hyde


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William HYDE   
OU Electrostatic Generator



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The
Hyde Generator notably converts high-V / low-A ES energy to
low-V / high-A DC -- and it allegedly is an over-unity device :
a free energy generator, according to Moray B. King, who
investigated it :  

<http://rimstar.org/sdenergy/hyde_generator/index.htm>
--- "It's documented fairly well in US patent 4897592
- Electrostatic energy field power generating system. From
private correspondance between William Hyde and Moray B. King
(1), a prototype from 1987 that contained around 2000
capacitors and diodes produced the following results: No.
rotor segments = 240 // No. stator segments  = 480 //
Rotor speed = 6000 rpm // Output voltage = 602 VDC // Output
current = 38 amps // Output power = 22.9 kW // Input power =
2.4 kW // Net output power (while free running) = 20.5 kW
...

---

  

US Patent # 4,897,592   
  
Electrostatic Energy Field Power Generating System   
  
William HYDE

  
January 30, 1990

1685 Whitney, Idaho Falls, ID 83402

Abstract
-- Externally charged electrodes of an electrostatic
generator induce charges of opposite polarity on segments of a
pair of confronting stators by means of electric fields within
which a pair of rotors are confined during rotation to vary the
charge binding field linkages between confronting rotors and
stators by a shielding action of the rotors in a plane
perpendicular to the field flux. A high electric potential
difference induced between the stators resulting from such
rotation of the rotors, is transformed by an output circuit into a
reduced DC voltage applied to a load with a correspondingly
increase current conducted therethrough.  

Current U.S. Class: 322/2A; 310/309   
Intern'l Class:  H02N 001/08   
References Cited [Referenced By]

U.S. Patent Documents   
2522106 -- Sep., 1950 Felici 310/309.   
3013201 -- Dec., 1961 Goldie 322/2.   
4127804 -- Nov., 1973 Breaux 322/2.   
4151409 -- Apr., 1979 O'Hare 250/212.   
4595852 -- Jun., 1986 Gundlach 310/309.   
4622510 -- Nov., 1986 Cap 322/2.

Description

BACKGROUND OF THE
INVENTION

This invention relates to the
generation of electrical power by conversion of energy from an
electrostatic field.

The conversion of energy from a static
electric field into useful electrical energy by means of an
electrostatic generator is already well known in the art as
exemplified by the disclosures in U.S. Pat. Nos. 2,522,106,
3,013,201, 4,127,804, 4,151,409 and 4,595,852. Generally, the
energy conversion process associated with such prior art
electrostatic generators involves the input of mechanical energy
to separate charges so that a considerable portion of the output
is derived from the conversion of mechanical energy.

It is therefore an important object of
the present invention to provide an electrostatic generator in
which electrical power is derived from the energy of static
electric fields with a minimized input of mechanical power.

SUMMARY OF THE
INVENTION

In accordance with the present
invention, static electric fields are established between
electrodes externally maintained at charge levels of opposite
polarity and a pair of internal stator discs having segmental
surfaces that are dielectrically spaced to confine thereon charges
induced by the electric fields. A pair of rotor discs are rotated
within continuous electric fields in planes perpendicular to the
field flux to locationally vary the charge linkage established by
the electric fields between the electrodes and stator discs. Such
changes in charge linkage are effected by rotation of electrically
conductive segments of the rotor angularly spaced from each other
to partially shield the stator discs from the electric fields. The
segments of each rotor disc have charged faces confronting the
electrodes in its field to shield the stator disc over a total
face area that is one-half the total area of the confronting
segment surfaces on the stator disc to which the induced charges
are confined. Charges on the rotors and stators are equalized by
electrical interconnections established through the rotor shafts.
The stator discs are electrically interconnected with an
electrical load through an output circuit transforming a high
potential between the stator discs into a reduced dc voltage to
conduct a correspondingly multiplied current through the load.

