A Practical Guide to 'Free-Energy' Devices

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and may envelope the lower shell 4. Even though the preferred embodiment has two rotating elements, those skilled in the art may envision only one rotating element, or three or more rotation elements, all within the scope of this invention. Upper means for generating an electromagnetic field 8 are disposed between the hollow superconductive shield 1 and the upper shell 3. The upper means for generating an electromagnetic field 8 are fixed to the upper rotating element 6 at an electromagnetic field-penetrable distance to the hollow superconductive shield 1. Lower means for generating an electromagnetic field 9 are disposed between the hollow superconductive shield 1 and the lower shell 4. The lower means for generating an electromagnetic field 9 are fixed to the lower rotating element 7 at an electromagnetic field-penetrable distance to the hollow superconductive shield 1. The upper means for generating an electromagnetic field 8 and the lower means for generating an electromagnetic field 9 could be solenoid coils or electromagnets. In the process of operation of the space vehicle, the electromagnetic field identified by flux lines 10, is controllably and variably applied to the hollow superconductive shield 1. Electric motors are disposed inside the hollow superconductive shield along its central axis. A power source 11 is disposed inside the hollow superconductive shield 1 and may be disposed inside the lower shell 4. The power source 11 is electrically connected with the upper means for generating an electromagnetic field 8, the lower means for generating an electromagnetic field 9, and the electric motors. The upper means for generating an electromagnetic field 8, the lower means for generating an electromagnetic field 9, and the electric motors provide for the rotation of the upper rotating element 6 and the lower rotating element 7. The power source 11 may be a nuclear power generator. Life-support equipment 12 is disposed inside the inner shield 2, and may be disposed inside the lower shell 4. The life-support equipment 12 may include oxygen, water, and food. A flux modulation controller 13 is disposed inside the inner shield 2, and may be disposed inside the upper shell 3. The flux modulation controller 13 is in communication with the upper means for generating an electromagnetic field 8, the lower means for generating an electromagnetic field 9, the power source 11, and the electric motors. The flux modulation controller 8 may be executed as a computer or a microprocessor. The flux modulation controller 8 is provided with a capability of modulating the performance parameters of the upper means for generating an electromagnetic field 8, the lower means for generating an electromagnetic field 9, the power source 11, and the electric motors. A crew 14 may be located inside the upper shell 3 of the inner shield 2 and may consist of one or more astronauts. The crew has a free access to the life-support equipment 12 and the flux modulation controller 8. A person skilled in the art, may envision a fully-automated, pilotless craft, which is also within the scope of this invention. A person skilled in the art, may also envision the embodiment (not shown), also within the scope of this invention, where the hollow superconductive shield is pivotable, and the support structure with the means for generating an electromagnetic field is affixed on the outside of the inner shield. Fig.2A and Fig.2B are diagrams showing the results of the quantised electromagnetic turbulence within the superconductive shell of the hollow superconductive shield provided by the relative rotational motion of the hollow superconductive shield against the upper means for generating an electromagnetic field. Fig.2A shows the clockwise relative rotational motion of the hollow superconductive shield, this motion identified by a clockwise shield motion vector 15, and the counter-clockwise relative rotational motion of upper means for generating an electromagnetic field, this motion identified by a counter-clockwise EMF motion vector 16. The electromagnetic field, controllably and variably applied by the upper means for generating an electromagnetic field, whose various positions are identified by a wire grid 17, to the hollow superconductive shield (not shown), causes quantised electromagnetic turbulence within the hollow superconductive shield. This turbulence is represented by a plurality of clockwise quantised vortices of lattice ions 18. Only one line of the clockwise quantised vortices of lattice ions 18, (not to scale), is shown for illustration purposes only. Each of the clockwise quantised vortices of lattice ions 18 generates a gravitomagnetic field identified by an outward gravitomagnetic field vector 19 directed orthogonally away from the hollow superconductive shield. A - 914
