AU727173B2

AU727173B2 - Extended application of hyperbolic sheath and coil

Info

Publication number: AU727173B2
Application number: AU60658/96A
Authority: AU
Inventors: George Anthony Contoleon
Original assignee: Individual
Current assignee: Individual
Priority date: 1996-03-11
Filing date: 1996-07-24
Publication date: 2000-12-07
Anticipated expiration: 2016-07-24
Also published as: AU6065896A

Description

1 This invention serves primarily to promote the release of energy in high temperature plasmas greater than 109 K (Kelvin) but also has other uses to be defined with this very clean form of energy not generating any radioactive wastes of any measureable significance. The invention among other things is related to the properties of directional high temperature plasmas which give very highly ordered resonances from directionally bombarded nuclides projecting higly extended nuclear field pulses which exist for very small fractions of a atto-second and are particularly evidently seen in 10 Atomic bomb blasts as directional protrusions from the blast itself.

This property directionalizes flow by nuclear impulse projections between the nuclides of atoms or molecules pulling by attractive force to directionalize flow. This abundance of nuclear field interactions means surrounding matter is drawn into the vicinity of 15 nuclear field releases which propagate directionally or near directionally from the very high temperature directional source by subelectron mass that is basically just dark matter that constitutes 95% of the galaxy. The sub-electron mass or dark matter is activated in the high temperature directional plasma source and nuclear vibrational order which give the high strength nuclear field pulses is duplicated by the sub-electron mass entering the Fermi gas of each nucleon in surroundings and building the resonance or vibrational patterns responsible for the nuclear field pulses such that this nuclear vibrational order transfered by converging sub-electron mass then eminates as energized particles from the high temperature directional plasma source which is releasing energy in terms of 2 depleated mass according to E mc 2 (E Energy,m mass lost, c velocity of light).

A The intensity and density of the sub-electron mass particle 2 field builds in surroundings with minimal or undetectable energy release. A large volume of nuclear field activity affecting surroundings atoms and molecules means that this volume attracts large amounts of sub-electron mass that is energized and attracted by depleated mass collisional interactions from nuclear field projections such that the affective temperature of this sub-electron mass particle field is less than 1 K and is undetectable to surroundings in terms of temperature. This large volume of energized sub-electron mass particle field has a very high viscosity and arrests motions that are atomic or molecular meaning flows and energy is transferred to the highly viscous sub-electron mass S: particle field which has a very high penetrability through solids e:e etc., and escapes after significant energy from surroundings has been absorbed. Energy in the sub-electron mass particle field absorbed from surroundings is released as sub-electron mass particle S field disapates or expands in larger volumes of surroundings and also as sub-electron mass particles bombard and enter nuclides of surroundings but basically harmlessly expands and disapates and Sis lost. Energy to mass conversions exist in the collapsable-expandable Fermi gas of the nucleons of nuclides so vibrational energy sites can collapse to sites of dense mass in the Fermi gas of the nucleon. This capability of harmlessly and unnoticably absorbing energy from surroundings means that this sub-electron mass particle field constitutes a large capability to harmlessly absorb and disapate energy i.e. fires and explosions. This accumulated and activated sub-electron mass particle field constitutes a anti-nuclear field in terms of limiting the strengths of explosions and fast motions of objects by the Second law of Thermodynamics such that -,_energy always passes to the less than 1°K sub-electron mass particle -3field with high viscosity, also containing pressuret such that bombardment rapidly transfers energy to field which builds resonance energy which activates the sub-electron mass particle field and precipitates a collapse of more sub-electron mass.

The invention itself is a sheath that is electrically conductive and accelerates ions magnetically over a ion layer as in Patent application 26,321/92 but the directional nature of the plasma requires that over 10 Mev. ion or nuclide energies are achieved with this directional plasma interaction compressing the like ion S..10 film to over 300,000 Pa. (pascal) or a charge density of greater than one nano-coulomb per cubic millimeter of ion film. This high charge density of the ion film ensures that ions only directionally interact without going into the film such that repetitive collisions of up to 10 5 ev. (electron volt) or greater occur to the same positive 15 nuclide on its path down the sheath. With this largenumber of ions compressed into the ion film large numbers of ions must be :II: injected into the sheath from the vacuum reservoir at about 10 6 S atmospheric density which means collection, ionization and injection of vacuum constituents being Hydrogen or Helium( He) is achieved 2 20 by a minQture plate assembly as defined in application 64,799/94 which operates at greater than 4,000 volts between plates with three or more active plate series and three or more of these minature plate assemblies being arrayed at the large front end of the sheath. This draws significantly large numbers of ions into the passage of the minature plate assembly due to the high voltage and ions are thus injected through plate assembly passage into the sheath and considerable compression of the ion film occurs.. The ion or nuclides that emerge from the sheath are r0e~r 10 Mev. and possess very high nuclear order or numerous dense -4phased vibrational zones of high energy which collapse and expand thus resonating to give high strength nuclear field projection pulses .which are configured to collisional orientations and thus bring about a convergence in sub-electron mass. As the highly ordered 10 Mev. ions or nuclides enter a plasma chamber containing plasma at greater than 109 OK order is transfered to the 10 9

OK

plasma at densities greater than 106 Pa.(pascal) by converging subelectron mass bombarding and entering the nuclides of the 10 9

°K

plasma. This means that this almost directional motion of plasma towards the front of cone in Hyperbolic magnetic field described in Patent application 44,494/93 multiplies the sheath's order affects by increased numbers of 109 K collisional interactions such that greater convergence of sub-electron mass particles occurs with o: energy release in the plasma by nuclear field projection interaction occurring for fractions of a atto-second thus increasing the energy of the plasma giving energy release from cone as thermal energy in terms of depleated mass of the colliding nuclides of the plasma.

9 0 The 10 K plasma inside the cone activated by the non-consevative magnetic field of the tapered coil wound on a hyperbolic sheath 20 generates the nuclear field impulses that spread to surroundings and convergence of the sub-electron mass particle field gives energy absorbtion with harmless disapation which characterizes a anti-nuclear field. Activation of the sub-electron mass particle field occurs building energy of the sub-electron mass particle field by collisional interaction and nuclear field pulse exchanges but this energy is entirely background and is rapidly transfered to the nuclides of the surroundings and stored safely for considerable time as well as disapating harmlessly to surroundings with the ^d energy released over a long period of time as very small nuclear shock energy pulses rippling through surroundings increasing the energy of surroundings very insignificantly or very unnoticeably.

Nuclear shock energy pulses at specific frequencies are responsible for the first order decay kinetics of radioactive substances which means that the rate of decay of any radioactive substance is proportional to amount of radioactive substance at a specific location.

The viscous sub-electron mass particle field also disapates harmlessly to surroundings by virtually diffusing into surroundings and its plasma like behaviour is lost as it encounters large volumes of surrounding material. This energy stiffling process exists around the plasma cone and equipment responsible for sub-electron mass particle field convergence and activation but energy as heat can be oooo released through cone to heat gases such as hydrogen which can be allowed to circulate through a turbine giving principally mechanical rotational energy and is directionally returned to surface of cone for re-heating and re-circulation through turbine but this high energy process is limited to the near vicinity of the cone where the nuclear order is high and viscosity and energy level of sub-electron mass particle field is lower than at some further 20 immediate distance by the fact that high orders linearize flow by nuclear field pulse attractions thus reducing the viscosity of the particle field near the cone allowing flow and expansion to a lower energy level and lower viscosity. Immediately next to this the sub-electron mass particle field has built in energy and viscosity due to rapidly declining nuclear order and diminishing directional properties of the particle field from the nuclear order source (the cone). Energy can be harnessed and utilized in this process close to the 109 OK plasma cone in this way. The plasma n one contains a Thorium oxide lining on the sides of the cone with 6 149 about to 15% by weight Samarium oxide which contains 62 Sm which has a very high natural cross-section and a metallic binder of up to 2% by weight (Silver and Ruthenium) such that this isotope of high natural cross-section means the dense zones in the Fermi 149 Gas of the nucleons of 62 m resonate and open nuclear field channels so that by sub-electron mass particle entry into fermi gas dense vibrational zones of permanent order are alligned in phase thus increasing the order of the plasma process and leaving a permanent 149 order in the 1 49 m or isotope of high natural cross-section which 62 adds to the nuclear vibrational order of the plasma increasing energy output of the 10 OK plasma and increasing sub-electron mass particle field affect to surroundings in terms of energy and viscosity and volume spread to surroundings. With this high order resonance behaviour and transfer by sub-electron mass occurs to Thorium and significant energy release in terms of depleated mass and collisional 9 o interaction by the 10 K plasma nuclides colliding with the surface nuclides of Thorium and releasing energy by nuclear field interaction.