BRIEF DESCRIPTION
OF DRAWING FIGURES

These and other objects and features
of the present invention will become apparent from the following
description taken in conjunction with the preferred embodiments
thereof with reference to the accompanying drawings in which like
parts or elements are denoted by like reference numerals
throughout the several views of the drawings and wherein:

FIG.
1 is a simplified electrical circuit diagram
corresponding to the energy conversion system of the present
invention.

![](fig1.gif)

FIG.
2 is a side section view of an electrostatic generator
embodying the system of FIG. 1 in accordance with one embodiment
of the invention.

![](fig2.gif)

FIGS.
3 and 4 are partial section views taken substantially
through planes indicated by section lines 3--3 and 4--4 in FIG. 2.

![](fig34.gif)

FIGS.
5A and 5B are schematic partial laid out top views of the
electrostatic generator of FIGS. 2-4, under static and dynamic
charge distribution condictions, respectively.

![](fig5a.gif)   ![](fig5b.gif)

FIG.
6 is an electrical circuit diagram of the output circuit
of the generator shown in FIG. 2, in accordance with one
embodiment.

![](fig6.gif)

DETAILED
DESCRIPTION OF PREFERRED EMBODIMENT

Referring now to the drawings in
detail, FIG. 1 diagrammatically depicts the energy conversion
system of the present invention generally referred to by reference
numeral 10. As diagrammed in FIG. 1, the system includes a pair of
electrostatic fields 12 and 14 established by electrostatic
charges of opposite polarity applied to electrode plates 16 and 18
from some external energy source. Thus, the electrostatic field 12
is established between electrode 16 and a stator disc 20 while the
electrostatic field 14 is established between electrode 18 and a
stator disc 22. In accordance with the present invention,
electrostatic charge linkages established by the flux of the
fields between the electrodes and stators are periodically varied
by displacement within continuous energy fields 12 and 14 in
response to rotation of rotors 24 and 26 aligned with planes
perpendicular to their common rotational axis and the field flux
as will be hereinafter described. The rotors are mechanically
interconnected with an electric motor 28, as diagrammatically
illustrated in FIG. 1, for rotation about the common rotational
axis. Electrical energy may be extracted from the electric fields
12 and 14 during rotation of the rotors 24 and 26 by motor 28
through an output circuit generally referred to by reference
numeral 30. The output circuit 30 as shown, in FIG. 1 in a
simplified fashion, includes two pair of current conducting diodes
32A, 32B and 34A, 34B. The diodes of each pair are oppositely
poled and each pair is connected in parallel to one of the stators
20 and 22. The diodes of each pair are also electrically connected
across an electrical load represented by resistors 36A and 36B
with capacitor networks 38A and 38B interconnected between each
pair of diodes by means of which the voltage potential between the
stators 20 and 22 is reduced in favor of an increased current
through the electrical load.

Referring now to FIGS. 2, 3 and 4 in
particular, a physical embodiment of the energy conversion system
diagrammed in FIG. 1 is shown. The electrodes 16 and 18 are in the
form of circular plates or discs made of an electrically
conductive metal having external surfaces 40 and 42 adapted to be
charged from the external source as aforementioned. The internal
surface 44 of electrode 18 is thereby adapted to maintain a
positive charge opposite in polarity to the negative charge of the
electrode 16 which is maintained in a stable ion form within a
dielectric surface portion 46 of the electrode 16. The energy
conversion system may be enclosed within an outer housing 48 to
which the electrodes 16 and 18 are secured.

With continued reference to FIG. 2,
the stators 20 and 22 mounted by housing 48 in axially fixed
spaced relation to the electrodes 16 and 18 are provided with
bearings 50 and 52 establishing the aforementioned common
rotational rotor axis journaling a powered shaft assembly having
electrically conductive shaft sections 54 and 56 to which the
rotors 24 and 26 are respectively connected. In the embodiment
illustrated in FIG. 2, the drive motor 28 is mechanically
interconnected with the shaft sections 54 and 56 through an
electrically nonconductive shaft section 58 of the power shaft
assembly for simultaneous rotation of both rotors 24 and 26 at the
same speed and in the same direction about the common rotational
axis perpendicular to parallel spaced planes with which the
electrode and stator discs are aligned. The electrically
conductive shaft sections 54 and 56 are respectively keyed or
secured in any suitable fashion to hub portions 60 and 62 of the
rotors and are provided with flange portions 64 and 66 forming
electrical wipers in contact with confronting surfaces of the
stators 20 and 22, which are inductively charged by the static
electric fields 12 and 14 to equal levels of opposite polarity.

