rexresearch
Baltzar
von PLATEN
Perpetual Thermal Engine

Prof. Baltzar von Platen
(1898–1984)
The Diamond Makers - Page 63 - Google Books Result
http://books.google.com/books?isbn=0521654742
Robert M. Hazen - 1999 ... was to solve the world energy problem
by designing a perpetual motion system. ... Many years after the
ASEA effort, Baltzar von Platen contributed a strange ...
http://effort.academickids.com/.../Talk:Baltzar_von_Platen_(1898-1984)
An Encyclopedia article about Talk:Baltzar von Platen
(1898-1984) ... (10th October 2003) 4) A near "perpetual motion
" device based on the fact that he proved ...
Below text moved from "Baltzar von Platen (1898-1984" (sic):
I worked with Baltzar in the late 70's (looking for finance) on
many projects which included :
1) A device to manufacture gem size diamonds.
2) A "water" driven car engine the patent of which he sold to
Volvo.
3) A space engine that worked best at -273 degrees, rejected by
the German Patent office because they said there was no such
temperature ( 1925 or so ). Note the Nobel Prize in Physics
awarded this week (10th October 2003).
4) A near "perpetual motion " device based on the fact that he
proved that very close to absolute zero, resistance disappeared.
Again refer to this years Nobel prize winners.
5) Curing a facial melanoma by catching some shark in front of
the Saltsjebad Hotel , drying the fins and applying the powder
to his face
The above was all current in the 80's but of course in the 30's
he produced the first synthetic industrial diamonds with ASEA
and the first commercial refrigerator with a Swedish
refrigerator company.( He called it "ice from a flame" ),
He of course wrote a book explaining that he learned his science
( 100 years ahead of anyone else ) from two visits and meetings
with visitors from space !!!!!!!!!
I lent my signed copy to someone and never got it back.!!!!!!
Sincerely
Hugh Nathan
http://gopherproxy.meulie.net/gopher.meulie.net/0/textfiles/.../platen.asc
http://Keelynet.com/platen.asc
November 29, 1992
Canberra Times, May 7, 1975
A
Radical New Thermal Engine
A Swedish scientist has revived a centuries-old controversy with
contentions that he has discovered the theoretical basis for a
perpetual-motion machine.
Most foreign scientists dismiss the notion of such a device as
contravening fundamental laws of thermodynamics, but the Swedish
claim has created much excitement among scientific circles in
Stockholm.
The man making the claim is Professor Baltzar von Platen, 77,
regarded in Sweden as the inventor of the modern refrigerator
and the first person to produce synthetic diamonds.
His theories involve the production of energy through a complex
process involving air, ammonia, and salt in an apparatus
rotating at very high speed, but scientific sources said the
system was difficult to explain in layman's language.
Professor von Platen has said in newspaper interviews that
unless his ideas are invalidated by some natural law, the energy
could be harnessed to run cars, warm houses, or power aircraft.
He is expected to file a patent application soon and the
secretary of the Royal Academy of Science, Professor Sam
Nilsson, said he had gone through the 50-page documents and
could find no basic flaw. He said the theory put Professor
von Platen in a class with Thomas Edison, who perfected
the electric light bulb, and Marconi, who developed the modern
radio.
But other scientists were more skeptical. One physicist said the
theory ran counter to all known laws.
"There is only a limited amount of energy around, if you use
energy up and don't replace it, you run out", he said.
The physicist was asked if it was possible that Professor von
Platen had hit upon an entirely new law of
thermodynamics that could explain his ideas.
"Every day there are millions of processes going on and they all
obey the laws as we know them", he said.
At the heart of Professor von Platen's idea is a spontaneous
heating process which is continuous.
It begins with the air-water-ammonia process in the centrifuge.
As it spins faster and faster, the pressure at the
extremities increases up to 1,000 times that of the atmosphere
(14.7 x 1000 = 14,700 PSI), generating heat which could be used
to drive a turbine.
Professor Sven Brohult, director of the National Academy of
Engineering Sciences, said that even if the theory was only
partly correct, the practical applications could be enormous.
Vangard Note -- We understand that heat pumps are routinely
claimed to have excess energy outputs in the range of 2 to 5
times what it take to operate the heat pump. An engineer we met
here in Dallas named Mike Eskely also claimed to have a turbine
which generated overunity by high velocity rotation of gases.
Although we never saw a working model, he is convinced he
is onto something and has over 50 patents to his name. Mr.
Eskely told us that in Texas, there were laws that protected the
power companies from having to purchase energy that was not
produced using "acceptable" co-generation sources.
One of the methods that is forbidden is HEAT PUMPS. If you try
to sell your excess power (generated through a Heat
Pump cogenerator) back to the power company, they are NOT
REQUIRED to buy it. As we understand it, they ARE REQUIRED
to purchase excess power generated from Solar, Wind,
Fossil Fuel, Geothermal or Hydro co-generated systems.