(Summary of Invention) Equipment for energy release by depleating mass of nuclides or electrons fractionally compared to nuclear transitions 20 does not alter nuclide in anyway apart from small fractional mass change with energy released according to E mc 2 where E is energy released, m the fractional mass change and c the velocity of light.

Also a sub-electron mass particle field is released and this builds by direct precipitation to energy rich surroundings by nuclear field order transfered to surroundings and subsequent attraction collapse and sub-electron mass particle field absorbs energy (being cold or less than 1 K and energy always passes from hotter body to colder body by Second law of Thermodynamics) and then harmlessly capes through surroundings. Similarly the opposite nuclear order 7 (low nuclear order) sub-electron mass particle field absorbs energy from surroundingsand builds in number by chain reaction release of sub-electron mass and sub-electron mass gains relativistic mass as energy is absorbed and harmlessly escapes through surroundings and this property of absorbing energy from surroundings classes the sub-electron mass field as a Anti-nuclear field capable of absorbing energy from blasts or Atomic bomb blasts and then harmlessly disapating through surroundings. Basically this equipment is a glass accelerator sheath with a conductive external film that generates a magnetic field that accelerates positive nuclides down sheath of over 10 Mev. with high nuclear order or low nuclear order in reverse polarity when electrons are accelerated down sheath. The particles from 0 9o accelerator pass into a plasma chamber where a plasma of 109 OK or 0 over is generated and thermal energy or direct electrical energy is obtained from plasma cone. A Thorium lining on inside of plasma '000. cone is bombarded by plasma of plasma cone giving depleated mass 9 00.00 energy release in Order energy release mode or Disorder energy release mode. This mass of Thorium nuclides is changed very fractionally and energy is released. High speed inert gas flowing over 20 Tungsten Plasma cone's surface absorbs energy which is hot,high pressure inert gas which is vented through a expansion-contraction Turbine which can spin in either direction depending which end hot compressed inert gas is vented at. This gives two directional thrust from turbine particularly as a pressure jet and blade thrust in the contraction section of the turbine (depending on which side hot inert gas is vented at) enhanced by a crease in blades which forms a pressure zone under blades. As plasma circulates or rotates in plasma cone thrust is derived as forward thrust from electrons ,~waQwards large front end of cone) in low nuclear order mode Q4act5 Q/- -8- _t polarity down conductive accelerator sheath giving reverse thrust in cone from positive nuclides down sheath (straight polarity down sheath) with high nuclear order energy release. A plate assembly for principally electrostatic thrust and ion introduction into turbine gives low energy, high magnitude thrust.in turbine and one is at each end of Turbine with the one active at the end where the hot inert gas is vented at. The magnetic field of Turbines contraction and expansion sections are active with the expansion section magnetic field contributing to enhanced thermal to mechanical energy transitions by 10 free electrons in hot inert gas of Turbine. The magnetic field of S plasma cone separates charges and gives direct electrical output.

Magnetic thrust exists in Turbine and plasma cone by direct force gig *go* reaction to moving ions from stationary coil of plasma cone or Turbine. Direct rotational energy of turbine gives thrust which means this equipment is a space engine that can be placed on a •ol Orbiting Space Craft to change orbit or tow Lander craft into space ooo• or to another planet in the Solar system. As plate assemblies of *oo: Turbine are very close to plasma cone and plasma' is high temperature further mass depleation can occur at pressure zone at end of plate *oo* assembly and subsequent energy release in high nuclear order mode or low nuclear order mode (Disorder) depending on polarity giving additional energy release in Expansion-Contraction Turbine. Also rotational energy can be obtained from Turbine making it a engine for direct transmission of Torque. (End of Summary of Invention) The turbine through which.the hot hydrogen heated from the surface of the 109 OK plasma cone circulates is a hyperbolic expanding section followed by a hyperbolic contracting sequence and is the same size as the turbine in application 64,799/94 expanding from Sto 250mm. and contracting from 250mm. to 65mm. with a plate 9 assembly of high voltage plates as in application 64,799/94 at each end of the turbine with the blade shape such that gas can enter the turbine from one end flowing through and around plate assembly (which is connected to external electrical supply) expandingto rotate shaft by flow over blades and enter contraction section as hydrogen by this stage which has expended significant energy and the cooled hydrogen is compressed by rotating shaft with some energy transfer to blades of rear contraction section.

The magnetic coils of greater than 2 tesla magnetic field strength 10 being tapered perpendicularly wound coils in plane perpendicular to direction of flow are tapered in direction of convergence of hyperbolic sheath of turbine. The Turbine configuration of a plate ee assembly at each end, expanding and then contracting means with the blades at the same angle in each turbine section gas can be allowed to enter from either end. From one end the plate assembly is electrically active at that end and turbine shaft rotates in one direction (clockwise or anti-clockwise) depending on magnetic field eeo• direction which assists thermal energy transfer to mechanical energy S. S by ion atmosphere drag accross blade surface. The hydrogen exits 20 at the other end cooled and re-compressed for re-circulation. Once the cone is releasing thermal energy hydrogen is released into system and the turbine is spun at greater than 10,000R.P.M. to initiate compression and circulation. If hydrogen gas enters from other end the turbine must be initiated to rotate in opposite direction with magnetic field direction reversed and plate assembly at that end is electrically active. The reason for this is thrust derived at the end of the passages of the electrically active plate assembly plus pressure thrust around plate assembly as in application ,_,64,799/94. Further to this blades being of plates pressed have a 10 crease pressed into the end of the flat surface so that this constitutes a fold or bend in angle with most of the blade surface angled to deflect gases down turbine or absorb flow and convert to rotational energy. In the expansion section the small area crease is at the front of the blade and helps to deflect gas along blade surface but in the contraction section the small area crease that runs almost radially on plate of blades acts to build a pressure zone around surface of blade as it turns through congested, churned flows of the contraction hyperbolic turbine section giving increased thrust from blades in contraction hyperbolic turbine section. When see rotation of shaft is reversed and gas enters from opposite end S. the active plate assembly at the other end plus pressure thrust around that plate assembly is in the opposite direction along with 0 so: the configuration of creases in opposite flow and rotation directions 15 giving enhanced blade thrust in the opposite direction. Finally two electrodes inserted at different depths and thermally shielded 6000 from hydrogen flowing over cones surface give a voltage output 0o00 0 because electrons in the 10 9 OK plasma cause charge separation with

C

:0 some current flow. After hot hydrogen has emerged cooled and recompressed from the contraction section of turbine some hydrogen is diverted to the coil around cone activating 109 OK plasma cone and coils over expansion/contraction hyperbolicturbine for cooling and then released back into main flow that is re-directed into flow from hot cone's surface to expansion hyperbolic turbine section. The following five main drawings are of the equipment required to generate rotational and thrust energy and a anti-nuclear field.

Figure 1 is a schematic drawing of the equipment needed to generate a anti-nuclear field which spreads to surroundings along with deDleated mass energy in the 109 OK plasma by nuclear interactions 11 of the nuclides of the plasma where depleated mass gives energy 2 according to E me 2 The sheath 1 has current flowing to narrow base for acceleration of positive ions 3 which build the ion film that ions skim over. The ions are injected by three or more minature plate assemblies 2 at front or at large end of sheath. The positive ions of greater than 10Mev. possess very high nuclear resonance order and propagate a nuclear field 4 to surroundings which spreads and is amplified by nuclear field interactions in 10 9 oK plasma nuclides 9 in cone 8. This causes a convergence of a sub-electron mass particle field 5 which is activated or energized to significant viscosity and density by the nuclear field interactions in 0 .0 surroundings and acts to impede molecular,atomic and fast motions of objects and is essentially a anti-nuclear field with a large capacity to absorb and harmlessly disapate energy from fires or 15 explosions. The tapered coil 6 which is laterally wound or wound in the plane perpendicular to the direction of taper of the hyper- S bolic sheath 7 it is wound over has a magnetic field strength of over 2 tesla to activate the 109 oK plasma. As the 109 0 K plasma interact by nuclear fields inside the cone at pressures up to 10 Pa.

20 bombardment occurs with the Thorium oxide lining 17 releasing further energy by nuclear field interactions transfered by the sub-electron mass particle field which transfers the nuclear vibrational order to Thorium nuclides and permanently imprints 149 nuclear orders in Samarium nuclides 62 Sm) of Samarium oxide 62 in the Thorium lining of cone. On bombardment by plasma these perm- 149 anent orders in Samarium nuclides 62 Sm) give high order nuclear field interactions which causes convergence of sub-electron mass which in turn transfers nuclear orders to 10 9 oK plasma, Thorium i clides and surroundings and increases energy release from 10 oK 12 plasma in cone and Thorium in cone's lining as well as helping spread nuclear order to surroundings for convergence of sub-electron mass particle field which is a anti-nuclear field. A copper strip forms a collar 10 for electrical contact on the externally silvered glass hyperbolic sheath at the large curved end of the hyperbolic sheath. At the other narrow parallel end of hyperbolic glass sheath electrical contact is made with the external silver layer by a split copper tube 11 which conveys the nuclides of 10 Mev. or greater energies possessing high nuclear order into the plasma cone.

