Background--Field of Invention This invention relates to spark control on the commutator, specifically zero spark suppression whereby full cycle sparking and plasma streams with resultant charge clusters, radiation, electromotive force, discrete wave and discrete particle generation are achieved.

Background--Description of Prior Art All previous commutators used in DC motors or generators have been designed to reduce sparking by etaborate means whereby no examples are referable as simiiar, only contrary by means. Traditional design goals have been to reduce commutator sparking, yet complete suppression seems to be mythical. The common physical effects include hysteresis, inductive and conductive heating in the armature and rotor facilitating the need for heavy gauge 600 degree insulated conductors, special heat resistant bonding agents, and air flow cooling means which further reduces efficiency. Sparking by itself adds to commutator erosion and added heating, also requiring cooling. Counter electromotive force, generally referred to as counter-EMF is evident in both modern and historic patent designs and has been considered something to avoid. Likewise the effects of the Collapsing Magnetic Field, further referred to as CMF, is caused when a complete break in the circuit occurs at the commutator resulting in conductor erosion and copious heat production.

(a) When a motor/generator uses laminate steel as an armature or coil support, it is these laminates which add useless weight, carry eddie currents & interfere with permanent and generated magnetic fields.

(b) Counter-EMF also contributes to magnetic breaking which requires additional current to drive the motor to required speed.

(c) Past motor/generator design had only low flux density magnets available to them, requiring application of greater currents to drive the electromagnetic fields. This resulted in high internal heat which proved problematic for the high BH. sub. max permanent magnets otherwise known as neodymium iron boron, having a relative low curie point.

(d) U. S. patent 5,861,693 Takahashi: Yoshiaki (01/19/1999) is for a motor using now conventional components such as high BH. sub. max permanent magnets, however its use of steel laminates causes drag within the high strength magnetic fields, creating useless heat and further built-in inefficiencies to overcome. Furthermore his use of induction coils to produce electricity is not new as evidenced in U. S. patent 5,661,354 to Burtis; Wilson A. (08/26/1997), U. S. patent 5,408,165 to Voet; Eduard J. (04/18/1995) and U. S. patent 4,720,662 to Lanser; Leslie V. (01119/1988). These methods seem to rely on the lines of force from the permanent magnetic field cutting through the conductor to produce a flow of current as in a standard generator. This is known and indicated by Takashi when he states, a lower power consumption by omitting the induction coil from the above mentioned motor.

(e) ln U. S. patent 5208844 to Puthoff : Harold E (Austin, TX); Church, Jr.; George W. (San Antonio, TX); Clifton; David B. (Leander, TX); Little; Scott R. (Austin, TX) (05/04/1993) and U. S. patent 5153901 to Shoulders; Kenneth R. (Austin TX) (10/06/1992) we find the use of voltages at a high potential, near 30KeV and bulky equipment are needed to produce charged particle clusters, radiation, EV and possible NEV effects, however system charge times are not mentioned and presumed slow. In U. S. patent 5,034,183 to Blewett; John P. (07/23/1991) it states that tritium production occurs as well as producing anti-protons at multi-GeV energies, specifically anti-hydrogen.

(U. U. S. patents 512,340 to Tesla; Nikola (01/09/1894) and 685957 to Tesla ; Nikola (12105/1901) might be of use herein, however my system is not limited to DC motor operation, it also has means for sub-atomic particle discovery.

Summary Including Objects and Advantages A pulsed plasma electromagnetic motor, comprises a novel commutator, a hermetically sealed plasma area, energy sensors, a pulsed plasma flow of voltage allowing DC motor operation, charged participe clusters, discrete particles, discrete waves, having means of radiated energy retrieval, x-ray transmission and anti-matter factors are present.

Objects and Advantages Accordingly, several objects and advantages of my invention are the novel use of unsuppressed sparking to generate a multitude of heretofore unrealized effects in an electromagnetic motor of unique properties using a standard coil and rotor design. This novel approach insures absolute zero spark suppression, thereby allowing a pulsed field motor/generator to access heretofore unavailable energies from the CMF as well as now useful counter-EMF forces which have caused commutator destruction as far back as the first electric motor in circa 1835. This unique electrical transmission means allows advantages far in advance of simple use in motor/generators. High energy particle division and associated transmutation at sub-GeV, even sub KeV applied energies now seems possible.