Fig.2B shows the counter-clockwise relative rotational motion of the hollow superconductive shield, this motion identified by a counter-clockwise shield motion vector 20, and the clockwise relative rotational motion of upper means for generating an electromagnetic field, this motion identified by a clockwise EMF motion vector 21. The electromagnetic field, controllably and variably applied by the upper means for generating an electromagnetic field identified by the wire grid 17, to the hollow superconductive shield (not shown), causes quantised electromagnetic turbulence within the hollow superconductive shield, this turbulence represented by a plurality of counter-clockwise quantised vortices of lattice ions 22. Only one line of the counter-clockwise quantised vortices of lattice ions 22, (not to scale), is shown for illustration purposes only. Each of the counter-clockwise quantised vortices of lattice ions 22 generates a gravitomagnetic field identified by an inward gravitomagnetic field vector 23 directed orthogonally toward the hollow superconductive shield. The electrical requirements for providing the Li-Torr effect are as follows: Podkletnov has reported using the high frequency current of 105 Hz. He also used 6 solenoid coils @ 850 Gauss each. The reported system's efficiency reached 100% and the total field in the Podkletnov's disk was about 0.5 Tesla. The maximum weight loss reported by Podkletnov was 2.1%. The preferred embodiment of the device of current invention is capable of housing 2-3 astronauts and therefore is envisioned to be about 5 meters in diameter at the widest point. The preferred space vehicle's acceleration is set at 9.8 m/s/s providing that gravity on board is similar to that on the surface of Earth. The means for generating an electromagnetic field may be comprised of 124 solenoid coils. At the same 100% efficiency reported by Podkletnov, the total field required providing the acceleration of 9.8 m/s/s is 5,000 Tesla, or about 40 Tesla per coil. Skeggs suggests that on the Podkletnov device, out of 850 Gauss developed on the coil surface, the field affecting the superconductor and causing the gravitomagnetism is only 400 Gauss ("Engineering Analysis of the Podkletnov Gravity Shielding Experiment, Peter L. Skeggs, Quantum Forum, Nov. 7, 1997, http://www.inetarena.com/˜noetic/pls/podlev.html, 7 pages). This translates into 47% device efficiency. In this 47%-efficient space vehicle, the total field required achieving the 9.8 m/s/s acceleration is about 10,600 Tesla, or 85.5 Tesla per each of 124 solenoid coils. It must be noted that at this acceleration rate, it would take nearly a year for the space vehicle to reach the speed of light. It also must be noted that Skeggs has detected a discrepancy between the Li-Torr estimates and Podkletnov's practical results. If Podkletnov's experimental results are erroneous while the Li-Torr estimates are indeed applicable to the space vehicle of this invention, then the energy requirements for achieving the sought speed would be substantially higher than the above estimate of 10,600 Tesla. Podkletnov has concluded that, in order for the vacuum pressure density anomaly to take place, the Earth-bound device must be in the condition of Meissner levitation. As are all space bodies, the space vehicle is a subject to the pressure inflationary vacuum state and the gravitational force, which, within the migrating locality of the expanding Universe, in any single linear direction, are substantially in equilibrium. Thus, for the space vehicle, the requirement of Meissner levitation is waved. The propagation of the gravitomagnetic field identified by the outward gravitomagnetic field vector 19 and the inward gravitomagnetic field vector 23 would cause exotic quantised processes in the vacuum's subatomic particles that include particle polarisation, ZPF field defects, and the matter-energy transformation per E=mc 2 . The combination of these processes would result in the gravitational anomaly. According to the general relativity theory, gravitational attraction is explained as the result of the curvature of space-time being proportional to the gravitational constant. Thus, the change in the gravitational attraction of the vacuum's subatomic particles would cause a local anomaly in the curvature of the Einsteinean space-time. Gravity is the same thing as bent space, propagating with the speed of light characteristic for the particular spacetime curvature. When bent space is affected, there is a change in the speed of propagation of gravity within the space-time curvature anomaly. The local speed of light, according to Fomalont and Kopeikin always equal to the local speed of propagation of gravity, is also affected within the locality of space-time curvature anomaly. Creation of space-time curvature anomalies adjacent to, or around, the space vehicle, these anomalies characterised by the local gravity and light-speed change, has been the main object of this invention. Fig.3A shows a diagram of a vacuum pressure density anomaly associated with lowered pressure of inflationary vacuum state 24 on the background of Universal curvature of inflationary vacuum state 25. The vacuum pressure density anomaly associated with lowered pressure of inflationary vacuum state 24 is formed by a multitude of the inward gravitomagnetic field vectors. According to the cosmological constant equation, A - 915
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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
Page 41 and 42: The pulses R1 and S1 are of the sam
Page 43 and 44: DISCLOSURE OF THE INVENTION The inv
Page 45 and 46: A - 867
Page 47 and 48: Fig.5B shows a stylised representat
Page 49 and 50: Fig.6 shows a gas collection system
Page 51 and 52: Fig.8A and Fig.8B are views of a se
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Page 55 and 56: Figs.16-30 are graphs supporting th
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Page 67 and 68: If it is the case that the hydrogen
Page 69 and 70: plate shown in Fig.1A and Fig.1B an
Page 71 and 72: is in equilibrium where the 10 watt
Page 73 and 74: The previously mentioned prior art
Page 75 and 76: The stores of high pressure gases c
Page 77 and 78: unit to retain operational gas pres
Page 79 and 80: HENRY PAINE This is a very interest
Page 81 and 82: Henry Paine’s apparatus would the
Page 83 and 84: some form of distortion of space. I
Page 85 and 86: superconductive disk is made part o