Hydrogen introduced into closed hyperbolic corridor 12 containing plasma cone enters near base of cone, expands and heats on surface of energy producing plasma cone. Hot hydrogen flowing over cones surface emerges into volume of slightly diminished pressure 13.

Hot hydrogen from cone and volume of slightly diminished pressure 13 and ready to be vented through turbine is conveyed through 0000 channel 16. Returned cooler hydrogen 14 is passed through coil 0000 housing to cool windings of coil and after emerging from coil 000000 housing 15 is then directed into hot volume of hydrogen of diminished pressure 13.

Figure 2 is a schematic of the turbine with the two basic circulation routes for hot hydrogen from the surface of the cone to generate rotational energy and reverse thrust. Items 6a and 6b are the coil and coils housings for the left and right hand turbine sections respectively. Each coil operates by essentially electrons which have a atmosphere and drag gaseous molecules over blades and to blade surface thus energizing gas and making thermal energy transfer to mechanical blade energy more efficient. For field direction left to right which is current flow in a clockwise _.-Irection seen from the left which means blades must spin in a 13 clockwise direction seen from the left for flow through the turbine from left to right with the left hand plate assembly 24 electrically active for ion generation and pressure jet thrust through the hyperbolically tapering passages when flow is from left to right through turbine. For field direction right to left which is current flow in a anti-clockwise direction seen from the left for flow through the turbine from right to left with the right hand plate assembly 24a electrically active for ion generation and pressure jet thrust through the hyperbolically tapering passages when flow is from I10 right to left through turbine with blades turning anti-clockwise seen oo from left over the same angled blade surfaces. Item 14a depicts returned and cooled hydrogen from venting through turbine to cooling windings in coil housing on left hand hyperbolic turbine with 15a depicting emerging hydrogen from coil housing circulated back 15. to the back of thecone 12 for heating, expansion and pressure drop before venting again through turbine. Item 14b depicts returned and :oo cooled hydrogen from venting through turbine to cooling windings oo in coil housing on right hand hyperbolic turbine section with Sg depicting emerging hydrogen from coil circulated back to back of 20 cone 12 for heating, expansion and pressure drop before venting again through turbine. Hot hydrogen from the cone's surface and expanded lower pressure region is entered into turbine 16. The valve 18 for directing hot hydrogen for right to left flow through turbine with 19 the valve for allowing hot hydrogen for left to right flow throughturbine. Item 20 is the valve for allowing spent hydrogen from right to left flow through turbine to return to base of cone 12 for re-heating. Flow 21 is return flow of spent hydrogen from right to left flow through turbine to return to base of cone 12 for ee-5 ,-heating. The diverted flow 22 through valve 18 of hot hydrogen 14 is for venting hydrogen through turbine in right to left flow.

Spent hydrogen from left to right flow through turbine is returned along flow channel 23 to base of cone 12 for re-heating. Valve allows the flow of spent hydrogen to return to base of cone 12 through channel 23 for re-heating. Item 26 represents the blades of the turbine. Item 27 represents left to right flow through turbine when valves 19 and 25 are open and valves 18 and 20 are shut. Item 28 represents right to left flow through turbine when valves 18 and are open and valves 19 and 25 are shut.

0.10 Figure 3 shows the sheath's housing and vacuum support system Si: with Figure 3a a detailed drawing of the 3 plate series minature plate assembly with 3mm. between plates and 3mm. thick ceramic inserts. Figure 3b is a detailed drawing of the sliding rod valve with allignment groove and ring seals.

15 In Figure 3 item 1 shows current flow down sheath for positive **s G ion acceleration with 2 the minature plate assembly with three G sequences and greater than 4,00V (volts) on plates. Accelerated sees*: positive ion 3 is shown moving down sheath. Copper strip 10 that *0

*S

forms a collar around large end of externally silvered glass hyper- '20 bolic sheath and makes electrical contact with external conductive layer on hyperbolic sheath. A split copper tube 11 makes electrical contact around base of externally Silver coated hyperbolic sheath.

Item 29 is a ceramic rod or slug of glazed alumina grit with Sodium Silicate with two electrically isolated high voltage electrodes at greater than 4,000V through a plastic ferrell that makes electrical contact with the minature plate assembly 2 and the vacuum is kept by the plastic ferrell backed by a rubber ring in compression fitting in plate 33. Support rod 30 for minature plate assembly -Rkelectrically isolated from high voltage supply through compression 15 fitting in plate 33 and vacuum sealed by plastic ferrell and "o" ring for backing. Electrically active rod carrying 600 amps and 6 volts 31 and vacuum sealed by plastic ferrell and ring backing through compression fitting in plate 33 is split inside vacuum chamber to distribute current to coated sheath through copper collar thus supporting sheath inside vacuum chamber. Electrical contacts 32 from glazed alumina slug or rod 29 containing electrically isolated tungsten electrodes which supply 4,000V. or greater to minature plate assembly. Plate 33 is on end of end cap of vacuum o. 10 chamber for hyperbolic sheath containing compression fittings for *O 0 glazed alumina rod for high voltage connections 29 to minature plate assembly with compression fittings for electrically isolated support rod 30 to minature plate assembly with electrically isolated s high current rod to large end of sheath 31 through compression 15 fitting and split so as to support sheath in vacuum chamber and making electrical contact with copper collar on large end of sheath.

rings 37 seal the vacuum chamber segments such as end cap ends and end caps to central segment to end caps bolted by bolts through flanges 34 welded to thick hollow bar section 36 such that over-lap of hollow bar occurs with the flange so radiation shine from high energy X-rays around and through bolted joins and rings of low shielding capability is not a problem. Item 38 is a evacuation line of greater than 16mm. bore brazed into plate 33 for sealing end cap of vacuum equipment for hyperbolic sheath. The split copper tube 11 which makes electrical contact with the narrow end of the externally coated electrically conductive sheath and is electrically isolated from compression fitting 41 through a plastic bush and ferrell backed by a ring to seal vacuum system of sheath. A -sliding rod valve 39 with a hole allows passage of 10 Mev. nuclides 16 directly through straight copper tube passage through to 10 9

OK

pla.sma cone In Figure 3a item 30 is a split bracket for mounting and isolating bracket from the 5mm. threaded shaft by a bush through hole in bracket and behind bracket-48. Cerami-c washer 49 holds bracket isolated and the connection 32 is made to threaded shaft 50 and held by nut 42. The parallel connection to plates 46 is made by the threaded rod 50 but on one side ceramic bushes 44 isolate threaded rod electrically from alternate plates and on other side of plate assembly ceramic bushes 44a isolate positive plates from electrical connection to shaft 50. Ceramic inserts 43 cover the whole negative to positive surfaces so motion of positive ions through plate assembly 53 is not repelled. Ceramic spacers 45 that do not cover whole positive to negative surface space and between plates 46 that are :15 about .7mm. thick and about 25mm. in diameter with bushes 44,44a isolating the shaft from plates electrically. On negative terminal or shaft a nut 51 fastens plate assembly together tightly and on positive terminal or shaft a ceramic isolating bush 52 prevents electrical contact with end negative plate with a nut 47 holding plate assembly together tightly on that side.

In Figure 3b the rod valve for vacuum isolation of the vacuum chamber housing the hyperbolic sheath with handle 54 for pushing down to open and pulling up to close. The casing 55 of the valve is brass or stainless steel finished with 600 grit sand paper and is a very smooth surface for ultra vacuums. The first ring 56 is a larger diameter than second ring 57 and these two rings seal and hold the vacuum. More than one ring can be placed at each position 56 and 57 on the valve stem 60. When valve stem is R ,hed down fully hole 58 alligns with passage allowing 10 Mev.

17 nuclides to traverse valve stem into conical plasma chamber. The allignment groove 59 that prevents turning of the stem can be two off-centre thin rods attached to base of stem that slide into accurately positioned off centre holes and prevent turning of valve stem.

In Figure 4 the coil housing 6 is over hyperbolic sheath 7 and enclosure on which coil housing is situated. A preferably Tungsten plasma cone 8 contains 10 9 OK plasma 9. The tube 11 conveys 10 Mev.

nuclides from hyperbolic sheath in a straight line so interaction 10 with side of tube is minimized. The passage of hydrogen over cones surface absorbs heat at less than or up to 1200 0 C such that hydrogen emerges into hot lower pressure region. Input of cooling hydrogen into coil housing 14 through thin Stainless Steel tubing system with small holes along length. Output of cooling hydrogen from coil 15 housing 15 is vented into high temperature lower pressure region 13.

