A Practical Guide to 'Free-Energy' Devices

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the various inert gases, which layering is designed to confine the input energy in the innermost layers during preexcitement and ignition, to provide thermal insulation for the container walls during and after ignition, to transmit power resulting from the ignition through the layers in turn to the piston, to absorb the pressure generated during ignition to protect the cylinder walls, and to provide an orderly, predictable positioning of the argon layer during the BDC to TDC portion of the engine cycle. The third concept of this invention involves utilising electric current produced in one cylinder of a pair to perform functions in the other cylinder of that pair. This concept includes the sub-concepts of generating electric current by atomic recombination and of electric generation in place resulting from the rotation of layered inert gases within each cylinder because of the changed polarity of the encircling coils at BDC, from judicious placement of coils which produce magnetic field lines which are cut by a near perfect conductor (polarised argon), and from movement of said near perfect conductor through the magnetic field. The fourth and fifth concepts of this invention are the transformation of rapid, intense, but short duration thermonuclear reactions into pressure that is transmitted from inert gas to inert gas until it creates linear kinetic energy at the piston, which energy is converted into rotary kinetic energy by a crankshaft, and the use of a shaftdriven generator to provide power to spaced field coils during the BDC to TDC portion of the cycle of each cylinder. The sixth concept concerns adequate pre-excitement of the inert gas fuel and more particularly involves the subconcepts of pre-exciting the fuel in the mixing process, of manipulation of the currents in the coils surrounding each cylinder, of discharging the capacitors surrounding each cylinder at predetermined times in the cycles, of causing a stream of electrical particles to flow between electrodes and a conductive discharge point on the piston, of emitting alpha, beta and gamma rays from an anode and a cathode containing low level radioactive material to the piston's discharge point, of accelerating the alpha, beta and gamma rays by the application of a high-voltage field, and of situating capacitor plates 90 degrees from the anode and cathode to slow and reflect neutrons generated during ignition. The seventh concept involves the provision of a minute, pellet-type fission ignition, the heat from which causes a minute fusion as the result of the ignition chamber shape and arrangement, as a result of the collision of the alpha, beta and gamma rays and the electrical particles at a focal point in conjunction with the discharge of the capacitors that surround the cylinder through the electrodes, and as a result of increasing the magnetic field in the direction of the movement of each piston. A - 1186
Robert Britt US Patent 3,977,191 31st August 1976 Inventor: Robert G. Britt ABSTRACT ATOMIC EXPANSION REFLEX OPTICS POWER SOURCE (AEROPS) ENGINE An engine is provided which will greatly reduce atmospheric pollution and noise by providing a sealed system engine power source which has no exhaust nor intake ports. The engine includes a spherical hollow pressure chamber which is provided with a reflecting mirror surface. A noble gas mixture within the chamber is energised by electrodes and work is derived from the expansion of the gas mixture against a piston. SUMMARY OF THE INVENTION An atomic expansion reflex optics power source (AEROPS) engine, having a central crankshaft surrounded by a crankcase. The crankcase has a number of cylinders and a number of pistons located within the cylinders. The pistons are connected to the crankshaft by a number of connecting rods. As the crankshaft turns, the pistons move in a reciprocating motion within the cylinders. An assembly consisting of a number of hollow spherical pressure chambers, having a number of electrodes and hollow tubes, with air-cooling fins, is mounted on the top of each cylinder. The necessary gaskets are provided as needed to seal the complete engine assemblies from atmospheric pressure. A means is provided to charge the hollow spherical pressure chamber assembly and the engine crankcase with noble gas mixtures through a series of valves and tubes. A source of medium-voltage pulses is applied to two of the electrodes extending into each of the hollow spherical pressure chambers. When a source of high-voltage pulses is applied from an electrical rotary distributor switch to other electrodes extending into each of the hollow spherical pressure chambers in a continuous firing order, electrical discharges take place periodically in the various hollow spherical pressure chambers. When the electrical discharges take place, high energy photons are released on many different electromagnetic frequencies. The photons strike the atoms of the various mixed gases, e.g., xenon, krypton, helium and mercury, at different electromagnetic frequencies to which each is selectively sensitive, and the atoms become excited. The first photons emitted are reflected back into the mass of excited atoms by a reflecting mirror surface on the inside wall of any particular hollow spherical pressure chamber, and this triggers more photons to be released by these atoms. They are reflected likewise and strike other atoms into excitation and photon energy release. The electrons orbiting around the protons of each excited atom in any hollow spherical pressure chamber increase in speed and expand outward from centre via centrifugal force causing the atoms to enlarge in size. Consequently, a pressure wave is developed, the gases expand and the pressure of the gas increases. As the gases expand, the increased pressure is applied to the top of the pistons in the various cylinders fired selectively by the electrical distributor. The force periodically applied to the pistons is transmitted to