Through out the world others are also building
Implosion Motors in search of mother earths greatest secret. This secret
still eludes the greatest of minds. These pictures provided by a
co heart in Europe who saw this one first hand.
EDAV PROJECT PART 6 is a continuing progress in search of this
The Implosion Motor is simply a device that acts as an air
expander/compressor all at the same time. I have studied this last year gas
turbine technology and find many similarities between the engines. My
research also has let me more into the research of compressed air technology
and the answers I find by associating the two
technologies become very interesting. Thanks to a welcomed investor this
last year the “Air Engine Generator Project” took shape and many
tests were able to be performed to prove these theories. These tests were
important, for the understanding and inclusion of heat into a compressed air
stream showed a substantial increase in volume with very little loss’s.
These same scientific circumstances are seen in the Implosion motor.
Therefore under the laws of Charles and Boyles an increase in the power
potential can be obtained from this thru a natural form of heat that really
costs nothing to get to. So you wonder why this is relevant to this project.
Heat is a vital part to the working of any engine. Due to the rotational
compression factor inside the wave plate, the potential for heat can rise to
500 degrees. As the rotation velocity increases the compression factor
rises therefore increasing the heat and volume and the more kinetic thrust
is jetted This becomes a power potential that actually acts in the wrong
direction of known physical laws. A rotational velocity that can increase by
itself without any input of outside energy. Our current understanding
stipulating that frictional loss’s always will
subdue any gains in power therefore decreasing rotation over a period of
Let me put it this way, one pound of air
increases in volume by heat from 12.387 cu ft at 32 degrees to 19.323 cu ft
at 328 degrees which is a 6.939 cu ft increase. An equal amount of increase
in pressure must also happen with the increase in volume. I was working with
dry heated air in the air engine, but if moisture is present to the
point of saturation, the pressures are greatly increased. This is another
reason why water injection is shown in some of the implosion motor
assemblies. In a high rotational device the water molecules also help pack
the air molecules at the peripheral helping to cause the implosive results
to emerge. But higher rpm must be used.
air at 30 degrees be taken as unity (1.0), dry air at 212 degrees will
occupy a volume of 1.675, and saturated air at the same temperature 2.672 or
double. If the implosion plates can reach double that temperature simply
using a natural heat process, then the effect gets even greater with no
outside energy input. So in reality the faster it goes the hotter it gets
the more pressure it can induce and that pressure turned into kinetic energy
creates a much faster spin rate. (Higher efficiency achieved)
So all this pressure has to be directed some how to
create kinetic spin when being released from the wave plates. This picture
below shows a perfect illustration how this can be accomplished. (See
picture 2a & 2b)
Pictures supplied by an unnamed outside source.
All engines work off the Carnet Cycle and the
implosion motor is not exempt from this as well. But the difference is the
amount of energy being transformed from heat to do work costs very little
for the amount of work energy output that is obtained from it. Taking also
into effect the mass x velocity adds stored kinetic energy into the
rotational velocity as well, the larger size (12”) can have a much higher
torque output for a much less needed air supply. The larger the radius the
more torque output can be generated with a decrease in actual air supply
required to create the rotation. So the efficiency of the engine starts
climbing higher to 96 percent or better.
Victor Schauberger referred to his wave plates as being a form of “Descending
Piston”. I found this several times in the Callum Coats books. This type
of design in this way is able to create an expansion process at the same
time it is compressing. In all the wave forms presented to me so far do not
take this into consideration there fore the effect there out to achieve is
still outside their grasp. The wave forms should carry more of a design as I
show here on page 3. Each wave form carries a different shape as it flattens
out more to the peripheral.
Refer to Picture 3a: Shows the lower wave form with the pressed
Picture 3b : Shows the directional skirt attached.
Picture 3c : Shows the upper wave plate set in place and how the
exiting jet fluid creates the
Picture 3d : Shows the cover attached on the wave plate assembly.
This shows that the bottom wave plate has to rotate on a bearing while the
is in a stationary position. The top cover extends over the directional
skirt in order
to be able to direct the pressure flow downward. The exiting pressure then
upward thrust to the turbine creating a lifting effect.
What I am trying to say here is that the shape of the wave form has to have
a descending cavity in order for the implosion or compressing effect to
happen. As I have written in earlier Chapters verifying this fact.
Here is another couple of pictures of another implosion motor being
experimented with also from Europe. The workmanship on this unit is
extremely good compared to others.
