DEVICE AND CONTROL SYSTEM FOR PRODUCING ELECTRICAL POWER

Abstract

Briefly, the invention involves a system and method for generating electrical power. The system includes an electromagnet positioned with one pole directed toward a like pole of a permanent magnet. The permanent magnet is preferably mounted for oscillating movement toward the pole of the electromagnet. A control system for the electromagnet is provided to supply direct current (DC) power in the form of square wave pulses which coincide with the position of the permanent magnet. Power is collected upon the collapse of the magnetic field within the electromagnetic magnet. In some embodiments the present device is supplied in the form of a reciprocating engine which provides rotary motion in addition to the electrical power generated.

Claims

1. A method of controlling the temperature of an electrical device comprising: providing a core for an electromagnet assembly; positioning a coil sized for placement about said core forming an electromagnet assembly having a first positive magnetic pole and a first negative magnetic pole defining a longitudinal axis of said electromagnet assembly; providing a permanent magnet having a second positive pole and a second negative pole; positioning said first positive magnetic pole in alignment with said second magnetic pole; delivering an electrical signal to said coil to energize said electromagnet assembly causing said electromagnet assembly to generate a magnetic field; connecting an output cable to said electromagnet assembly for distributing an electrical pulse generated upon the collapse of said magnetic field.

2. The method of controlling the temperature of an electrical device of claim 1 wherein said electrical signal is an electrical pulse.

3. The method of controlling the temperature of an electrical device of claim 2 wherein said electrical pulse is in the form of a square wave.

4. The method of controlling the temperature of an electrical device of claim 3 wherein said square pulses are delivered at a rate of at least one kilohertz.

5. The method of controlling the temperature of an electrical device of claim 1 wherein said core is longer than said coil.

6. The method of controlling the temperature of an electrical device of claim 5 wherein said core is twice as long as said coil.

7. The method of controlling the temperature of an electrical device of claim 1 wherein said first negative pole is aligned with said second negative pole.

8. The method of controlling the temperature of an electrical device of claim 1 wherein one of said electromagnet assembly or said permanent magnet assembly is oscillated with respect to the other during delivery of said electrical signal.

9. The method of controlling the temperature of an electrical device of claim 1 wherein both of said electromagnet assembly and said permanent magnet assembly is oscillated with respect to the other delivery of said electrical signal.

10. The method of controlling the temperature of an electrical device of claim 1 including an external electrically powered device, said external device being in electrical communication with said distributed electrical pulse.

11. The method of controlling the temperature of an electrical device of claim 10 wherein said external electrical device is a fusion reactor.

12. The method of controlling the temperature of an electrical device of claim 10 wherein said external electrical device is a low energy nuclear reaction.

13. The method of controlling the temperature of an electrical device of claim 10 wherein said external electrical device is an electrolysis reaction.

14. The method of controlling the temperature of an electrical device of claim 1 including the step of connecting a signal controller to said electromagnet assembly for varying said electrical signal supplied to electromagnet assembly.

15. The method of controlling the temperature of an electrical device of claim 14 wherein said electrical signal is varied based upon a temperature of an external electrical device in electrical communication with said distributed electrical pulse.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0019] FIG. 1 is a top view partially in section illustrating one embodiment of the present invention;

[0020] FIG. 2 is a top view of an alternative embodiment of the present invention;

[0021] FIG. 3 is a side view of an alternative embodiment of the present invention;

[0022] FIG. 4 is a perspective view illustrating one embodiment of a coil assembly of the present invention;

[0023] FIG. 5 is an electrical schematic of one embodiment of the present invention;

[0024] FIG. 6 is a partial view of the schematic illustrated in FIG. 5;

[0025] FIG. 7 is a partial view of the schematic illustrated in FIG. 5;

[0026] FIG. 8 is a partial view of the schematic illustrated in FIG. 5;

[0027] FIG. 9 is a partial view of the schematic illustrated in FIG. 5;

[0028] FIG. 10 is a partial view of the schematic illustrated in FIG. 5;

[0029] FIG. 11 is a partial view of the schematic illustrated in FIG. 5;

[0030] FIG. 12 is an electrical schematic of a power control circuit of one embodiment of the present invention;

[0031] FIG. 13 illustrates one embodiment of the power delivery to the electromagnetic coils when the power control circuit of FIG. 12 is utilized;

[0032] FIG. 14 illustrates a portion of a dynamometer test conducted on the system illustrated in FIG. 1; and

[0033] FIG. 15 is a schematic representation of one embodiment of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0034] While the present invention is susceptible of embodiment in various forms, there is shown in the drawings and will hereinafter be described a presently preferred embodiment with the understanding that the present disclosure is to be considered an exemplification of the invention and is not intended to limit the invention to the specific embodiments illustrated.

