism 102. The automatic spring-loaded lock arm 702 holds the first magnetor assembly 402-1 in the designated place as shown in FIG. 7C until it is released by the action of levers 416-1 once the first magnetor assembly 204-1 in lift mechanism 200 triggers the release mechanism as shown in FIG.7D. The first magnetor assembly 402-1 is released from a locked state and retreats and moves in opposite direction with force and speed, thereby the potential energy of magnetic repulsion force is transformed into kinetic energy.

[00102] Engagement mechanism can include lock release arms (416-1, 416-2) which is connected to release arm connection aperture (216-1, 216-2) and operatable relative to the movements of the first and second magnetor assemblies (204-1, 204-2). The engagement mechanism engages a portion of lock arms (414-1, 414-2)when the first magnetor assembly 402-1 and second magnetor assembly402-2moves into lock position.

[00103] By holding the like pole magnets (206-1, 408-1) in opposing near-contact position helps the magnets to build up repulsion force within the mechanism, when the first magnetor assembly 402-1 is released by the action of lock release arm 416-1, the repulsive force pushes the first magnetor assembly 402-1 in the linear rails (406-1, 406-2) which creates powerful repulsion force for each stroke, with help of linear ball bearings (420-1, 420- 2). The first magnetor assembly 402-1 moves with force and torque on the linear rails (406-1, 406-2) in a backward motion, and the crank rod (802-1) connected to the first magnetor assembly 402-1 turns the crank assembly 800. The second magnetor assembly 402-2 which is in backward position can be pushed to forward position on rails (406-3, 406-4) due to the reciprocal mechanism of the crank assembly 800, once the second magnetor assemblies 402-

2 reach the designated position, the sensors are triggered to operate lever mechanism 102, aforesaid actions are repeated thus creating the rotational motion in crank assembly 800. Thus, this mechanism is used to transform the generated magnetic repulsion force and torque to the crankshaft assembly 800 as mechanical force. The mechanism method of the magnetor assemblies (402-1, 402-2) operating in reciprocal action creates full circumferential rotational motion in the crankshaft assembly 800.

[00104] FIG. 8A illustrates an exemplary view of crank assembly 800, in accordance with an embodiment of the present disclosure.

[00105] Referring to FIG. 8A, crank assembly 800 can include flywheel 804, two reciprocating crank arm assemblies (802-3, 802-4) (as shown in FIG. 8B), main shaft (808-1, 808-2, 808-3), two crank rods (802-1, 802-2) and gearbox 810, and torque transfer shaft 812(also interchangeably referred to as drive shaft 812, herein) assembled in appropriate positions according to the present disclosure. The main shaft (808-1, 808-2, 808-3) is mounted through main bearing blocks (814-1 to 814-6) each bearing assembled at the appropriate location to balance the main shaft efficiently and effectively. The crankshaft assembly 800 can include crank rods (802-1, 802-2) having first end(802-lb, 802-2b) and second end (802- la, 802-2a), the first end(802-lb, 802-2b) pivotally coupled to the main shafts (808-1, 808-2, 808-3) and second end (802-la, 802-2a) pivotally coupled to the corresponding magnetor assemblies (402-1, 402-2) at crank pins (424-1, 424-2) respectively.

[00106] Further, the first end (802- lb, 802-2b) of the crank rods (802-1, 802-2) is rotatably coupled to crank arms (806- lb, 806-2b, 806-3b, 806-4b) respectively secured through crank arm pins (810-1, 810-2). Further the crank arms (806- lb, 806-2b) pivotally connected to main shafts (808-2, 808-1) and the crank arms (806-3b, 806-4b) pivotally connected to main shafts (808-1, 808-3). The forward and/or backward motion of the corresponding magnetor assemblies (402-1, 402-2) creates reciprocating motion of corresponding crank rods (802-1, 802-2) such that the reciprocating motion of the crank rods converted to rotational motion of the main shaft (808-1, 808-2, 808-3) that is transferred to the drive shaft 812 of the crankshaft assembly 800.

[00107] One end of the main shaft 808-2 is mounted through main bearings (814-5, 814- 6) and conjoined with crank arm flange 816-1 and other end of the main shaft 808-2 conjoined with flywheel 804, where the flywheel 804 aids the rotational motion into smooth rotational motion. One end of the main shaft 808-1 is mounted through main bearings (814-1, 814-2) and conjoined with crank arm flange 816-2 and the other end is conjoined with crank arm flange 816-3. One end of the main shaft 808-3 is mounted through main bearings (814-3, 814-4) and conjoined with crank arm flange (816-4) and the other end connected with the gearbox 810.