the connecting rods which turn the crankshaft to produce rotary power. Throttle control valves and connecting tubes form a bypass between opposing hollow spherical pressure chambers of each engine section thereby providing a means of controlling engine speed and power. The means whereby the excited atoms are returned to normal minimum energy ground-state and minimum pressure level, is provided by disrupting the electrical discharge between the medium-voltage electrodes, by cooling the atoms as they pass through a heat transfer assembly, and by the increase in the volume area above the pistons at the bottom of their power stroke. The AEROPS engine as described above provides a sealed unit power source which has no atmospheric air intake nor exhaust emission. The AEROPS engine is therefore pollution free. BRIEF OBJECTIVE OF THE INVENTION This invention relates to the development of an atomic expansion reflex optics power source (AEROPS) engine, having the advantages of greater safety, economy and efficiency over those disclosed in the prior art. The principal object of this invention is to provide a new engine power technology which will greatly reduce atmospheric pollution and noise, by providing a sealed system engine power source which has no exhaust nor intake ports. Engine power is provided by expanding the atoms of various noble gas mixtures. The pressure of the gases increases periodically to drive the pistons and crankshaft in the engine to produce safe rotary power. The objects A - 1187
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JUAN AGUERO Patent Application EP04
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the exhaust manifold. This heats so
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combustion chambers. The hydrogen i
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21. The system of claim 20, charact
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electrolysis of water at such a rat
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Fig.4 is an elevation view of the h
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Fig.10 is a cross-section on the li
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Fig.16 is a cross-section on the li
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Fig.23 is an enlargement of part of
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Fig.33 is a perspective view of a v
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A - 843
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through a resistor R4 to provide tr
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The installation of the above circu
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cathode in the upper region of the
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transformer and, assuming an input
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valve apparatus to control engine s
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. a first hollow cylindrical electr
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CHRISTOPHER ECCLES UK Patent App. 2
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Fig.1 is a circuit diagram of fract
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If a large electric field is applie
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The pulses R1 and S1 are of the sam
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DISCLOSURE OF THE INVENTION The inv
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A - 867
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Fig.5B shows a stylised representat
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Fig.6 shows a gas collection system
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Fig.8A and Fig.8B are views of a se
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A - 875
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Figs.16-30 are graphs supporting th
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A - 879
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A - 881
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A - 883
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A - 885
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A - 887
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If it is the case that the hydrogen
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plate shown in Fig.1A and Fig.1B an
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is in equilibrium where the 10 watt
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The previously mentioned prior art
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The stores of high pressure gases c
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unit to retain operational gas pres
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HENRY PAINE This is a very interest
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Henry Paine’s apparatus would the
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some form of distortion of space. I
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superconductive disk is made part o
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Fig.2A and Fig.2B are diagrams, pre
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Fig.4A and Fig.4B are diagrams, pre
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#1 hollow superconductive shield #2
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Fig.2B shows the counter-clockwise
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In this example, the difference bet
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CHARLES POGUE US Patent 642,434 12t
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Fig.3 is a horizontal sectional vie
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Fig.9 and Fig.10 are detail section
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having a valve 52 in it. Chamber 50
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CHARLES POGUE US Patent 1,997,497 9
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Fig.4 is a detail sectional view of