[0035] Referring to FIG. 1, one embodiment of the present power generation system is illustrated in the form of a magnetically operated reciprocating engine 10. The magnetically operated reciprocating engine 10 includes at least one piston 12 constructed and arranged to reciprocate along a substantially linear path illustrated herein as a cylinder 14. The piston 12 includes at least one, and preferably a plurality of permanent magnets 16 secured thereto. The magnets are preferably secured to a top surface of the piston 12 via a non-metallic member or assembly. The piston 12 is pivotally secured to a connecting rod 18 that is rotationally connected to a crankshaft 20 to convert the reciprocating movement of the piston into rotary motion at the crankshaft. An electromagnet assembly 22 is secured beyond the end of the piston 12 stroke at a position to react with the permanent piston magnets 16 when energized in a controlled manner. A timing/firing system 100 is utilized to monitor rotation of the crankshaft for causing the electromagnet assembly 22 to generate a magnetic field in response to crankshaft position. The electromagnet assembly 22 and permanent magnets 16 are preferably configured so that a pushing force is created between the coil banks and the pistons. In an alternative embodiment one bank may be electromagnetically pushing while the opposite bank is electromagnetically pulling. It should be noted that while a horizontally opposed engine is illustrated, the instant invention can be utilized on any reciprocating engine configuration known in the art without departing from the scope of the invention. Such engine configurations include, but should not be limited to, V-configurations, W-configurations, in line configurations, radial configurations and the like.

[0036] Referring to FIG. 2, an alternative embodiment of the present invention is illustrated. In this embodiment, the power generation system includes at least one permanent magnet 16 constructed and arranged to reciprocate or oscillate along a substantially linear path. The at least one magnet 16 may be guided by a cylinder, partial cylinder, rail or any other means known in the art for guiding mechanical assemblies. A cam assembly 224 is secured behind the permanent magnet 16 for moving the permanent magnet in a reciprocating motion. The cam assembly 224 preferably includes a camshaft 226 having at least one eccentric lobe 228 and a motor 230 for rotating the camshaft. The at least one magnet may include springs, gas cylinders or the like (not shown) to maintain contact between the camshaft lobe and the permanent magnet. In this manner, the magnet will reciprocate back and forth with rotation of the camshaft. An electromagnet assembly 22 is secured beyond the end of the stroke of the at least one permanent magnet at a position to react with the permanent magnets 16 when energized in a controlled manner. A timing/firing system 100 is utilized to monitor rotation of the camshaft for causing the electromagnet assembly 22 to generate a magnetic field in response to camshaft position. The electromagnet assembly 22 and permanent magnets 16 are preferably configured so that a pushing force is created between the electromagnet assembly and the at least one permanent magnet. It should be appreciated that while only one permanent magnet, cam and electromagnet assembly are illustrated, the power generation device may include any number of assemblies which may operate independently or in combination with each other. It should also be appreciated, that while a cam and motor are illustrated other means of reciprocating the permanent magnet(s) may be substituted without departing from the scope of the invention. Such reciprocating means may include, but should not be limited to, solenoids, linear motors, pneumatics, hydraulics, diaphragms, springs, shape memory alloys and the like.

[0037] Referring to FIG. 3, another alternative embodiment of the present invention is illustrated. In this embodiment, the power generation system includes at least one permanent magnet 16 in an adjustable yet fixed position with respect to the electromagnet assembly 22. The at least one permanent magnet 16 is preferably secured to an adjuster assembly 302. The adjuster assembly 302 is secured behind the permanent magnet 16 for allowing positional adjustment of the permanent magnet in a linear path toward or away from the electromagnet assembly. The adjuster assembly 302 preferably includes a threaded shaft 304 having at least one lock nut 306 for adjusting the position of the permanent magnet. A timing/firing system 100 is utilized for causing the electromagnet assembly 22 to generate a magnetic field. The electromagnet assembly 22 and permanent magnets 16 are preferably configured so that a pushing force is created between the electromagnet assembly and the at least one permanent magnet. In at least one embodiment, a device may be secured between the adjuster assembly and one of the magnets to cause the magnet to vibrate or oscillate in a controlled manner whereby the poles of the magnets interact with each other during the oscillations. One non-limiting device suitable for providing the oscillations would be a piezoelectric crystal or a combination of piezoelectric crystals. The piezoelectric crystal(s) may be stimulated by an electrical current to ultrasonic levels thereby moving the magnet at the same oscillation level. It should be appreciated that while only one permanent magnet and electromagnet assembly are illustrated, the power generation device may include any number of assemblies which may operate independently or in combination with each other.