Fuel for thought
Nobody can say that the implosion motor does not run off of any fuel. This
really is a totally bogus statement for it is a known fact that the fuel
source is normal breathable air and water. Using the moisture content helps
pack the air molecules at the peripheral.
But let’s look at another source of potential power. For those of you who
might have a copy of the Callum Coats book “The Energy Evolution”
I am going to refer to page 44
“If specifically heavy high quality water is atomized and the resultant
water vapor is compressed by a Descending Piston with a simultaneous
infusion of atmospheric oxygen, then this aqueous mixture of air is
instantaneously transformed into increased and highly potentiated stocks of
new air. The expansive pressure produced in this way corresponds to the
power of about 2,000 atmospheres per liter of water.” (2000 x 14.7 = 29,400
psi ) (1 Liter = .26 gal.)
First off “Heavy Water” is known as Deuterium
and contains 1 proton, 1 neutron, and 1 electron and is mostly used in the
nuclear industry to help contain nuclear reactors. From what I can find out
the cost of a gallon of heavy water is about $88.00 per gallon. This might
seem a bit much but to produce 117,600 psi of air pressure comes to 1,336.36
psi per dollar. But if that pressure can be used in an implosion motor in a
recirculation effect, the cost just got substantially cheaper. But you can
make heavy water yourself at home at a fraction of the cost. But the big
question here as when it mix’s with pure oxygen which has 8 protons, 11
neutrons, and 8 electrons what causes the nuclear reaction to create this
clean expansion of new stocks of air. It is still not clear to
me yet how this reaction can take place within the high heat compression
state of the wave plate chamber. But I will leave that up to the new
generation of PhD graduates with chemical backgrounds to figure out this
wild equation. This is another true form of kinetic energy achieved thru
expansion and not combustion as we have known for 100 years. So this has to
be proved whether or not Victor Schauberger was correct in this paragraph.
It cost me $20.00 to fill my one scuba tank so that’s 3200 psi so that’s
about 160 psi per dollar spent. So117,600 psi = $735 dollars to fill an
equivalent of 37 scuba tanks with about 94 cu ft of gas per tank cylinder.
My air engine would run thru 18,500 psi in 105 minutes so if injected with
this reaction, I then could run it 6 times longer or almost 10 hours. But if
that was used in a properly built implosion motor that could equate to 100
hours or more depending on how you use the expended air pressure. Adding the
input time of compressed air still being generated into the equation, it
still gets considerable longer maybe up to 16 hours. Compare this to the
cost of fuel to operate a 40 kw generator which can consume 4 gallons of
fuel per hour ($3.00)or $12.00 hour x 16 hours would come to about $200.00
in a 16 hour comparable period. The cost savings is still less.
So what I think is that the implosion motor was not designed to run on just
water and air but was also designed to run on something that looked like
water and this is Deuterium. As we have all read the stories
of how the implosion motor went thru the roof of the hanger that is so well
known in much of others writings, here is the proof that that turbine was
probably fueled with heavy water. Only in this way could have the implosion
turbine been expanded at such a rapid rate that the amount of vertical
thrust have been achieved.
Normal water and air could not achieve such a result. If so prove it to me!
Yes, and let’s not forget this fact also:
Vacuum+Resonant Material+Rotating Copper Disc+ Magnetic Field =
Production of Electrical Energy (electrons.... a huge amount of electrons).
Now I think I have proved that the implosion turbine is not exactly a free
energy device but also an engine designed to run on other fuel sources not
generally established in our line of thinking today. But also the fact that
the running cost of such an engine when compared to a combustion type is by
far less expensive to operate and the exhaust is clean new air for us all to
breath. The simplicity of this design is also far greater in economics and
maintenance costs compared to ICE designs.
Implosion Turbine, An Alternative Space Engine
I want to start addressing the fact that the implosion turbine especially
designed as a closed loop system and fueled by pure oxygen and Deuterium is
capable of upper atmosphere penetration. A small 2 man craft powered by this
sort of energy system would be capable of reaching the space environment
simply because of the power to weight ratio would be well in our favor.
In the earlier writings referring to EDAV Part 4
on page 4, I speak about the SPACEPLANE which was brought to America
from Germany hidden in the belly of a giant submarine U-234. On board of
that submarine were several drums of heavy water. I here now submit this
fact of evidence that these drums were the fuel for the SPACEPLANE. This new
aircraft had the capability of reaching into sub space orbit without the use
of rocket fuel. For this full story again refer to the book
“CRITICAL MASS” by Carter Plymouth Hydrick. (see page 2)
as well as a mysterious “stratosphere plane” apparently an aircraft
that could reach and cruise in the rarefied atmosphere of near space.