As more clearly seen in FIGS. 2 and 3,
the rotor 24 has a plurality of angularly spaced, field linkage
controlling segments 68 projecting radially outwardly from the hub
portion 60. Each rotor segment 68 is made of an electrically
conductive metal having a face 70 on one axial side confronting
the adjacent electrode 16. The faces 70 confronting the electrode
16 are charged positively by the electric field 12 extending
between the dielectric surface portion 46 of electrode 16 and the
stator disc 20. While the electric field 12 projects through the
spaces 72 between the rotor segments 68, the rotor segments 68
themselves shield portions of the stator disc 20 from the electric
field.

The rotor 26 is similarly formed with
rotor segments 74 angularly spaced from each other by spaces 76
through which the electric field 14 extends between the positively
charged surface 44 of electrode 18 and the stator 22. The rotor
segments 74 of rotor 26 as shown in FIG. 2, are provided with
dielectric surface portions 78 confronting the internally charged
surface 44 of electrode 18. While the rotor segments 74 are
negatively charged by the electric field 14 within the surface
portions 78, they also shield portions of the stator disc 22 from
the electric field as in the case of the rotor segments 68
hereinbefore described. The internal dielectric surface portion 46
of electrode 16 and dielectric surface portions 78 of rotor 26 act
as a stabilizer to prevent eddy currents and leakage of negative
charge. Further, in view of the electrical connections established
between the rotors and the stator discs, the charge on each stator
is equalized with that of the charge on its associated rotor.

As shown in FIGS. 2 and 4, the stator
disc 20 includes a plurality of segments 82 to which charges are
confined, closely spaced from each other by dielectric spacers 80.
The segments 82 are electrically interconnected with the rotor
segments 68 through rotor shaft section 54. Similarly, the
segments 84 of the stator 22 are electrically interconnected with
the rotor segments 74 through rotor shaft section 56. The stator
segments 82 and 84 are therefore also made of electrically
conductive metal. Each of the segments 82 of stator 20 is
electrically interconnected through the output circuit 30 with
each of the segments 84 of the stator. The stator discs being
fixedly mounted within the housing 48, centrally mount the
bearings 50 and 52 through which the electrically nonconductive
motor shaft section 58 is journaled as shown in the embodiment of
the invention illustrated in FIG. 2. Further, the total area of
the charged segment surfaces on each of the stator discs is
greater than the total area of the faces 70 or 78 on the segments
of each associated rotor disc 24 or 26. According to one
embodiment, the total charged stator surface area is twice that of
the rotor face area.

According to the embodiment of the
invention illustrated in FIG. 6, the output circuit 30 includes
the two oppositely poled capacitive circuit networks 38A and 38B
connected across each aligned pair of stator segments 82 and 84 on
the stators 20 and 22 by means of the oppositely poled diodes 32A
and 34A. Each of such capacitive circuit networks includes a
capacitor 86, the opposite sides of which are connected by
oppositely poled diodes 88 and 90 to positive and negative load
terminals 92 and 94 across which a suitable electrical voltage is
established for operating an electrical load. The diode 88 is
connected to the junction 102 between diode 104 and one side of
capacitor 106. The diode 88 is also connected to the junction
between one side of capacitor 100 and the diode 32A. The diode 90,
on the other hand, is interconnected with the junction 96 between
diode 108 and capacitor 100. Also, diode 90 is connected to the
junction between the other side of capacitor 106 and the diode
34A. The foregoing circuit arrangement of capacitive network 38A
is the same as that of network 38B by means of which aligned pairs
of the stator segments 82 and 84 have the electrical potentials
therebetween transformed into a lower voltage across the load
terminals 92 and 94 to conduct a higher load current.