Still further objects and advantages will become apparent from a consideration of the ensuing description and accompanying drawings. Other possible effects are the generation of positrons. anti-matter, gravity waves, magnetic vortexes and an altered space-time reference from one or more of the following; rotating magnetic fieids, pulsed magnetic field, EV and emitted radiation resultant of charged particle clusters, EMP and regenerative means, CMF and counter-EMF containment in a resonant circuit, eddy current suppression. Regardless of theory, the groundbreaking discovery of Entropy or heat loss has been evidenced therewith repeatedly in the system.

(a) The use of steel laminates near high BH. sub. max magnets, results in system drag as these magnets are attracted to even stainless steel, thereby laminate use is to be avoided. As magnetic attraction to aluminum, copper and other metals is evident, the novel use of non-conductive support elements is suggested, whereby hysteresis and eddy currents can not propagate. Support elements include coif supports, housing & core elements. Use of extraneous conductors should be limited to standard exterior RF shielding as required, however this may be at a distance depending on requirements, in example a test room shield.

(b) Previous commutation means lead to suppress counter-EMF as it causes magnetic breaking which must be overcome by applying higher driving currents to counter its effects, thus causing an increase in system heating resulting in, removal means and requiring excess insulation and increased wire gauge. Whereas my novel commutator not only refuses to neutralize counter-EMF but transmutes its use into increased system performance, whereby small wire gauge transmission means are possible as current flow is restricted within this system and even substantial lengths of fine 38 GA wire can be used with minimal thermal radiation, and at times remission.

(c) High BH. sub. max permanent magnets with a field strength higher than 36 MGOe such as 50MGOe, 100 MGOe and higher are required for specific function in my devices.

(d) Induction coils as such are not used, the function of the receiving coils are to collect discrete and tuned energies radiated from the pulsed electromagnetic field and should be positioned at a distance, not to interfere with but receive the signal for transformation. The receiving coil can envelope the drive coil or be placed adjacent to it, whereby under direct short circuit should not cause substantial drag on the magnetic core due to induction, as this is not its main energy collection goal.

(e) Whereas others use KeV and GeV charges to attain particle separation and system charge times vary, my system demands are fractional in comparison. In my device the system supply voltage is fractionat however voltage potential within the plasma is extremely high, contained. and fast in cycle. A rate of 2.200 plasma discharges per second is normal and even if a potentially smaller particle separation were to be expected in each cycle, an increased efficiency over current devices would be anticipated.

( Due to the extremely low power consumption of my device, the patents of Nikola Tesla from the past may shed new light in the future as well as provide a means to capture the needed energy to run, as well as recapture radiated energies from within this system. A suitable antenna can be used to recapture the energy, however meager required to sustain core movement.

Brief Description of the drawings Fig. 1 is a two part view of my invention.

Fig. 2 is a side view of magnetic rotor 16.

Fig. 3 shows two views of the commutator.

Fig. 4 is a schematic view of my invention.

Fig. 5 is a partial view of an alternate contact placement.

Fig. 6 is an altemate embodiment and new use solenoid.

Fig. 7 is an alternate embodiment and new use rotary spark gap.

Fig. 8 is the general waveform.

