OA16330A - System and method for separating fluids and creating magnetic fields. - Google Patents

Abstract

A system and method in at least one embodiment for separating fluids including liquids and gases into subcomponents by passing the fluid through a vortex chamber into an expansion chamber and then through at least a portion of a waveform pattern present between at least two rotors and/or disks. In further embodiments, a system and method is offered for harnessing fields created by a system having rotating rotors and/or disks having waveform patterns on at least one side to produce current within a plurality of coils. In at least one embodiment, the waveform patterns include a plurality of hyperbolic waveforms axially aligned around a horizontal center of the system.

Description

SYSTEM AND METHOD FOR SEPARATING FLUIDS AND CREATING MAGNETIC FIELDS provisional Application Serial No. 61/376,438, [0001] This application ciaims the benefit of U.S.

fîled August 24, 2010 and U.S. patent Application Serial No. 13/213,452, filed August 19, 2011, which are hereby incorporated by reference.

fhod of at least one embodiment of the présent uctures and dynamics that may be used to

I. Field of the Invention [0002] The présent invention relates to a system and method for processing a fluid to dissociate fluid in one or more embodiments and for dissocUiting components of the fluid in one or more embodiments. More particularly, the system and me invention provides rotating hyperbolic waveform st controllably affect the fundamental properties of fluids and/or fields for séparation of gases and/or power génération.

adsorbent becomes saturated, the adsorbent is is continued development work in improving the

II. Background of the Invention [0003] Current gas séparation Systems for the production of industrial gases using air séparation rely on pressure swing adsorption (PSA) and vacuum pressure swing adsorption (VPSA) processes, ln both of these processes, compressed air is pumpcd through a fixed bed of adsorbent that absorbs one of the main constituents contained in the compressed air resulting in a stream of air containing the non-adsorbed constituents for collection. As the purged and the discharged gas is collected. There efficiencies of these processes both in terms of prodi ction and power requirements.

[0004] ln Systems that make use of a vortex tube, point along the height of the vortex tube to allow for l ghter particles to flow up and heavier particles to drop. Typicalîy, the vortex created is using mechanical forces within the vortex tube.

[0005] Power génération Systems typicalîy include magnets. Either the coils or the magnets are preser t on the rotor with the other présent on the stator. Electrical power is generated from the création of a rotor. The rotor îs typicalîy rotated with the use of n rising steam, and blowing wind.

the gas being separated is inlet into the tube at a a rotor and stator and include a set of coils and magnetic field in the coils from the rotation of the lechanical forces from, for example, falling water,

III. Summary of the Invention ln at least one embodiment, this invention provides a system including a housing having at mmunication with the at least one feed inlet; a distribution chamber; at least one coil array in rm disks; at least one rotating disk rotatable about [0006] least one feed inlet, a vortex chamber in fluid cc plurality of waveform disks in fluid communication \ /ith the vortex chamber, the plurality of waveform disks forming an axially centered expansion and magnetic communication with the plurality of waveft i the housing, wherein the disk includes an array of nagnets; and a drive system engaging the plurality of waveform disks.

[0007] In at least one embodiment, this invention driving a plurality of disks having mating waveform: s, feeding a fluid into a central chamber defined by openings passing through a majority of the plurality of disks with the fluid flowing into spaces formed provides a method for generating power including between the disks to cause the fluid to dissociate into separate components, and inducing current flow through a plurality of coils residing in a magnetic field created between the waveform disks and at least one magnet platform rotating through magnetic cbupling with the waveform disks.

Brîef Description ofthe Drawings

IV.

[0008] The présent invention is described with reference to the accompanying drawings. In the drawings, like reference numbers indicate identical or functionally similar éléments. The use of crosshatching and shading within the drawings is not intended as limiting the type of materials that may be used to manufacture the invention.

[0009] FIG. 1 illustrâtes a block diagram in accorde nce with présent invention. FIG. 2 illustrâtes a top view of an embodiment according to the invention system illustrated în FIG. 2 taken at 3-3. FIG. 4 illustrâtes an exploded and partial cross-sectional view of the system illustrated in FIG. 2. FIG. 5 illustre tes a partial cross-sectional view of the system illustrated in FIG. 2. !

[0010] FIGs. 6A and 6B illustrate side and perspective views of another embodiment according to the invention.

[0011] [0012] [0013]

FIG. 3 illustrâtes a cross-sectional view of the pack turbine according to the invention.

FIG. 12 illustrâtes a top view of another eyibodiment according to the invention. FIG. 13 12. FIG. 14 illustrâtes a cross-sectional view of

FIGs. 7A and 7B illustrate an example disk-f ack turbine according to the invention.

FIGs. 8A-8C illustrate another example diskFIG. 9A illustrâtes a side view of another e nbodiment according to the invention. FIG. 9B illustrâtes a top view of the system illustrated in FIG. )A. FIG. 9C illustrâtes a partial cross-section of an embodiment according to the invention take at EC-9C in FIG. 9B. FIG. 10 illustrâtes a crosssectional view of the embodiment taken at 10-10 in FIG. 9B. FIG. 11 illustrâtes a cross-sectional view ofthe embodiment taken at 11-11 in FIG. 9B.

[0014] illustrâtes a side view of the system illustrated in FIG. the system illustrated in FIG. 12 taken at 14-14 in FIG. 12.

.sk-pack turbine according to the invention, bodiment according to the invention, bodiment according to the invention, bodiment according to the invention, sk-pack turbine according to the invention, ther example disk according to the invention.

[0015] [0016] [0017] [0018] [0019] [0020] [0021] [00221 [0023] évident to a person of ordinary skill in the art.

FIGs. 15A-15D illustrate another example di

FIG. 16 illustrâtes a side view of another erril

FIG. 17 illustrâtes a side view of another err I

FIG. 18 illustrâtes a side view of another en

FIGs. 19A-19E illustrate another example d :

FIG. 20 illustrâtes a perspective view of ancl

FIG. 21A-21D illustrate another example dii k-pack turbine according to the invention.

FIG. 22 illustrâtes another example disk-pack turbine according to the invention.

Given the following enabling description of the drawings, the invention should become

V. Detailed Description of the Drawings [0024] The présent invention, in at least one emltodiment, provides a highly efficient system and method for processing fluid to harness the energy contained in the fluid and the environment and/or to dissociate éléments of the fluid. In order to accomplish the results provided herein, in at least one ' embodiment the présent invention utilizes élégant, tjighly-specialized rotating hyperbolic waveform structures and dynamics. it is believed these rotating hyperbolic waveform structures and dynamics, in at least one embodiment, are capable of efficient|y propagating at ambient température desired effects up to the fifth state of matter, i.e., the etheric/particle state, and help accomplish many of the functional principles of at least one embodiment of the présent invention. More particularly, in at least one embodiment, the system of the présent invention is capable of producing very strong field energy at ambient températures while using relatively minimal input energy to provide rotational movement to the waveform disks. As will be more fully developed in this disclosure, the waveform patterns on facing disk surfaces form chambers (or passageways) for fluid to travel through including towards the periphery and/or center while being exposed to a compress, expand and/or change direction and/or rotation of the fluid particles.

[0025] biaxial forms, variety of pressure zones that, for example, are not limited to, circular, sinusoïdal, biaxial,

In this disclosure, waveforms include, but sinucircular, a sériés of interconnected scallap shapes, a sériés of interconnected arcuate hyperbolic, and/or multl-axial including con binations of these that when rotated provide progressive, disk channels with the waveforms being substantially centered about an expansion chamber. The waveforms are formed by a plurality grooves, and dépréssions (or descending waveform!.

having different heights and/or depths compared to other features and/or along the individual features. In some embodiments, the height in the radius of the disk chambers vary along a radius as embodiments, the waveforms are implemented as ri lges that hâve different waveforms for each side (or face) of the ridge. In this disclosure, waveform p; itterns (or geometries) are a set of waveforms on one disk surface. Neighboring rotor and/or disk suri aces hâve matching waveform patterns that form a channel running from the expansion chamber te matching waveforms include complimentary wavef irms, mirroring geometries that include cavities and other bénéficiai géométrie features. FIGs. 3-5, illustrate a variety of examples of these waveforms.

[0026] In this disclosure, a bearing may take between components with examples of material ceramîcs, nylon, phenolics, bronze, and the like. Es bushings and bail bearings.

[0027] In this disclosure, examples of non-cond jeting material for electrical isolation include, but are not limited to, non-conducting ceramîcs, phstics, Plexiglass, phenolics, nylon or similarly electrically inert material. In some embodiments, component to provide the electrical isolation.

[0028] In this disclosure, examples of non-magnetic (or very low magnetic) materials for use in housings, plates, disks, rotors, and frames include, brass, brass alloys, stainless steel such as austen alloys, bismuth, bismuth alloys, magnésium alloys, non-magnetic materials for use in bearings, space rs, and tubing include, but are not limited to, inert ¹ of ridges (or protrusions or rising waveform s), .) in the waveform surface including the features vertical axis and/or the depth measured along a illustrated, for example, in FIG. 15D. In some the periphery of the disks. In this disclosure,

7A-7B, 8B, 8C, 9C-11, 14, 15B-15D, and 19A-22 a variety of forms while minimizing the friction for a bearing including, but are not limited to, amples of bearings include, but are not limited to, the non-conducting material is a coating over a , but are not limited to, aluminum, aluminum alloys, i tic grade stainless steel, copper, beryllium-copper silver, silver alloys, and inert plastics. Examples of liquide and gases for applications such as ig and rendering of pure and complex gases, plastics, non-conductive ceramics, nylon, and phenolics.

[0029] In this disclosure, examples of diamagnel|ic materials include, but are not limited to, aluminum, brass, stainless steel, carbon fibers, coppefl, magnésium, other non-ferrous material alloys some of which containing high amounts of bismuth relative to other metals.