We all know that an aircraft of this capability would have to be running on
some sort of rocket fueled technology or a jet engine technology. But this
was a technology that was used as a trade for freedom. As you can see from
the picture I show in EDAV PART 4, that particular aircrafts unknown
existence, since nobody wants to claim its existence must have belonged to
Germany. This plane because of its size and weight was probably running on a
type of implosion turbine with heavy water as its fuel.
I can tell you now it won’t be to much longer that I will prove this
The closer an implosion engine gets to near space the better it will run.
When it reaches the atmosphere of space where it now is running on helium
and hydrogen this mixture of gas’s in a vacuum and high rotational velocity
will create a plasma effect that will continue to drive the workings of the
turbine. If the turbines velocity is operational in a total vacuum then
since there is no gravitational effect or air friction to affect its running
ability the speed of the turbine will increase to such a velocity as to
create a high electrical effect to also take place. The accumulation of
electrons will produce a high current of electrical energy, enough to
produce electro kinetic thrust. This is the choice of energy systems to
power a space vehicle thru space.
It is also a distinct possibility that when Deuterium is run thru the
Waveplates, the one electron could be detached from the atom making this
Deuteron consists of one proton, and one neutron. If the gas from the
implosion motor may be routed into an expansion chamber and mixed with
Helium 3 then the thrust achieved from this expansive mixture is 1000 times
more powerful than a rocket engine
and is not combustion.
I quote this from “Flying Saucers and Science” by Stanton T. Friedman
“ If a Deuteron is reacted with a helium-3 nucleus( two protons and
one neutron), a large amount of energy is released. It comes from converting
a little of the mass to a lot of energy, and all but 2.5 percent of the
energy is in the form of charged particles. These have the enormous
advantage of being able to be directed by electric and magnetic fields, so
they can be emitted out the back end of a rocket, unlike the situation with
the neutrons. The ejected particles have about 10 million times as much
energy per particle as can be obtained in a chemical rocket. “
The problem is where to obtain a quantity of Helium-3 which is a very rare
ingredient indeed. Well the moon surface is loaded with it. In fact it is
about 0.01 ppm in content. In December of 1995 Professor Hiromu Momota of
Japan’s National Institute of Fusion Science stated in a meeting that “there
is enough fuel in the first 10 feet of the moon’s surface to power the earth
for the next 700 years, and that scientists were hoping to send miners to
the moon to excavate the vast store of hel-3” He also said that “using the
moons helium-3 will also make it possible to build machines to power
spacecraft and even generate high energy beams to treat cancer.” The
fact also remains that Jupiter and Saturn have infinite reserves. The U.S.
Air Force has been mining the moon for 35 years for Helium-3. Refer to the
book “Mexico’s Roswell” by Noe Torres & Ruben Uriarte there you will find
the information of a UFO crash in Chihuahua, Mexico August 25, 1974.
This crash between a flying disk and a small aircraft was covered up. The
disk was confiscated from Mexico by the U.S Military under false pretences.
All evidence was destroyed as usual. But the fact remains that this was a
remote control vehicle operated by our military and it was bringing back
moon material to be refined into Helium-3.
Reason being this flying disk only had forward vision and did not see the
other aircraft approaching from a side projectory. If it was being driven by
the hands of ET’S they certainly would have avoided the collision at all
costs because they would have been on board of the saucer an aware of an
approaching aircraft. Nobody was on board that flying disk, so it was
thereby being operated by remote control.
It is a known fact that two individuals in Washington D.C. own all the
mineral rights to the moon. Why would 2 people want all the mineral
rights to the moon if we are not going there or even have the capability to
The moon is being mined by our military and this is my proof.
The moon dust is then refined and the helium-3 extracted to be used to power
other space ship technology like the flying disk in question. That is why
our government is not going to allow any more missions to the moon so this
discovery does not come to light with the American people. This is why
NASA’s funding has been scaled back.
ELECTRIC WING Technology
These electric wings were built by me this last year to understand electro
kinetic thrust. You can also pay a visit to Jnaudins Home page web site
concerning this and learn more about the Lifters and to get a better
understanding about this growing technology.
Electro-kinetic thrust is obtained by using high
voltage energy to propel the wings.