[00108] In another embodiment, one end of the crank rods(802-l, 802-2) pivoted to the first and second magnetor assemblies (402-1, 402-2) respectively. The other end of the crank rods(802-l, 802-2) is rotatably mounted to the crank of the main shaft (808-1, 808-2, 808-3) for converting the reciprocating movement of the crank rod (802-1, 802-2) to the rotational movement of the main shaft (808-1, 808-2, 808-3). The crank rod 802-1 having the first end points (802-lb, 802-2b), and the second end points (802-la, 802-2a)acts as a rocker which converts reciprocating push and pull force into a continuous rotational motion through main shaft 808-1 and gear box 810 then through gearbox to the torque transfer shaft 812.

[00109] Reciprocating crank assemblies can include crank assemblies (802-3, 802-4). A crank arm 806-1 having end points (806-la, 806-lb), crank arm 806-2 having end points at (806-2a, 806-2b). Crank arm 806- lis comprised of crank arm flange 816-1 at the perfect center of the arm, counter weight is attached at 806- la of the crank arm 806-1 and other end 806-lbof the crank arm 806-1 is fitted with the crank arm flange bearing 816-1. Crank arm 806-2 is comprised of crank arm flange 816-2 at the perfect center of the arm, counter weight is attached at end point 806-2a of the crank arm 806-2 and other end 806-2b of the crank arm 806-2 is fitted with the crank arm flange bearing 816-2. Counter weight at end points (806-la, 806-2a) diametrically opposite each crank arms (806-1, 806-2) equalling the weight of the crank pin plus the weight of the adjacent end of the crank pin crank rod. This weight is preferably proportioned between the ends of the crankshaft adjacent to the particular crank pin so that its effective point can be diametrically opposite the center of the crank pin to thus eliminate the rotating couple otherwise produced.

[00110] Crank arm 806-3 having end points (806-3a, 806-3b), crank arm 806-4 having end points at (806-4a, 806-4b). Crank arm 806-3 is comprised of crank arm flange 816-3 at the perfect center of the arm, counter weight is attached at 806-3b of the crank arm 806-3 and other end 806-3a of the crank arm 806-3 is fitted with the crank arm flange bearing 816-3. Crank arm 806-4 is comprised of crank arm flange 816-4 at the perfect center of the arm, counter weight is attached at end point 806-4b of the crank arm 806-4 and other end 806-4a of the crank arm 806-4 is fitted with the crank arm flange bearing 816-4. Counter weight at end points (806-3b, 806-4b) diametrically opposite each crank arms (806-3, 806-4) equalling the weight of the crank pin plus the weight of the adjacent end of the crank pin and crank rod. This weight is preferably proportioned between the ends of the crankshaft adjacent to the particular crank pin so that its effective point can be diametrically opposite the center of the crank pin to thus eliminate the rotating couple otherwise produced.

[00111] The crank assembly 802-3 can include crank arms (806-1, 806-2), where the crank arm pin 810-1 is inserted through the flange bearing of crank arm 806-1 and through the end 802- lb of the crank rod 802-1 and secured with bolts in appropriate location to retain the crank arm pin 810-1 in place, thus forming a crank assembly 802-3. Crank Assembly 802- 4 can include crank arms (806-3, 806-4), where the crank arm pin 810-2 is inserted through the flange bearing of crank arm 806-3 through the end 802-2b of crank rod 802-2 and secured with bolts in appropriate location to retain the crank arm pin 810-2 in place, thus forming the crank assembly 802-4.

[00112] FIG. 8B illustrates position of crank rods, in accordance with an embodiment of the present disclosure. FIG. 8B depicts forward position of crank rod 802-1 and backward position of crank rod 802-2.

[00113] FIG. 8C illustrates a top view of crank assembly coupled with prime mover assembly, in accordance with an embodiment of the present disclosure.