[0030] The présent invention in at least one embodiment provides a novel approach to the manipulation and hamessing of energy and matter, resulting in, for example: (a) Systems and methods for economical, efficient, environmentally positive séparation, expansion, dissociation, combination, transformation, and/or conditioning of dissociation of water for energy, elemental restructuri and the production of highly energetic gases for dire ct, dynamic application: and (b) Systems and methods for the production, transformation, and/or eonversion of mass/matter to highly energetic eiectrical, magnetic, diamagnetic, paramagnetic, kine'ic, polar and non-polar fluxes and fields. The présent invention provides, in one or more embodimerts, Systems and methods that are bénéficiai for electrical power génération.

[0031] The Systems and methods of the présent in mention in at least one embodiment include an intake chamber and a disk-pack turbine having an expansion and distribution chamber (or expansion chamber) in fluid communication with the intake chamber, and disk chambers formed between the rotors and/or disks that form the expansion chamber e chamber serves to draw charging media, i.e., liquids < ii as fluid or media or “material) into the System expansion chamber. The expansion chamber is foimed by two or more stacked rotatable rotors The stacked rotatable rotors and/or disk(s) are aligned whereby the aligned openings form the include a variety of shapes, ranging from a egrees of converging and diverging structures, chamber includes both a convergent structure and then expand the media. The disks in at s illustrated, for example, in FIG. 1. The intake ind/or gases (hereinafter collectively referred to before passing the charging media into the and/or disks having an opening in their center. centered axially such that one or more openings are expansion chamber. The expansion chamber may horizontal substantially cylindrical shape to varying d However, in at least one embodiment, the expansion and a divergent structure designed to first compress least one embodiment also include one or more patterns of waveform structure which may be highly application spécifie. In an alternative embodiment, the System draws in fluid from the periphery in addition or in place of the intake chamber.

[0032] In some embodiments the intake chamber that créâtes a vertical vortex in the charging media, liquid and/or gas, in order to impart desired physical characteristics on the fluid. Examples of how the charging media is provided include ambient air, pressurized supply, and metered flow. The vertical vortex acts to shape, concentrate, and accelerate th 3 charging media into a through-flowing vortex, thereby causing a decrease in température of the charging media and conversion of heat into kinetic energy. These effects are realized as the charging η i< as it is drawn into the expansion chamber by the centrifugal suction/vacuum created by the dynamic rotation and progressive geometry of the disks. The vortex also assists the fluid in progressing through the System, i.e., from the vortex induction chamber, into the expansion chamber, through the y/ * may be formed as a vortex induction chamber which in most embodiments is a fluid including ledia is first compressed, then rapidly expanded disk chambers formed by the patterns and channels icreated by the waveforms such as hyperbolic waveforms on the disks, and out of the system. In some embodiments. there may also be a reverse flow of fluid within the system where fluid comporjents that are dissociated flow from the disk chambers to the expansion chamber back up (i.e.,| flow simultaneously axially and peripherally) through the vortex chamber and, in some embodiments, out the fluid intakes. Media (or material) tends toward being divided relative to mass/specific gravity, with the lighter materials discharging up through the eye of the vortex while simultaneously discharging gases/fluids of greater mass at the flows of fluid as the fluid progresses over the the incorporation of geometries as well as to supplément and intensify desired energetic periphery. While progressing through the waveform geometries, the charging media is exposed to a multiplicity of dynamic action and reactionary forces and influences such as alternating pressure zones and changing circular, vortex and multi-axial valleys and peaks and highly variable hyperbolic and/ir non-hyperbolic geometries.

[0033] The number and arrangement of disks can i ary depending upon the particular embodiment. Systemic effects may be selectively amplified by complimentary components and features that serve influences such as sympathetic vibratory physics (harmonie, sympathetic and/or dissonant, electrical charging, polar différentiation, spécifie component Isc lation, i.e., electrical continuity, and magnetismgenerated fixed/static permanent magnetic fields, magnetic fields, etc.). Examples of the various dibk arrangements include paired disks paired disks, stacked disks, pluralities of stackec combinations of these disk arrangements as illustrai i 11,15D, 19E, and 22. Further examples add one or complété assembly with rotors and/or disks being e one embodiment, the bottom rotor (or disk) includes a parabolic/concave rigid feature that forms the bottom of the expansion chamber.

[0034] As the highly energized charging media passes from the vortex induction chamber into the expansion chamber, the charging media is divided ai on the stacked disks. Once within the rotating numerous energetic influences, including sinusoïdal, with simultaneous centrifugal and centripetal dynariics. See, e.g., FIGs. 5. These dynamics in at Ieast one embodiment include a multiplicity of multi-axial high pressure centrifugal flow zones and low pressure centripetal flow zones, the majority of whic, j are vortexual in nature.

a. Overview [0035] FIG. 1 provides a broad overview of an invention.

components of the various embodiments of the pre below. The system as illustrated in FIG. 1 includes and a disk-pack module 200 having an expansion 252 and a disk-pack turbine 250. To simplify the pack turbine 250 îs not included in FIG. 1. The e>:| the recess présent in the rotors and/or disk(s) that permanent dynamic magnetic fields, induced multiple various disks, multi-staged disk arrays, and ed, for example, in FIGs. 3, 7A, 8A-8C, 9C, 10, more rotors to the disks. A disk-pack turbine is a ements within the disk-pack turbine. In at Ieast ii îd drawn into channels created by the waveforms waveform patterns, the media is subjected to tortile, and reciprocating motions in conjunction example of a system according to the présent a basis for understanding the principles and

This overview îs intended to providi i sent invention that will be discussed in more detail i an intake module 100 with an intake chamber 130 and distribution chamber (or expansion chamber) discussion, the optional housing around the diskpansion chamber 252 is formed by openings and form the disk-pack turbine 250. See, e.g., FIGs. 3 up and 4. The rotatable rotors and/or disks are stacked or placed adjacent to each other such that a small space of séparation remains between the adjacent members to form disk chambers. The intake chamber 130 is in fluid communication with the expansion chamber 252. A drive system 300 is connected to the disk-pack turbine 250 to provide rotational movement to the disk-pack turbine 250. [0036] The drive system 300 in at least one embodiment is connected to the disk-pack turbine 250 through a drive shaft 314 or other mechanical linkage 316 (see, e.g., FIGs. 4 and 6A) such as a belt, i-s and/or disks in the disk-pack turbine 250. In Us a centrifugal suction or vacuum within the ambers 262 and in some embodiments back embodiment, components of the fluid reverse and in a further embodiment the drive System 300 is cpnnected directly to the disk-pack turbine 250. In use, the drive System 300 rotâtes the plurality of roto at least one embodiment, the rotation of which créai system that causes a charging media to be drawn intd the intake chamber 130 via inlets 132 and in further embodiments the fluid is drawn in from a periphery of the disk-pack turbine 250.

[0037] The intake chamber 130 concentrâtes (compresses) and passes the charging media into the expansion chamber 252. The expansion chamber 21 i2 causes the compressed charging media to quickly expand and distribute through the disk chambers 262 and over the surfaces of the disk-pack turbine members towards a periphery via the disk et towards the expansion chamber 252. In at least one course through the system, for example, lighter elemer ts présent in the fluid that are dissociated from heavier éléments présent in the fluid. In at least one embodiment, the system includes a capture system for one or more of the dissociated fluid elemer ts. See, e.g., FIGs. 6A and 6B. The media is conditioned as it passes between the rotating disks from the center towards the periphery of the disks. In at least one embodiment, the intake chamber 130 is omitted.

b. Fluid Conditioning

FIGs. 2-4 provide various views of an example embodiment of the présent invention that is the conditioning, separating, dissociating, a id/or transforming Iiquids, gases and/or other FIGs. 2 and 3 illustrate an embodiment of he fluid conditioning system according to the [0038] useful in ber) 130 and a disk-pack module 200 with a source of the charging medium provided to the is. 3 and 4 is around the disk-pack turbine 250 matter.

présent invention. In accordance with this embodimènt, the system includes a fluid intake module 100 with a vortex induction chamber (or vortex cham housing 220, and a disk-pack turbine 250 with an expansion and distribution chamber (or expansion chamber) 252. The fluid intake module 100 acts as a disk-pack module 200.

[0039] Charging media enters the vortex chamber 130 via fluid inlets 132. The fluid inlets 132 may also be sized and angled to assist in creating a vortex in the charging media within the vortex chamber 130 as illustrated, for example, in FIG. 2. The vortex chamber 130 provides the initial stage of fluid processing. The housing 220 illustrated in FIGi and is an example of how to collect fluid components t lat exit from the periphery of the disk chambers 262.

[0040] FIGs. 3 and 4 illustrate, respectîvely, a crosi conditioning system in accordance with an embodiment illustrated in FIG. 2. The housing 220 around the disk-pack turbine 250 provides an enclosure in wh ch the disk(s) 260 and rotors 264, 266 are able to rotate. The following disclosure provides an exan· pie of how these modules may be constructed y/

-section view and an exploded view of the fluid and assembled.

[0041] The fluid intake module 100 includes a vortlex chamber (or intake chamber) 130 within a housing 120 having fluid inlets 132 in fluid inlets in at least one embodiment are sized and angled to assist in creating a vortex in the charging medium within the vortex chamber 130. The vortex chamber 130 is illustrated as including an annular mounting collar 125 having an opening 138. The collar 125 allows the intake chamber 130 to be connected in fluid communication with the expansion vrith the vortex chamber 130. The fluid exits from 252. The expansion chamber 252 as illustrated lower rotor (or lower disk) 266 in the disk-pack center holes in the stacked disks 260 and an are multiple expansion chambers within the disktigid feature 2522. See, e.g., FIGs. 9 and 10 and disk(s) 260 and rotors 264, 266 are stacked or ice of séparation remains between the adjacent the charging media will enter from the expansion waveforms 261 that are complementary between i FIGs. 8A-8C, 15A, and 15B. In at least one ong any radius extending from a start of the chamber 252. The fluid intake module 100 sits above the disk-pack module 200 and provides the initial stage of fluid processing. In at ieast one embodiment, the vortex chamber 130 is stationary in the System with flow of the charging media through i driven, at least in part, by rotation of the diskpack turbine 250 présent in the housing 220. In anoiher embodiment, a vortex is not created in the charging media but, instead, the vortex chamber 130 sets as a conduit for moving the charging media from its source to the expansion chamber 252.