[0038] Referring to FIG. 4, a partial section view of an electromagnet assembly 22 suitable for use with the present invention is illustrated. The coil includes a central core 24 constructed of a ferromagnetic material suitable for creating a magnetic field. In a most preferred embodiment, the core is constructed of a material with high magnetic permeability and low coercivity and magnetostriction resulting in low hysteresis loss. In a most preferred embodiment, the core material is a cobalt-iron alloy approximately 50% cobalt and 50% iron. However, some alloys may contain about 49% cobalt, 49% iron with up to about 2% silicon, and trace amounts of manganese and/or niobium. Such material is sold under various trade names such as PERMENDUR, PERMENDUR 2V, HYPERCO 50, HYPERCO 50HS, and HYPERCO 50A. The core material should be annealed in a non-oxygen atmosphere to achieve large grain structure of the metal. In some embodiments, the core material may be magnetized prior to the anneal process. In other embodiments, the core material may be annealed within a magnetic environment. It should be noted that these materials while generally stable may be excited upon receiving an electrical or magnetic pulse at a natural frequency to enhance the production of electricity with the teachings of the present application. The Applicants have found various frequencies that significantly increase the production of electricity. One preferred frequency is about 10 kilohertz while an even more preferred frequency is about 37 kilohertz with a square wave form. Wrapped around the core is preferably a barrier layer 26 of DuPont KAPTON or some other well-known insulation. A plurality of wire wraps 28 extend around the core 24 to create the electrical field. In the preferred non-limiting embodiment about 752 turns in 16 layers of 12 gauge copper wire wrapped in high heat polymer insulation 26 to form a coil 28. The distal ends 30 and 32 of the coil wire extend outwardly from the coil for attachment to the timing/firing system. It should be noted that providing more wraps of wire will provide a larger magnetic field when energized and less wraps will provide a smaller magnetic field as is known in the art. It should also be noted that in some embodiments the core includes a length that is about twice as long as the coil 28. In these embodiments, the coil is preferably positioned close to one distal end of the core with the remainder of the core extending outwardly from the coil.

[0039] Referring to FIGS. 5-12, a wiring diagram showing one embodiment of the timing/firing system 100 is illustrated. It should be noted that the timing/firing system illustrated is for the embodiment illustrated in FIG. 1 having four electromagnetic coils, those skilled in the art will readily appreciate that the timing/firing system could be simplified for the embodiments illustrated in FIGS. 2 and 3. Those skilled in the art will also appreciate that additional coils could be added to the timing/firing circuit in the event that additional coils are utilized. The timing/firing system generally includes a low voltage power supply module 102, a high voltage supply module 104, a timing module 106, and a firing module 108. The low voltage power supply module 102 is comprised of a power inverter 110 and a plurality of power supplies 112, 114, 116, 118 having various output voltages for operation of the electronic components that make up the timing and firing modules 106, 108 respectively. The power inverter 110 preferably converts a 12V DC 120 supply of power to 120V AC 122, filtering and conditioning the 12V DC power to have a sine wave form. The converted power 122 is preferably supplied to four power supplies: a first 112 and a second 114 converting the 120V AC power 122 to 15V DC 124, a third 116 converting the 120V AC power to 12V DC 126, and a fourth 118 that converts 120V AC power to 5V DC 128. Because the high magnetic pulse flux that the timing/firing system is subject to can interfere with signaling and sensing functions, the inverter 110 and power supplies 112-118 redundantly filter and condition the power for supply to the other electronic components. This construction greatly reduces the possibility of transient spike anomalies that could cause premature firings, distorted timing, over currents, over voltage or even avalanche breakdowns that could cause electronic components to fail.