[00114] Assembly method of crank rods (802-1, 802-2) shown in FIG. 8C, first end 802- lb of the crank rod 802-1 is connected to the crank arm pin 810-1 of the crank assembly 802- 3 and second end 802- la of crank rod 802-1 is connected to the crank pin 424-1 of the first magnetor assembly 402-1. Similarly, one end 802-2b of the crank rod 802-2 is connected to the crank arm pin 810-2 and other end 802-2a of crank rod 802-2 is connected to the crank pin 424-2 of the second magnetor assembly 402-2. The crank rod 802-1 having end point 802- la is fixed with flange bearings having shaft aperture is inserted into crank pin 424-1 which is fixed at the back of first magnetor assembly 402-1. The crank rod 802-2 having end point 802-2a is fixed with flange bearings having shaft aperture is inserted into crank pin 424-2 which is fixed at the back of second magnetor assembly 402-2.

[00115] As shown in FIG. 8C, whenever the first magnetor assembly 402-1 moves in forward direction or backward direction, push and pull action of crank rod 802-1 is created and whenever the second magnetor assembly 402-2 moves in forward direction or backward direction push and pull action of crank rod 802-2 is created, which creates reciprocating rotational motion in the main shaft (808-1 to 808-3) then transferred to gearbox 810 consequently to the drive shaft 812.

[00116] For example, when magnetic repulsion force is exerted on the first magnetor assembly 402-1, the first magnetor assembly 402-1 moves on the rails (406-1, 406-2). As the first magnetor assembly 402-1 moves, the force is transformed into linear motion, second end 802- la of the crank rod 802-1 which is connected to crank pin 424-1 and first end 802-lbof the crank rod 802-1 connected to crank arm pin 810-1 of the crank rod 802-1 pushes the crank assembly 800 in upward rotation movement, which turns conjoined crank shafts (808-1 to 808-3) and consequently a reciprocating mechanism of crank shaft assembly moves downwards and crank rod 802-2 having end points 802-2b which is connected to crank arm pin 810-2 and other end 802-2a is connected to crank pin 424-2 of the second magnetor assembly 402-2 pushes the second magnetor assembly 402-2 in forward motion on prime mover rails (406-3, 406-4), where reciprocating action of crankshaft creates rotational motion which is further transformed in electricity preferably as per present disclosure.

[00117] In an embodiment, the decoupler (as illustrated in FIG. 10A) interposed between the drive shaft 812 of the crank assembly 800 and driven shaft 908 of the generator assembly 900, where the decoupler 902 enables the transfer of rotational torque of the drive shaft 812 to the driven shaft 908, and disengages the driven shaft 908 from the drive shaft 812 to enable the driven shaft 908 to rotate at a speed different from that of the speed of the drive shaft 812.

[00118] The decoupler 902 enables the driven shaft 908 to rotate faster with accumulated angular moment force of a flywheel 904, the decoupler 902 enables the flywheel to continue rotation until the accumulated angular moment force gets depleted even when the drive shaft 812 is in idle condition. The flywheel 904 interposed between decoupler 902 and generator 906 of the generator assembly to maintain the smooth rotational motion, and delivers the accumulated speed and angular momentum to the driven shaft 908 of the generator 906 to generate power/electricity.

[00119] FIGs. 9A to 9Cillustrate exploded exemplary view of non-combustion magnetor engine, in accordance with an embodiment of the present disclosure. The exploded view of lever assembly 102, lift assembly 200 with connection apertures (216-1, 216-2), at least two prime mover assemblies(400-l, 400-2), lock release arms (416-1, 416-2) and crank assembly 800 is disclosed. The lever assembly 102, the prime mover assemblies(400- 1,400- 2)interlinked with the crank assembly 800 are shown in FIG. 9A. The upstroke movement of the lever assembly 102 enables upward and downward motion of the lift assembly 200, the forward motion of the prime mover assembly 400-1 and backward motion of the prime mover assembly 400-2 is illustrated in FIG. 9B. Similarly, the down stroke movement of the lever assembly 102, upon operation of the drive unit 300, the forward position of the prime mover assembly 400-2 and backward position of the prime mover assembly 400-1 interlinked with the crank assembly 800 and upward and downward motion of the lift assembly 200 is illustrated in FIG. 9C.