The Lifters Experiments home page by Jean-Louis Naudin
Study the Townsend Brown Effect to learn
more about this. In order to have an aircraft that can fly on this type of
energy first you have to have a suitable power plant capable of an output of
enough electrical energy to create electric thrust. With my new upcoming air
turbine technology the capability of creating ½ m watts of power on board
this small aircraft for about a weight exchange of 500 lbs which is only an
exchange in wing lift area gives me the voltage required to make this
happen. I realize that the schematics supplied with my voltage box HV35 can
be greatly enhanced to produce the required voltage for a full sized
aircraft after review of this with a EE engineer..
NEW HIGH SPEED AIR turbine (Super Heated Re
circulating Air Turbine) SHRAT
In the last recent months I have been designing a New Super Heated Air
turbine. By the time you read this I will be well under way in the
building process. My math computations regarding this SHRAT turbine
has determined that if unity be 1.0 then my turbine is 1.38. Well past the
line that justifies the existence of over-unity. I have had several PhD
scholars already verify the math to prove its validity. The turbine does
encompass a power turbine and exhaust turbine with a built in re compressor,
and custom designed high pressure compressor. If you study gas turbine
technology you will find all above items mentioned involved in creating
thrust. Except I have in the design a new application not see elsewhere.
This will give it a super efficiency that pushes over unity to its outer
IS OVER UNITY
14 cu ft of air required to operate the air engine.
The above chart shows how the cu ft of air used in the
air engine is broken down. As the compressor is compressing 6 cu ft of air
per minute back into the compressed air storage tanks, the engine is only
consuming a smaller amount of air from storage. Another increase in the
volume of air is the input from the Heat Reactors. As the air from the
storage tanks are passing thru these reactors an increase of volume is
realized up to 3 cu ft per minute from 1 cu ft of air. The air going from a
input temperature of 65 degrees to over 350 degrees in just a few seconds.
It appears therefore that in heating a given quantity of dry air to 328
degrees, it will be increased in volume under constant pressure over 50
percent. (Charles & Boyles Law)
(A) 5 cu ft of air from storage.
(B) 6 cu ft of air from the compressor back into storage under constant use.
(C) 3 cu ft of expanded air volume as passed thru the heat reactors.
So the actual amount of air being consumed from storage is 5 cu ft per
Utilizing a 25,000 watt generator has a usable output of 22,000 wts.
Subtracting the 3730 watts required to run the compressor leaves us 18,270
watts. Also minus 700 watts for the heat reactors elements, now leaves us
with 17,570 watts remaining output from generator. This gives us a 20
percent loss for regeneration purposes. If the air engine is using 14 cu ft
of air to operate and is operating on a full cylinder stroke then the air
usage is not efficient. Generally an air cylinder using a full stroke of
compressed air is not required since the stroke only needs ½ that amount to
accomplish the same amount of work. Knowing this then the amount of air the
air engine is consuming can therefore be cut in half from 14 to 7 cu ft. See
basic power stroke chart BELOW.
Power stroke chart reveals that all work is fully
accomplished in a push or pull cylinder at 90 degrees of a 180 stroke of an
air engine piston cylinder.
This changes our pie chart considerably. If the compressor still has an
input of 6 cu ft per minute into the storage cylinders then this leaves us
with only 1 cu ft per minute actually leaving the storage to be used in the
engine. But if that 1 cu ft of compressed air now passes into the heat
reactors and now comes out as 3 cu ft, then the Pie chart has to show a -2
cu ft per minute. This change automatically pushes the system into a over
(A) 1 Cu ft per minute air from storage supply
(B) 6 Cu ft per minute air from 5 hp compressor
(C) 3 Cu ft per minute heated expanded air from Heat Reactors.
So the engine is using the 6 cu ft per minute of air from the compressor
plus it is only
consuming 1 cu ft from the air storage bottles to operate. But as we add the
3 cu ft of
expanded volume supplied from the Heat Reactor (according to Charles and
the system is now compressing more air into the storage system faster than
air engine is drawing on to run. This happens because the air pressure from
the air storage
cylinders is held back by the heat reactors. So the gauge on the input
can clearly show a smaller amount while the gauge on the heat reactor can
increase in pressure by as much as 40 percent depending on the applied heat.
Adding a second compressor to this equation.
Lets say if we add a second compressor to this configuration, another 2 hp 3
cu ft per minute output this would bring the compressed air input to 9 cu ft
per minute. Total wattage used would be 5222 watts. This leaves us now with
16,778 watts of energy out put. Even without the use of the heat reactors
would now throw us -2 cu ft into the over unity section. But we would now
have a 29 percent loss of power to regeneration.