[0042] The disk-pack module 200 includes at leas¹ one disk-pack turbine 250 that defines at least one expansion chamber 252 in fluid communication the vortex chamber 130 into the expansion chamber is formed by a rigid feature 2522 incorporated into a turbine 250 with the volumétrie area defined by th£ upper rotor 264. In at least one embodiment, there pack turbine each having a lower disk 266 with the the next section of this disclosure.

[0043] As illustrated, the disk-pack turbine 250 indiudes an upper rotor 264, a middle disk 260, and a lower rotor 266 with each member having at lei st one surface having a waveform pattern 261 présent on it. The illustrated at least one rotatable placed adjacent to each other such that a small spb disk/rotor to form disk chambers 262 through which chamber 252. The disk chambers 262 are lined with adjacent rotor/disk(s) as illustrated, for example, i i embodiment, the waveforms include no angles t fl waveform pattern to the end of the waveform pattern. In FIG. 4, the illustrated waveform patterns 261 are a sériés of concentric circles, but based on concentric circles can be replaced by other patternb discussed in this disclosure and depicted in the figures. The illustrated rotors 264, 266 and disk(s) 260 are spaced from each other to form disk chambers 262 between them that are in fluid communication with the expansion chamber 252. One way to space them apart is illustrated in FIGs. 3 an 1 4, where impellers 270 such as ceramic spacers are used to separate them and also to interconiect them together so that they rotate together. Alternative materials besides ceramics that would v ork include materials that do not conduct electrical current to electrically isolate the illustrated rotors a id disk from each other and the System. In further embodiments one or more of the upper rotor 264, electrically connected. Another way they may be to support bolts running between the top and lowçr rotors 264, 266. The illustrated lower rotor 266 ></ ‘ his discfosure it should be understood that the , the middle disk 264, and the lower rotor 266 are separated is using support pièces fixedly attached includes a parabolic/concave rigid feature 2522 that forms the bottom of the expansion chamber 252.

In an alternative embodiment, the rotors 264, 266 i and the diskfs) 260 are attached on their périphéries. I

In the illustrated embodiment, the upper rotor

226 to engage the drive shaft 314. The lower rotor 264 and the lower rotor 266 include a îesting hole is defined by a periphery wall with is passlng over its surface. As the center disk

264, 266, the disk chambers 262 will be in

The resultîng motion in at least one of the disk-pack turbine components may be at désirable frequencies from sources 320.

electrical charges to rotating disk-pack turbine means of affecting a polar fluid, i.e., when it is [0044] The upper rotor 264 and the lower rotor 266 include shoulders 2642, 2662 extending from their respective non-waveform surface. The upper rotor 264 includes a raised shoulder 2642 that passes through an opening 2222 in the upper case 222 of the disk-pack module 200 to establish a fluid pathway connection with the intake chamber 130.

shoulder 2642 is ringed by a bearing 280 around it that rests on a flange 2224 of the upper case 222 and against the inside of the collar 125 of the intake chamber housing 120. The lower rotor shoulder 2662 passes through an opening 2262 in a lower case rotor shoulder 2662 is surrounded by a bearing 280 that rests against the flange 2264 of the lower case 226. In an alternative embodiment, the upper nesting hole for receiving a waveform disk where the gaps for receiving a connection member of the wavefoilm disk. See, e.g., FIG. 15D.

[0045] In at least one embodiment, the center disk Î 60 will begin to resonate during use as it spins around the central vertical axis of the system and fluid 260 resonates between the upper and lower rotors constant flux, creating additional and variable zones of expansion and compression in the disk chambers 262 as the middle disk resonates between tne upper and lower rotors 264, 266, which in at least one embodiment results in varied exotic me lion.

embodiment is a predetermined résonance, sympathy, and/or dissonance at varying stages of progression with the frequency targeted to the frequer cy of the molecules/atoms of the material being processed to manipulate through harmonics/dissonant e of the material.

[0046] In at least one embodiment, one or more prepared/equipped with a capacity for the inductioh of specifically selected and/or differentiated electrical charges which may be static or pulsed

Examples of how electrical charges may be delivdred to spécifie components include electrical brushes or electromechanical isolated devices, ind jetion, etc., capable of delivering an isolated charge to spécifie components such as alternately chargîng disks within a rotor with opposite/opposing polarities. In addition to inducing components, electrical chargîng can also be a useful désirable to expose a subject chargîng medium to opposing attractive influences or, in some cases, pre-ionization of a fluid. For example, passing in-flo pre-excitation of molecular structures prior to entry ir i into the expansion and distribution chamber may enhai [0047] The housing 220 includes a chamber 230 illustrated in FIGs. 3 and 4, the housing chamber 230

250 in at least one embodiment hâve complementary surfaces. The illustrated housing 220 includes the upper case 222, the bottom case 226, and a pi ripheral case 224. The illustrated housing 222 also includes a pair of flow inhibitors 223, 225 attac i/ving media through a charged ion chamber for to the vortex chamber, followed by progression ince dissociative efficiencies.

in which the disk-pack turbine 250 rotâtes. As and the outside surface of the disk-pack turbine ied respectively to the upper case 222 and the yy bottom case 226. Based on this disclosure, it should be appreciated that some components of the housing 220 may be integrally formed together as one piece. FIG. 3 also illustrâtes how the housing 220 may include a paraboloid feature 234 for the chamber 230 in which the disk-pack turbine 250 rotâtes. The paraboloid shape of the outside surface of the disk-pack turbine 250, in at ieast one embodiment, assists with obtaining the harmonie frequency of the rotors 264, 266 and disk(s) 260 themselves as they spin in the chamber 230, thus increasing the dissociation process for the fluid passing through the system. In at least one embodiment, the rotors 264, 266 hâve complementary outer faces to the shape of the chamber 230.

[0048] The upper case 222 includes an opening 2122 passing through its top that is aligned with the opening in the bearing 280. As illustrated in FIGi. 3 and 4, a bearing 280 is présent to minimize any friction that might exist between the shoulder 264 ï of the top rotor 264 and the housing collar 125 and the upper case 222. The bearing 280, in at least one embodiment, also helps to align the top 2524 of the expansion chamber 252 with the outlet lower case 226 includes an opening 2262 passing th that surrounds the shoulder (or motor hub) 2662 of th< ! lower disk 266.

[0049] The peripheral case 224 includes a plur ality of discharge ports 232 spaced about its perimeter. The discharge ports 232 are in fluid communication with the disk chambers 262. The flow inhibitors 223, 225 in the illustrated system, in at least one embodiment, assist with routing the flow of fluid exiting from the periphery of the disk-pack turbir n points) 132 in the housing 220. In at least one embodiment, there is a containment vessel 900 (see, e.g., FIGs. 6 and 7) around the housing 220 to collée the discharged gas from the system.

[0050] Additional examples of electrical isolation The drive system/spindle/shaft is electrically isolated conductive material, which créâtes discontinuity betJ/een the drive shaft and ground. In at least one embodiment, ail disk-pack turbine components are electrically isolated from one another utilizing, for example, non-conducting tubes, shims, bushings, isolation rings, and washers. The main feed tube (or intake chamber) is also electrically isolated from the top rotor via the use of an additional isolation ring. The feed tube and support structure around tie system are electrically isolated via the use of additional isolation éléments such as nylon bolts.

between any components, from drive shaft progress ng upward through ail rotating components to the top of the vortex chamber and support structures.

continuity is désirable as described previously.

[0051] into a through-flowing vortex that serves to accumli charging media as it is drawn into the expansion chamber 252 by centrifugal suction. As the rotating compressed charging media passes through the base opening 138 of the vortex chamber 130, it rapidly expands as it enfers into the revolving exp insion chamber 252. Once within the expansion chamber 252, the charging media is further acceler ited and expanded while being divided and drawn by means of a rotary vacuum into the waveform dis k channels 262 of the rotors 264, 266 and disk(s) 260 around the expansion chamber 252. While progressing through the waveform geometries of the^i

138 of the vortex chamber 130. Likewise, the wgh its bottom that is lined with a bearing 280 ie 250 towards the discharge ports (or collection components include the following approaches. via the use of a large isolation ring made of nonIn most cases, there is no electrical continuity

There are, however, occasions when electrical

In at least one embodiment, the vortex chamber 130 shapes the inflowing charging media ulate, accelerate, stimulate, and concentrate the rotors and disks around the expansion chamber 252, the charging media is exposed to a multiplicity of dynamic action and reactionary forces and influentes which work in concert to achieve desired outcomes relative to conditioning, séparation, and/or transformation of liquide and gases and/or other matter.

the bonds between atoms in at least one [0052] FIG. 5 illustrâtes a partial cutaway view of the embodiment illustrated in FIGs. 2-4. FIG. 5 provides an example of the fluid flow dynamics within the disks in accordance with the présent invention. Waveforms channels are formed in the disk chambers 262 by the géométrie patterns 261 on the rotors 264, 266 and disk(s) 260. FIG. 5 illustiates how stepped waveform harmonies cause high and low pressure zones to form in the channels with the circulation of the flow illustrated from the top to the bottom of the zones by the C’s (clockwise) and backward C’s (counterclockwise) that reflect the circulation. These pressure zones and fertile reci irocating motion allow the charging media and material to flow within the channels and to break embodiment. As the disk-pack turbine 250 rotâtes thf charging media within the expansion chamber 252, the charging media flows from the center ofthe disk-packturbine 250 through the disk chambers 262 towards the periphery of the disk-pack turbine 2!>0. As the charging media passes through the disk chambers 262 the media is conditioned, separited, dissociated, and/or transformed based on controllable variables such as construction material;, progressions, waveform diameters, disk stack densitie ! media composition.

