In Evolution of Gravity Fields

Abstract

A forever technologies ultimate energy device affecting energy dynamics planet genesis, gravity fields do: embodies sui generis boundaries perfections in ultimately compact structures, discerns, distinguishes forms of cycling energy genres, effectuates an energy form respective directionality and embraces energy cycling maximum conductance, or maximum ultimate Heat Rate efficiency or maximally, ultimately short paths-of-passage lengths' sums comprising a least sum (PPLSLS).

Claims

1. A forever technologies ultimate energy device affecting energy dynamics planet genesis, gravity fields do: embodies sui generis boundaries perfections in ultimately compact structures, discerns, distinguishes forms of cycling energy genres, effectuates an energy form respective directionality and embraces energy cycling maximum conductance, or maximum ultimate Heat Rate efficiency or maximally, ultimately short paths-of-passage lengths' sums comprising a least sum (PPLSLS).

2. An ultimate induction device affects a plurality of sui generis successive boundaries perfections an ultimately compact energy structure, thermal energy maximum conductance, electrical energy maximum conductance, where electrical energy cycling densities transfer to electromagnetic flux cycling densities greatly increase over the prior art by the ultimate energy device said plurality of sui generis successive boundaries perfections in the ultimately compact energy structure. Where, thermal energy maximum conductance, electrical energy maximum conductance in said plurality of said sui generis successive boundaries perfections embody absolute maximum surface areas of respective interacting perimeter surfaces of stator coils and stator coils dual layer, which imposes electrical insulation compressed insulation volume least needed thicknesses least needed volume.

3. The maximum conductance of claim 2, engendering Said plurality of said sui generis successive boundaries perfections of the ultimate energy device, where said ultimate maximum conductance of electromagnetic thermal energies cycling energies boosts cycling energies cycled Heat Rate efficiency of Earth's gravity field, where the Wheel of Nature said maximum conductance positively, absolutely minimizes global air warming effects.

4. The ultimate energy device of claim 1, engendering the maximum conductance or maximum ultimate Heat Rate efficiency, the maximally, ultimately short paths-of-passage lengths' sums affecting the least sum (PPLSLS), the forever technologies, wherein, only at least one of said three can affirm positively, absolutely the forever technologies.

5. The ultimate energy device of claim 1, wherein the ultimate device, the Earth's gravity field induction device spawned an in common a plurality of the suit generis boundaries Universe energy structure effectuates the Universe energy structure an in common, a plurality of boundaries perfections energy reactions to insolation energy actions balancing the lapping of the Universe, Milky Way Galaxy, Sun and Earth evolving gravity fields.

6. The Earth's gravity field induction device of claim 5, wherein in the Solar System gravity field, technologies solution utilizes the lapping gravity fields cycling energy structure a model of the Universe, the Universe energy structure, comprising the potential energy field, the potential energy one field that balances itself by balancing cycling energy inside the planets and the Solar System respective boundaries perfections; wherein, space rocket launch from the Earth disintegrates outermost Ring of Saturn Rings, directing most of disintegrated ring pieces towards the Earth, the Sun, which, of course, only possesses a marginal chance of success.

7. The energy dynamics forever technologies, planet genesis, gravity field spawns of claim 1, claim continuation in part continuity of the prior applications claiming sciences and technologies under the cosmological (FEIIPMII) global PMII technologies, herein, the forever technologies, affected sciences and technologies inventions and innovations, according to criteria of the ultimate energy device, claim 1 states, affect sole solutions to global air warming phenomenon.