Reference Numerals 9 power generating electromagnetic motor 10 receiving coil 12 drive coil 12A drive coil 13 drive coil assembly 14 high BH. sub. max permanent magnet 14A high BH. sub. max permanent magnet 16 bi-polar magnetic rotor 18 core element 18A core element 20 shaft 20A shaft 20B shaft 22 pulsed plasma commutator 24 non conductive disk 26 shaft insulator tube 28 annular conductive ring 28B annular conductive ring 30 pulsed solenoid 32 arched lobe 32A arched lobe 36 peripheral surface 36A peripheral surface 36B peripheral surface 38 radial contacts 38A radial contacts 40 momentary starter 42 conductor wire 42A conductor wire 42B conductor wire 42C conductor wire 42D conductor wire 42E conductor wire 42F conductor wire 44 pulsed plasma spark gap 46 ring contact bar 46A ring contact bar 50 tension bar 50A tension bar 54 tension spring 54A tension spring 62 terminal 62A terminal 62C terminal 64 primary firing assembly 66 primary contact 66A primary contact 68 primary contact holder 70 primary conductor terminal 72 primary adjustment means 72A primary adjustment means 73 primary guild 74 tube retainer 78 drive coil wire 78A drive coil wire 78B drive coil wire 78C drive coil wire 82 capacitor 82A capacitor 84 capacitor terminal 84A capacitor terminal 86 wire 86A wire 86B wire 86C wire 86D wire 86E wire 86G wire 86H wire 861 wire 86J wire 88 DC battery 88A DC battery 90 battery terminal 90A battery terminal 90B battery terminal 90C battery terminal 92 junction 92A junction 92B junction 94 spring bar 94A spring bar 96 magnetic coupler 96A magnetic coupler 96B magnetic coupler 96C magnetic coupler 98 hermetically sealed container 100 bonding filler 114 valve 114A valve 116 post 116A post 118 threaded bar 120 bearing 120A bearing 120B bearing 120C bearing 122 point 122A point 122B point 122C point 122D point 122E point 122F point 124 frame 126 contact 128 slot Preferred Embodiment--Description Referring to Fig. 1, a power generating electromagnetic motor 9 consisting of a drive coil assembly 13 attached to a magnetic coupler 96C adjacent to a hermetically sealed container 98, which contains a magnetic coupler 96B so attached at point 122B is a shaft 20 journaled through a bearing 120 and a bearing 120A, at point 122C a novel pulsed plasma commutator 22 as detailed in Fig. 3, is secured by a tube retainer 74 in a shaft insulator tube 26 so affixed is a non conductive disk 24, thereon its peripheral face 36 is an arched lobe 32 holding radial contacts 38, said arched lobe 32 is affixed to a conductor wire 42 so affixed to an annular conductive ring 28 in sliding contact with a ring contact bar 46 so affixed to a tension bar 50 so attached to said conductor wire 42 ending at terminal 62 and said tension bar 50 is attached to a tension spring 54 terminating at post 116. Counterpoised to said arched lobe 32 on said peripheral face 36 are radial contacts 38A so affixed to an arched lobe 32A so affixed to a conductor wire 42A so connected to an annular conductive ring 28A being in sliding contact with a ring contact bar 46A so attached to a tension bar 50A having a conductor wire 42C which ends at terminal 62A and said tension bar 50A is so attached to a tension spring 54A terminating at post 116A.

Referring to Fig. 3 primary adjustment means 72 has a magnetic coupler 96A with a suitable locking device outside of said hermetically sealed container 98 being magnetically coupled to a magnetic coupler 96 so affixed to a point 122B of a threaded bar 118 secured by a bearing 120B and a bearing 120C whereas said threaded bar 118 is journaled through a primary firing assembly 64 at point 122A, to said assembly 64 is attached a primary point holder 68 where a primary contact 66 is affixed, said primary firing assembly 64 terminates in a primary guild 73 and said holder 68 has affixed a conductor wire 42F which so ends at primary conductor terminal 70 and said hermetically sealed container 98 is so equipped with a valve 114 and a valve 114A for vacuum or gas insertion into said hermetically sealed container 98.

Referring to Fig. 1A, a drive coil assembly 13 consists of a receiving coil 10 adjacent to a drive coil 12 having a drive coil wire 78 and a drive coil wire 78A, said drive coil 12 holds a bipolar magnetic rotor 16 so journaled and secured to a shaft 20A by a bearing 120B and a bearing 120C whereas a magnetic coupler 96C is attached to a point 122D, adjacent to momentary starter 40 and said bipolar magnetic rotor 16 has, as referred to in Fig. 2 a core element 18 with suitably attached plurality of a high BH. sub. max permanent magnet 14, said bipolar magnetic rotor 16 with a bonding filler 100 to limit air drag in system.