[0053] FIGs. 6A and 6B illustrate an embodiment 904, 906, 908 for further separating gases based containment vessel 900 that encloses the disk-pack motor 310A driving the driveshaft 312A with a belt 3l6A and a work surface (or bench/platform) 910. The illustrated embodiment shares some similarities with the previous embodiment including the presence of an intake module 100A with an intake 13 [0054] The illustrated System includes at least five the System. Extending out from the containment vesiel 900 is a séparation conduit 902 that branches twice into a first branch conduit 904 and a second b anch conduit 906. The first branch conduit 904 provides three points at which fluid may be withdrawi The second branch conduit 906 leads to valve 933.

branch conduit 908 that leads to valve 934. Based the séparation conduits can take a variety of forms and 6B. The gases (or fluids) are separated în at following: spécifie gravity, exit velocity, opposite-atti actors installed along the conduit or proxîmate to a valve, electric and/or magnetic for matter with positive/negative or North/South polar prédominance, (n at least one embodiment the waveform disks illui trated in FIGs. 7A and 7B were used to in a gas séparation designed System. In at least one embod illustrated in FIGs. 7A and 7B were rotated between 3,680 and 11,000 RPM that hydrogen was separated out from environ mental air.

[0055] FIG. 7A illustrâtes a pair of disks 260Z insialled in a top rotor 264Z and a bottom rotor 266Z, Ύ , waveform geometry, tolérances, numbers of s, internai and external influences and charging liavîng a plurality of gas collection conduits 902, on weight. The illustrated System includes a nodule 200A. Also illustrated is an example of !A and a disk-pack module 200A.

joints for removal of gas and other material from from the System through valves 930, 931, 932. xtending from the intake module 100A is a third on this disclosure, it should be appreciated that other than those that are illustrated in FIGs. 6A least one embodiment using at least one of the ment, it was found that when the waveform disks respectively, that hâve been found to be bénéficiai for a gas séparation embodiment. The illustrated disks 260Z include matched waveform patterns with two sets of hyperbolic waveforms 2642Z and three sets of substantially circular waveforms 2646Z. FIGs. 7A and 7B illustrate an alternative embodiment that includes exit ports including multiple convergent exit ports 2649Z and multiple divergent exit ports 2648Z that pair together to form convergent/divergent ports. FIG. 7B illustrâtes an reduction/diminishing flow tolérances for the , molecularly reorganized charging media for testing session with a system built according to nd the disk-pack module 200A illustrated in FIG.

content in the air, itself, was being dissociated, example of a waveform changing height as it travels around the disk (2611Z represents the low level and 2612Z represents the high level). FIG. 7B illustrâtes an example of how the waveforms may vary in width (2613Z represents a wide segment and 26142 represents a thinner segment).

[0056] For various applications, it may be désirât le to hâve an internai geometry conducive to hyper-expansion of the charging media followed b) purpose of compression or reconstitution of the charging media. This secondary compression cycle is useful for producing concentrated, highly energetic applications such as fuel formulation.

[0057] One cool, moîst morning prior to starting a the invention similar to the fluid intake module 100A £ 6A, a system valve 132A in fluid communication wit ί the containment vessel (or housing) 900 was pulled open. This resulted in a relatively loud thump/energetic reaction/phoom. On the next day, another individual was asked to pull the valve 132m open for vérification. The reactionary phoom occurred again. It was understood that the moisture with the lighter material being contained in the uppe r, domed part of the sealed vessel and trapped therein by a cushion of air. For vérification, ail valves were closed and the System was allowed to run at 2700 RPM in this closed condition for 5 minutes. . valve 132A was slowly pulled open and a flame applied to the discharging material, which resulted flame. Further testing and refinement of the moisture/water concentrations in the form of atomiz and tubing arrangements were set up for rudimente in FIGs. 6A and 6B. Utilizing a small biaxial configuration for the disk-pack turbine, which included just an upper rotor 264A and a lower rotor 266A, dissociation achieved through hyperbolic rotary mo ion alone. An example of the rotors 264A, 266A of the disk-pack turbine 250A is illustrated in FIGs. 8A-8C. FIG. 8A illustrâtes the top of the disk-pack turbine 250A, FIG. 8B illustrâtes the bottom face ol top face of the lower rotor 266A. The illustrated wî iveform pattern includes a sinusoïdal ridge 2642A and a circular ridge 2646A. The lower rotor 266A illustrated is an example of mounting holes 2502A alternative embodiment, the wave patterns are switched between the upper rotor 264A and the bottom rotor 266A. Stoichiometric gas concentre lions capable of sustaining flame were achieved through broad variations in systemic configuration « nd operating conditions.

I în the valve erupting in a momentary pale blue J process included the introduction of higher :sd mist and water injection. Simple vessel valve ry gas product division and capture as illustrated was sufficient to establish repeatable, vérifiable the upper rotor 264A, and FIG. 8C illustrâtes the includes a circular outer face ridge 2668A. Also, for assembling the disk-pack turbine 250A. In an

Multi-stage Systems [0058] FIGs. 9A-11 illustrate different embodiments of a multiple stage system that includes diskpack turbines 250B-250D for each stage of the

c.

System. The illustrated disk-pack turbines are w¹ different, because the waveform disks are conical shape with circuiar waveform patterns. FIGs. 9A and 9B illustrate a common housing 220B, intake modjle 100B, and discharge port 232B. Each diskpack turbine includes at least one expansion chamber 252B-252D that routes fluid into the at least and 11. These figures illustrate the disk-pack illustrated to represent the vortex chamber (or rf the housing, the driveshaft (not illustrated) owest rotor. Between the individual disk-pack in FIG. 9C that extend through the top rotating each pair of disks that are not mounted to the

FIGs. 10 and 11 except there is no flange ^B. Below each disk-pack turbine is a discharge surface to funnel the captured gas through one disk chamber 260 of the disk-pack turbine 250B-250D. in the illustrated examples, each diskpack turbine 250B-250D includes a top rotor 264B-264D that substantially provides a barrier to fluid exiting the periphery from flowing upwards above the disk-pack turbine to assist in routing the exiting fluid to the next stage or the at least one discharge pbrt. In a further embodiment, the at least one discharge port is located along the periphery of the last disk-pack turbine instead of or in addition to the illustrated bottom discharge port 232B in FIGs. 10 module housing 220B with only a représentative input alternatively an intake chamber that is substantially cylindrical) thatfeeds these illustrated Systems. [0059] When the discharge port is at the bottom passes up through the discharge port to engage the turbines there are driveshafts such as those illustrated rotor/disk of the lower disk-pack turbine to the boltom rotor of the higher disk-pack turbine or alternatively there are a plurality of impellers between housing. The driveshafts 312B will connect to the rotating disk via support members to allow for the flow of fluid through the expansion chamber. FIG. i C illustrâtes a partial cross-section of a multistage system with a disk-pack turbine 250D’ and a second disk-pack turbine 250B' that are similar to the disk-pack turbines dîscussed in connection witt depicted on the top rotor and the bottom of the expan iion chambers is provided by a concave feature 3122B and 3214B incorporated into the driveshaft 31 module that includes discharge ports 232’ in a toi discharge outlet 2322’ into the next stage or the dischnrge port of the system.

[0060] FIG. 10 illustrâtes a cross-sectional and conceptual view of an example of a multi-stage stacked waveform disk system in accordance with an embodiment of the présent invention. The illustrated multi-stage system includes a plurality of stacked disk-pack turbines 250B-250D that are designed to first expand/dissociate and then compri ss/concentrate the charging media through the expansion chamber and the disk chambers in each dsk-pack turbine. In an alternative embodiment, additionaî ports are added around the periphery at fluid) to be added or material to be recovered/removeb [00611 waveform channels. Disk-pack turbine 250C is a sei disk-pack turbine. Disk-pack turbine 250B is a third pack turbine that provides an example of just a pair intake chamber 130B in fluid communication with chamber 252B is formed by openings in the centei 260B that form disk-pack turbine 250B. The bottor i 250D, respectively, are solid and do not hâve an opei concave feature 2522B, 2522C, 2522D that forms tlie bottom of the expansion chamber 252B. The jne or more of the stages to allow material (or from the System.

Disk-pack turbine 250B is an expansive whveform disk-pack turbine and includes multiple h :ond stage concentrating/compressive waveform stage concentrating/compressive waveform diskof rotors. The illustrated system includes an the expansion chamber 252B. The expansion of the plurality of rotors 264B, 266B and disks rotors 266B-266D in disk-pack turbines 250Bning in the center, but instead include a bottom solid bottom rotors 266B-266D prevent fluid from flowing completely through the center of the diskpack turbine 250B-250D and encourage the fluid to be* distributed into the various disk chambers 262 within the disk-pack turbines 250B-250D such that the fluid flows from the center to the periphery. Each of the top rotors 264B-264D in disk-pack turbines 250B-250D includes lips 2646 that .-pack turbine 250C in fluid communication.

channel 253D connects disk-pack turbine 250D alternative embodiment, the top rotors do not s.

of another example of a multi-stage stacked ment of the présent invention. The multi-stage disk-pack turbines. The illustrated disk-pack illy pre-condîtioned or pre-sweetened prior to that can be molecuiarly blended or corn pou nded may be introduced as the media enters into and substantially seal the perimeter of the top disk with a housing 220. The lips 2646 thereby encourage fluid to flow within discharge channels 253B-253D. Discharge channel 253B connects disk-pack turbine 250B and the expansion chamber of dis

Discharge channel 253C connects disk-pack turbine 2500 and the expansion chamber 252B of diskpack turbine 250B in fluid communication. Discharge in fluid communication with fluid outlet 232B. In an rotate and are attached to the housing to form the sea : [0062] FIG. 11 illustrâtes a cross-sectional view waveform disk system in accordance with an embod i system of this embodiment includes a plurality of turbines 250D, 250C, 250B are taken from the previ jus embodiment illustrated in FIG. 10 and hâve been reordered to provide a further example of the f exibility provided by at least one embodiment of the invention.