Hot hydrogen from cone and lower pressure region 16 is shown ready to be vented through turbine. The Thorium oxide with Samarium oxide S lining 17 in cone is shown. The external cover 61 of the coil hous- *o°*o ing 62 with alumina fibre insulation 63 which also electrically insulates windings from base of coil housing is shown. A cooling gas tubing system 64 of thin stainless tubing is at base of coil housing with tiny holes along length for venting cooling hydrogen into coil housing. Copper strip windings 65 isolated by greater than grit and Sodium Silicate binder. The top plate of cone 66 made of preferably Tungsten. Soft copper or preferably Nickel foil gasket 67 is at top of cone for vacuum seal of cone. The cone wall 68 made of sintered powdered Tungsten and is infiltrated with Ruthenium Nitrosylnitrate, heated then electroplated with Ruthenium to seal sintered Tungsten. Tensioning Rods 69 made of heat resistant low 18 creep alloy i.e. Inconel 600 holds top plate 66 and base plate 72 of Ruthenium electroplated Tungsten by welded flanges 70 to tensioning rod on both sides of Tungsten Top Plate brazed to Tungsten top plate by high temperature braze (greater than 1,300 0 C liquidus region) comprising about 25% Silver by weight or less, in Palladium. A soft copper gasket 71 seals base plate to cone on cooler end of cone. The brazed bush 73 is on end of base plate 72 of cone through which tensioning rod 69 slides. A soft copper ferrell 74 for sealing high vacuum in cone between surface bush 73 for tensioning rod 69 and tensioning rod cover 87 as well as contracting and sealing tensioning rod surface but still allowing tensioning rod to slide through ferrell. The compression fitting 75 on base plate 72 (not clearly shown) is for sealing and holding straight copper tube 11 for conveying 10 Mev. nuclides into plasma cone. One Tungsten electrode 76 for conducting some electricity generated by charge separation in magnetic field at a specified depth in cone with electrode through glazed alumina slug or rod in compression fitting in base o: plate of cone and base of hyperbolic'housing for cone. The other Tungsten electrode 77 for conducting some electricity generated by charge separation in magnetic field at a greater depth in cone than other electrode being positioned by glazed alumina slug or rod in compression fitting in base plate of cone and also in base of hyperbolic housing. Vacuum evacuation tube 78 for cone through compression fitting seals in base plate and end of Hyperbolic housing. Thermocouple wires 79 sealed in glazed alumina slug or rod in compression fitting of base plate and in Alumina slug or rod through compression fitting of end of hyperbolic housing with thermocouple attached to side of cone. The 12mm. thick lead case supported by R, i, plate 80 is present for the unlikely event of cone rupture 19 (cone being of 5mm. thick tungsten, enough to prevent any abnormal level of 10 5 ev. X-rays escaping from 10 9 OK plasma cone). The 1.6mm.

thick tungsten plates 81 stacked behind each other in expanding exit 82 in event of cone rupture and X-rays escaping and radiation shine. Spring 83 for pressing tensioning rods sheaths 87 to base plate of base of cone for vacuum seal by copper ferrell 74. Nuts 84 for pre-loading springs such that a pressure relief system exists on cone so pressures are not high enough to rupture cone. Flanges for sealing top of hyperbolic housing for cone where hydrogen is 10 heated to up to 1200 °C with bolts 86 for attaching top of hyperbolic housing through flanges 85. Tensioning rod covers or sheaths 87 support cone through compression fittings in heating chamber that contains cone through which tensioning rod slides. The compression fittings and ferrells on the vacuum system of the cone is at high temp- 15 eratures as well as copper and Nickel gaskets 67 and 71 all require 99 9 that a good seal forms to hold high vacuum and this is enhanced by spraying the Silver Nitrate solution and heating back to metallic Silver to help make good seal on gaskets and ferrells and spraying ferrells in the compression fittings and spraying Silver Nitrate solution around the gaskets between the contact surfaces in the actual cone. The actual 109 oK plasma exhibits pressure thrust to surfaces in the cone. Reverse thrust on rear sides of cone. mean current flow in coil is in anti-clockwise direction seen from the left with field direction being right to left seen from left and current flow in clockwise direction seen from left gives a left to right field such that the expanding plasma to sides and to large front surface demonstrates circulation due to fast electrons with energy from positive nuclides or protons giving mainly reverse rust on rear sides of cone as electrons expand to front of cone, 20 circulation is clockwise seen from left when field is left to right and anti-clockwise plasma circulation seen from left when field is right to left.

Up till now the invention has been to facilitate nuclear order resonance pulses but other fundamental mechanisms exist and energy can be generated and sub-electron mass fields in surroundings that are anti-nuclear fields can be generated. Basically shock energy from fast electron collisions focused down hyperbolic sheath when current flows are reversed with polarities on minature plate assemblies expanding periphery of electron's Fermi gas which lowers the surface energy and maximizes disorder and states in the Fermi gas *i 9 9 on entry into cone bombarding electrons at 10 9 K travelling at the speed of light release energy and a sequence of particles at around I0- 21 proton mass U= atomic mass unit,1.6x10 2 7 Kilograms) 66 15 at O10 Pa. plasma pressure with electrons released into cone a a through electrodes 76 and 77 with one electrode being a cathode such that the cathode is behind a anode grid and electrons pass through I' grid towards front of cone. A pilot voltage of greater than 4,000V and electron supply of 600 Volts and 5 Amps is superimposed on pilot voltage. In the plasma cone the energy release depends on the initiating electrons from sheath expanded by shockenergy with shock energy diminishing from initiation site in cone as the sub-electron mass generated collapses in less than pico-seconds (due to high surface forces) from the initiation site and the chain reaction of sub-electron mass releases in 109 0 K bombarded collisional electron plasma and surface layers of Thorium oxide lining 17 of cone diminishing to no energy release within the small limited volume of cone -b the rapid collapsing bombarding sub-electron mass field. Sub-electrcrn mass builds in surroundings by release from cone and very small 21 amounts of energy released by chain reaction bombardment of eminating sub-electron mass particle field such that particle field absorbs energy by the Second Law of Thermodynamics as energy is transfered to the less than 10 6 oK particle field which quickly gains mass as the energy gained in the particle field becomes relativistic mass as the sub-electron mass particles are travelling close to the speed of light. The cone system now has forward thrust for current flow clockwise or anti-clockwise seen from left. Clockwise current seen from left gives left to right field with clockwise circulation 0 of plasma seen from left with anti-clockwise current seen from left gives right to left field with anti-clockwise circulation of 4 plasma seen from left. Hydrogen or Helium 2 He) is still in plasma cone but radioactive vapours or gases can be bled into high vacuum of cone through evacuation line 78 for destruction by bombardment by 109 OK protons or Helium plasma or electron 109 OK bombardments when reverse polarity is applied to cone's electrodes,76 and 77 are input terminals for electrons. Also the connection of copper tube to ooeoo: sheath 11 from very high vacuum to lower range in cone is maintained by force of ions from sheath and cooling of plasma in cone as plasma hits around tube opening and pressure at opening of tube in cone drops.

Figure 5 is a disproportionate drawing of turbine and bearing mounts and gear box with the turbine looking shorter in relation to bearing mounts. Figure 5a is a detailed drawing of bearing mount with gear reduction assembly. Figure 5b details the plate assembly in end of turbine and details mounting of turbine. In Figure 5, 6a is the left hand tapered laterally wound coil and 6b is the right hand tapered laterally wound coil. Item 14a is returned hydrogen entering left hand coil housing and 14b is returned hydrogen enter- 22 ing right hand coil housing. Emerging hydrogen 15a from left hand coil housing and 15b from right hand coil housing is shown. Hot hydrogen from cone 16 entering turbine with left to right flow.