[0040] The high voltage system (HVDC) 104 is preferably a plurality of batteries 130 and capacitors 132. In a most preferred embodiment the array of batteries 130 comprises ten 12V DC batteries 134 hooked up in series to provide a total of 120V DC power 136 to the electromagnetic coils. The array of capacitors 132 preferably comprises about twelve 10,000 Pico Farad capacitors 138. The capacitors are generally constructed and arranged to smooth the draw on the batteries to provide extended run times, reduce heat build-up in the batteries 134 and provide a smoother power signal to the coils. The positive polarity of the battery array 140 connects to the line side of a single pole single throw switch which acts as the main power switch 142 and can either energize or shut down all of the 120V DC supplied components throughout the HVDC system. From the load side of the main power switch 142, the 120 v DC positive polarity is divided into two separate HVDC supply legs 144, 146. A first leg 144 connects to the collector 149 of the first insulated gate bipolar transistor (IGBT) 148 supplying power to coil bank 1 150, including coils 1 and 4 156, 158, while the second leg 146 connects to the collector 151 of the second IGBT 152 supplying power to coil bank 2 154, including coils 2 and 3 160, 162.

[0041] In a preferred embodiment, the first and second IGBTs 148, 152 are MITSUBISHI part no. CM1200DC 34N and are each rated at 1,700 Volts 1,200 Amps. The first and second IGBTs 148, 152 are configured to include dual switching (two channels) capability and can be operated either independently, in tandem, or in an alternating pattern. When two IGBTs are utilized, Channel one 164, 166 respectively of each IGBT provides independent switching of the coil banks 1 & 2. It should also be noted that while the preferred embodiment includes two IGBTs, more or less IGBTs may be utilized without departing from the scope of the invention. From the Channel one 164 emitter of the first IGBT 148 the 120 v DC power passes through blocking diode 168; and from the Channel 1 166 emitter of the second IGBT 152 the 120 v DC power passes through a blocking diode 170. Diodes 168 and 170 are preferably power diodes, VISHAY part no. SDIIOOC16 B-PUK, rated at 1400 Amp 1600 Volts. Diode 168 is connected to coil bank 1 150, and diode 170 is connected to coil bank 2 154. Diodes 168 and 170 prevent any back EMF caused by a failure in fly-back diodes 172 or 174 from reaching the first or second IGBTs.

[0042] Still referring to FIGS. 4-10, the main components of the timing system 106 are two RT-610-10 U-shaped photoelectric infrared sensors 176, 178. The infra-red sensors 176, 178 cooperate with timing disc 181 (FIG. 1) to provide timing with respect to position of the crankshaft 20, and thus pistons 12 to initiate energizing coil bank one 150 or coil bank two 154 and when to shutdown/de-energize coil bank one and/or coil bank two. In this manner the infrared sensors operate to specify duration for independent operation of the coil banks. A low voltage ON or OFF digital signal regarding the specific duration is sent to a respective low voltage power modulator and pulse controller 180, 182. In operation, each photoelectric infrared sensor 176, 178 senses rotation of the timing disc 181 signaling the respective power modulator and pulse controller 180, 182 when to send power to a respective IGBT 148, 152 to energize a respective coil bank 150, 154. The signal is preferably a 12 v DC signal of a specific duration via an EMF shielded cable to the respective true bypass (TB) opto-coupler 184, 186. In a most preferred embodiment, one RT-610-10, one Power Modulator and Pulse Controller and one opto-coupler are provided for each bank of cylinders. Providing independent pulse width modulators (PWM) to TB opto-coupler groups for each coil bank isolates possibility of failures from cascading and increases options for function configurations of the coil banks. Each respective low voltage power modulator and pulse controller 180, 182 functions to interface the timing/firing system 100 with the fiber optically interfaced IGBTs 148, 152. The power modulator and pulse controllers 180, 182 also convert the steady on/off digital signal received from the timing/firing module 100 to a signal that can be manually varied in duty cycle within the signal time frame/duration sent. The purpose is to reduce heat produced by the DC high voltage/amperage supply 104 to the IGBT switching components and the electromagnetic coils in their respective coil bank, to be able to manually vary the revolutions per minute (RPMs) of the motor 10 by reducing the effective voltage supplied to the electromagnetic coils 22 in their respective coil bank and to bring efficiency to the collection of back EMF. This is accomplished via a Pulse Width Modulator within the power modulator and pulse controllers. In operation, when the TB Opto-coupler components 184, 186 receive the shielded 12 v DC ON digital signal from the RT-610-10 U-shaped photoelectric infrared sensor 176, 178 it closes an opto-isolating switch 188, 190. This action allows a pulse width modulated 5 v DC signal mirroring in duration the signal sent by the RT-610-10 photoelectric infrared sensor 176, 178, that is electrically isolated from the RT-610-10 in the Timing/Firing system 100. Opto-isolating is used to fire-wall one part of the system from another, preventing problems caused by cascading avalanche breakdown, induced EMF, spikes, and voltage clips. The pulse width modulated 5 v DC signal powers a fiber optic transmitter 192, 194 on the TB Opto-coupler, converting the signal from a pulsed width modulated electrical signal to pulsed width modulated laser light signal. The pulsed width modulated laser light ON or OFF digital signal is sent via a fiber optic cable 196, 198 to the fiber optically interfaced IGBT Driver 200, 202 which in turn will open or close the IGBT controlling the high voltage DC power. It should be appreciated that because fiber optics are immune to the high magnetic flux environment, converting the pulsed electrical signal to a laser pulsed signal maintains very low attenuation and high integrity of the signal to maintain the integrity of the signal to eliminate the need for EMF shielding and give greater latitude to the range of pulse width that can be utilized. Thus, much higher pulsing can be employed, allowing system design options regarding back EMF that are excluded by standard hard-wired IGBT drivers.