FIG. 5A illustrates the distribution
of charges established in the electric fields 12 and 14 between
the electrodes and stators under static conditions in which each
of the rotor segments 68 and 74 is positioned in alignment with
one of the stator segments 82 and 84 to thereby shield alternate
stator segments from the electric fields. The charges established
by the electric fields are therefore confined to the faces of
alternate stator segments confronting the electrodes and are
equalized with the charges established on and confined to the
shielding faces of the rotor segments confronting the electrodes
by virtue of the electrical interconnection between the rotors and
stators as aforementioned. As depicted in FIG. 5B, when rotation
is imparted to the rotors, the charge linkages established by the
electric fields between the electrodes and alternate stator
segments 82 or 84 are interrupted by the moving rotor segments 68
or 74 so that previously sielded stator segments become exposed to
the fields to reestablish field energy linkages with the
associated electrodes. Such action causes electrical potentials to
be established between the stator segments 82 and 84.

It will be apparent from the foregoing
description that the electrostatic energy fields 12 and 14 of
opposite polarity are established maintained between the
externally charged electrodes 16 and 18 and the internally charged
stators 20 and 22 under static conditions as depicted in FIG. 5A.
During rotation, the rotors 24 and 26 continuously disposed within
such energy fields 12 and 14, exert forces in directions
perpendicular to the field flux representing the energy linkages
between electrodes and stators to cause interruptions and
reestablishment of energy linkages with portions of different
stator segments as depicted in FIG. 5B. Such energy linkage
locational changes and the charge binding and unbinding actions
between electrodes and stators creates an electrical potential and
current to flow between stators through the output circuit 30.
Thus, the output circuit when loaded extracts energy from the
electric fields 12 and 14 as a result of the field linkage charge
bindinbg and unbinding actions induced by rotation of the rotors.
The stator segments 82 and 84 shielded from the electric fields by
the moving rotor segments 68 and 74 as depicted in FIG. 5B, have
electric potentials of polarity opposite to those of the external
electrodes 16 and 18 because of the field linkage charge unbinding
action. Previously shielded stator segments being exposed to the
electric fields by the moving rotor segments, have the same
electric potential polarity as those of the external electrodes
because of field linkage binding action. Since the forces exerted
on the respective rotors by the electric fields 12 and 14 of
opposite polarity act on the common rotor shaft assembly
perpendicular to said fields, such forces cancel each other. The
energy input to the system may therefore be substantially limited
to mechanical bearing losses and windage during conversion of
electrostatic field energy to electrical energy as well as
electrical resistance losses and other electrical losses
encountered in the output circuit 30.

Based upon the foregoing operational
characteristics, rotation of the rotors in accordance with the
present invention does not perform any substantial work against
the external electric fields 12 and 14 since there is no net
change in capacitance thereby enabling the system to convert
energy with a reduced input of mechanical energy and high
efficiency, as evidenced by minimal loss of charge on the
electrodes. It was therefore found that working embodiments of the
present invention require less than ten percent of the electrical
output energy for the mechanical input. Further, according to one
prototype model of the invention, a relatively high output voltage
of 300,000 volts was obtained across the stators. By reason of
such high voltage, an output circuit 30 having a voltage reducing
and current multiplying attribute as hereinbefore described was
selected so as to render the system suitable for many practical
applications.

The foregoing is considered as
illustrative only of the principles of the invention. Further
since numerous modifications and changes will readily occur to
those skilled in the art, it is not desired to limit the invention
to the exact construction and operation shown and described, and,
accordingly, all suitable modifications and equivalents may be
resorted to, falling within the scope of the invention.