8. A three phase, four pole induction motor of ultimately compact device utilizes a stator, a yoke, a plurality of stator teeth, a plurality of stator slots, a maximum ultimate copper fill by a hexagonal barely rectangular cross-sectional area of wound coil rows, wound coil columns wound precisely concentric wire coils, the coils, comprising: a maximum ultimate number of wound wire coils of a magnet wire, the magnet wire, in each of the slots; a least length of the wire length in the maximum ultimate number of the wound precisely concentric wire coils in a magnetic pole, a magnetic pole pair and pairs of magnetic poles; a column of pre-insulated coils, wherein the wound coil columns in position press and wedge in grooves and ridges of concentric wire coils in place and/or into insulation in base of the slot; a row of pre-insulated coils, wherein the wound coil columns of the wound coil rows wedge the row each outermost coil into grooves and ridges in insulation of respective walls of each slot; a volume of an electrical insulation in the coils of stator slots, wherein the maximum ultimate copper fill compresses the volume of the electrical insulation in a plurality of the stator slots; a layer bundle, wherein perimeter coils of the layer bundle are pressing on and wedging into groves and ridges in the electrical insulation of the slot; a coil, a coil pair and coil pairs, wherein the maximum ultimate number of the wound precisely concentric wire coils maximize the maximal ultimate number of the wound wire coils and, also, maximize the maximum ultimate copper fill in the slot; a winding coils group of the wound precisely concentric wire coils of a dual layer bundle and a perimeter two surfaces of compress volume of an insulation lining the slot and surface perimeter of the slot affects an absolute maximum surface area of respective interacting perimeter surfaces; a thermal energy most direct outflow path flows from maximum perimeter surfaces of each of the coils and from surfaces of slot perimeters within a stator yoke; a rectangular hexagon cross-sectional area of the coils and the slots absolutely maximized respective perimeters surface areas maximized heat energy outflow conductance; a structure configuration of the slot maximized respective electrical, thermal, electromagnetic energy cycling comprising the slot sui generis surfaces boundaries of the structure configuration; a compacted configuration slot compacting the slot cross-sectional area, in turn, the steel laminations required a stator diameter size and, in turn, diameter size of the yoke, the motor; a compacted slot cross-sectional area, in turn, minimized weight of the induction device; wherein, the motor, the induction device, the induction motor, the ultimate induction device is one and the same device; wherein, the layer bundle of the wound precisely concentric wire coils, the compacted columns of the wound wire coils of the layer bundle compacts the wound coil rows of the layer bundle; wherein, the wound precisely concentric wire coils compress a thickness of an electrical insulation of the slot, compress a flexible coat portion of a pre-insulation insulation of the wound coil rows to a least needed insulation thickness in the layer bundle and an insulation lining the slot to maximize outflowing heat energy conductance of the coils and of the stator slots; wherein, the hexagonal barely rectangular cross-sectional area of the wound coil rows, wound coil columns wound precisely concentric wire coils comprising said wires coils, a wire coil an absolute maximum surface area that conducts/transfers heat energy in a radial direction; wherein, a biaxial compression of a compressed volume of an electrical insulation in the slot affects an ultimately compact volume, the ultimately compact structure of the slot; wherein, a cross-sectional area of a hexagonal barely rectangular cross-sectional area a conforming to the equal entirely round cross-sectional area affecting a significant increase in the conductance of a heat energy dissipation increased conductance of cycling electrical energy and decreased a rising temperature increase by the heat energy dissipation of cycling heat energy; wherein, the cross-sectional area of the hexagonal barely rectangular cross-section conforming to the equal entirely round cross-sectional area affecting the significant increase in the conductance of the heat energy dissipation, the increased conductance of the cycling electrical energy, a decreased rising temperature increases increase cycling electromagnetic flux density; wherein, the cross-sectional area of the hexagonal barely rectangular cross-section conforming to the equal entirely round cross-sectional area an increase in electrical energy cycling transfer to electromagnetic flux density cycling increases Heat Rate efficiency of cycling energies transfer; wherein, the cross-sectional area of the hexagonal barely rectangular cross-sectional area of the wound coil rows in each of the stator slots winds concentric without a torsional twisting; wherein, the cross-sectional area of the hexagonal barely rectangular cross-sectional area of the wound coil rows in each of the stator slots winding concentric without the torsional twisting in the stator slots minimizes the torsional twisting on outside of the stator slots and minimizes the torsional twisting of the wire coil and the winding layer; wherein, the cross-sectional area of the hexagonal barely rectangular cross-section no torsional twisting in the slots and torsional minimized twisting outside of the slots engenders compressed insulation volume maximized thermal energy conductance maximized electrical energy conductance; wherein, the maximum ultimate copper fill, a maximum coil number, a compressed volume of insulation thicknesses, a maximum conductance of electrical energy, a maximum conductance of thermal energy respective cycling yield an electromagnetic maximum torque and a mechanical maximum torque at relatively low a slot temperature; wherein, the structure configuration of the slot maximized respective electrical, thermal, electromagnetic energy cycling comprising the slot sui generis surfaces boundaries of the structure configuration comprising energy specific directionalities preferred directions; wherein, electrical insolation in the slot, in the coil, in the coil pair, in the coil pairs comprises the compressed insulation volume least needed thicknesses of electrical insulation least needed volume in insulation coat of the wire windings of the coils and the insulation lining of the stator teeth; and, wherein, 60 slot arrangement associated with the yoke illustrates the stator of the present invention; and, the three phase, four pole induction motor of ultimately compact device further comprises a rotor yoke thickness of a rotor yoke comprising: a plurality of rotor teeth which extend radially and outwardly away from a rotor center axis; a common tooth length of the plurality of the rotor teeth: wherein each tooth of the plurality of the rotor teeth has two sides; wherein each pair of the rotor teeth has the side surfaces parallel; wherein the plurality of the rotor teeth comprises the side surfaces in parallel; wherein each pair of the rotor teeth embodies a rotor tooth slot; wherein a rotor bridge seals the rotor tooth slot, therein, affecting a surface of the air gap; and, wherein, the illustrated example shows 72 rotor teeth.