[0063] The charging media may also be externi I entering the system. The pre-conditioning of the chsrging media may be accomplished by including or mixing into the charging media désirable material with the prédominant charging media. This material progresses through the System, or at any stage v rithîn the process. Polar electrical charging or excitation of the media may also be désirable. Electrical charging of the media may be accomplished by pre-ionizing the media prior to entering the system, or by exposing the media to induced frequency spécifie pulsed polar electrical charges as the medi a flows through the system via passage over the surface of the disks.

d. Power Génération [0064] These objectives are accomplished, for example, via the harnessing and utilization of transformational dynamics and forces propagated a 5 the resuit of liquids, gases, and/or other forms of matter and energy progressing through and/or inter< icting with rotating hyperbolic waveform structure. [0065] In at least one embodiment the présent invention provides a system and method for producing and harnessing energy from ambient sources at rates that are over unity, i.e., the electrical energy produced is higher than the electrical ene^-gy consumed (or electrical energy out is greater than electrical energy in). The system and me hod in at least one embodiment of the présent invention utîlize rotating waveforms to manipulatt , condition, and transform mass and matter into highly energetic fields, e.g., polar flux, electrical, aind electro-magnetic fields. The présent invention, in at least one embodiment, is also capable of jenerating diamagnetic fields as strong forces at ambient operational températures.

[0066] FIGs. 12-15D illustrate an example embodiment of the présent invention that is useful in generating electrical energy. The illustrated systt «n uses as înputs environmental energies, air and electrical energy to drive a motor to rotate the disk-pack turbine and, in a further embodiment, it harnesses the environment around the system to form magnetic fields. The présent invention in at least one embodiment is capable of producing very strong field energy at ambient températures while using relatively minimal input electrical energy compared to the electrical energy production. FIGs. 15A-15D illustrate a pair of waveform disks that can be mated together with a pair of rotors. The illustrated waveform disks are depicted in FIG. 14. FIG. 15A illustrâtes the top of a disk-pack turbine 250E with a top rotor 264E with an opening into the expansion chamber 2522E. FIGs. 15B and 15C illustrate a pair of mated disks for use in power gener stion according to the invention. The disks are considered to be mated because they fit together as 262E is formed between them while allowing fluid illustrâtes an example of the mated disks 260E place* 266E with bolts attaching the components together ai bolts in at least one embodiment pass through a nylo nylon rings.

[0067] The création of a magnetic field to generate disk-pack turbine 250E and at least one magnet disk from the disk-pack turbine. In at least one embodims n 512 that are connected into multiple-phase sets. Tie disclosure that follows provides additional discussion ofthe embodiment illustrated in FIGs. 12130E and proceeding down through the system. A; with the previous embodiments, the chamber 130E feeds the charging media to the disk-pack turbine 250E during operation of the system and in at least one further embodiment the chamber 130E is imitted as depicted în FIGs. 16 and 17. In the embodiments depicted in FIGs. 16 and 17, the intake occurs through the feed housing 126E and/or the periphery of the disk-pack turbine 25OE.

[0068] In at least one embodiment, the intake chamber 100E includes a cap 122E, a housing 120E connected to an intake port 132E, a lower housing example, in FIG. 14. In an alternative embodiment, are integrally formed together. The housing 120E funnel section that tapers the wall inward from the aligned with the feed chamber 136E. The funnel section in at least one embodiment is formed by a wall that has sides that follow a long radial path in the vertical descend ing direction from a top to the feed chamber 136E (or other receiving section or e>| the formation of a vortex flow of charging medium do wnward into the system.

[0069] Below the main part of the chamber 130E depicted in FIG. 15D, because a disk channel to pass between the disks 260E. FIG. 15D ! 1 between a top rotor 264E and a bottom rotor round the periphery. As mentioned earlier, the i (or similar material) tube and the spacers are : electrical current results from the rotation of a 502 that îs on an opposite side of the coil disk nt, the coil disk 510 includes a plurality of coils

15D; as an example, starting with the chamber

124E around a bearing 280E as illustrated, for one or more of the intake chamber components includes a vortex chamber 130E that includes a s intake ports 132E to an opening that is axially pansion chamber). The funnel section assists in is a tri-arm centering member 602 that holds in place the system in axial alignaient with the drive s haft 314E. The vortex chamber 130E is in fluid communication with feed chamber 136E présent in feed housing 126E. The feed housing 126E f passes through a collar housing 125E and a magnat plate 502, which is positioned and in rotational engagement with the collar housing 125E. The through bearings 282E with the collar housing 1Î5E. The collar housing 125E is supported by bearing 282E that rides on the top of the lower feet ^reed housing 126E is in rotational engagement housing 127E that is connected to the disk-pack Y turbine 250E. The feed chamber 136E opens up into a bell-shaped section 13&E starting the expansion back out of the flow of the charging medium for receipt by the expansion chamber 252E. The intake housing components 120E, 122E, 124E together with the feed housing 138E in at least one embodîment together are the intake module 100E.

[0070] The magnet plate 502 includes a first array of six magnets (not shown) attached to or embedded in it that in the illustrated embodîment are held in place by bolts 5022 as illustrated, for example, in FIG. 14. In another embodîment, the n jmber of magnets is determined based on the number of phases and the number of coils such that t te magnets of the same polarity pass over each of coils in each phase-set geometrically at the exact r loment of passage. The magnet plate 502 in at least one embodîment is electrically isolated from th( for example, electrically insulated/non-conducting be< u to freely rotate about the center axis of the disk-pack made from, for example, aluminum which is bolted ti the top of the upper round plate 502 and has two centrally located bail bearing assemblies, an upf er bearing 282E and a lower bearing 283E, that slide over the central feed housing 126E, which servf : between the magnet plate 502 and the top of the dis k-pack turbine 250E is maintained, for example, by a mechanical set collar, shims, or spacers.

[0071] During operation, the first array of magnets is in magnetic and/or flux communication with a plurality of coils 512 présent on or in a stationary platform 510 is supported by support members 604 the array of magnets and the disk-pack turbine 250L. The platform 510 in the illustrated embodîment is electrically isolated from the rest of the system. manufacturée! from Plexiglas, plastic, phenolic or a s [0072] A disk-pack turbine 250E is in rotational eigagement with the feed chamber 138E. As with the other embodiments, the disk-pack turbine 250I i includes an expansion chamber 252E that is in fluid communication with the intakechamber 130E ta establish a fluid pathwayfrom the inlets to the at least one disk chamber 262E (two are illustrated n FIGs. 14) in the disk-pack turbine 250E. The illustrated embodîment includes two pairs of matée disks 260E sandwiched by a pair of rotors 264E, 266E where the disks 260E and the top rotor 264 Ξ each includes an opening passing therethrough and the bottom rotor 266E includes a rigid feature ‘ ’522E that together define the expansion chamber 252E. The disk chambers 262 in the illustrated t mbodiment are présent between the two disks in each mated pair with slightly paraboloid shaped being présent between the neighboring disks, whéi the top disk of the bottom mated disk pair are thi pairs of disks is formed of complimentary non-n lagnetic materials by classification, such that the mated pair incorporating internai hyperboiic relational waveform geometries créâtes a disk that causes lines of magnetic flux to be looped into a f eld of powerful diamagnetic tori and repelled by the disk. An example of material to place between the mated disk pairs is phenolic eut into a ring shape to match the shape of the disks.

[0073] In the illustrated embodîment, the botto n rotor 266E provides the interface 2662E with the vV feed housing 126E and the rest of system via, irings (not shown). The upper plate 502 is able turbine 250E by way of the collar housing 125E is as a support shaft. The distance of séparation lon-conductive disk (or platform) 510. The coil attached to the frame 600 in a position between

In at least one embodîment, the platform 510 is imilarly electrically inert material or carbon fiber.

surfaces (although they could be tapered or fiat) ire the bottom disk of the top mated disk pair and neighboring disks. Each disk 260E of the mated drive System 314E. In at least one embodiment, the rotors will be directly connected to the respective disks without electrically isolating the rotor from the njested disk. In another embodiment, the disks are electrically isolated from the rotor nesting the disk. The illustrated configuration provides for flexibility in changîng disks 260E into and out of the disk-pack turbine 250E and/or rearranging the disks 260E.

jf a drive shaft 314E that drives the rotation of plate 504 in at least one embodiment is in free i. a bearing. The drive shaft 314E is driven by a >r magnetic coupling.

second array of coils 512’ are interconnected to : arrangement with 9 and 12 coils, respectively. i ί FIG. 12) that provides a neutral/common to ail n for Earth/ground. Although not illustrated, it here are a variety of ways to interconnect the a single phase by connecting coils in sériés or of junction points that are used to connect to >124 attaches to electrical power out while the [0074] A lower coil platform 510’ may also be attached to the frame 600 with a plurality of support members 604. The lower platform 510' includes a second array of coils 512’ adjacent and below the disk-pack turbine 250E. An optional second array of six magnets (not shown) présent in magnet plate 504 are illustrated as being in rotational engagement the disk-pack turbine 250E, but the bottom magnet rotation about the drive shaft 314E using, for example_; motor, for example, either directly or via a mechanical [00751 Each of the first array of coils 512 and the i form a phased array such as a three or four phase Each coil set includes a junction box 5122 (illustrated of the coils présent on the coil disk 510 and provisic|i should be understood based on this disclosure that coils to form multiple phases in wye or delta or even parallel. As illustrated, for each coil, there are a pai· comrnon and positive and as illustrated the left box right box 5126 connects to neutral/common.