Return flow hydrogen 21 from turbine in right to left flow goes back to cone for re-heating. Hot hydrogen from cone 22 enters turbine for right to left flow. Spent hydrogen from right to left flow through turbine returns to cone for re-heating. The left hand plate assembly 24 is active for left to right flow through turbine. The right hand plate assembly 24a is active for right to left flow through turbine. The blades of the turbine are indicated by 26 with crease such that for a left to right field with clockwise current flow seen from left blades spin clockwise seen from left for left to right flow and visa versa for a right to left field with a anti-clockwise current flow seen from left blades spin anti-clockwise seen from left for 15 a right toleft flow whichmeans looking from left top part of plate of blades (attached to shaft) angles to left with crease at upper top side so on looking at bottom blade the bottom blade angles to go right with crease on upper top side in the expansion section but in the contraction section of turbine with blade at top angling to left with crease on bottom under-side and on bottom blade, blade angles to right with crease on bottom underside with crease only a small area of blade which drags and builds pressure zone around crease of blade in each respective contraction section. With this blade pattern right to left flow with anti-clockwise rotation seen from left builds a pressure zone at end of blade in the now left hand contraction section. Item 61a the external cover of coil housing of left side coil seals by being pressed onachined surface of left side coil housing 62a with alumina fibre insulation 63a at bottom of coil housing with a system of tubing 64a for cooling gas hydrogen going through grit 23 spaced copper strip windings 65a of left hand coil. Item 61b the external cover of coil housing of right side coil seals by being pressed on machined surface of right side coil housing 62b with alumina fibre insulation 63b at bottom of coil housing with a system of tubing 64b for cooling gas hydrogen going through grit spaced copper strip winding 65b of right hand coil. Item 88 depicts the gear reduction housing with 89b the bearing housing on right side.

Item 89a is the bearing housing on left side. Bolts 91 through flange 90a on left side coil housing cover and flange 90b on right 10 side coil housing cover pulls to seal covers on machined surfaces S on coil housings. Bolts 93 hold flange 92a on left side sheath of turbine to flange 92b on right side sheath of turbine. Compression fitting 94a holds alumina bush 95a which insulates left plate assembly electrically from tubular shaft. Compression fitting 94b .15 holds sintered alumina bush 95b which insulates right plate assem- S bly electrically from tubular shaft. Compression fittings 96a and 96b have a Silica liner through ferrell for electrically insulated connection to left side plate assembly. Compression fittings 96c and 96d have Silica liner through ferrell for electrically insulated connection to right side plate assembly. Vacuum line bleed off 97a for any hydrogen escaping left side from turbine through two sets of seals.Vacuum line bleed off 97b for any hydrogen escaping right side from turbine through two sets of seals. The rigid right handed section 98 has a thick fork plate 99a on left side with accurate 900 surface with another thick fork plate 99b on right side with accurate 900 surface to which turbine is mounted. Accurate positioning surface 100a in plate for turbine on left side.Accurate positioning surface 100b in plate for turbine on right side.The 19mm.

fRA\ick plate 101a for mounting and alligning bearing housing cover 24 102a which alligns positioning plate 105a which has accurate positioning surface 100a all on left side. The 19mm. thick plate 101b for mounting and alligning bearing housing cover 102b which alligns positioning plate 105b which has accurate positioning surface 100b all on right side. Threaded collars 103 on either side of plate of blades on threaded sections of shaft of turbine fix plate of blades to turbine shaft. Weld tacs can also secure threaded collars to plate of blades and shaft without any noticeable dynamic balance loss within a radius of 15mm.. Split copper bushes 104 brazed togeth- ::10 er with support rings with grooves fot flow of water are brazed into hollow copper bushes for pressure support and water cooling of bearings after being accurately machined. Split bush 106 is joined o together by threaded collar and weld tacked,limits escape of hydrogen from.turbine.The cooling water flow through tubular shaft of turbine is shown by arrow 107. Threaded bush 108 on end of shaft at end of bearing housing is welded internally to shaft for pre-loading bearings with allignment surfaces 109 for accurate allignment of internal spinning surface with close tolerances 113 close to stationary **o plate with bush to which water line through tubular shaft of turbine goes out at 116 at end of shaft through stationary bush 110. Water goes into hollow copper cooling bushes for bearings shown by 111 and flows to next hollow copper cooling bush by adjacent alligned holes.

Water from hollow copper cooling bushes comes out at 112a at the right bearing housing. Water from hollow copper cooling bushes comes out at 112b at the left bearing housing. Oil goes into bearing housings at 114 and comes out at 115a from other end of left hand bearing housing after going through eight angular thrust left hand bear- Smount bearings and also comes out at 115b from other end of right han earing housing after going through eight angular thrust right 25 hand bearing mount bearings and gear reduction housing. Water 107 emerges through stationary bush and plate 110 shown by flow 116.

In Figure 5a hot hydrogen from cone 22 to enter turbine for right to left flow is seen. Return spent hydrogen from turbine in left to right flow leaves turbine via 23 to return to cone for re-heating. Gear reduction housing 88 reduces rotation rate by at least a factor of five times and is over right side bearing housing. Hydrogen through a series of seals through two series of split plastic ferrells in compression fittings emerges from a vacuum bleed line 97b. Accurate alligning surface 100b in positioning plate 105b for right side of turbine. The 19mm. thick plate 101b for mounting and alligning right bearing housing cover 102b which alligns positioning plate 105b. Split copper bushes 104 brazed together with 0 support rings with grooves for flow of water are brazed into hollow copper bushes for pressure support and water cooling of bearings after being accurately machined. Split bush 106 is joined together by threaded collar and weld tacked, limits escape from turbine.

Items 107 to 116 are the same as Figure 5 but drawn more clearly.

Internal weld to shaft 117 of threaded bush 108 for pre-loading bearings, the join in shaft 118 that emerges from turbine allows easier assembly and utilizes allignment surfaces. Shaft 119 for bearings for intermediate gears in gear reduction housing is bolted by threaded end to outside large bearing sleeve 121 and mount for bearings for intermediate gears bolted to bearing cover. Bearings for intermediate gears in gear reduction housing are ~oposed angular.thrust bearings 120. Plastic oil seal 122 has close tolerances and seals oil in gear reduction housing at both ends.

Spacing bushes 123 between bearing pairs connect load forces to each y0'0Riges of bearing pairs. Two large opposed angular thrust bearings 26 on external sleeve to bearing cover allow the gear reduction housing to rotate. In Figure 5b hot hydrogen 16 enters turbine through tube in welded fitting 138 for left to right flow. Return cooled hydrogen 21 leaves turbine through tube in welded fitting 139 fo r right to left flow through turbine. Top of plate of blades 26a looking from left, angles to left with crease on top upperside with bottom of plate of blades 26b angling to right with crease on top upperside looking from left. Bearing housing 89a on left side is seen. The alumina bush 95a that separates shaft from plate assembly in compression fitting 94a compensated against thermal expansion by having a double, angled metal pair of bushes with one bush slitted 132. Compression fittings 96a and 96b with Silica linings insulate plate assembly connections from turbine sheath. Accurate positioning surface 100a in positioning plate on right side of 105a is shown. The 19mm. plate on left side 101a.holds left bearing housing holder 102a accurately in position and to left fork plate 99a of R.H.S. base 98. Bolts 124 hold turbine sheath to mounting and positioning plates. Ceramic insert 125 between plates of plate assembly with alternate spacers 126 around two 10mm. tungsten bolts *see.* (for thermal expansion compatability) as connection rod to alternate plates as in minature plate assembly (Figure 3a) with a further two.

rods also supporting plate assembly to 1.6mm. plate 134 welded, 135 2 to hyperbolic turbine sheath 127 with over 700mm of less than .4mm. holes 140 for input of hot hydrogen to flow around plate assembly and give distinct pressure propulsion advantage over momentum transfer thrust shown by flow 133. Split bush 106 helps limit escape of hydrogen from turbine. Spot welds or weld tacs 136 to plate of blades and threaded collars and threaded sections.of shaft 11 radii so as not to affect dynamic balancing. The nut 128 27 holds plate assembly together on tungsten bolts with ceramic spacer 129 and at other end alumina bushes 130 hold connection to tungsten rod by nut 131. One of the twelve hyperbolic tapering passages is shown by 137 with Barium Titanate 141 (or material of high Dielectric constant) mixed with Alumina in the ceramic insert 125 near the passage of the plate assembly for increasing the charge density on the plate surfaces in the exposed plate surfaces in the passages of the plate assembly.

Basically this equipment for depleated mass energy release from protons, nuclides or electrons is a sheath about 400mm. long with S the external Silver coating conducting 600 amps at 6 volts which

S.

gives a field strength in excess of .2 tesla accelerating protons, nuclides or electrons on reverse polarity past 10 Mev. with each minature plate assembly at 4,000 volts and having a input of :15 greater than 40 watts which injects sufficient ions into sheath to attain like ion densities of greater than 10 9 coulombs per mm 3 and/or greater than 300,00OPa. pressure on side of sheath. The particles or nuclides enter the 5mm. thick tungsten cone which is 200mm. long and 60mm. in diameter at small base and 150mm. in diameter at large end in terms of external diamensions and is activated by a 2 tesla field with copper strip windings spaced by greater than .5mm. grit with a 12 volt, 600 amps power supply with 1/8 of a inch stainless steel tubing for cooling hydrogen release into the coil housing, which sheath coil is wound on, being a series going from 200mm. to 161mm. to 127mm. to 98mm. internal diamensions with each cone segment being 100mm. long. The tungsten cone has a capacity to generate and release over 10 6 watts of thermal power but hydrogen or other inert heat transfer gas must rapidly extract -,_hermal power from cone surface otherwise cone will rupture.