9. The forever technologies ultimate energy device according to claim 1, wherein one cannot possibly evaluate a structure appearance and not do accurate energy genres tracing of cycling energy dynamics. Especially, an evaluating of an energy structure energy directionalities can mislead. Since the advent of science, a structure appearance misleads; it misleads Newton at al., Einstein at al., scientific community at al., all whom rely on apparent appearance of the Earth structure in the Universe structure; drawings illustrate, therein describe a device structure claims.

10. The three phase, four pole induction motor of ultimately compact device of claim 8, wherein the precisely concentric wire coils concomitantly affect the maximum conductance cycling electrical energy and the maximum conductance cycling thermal energy two priorities in the stator slot and the stator tooth construction, to unavoidably engender ultimate priorityan electromagnetic field cycling flux maximum densities which are the ultimate priority of the induction devicewhich is what winding the precisely concentric wire coils does.

11. The three phase, four pole induction motor of ultimately compact device according to claim 8, wherein a compacting of the coil rows, where the coil rows, compacts the winding coils each coil column and the insulation volume thicknesses of electrical insulation in the stator slots biaxial compression, in thermal expansion triaxial stresses, compresses electrical insolation to the needed minimal insulation thicknesses in the slot, the coil, the coil pair, the coil pairs, compress to insulation volume needed least thicknesses.

12. The three phase, four pole induction motor of ultimately compact device of claim 8, wherein another aspect of the present invention illustrated by example provides a procedure for packing the wound coil rows, the wound coil columns wound precisely concentric wire coils of said coils preferred cross-section of the magnetic wire. Each layer of the dual layer selected for illustration has 31 of the winding coils. The base of the stator slot is at a stator slot bottom and is a region of the stator slot away from the stator bore. A region of a stator slot opening is proximate the stator bore and is top of the slot. The dual layer in the stator slot has 5 coil rows in the dual layer lower layer and 6 coil rows in the top layer for a total of 11 coil rows. Each of the coil rows 1, 7, 9 and 11 has the coil group of five coils. Each of the coil rows 2, 4, 6 and 8 makes the coil group of six coils. Each of the of the coil rows 3 and 5 has seven coils in the coil row. Coil row 10 four coils pass thru the slot opening as one row. The other coil rows pass thru the slot opening split in two, having four coils on bottom with the remaining coils of the coil row on top. The coil rows 1, 7, 9 and 11 have coil number 1, 2, 4 and 5 positioned under coil number 3 positioned to be lowered to designated center position. The coil rows 2, 4, 6 and 8 have coil number 1, 3, 4 and 6 under coils 2 and 5 positioned to be lowered to respective designated positions. In positioning coil rows 1-9, an anvil bobbin preferably guides the coils to respective predesignated positions, while a hammer bobbin lowers the coils into designated positions. Where, the dual layer or multiple layers or one layer of said coils, the coils, spawns the maximum ultimate copper fill of the stator slots, wherein any number of said coils may comprise the dual layer, the multiple layers and the one layer. Any number of three phases and of each phase lapping, the wound precisely concentric wire coils row may affect, and each phase change the coil rows a coils row may affect lapping in any stator slot.

13. The ultimate induction device in accordance with claim 2, wherein the stator slot illustrated example engenders the forever technologies four energy characteristics, comprising sui generis successive boundaries perfections an ultimately compact energy structure, electromagnetic, thermal energy maximum conductance, and transferring into mechanical energy cycled maximum ultimate Heat Rate efficiency under confining pressure of Earth's gravity field; where, unbalanced one of the four energy characteristics evolves the other three, where, the prior sciences, technologies and art not one energy device has the ultimately compact energy structure.

14. said plurality of sui generis successive boundaries perfections according to claim 2, wherein the application explains the energy source of gravitational energy. The thermodynamics Second Law origin tracing of the gravitational energy in the Universe claims energy technologies science and cosmological gravitational dynamics science technologies, respectively. Proven and verified fundamental science and technologies correct the prior science profound deep flaws promulgated by classic science theories. The prior sciences corrected flaws allows licensing key technologies.