[00120] The apparatus 100 for generation of electricity, the apparatus can include the lever assembly 102 with the primary lever beam 104 coupled to the secondary lever beam 106 by the extended lever beam 120, the motion of the effort arm 108 of the primary lever beam 104 creates reciprocating motion on the effort arm 122 of the secondary lever beam 106. The vertical lift assembly 200 can include one or more magnets (206-1, 206-2) secured to the first magnetor assembly 204-1 and the second magnetor assembly 204-2 respectively, where the first magnetor assembly 204-1 and the second magnetor assembly 204-2, upon operation of the lever assembly 102, configured to slide in upward direction and downward direction along one or more parallel vertical rails (202-1 to 202-4). The at least two prime mover assemblies (400-1, 400-2) with one or more magnets (408-1, 408-2) secured to the first magnetor assembly 402-1 and the second magnetor assembly 402-2 respectively, where the first magnetor assembly 402-1 and the second magnetor assembly 402-2 operable to move in the forward and backward direction horizontally along one or more parallel rails (406-1 to 406-4).

[00121] At least two lock release arms (416-1, 416-2) of corresponding prime mover assemblies (400-1, 400-2) coupled to corresponding connection apertures (216-1, 216-2) of the lift assembly 200 and operatable relative to the movements of corresponding magnetor assemblies (204-1, 204-2). A decoupler 902 configured in a generator assembly 900 of the apparatus 100 to transfer rotational motion of a crankshaft assembly 800 to a generator 906, the crankshaft assembly 800 interlinked with the corresponding prime mover assemblies (400-1, 400-2).

[00122] The sensors (208-1, 208-2, 410-1, 410-2, 426-1, 426-2) configured in the lift assembly 200 and in at least two prime mover assemblies (400-1, 400-2) to generate the set of input signals pertaining to motion attributes of the at least two prime mover assemblies (400-1, 400-2) and the lift assembly 200. The motor 302 configured in the drive unit 300 of the apparatus 100. The controller 210 coupled to the one or more sensors and the motor 302, the controller (210) configured to operate, on receipt of the set of input signals from the one or more sensors, the motor 302 to activate the lever assembly 102 so as to enable corresponding magnetor assemblies (204-1, 204-2) to perform reciprocating motion in conjunction with the lever assembly 102, where the upward motion of the first magnetor assembly 204-1 and forward motion of the first magnetor assembly 402-1 enables same polarity magnets (206-1, 408-1) to face one another to generate a repulsion force, the repulsion force is augmented by engaging the same polarity magnets (206-1, 408-1) at a designated position.

[00123] Upon releasing the first magnetor assembly 402-1 from the engaged state, the generated repulsion force enables the first magnetor assembly 402-1 to move backward with torque such that the second magnetor assembly 402-2 is moved forward based on the reciprocal motion of a crankshaft assembly 800 interlinked with the corresponding prime mover assemblies (400-1, 400-2), the forward and backward motion of the prime move assemblies (400-1, 400-2) generates rotational motion in the crankshaft assembly 800 that is transferred to the generator 906 through the decoupler 902 to generate power, the generated output power is amplified in contrast to the applied input force.

[00124] FIG. 10A illustrates an exemplary view of generator assembly, in accordance with an embodiment of the present disclosure.

[00125] Referring to FIG. 10A, the generator assembly 900 can include decoupler 902, flywheel 904, generator906, bearing(910-l to 910-6) and driven shaft 908, where the driven shaft 908 is inserted through bearing (910-1 to 910-6), the bearings assembled at the appropriate location to balance the driven shaft 908to rotate smoothly, efficiently and effectively. The coupling of the crank assembly 800 with the generator assembly 900 is illustrated in FIG. lOB.The mechanical power, torque and rotational motion transferred through torque transfer shaft 812(also interchangeably referred to as drive shaft 812, herein) to the decoupler mechanism 902, where a drive hub 902-2of decoupler mechanism 902 transfers the rotational motion to the shaft908, where the flywheel 904 at the center of the assembly maintains the smooth rotational motion, maintains and accumulates the speed and angular momentum and delivers to the shaft 908 to rotate the shaft of generator 906.

[00126] FIG. IOC illustrates an exemplary view of decoupled mechanism, in accordance with an embodiment of the present disclosure. [00127] The decoupler mechanism 902 is provided for transferring rotational torque between the drive shaft 812 and the driven shaft 908 of the flywheel assembly 904. The decoupler mechanism 902 can include a driven hub 902-1 and a drive hub 902-2, where the drive hub 902-2is configured to be secured to the drive shaft 812 and the driven hub 902-1 configured to be secured to the driven shaft 908.