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<http://rimstar.org/sdenergy/hyde_generator/index.htm>  
  

Hyde
Generator Replication

  
The Hyde generator is a device developed by William W. Hyde that
puts out more energy than is used to run it (to me this means it
must tap into some unexpected energy source.) It's basically a
large high voltage capacitor with spinning rotor segments actually
in between the capacitor plates, chopping the electric field at
high speed (> 6000 RPM.) Stator segments are also in between
the capacitor plates and it is actually the electric field between
the stator segments and the capacitor plates that is chopped. The
resulting output energy is taken off of the stator plates using
capacitor/diode networks.  
  
It's documented fairly well in US patent 4897592 - Electrostatic
energy field power generating system. From private correspondance
between William Hyde and Moray B. King (1), a prototype from 1987
that contained around 2000 capacitors and diodes produced the
following results:  
  
No. rotor segments    240  
No. stator segments    480  
Rotor speed    6000 rpm  
Output voltage    602 VDC  
Output current    38 amps  
Output power    22.9 kW  
Input power    2.4
kW  
Net output power (while free
running)    20.5 kW  
  
My 1st replication attempt  
  
My 1st attempt was with a vacuum cleaner motor at one end and an
18" long shaft with everything attached. The long shaft made it
too unstable at high speed. The best I could safely do was around
2700 RPM.   
  
My 2nd replication attempt  
  
I first finished all parts for my 2nd attempt, assembled it and
ran it for the first time on April 7, 2009. By April 23, 2009 I'd
found I was unable to get the motor to spin the disks faster than
4000 RPM. The motor is rated at 10,000 RPM no-load and can do that
with featureless disks but can do only 4000 RPM with the completed
disks. My guess is the disks with their radially cut slots and
metal segments attached act like fans and the air load is too
high.   
  
The construction details are below, following these updates.  
  
May 1, 2009 - Lowered air pressure to decrease load  
  
At the suggestion of Paul on overunity.com I sealed the box and
lowered the pressure with a household vacuum cleaner motor. I
managed to drop the pressure by about 0.5 PSI ( around 1 inch Hg).
I didn't see any improvement in RPM, the best being around 3900
RPM, so I would have to drop the air pressure even more. The outer
acrylic window was seriously bowed inward so I don't think I'd
want to do further improved sealing without replacing the window
with a solid board. I'd also be afraid of going further out of
fear of damaging my vacuum cleaner. It was worth a try though.   
  
May 5, 2009 - Sealed edges with packing tape - 4500 RPM!  
  
I guessed that maybe if I sealed the area where each rotor is,
once the air gets moving, since it's enclosed in a circular
pathway, it will keep most of its momentum and act like less of a
load and I'd be picking up less new dead air. Plus, in the patent
the rotors are sealed in a circular housing in the same manner. I
got 4500 RPM, an encouraging improvement. I used clear packing
tape so I wonder if I used something less crinkly if it would be
even better. Still no HV spikes, but Hyde didn't get those until
around 6000 RPM  
  
May 19, 2009 - Higher input voltage, sealed rest of housing, and a
bang! - 5200 RPM!  
  
At Luc's suggestion I decided to run it with higher than the
motor's rated input voltage of 110VAC, something I was previously
reluctant to do but as Luc said "I was so close to the 6000 RPM".
Luc pointed out to me how to get 2 phases out of my wall sockets
to get up to 220VAC and even more using variacs (which I didn't
realize variacs would do), but for starters I tried it with just
one variac at its maximum output of 130VAC. I got 4660 RPM! My
previous best at 4500 RPM at 110VAC so it looks like I'd get
around 80 RPM for each 10VAC I add; not much.  
  
Then I decided that since I had big success on May 5 (reported
above) with sealing just the area where the rotors were and since
at 4660 RPM it was screaming like a banshee from the air coming
out of the holes in the wooden box, I should seal the area where
the motor was too, just as is done in the patent. Success, I got
5200 RPM! Only 800 RPM to go.   
  