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A low-speed or idling jet 25 has it
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DESCRIPTION OF THE DRAWINGS Fig.1 i
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Fig.5 is a detail sectional view on
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Vapour formed by air bubbling throu
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From the foregoing description it w
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Fig.2 is an enlarged view of the de
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Fig.6 is a section taken along line
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ROBERT SHELTON US Patent 2,982,528
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Fig.4 is a transverse sectional vie
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HAROLD SCHWARTZ US Patent 3,294,381
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182,420 now abandoned. The present
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DESCRIPTION OF THE INVENTION The ca
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THOMAS OGLE US Patent 4,177,779 11t
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In accordance with other aspects of
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Fig.3 is a sectional view of the va
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Fig.7 is a partial side, partial se
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The cooling system of the vehicle c
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Upon initial starting of the engine
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(f) A filter positioned in the vapo
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with the magnitude of the current a
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Fig.1B is a perspective view of the
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Fig.3 is a top view of the motor of
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Fig.7 is an isometric view showing
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Fig.10 is a top view showing the ro
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Fig.13 is a top view of a pair of r
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Extending in opposite diametric dir
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Fig.5 shows the state of the switch
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otor magnets 42 - 49 when in the ho
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Fig.9 and Fig.10 show a second arra
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constructed otherwise than as speci
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12. The motor of claim 11 wherein t
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timer or a control mechanism mounte
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Fig.4 is a view similar to Fig.3 bu
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Fig.10 is a view similar to Fig.3 f
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Fig.13 is a schematic circuit diagr
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Fig.16 is a simplified embodiment o
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Fig.22 to Fig.25 are similar to Fig
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Referring to Fig.2, the permanent m
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Fig.7 shows a modified embodiment w
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them, will depend upon the order in
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Fig.14, shows another embodiment 14
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Fig.18 shows the air coil 210 posit
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Figs. 22-25 show four different pos
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movement with the first permanent m
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a shaft and means journaling the sh
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CLAUDE MEAD and WILLIAM HOLMES US P
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Fig.2 is a front elevation of the w
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impactors and drills. The turbine d
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(a) fourth rotating means responsiv
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path to the other side of the perma
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Fig.3 is an oscilloscope waveform t
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DETAILED DESCRIPTION OF THE PREFERR
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although it is by no means obvious
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second diode connected at its posit
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In the present invention, a permane
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Fig.4 is a circuit diagram, illustr
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and Fig.3. In practice, this coil m
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y a simultaneous magnetic accelerat
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Mr. P.G. Mallory started out in 191
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All models have a 30 Watt power rat
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In the auto racing circles it has a
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BATTERY + _ SIMPLIFIED MULTIVIBRATO
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Schematic Wiring Diagrams for two P
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motor. What is not generally known,
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Mark McKay's investigation of Edwin
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Investor Photo #012D Popping a coil
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capacitors connected in series, wit
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PULSE WIDTH TIME IN mS went to the