[00128] The drive hub 902-2 having first end 912-1 and second end 912-2, the first end 912-1 of the drive hub 902-2 having axial shaft aperture, the first end 912-1 of the drive hub 902-2 is configured to be secured to the drive shaft 812. A second end 912-2 of the of the drive hub 902-2 having cap aperture configured to be securely attached to the radial rim element 914 of a freewheel mechanism 918.

[00129] The driven hub 902-1 configured to be secured to the driven shaft 908, the driven hub 902-1 having a first end 912-3 and a second end 912-4, where the first end 912-3 of the driven hub 902-1 is having straight through shaft lock pin hole 912-5. The first end 912-3 can include shaft lock pin 912-6and the shaft collar 912-7, where the shaft collar 912-7 is securely attached to the first end 912-3 by inserting shaft lock pin 912-6 through the securely attached shaft collar lock pin hole 912-5. The driven hub 902- 1 can include freewheel mechanism 918 secured to the driven hub shaft 902-1. The driven hub 902-1 further include a shaft lock pin 912-8 inserted through the driven hub shaft hole which rigidly holds the inner rim 914 of the freewheel mechanism 918 from turning independently of the driven hub shaft. The driven hub 902-1 further includes a ball bearing 916 which is securely inserted on to the driven hub shaft 902-1. The second end 912-4 of the driven hub 902-1 is configured to be secured to the driven shaft 908 through the shaft aperture of driven hub shaft 902- 1.The driven hub radial rim element 914 of freewheel mechanism 918 is securely attached to cap aperture 912-2 of the drive hub 902-2 using bolts.

[00130] Decoupler mechanism 902 enables the transferring of rotational torque of drive shaft 812 to the driven shaft 908, decoupler mechanism 902 allows the driven assembly to overrun or operate temporarily at a speed different from that of the crankshaft assembly800 and to decouple or mechanically isolate the driven assembly from the crankshaft assembly800 and reduce torsional vibrations there between. Decoupler mechanism 902 transmits smooth shaft rotation, speed and torque to shaft 908, decoupler mechanism is interposed between the driving shaft 812 and driven shaft 908 having a reciprocating rotary motion about axis 0 which is transferred to the driven shaft 908. [00131] As shown in FIG. IOC, custom-designed decoupler mechanism 902 permits the shaft 908 to rotate on freeform from the shaft 812. This mechanism enables the shaft 908 to rotate faster and continue rotating with the accumulated angular moment force of flywheel 904 even when the shaft 812 is not rotating or in idle condition while there is operational mechanical time gap between reciprocating magnetor assemblies (402-1, 402-2) operation which transfers the pull and push motion to crankshaft 800 through cranks rods (802-1, 802- 2). Decoupler mechanism 902 disengages the driven shaft 908 from the torque transfer shaft 812, this enables the flywheel 904 to continue its rotational motion by excreting its accumulated angular movement, where the accumulated angular movement and force of flywheel 904 enables the generator 906 to continue functioning even while there is rotation speed variation or idle rotational motion gap between gearbox shaft 812 and shaft 908.

[00132] In another embodiment, the flywheel 904 conserves the angular momentum to efficiently store rotational energy and the stored mechanical energy is utilized when there is a drop in input rotational force and can conversely absorb any excess input rotational force in the form of rotational energy, flywheel 904 inherently smoothen sufficiently small deviations in the power output of a system, thus enabling enhanced force transfer from the driving side 812 to the driven shaft 908. As the flywheel 904 delivers enhanced rotational force to the generator 906, the generator 906 produces power at low revolutions per minute (RPM) even at 1st RPM as soon as rotor shaft 908 starts rotating, due to low RPM and high output design. In an exemplary embodiment, the generator 906 is a low RPM PM generator 906.

[00133] The embodiments of the present disclosure described above provide several advantages. One or more of the embodiments suffice the speed requirement of the generator to produce expected amps, frequency and power, further low RPM design inherits the advantages of low cost, lightweight mechanisms, low maintenance, aids in the longevity of mechanical components, reliable power output, simple design and the likes. The present disclosure can be used to produce clean, eco-friendly electricity without any kind of fuel burning or without any type of additional external source of power to produce electricity, but not just limited to electricity production, the present disclosure can be used to produce any type motions like rotational motion, pull and push motion but not essentially limited to, whereas the present disclosure can be used in a wide range of applications.