15. A forever technologies in accordance with claim 1, where The forever technologies continued the Fluid Elements ions, isotopes, principles, methodologies, inventions, and innovations continue the continuation-in-part continuity of the prior applications, which disclose, illustrate and claim said sui generis boundaries perfections in ultimately compact structures of energy devices and set forth either the PPLSLS or Heat Rate maximum efficiencies; wherein, the forever technologies pack energy structures affected ultimately compacted, ultimate compact structures, the Universe energy structure packs energy into eternally compact structures.

16. The induction energy device said energy dynamics gravity fields do of claim 1, wherein Said forever technologies with said energy dynamics gravity fields spawn, spawns energy modes cycling dynamics engendering those gravity fields do, yield energy structures and energy devices Heat Rate efficiencies maximum efficiencies, in turn, yielding maximum service life longevities.

17. A procedure for packing the wound coil rows, the wound coil columns, comprising a procedure, the procedure, for making of the coils sets forth the wound coil rows, the wound coil columns of each coil specific number, each coil row specific number and a number of coils in each coils row and a number of coil rows in each layer of a dual layer or in one layer are comprised to configure an ultimate maximum number of wound precisely concentric coils of magnet wire and which is a maximum ultimate copper fill in stator slots each slot of an ultimate induction device, or a motor.

18. The procedure for packing the wound coil rows, the wound coil columns of claim 17, wherein the procedure winds precisely concentric the wound coil rows, the wound coil columns, by each coil specific number, each coil row specific number, a number of coils in each coils row having a number of coil rows in a layer or layers of the dual layer and is comprised to embody an ultimate maximum number of the coils of the magnet wire that yield the maximum ultimate copper fills in each of the stator slots of the ultimate induction device or an electrical motor; where, the wound coil rows wedge the coils row compressed in a winding pattern of each row of the wound coils of pre-insulated coils, where the wound coil columns push each of coil row each outermost coil into grooves and ridges in insulation of respective walls of each slot, which wedges in each coils row.

19. The procedure for packing the wound coil rows, the wound coil columns of claim 17, wherein the procedure for packing of the coils grants lapping each of electrical phases by a coil and coils and lapping any two phases by a coils pair, or pairs of coils, or the three phases by three coils and pairs of the three coils and one phase, two phases, and three phase combinations of coils in a dual layer, each layer of the dual layers, or a single layer, or in any number of precise specific lapping dispositions comprised lapping dispositions in stator slots of an energy device, or a motor device.

20. An electrical wiring procedure that wires wound coil rows, wound coil columns wound precisely concentric magnetic wire coils comprised of a preferred gage of a hexagonal wire cross-sectional area, by designating coils row number with designated wire coils each wire coil number, in stator slots of a stator yoke in an energy device comprised an electrical motor or an electrical generator.

21. The three phase, four pole induction motor of ultimately compact device of claim 8, wherein the ultimate energy device outflows thermal radiation to space and into ground surface, whereby thermal load is reduced on cycling phases in Air Cells energy dynamics; concomitantly air intake ports direct air circulation at the motor to run cooler at higher Heat Rate efficiency, which avoids a cooling fan and preferably further boost the motor Heat Rate efficiency.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0892] FIG. 1 on Drawing page 1 of 7 shows a simplified top view of the ultimate induction device;

[0893] FIG. 2 on Drawing page 2 of 7 provides a simplified axial view of the ultimate induction device of the present invention;

[0894] FIG. 3, FIG. 4, FIG. 5 on Drawing page 3 of 7 provide a stator slot make up and a Procedure for packing winding coils;

[0895] FIG. 3 illustrates a cross-sectional view of a stator slot 19 having a plurality of 60 slots in stator 101;

[0896] FIG. 4 shows slot 19 in a single layer, no slot phase separator 41;

[0897] FIG. 5A of FIG. 5A, FIG. 5B, FIG. 5C illustrates packing procedure;

[0898] FIG. 5B of FIG. 5A, FIG. 5B, FIG. 5C illustrates packing procedure;

[0899] FIG. 5C of FIG. 5A, FIG. 5B, FIG. 5C illustrates packing procedure;

[0900] FIG. 6 on Drawing page 6 of 7 provides electrical wiring diagram for three phase, four pole electrical motor;

[0901] FIG. 7 on Drawing page 4 of 7 details three stator slots portion shown coil windings of Section 9-9 of the stator;

[0902] FIG. 8 on Drawing page 5 of 7 details Section 8-8 two rotor slots portion of the rotor; and,

[0903] Three figures Comparison FIG. 9A, FIG. 9B and FIG. 9C on Drawings page 7 of 7;

[0904] The first of the illustrated slots shows the Prior Art on page 7 of 7;

[0905] FIG. 9B figure of FIGS. 9A, 9B and 9C shows the same slot outline of the first figure and the present invention compacting procedure affected nigh 98% compaction copper fill by copper wire coils;

[0906] FIG. 9C figure more of coil windings replaces the Prior Art, Drawings page 7/7.