28 Over 10 6 w. (watts) of power is attained from cone in the form of energy of motion at very high energy conversion ratios from the plasma at greater than 109 OK and 106Pa. which exerts a one sided force in terms of thrust. Towards sides of cone for protons and positive nuclides from resonance order energy and with reverse polarity thrust from electron energy is mainly towards front of cone, but system must be moving for energy to be efficiently converted to energy of motion. Swirling of plasma helps direct thrust forward or backwards by mainly electron expansion to side ":10 of cone. Maintaining the vacuum at 10 6 atmospheric density is sufficient as some hydrogen diffuses through cone wall so vacuum 0 0 foe* system must intermittently or constantly operate and with depleated o 0o: mass energy from the shock energy initiated electron collisions 00.0 being supplied by electrodes 76 and 77 with one a cathode sending oo00 electrons through a anode grid such that a pilot voltage of 4,000 volts at 40w. operates with a superimposed voltage of 600 volts 0 S and 5 amps. In.. the case of depleated mass electrons the opposite 00 to nuclear order exists and order turns to disorder with expanded mass and maximization of number of Fermi states and this can be promoted by having highly expanded nuclides in cone lining that 187 have a natural high affinity to block gamma rays such as 76 Os which is mixed with the Thorium oxide and Samarium oxide and binders of Ruthenium Nitrosylnitrate and Silver Nitrate in the form of Osmium Nitrate. This is very expensive so less than one 187^ milli-gram per cone lining of 176s is used. Maximized disorder 76187 and disorder imprints of expanded mass can be left with the 76s 18776 with a very disordered array of zones which give the 18 76Os its 76 -28 2 natural cross-section of around 300 Barns (10-28 m One system _a'tes independently of the other destoying permanent orders left 29 i.e. if proton resonance order is used order increases in 187Os 76 and fermi gas collapses slightly and if electron particle energy release is used with reverse polarity on sheath and minature plate assemblies with cathode and anode grid for electrodes 76 and 77 187 149m are then fermi gas expands in 76Os and permanent orders in 62 Sm are lost. So in the long term it is preferable to have a separate system for each type of energy release (resonance or chain reaction particle release) i.e. a separate cone. The turbine sheath is a symmetric cone system expanding from 65mm. to 250mm. diameter through five cones 120mm. long as in turbine in application 64,799/94 and ~:...contracting from 250mm. to 65mm. in the same way means the closed cycle system is designed to handle greater than 10 6 w. of thermal energy with about 700 Newtons thrust from support plate 134 holes 6o with significantly higher thrust developed by creases on blades 5 particularly in the contraction section of turbine called blade thrust which means that if more blade plates are introduced into 6000 turbine system at low diameter section with eight or more sets of 606660 blade plates instead of two sets in lower diameter parts torque conversions from low diameter sections convert to pressure zone blade thrusts at large diameter blades in contraction section which give greater than 2,000N. (newtons) blade thrusts at Rotation rates of up to 45,000 R.P.M. (Revolutions per minute). Further to energy release from cone is energy release from a pressure ball at the end of each passage of the plate assembly. Again two types of energy release exist. Particle and ion activation occurs down passage of plate assembly and with resonance energy release nuclear order is transfered by sub-electron mass from cone close to turbine so viscosity and anti-nuclear field expansion allows the hot gases from cone to transfer energy. Order transfer from cone is essential 30 for energy release in a pressure ball at end of cone and again volume is limited as directional plasma from passage of plate assembly loses order in less than pico-seconds. The extra energy in the turbine is converted directly to thrust energy at high efficiency if moving or transfered to extra rotational energy'.

For resonance energy the exposed negative surface activate protons or nuclides 2 He) as directional plasma and mass depleates as resonance energy. In the case of reverse polarity electron plasma activated by the now exposed positive surfaces of the passage, shock energy is focused down the hyperbolic passage which tapers 00 from 10mm. to 2mm. diameter thus focusing significant amounts of shock energy which expands periphery of electron's fermi gas allowing a brief chain reaction in less than pico-seconds to occur allowing release of energy and sub-electron mass particle field in a small volume. Energy for electron bombardment release occurs close to cone and turbine in anti-nuclear field by shock energy eminating from source and carrying and thus diminishing sub-electron particle field density close to turbine and cone. Another aspect of thrust is pressure jet thrust from the very viscous positive ion or negative ion plasma from the passages of the plate assembly with excess ions of one type being responsible for very high viSCoSity of plasma. Such that charge excess plasma develops in end of passage of plate assembly producing high pressure low speed flows with pressures over.10 Pa. in end of passages assisted by high charge density on plates by Barium Titanate in ceramic inserts close to passages which also gives electrodynamic thrust or "pull" attractive thrust of ions towards exposed charged surface such that reaction force is experienced by mounted plate assembly on ,s{pport plate 134 which transfers thrust to turbine housing. This 31 low energy, high thrust output system is useful in that low energy, high thrust allows a secondary thrust system to operate in motion by releasing energy as thrust to energy of motion while a low energy,high thrust operates. Which means the 700N. of pressure thrust from holes in plate 134 operate while the lower energy, high thrust of the twelve passage plate assembly gives over 2,500N.

thrust or over 200N. per passage. The excess charge density is over 10-8 coulombs/mm 3 in end of passage. Operation of turbine can go to 45,000 R.P.M. but is designed to operate at 25,000 R.P.M. with 7.2 Kilo-watts of 600 amps,12 volts supplied to each coil of each turbine section (expansion and contraction section) with 900V. at 4 amps supplied to each plate assembly.

The total system is designed to operate at basically 10 w. but 5 the turbine can handle up to 3x 10 w. and greater than 10 6 w. can 15 be released as pressure thrust power of motion if cone is moving.

This equipment serves also to generate a sub-electron mass field s that eminates from cone and causes a convergence of further sub-

S

electron mass that builds the anti-nuclear field In the 0 case of electron chain reaction release small amounts of energy release by chain reaction also helps build field. The resonance A.N.F. is basically a positive charge excess field while chain reaction with surroundings nuclides (according to conservation of charge in particle releases) means A.N.F. in this case is negative charge excess field. One field causes attrition of the other field by primarily affecting the order of nuclides of the surroundings and also balancing charge thus reducing viscosity and allowing rapid release. Basically this equipment generates a A.N.F. that eminates to sites that are rich in energy and A.N.F. builds rapidly Sin'.'kese locations fires, explosions and fast moving objects.

32 With energy in terms of a resonance field going to mass (relativistic affect) and a bombardment field also increasing in mass (relativistic affect). Size of spread is related to output energy of cone. So this means that this equipment with a large enough output for sufficient spread to a Atomic blast site of 1015 Joules such that a A.N.F. builds rapidly to 10 4 0 particles of initial mass -21 of 10 2 1 u. can reach 10-u. and start to discharge and release field at a rate not humanly noticeable. A.N.F.'s that build at a particular site slowly equalize in charge and dispel.

Omitted was the aspect that the gear on the shaft of the turbine @0 is threaded to the shaft on a threaded section between two threaded collars weld tacked to shaft. Also magnetic thrust exists in turbine by action-reaction force from ions moving and being created by collisional multiplication in magnetic field through turbine. The voltage on plate assemblies of turbine is 900 volts or up to 4,000 volts can be applied.

6 o *0

Claims

1. Equipment for the release of depleted mass energy or mass to energy and the generation of a anti-nuclear field comprises a glass sheath which is externally silvered such that the electrically conducting sheath is supported by electrodes through electrically isolating compression fittings in plates at front of a three part sheath housing such that the field strength is about .2 tesla with about three minature plate assemblies of about three active sequences for acceleration and non-active sequences blocked by ceramic inserts S. 10 between charged plates being at front of sheath to inject ions into 3 sheath attaining over 10 9 coulombs/mm excess charge or greater o than 300,000 Pa. ion pressure such that these accelerated ions that are over 10 Mev. (mega-electron volts) undergo considerable collis- ional interaction passing into a preferably tungsten cone with 15 plasma over 109 OK activated by a tapering hyperbolically wound oooo coil increasing in number of windings towards large expanded hyper- bolic front with a vacuum of better than 10 6 atmospheric density maintained in sheath housing and cone which contains hydrogen or helium with a magnetic field strength of greater than 2 tesla in large front end of cone with energy release converted to heat that heats cone and inert gas, preferably hydrogen flowing over cone in hyperbolic void that contains cone which is heated and then vented through a turbine having a hyperbolic expansion section followed by a hyperbolic contraction section which re-compresses the vented, cooled hydrogen that has expended its energy in the expansion section of turbine as rotational or pressure thrust energy (if moving) so that the turbine has dual directional flow with the rotational direction changed for entry from oppositeend, with r iompressed, cooled hydrogen exiting turbine for re-entry to base 34 of hyperbolic void where cone is for re-heating and re-circulation through turbine such that a diminished pressure hot zone exists at large front end of cone for flow circulation to exist giving a system that releases energy and sub-electron mass from the energy release plasma in cone that absorbs energy and perpetuates further generation of sub-electron mass that builds a particle field of less than 10 K that absorbs energy from surroundings and is a anti-nuclear field which absorbs energy of fires, explosions or fast moving objects and then harmlessly disapates without being humanly noticeable.