[00134] In an example implementation, the motor 302 can rotate the crankshaft 312 having endpoints (310-1, 310-2), the direction of the rotation of the gear motor shaft 312 depends on the signal received from the sensors (208-1, 208-2, 426-1, 426-2). On receipt of the signals received from the sensors (208-1, 208-2, 426-1, 426-2) and motor controller 210, the gear motor shaft 312 rotates either in clockwise or anti-clockwise direction. The endpoint 310-1 is connected through the shaft pin to the crank arm 114 of the lever beam 104. In case motor shaft 312 performs down stroke movement as per the signals received from sensors (208-1, 208-2, 426-1, 426-2) and motor controller (210), the effort arm 108 moves downward and consequently load arm 110 moves upward and lifts the first magnetor assembly 204-lupward in the rails (202-1, 202-2) and due to the incorporated reciprocal mechanism, the load arm 110 upward movement forces the effort arm 122 of the secondary lever beam 106 to lift upwards and the load arm 124 to move downwards, where the second magnetor assembly204-2 moves downward due to inherent self-weight. Both the load arms (110, 124) stopat the designated location and the sensor 208-1 sends signal to stop the motor 302, at the same time, the release arm 212-1 lifts up the lock release arm 416-1, which releases and forces the first magnetor assembly 402-1 which contains extremely strong magnet in backward motion due to the magnetic repulsion force of the same poles of magnet 408-1 in the first magnetor assembly 402-1 and magnet 206-1 in the first magnetor assembly 204-1.

[00135] As soon as the first magnetor assembly 402-1 starts moving backward with magnetic repulsion force, the crank rod 802-1 having endpoints 802- la connected to the crank pin 424-1 and endpoint 802-lbconnected to crank assembly rod 802-3pushes the crank assembly 800 in upward rotation movement, which turns conjoined main shafts (808-1 to 808-3) and consequently a reciprocating mechanism of crankshaft assembly 800moves downwards and crank rod 802-2having end points 802-2bwhich is connected to crank assembly rod 802-4 and crank rod 802-2a which is connected to crank pin 424-2 of the second magnetor assembly 402-2 pushes the second magnetor assembly 402-2 in forward motion on the prime mover rails (406-3, 406-4 ) and gets locked due to embedded spring action in the lock arm 414-2. Both the magnetor assemblies (402-1, 402-2) stops at the designated location due to the reciprocating action of cranks shaft assembly 800

[00136] As soon as the magnetor assemblies (402-1, 402-2) stops at the designated location, sensors(410-l, 410-2) send signal to the motor controller 210, where the motor controller 210 control the motor 302 to rotate in anti-clockwise direction, which creates upstroke movement of the motor shaft 312. Upon upstroke movement, the effort arm 108 moves upward and consequently load arm 110 moves downward and the first magnetor assembly 204-1 in lift rails (202-1, 202-2) moves downward. Due to inherent self-weight and due to the incorporated reciprocal mechanism, the load arm 110 downward movement forces the effort arm 122 to move downward and the load arm 124 moves upward and the second magnetor assembly 204-2 moves upward. Both load arms (110, 124) stops at the designated location and sensor 208-1 sends the signal to stop the motor, at the same time, release arm 212-2 lifts up the lock release arm 414-2 which releases and forces the second magnetor assembly 402-2 which contains extremely strong magnet in backward motion due to the magnetic repulsion force of the same poles of magnet 408-2 in second magnetor assembly 402-2 and magnet 206-2 in the second magnetor assembly 204-2.

[00137] As the second magnetor assembly 402-2 starts moving backward with magnetic repulsion force, the crank rod 802-2 having endpoints 802-2a connected to crank pin 424-2 and crank rod endpoint 802-2bconnected to crank assembly rod 802-4 pushes the crank assembly in upward rotation movement, which turns conjoined crank shafts (808-1 to 808-3) and consequently a reciprocating mechanism of crank shaft assembly moves downwards and crank rod 802-1 pushes the first magnetor assembly 402-1 in forward motion on the prime mover rails (406-1, 406-2) and gets locked due to embedded spring action in magnetor assembly lock arm 414-1. Both magnetor assemblies (402-1, 402-2) stops at the designated location due to the reciprocating action of cranks shaft assembly.