DESCRIPTION OF THE SPECIFIC EMBODIMENTS

[0907] FIGS. 1 and 2 of the ultimate induction device 100 motor 10 and FIG. 3-5 stator slot show crucial energy device genres that in very significant aspects vary from the prior art, which the following explain; noteworthy among many is a moving vehicle about doubled range Heat Rate efficiency. Wherein, motor shaft 22 is coupled to rotor 102 supported on bearings of stator 101. Motor shaft 22 of motor 10, which comprises the ultimate energy device 100, comprises means for coupling various drive train devices and mechanisms. The motor 10 utilized in many varied mechanisms.

[0908] FIG. 1 shows a top view of an ultimate induction device 100 in an automobile setting, where a car's rear axle is also a shaft 22 of a rotor 102. The FIG. 1 illustrates fundamental outline of the device 100 detailed, herein. Aspects of the present invention are susceptible of embodiments in many different versions. There is shown in the present invention specific embodiments with the understanding that disclosures of the present invention are exemplifications in fundamentals of technologies advanced sciences, wherein energy devices, technologies and sciences advancement are one and the same. Wherein, the prior sciences, technologies and art stray into bizarre claims.

[0909] Said embodiments different versions also very numerous in the prior art herewith examples show are less than environmentally friendly, which should be amply corrected to conform, preferable sooner rather than later. The ultimate energy device, motor 100 a simplified schematic, shows Rotor 102 coupled to shaft 101. Rotor 102 is separated from stator 101 by air gap 15 between 0.5 millimeters and 0.8 millimeters, shown end rings 103 and is coupled to shaft 110 engenders axial centerline 104 and, also, axial centerline of the stator bore. Air duct 107 and air duct 108 direct air flow at the motor under a moving load due to a vehicle in motion. Air filter 109 in air duct 107 and air filter 109 in air duct 108 filter air directed at the motor. Air outflow duct, stack 111, extends from above stator 101 affecting a very small air separation from stator and extends upwardly through a body periphery of the vehicle, where stator 101 is exposed to radiate thermal energy into ground surface and through air outflow duct stack 111 and the atmosphere. Wherein, another aspect of the ultimate energy device outflows thermal radiation to space and into ground surface, whereby thermal load is reduced on cycling phases in Air Cells energy dynamics, while the motor runs cooler at higher Heat Rate efficiency. Concomitantly, air intake ports direct air circulation at the motor to run cooler at higher Heat Rate efficiency, which avoids a cooling fan and preferably further boost the motor Heat Rate efficiency. The vehicle may have one motor or up to two motors per axle. Preferably, stator 101 has black color two shellac protective coatings, protection against weather elements, wherein a blowing fan to cool the motor is avoided, which may further boosts Heat Rate efficiency of the motor. Proximate the stator, preferably stack 111, air duct 107 and air duct 108 are made of aluminum. Air intake portal locations for air duct 107 and air duct 108 proximate location of the motor may be situated under a chassis, in general, in front of wheel wells in the rear side panels and in a front grill and side panels of the vehicle. The ultimate induction device 100 motor may very well double the EPAct Energy-Efficient, NEMA Premium Motors Minimal Nominal Efficiency respective range of 87.5 to 96.2 at 100% load. FIG. 3 and the Prior Art FIG. 9B explained illustration further explain this aspect of the present invention.

[0910] FIG. 2 shows a cross-sectional area axial view of the motor 10 of the ultimate induction device 100 simplified schematic, shows stator 101, stator yoke 102, rotor 102, rotor yoke 11, stator slots 19, stator teeth 18, rotor slots 23, rotor teeth 24, motor shaft 22 and stator diameter 20. Section 9-9 and Section 8-8 of motor 10 of ultimate induction device 100 respective portions respective sectional configurations of stator 101, rotor 102. For illustration purposes, a 60-slot stator 101 is selected, where for three phases at least two poles per phase, here, four poles per phase make 24, 36, 48, or 72 slot common arrangements. Electrical schematic diagram of three phase, four poles configuration known in the art FIG. 6 illustrates. For illustration purpose the present invention is taken to have eleven coil rows; where, a coil row is compacted in specific order from row one to eleven in precisely concentric wound coil rows, wound coil columns wound precisely concentric magnetic wire coils. That specific aspect of the present invention FIG. 3-5 illustrate and explain. Motor 10, affects physically compacted compact energy structure and the ultimate energy device, the ultimately compact structure 100 in a moving vehicles embodies stator 101 of laminated steel plates, consistent with best manufacturing practices for making such structures, including quality assurance paper work, for steel plate laminating, for copper entry stock, for insulating insulation, physically marked, where appropriate. Steel laminations of stator 101, yoke 112, slots 23, and teeth 24 are manufactured by computer-controlled laser cutting machines, preferably cut in one piece. Wherein, said stator, yoke, slots and teeth common length, according to empirical data the prior art derived, is preferably less than 1.50 of stator diameter 20. Stator slots 19 small compact slots and stator teeth 18 warrant a corresponding small stator yoke 112, stator 101 smaller lighter ultimately compact structure 100 of the ultimate energy device, motor 10, than the prior art. The present invention and the maximum ultimate copper fill by a hexagonal barely rectangular cross-sectional area of wound coil rows, wound coil columns wound precisely concentric wire coils in yoke, stator 101 lighter structure higher Heat Rate efficiency can double range of energy devices.