Referring to Fig. 4, is a schematic diagram of main components; a DC battery 88, a DC battery 88A, a capacitor 82, a capacitor 82A, a receiving coil 10 so adjacent to a drive coil 12 having a drive coil wire 78 and a drive coil wire 78A, said drive coil 12 has an air gap so between bipolar magnetic rotor 16, so affixed to a shaft 20A at a point 122 is magnetic coupler 96C to so connect said bipolar magnetic rotor 16 to a hermetically sealed container 98. Connected to said drive coil wire 78 is a wire 86 which so connects to a junction 92 joining a wire 86B and capacitor terminal 84, said wire 86B is connected to a battery terminal 90A and a battery terminal 90 is then connected to a wire 86C that attaches to a terminal 62, said drive coil wire 78A is attached to a wire 86A which then attaches to a capacitor terminal 84A, a wire 86D completes the circuit by joining said capacitor terminal 84A and a primary conductor terminal 70 at a junction 92B. Then, said drive coil wire 78A is attached to a wire 86F then joining a wire 86G at a junction 92A so connecting battery terminal 90B, a battery terminal 90C is attached to a wire 86E so attached to a terminal 62A, and said wire 86G then attaches to a capacitor terminal 84C, a capacitor terminal 84B has attached both a wire 86H and a wire 861, said wire 861 is attached to said wire 86 which is so joined to said drive coil wire 78. The multiplex detector has an array 80 which ends at terminal 62C.

Referring to Fig. 5; is a partial view of an alternate configuration of the contacts, showing contacts 38 and 66 in relation to radial spacing in degrees.

Preferred Embodiment--Operation In the power generating electromagnetic motor 9 according to the present invention, a drive coil assembly 13 consists of a drive coil 12 and a bipolar magnetic rotor 16 so composed of a sufficient number of high BH. sub. max permanent magnet 14 elements designed in a cylindrical form with a uniform arcuate curve and an air gap between it and said drive coil 12. Said bipolar magnetic rotor 16 is designed to have a core element 18 composed of a soft iron or even an insulator, in either case steel laminates are not preferred whereby steel laminates should be prohibited from use in the drive coil 12 as their resultant drag against said high BH. sub. max permanent magnet 14 elements is proven, and creates power loss, increased power consumption, hysteresis & eddy current travel. Said core element 18 and said shaft 20A can be composed of other materials chosen from the group of high strength and low weight materials; such as, ceramics, carbon fiber composites, or titanium. Said bipolar magnetic rotor 16 can be finished with a suitable fiberglass wrapper and Gougeon bonding products or other suitable containment means. The object of a magnetic couplers 96B and C is to establish a positive magnetic lock as known to those skilled in the art, with said pulsed plasma commutator 22 as housed in a hermetically sealed container 98. The multiple function of said hermetically sealed container 98 is not limited to however includes, sealed sensor area, contaminant containment, gas vacuum, gas pressurization, radiation containment and direction. Furthermore, the magnetic couplers 96 and 96A are for adjustments of the primary without container breach or the added expense of robotics. The basic components associated with the plasma stream as housed in said hermetically sealed container 98 wherein said commutator 22 consists of; conductive rings 28 and 28A, ring contacts 46 and 46A. contacts 38 and 38A as well as contact 66 are, selected from the group of high metting point conductors, not limited to yet however in this case, platinum and tungsten.

An array 80 having a terminal 62C is a multiplex sensor to track various radiation levels, charged particle clusters, discrete particles, discrete waves, EV and possible NEV as referenced in patents, #685957,5034183 and 5208844. Under the influence of patent # 512,340 it may be feasible to remove capacitance completely from the system.

The suitable spacing of radial contacts 38 and 38A has been found to be near 5 degrees between each radial contact so affixed to a lobe, however such adjustments to voltage and capacitance can effect optimal spacing allowing even doser spacing as long as an intermittent firing sequence is maintained. Therefor one can predict the use of fewer radial contacts and increased as well as staggered positioning of the primary contact 66 as in Fig. 5 showing, a 20 degree spacing is compensated by multiple primary contact 66 spaced at a 5 degree radius. A further option for contact placement include positioning the radial contacts facing inward toward a central primary contact as well as other spacing is possible, as long as the full pulsed cycle is maintained between each firing sequence, unless a fractional area of the wave form must be isolated for specific use.