[0043] Referring to the firing system 100, the Fiber Optically Interfaced IGBT Driver 200,202 is constructed and arranged to control the opening and closing of the IGBT gates, thus switching on or off the HVDC power to the coil banks. Power supplied to the IGBT driver board 200, 202 is a filtered and conditioned 15 v DC 0.5 Amp. via shield twisted pair wires 124 extending from power supplies 112, 114. The IGBT Driver 200, 202 is also constructed and arranged to include features that can be incorporated as torque power output IC Controller/Sensors that allow the shift from a push-push system between the electromagnets and the permanent magnets to a system that pushes on one coil bank while the other coil bank pulls (attracts) thus adding more torque to the power stroke. Shifting from a push-push mode to a push-pull mode may be accomplished on the fly.

[0044] High voltage DC switching is accomplished by two high voltage, high amperage insulated gate bipolar transistors (IGBT) 148, 152 and are preferably HVIGBT MODULES MITSUBISHI part no. CM1200DC 34N, each rated at 1700 volts 1200 amps. Each IGBT is controlled by a driver board 200, 202 that is fiber optically interfaced to a respective TB opto-coupler component 184, 186 located in the low voltage power modulator and pulse controller. Each IGBT gates power to a respective coil bank or cylinder independently of other IGBTs being utilized. Each electromagnetic coil bank 150, 154 preferably include a flyback diode 204, 206 across its positive and negative connection. It has been found that VISHAY part no. SDI500030L B-PUK is rated at 1600A 3000V diodes, and is suitable to eliminate flyback. Flyback is the sudden voltage spike seen across the inductive load presented by the coil banks when its supply voltage is abruptly changed by the systems pulsing and switching frequency. From each coil bank the high voltage DC continues through another isolation diode 208, 210, preferably VISHAY part no. SD1500030L B-PUK 1600A 3000V. Isolation diodes 208, 210 are to be considered legacy components; their primary function is to isolate the magnetic coil banks from one another. Isolation diodes 208, 210 connect to a common copper buss 212 which connects to the negative terminal of the high voltage DC 120V Power Supply battery array.

[0045] Referring to FIGS. 11 and 12, an alternative opto-isolator construction is illustrated. In this embodiment a timer circuit 222 and potentiometer 224 are included. With this arrangement, the firing window of the IGBTs can be broken into more than one pulse signal to allow additional control over the electromagnets and the power supply as illustrated in FIG. 12. This configuration allows an initial electrical impulse 226 followed by a second electrical pulse 228. Those skilled in the art will recognize that this construction allows the duty cycle of the electromagnets to be customized to a particular application. This construction also allows the duty cycle of the electromagnets to be altered based upon inputs from sensors, such as torque sensors, to reduce power consumption based on engine load. Other advantages include control over peak torque produced during the firing window which may include a lower duty cycle during the first portion of the firing window and a higher duty cycle during the second portion of the firing window.