Page 87 and 88: Fig.2A and Fig.2B are diagrams, pre
Page 89 and 90: Fig.4A and Fig.4B are diagrams, pre
Page 91: #1 hollow superconductive shield #2
Page 95 and 96: In this example, the difference bet
Page 97 and 98: CHARLES POGUE US Patent 642,434 12t
Page 99 and 100: Fig.3 is a horizontal sectional vie
Page 101 and 102: Fig.9 and Fig.10 are detail section
Page 103 and 104: having a valve 52 in it. Chamber 50
Page 105 and 106: CHARLES POGUE US Patent 1,997,497 9
Page 107 and 108: Fig.4 is a detail sectional view of
Page 109 and 110: A low-speed or idling jet 25 has it
Page 111 and 112: DESCRIPTION OF THE DRAWINGS Fig.1 i
Page 113 and 114: Fig.5 is a detail sectional view on
Page 115 and 116: Vapour formed by air bubbling throu
Page 117 and 118: From the foregoing description it w
Page 119 and 120: Fig.2 is an enlarged view of the de
Page 121 and 122: Fig.6 is a section taken along line
Page 123 and 124: ROBERT SHELTON US Patent 2,982,528
Page 125 and 126: Fig.4 is a transverse sectional vie
Page 127 and 128: HAROLD SCHWARTZ US Patent 3,294,381
Page 129 and 130: 182,420 now abandoned. The present
Page 131 and 132: DESCRIPTION OF THE INVENTION The ca
Page 133 and 134: THOMAS OGLE US Patent 4,177,779 11t
Page 135 and 136: In accordance with other aspects of
Page 137 and 138: Fig.3 is a sectional view of the va
Page 139 and 140: Fig.7 is a partial side, partial se
Page 141 and 142: 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
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Preferred embodiments of a method a
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Fig.6 is a cross-sectional view of
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tapped hole in the cylinder 20 typi
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A second embodiment of a valve actu
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otates faster, the other end 98 of
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In normal operation (as seen in Fig
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Eber Van Valkinburg Patent US 3,744
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Referring to the drawings in detail
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Since the pump depends for its supp
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Briefly, in one aspect the engine o
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Fig.12 is a cross-sectional view si
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Fig.14 is a schematic diagram of an
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A - 1163
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A - 1165
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Figs.20A-20F are schematic diagrams
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Note: Corresponding reference chara
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Integral with the piston bodies are
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The piston has a generally semi-tor
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Referring back to Fig.13A, for engi
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As piston 39A reaches BDC, distribu
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mixture and do not combine because
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These wires are about twelve gauge,
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cold-cathode tube 391, and an x-ray
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Fig.17D), polariser 289, branch B17
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Robert Britt US Patent 3,977,191 31
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Fig.3 is an elevational view of the
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Fig.7 is an electrical schematic of
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Referring now to Fig.3 of the drawi
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and drives Q1 into conduction. The
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Floyd Sweet Recently, some addition
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The day when we witnessed the VTA d
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up to see Floyd. Floyd was with the
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Energy cannot enter a space of zero
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electromagnetic and gravitational f
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or in another form: So, the e.m.f.
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Example 2: Suppose the conductor wi
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Meguer Kalfaian There is a patent a
Page 391 and 392:
Fig.2 illustrates a controlled top
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Fig.9 is a modification of Fig.6; a
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the outer periphery of the magnet,
Page 397 and 398:
wobbling top is sufficient, as proo
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Theodore Annis & Patrick Eberly US
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BRIEF DESCRIPTION OF THE DRAWINGS F
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Fig.6 is a schematic diagram of a s
Page 405 and 406:
DETAILED DESCRIPTION OF THE PREFERR
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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,
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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
Page 421 and 422:
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
Page 431 and 432:
Scientific Papers The following lin
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