Proper voltage is applied to the system as referred to in Fig. 1; momentary starter is activated, initiating the rotation of bipolar magnetic rotor 16 as referred to in Fig 1A, resulting in the annular rotation of said pulsed plasma commutator 22 aligning a radial contact 38 into electrical contact with primary contact 66 of primary firing assembly 64, it is only necessary to move the commutator a maximum of 15 degrees or until electricat contact is made. When contact is made a pulse of electrical energy is sent into the drive coil 12 where resultant electromagnetic force causes the rotor 16 to move, resulting in a break in the electrical flow as contacts disconnect in passing. This break causes a collapsing of the electromagnetic field, squeezing the electrical charge from the drive coil 12 resulting in tremendous force buildup as the charge attempts to leave, yet is trapped within the system. At this time an undamped AC current component is introduced into the system which may act to recondition the DC batteries or add discrete components useful to this system. It is at this point extremely high voltage potentials are reached and nuclear bond breakdown occurs forming x-rays, anti-matter components, EV charged particle clusters as well as others. I believe the electrical collapse is responsible for stripping sub-atomic components from the retreating charge, not aboie to fully retreat, whereby removing its natural balance, a balance is sought within the system pulling at forces through the insulators themselves.

Because the natural balance has been altered, now trapped it attempts equilibrium through nuclear attraction of exterior matter from within or without our current space-time reference, producing the physical presence of entropy in the system. The excess charge which now is lacking within the system, radiates in the plasma at primary contact 66. Whereas the dis-equilibrium within the system is spread throughout a relatively large amount of matter and can be considered dilute, whereby the excess charge now radiating within the plasma is extremely compact and potent. Energies heretofore called counter-EMF should slow rotation, yet do not show this effect and are believed to be converted into or part of the AC component which radiates to the extemal receiving coil for recycling. What appears to happen is, the energy of resultant discrete and counter-EMF force is sent into resonance with the circuit of the capacitor 82 and DC battery 88 whereby trapping this energy in a fluctuating waveform of decreasing amplitude as referred to in Fig. 8. This is only one form of energy radiating from the system and can be collected at a distance from the system. As the waveform subsides and with proper rotation, inertia in the rotor 16 brings the next radial contact into connection with the primary contact 66 repeating the process until the next lobe of contacts is reached. When the primary contact is aligned with the next radial contact the voltage is so switched in relation to the former, each point in succession fires voltage directly into the drive coil that now forms a resonant circuit with capacitor 82A and battery 88A. The primary contact is both the anode and cathode, however in altemate lobe contact. in only the most basic form, this system runs in accordance to a DC motor however by novel means, as known to those skilled in the art this is a sub-atomic particle generator operating with anti-matter factors.

As the commutation means reduces power consumption to heretofore unattainably low current draw. I believe patent # 685,957 will be of assistance in running the aforementioned device from the radiant energy not normally accessible within or out of the atmosphere.

Referring to Fig. 4, is a schematic view of the invention described in the main embodiment.

Pulsed plasma commutator--Description A novel pulsed plasma commutator 22 as detailed in Fig. 3, is secured by a tube retainer 74 in a shaft insulator tube 26 so affixed is a non conductive disk 24, thereon its peripheral face 36 is an arched lobe 32 holding radial contacts 38, said arched lobe 32 is affixed to a conductor wire 42 so affixed to an annular conductive ring 28 in sliding contact with a ring contact bar 46 so affixed to a tension bar 50 so attached to a conductor wire 42 ending at terminal 62 and said tension bar 50 is attached to a tension spring 54 terminating at post 116. Counterpoised to said arched lobe 32 are radial contacts 38A thus affixed to an arched lobe 32A so affixed to a conductor wire 42A so connected to an annular conductive ring 28A in sliding contact with a ring contact bar 46A thus attached to a tension bar 50A so attached to a conductor wire 42C ending at terminal 62A and said tension bar 50A is attached to a tension spring 54A terminating at post 116A.