[0911] FIG. 3 illustrates a cross-sectional view of a stator slot 19 having a plurality of 60 slots in stator 101. Stator teeth 18, one on each of two sides embrace a slot 19. Preferably, cross-sectional area of hexagonal barely rectangular cross-sectional area of the magnetic wire coils fills each slot 19, in fact, yielding the maximum ultimate copper fill in each slot 19. From a structural aspect point of view, hexagonal wire cross-section packs well, yielding maximum surface areas suitable to fill a plurality of slots of slot 19. Preferably, a barely rectangular cross-section is utilized. Empirical data suggest that preference and arranged, which recognizes and preserves as such the sui generis boundaries of hexagonal geometrics, which, concomitantly engender, where properly packed and configured structure comprising a maximum cross-sectional area and maximum surface area, and extremely stable energy structure. Dual layer 43 44 is that structure; wedged into the groves and ridges in stator teeth 18 stator slot 19 perimeter, unpacking of dual layer 43 44 energy structure is an impossible possible task. Thermal energy could possibly do it. Wherein, rectangular hexagon cross-sectional area of the coils 1 and the slots 19 absolutely maximized respective perimeters 39 18 and 38 19 surface areas maximized heat energy outflow thru conductance of the compressed insulation needed volume least thicknesses 39 of electrical insulation least volume needed and in insulation coat of the wire windings of the coils 1 and the insulation lining of the stator teeth 39. Wherein, weak axis of coils 1 facilitates bending of the coils 1, while strong axis minimizes all twisting of the wire windings of the coils 1, which conserves current and magnetic flux densities.

[0912] For the above listed reasons, coils 1, coil numbers 42, dual layer lower layer 43, upper layer 44, stator slot perimeter 39 19, stator teeth perimeter 39 18 and insulation 39 needed least volume, all comprise individually and in common the sui generis boundaries of the stator slots 19. Slot wedge 37 hooks under teeth lip 45 assures coils 1 42 stay in place; stator slot bottom is marked 47 and the top is 48, where phase insulation is marked 41 and 11 coil rows is marked 38R. Most importantly these energy, structure boundaries engender concomitantly maximum electrical and electromagnetic densities highest conductance least thermal energy byproduct and, in turn, the thermal energy byproduct highest outflowing conductance. Wherein, stator yoke 112 completes that outflowing consistent with the prior art empirical data. Where, motion of a moving vehicle is performing useful work and thermal energy byproduct increases the ultimate induction device 100 outflowing that energy increases by faster moving of that moving vehicle; wherein yoke 112 radiates, at the speed of light, a thermal energy portion to Earth's surface for irradiation and into the Universe energy structure, the potential energy one field, which make the ultimate induction 100 device participate in the Wheel of Nature cycling energy thru the Universe energy structure. Summary of the Invention details numerous aspects of these issues in technologies and sciences. The ultimate induction device 100 in a moving vehicle affects Heat Rate efficiency high possible and way above EPAct Energy-Efficient, NEMA Premium Motors Minimal Nominal Efficiency respective range of 87.5 to 96.2 at 100% load and may very well double such efficiency ratings. Stator 101 affects large torque at 100% load and thus can run cooler than conventional motors; preferably yoke 112 thickness is less than 100% larger than stator teeth 18 length Lsl and each stator tooth 18 length Ls1 is in range of four to seven times larger than minimum width Wst, and, where, preferably ratio of stator diameter to stator length is less than 1.5.

[0913] FIG. 4 shows slot 19 in a single layer, no slot phase separator 41, which, likewise shows, where preferred, stator slots filled with coil wires having hexagonal cross wire can readily compact in more than two layers, which reduces number of coil wires concomitantly wound. Wherein, for practical purposes wire coils one coil row at a time is concomitantly wound and wedge in place.