Here are some scope shots. The AC is expected and normal. It's HV
spikes that I'm after but at no speed or voltage did I see any.
The 757 Hz from the scope shot below is per segment, not per
rotation of the entire rotor. There are 9 segments per rotor so to
get RPM take the 757 Hz and divide by 9 to get rotations per
second for the whole rotor. Then multiply by 60 to get rotations
per minute (RPM), 5046 RPM. However, I did get 5200 RPM at one
point, just no photo of the scope at the time. The voltage was set
to 3kV when it was at 5200 RPM, the same voltage Hyde was using
when he was doing 2 kW in and getting 20 kW out.  
  
And then there was a muffled bang and the whole box began to
slowly slide across the floor. One of the segments had come off a
rotor (the bang) and this unbalanced the whole thing (the slow
sliding.) The only damage was a hole in the packing tape where the
segment flew out from between the rotor/stator area and the
mangled segment from when it hit the inside of the box in an
awkward area which caused it to bounce around.  
  
Disks --  
![](1-hyde-disk.JPG)  
  
Hubs --   
![](1-hyde-hubs.JPG)  
  
Assemblage --  
![](1-hydewobands.JPG)  
  
With rubber bands --  
![](1-hyde-bands.JPG)  
  
Closeup --  
![](1-hyde-closeup.jpg)  
  
Sealed Unit --  
![](1-hyde-sealed.jpg)  
  


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<http://www.sae.org/technical/papers/929472>  
  

An
Enhanced Quad-Disc Electrostatic Generator

  
Document Number: 929472  
Date Published: August 1992  
Author(s): Donald A. Kelly -
Space Energy Association  
  
Abstract : The
conventional twin-disc wimshurst type of electrostatic generator
has considerably increased potential as a high voltage output
sources when two additional stator discs are utilized on each side
of the usual twin, counterrotating rotor discs. The emergence of
the hyde type of electrostatic generator has spurred some interest
in high voltage elect rostatic generators of this general type,
but unfortunately the hyde E/S technology is not practical, and
has a number of technical errors in it which make it unworkable.
In the quad-disc electrostatic the basic principles of the
wimshurst twin counterrotating E/S discs are preserved, and in
addition a twin rotor-to-stator E/S generating factor is included
in this composite quad-disc electrostatic generator. The twin,
counterrotating rotor discs form the basic E/S components, and
have both the non-contacting neutralizing brushes, and the
non-contacting collector brushes. The positive and negative
satator discs on each side of each rotor disc receive E/S transfer
from the multiple conductive segments on the outer sides of each
rotor disc. The normal E/S transfer occurs from the segments on
the inner surfaces of each of the rotor discs. The number of
conductive segments of each of the rotor and stator discs will
range from a low of 30 segments, to a maximum of 60 segments,
depending on the disc diameter and the voltage/amperage balance
per segment. The voltage and current amplification function for
the enhanced quad-disc E/S generator will be accomplished by twin,
large capacitive transformers, similar to those used in the
present Swiss M-L converter.  
  
The key components within these twin large captive transformers
are the twin, large bi-filar wound coils over ferrite magnet
stacks which transduce space energy into these polarized
components. The wattage amplification factor is not generally
recognized in present applied physics, but since the phenomena
occurs in four F/E projects, past and present, it is an
accomplished fact in advanced physics today! The enhanced quad-
disc electrostatic generator design holds considerable promise for
providing a useful high-voltage-to-normal wattage power source, as
the concept is further evolved and developed.   
  


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[http://www.icestuff.com/~energy21/notes.htm](http://www.icestuff.com/%7Eenergy21/notes.htm)  
  
Excerpts --  
  

Back-Engineered Methernitha  Notes

  

by
John
BEDINI

  
Note 23  Some other
generators with similarities to the Testatika machine are the
"Electrostatic Energy Field Power Generating System" invented by
William W. Hyde (US Patent 4897592 of Jan 30 1990) is a
rotor/stator variable capacitance machine capable of producing 300
KV... [ &c. ]  
  
Note 1  For more
information on the Pidgeon machine see "Electrical Influence
Machines" by John Gray 1903 pp206 & "Philosophical Magazine"
Dec 1898 pp564, and of course the Pidgeon patents.  
  