Pulsed plasma commutator--Operation The pulsed plasma commutator 22 operates as in the main embodiment however, can be attached to a standard DC motor by one skilled in the art, as it is not just a DC motor I desire to protect, its main component is the commutator.

Plasma drive solenoid--Description Referring to Fig. 6 and 6A is a novel use pulsed solenoid 6 consisting of a drive coil 12A having a drive coil wire 78B and a drive coil wire 78C, within said drive coil 12A is a high BH. sub. max permanent magnet 14A so connected to a core element 18A so connected to a shaft 20B which is journaled through bearing 120D and held in position by a slot 128 as suitably journaled, said shaft 20B has suitably affixed a contact 126 which is connected to a conductor wire 42D which so connects to a suitable point 122F on frame 124 of which is suitably connected to said drive coii 12A. At a point 122E on said frame 124 is attached a primary adjustment means 72A which holds a primary contact 66A, a conductor wire 42E is attached to said primary contact 66A through said primary adjustment means 72A.

Plasma drive solenoid--Operation The pulsed solenoid 30 can now benefit from the heretofore destructive forces of the collapsing electromagnetic field and also generate power on post plasma discharge on assent as in Fig. 6A showing maximum extension, and at rest as in Fig. 6 which refers to starting position. Battery power and capacitance is applied in a standard manner as know to those skilled in the art, to drive coil 12A at drive coil wire 78B and conductor wire 42D whereas drive coil wire 78C is attached to conductor wire 42E of primary adjustment means 72A which is positioned at a point 122E on an insulated frame 124. A bearing 120D is preferably constructed of TFE for long lasting service as well as hold a shaft 20A also preferably constructed of TFE or a material coated in it in a stable gliding position by slot 128, so alignment is maintained between contact 126 and primary contact 66A for proper voltage transfer. Said shaft 20A can take any formed shape that matches receptacle of said bearing 120D so long as alignment of said contact 126 and primary contact 66A is maintained. Said contact 126 is connected to conductor wire 42D so suitably affixed to suitable point 122F on said frame 124. When voltage is applied to this unit at rest, the primary contact 66A is in contact with contact 126 producing a flow of electricity through said drive coil 12A thereby producing a magnetic field. This magnetic field pulls the high BH. sub. max permanent magnet 14A toward said bearing 120D with one reactive pulse, next the field collapses as the connection is broken sending a burst of counter-EMF into the system, however now the electrical contact is broken, trapping the counter-EMF energy between the said drive coil 12A and the DC batteries and capacitors, now pushing the magnet further away by the very virtue of the opposite energy pulse called counter-EMF. Once the said high BH. sub. max permanent magnet 14A has reached its farthest point of travel, the spring begins sending the said high BH. sub. max permanent magnet 14A on a return trip into the drive coil 12A, however now the said high BH. sub. max permanent magnet 14A must generate current as it cuts through the conductor. This unit will cycle until power is removed. Said high BH. sub. max permanent magnet 14A seems best connected to shaft 20A by a non conductive core element 18A, so not to add to hysteresis heating or eddy current transfers.

It is well known that extremely high voltages can be produced from a small voltage when run through a standard ignition coil or solenoid, however the contacts are quickly eroded if upper limits are passed and a steady current must be applied which produces inductive and conductive heating. By the use of conductors chosen from the group of high melting point materials, in this case tungsten and platinum are used, not only are the problems of the past virtually eliminated, new and heretofore unrealized energies are produced at little energy expense as heat rise is severely limited and at times reversed, as the intermittent pulsed current means will not allow power draw from the batteries for 99 percent of a full cycle, as only one pulse per cycle is possible. This extra energy has always been present, yet wasted by applied cooling means and heat losses, furthermore suppressed because a means had not previously been found to control it. Testing has shown electrolysis at 1-2 watts power draw as well as unmeasured strong mechanical energies being available, yet not drawn off the system.

Normal electrolysis generally cannot noticeably occur at 1-2 watts, therefor I believe its cause is charged particle cluster formation, whereby possible transmutation can occur.