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TOP DEAD CENTER 0° REFERENCE Accor
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The recovery and simple analysis of
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FILTER CAPACITOR + 2 OHM 200 WATT R
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Subject: CSET design Date: Sun Feb
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Date: Fri Feb 28, 2003 8:25 pm (Tim
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(Tad Johnson) I'm being as careful
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SANGAMO ENERGY DISCHARGE CAPACITOR
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(Alan Francoeur) But I also measure
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Subject: Progress Date: Sun Mar 30,
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● all electrical connections were
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Mark Gray claims that the heart and
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Mark Gray claims that some potentia
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Radio Frequency (RF) Generator Gene
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Some time during 1987 - 1988, Gray
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The two-channel trace from the osci
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What “maximum squareness” means
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Zo = 112 Ohms Td of 293 nS. 50 KV 8
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MIKE BRADY’S “PERENDEV” MAGNE
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Fig.3 is a perspective view showing
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Fig.7 is a perspective view showing
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In the rotor assembly 30 of Fig.2,
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Fig.7 shows a typical magnetic sour
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DONALD A. KELLY ABSTRACT Patent US
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This series of magnetic oscillating
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Because there is no natural, lock-i
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Fig.3 is an enlarged top view of on
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An arm 9, is fastened to a flat fac
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Fig.2 is a vertical transverse cros
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Fig.6 is a vertical, longitudinal,
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Working inside the cylinders 12 are
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Leroy K. Rogers Patent US 4,292,804
Page 313 and 314: Preferred embodiments of a method a
Page 315 and 316: Fig.6 is a cross-sectional view of
Page 319 and 320: tapped hole in the cylinder 20 typi
Page 321 and 322: A second embodiment of a valve actu
Page 323 and 324: otates faster, the other end 98 of
Page 325 and 326: In normal operation (as seen in Fig
Page 327 and 328: Eber Van Valkinburg Patent US 3,744
Page 329 and 330: Referring to the drawings in detail
Page 331 and 332: Since the pump depends for its supp
Page 333 and 334: Briefly, in one aspect the engine o
Page 337 and 338: Fig.12 is a cross-sectional view si
Page 339 and 340: Fig.14 is a schematic diagram of an
Page 341 and 342: A - 1163
Page 343 and 344: A - 1165
Page 345 and 346: Figs.20A-20F are schematic diagrams
Page 347 and 348: Note: Corresponding reference chara
Page 349 and 350: Integral with the piston bodies are
Page 351 and 352: The piston has a generally semi-tor
Page 353 and 354: Referring back to Fig.13A, for engi
Page 355 and 356: As piston 39A reaches BDC, distribu
Page 357 and 358: mixture and do not combine because
Page 359 and 360: These wires are about twelve gauge,
Page 361 and 362: cold-cathode tube 391, and an x-ray
Page 363: Fig.17D), polariser 289, branch B17
Page 367 and 368: Fig.3 is an elevational view of the
Page 369 and 370: Fig.7 is an electrical schematic of
Page 371 and 372: Referring now to Fig.3 of the drawi
Page 373 and 374: and drives Q1 into conduction. The
Page 375 and 376: Floyd Sweet Recently, some addition
Page 377 and 378: The day when we witnessed the VTA d
Page 379 and 380: up to see Floyd. Floyd was with the
Page 381 and 382: Energy cannot enter a space of zero
Page 383 and 384: electromagnetic and gravitational f
Page 385 and 386: or in another form: So, the e.m.f.
Page 387 and 388: Example 2: Suppose the conductor wi
Page 389 and 390: Meguer Kalfaian There is a patent a
Page 391 and 392: Fig.2 illustrates a controlled top
Page 393 and 394: Fig.9 is a modification of Fig.6; a
Page 395 and 396: the outer periphery of the magnet,
Page 397 and 398: wobbling top is sufficient, as proo
Page 399 and 400: Theodore Annis & Patrick Eberly US
Page 401 and 402: BRIEF DESCRIPTION OF THE DRAWINGS F
Page 403 and 404: Fig.6 is a schematic diagram of a s
Page 405 and 406: DETAILED DESCRIPTION OF THE PREFERR
Page 407 and 408: Fig.5 is a detail drawing of an alt
Page 409 and 410: In the preferred implementation of
Page 411 and 412: William McDavid junior US Patent 6,
Page 413 and 414: This sloping floor causes the drive
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FIG.3 is a side elevational view of
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FIG.9 is a horizontal cross-section
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otational downstream annular chambe
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In Fig.5 is shown a perspective vie
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small hydro-electric version of the
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Fig.10 is a perspective view of a s
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longitudinally mounted in the upstr
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shaft in the central aperture, said
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Scientific Papers The following lin
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