Considering the fact that the tanks would never run empty, the engine would
never shut down from loss of air. Although there will come a time when the
second compressor will have to shut off when the tanks reach there maximum
So it doesn’t really matter on the amount of air storage capacity you should
retain for the
kinetic power requirements to the engine. If the situation is now that the
engine is a self supporting design and would never run out of air, how much
air do you really need for storage above and beyond one medium size tank.
The buildup of the prototype will prove if an engine can become a self
running concept. Does this break the laws of conservation of energy or just
manipulate the laws some what? If an air engine can return after hours of
running time with more air than it started with, does this justify over
unity? I believe it is just a fact of a reduction in frictional loss’s
associated with a better application in the use of thermal dynamics that
this can be made to come about. The SHRAT turbine is a form of jet
engine that uses the four basis parts of a jet engine. Those are
compressor, turbine, combustion chamber, and propelling nozzles.
Except the SHRAT uses it as: scroll compressor, power turbine
with super heated chambers and propelling nozzles attached to an
exhaust turbine. Except I do not combust fuel but only use
natural expansion energies to create thrust. But by injecting Deuterium
and oxygen into my turbine can produce a chemical expansion reaction.
This is not combustion but a new type of expansion principals not seen
elsewhere. Injected in small amounts would sustain the engine in a space
environment for several weeks.
It is a well known fact that UFO’s fly on some type of electro kinetic
thrust. This is the ultimate way to transfer from an earth atmosphere to a
space atmosphere with out using rockets. It’s like you can drive a car as
fast as you can to go from the west to the east coast of America, but you
can also peddle a bicycle to get there and burn no combustion fuel. As I
have shown here the air turbine/generator can supply enough power to achieve
space orbit in a small 2 man EK craft. The turbine can run as a closed loop
system when it reaches the upper atmosphere. The air simply re circulates
from the exhaust side of the turbine back thru the compressor and is re
compressed into the storage tank for re use. Some new air from the air
storage might be needed but not as much since the environment has now
changed to a non gravity, non friction vacuum atmosphere in which the
turbine will pick up a greater speed with less resistance. Even an air
compressor running in space is a completely different animal. But can the
atmosphere of space which is helium and hydrogen be compressed in a normal
operational compressor and this gas put thru the power part of the turbine
to create kinetic energy to power my generator? If this can happen then
indeed my turbine can transfer from an oxygen/ nitrogen atmosphere to an
atmosphere of space and back.
These are exactly the concepts that Victor Schauberger was working on. On
page 183 of TEE book, last sentence Callum Coats writes that the
Implosion Motors can achieve a 96 percent efficiency. The implosion motor
wave plate turbine can achieve this because it is a rotary turbine design.
If the power part of the wave plates can reach this high efficiency, then
when you add in the power out put of the exhaust turbine, this cancels out
not only the loss’s sustained by the power turbine but pushes the power
curve efficiency into OVERUNITY.
This demonstrable evidence would indicate not so much that we are
witnessing an anomaly but rather a different application of the rules. L.G.
In the words of Sir Arthur Edddington who was equally addressing the present
when in 1933 he wrote, “We have turned a corner in the path of
progress and our ignorance stands before us, appalling and insistent. There
is something wrong with the present fundamental conception of physics and we
do not know how to set it right.”
It has not been easy proving the math calculations behind this air turbine.
But I have in my possession these numbers to prove that Victor Schauberger
was correct in his thinking and design of implosion turbine technology. It
is my firm belief that this is why the “Powers to be” have tried to keep it
out of the public domain. If you couple this power turbine to the right
electromagnetic fields, the force of creating negative gravity thru the
creation of the “Strong Force”, will overcome the “Weak Force” of gravity.
Part 7 of the EDAV PROJECT will begin to show some buildup design on
the circular airframe structure along with the design and mountings of the
SHRAT turbine generators. This aircraft will be carrying 600,000 watts of
power. That’s enough to power 50 American homes at one time. If the power
from the aircraft could be sold back into the grid, that would equal to
about $43,200.00 a month pay check from the power utility. Imagine the fact
if you weren’t flying the vehicle craft how much money it could make for you
in a year. This is a very powerful EV2G vehicle as not to mention its
use as a power station.
As my research and building still continues, I have new drawings and
information to design even better systems than Victor Schauberger could have
dreamed about. What I tell you here is a tip of a rather large iceberg of
information now in my possession. Eventually this information will be
released on this web site.
Researcher & Entrepreneur