[00138] When the magnetor assemblies (402-1, 402-2) stops at the designated location, position sensor (410-2, 410-1) send the signal to the motor controller 210, where the motor controller 210 control the motor 302 to rotate in the anti-clockwise direction which creates down stroke movement of the motor shaft 312. Consequently, mechanical actions mentioned in the above get repeated endlessly unless motor 302 is switched off.

[00139] Aforesaid mentioned mechanical activity creates rotational motion in the crank shaft 800 which is conjoined with gear box through shaft, where the speed is increased in 1:2 ration and transferred through shaft 812 to decoupler mechanism 902 and then to the flywheel 904, where the force accumulated and retained in the flywheel 904 in turn rotates the low RPM, highly efficient permanent magnet generator 906 through the shaft 908 to generate electricity. Low RPM permanent magnet generator is used in the disclosure to generate electricity, thus high speed shaft rotation of the generator is not required. Low RPM permanent magnet generators starts producing power at low RPM as low as 1st RPM. [00140] The generated magnetic repulsion force is then converted into directed pull and push force to rotate the crankshaft thus creating rotational motion. The bigger the magnet, the more force, speed and torque can be generated. There greater the force, speed and torque is produced the more rotational force and/or pull and push torque can be produced. The potential of the proposed engine is just limited only by the repulsion force of magnet used in this engine. More the repulsion force is, the more powerful the engine becomes.

[00141] FIGs. 11A tollB illustrate exemplary view of non-combustion magnetor engine 100, in accordance with an embodiment of the present disclosure. FIGs. 11A and FIG. 11B depicts the assembling of lever assembly 102, drive unit 300, lift assembly 200, at least two prime mover assemblies (400-1, 400-2), crankshaft assembly 800and generator assembly 900 with decoupler 902. The present disclosure provides the apparatus that enable the transportation system to have smokeless, emission less vehicles and to produce clean, safe, eco-friendly, smart electricity generation without fuel-burning or any type of additional external source of power to produce electricity.

[00142] The apparatus 100 provides decentralized electricity generation and distribution to provide easy access of electricity to millions of users to empower and enable the users to meet their energy demands and can be used in time of disaster. The present disclosure reduces the acquisition of farmlands, wildlife lands, fertile lands for building transmission lines, distribution power stations, power plants, wind farms, solar power farms and the likes. Further, the apparatus can be re-cycled without the emission of hazardous materials into the environment.

[00143] FIG 12 illustrates an exemplary circuit connection of motor control and sensor system, in accordance with an embodiment of the present disclosure.

[00144] The motor control and changeover electrical switch system 1000 can be configured for managing power flow that can include one or more electrical cables configured to connect to the electrical input system and to the changeover electrical switch and motor controllers, where the electrical cables are configured to allow power flow to the changeover electrical switch and motor controller system to control the start, stop and rotational direction of motor as per the present embodiments of the disclosure.

[00145] The motor control and changeover electrical switch system 1000 can include one or more electrical cables (1002-1, 1002-2, 1002-3) and changeover electrical switches (208-1, 208-2, 410-1, 410-2)(also interchangeably referred to as sensors, herein) and the motor controller 210. The controlled electrical power input is provided to the switching system through cable (1002-1, 1002-2), where the cable 1002-1 indicates negative input, the cable 1002-2 indicates positive input and cable 1002-3 indicates positive output.

[00146] The second end of the cable 1002-1 is connected to the power input slot of the motor controller 210. A first end power input cable 208-la is connected to power input slot of changeover electrical switch 208-1 and a second end 208- lb is connected to second phase power input cablel002-4.

[00147] A first end 208-2aconnected to the power input slot of changeover electrical switch208-2 and a second end 208-2b is connected to a second phase power input cable 1002- 4.The power output from changeover electrical switch 208-1 is received through first end power receiving cable 208- lc and second end 208- Id is connected to power input slot of changeover electrical switch 410-1, where the power output slot of changeover electrical switch 410-1 is connected to first end 410-la of electrical cable. The power output from changeover electrical switch 208-2 is received through first end power receiving cable 208- 2cand second end 208-2d is connected to power input slot of changeover electrical switch 410-2, power output slot of changeover electrical switch 410-2 is connected to the first end 410-2a of electrical cable.

[00148] Second end of power cable 410- lb and second end of power cable 410-2b is connected to second end of power cable 210-b, first end power cable 210-a is connected to power input slot 2 of the motor controller 210. Power output slots of motor control 210 are further connected to motor 302 power input slots.