Note 2  See "Modern High
Speed Influence Machines" by V.E.Johnson 1921 pp76. Johnson was
not only a researcher of electrostatic machines but was also an
innovative constructor of them, and as such was keen to try any
technique that made his generators more powerful than even the
specialised Wommelsdorf multi-disc condenser machines. This book
is an absolute must for those who wish to work in this field.  
  
Note 3  See
"Self-Excited, Alternating, High-Voltage Generation Using A
Modified Electrostatic Influence Machine" by M.Zahn et al,
American Journal of Physics Vol 42 (1974) pp289.  
  
Note 4  The Methernitha
designers have taken a basic Pidgeon electric field system and
added a few modifications of their own, partly to lock a certain
polarity of charge to a certain area so as to stabilise it, and
also to boost certain areas with charge... [ &c ]   
  
Note 7  See US Patent
1,540,998 (9 June 1925) Conversion of Atmospheric Electric Energy
by Hermann Plauson. He also wrote a book of the subject titled
"Gewinnung und Verwertung der Atmospharischen Elektrizitat" in
1920 in German.  
  
Note 11  The phenomenon
of electrostatic motors has been well researched over the years
(see "Electrostatic Motors" O.Jefimenko in "Physics Teacher" Vol 9
March 1971 p121-9, and in "Electrostatics  And Its Applications"
by A.D.Moore (1973) p131-147; "Electrostatic Motors" by B.Bollee
in "Philips Tech. Review" Vol 30 1969 p178-194)... [ &. ]  
  
Note 12  J.G.Trump
worked for the US Air Force and pioneered some highly efficient
electrostatic machines around the 1960s (see"Electrostatic
Sources of Electric Power" in "Elec. Eng" 66:525 June 1947; and
"High Voltage Generation in Space:The Parametric Electrostatic
Machine" in "Progr. Astronaut. Rocketry" (vol 3  Energy
Conversion for Space Power) 1961 p745).  
  
Note 14  See "Plasma 
The Fourth State of Matter" by D.A. Frank-Kamenetskii (1972) pp10,
and Dr.Patrick Flanagans US patents 4,743,275(May 10 1988) and
4,391,773(Jul 5 1983).  
  
Note 21  US patents
3,323,069 (May 30 1967) and 3,187,208 (June 1 1965). This system
by Van de Graaff may be a little too complicated for the
Methernitha, but, nevertheless, may be of some interest.  
  
Note 22  Dr. Flanagan
modified his insulator blocks, made of resin, by doping them with
paramagnetic granules (such as silicon carbide) to enhance even
more the electron cascade effect; which is an idea that the
physicist Thomas Townsend Brown first experimented with (by using
lead oxide granules) in his US patent 3,187,206 (June 1 1965) to
good effect.  
  
Note 23  Some other
generators with similarities to the Testatika machine are the
"Electrostatic Energy Field Power Generating System" invented by
William W. Hyde (US Patent 4897592 of Jan 30 1990) is a
rotor/stator variable capacitance machine capable of producing 300
KV. Other such generators are; "Parametric Electric Machine"
invented by Ferdinand Cap (US Patent 4622510 of Nov 11 1986) which
has a series resonant (LCR) circuit structured into it so that it
oscillates - and indeed operates AT RESONANCE to ensure a high
output; "Electrostatic Generator" invented by Dan B. Le May (et
al) (US Patent 3094653 of Jun 18 1963) is a very ingenious system
of variable capacitance; the "Electrostatic Machine" by Noel
Felici (US Patent 2522106 of Sep 12 1950) is a good standard which
utilizes a valve rectifier; and the "Electrostatic Generator" by
William S. Spencer (US Patent 1415779 of May 9 1922) is an early
rotor/stator generator which transferred its electric impulses
through a transformer to produce a higher current output.  
  


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