[0076] In at least one embodiment with a three pljase arrangement, the coils for each phase are separated by 120 degrees with the magnets in the m; gnet plate spaced every 60 degrees around the magnet plate. The first array of magnets, the first ai ray of coils 512, the second array of coils 512’, and second array of magnets should each be arran jed in a pattern substantially within the vertical circumference of the disk-pack turbine 250E, e.g., in circular patterns or staggered circular patterns of a substantially similar diameter as the disks 160E.

platforms and/or coil arrays between the disk-pack tuibine and the magnet plate.

[0077] The lower magnet plate 504 has a central lub 5042 bolted to it which also bouses two bail bearing assemblies 282E, which are slid over the m< ii turbine 250E is attached. This allows the lower ms axis of the system and the distance of séparation between the lower plate 504E and disk-pack turbine 250E is maintained, for example, by a mechanical set collar, spacers, and/or shims or the height of the driveshaft 314E.

[0078] Suitable magnets for use in at least one einbodiment of the invention are rare earth and/or electromagnets. An example is using three inch dis k type rare earth magnets rated at 140 pounds. Depending on the construction used, ail may be N >rth magnets, South magnets, or a combination such as alternating magnets. In at least one embodi nent, ail metallic system components, e.g., frame 600, chamber housing 120E, magnet plates 502, magnetic material with other system components, e <

In another embodiment, there are multiple coil in spindle drive shaft 314E before the disk-pack gnet plate 504 to freely rotate about the center

504, are formed of non-magnetic or very low

g., bearings, spacers, tubing, etc., are preferably formed of non-magnetîc materials. The system, including frame 600 and lower platform 504, in at least one embodiment are electrically grounded (Earth). In a further embodiment, ail movable components, particularly including chamber housing 120E and individual components of the disk-pack turbine 250E, are ail electrically isolated by insulators such as non-conductive ceramic or phenolic bearings, and/or spacers.

[0079] In a further embodiment, the magnet plate(s) is mechanically coupled to the waveform disks. In a still further embodiment, the magnet plate(s) is mechanically locked to rotate in a fixed relationship with the disk-pack turbine through for exemple the collar housing 125E Illustrated in FIG. 13. This results in lower, but very stable and safe oui put values. In a further embodiment, one set of coil platform and magnet plate are omitted from the illustrated embodiments of FIG. 12-17.

[0080] In use of the illustrated embodiment of FIGs. 12-14, the rotatable disk-pack turbine is driven by an external power source. As the disk-pack turbine rotâtes a vacuum or suction is created in the System according to at least one embodiment. This vacuum draws a charging media into the intake chamber 130E via fluid inlets 132E. The intake char iber 130E transforms the drawn charging media into a vortex that further facilitâtes passing the charging media into the expansion chamber. As the charging media passes through the system, at least transformed into polar fluxes which are discharged System. This magnetic polar energy discharges at tli pack turbine. For example, when the magnetic pohr energy discharged at the periphery is a North polar flow, the magnetic energy discharged at the introducing north-facing permanent magnets on m^i répulsive forces are realized. By placing the Northrotatable disk-pack turbine is driven by the repelling ambient environmental energies and air as the char at a maximum allowed speed. Simultaneously, whi periphery of the disk-pack turbine 250E, powerful, through the top and bottom surfaces of the disk-pdek turbine. The field strength of the diamagnetic fields is directly proportionate to the speed of rota ion of the magnet arrays and magnet strength in relation to the rotating disk-pack turbine. Each of ti < capable of producing very strong field energy at ambient températures while utilizing an extraordinarily small amount of input energy. As waveform disks 160E is capable of producing wdll over one thousand (1,000) pounds of résistive, répulsive, levitative field energy. That is, the System is capable of repeatedly, sustainably and controllably producing a profoundly powerful diam: i< relatively minimal input energy.

[0081] In a further embodiment illustrated, for e; ample, in FIG. 16, the chamber 120E above the triarm support member 602 is omitted and the expansion chamber pulls charging material from the atmosphère as opposed to through the intake ch< mber 120. In at least one embodiment, material is pulled from and discharged at the periphery of the [0082] < portion of the through-flowing charging media is or emanated from spécifie exit points within the e center axis and periphery of the rotatable diskaxis is a South polar flow. In this example, by gnet plates 502, 504 into the north-flowing flux, ^racing polar arrays at spécifie oblique angles, the l polar flux. Utilizing only the polar drive force and jing media, the system is capable of being driven e generating polar flux discharges at the axis and iîgh torque, levitative diamagnetic fields manifest ie mated pairs of rotatable waveform disks 160E is an example, each of the mated pairs of rotatable ignetic field at ambient températures while utilizing disk-pack turbine 250E simultaneously.

FIG. 17 illustrâtes an alternative embodiment to that illustrated in FIG. 16. The illustrated embodiment includes a flux return 700 to restrain the magnetic fields and concentrate the magnetic flux created by the disk-pack turbine 250E and increase the flux density on the magnet plate 502 and coils 512. An example of material that can be used for the flux return 700 is steel. In at least one embodiment, the flux shield 600 is srzed to match the outer diameter of the outer edge of the magnets on the magnet plate 502.

[00831 Another example embodiment of the presenjt invention is illustrated in FIG. 18 and includes two disk-pack turbines 250F having a pair of rotors 264F, 266F sandwiching a pair of disks 260F, two sets of electrical coil arrays configured for the prodi < bearing-mounted, free-floating, ail North-facing magnetic arrays, along with various additional circuits, controls and devices. One différence with the previous embodiments is that the disk-pack turbines 250F are spaced apart leaving an open area between [0084] Another différence for the power-gener; embodiments is the omission of a housing around ail différence disclosure dôme (or ction of three-phase electrical power, and two ali disks are manufactured as nesting pairs. Each ï ials, depending on design criteria, i.e., aluminum illy isolated from one another by means of no nd assembly methods and éléments like those >ach disk pair that provide for highly exotic flow

Ithem.

iion embodiments from the other described □f the rotating components. One reason for this is that the illustrated embodiment is dirjcted at power génération, but based on this it should be understood that an alternai ive embodiment adds a collection/containment wall) to this illustrated system to provi ie a means of collecting and harnessing for application/utilization the profound additional enviromnental electrical fields/DC voltages and dramatic currents/field amperage as well as the collection of ί ny fluid components that manifest as a resuit of the power génération processes.

[0100] The nature of electricity generated by this e mbodiment is substantially different as compared to conventional power génération. The waveform < waveform disk pair may be of like or dissimilar mate and aluminum, or, as example, aluminum, brass or copper. When a waveform disk pair is separated by a spécifie small distance/gap and are electricî I mechanical contact and non-conducting isolation îi described earlier, chambers are formed between e;

paths, motion, screening currents, frequencies, pressure differentials, and many other actionary and reactionary fluid and energetic dynamics and novrl electrical and polar phenomena. Immediately upon energizing the drive motor to set the disk-pac : turbine rotor in motion, the inner disk hyperbolic geometries begin to interact with the magnetic fields provided by the rotatable Rare Earth magnet arrays, even though there are no magnetic materiiils incorporated into the manufacture of the diskpack turbine. By the time the disk-pack turbine reaches the speed of approximately 60 RPM, diamagnetic field effects between the disk-pack ti irbine faces and magnet arrays are sufficient to establish a driving/impelling link between the disk-p;

[0101] A variety of magnetic polar fluxes and ele i increase in proportion to speed of rotation. Diamagnetism manifeste as a profoundly strong force at the upper and lower rotor faces as primarily vertic il influences which, through repellent diamagnetic fields, act to drive the magnet arrays while simult aneously generating a significant rotational torque component. it has been determined that these sti through/passed through insulators to other metall· « ick turbine and magnet array faces.

ctrical currents begin to manifest and dramaticaliy ïrong force diamagnetic fields can be transmitted ic materials such as aluminum and brass. These *16330 diamagnetic fields, generated at ambient températures, are always répétant irrespective of magnet polarity. Although mechanically generated, these diamagnetic fields are, believed to be in fact, screening and/or eddy currents previously only recognized as a strong force associated with magnetic fields as they relate to superconductors operating at cryogénie températures. The system is configured to rotate on the horizontal plane, resulting in the most profound magnetic field effects manifesting and emanating at an oblique, though near faces. The most profound electrical outputs in the s pack turbine and are measurable as very high field example, when attaching a hand held amp meterto built system illustrated, for exampie, in FIG. 12, it is crimmon to observe amperages of over 150 amps per electrically isolated riser. Polar/magnetic fluxes are the primary fluid acting in this system configured for electrical power génération. An additional component acting within the system is atmospheric air. In certain implémentations, allowir g the intake, dissociation, and discharge of the éléments within atmospheric air as well as exposure magnetic field effects and eiectrical power output potential by plus/minus 40%.