[0046] Referring to FIG. 14, a screen-print from a dynamometer test conducted on the system illustrated in FIG. 1 is illustrated. As illustrated at Channel one 302, the system was coupled to a 250 volt DC power source. It can also be seen at Channels 8 304 and channel nine 306 that the coils 1 and 3, as numbered on FIG. 1 were taking in about 200 amps during operation. It can also be seen that at channel ten the voltage coming out of the device was at 400 volts DC and at channel six 5000 amps were coming out of the device during operation. It should be noted that this test was re-conducted by an independent team at the University of Alabama where very similar results were recorded. As is best understood at this time, there are at least two scientific explanations for the results seen in the testing. The first explanation is back EMF which can be captured for re-use in the battery or diverted for work. The second is thermo-electric power capture as a result of electron spin-flip transition. It is believed that this system utilizes at least one and more likely utilizes both of the back EMF and thermo-electric power capture.

[0047] The present system comprises a highly polarized permanent magnet (PM) 16 adjacent to or in close proximity to a metallic magnon gain medium (MMGM), e.g. the core 24. The magnetic field imparted on the adjacent MMGM forms a localized spin accumulation, also known as a spin bias, or accumulation of non-equilibrium electrons. Since the spin accumulation in the MMGM is greatest in close proximity to the magnet, a spin diffusion gradient is formed through the length of the MMGM. Due to the elements present in the MMGM and the Fermi energies associated with the elements within the MMGM, the spin diffusion gradient sets up a preferred direction for the movement of magnon waves in the MMGM (magnon bias). The coil 28 that surrounds the MMGM is energized; preferably with DC square wave pulses from the firing system 100. The DC pulses provide an EMF in the direction of the interface between the PM and MMGM. Since the PM has already exerted a magnetic field great enough to spin polarize electrons in the nearby MMGM, equilibrium electrons (the ones that have not been spin biased) within this spin diffusion zone are already under EMF from the PM that brings them close to the spin-flip transition point (as described by the Zeeman Effect and Paschen Back Effect). The introduction of DC pulsed current at specific frequencies, voltages and currents provides the extra current needed to accomplish the spin-flip transition so that electron pairs in equilibrium (equal spin up and spin down) become non-equilibrium and become spin polarized for the duration of the square wave pulse. This is known as the spin-flip transition, and it takes place in the MMGM when the coil is energized. Magnon waves are already present due to the ambient heat in the atmosphere, the room or any location where the power generation apparatus resides. Therefore, magnon waves are present in the MMGM since it is at approximately the same temperature as the environment surrounding it. By nature, magnon waves are randomly oriented and cause random lattice vibrations between the atoms in any solid, including the MMGM. Magnon waves are present in any material that is warmer than absolute zero. When the coil around the MMGM turns on, inducing a magnetic field with sufficient intensity to exceed the localized Zeeman energy or spin-flip transition energy for equilibrium electrons in the metal atoms in the MMGM, electrons in these become spin biased and absorb a magnon to conserve energy during the spin flip. Therefore, with sufficient current delivered to the coil, the MMGM can saturate causing the maximum number of electrons to become spin biased and absorb magnons in the MMGM. As the square wave pulse falls to zero thus de-energizing the coil, normal spin relaxation occurs within the MMGM allowing substantially all of the magnons absorbed to be released at the same time, as a large percentage of the electrons in the MMGM flip back to their original spin orientation. Since all the magnons are dumped at once, they create an avalanche effect much like photons in a laser. When all of these magnons waves are released at the same time they are released toward the permanent magnet due to the polarization force of the magnet creating a spin bias or gradient in the MMGM, thus creating a preferred direction for the magnons to travel when they are released. As the magnons saturate or overload the MMGM with magnon waves in one direction, they collide with the end of the material at the point where the MMGM ends and the PM is positioned (known as the interface). The collapse of the magnetic field and the magnon bias direction is responsible for annihilating magnon waves through wave collision at the interface. When the magnon waves are destroyed, heat is destroyed making the temperature of the material drop. Since energy cannot be created or destroyed per the laws of thermodynamics, the ambient heat energy that caused the original randomly moving magnons in the MMGT core is converted back to a forceful spin wave in the MMGT core. This spin wave is propagated through the MMGT core as a strong electromagnetic pulse that can be collected via classical induction by the coil around the MMGT core. Once collected, the electrical power can be stored and applied to perform useful work.