Pulsed Plasma Spark gap--Description In reference to Fig. 7; a pulsed plasma spark gap 44 consisting of: a shaft 20 having affixed a shaft insulator tube 26 so affixed is an annular conductive ring 28, attached to said non conductive disk 24 is an annular conductive ring 28 and connected thereon at a peripheral face 36 is an annular conductive ring 28A so joined with said annular conductive ring 28 by a conductor wire 42 and said annular conductive ring 28A has so affixed a plurality of radial contacts 38. In sliding contact with said annular conductive ring 28 is a ring contact bar 46 so joined to a tension bar 50 having a conductor wire 42B affixed thereon. A tension spring 54 joins said ring contact bar 46 to post 116. not shown. which is suitably anchored.

Pulsed Plasma Spark gap--Operation In the pulsed plasma spark gap according to the present invention, a motor of variable speed, not shown, is attached to said pulsed plasma spark gap 44 and rotation begins after a selected voltage is suppiied to primary contact 66 and conductor wire 42B whereas radial contacts 38 will repeatedly make contact with primary contact 66. As a rotary spark gap is known to those skilled in the art, its basic function is also similar however, novel and unique features are evident. Contacts 38,66,28 and 46 are made of materials selected from the group of high melting point electrical conductors, in this case they are tungsten and platinum however iridium as well as others may be substituted. Uses include the driver for the receiving coil of my pulsed plasma power generating electromagnetic motor 9 whereby a pulsed discharge field will incrementally draw collecte charge from said receiving coil to pulse power other devices. A Tesla coil may also be driven by this device allowing greatly extended use with increased potentials and a faster plasma blow-out between cycles, allowing for higher frequencies and voltage potentials in the secondary.

An alternate use is toward a tabletop device of similar means as said power generating electromagnetic motor 9, minus the rotating magnetic field of the bipolar magnetic rotor 16. In this case the gap 44 is attached to a suitable coil, DC batteries and capacitance.

The resultant plasma flow between contacts 66 and 38 will produce suitable discrete particles and wave activity to prove its novel use in the field of sub-atomic particle discovery.

Conclusions, Ramifications, and Scope Accordingly, it can be seen that the power generating electromagnetic motor 2 using a pulsed plasma commutator 22 has novel and heretofore thought impossible operating means, however the prototypes consistently produce effects sought after in sub-atomic particle physics, whereby acting like a DC motor one may not realize its true potential as a tabletop charged particle cluster producer. I believe one by-product is radiation at a nuclear level whereby other sub-atomic particles are released as charged particle clusters causing for one, transmutation due to the particle seeking rebalance when striking another. Current theory suggests X-ray production occurs at a potential near 70KV, however gamma and x-ray testing underway should lead to a low cost, low power draw, low weight, portable, and useful X-ray unit as can be produced for unlimited applications as well as emergency and long range use. I believe a possible cause for heat loss in some applications is due to one or a combination of discrete wave/particle, anti-matter production/release, influence of charged particle clusters or possibly a harmonic sympathy with a space/time component. Still stranger, is the resultant heat loss from within the system, also heretofore thought an impossibility. I believe an anti-matter component is responsible for the heat toss, however other factors may be involved.

Although the description above contains many specificity's, these should not be construed as limiting the scope of the invention but as merely providing illustrations of some of the presently preferred embodiments of this invention. Various other embodiments and ramifications are possible within it's scope. For example, other arrangements of the components and contact means are possible as well as needed in configurations of more than one driving coil. In the case of a driver for a heretofore simple solenoid, reconstruction of components as referred to in Fig. 6, as zero spark suppression represents the means whereby novelty is proven.

The optimal spacing of radial contacts 38 and 38A has been found to be 5 degrees, however such adjustments to voltage and capacitance can in effect alter this perimeter, allowing for even doser spacing as long as an intermittent firing sequence is maintained. Therefore one can predict the use of fewer radial contacts and increase as well as stagger the positioning of the primary contact 66 as in Fig. 6. Here, a 20 degree spacing is compensated by multiple primary contact 66, each now spaced at 5 degrees. It is one goal of the inventor to transform system advances toward an eventual space warp drive propulsion means, through a folding of space/time.