[00149] Functioning of an above-stated system can be further described as follows, the one or more electrical cables, motor controller 210, changeover electrical switches (208-1, 208-2, 410-1, 410-2) are configured to control the power supply to motor 302 that controls the operation of double-acting lever mechanism 102, magnetor assembly 200, prime mover assembly (400-1, 400-2), where changeover electrical switches (208-1, 208-2, 410-1, 410-2) are assembled at the appropriate position so that changeover electrical switches (208-1, 208- 2, 410-1, 410-2) can be triggered when magnetor assemblies (402-1, 402-2)moves on the rails (406-1, 406-2) from the start point (418-1, 418-2) to endpoints (418-1, 418-2) and vice versa, as per the present embodiments of the disclosure. The motor 302 rotates the crankshaft 314 having endpoints (310-1, 310-2), the direction of the rotation of the gear motor shaft 312 depends on the signal received from the changeover electrical switch (208-1, 208-2, 410-1, 410-2) and motor controller 210, where depending on the signals received from sensors and motor controller, the gear motor shaft 312 rotates either in clockwise direction or anti clockwise direction.

[00150] The engine 100 require very low startup power which can be utilized from single battery, once the engines start producing power, battery switches from supply mode to charging mode and simultaneously power for motor can be drawn from generator output power source instead of battery. Once start-up battery is fully charged, full out power can be redirected to main supply. Thus, any kind of fuel combustion or any kind of human intervention or external source of powers like solar, wind, water, steam, nuclear power, atomic power, thermal power or any kind of external force out of the system is not required to run the proposed engine.

[00151] It will be apparent to those skilled in the art that the apparatus 100 of the disclosure may be provided using some or all of the mentioned features and components without departing from the scope of the present disclosure. While various embodiments of the present disclosure have been illustrated and described herein, it will be clear that the disclosure is not limited to these embodiments only. Numerous modifications, changes, variations, substitutions, and equivalents will be apparent to those skilled in the art, without departing from the scope of the disclosure, as described in the claims.

ADVANTAGES OF THE PRESENT DISCLOSURE

[00152] The present disclosure provides an apparatus that enable the transportation system to have smokeless, emission less vehicles and to produce clean, safe, eco-friendly, smart electricity generation without fuel-burning or any type of additional external source of power to produce electricity.

[00153] The present disclosure provides an apparatus that provides decentralized electricity generation and distribution to provide easy access of electricity to millions of people to whom electricity is still unaffordable and a distant dream in many poor countries and to empower and enable the users to meet their own energy demands and provide uninterrupted power supply that can be used always and during the time of natural disasters. [00154] The present disclosure provides an apparatus that reduces the acquisition of farmlands, wildlife lands, fertile lands for building transmission lines, distribution power stations, power plants, wind farms, solar power farms and the likes.

[00155] The present disclosure provides an apparatus that increases the lifting force while utilizing lower input force to perform the mechanism. The torque and force required to operate the machine are reduced based on the size of the levers to operate the mechanism, thereby reduces the size of the motor required to operate the mechanism, consequently time and power required to operate the mechanism is reduced.

[00156] The present disclosure provides an apparatus that consists of magnets that slide on linear rails using linear bearing base assembly from bottom to top or in any other sliding angles that reduces the force required to bring the repelling magnets to near-contact position.

[00157] The present disclosure provides lock and release mechanism that is used to lock and/or retain the like pole magnets in near-contact position and/or release the magnets in controlled operation to control force and torque building of the magnetic repulsion force within the set of magnetor assemblies to perform the intended action.

[00158] The present disclosure provides decoupler mechanism for transferring rotational torque between the drive shaft of crankshaft and the driven shaft of the generator assembly, this mechanism enables the shaft of the generator assembly to rotate faster and continue rotating with the accumulated angular moment force of flywheel even when the shaft of the crankshaft is not rotating or in idle condition.

[00159] The present disclosure produces expected amps, frequency and power at low cost, where the input energy required to rotate the shaft of the electricity generator is less than the total energy produced in each RPM.

[00160] The present disclosure provides an apparatus that has lightweight mechanisms, low maintenance, aids in the longevity of mechanical components, reliable power output, and simple design.

[00161] The present disclosure provides an apparatus that can be re-cycled without the emission of hazardous materials into the environment.