2. The equipment as claimed in claim 1 for the acceleration of positive particles or nuclides, current is flowing to narrow base of sheath and minature assemblies have exposed negative surfaces in passage for positive ion injection into sheath which develops 15 very high nuclear vibrational orders that develop to nuclear field resonance pulses such that the directional plasma particles or S nuclides enter plasma cone and nuclear field interactions trans- fered by converging dark matter or sub-electron mass and by deplet- S ed mass releases, energy is released in cone with this nuclear order then spreading to surroundings with the depleted order resonance still strong enough to precipitate further sub-electron mass that builds the anti-nuclear field which absorbs energy of fires, explosions or fast moving objects and then harmlessly disapates without being humanly noticeable.

3. The equipment as claimed in claim 1 for the acceleration of electrons current is flowing to large curved end of sheath and minature plate assemblies have exposed positive surfaces in passage for electron injection into sheath which gives large amounts of 4 f lear shock energy that is focused down sheath expanding 35 periphery of electrons and lowering surface energy such that on entry into plasma cone a brief set of chain reactions occur in 9 OK plasma releasing energy in terms of depleted mass and sub-electron mass released with very rapid collapse of sub-electron mass boundaries energy release is limited to small volume of cone and only very small amounts of energy are released in surroundings with sub-electron mass that chain reacts further with minute energy release building a sub-electron mass particle anti-nuclear field which absorbs energy of fires,explosions or fast moving objects 10 and then harmlessly disapates without being humanly noticeable.

4. The equipment as claimed in claiml or claim 2 generates the oo ~anti-nuclear field from positive nuclides or particles from sheath which produces a positive charge excess sub-electron mass particle field from surrounding dark matter that converges and resonance 9o interactions are amplified through 10 K plasma cone that precipit- ates more sub-electron mass so order spreads to surroundings 0 0 precipitating larger volumes and amounts of viscous, positive 0 0 charge excess sub-electron mass particle field that absorbs energy o* .0 ~from surroundings, intensifying and increasing in volume at energy rich locations, first, in surroundings and then charge equalizing after energy is absorbed and dispelling. The equipment as claimed in claim 1 or claim 3 generates the anti-nuclear field from electron bombardment which produces a negative charge excess sub-electron mass particle field by chain reaction release from 109 oK plasma cone and surroundings absorbing energy from surroundings, intensifying in volume at energy rich locations, first, in surroundings and then charge equalizing after energy is absorbed and dispelling. The equipment as claimed in claim 1 with externally silvered 36 sheath of magnetic field greater than .2 tesla producing greater than 10 Mev. nuclides or particles produces a like ion film on surface of sheath greater than 10 9 coulombs/mm 3 or greater than 300,000 Pascal pressure has sheath supported by split current carrying copper rod which connects to copper collar over large end of externally silvered sheath with split copper tube electrically connecting sheath and supporting other end with high ion pressures attained by three or more minature plate assemblies of up to 4,000 Volt plate voltage with three or more series of plate accelerating sequences to hyperbolic passage such that ceramic bushes alternat- ively connect to each connection rod with each connection rod as a o terminal with ions or plasma leaving minature plate assembly direct- ed into sheath such that ions accelerated by sheath are directed through tube through hole in sliding rod valve with two sets of rings with a allignment groove at end of sliding valve stem or two centrally offset allignment holes for rods on end of stem.

7. The equipment as claimed in claim 1 or claim 6 with plates on end of sheath housing contain compression fittings with plastic ferrells and are rubber ringed backed for vacuum seal and attachment with electrical connections to minature plate assemblies are sealed in glazed alumina slugs which are alumina and Sodium Silicate binder which has been fired with end plates of end caps adjoining central assembly and f/laces on thick hollow bar overlaping with hollow bar to prevent radiation shine through rings which vacuum seal end caps to central assembly.

8. The equipment as claimed in claim 1 generates the greater than Mev. particles or nuclides which emerge into a preferably sinter- ed tungsten cone that has been infiltrated with Ruthenium Nitrosyl- rate, heated back to metal and electroplated with Ruthenium to 37 seal substrate with a plate at front and back of cone with ten- sioning rods of heat resistant alloy sealing top and back plate (also of Ruthenium electroplated tungsten) to surfaces with copper or Nickel foil gaskets and also supporting cone through compression fittings at rear of hyperbolic void which cone is in.

9. The equipment as claimed in claim 1 or claim 8 with the cone containing 10 9 OK plasma basically of hydrogen that is activated by laterally wound coil around a hyperbolically expanding sheath made of a cone series such that the number of windings is increasing 0 in a taper towards larger end with a magnetic field strength of *.o about 2 tesla at large end. The equipment as claimed in claim 1 or claim 8 with the cone having inert gas preferably hydrogen heating and absorbing heat from cone's surface as depleted mass from resonance order or elec- tron bombardment releases energy and Thorium oxide lining releasing thermal energy as resonance interaction, or electron bombardment- ••go chain reaction energy.

11. The equipment as claimed in claim 1 or claim 8 has nuclear order 149 retaining isotopes of high natural cross-sections such as 62Sm are added to cone lining of Thorium oxide with up to 2% metallic binder by weight in the form of Silver Nitrate and Ruthenium Nitrosyl- nitrate and heated back to metal with, from to 15% by weight Samarium oxide as a order retaining isotope that helps build nuclear order in cone that increases resonance energy release as sub-electron mass converges and is energized in cone.

12. The equipment as claimed in claim 1 or claim8 has disorder 187^ promoting isotopes such as 176s doped lining by being mixed with metallic binder solution of Silver Nitrate and Ruthenium Nitrosyl- t ate as Osmium Nitrate such that this naturally highly expanded 38 nuclide promotes the expansion of mass by disorder as sub-electron mass interacts with isotope nuclides in cone lining and the result is a greater chain reaction of sub-electron mass release and depleted mass energy release from bombarding electrons.

13. The equipment as claimed in claim 1 or claim 8 having tension- ing rods that are brazed to top plate through flanges (welded to tensioning rods) by Palladium/Silver alloy braze with bottom plate pressured shut by spring to tensioning rod sheath external to cone which presses rod sheath to copper ferrell which seals rod to bush .10 which is brazed into base plate of cone such that tensioning rod can still slide through copper ferrell sealing tensioning rod to external bush of base plate.

14. The equipment as claimed in claim 1 or claim 8 for resonance energy release has electrodes protruding into cone at distinct 15 depths from base through compression fittings being located in 0 ,00 electrically isolating glazed alumina grit rod or slug in soft metal ferrell of compression fitting such that electricity is *.go* released through electrodes by charge separation of 10 9 OK plasma of cone with reverse thrust being felt on side of cone by pressure thrust from plasma with a swirling action of plasma that assists pressure thrust such that current flow in coil is anti-clockwise seen from left (cone's small base) gives a right to left magnetic field through cone with a anti-clockwise circulation of plasma seen from left (cone's small base) and with current flow in coil that is clockwise seen from left gives a left to right magnetic field through cone with clockwise circulation of plasma seen from left or narrow end of expanding hyperbolic void which cone is in. The equipment as claimed in claim 1 or claim 8 or claim 14 for ,S9 IV .\ectron bombardment chain reaction energy release has the electrodes 39 as in previous claim become a cathode source through which electrons pass through a anode grid towards front of cone with electrodes in glazed alumina rod or slug for electrical isolation through metal ferrell in compression fitting with a pilot high voltage supply of up to 4,000 Volts with a bulk supply of much higher current at about 600 Volts with forward pressure, plasma thrust on front of cone such that anti-clockwise current flow seen from left (cone's small base) gives right to left magnetic field with anti- clockwise circulation seen from left and with clockwise current 10 flow seen from left (cone's small base) giving left to right magnetic field with clockwise circulation seen from left or narrow end of expanding hyperbolic void which cone is in.