[0102] The diamagnetic fields utilized for electricel magnets within the magnet arrays to North, Soutl configuration. When ail North or South facing magr rotor fields, voltages and frequencies realized are extremely high. With ail North or South magnet orientation the diamagnetism, which is both North i nd South magnetic loops, provides the opposite polarity for the génération of AC electricity. By ctjnfiguring the system with alternating magnetic polarities and minor power output conditioning, it I values and bring the voltages and frequencies i combined upper coil array only, output values of 9' are typical. Based on research, it is believed the r lagnetic fluxes behave like gasses/fluids and can act as such. The addition/intake/dissociation of air the process; however, with the presence of magndtic fields interacting with the hyperbolic waveform structures alone, it is believed that both exotic, generated. It is believed it would be impossible t( without also simultaneously generating correspond: handheld, is introduced above the disk surface ar d the diamagnetic repellent effect is felt, electrical current is being produced, thereby creating the diai ri.

e. Testing of Prototype [0103] At least one prototype has been built ac rording to the invention to test the operation of the system and to gather data regarding its operation. The prototype shown in FIGs. 12-18 include a three phase arrangement of nine coils, three coils ?er phase using 16 gauge copper magnet wire with 140 turns and six magnets (three North and three South magnets alternating with each other) above the disk-pack turbine and coils. On the bottom side of the disk-pack turbine there is a four phase arrangement of 12 coiis, three colis per phase using 20 gauge copper magnet wire with 260 turns and six magnets. Based on this disclosure, it should be appreciated that the gauge and material of the iY' right angle relative to the upper and lower rotor /stem emanate from the periphery of the diskamperages and atmospheric voltages. As an s ny of the three structural aluminum rîsers of the to ambient atmospheric energies increases the

I power génération make it possible to orient ali :h, or in a customary North/South alternating ets are configured in relation to the diamagnetic tas been possible to practically divide the output into useful ranges. As an example, measuring K 0 volts at 60HZ with a rotor speed of 1200 RPM and other ambient influences adds significantly to magnetic phenomena as well as electricity are be generating these profound diamagnetic fields ng electrical currents. As soon as a magnet, even lagnetic phenomena.

wire and the number of turns and of coils can be Imodified and that the above descriptions are examples. The disk-pack turbine was assembled witn two pairs of mated disks between the top rotor and the bottom rotor as illustrated, for example, in FI0.16. In this particuiar configuration the two top waveform disks were made of aluminum and the bottom two waveform disks were made of brass. It has been found that alternating brass and aluminum disks, as opposed to nesting like disks results in significantly higher magnetic and electrical values being produced. In further testing when copper is used in place of brass, the voltages hâve stayed substantîally equal, but a much higher current has been produced. After one testing session, it was discovered that the brass disks were not electrically m was connected to a motor via a belt.

isolated from each other and there was still excess electrical power generated compared to the power required to run the motor. The feed tube (or intaie chamber) is made of brass and electrically isolated from the aluminum rotor face through use of a non-conductive isolation ring, which also is présent between the two mated disk pairs. The syste [0104] An interesting phenomenon has been noticed during operation of the prototype that indicates that ambient atmospheric energies from the surrounding environment is being transformed and harnessed by the System to create supplémente I background ionizing radiation présent ail around decreases from background levels when the syster i is in operation by an amount greater than the margin of error for the detector.

[0105] When the motor was not running, and thï disk-pack turbine was slowly rotated by hand, even at this very low speed, a diamagnetic field ar jse sufficient to engage the upper magnet plate (the magnet plate was not mechanically coupled), resulting in the production of enough electricity to cause a connected three-phase motor (2 HP, 230 turned by hand from the current produced in the coil arrays.

[0106] The lower magnet disk rotated with the disk-pack turbine while the upper magnet disk was magnetîcally coupled to the waveform disks. One power génération formulas. One of the greatest mathematically speaking, production of very high pc ' discernable heat generated through the process, ar d this phenomenon extends to devices connected and driven by this electricity, such as multiple three-phase high voltage electric motors. An example is prior to starting the system, ambient temperat jres for the induction coils and other associated devices were about 82° Fahrenheit. After runr température rise was as little as two or three degroes and, at times, the température has been found to actually fall slightly. The température measurec always has dropped a few degrees over time. Th a température of an unloaded three phase electric motor connected to the output will generally remain within one or two degrees of coil température. The three phases of the upper generating assemt ly were measured with each phase was producing plus/minus 200 volts at 875 RPM. Based on mes surements, each of the three coil sets in the threephase system measure out at 1.8 ohms. Divide 200 volts peak-to-peak by ohms equals about 111.11 Amps, times 200 volts equals about 22,222 Watts, times three phases equals about 66,666 total Watts. The motor powering the system was drawi ig 10.5 Amps with a line voltage of 230 volts, which

I electrical current. There is a certain amount of

The level of detected ionizing radiation us.

V) to rotate as the disk-pack turbine was being way to illustrate the results will be to use classic points of interest is that, even though there is, wer readings as relates to watts, there is very little ing the system for in excess of one hour, the at the core of the waveform rotor when measured yields us 2,415 Watts being consumed by the motor tolproduce this output of about 66,666 Watts. [0107] When the top magnet disk was locked with (rte waveform disks, the process was repeated. The upper coil array produced about 540 Volts peak-tp-peak between the three phases and about 60 Amps for a power génération of about 32,400 Watts. With regard to the lower generator, the math is actually quite different because there is a higher coil| set résistance of approximately 3.7 Ohms per coil set of three (four phases). So, with an output of 120 Volts peak-to-peak per phase divided by 3.7 Ohms equals 32.43 Amps times 120 Volts equals 3,891.6 Watts per phase times four equals 15,566.40 Watts. These readings are from running the system at a vîrtual idle of about 875. Testing has found that diamagnetic energy will really start to rise at 1700 RPM and up as do the corresponding electrical outputs.

[0108] Changing the material used for the intake cl ïamber in the built system from D2 steel to brass improved the strength of the diamagnetic field and re: ulting power génération by approximately 30%.

f. Discussion Regarding Diamagneti ;m [0109] Diamagnetism has generally only been kncwn to exist as a strong force from the screening currents that occur in opposition to load/current within superconductors operating at super low cryogénie températures, i.e., 0 degrees Kelvin (0 K) or -273 degrees Celsius (-273 C). When a superconductor-generated diamagnetic field is appr >ached by a magnetic field (irrespective of polar orientation) a resistive/repulsive force resists the magnetic field with ever-increasing repulsive/resistîve force as distance of séparation d( creases. The superconductor's résistive force is known to rise, in general, in a direct one-to-one ratio relative to the magnetic force applied. A 100 pound magnet can expect 100 pounds of diamagn ;tic résistance. A logical assumption would lead one to believe that this diamagnetic force, acting upon a superconductor in this way, would resuit in increases in system ic résistance and net losses in interaction results in a zéro net loss to the system.

[0110] As described above, diamagnetism manifeste as a strong force in superconductors due to the screening currents that occur at cryogénie temf the présent invention in at least one embodiment, internai oppositional currents, flows, counter-flows hyperbolic waveforms présent on the rotatable wiiveform disks. These forces in combination with spécifie metallic materials, material relationships, media as discussed in the example embodiments ί bove manifest as profoundly powerful diamagnetic fields at the bottom and top surfaces of the rotatatle disk-pack turbine at ambient températures. The diamagnetic waveform disks are fabricated frori non-magnetic materials that are incapable of maintaining/retaining a residual electric field in the absence of an applied charge. The diamagnetic fields created by the rotatable waveform disks are a direct product of the specialized waveform motions, interaction with environmental matter anc and centripitated ambient air.

[0111] The diamagnetic fields generated by tht waveform disks can be utilized as a substitute for the North or South magnetic potes of permanent

However, unlike the North/South lines of force çxhibited by common magnetic fields, diamagnetic — r ifficiency. The counter-intuitive reality is that this eratures. As with superconductors, the system of Jtilizes screening currents working in concert with reciprocating flows and pressures generated by component isolation technologies, and charging energies, and a modest amount of through-flowing magnets for the purpose of generating electricity.

so, when a coil or circuit is placed into the ns with actual repeatable readings being about fields manifest as North/South loops or tori that spin around their own central axis. This distinction results in the diamagnetic field not being a respecter of magnetic polarity and always repellent. The magnetic repellency allows one pôle of the north/sou h alternating magnetic fields to be substituted with the diamagnetic field generated by the waveform disks. In use, the upper array of magnets and the lower array of magnets float freely and are driven by the diamagnetic levitative rotational torque. As the ail north-facing rare earth magnets eut a circular right-angle path over the upper array of coils, and lower array of coils, electrical power is generated.

[0112] Systems utilizing this arrangement for electrical power génération, in at least one embodiment of the présent invention, have realized a multiplication in the production of voltage and current as compared to an electrical power génération arrangement utilizing traditional North to South pôle fluxuations. Further, power input required to run the Systems are extremely low while power production is accomplished with minimal rise in heat < c résistance, e.g., système températures of less than five degrees over ambient températures. A diamagnetic field, the résistance drops to near 0 Oh 0.01.

[0113] Further, in at least one embodiment, the system of the présent invention is capable of producing at very low operational speeds powerful diamagnetic fields that are capable of functioning as an invisible coupling between a rotating waveform disk and a rotatable magnetic array. The system drive side may be either the magnetic array e ide of the system or the diamagnetic disk side of the system. The magnets may move over the intimai waveform geometries, thereby causing the fields to arise, or vise-versa. Actual power/drive latios are established via progressive waveform amplitude and waveform itérations. The magneti: drive array will allow for the magnets to be dynamically/mechanicalfy progressed toward periph jry as systemic momentum increases and power requirements decrease. Conversely, when loads in :rease, the systemic driving magnets will migrate toward higher torque/lower speed producing geomet’ies.

g. Waveform Disks [0114] The previously described waveforms ari examples of the possibilities for their structure. Th 5 waveform patterns increase the surface area in which the charging media and fields pass over and through during operation of the system. It is believed the increased surface area as alluded to f arlîer in this disclosure provides an area in which the environmental fields in the atmosphère are scre ened in such a way as to provide a magnetic field in the presence of a magnet. This is even true wht i passed over its surface (either the waveform side and flow of the magnetic field track the waveforml patterns on the disk, manifesting in at least one embodiment as strong, géométrie eddy currents/ge imetric molasses .