[0914] FIG. 5A, FIG. 5B, FIG. 5C illustrates packing procedure, the procedure, for packing coils row 1 to 11 38R in stator slots 19, where anvil bobbin 72 is inserted into stator slot 19 on top of the slot bottom 47 on top of insulation 39, enumeration 34 or on top of previously packed coils which is enumerated 34. FIG. 5A show alignment prior to compacting coil rows 1, 7, 9 and 11, with five coils of coil rows 1-11 38R, by bobbin hammer 31. Bobbin anvil 33 and bobbin hammer 31 have side extensions, arrows shown, and are capable of breaching a stator slot 19 largest width Lsb2. The coils alignment and manipulating both bobbins occurs at either end or both ends of a stator slot 19. Coil numbers FIG. 3 shows, where FIG. 5A shows five coils placed in top row 57, bottom row 55 between hammer bobbin and anvil bobbin aligned for compaction. In position for compacting, coils 1, 2, 3, 4 and 5 are kept in that position by light tension. When hammer bobbin 58 comes down and pushes on coil 3 57, coils 1 and 5 of coils 1 2, 4 and 5 55 push against slot insulation 39; at that moment, anvil bobbin 72 is pulled out from under coils 1, 2, 4 and 5. Under pressure by hammer bobbin 58 outside coils 1 and 5 compress flexible portions of slot insulation 39 and wedge into grooves and ridges in predetermined positions and compresses insulation 39, compressing lightly flexible coating of coils 1, 2, 3, 4 and 5, which wedges in place these coil numbers of rows 1, 7, 9 and 11 in an ultimate compaction of rows 1-11 in stator slot 19, and wedge into grooves and ridges in predetermined positions now in compressed insulation 39. Wherein, FIG. 5B shows compacting of six coils of row 2, 4, 6 and 8 of coil rows 1-11 38R, where coil number 2 and 5 are positioned in a row 52 on top of coils 1, 3, 4 and 6, where coil 2 is centered on top between coils 1 and 3 and coil 5 is centered on tip of coils 4 and 6. Light tension in coils keeps coils in that position, when hammer bobbin 58 comes down and pushes on coils 2 and 5 52 to respectively separate coils 1 and 3, coils 4 and 6, where outside coil 1 and 6 push against slot insulation 39; at that moment, anvil bobbin 72 is pulled out from under coils 1, 3, 4 and 6. Under pressure by hammer bobbin 58, outside coils 1 and 6 compress flexible portions of slot insulation 39 and wedge into grooves and ridges in predetermined positions now compressed insulation 39. FIG. 5C shows compacting of seven coils of row 3 and 5 of coil rows 1-11 38R, where coils number 2, 4 and 6 are positioned in a row 54 on top of row of coils 1, 3, 5 and 6 and coil 2 is centered on top between coils 1 and 3, coil 4 is centered on top between coils 3 and 5 and coil 6 is centered on top and between coils 5 and 7. Light tension in coils keeps coils in that position. Hammer bobbin 58 comes down and pushes on coils 2, 4 and 6 54 to respectively separate coils 1 and 3, coils 3 and 5 and coils 5 and 7, where outside coil 1 and 6 push against slot insulation 39; at that moment, anvil bobbin 72 is pulled out from under coils 1, 3, 5 and 7. Under pressure by hammer bobbin, outside coils 1 and 7 compress slot insulation 39 flexible portions and wedge into grooves and ridges in predetermined positions in compressed insulation 39. Row 10 passes through slot opening; hammer bobbin 58 pushes row 10 in place as one unit.

[0915] Unavoidably, light pre-compressing of coil rows by hammer bobbin 58, lightly pre-compresses coil columns, which rows 1-11 comprise. Said pre-compressing put stator slots 19, stator teeth 18 in pre-compression hoop stresses by slots 19 packing. In turn, pre-compression of stator teeth 18 and fill of stator slot 19 affect tensile pre-stress in stator yoke 112, where pre-stressing energy in each stator teeth 18, in each stator slot 19 and yoke 112 by stresses energy action and energy reaction act as one structural unit and structural stresses uniformly distributed circumferentially and radially. In turn, thermal load stresses also distribute and outflow in same uniform manner comprising the maximum conductance of thermal byproduct outflowing. FIG. 6 shows electrical diagram of the winding coils for three phase, four poles per phase motor well known in the prior.

[0916] FIG. 6 electrical diagram shows the three phases of A1, A2, A3, A4 and B1, B2, B3, B4 and C14 C2, C3 and C4 poles arrangement. Summary of the Inventions details the Procedure for packing of these winding coils.