16. The equipment as claimed in claim 1 or claim 8 has hyperbolic sheath or void cone is in,surrounded by a coil housing which has 15 a branched system of stainless steel tubing with a multiplicity of tiny holes through which cooling hydrogen from turbine enters coil Shousing which has a cover pressing on machined surfaces to make gas seal and stainless steel tubing is electrically isolated from windings by alumina fibre insulation with windings set in Sodium Silicate bound grit greater than .5mm. in diameter.

17. The equipment as claimed in claim 1 or claim 8 has a 12mm. lead cover supported by plate steel and is around cone and hyperbolic sheath supporting coil housing in case of cone rupture and sudden X-ray release.

18. The equipment as claimed in claim 1 or claim 8 for outlet from hyperbolic void cone is in has the lower pressure, high temperature region outlet that has a series of 1.6mm. tungsten plates of increas- g diameter to stop release of X-rays in case of cone rupture. yhe equipment as claimed in claim 1 or claim 8 has return 40 hydrogen from turbine being cooled and re-compressed enters at base of cone flowing over surface for heating and de-pressurizes slightly in hot zone at front of cone before venting into turbine again.

20. The equipment as claimed in claim 1 or claim 8 has return hydrogen from cooling coils of cone and turbine sections entering at hot lower pressure region at front of cone for heating and before venting again through turbine.

21. The equipment as claimed in claim i or claim 8 has radioactive 0 vapour bled into vacuum evacuation line of cone for destruction 0Kpam oe of radioactive substances in 10 9 K plasma cone.

22. The equipment as claimed in claim 1 has hot hydrogen from hot see. oo. low pressure region at front of cone entering at base of turbine and entering turbine section through plate welded to sheath of 2 turbine with over 700mm. of less than .4mm. diameter holes for pressure propulsion and flow through plate assembly electrically p S active at that end with about twelve passages with a area reduction :of about twenty five times (through plate assembly) such that the expanding gas flows over blades for left to right hydrogen flow (through turbine) and a left to right magnetic field (through turbine) means current flows clockwise and blades spin clockwise seen from left and conversely for right to left hydrogen flow and a right to left magnetic field current flows anti-clockwise and blades spin anti- clockwise seen from left and so with left to right hydrogen flow blades at top angle to left with a crease at upper top side and at bottom blades angle to right with crease at upper top side looking from left expansion section with top blades in contraction section angling to left with crease on bottom under-side and bottom SRAngling to right with crease on bottom under-side such that a 4es angling to right with crease on bottom under-sd uhta 41 pressure zone generates at crease for increased blade thrust in contraction section after gas has expanded in expansion section and so with right to left hydrogen flow giving anti-clockwise blade spin seen from left and blade thrust in the opposite direction in the other section which is now a contraction section and with coils in coil housings going in the direction of left to right expansion for the dual hyperbolic turbine, going to a increasing number of windings in expansion section and in the contraction section, coil in coil housing tapering to fewer windings. 0 23. The equipment as claimed in claim 1 or claim 22 has coil housings of turbine having a branched system of stainless steel tubing with a multiplicity of tiny holes through which cooling hydrogen from turbine enters coil housing which has a cover with flange pressing on machined surfaces to make gas seal and stainless steel tubing 0000 15 is electrically isolated from windings by alumina fibre insulation with windings set in Sodium Silicate bound grit greater than 0000 in diameter with each of the adjacent coil housing covers bolted together through adjacent flanges.

24. The equipment as claimed in claim 1 or claim 22 has left and right sections of turbine bolted together and at each end a accurate allignment surface is bolted to plate with accurate allignment surface to which bearing housing adjoins and alligns to which then a bearing cover slides over and flange plate joins to which turbine assembly is mounted in accurate surfaces or forks at both ends of rigid right handed section steel. The equipment as claimed in claim 1 or claim 22 has a split bush joined by threaded collars and weld tacked around shaft at end of each turbine section through plates that allign bearing housing to A- th and this limits hydrogen escape from turbine with one plate -42 in bearing housing fixed with central compression fitting with split P ferrell to further limit hydrogen escape followed by another plate fixed with central compression fitting with split plastic ferrell to further limit hydrogen escape after which a vacuum bleed line draws off any residual hydrogen in compartment sealed by third fixed plate with central compression fitting with split plastic ferrell such that this split bush, system of three plates with compression fittings with split ferrells and vacuum line exists at both ends of turbine. 10 26. The equipment as claimed in claim 1 or claim 22 has threaded 99 collars for plates of blades fix plates of blades to threaded section of tubular shaft with weld tacs at low diameters for insignificant dynamic imbalance to permanently secure plates of blades with shaft having up to eight or more plate sets at low 15 diameter part of expansion section of turbine for adequate torque ••go conversion to blade thrust of large diameter blades in contraction section for each direction of flow. S27. The equipment as claimed in claim 1 or claim 22 has split copper 9.9 hollow bushes with rings having grooves for water flow, are brazed together and accurately machined so when set adjacent to each other holes for water flow are alligned so as to cool high rotation speed bearing pairs.

28. The equipment as claimed in claim i or claim 22 has shaft joined outside hydrogen bleed-off compartment by accurate alligned surfaces and weld tacked on left and right side outside turbine section with cut-away on right side being for gear threaded on shaft between two threaded collars, weld tacked to shaft which connects to two or more intermediate gears mounted by bolt through i/ ernal sleeve over bearing cover, bolted to bearing cover with 43 intermediate gears allowed to turn between two opposed angle, angular thrust bearings with these intermediate gears connecting to external cover with internal and external gear runner from which rotational drive is attained with external cover turning on two opposed angle, angular thrust large bearings with oil seals of low friction plastic on either end of moving external cover of gear housing.

29. The equipment as claimed in claim 1 or claim 22 has oil entering bearing housing on left side and flows around bearings and is bled 1 i*.0 off from other side of bearing housing next to join in shaft and on right enters from end of bearing housing flowing through bearings *see and gear housing and bearings of gear housing and is bled off at end 0*000 of bearing housing again. The equipment as claimed in claim 1 or claim 22 has cooling water 15 entering shaft through stationary bush over shaft with close 0 0 tolerances to spinning surface alligned by shaft and attached to end of shaft by threaded collar internally welded to shaft over which a collar is threaded to pre-load bearings with a external surface so a stationary plate with a fitting with accurate plastic bush forming a seal for oil.

31. The equipment as claimed in claim 1 or claim 22 has each plate assembly bolted to plate which is welded to narrow base of turbine sheath by four 10mm. tungsten bolts for expansion compatability with two bolts being connection rods with each alternate plate connected to tungsten rod which is electrically isolated by support plate by ceramic washers and electrically isolated from tungsten rod and every alternate plate by ceramic washers with ceramic sRAqerts blocking the non-active polarity sequences of plates with wi.h material of high Dielectric constant such as Barium Titanate 44 mixed with alumina near hyperbolically tapering passages to attain greater than ten nano-coulombs per cubic millimeter excess charge density for viscous low velocity pressure thrust in end of the greater than twenty five times area reduced hyperbolic passages plate assembly and give elctrodynamic thrust also in passages by pulling ions towards exposed internal surfaces during flow through passages in terms of reaction with greater than 200 Newtons thrust per passage at plate voltages up to 4,000 volts.

32. The equipment as claimed in claim 1 or claim 22 for negative 0 exposed surfaces in plate assembly a pressure ball of small volume of resonance energy forms at end of each hyperbolic tapering passage giving thrust of high efficiency and energy release close to nuclear o order releases from cone.

33. The equipment as claimed in claim 1 or claim 22 for reverse 15 polarity on plate assembly and positive exposed surfaces in plate assembly a pressure ball of small volume of bombardment chain oo*o S reaction energy due to focused shock energy down hyperbolic passage of plate assembly giving thrust of high efficiency and energy release.

34. The equipment as claimed in claim 1 or claim 22 has lower energy, high thrust output from plate assembly passage in terms of electro- dynamic thrust and pressure jet thrust gives secondary lower, higher energy thrusts of more efficiency as the pressure thrust is in the form of the blade thrust and pressure thrust through less than .4mm. holes in support plate for plate assembly.

35. The equipment as claimed in claim 1 or claim 22 alumina bush that electrically isolates plate assembly from spinning shaft is located in compression fitting in support plate and compensated against thermal expansion by having a dual angled metal bush with Rof the two halves slitted with the halves in front of the 04, of the two halves slitted with the halves in front of the 45 alumina bush.

36. The equipment as claimed in claim 1 or claim 22 having magnetic thrust existing in turbine by reaction to ion motion down through sheath of turbine with magnetic field multiplying ion number from plate assembly operation.

37. Equipment for the release of depleated mass energy being prin- cipally sheath, cone, turbine and housings substaintially as herein described with reference to accompanying drawings. GEORGE CONTOLEON 28TH. OF SEPTEMBER,2000. a* APPLICANT DATE g i 00 f S e S 9 S 9 S S