A Practical Guide to 'Free-Energy' Devices

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the central vortex chamber 12g by opening the hinged longitudinal louvers 61a which are mounted between the baffles in the openings defining chambers 12a and 12b. The remaining louvers remain closed, preventing the wind from exiting through the sides of the device. Thus, the wind-activated louvers are, in effect, one-way valves allowing the wind to flow into the central vortex chamber through the sides of the device, but only allowing the wind to exit through the top of the chamber, and through the turbine 22. Referring again to Fig.10, it can be seen that the longitudinal louvers 61a mounted in the upstream chamber 12 are hinged on the opposite side from the louvers 61b mounted in the downstream chamber 13. This is because the vortex in the downstream chamber rotates in the opposite direction from the vortex in the upstream chamber, and the downstream toroidal baffles 14b funnel the wind into the louvers 61b in the opposite direction. Like the louvers 61a in the upstream chamber 12, the louvers 61b in the downstream chamber 13 act as one-way valves allowing the wind to flow into the central vortex chamber through the sides of the device, but only allowing the wind to exit through the top of the chamber, and out of the device. This configuration helps to maintain the strength of both the upstream and the downstream vortices during operation of the device. It should be recognized that some degree of improved energy-conversion performance may be obtained in a configuration in which there are toroidal baffles 14a and hinged louvers 61a only in the upstream annular chamber 12 because this ensures that all of the wind or other fluid entering the sides of the upstream chamber flows through the turbine. The addition of toroidal baffles 14b in the downstream annular chamber 13 provides additional improved performance, particularly when the direction of rotation of the downstream vortex is opposite the direction of the upstream vortex. Optimum energy-conversion performance is provided by a device having oppositely configured toroidal baffles 14a and 14b, and oppositely hinged louvers 61a and 61b, for both the upstream annular chamber 12 and the downstream annular chamber 13. It is to be understood that even though numerous characteristics and advantages of the present invention have been set forth in the foregoing description, the disclosure is illustrative only, and changes may be made in detail, especially in matters of size, shape, and arrangement of parts within the principles of the invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed. Claims: What is claimed is: 1. A fluid-powered energy conversion device for converting energy in a moving fluid into mechanical energy, said device comprising: a rigid cylindrical frame having an upstream annular chamber and a downstream annular chamber, each of said chambers having sides that are open to allow entry of the moving fluid; a first set of baffles A - 1248
longitudinally mounted in the upstream chamber that operate to create in the upstream chamber, an upstream drive vortex rotating in a first direction when the moving fluid enters the upstream chamber through the upstream chamber's open sides and through openings between the baffles; a first set of hinged louvers positioned in the openings between the first set of baffles and encircling an upstream central vortex chamber cantered around a central longitudinal axis of the device, said first set of louvers being operable to permit entry of the moving fluid into the upstream central vortex chamber only when the fluid is rotating in the first direction, and to prevent the fluid from exiting the upstream central vortex chamber through the sides of the device; a floor of the upstream annular chamber that slopes toward the downstream chamber as the floor approaches the central longitudinal axis of the device, said floor causing the drive vortex to flow downstream through the upstream central vortex chamber and pass through a central aperture located between the upstream annular chamber and the downstream annular chamber; a longitudinal drive shaft centrally mounted in the central aperture; and a turbine mounted on the drive shaft in the central aperture, said turbine being rotated by the drive vortex as the drive vortex passes through the central aperture. 2. The fluid-powered energy conversion device of claim 1 further comprising a second set of baffles longitudinally mounted in the downstream chamber that operate to create in the downstream chamber, a downstream extraction vortex rotating in a direction opposite to the first direction when the moving fluid enters the downstream chamber through the downstream chamber's open sides and through openings between the baffles, whereby the turbine is rotated by the drive vortex as the drive vortex passes through the turbine and reverses direction to match the direction of the extraction vortex. 3. The fluid-powered energy conversion device of claim 2 further comprising an annular central divider between the upstream chamber and the downstream chamber, said divider having a downstream surface that slopes downstream as it approaches the central longitudinal axis of the device, said downstream surface causing the extraction vortex to flow downstream, thereby creating an area of reduced fluid pressure downstream of the turbine. 4. The fluid-powered energy conversion device of claim 2 further comprising a second set of hinged louvers positioned in the openings between the second set of baffles and encircling a downstream central vortex chamber cantered around the central longitudinal axis of the device, said second set of louvers being operable to permit entry of the moving fluid into the downstream central vortex chamber only when the fluid is rotating in the direction opposite to the first direction, and to prevent the fluid from exiting the downstream central vortex chamber through the sides of the device. 5. The fluid-powered energy conversion device of claim 4 wherein said first set of baffles are curved to form a toroidal pattern in the first direction, and said second set of baffles are curved to form a toroidal pattern in the direction opposite to the first direction. 6. The fluid-powered energy conversion device of claim 5 wherein said turbine comprises a set of rotating blades, each of said blades having a cross-sectional shape of a curved airfoil that generates a lift force, said lift force being directed in the direction of rotation of the turbine. 7. The fluid-powered energy conversion device of claim 1 further comprising a flywheel mounted on the drive shaft, said flywheel having sufficient mass to operate as an internal energy storage device due to its angular momentum. 8. The fluid-powered energy conversion device of claim 7 wherein said flywheel is a permanent magnet. 9. The fluid-powered energy conversion device of claim 7 wherein said flywheel is a fluid-filled flywheel that rotates with the drive shaft in a direction of rotation, said fluid-filled flywheel comprising: a hollow disk-shaped shell filled with fluid; and a set of radial bulkheads that separate the interior of the shell into separate sections, each of said bulkheads having at least one gate pivotally mounted thereon to open in a direction opposite to the direction of rotation, said gate covering an aperture in the bulkhead when the gate is pivoted to a closed position, and said gate opening the aperture when the gate is pivoted to an open position; whereby the gates are opened by the fluid when the flywheel accelerates in the direction of rotation, thus allowing the fluid to flow through the apertures in the bulkheads and reduce start-up inertia of the flywheel, and whereby the gates are closed by the fluid when the flywheel decelerates, thus preventing the fluid from flowing through the apertures, and causing the flywheel to maintain angular momentum like a solid flywheel. 10. The fluid-powered energy conversion device of claim 9 wherein the hollow disk-shaped shell includes: an annular compartment filled with the fluid; and a cooling fan mounted in a central hub section of the shell. 11. The fluid-powered energy conversion device of claim 1 further comprising an electrical generator mounted on the drive shaft, said generator converting mechanical energy from the rotation of the shaft into electrical energy. A - 1249
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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 - 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
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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
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
Page 415 and 416: FIG.3 is a side elevational view of
Page 417 and 418: FIG.9 is a horizontal cross-section
Page 419 and 420: otational downstream annular chambe
Page 421 and 422: In Fig.5 is shown a perspective vie
Page 423 and 424: small hydro-electric version of the
Page 425: Fig.10 is a perspective view of a s
Page 429 and 430: shaft in the central aperture, said
Page 431 and 432: Scientific Papers The following lin
Page 433 and 434: http://www.free-energy-info.co.uk/M
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