[0917] FIG. 7 details a stator plate Section 9-9 of stator 101 comprising stator yoke 112 thickness T.sub.sy, slot opening width L.sub.st, slot wedge 37, stator teeth 18 width W.sub.st, phase separation insulation 41, stator slots 19, slots width Lsb1 and Lsb2, slots bottom or base 47 and slots top 48. Stator slots 19 are spaced equally six angular degrees apart and stator teeth 18 are space equally six angular degrees apart, comprising said slot widths and said slot teeth width through 360 angular degrees. Slots top 48 is proximate the stator bore, where slot bottom or base is away from the stator bore. Stator teeth lip 45 comprise portion of the sui generis boundaries of stator teeth, which interface with the sui generis boundaries of the winding coils in dual layer top layer 44 and bottom layer 45 in stator slots 19, where coil row 11 wedges into flexible portion of slot insulation 39, under the stator lip 45. FIG. 3 description details high structural integrity of stator slots 19 stator teeth 18 pre-compressed by packing of the coils, thus, comprising very stable structure configuration with stator yoke, where stator teeth width is primarily electromagnetic density consideration for which empirical data is not available. Wherein, pairs of winding coils, which keeps each stator slot respective symmetry and each stator teeth symmetric may be added to each layer of a dual layer or a single layer. In turn, the sui generis boundaries between stator slots 19 and stator teeth 18 is maintained, providing enormous versatility in affecting stator slots and teeth configurations. Computer-controlled laser cutting machines cut steel plates of stator 112 laminations, preferably in one piece blank forms precise laminations fabrication, which includes subsequent annealing to maximize electromagnetic properties. Preferably, the computer-controlled laser cutting machine is programed to cut no smaller fillet radius than one programmed into computer that does affect precisely same outside fillets of the preferred hexagonal barely rectangular cross-sectional area of the magnetic wire coils, which the Turks Head machine does manufacturing the magnet wire coils. Punch press stamping blank stator plate laminations is acceptable, provided smooth inside and outside said small radius radii can be fabricated by a stamping of blank stator plates.

[0918] FIG. 8 shows a Sectional 8-8 of rotor 113 detailed two rotor slots 24, where each rotor tooth 24 comprises uniform thickness two parallel surfaces of each rotor tooth 24, rotor 113 yoke having thickness T.sub.ry, each rotor tooth 24 thickness W.sub.rt, rotor tooth length Lrt and a rotor slot 23, having a slot bridge thickness Br. Rotor slot top is designated 401 and rotor bottom designated 402, number of rotor slots is 72, where, preferably ratio of rotor teeth width to stator teeth width is between 1:1 and 1:1.2 and a number and number of rotor teeth is about 15% greater than the number of the stator teeth, and rotor yoke thickness T.sub.ry to rotor tooth length in range of about 25% to 70% larger.

[0919] Illustrating the present invention visual significant improvements of the Prior Art three figures of the Drawings page 7/7 visual appearance of three slots respective cross-sections show. All three figures show an outline of a slot the Prior Art slot has. The first of the illustrated slots shows the Prior Art slot cross-section, claiming concentric wound coils, which in a broad context they are. Such compacting at best achieves 75% copper fill in a slot. FIG. 9B figure shows the same slot outline of the first figure and the present invention compacting procedure affected nigh 98% compaction copper fill by copper wire coils. Each coil cross-sectional area is about 15% larger than the cross-sectional area of the wire coils FIG. 9B figure shows, comprising the present invention precisely concentric coil windings. About 15% of slot volume 181 comprising access insulation can be replaced either by more copper fill. FIG. 9C figure shows that 41% more of coil windings replaces said access insulation. All thee figure illustrate dual layer, where first and second figure show each layer having 22 coils, but coils in FIG. 9B have 15% larger cross-sectional area; the FIG. figure shows 31 coils in about the same slot perimeter and each coil 15% larger cross-sectional area, where 22+ and 31+ designates such larger areas cross-sections. Total magnetic flux density, B=.sub.o Ni/l, where .sub.o is magnetic constant, N the number of turns, i the current 1 and the length of coil. Ignoring end effects, the total magnetic through the coil, =.sub.o NiA/l, where A is cross-sectional area of the coil, and N and A affect the maximum ultimate copper fill and the length l, the least length of the coil for precisely concentric wound coils in the slot. And, we knowfor certainelectrical current conductance, thermal energy conductance is nigh absolute maximum, since the compressed insulation needed volume least thicknesses of electrical insulation least volume needed is in each slot and in biaxial compression by packing Procedure and in the slot triaxial compression spawned by thermal expansion of copper fill. All of which aspects of the present invention address.