[0115] As discussed above, the waveform disks in most embodiments are complimentary to each least one embodiment, the height in the vertical axis and/or the depth measured along a radius of the disk chambers vary along a radius as illustrai/sd, for example, in FIG. 15D.

embodiment, when a disk surface with the wavefo !

d the one illustrated in FIGs. 8B and 80 are •n the waveform disk is stationary and a magnet is or back side of the waveform disk), and the ebbs include a plurality of radii, grooves and ridges that other when présent on opposing surfaces. In at

In at least one ms on it is viewed looking towards the waveforms, —¹ the waveforms take a variety of shapes that radiate From the opening that passes through (or the ridge feature on) the disk, in at (east one embodiment, the number of peaks for each level of waveforms progressing out from the center increases, which in a further embodiment includes a multiplier selected from a range of 2 to 8 and more particularly in at least one embodiment is 2.

[0116] In at least one embodiment, the disk surfaces having waveforms présent on it éliminâtes almost ail right angles and fiat surfaces from the surface such that the surface includes a continuously curved face.

is a circular waveform 2646G in the center and is a biaxial, sinocircular, progressive waveform The illustrated disks mate together to form the

FIG. 19E illustrâtes how the three disks fit :bansion chamber 252G of a disk-pack turbine. In lar waveforms is modified to include a plurality of [0117] In at least one embodiment, at least one ridge includes a back channel formed into the outer side of the ridge that together with the complementary groove on the adjoining disk form an area having a vertical oval cross-section.

[0118] FIGs. 19A-19E illustrate a variety of additional waveform examples. The illustrated plates include two different waveforms. The first waveform around the periphery. The second waveform 2642G located between the two sets of circular waveforms.

disk channels discussed previously. Each of the disks includes a plurality of assembly flanges 2629G for mounting impellers between the disks.

[0119] FIG. 19A illustrâtes an example combiniition of biaxial, sinuocircular, progressive, and concentric sinusoïdal progressive waveform geomelry on a disk 260G according to the invention. FIG. 19B and 19C illustrate respectively the oppoiing sides of the middle disk 260G. FIG. 19D illustrâtes the top surface of the bottom disk 260G. together to form the disk chambers 262G and the ex an alternative embodiment, one or more ofthe circql biaxial segments.

[0120] FIG. 20 illustrâtes an example of a cerjter disk incorporating varied biaxial geometries between two sets of circular waveforms according te [0121] FIGs. 21A-21D illustrate a two disk disk-f the disk-pack turbine 250H with an expansion charr of the top disk 264H. FIG. 21C illustrâtes the toc surface of the bottom disk 266H including the concave feature 2522H that provides the bottom rf the expansion chamber 252H in the disk-pack turbine 250H. FIG. 21D illustrâtes the bottom of tht disk-pack turbine 250H including an example of a motor mount 2662H. The illustrated waveforms an circular, but as discussed previously a variety of waveforms including hyperbolic waveforms can be [0122] FIG. 22 illustrâtes another example of a 260I, and a bottom rotor 266I. The top rotor 264I the plane taken through the middle of the components. FIG. 22 also illustrâtes an embodiment where the components are attached around the peripiery of the opening that defines the expansion chamber 2501 through mounting holes 25021. Each of the waveform patterns on the top rotor 2641, the disk 2601, and the bottom rotor 2661 includes t no sets of circular waveforms 26461 and one set of hyperbolic waveforms 26421. «a/ the invention.

ack turbine 250H. FIG. 21A illustrâtes the top of ber 252H. FIG. 21B illustrâtes the bottom surface substituted for the illustrated circular waveforms. lisk-pack turbine 250I with a top rotor 2641, a disk and the disk 260I are shown in cross-section with

h. Conclusion [0123] While the invention has been described with reference to certain preferred embodiments, numerous changes, alterations and modifications to thie described embodiments are possible without departing from the spirit and scope of the invention, as defined in the appended daims and équivalents thereof. The number, location, and configuration of disks and/or rotors described above and illustrated are examples and for illustration only. Further, the terms disks and rotors are used interchangeably throughout the detailed description without departing from the invention.

[0124] The example and alternative embodiments described above may be combined in a variety it modifies but rather possessing more of the , and preferably, approaching or approximating of ways with each other without departing from the invention.

[0125] As used above “substantially, “generally, ind other words of degree are relative modifiers intended to indicate permissible variation from the ch aracteristic so modified. It îs not intended to be limited to the absolute value or characteristic which physical or functional characteristic than its opposite such a physical or functional characteristic. The foregoing description describes different components of embodiments being “connected” to other comi connections, fluid connections, magnetic connections, flux connections, and other types of connections capable of transmitting and sensing phy sical phenomena between the components. The foregoing description describes different component: i to other components. “i corn ponent/cham ber to another component/chamber [0126] Although the présent invention has been described in terms of particular embodiments, it is not limited to those embodiments. Alternative embodiments, examples, and modifications which would still be encompassed by the invention may t light of the foregoing teachings.

[0127] Those skilled in the art will appreciate that various adaptations and modifications of the embodiments described above can be configured without departing from the scope and spirit of the invention. Therefore, it is to be understood that invention may be practiced other than as specificall· < described herein.

(onents. These connections include physical of embodiments being in fluid communication” In fluid communication iijicludes the ability for fluid to travel from one e made by those skilled in the art, particularly in within the scope of the appended daims, the

least one waveform pattern formed on at least

Claims (15)

1. CLAIMS:

   1. A system comprising:

   a plurality of waveform disks, each having at one surface with said waveform pattern centered around an axial center of said plurality of waveform disks;

   at least one coil array in magnetic communication with said plurality of waveform disks; at least one magnet plate rotatable about saie.

   axial center of said plurality of waveform disks, wherein said plate includes an array of magnets where one of said at least one coil array is between one of said at least one magnet plate and said pluralit / of waveform disks; and a drive System engaging said plurality of wa¹ eform disks to rotate said plurality of waveform disks during operation.
2. 2. The system according to claim 1, further con ,| prising at least one feed inlet, and said plurality of waveform disks in fluid communication with said dt least one feed inlet, said plurality of waveform disks each having an opening passing therethrough f irming an axially centered expansion chamber.

   The System according to claim 2, wherein îaid expansion chamber includes a converging
3. 3.

   portion and a diverging portion.
4. 4. The System according to any one of claims 1 communication with said at least one coil array.
5. 5. The system according to any one of claînr

   -3, further comprising energy collection means in s 1-4, wherein said plurality of waveform disks includes at least one set of mated disks and between each set of mated disks is at least one aid housing, said rotors forming at least a portion sk having a waveform pattern, and passageway.
6. 6. A system comprising:

   a vortex induction chamber, a housing connected to said vortex induction chamber, said housing including a chamber having multiple discharge ports, a pair of rotors in rotational connection to £ of an expansion chamber, at least one mated disk pair having one disk mounted on at least one of said rotors, at least one passageway exists between said disks, each d a motor connected to said rotors; and a fluid pathway exists from said vortex nduction chamber into said expansion chamber through said at least one passageway to said housing chamber and said multiple discharge ports.
7. 7. The system according to any one of clams 1-6, each disk having the waveform pattern centered about an opening axially centered pa ising therethrough, the opening aligned with an opening passing through the top rotor, the wavefoi i least one of a neighboring disk.
8. 8. A disk array system, the System comprisin j:

   at least one pair of mated disks, said m sted disks are substantially parallel to each other, each disk having a top surface, ^z' τη patterns are complementary of waveforms on at a bottom surface, a waveform pattern on at Ieast one surface ofthe disk facing at Ieast one neighboring disk such that the neighboring waveform patterns subs antially form between said neighboring disks in said pair of mated disks a passageway, at Ieast one mated disk in each pair passing through its height, and a fluid pathway exists for directing fluid from the at Ieast one opening in said disks through the at Ieast one passageway towards the periphery of the disks; and each of said waveform patterns includes ei plurality of at Ieast one of protrusions and dépréssions.
9. 9.

   disks with the disk of each pair facing another pair surfaces having the waveform pattern facing the surfa se of the other disk in the mated disks.
10. 10. The system according to any one of claims 5- 3, wherein the passageway formed between two mated disks provides a plurality of low pressure zones and high pressure zones during operation with the pressure zones alternating along the radius of the
11. 11. The system according to any one of claims disk between said disks of at Ieast one mated pair, e< ch additional disk includes a top surface, a bottom surface, a waveform pattern on said top surface and said bottom surface such that the neighboring waveform patterns substantially form between sait neighboring disks within said mated disks a passageway, and an opening passing from said top surface to said bottom surface.

    -11, further comprising: of mated disks includes at Ieast one opening

    The system according to any one of claims 5j8, wherein there are at Ieast two pairs of mated of mated disks having a fiat surface with the disks.

    1-10, further comprising at Ieast one additional
12. 12. The System according to any one of claims ' a top rotor attached to one mated disk, a bottom rotor attached to second mated disk from î
13. 13. The system according to any one of claims Ieast one of hyperbolic waveforms;

    hyperbolic waveforms selected from a g oup including biaxial and multi-axial sinusoïdal waveforms;

    a plurality of rising waveforms as the protrusions and a plurality of descending waveforms as and descending waveforms traveling substantially accessible opening of the disk array; and second pair of mated disks.

    1-12, wherein said waveform patterns included at the dépréssions, said plurality of rising waveforms around and substantially axially centered about the at Ieast one biaxial waveform centered about the accessible opening of the disk array and at Ieast one multiple axial sinusoïdal waveform
14. 14. A method for generatîng power comprising driving a plurality of disks having matching wavefoii inducing current flow through a plurality of coils ms, and residing in a magnetic field created between the vA'' waveform disks and at least one magnet platform rotating through magnetic coupling with the waveform disks.
15. 15. The method according to claim 14, further comprising feeding a fluid into a central chamber defined by openings passing through a majority of the plurality of disks with the fluid flowing into 5 spaces formed between the disks to cause the fluid to lissociate into separate components. vV