[0048] It has also been discovered during experimentation that the temperature of the electromagnet(s), core(s) and an external assembly operating from the power generated by the present device can be manipulated by the application of specific tones, generated by varying the square wave power inputs to the coils. In these experiments, the external assemblies comprised electrolysis systems being operated by the power generation device. In these combined systems, the present power producing device was equipped with various sensors including, but not limited to, temperature sensors, voltage sensors, amperage sensors, and pressure sensors. The sensors were secured to measuring and recording equipment including an Astro-Med R TMX-18 portable data recorder as well as various video devices directed at mechanical gauges and the reaction within the electrolysis tank. The TMX is available from Astro-Med Inc. of 600 East Greenwich Ave. West Warwick R.I. 02893. Sweeps of various square wave patterns were supplied to the power producing device. Thereafter, the data was analyzed whereby correlations were found between power production and temperature within the system. The tones, e.g. frequencies of the square wave which produced desirable cooling or power production were then fed back into the power producing device as a constant or narrow band sweep signal to increase the desired effect. During this process it was discovered that specific frequencies caused cooling in the electrolysis portion of the system while other frequencies caused cooling in the electromagnet coils and cores of the electromagnets. Due to the speed in which the heat was eliminated, it is believed that this phenomenon is due to magnon conversion and/or annihilation around that portion of the system. Temperature drops of one hundred degrees Fahrenheit were observed to occur in 1 to 2 seconds in the coils and cores which have an included mass of about 20 pounds.

[0049] Referring to FIGS. 1-15, one embodiment of the present device is illustrated. In this embodiment, the present power generation device 10 is provided with at least one and more preferably a plurality of tone detectors 302, at least one and more preferably a plurality of sensors 304 and a computer 106 in bi-directional communication with the controller 100 and having an algorithm to monitor the tone detectors 302 and sensors 304 and in response to the tone detector 302 and sensor 304 outputs modify the square wave pattern to cause temperature and/or power output parameters of the system. In a most preferred embodiment, the power generation device 10 is connected to an external assembly, such as an electrolysis device 310 or Low Energy Nuclear Reaction (LENR), which is also provided with sensors 304 and tone detector(s) 302. In this manner, temperature and performance of the power generation device and the external assembly 310 can be manipulated and controlled for a desired result. The computer algorithm would compare power production to temperature and either provide a constant tone to the system or cycle various tones of the square waves to the system to balance power production and temperature of the components.

[0050] This system also has application for driving fusion and/or LENR reactions which are extremely prone to runaway heat related failures. The present system can be utilized to cool or throttle the fusion or LENR reaction in the same manner as the electrolysis reaction to prevent the unwanted runaway failures related to excessive heat production. In operation, the system can monitor the heat production of the fusion or LENR reactions and vary the frequency of the pulse being supplied to the coil(s) assembly to provide a periodic or constant cooling cycle to the reaction. The excess heat is converted to electrical power which can be directed away from the system for useful work or can be redirected into the system for use by the reaction. The present system may also have application for refrigeration and heating systems whereby the power generation could be utilized for heat while the magnon conversion/destruction could be utilized for cooling or refrigeration.

[0051] All patents and publications mentioned in this specification are indicative of the levels of those skilled in the art to which the invention pertains. All patents and publications are herein incorporated by reference to the same extent as if each individual publication was specifically and individually indicated to be incorporated by reference.

[0052] It is to be understood that while a certain form of the invention is illustrated, it is not to be limited to the specific form or arrangement herein described and shown. It will be apparent to those skilled in the art that various changes may be made without departing from the scope of the invention and the invention is not to be considered limited to what is shown and described in the specification and any drawings/figures included herein.

[0053] One skilled in the art will readily appreciate that the present invention is well adapted to carry out the objectives and obtain the ends and advantages mentioned, as well as those inherent therein. The embodiments, methods, procedures and techniques described herein are presently representative of the preferred embodiments, are intended to be exemplary and are not intended as limitations on the scope. Changes therein and other uses will occur to those skilled in the art which are encompassed within the spirit of the invention and are defined by the scope of the appended claims. Although the invention has been described in connection with specific preferred embodiments, it should be understood that the invention as claimed should not be unduly limited to such specific embodiments. Indeed, various modifications of the described modes for carrying out the invention which are obvious to those skilled in the art are intended to be within the scope of the following claims.