We would greatly appreciate further information relating to this
subject, especially details of Professor von Platen's work.
AU501680B2
Heat Transfer by Cyclic Thermodynamic Process
This invention relates to a method whereby a cyclic
thermodynamic process may be induced. By a method according to
the invention a steam engine , a refrigeration plant and a heat
pump (to name three relevant devices) of improved efficiency may
be constructed. The invention is based upon the combination of
two processes, one giving out, and the other absorbing work.
In 1850 the German physicist Clausius formulated a proposition
which has become known as the second law of thermodynamics. we
shall call this Clausius' theory, or the theory.
According to this theory (as is well known) heat cannot of
itself pass from a lower to a higher temperature, nor can it
transform itself into useful work. The theory implies a negation
by exclusion, namely that perpetual motion of the second order
is not possible.
It is now known and accepted that entropy-reducing processes, i.
e perpetual motion processes, exist not only in imaginary
experiments but also in reality. According to Clausius' theory,
however, such a process must,by nature, always be combined with
or join an entropy-increasing, destructive process which (again
according to the theory) must dominate and so undo that which
the former process would achieve.
The destructive process has (according to the aforementioned
theory) always shown itself to be dominant, for otherwise the
two processes in combination could constitute second-order
perpetual motion - which is unknown.
The following description will show how two such processes may
be combined in accordance with the invention and that it will
appear likely, at least theoretically, that the destructive
entropy-increasing process is also dominant in this case, and
for that reason second-order perpetual motion will not occur.
It has been established with certainty, however, that the
present invention makes possible the construction of a steam
engine, refrigeration plant or heat pump of significantly
greater efficiency than any such machine at present known, since
the entropy-reducing process assists the entropy-increasing
process.
The destructive entropy-increasing process is carried out by
known mechanical means such as pistons, cylinders, et al. To
describe and illustrate these devices more than absolutely
necessary would tend only to obscure the most interesting part
of the invention, namely thaf which is related to the second law
of thermodynamics. The following description will, therefore, be
confined mostly to the latter. The well known devices already
mentioned will merely be indicated schematically.
They are not shown at all in fig. 15, which represents a
practical adaptation, since it is assumed there that the second
law of thermodynamics is dominant - an assumption which may be
allowed to stand until the theoretical description accompanied
by the extremely important figs 7 and 8 can be shown to be
faulty. The theoretical description relating to the first five
figures is also an important proof that the proposition upon
which the invention is based, is correct. Nevertheless, the
description relating to figs 7 and 8 may, if so desired, be
studied without reference to figs 1 - 5.
In the physics of entropy-reducing second law of thermodynamics
processes giving out work, one important detail may be noted,
namely that diffusion between two or more substances always
occurs. In a process such as that represented by the first five
figures the path of diffusion is extremely short, or in the
order of a fraction of a millimeter. In a process such as that
represented by any of the other figures it is many times longer,
and in that of fig. 6 for example, is conveniently about 1 cm.
The invention relates to a method for transferring energy by
means of a cyclic thermodynamic process which is induced y means
of a medium comprising at least two substances or two groups of
substances A and B, characterized in that A is caused to diffuse
out of B at a location point u' and to diffuse into B at a
location point u"; the sum of the individual pressures of A and
D i. e. the total pressure, is so regulated that a difference
arises between the total pressures at points u' and u", the sign
and magnitude of t' s difference being so chosen that the said
cyclic process, in theory at least, tends to indicate a quality
of a perpetual motion of the second order.
In accordance with the invention there is provided a method for
transferring heat energy by means of a cyclic thermodynamic
process which method comprises providing a medium comprising a
substance (A), which passes through liquid and vapour states
during the process, and a substance (B) different from substance
(A) , separating (A) from (B) at a first location point by
inducing a change of state in substance (A) , reversing the
change of state of (A) at a second location point, maintaining a
pressure differential between said two points by subjecting the
medium to a force greater than that of gravity, combining (A)
with (B), and allowing (A) to return to said first point from
the location point of combination hy diffusion through substance
(B). whereby heat is transferred from the one of said points at
which (A) vapourises to the other of said points at which (A)
condenses.
The invention will new be described with reference to figs. 1 -
16. For reasons already stated the first 14 figures are
schematic, while Figs 15 and 16 show in principle how a
practical realization of the invention ray be constructed.
Figs. 1 and
3 contribute to a theoretical explanation of the invention.
Fig. 2 shows schematically how a machine might be
constructed, which functions according to the principles
described in connection with the figures 1, 3, 4 and 5.
Figs. 4 and 5 are graphs relating to said Figs. 1 and
3.
Figs. 6,
10, 11, 12 and 13 substance A may be propane (for example)
while substance B is a gas, or mixture of gases, which should
conveniently be heavy. In fig. 9 substance A may be assumed to
be ammonia or some other gas which is readily absorbed by
substance B, which is here assumed to be a solid body.
Figs. 7 and 8, which
are of great theoretical importance, A is assumed to be
ammonia whilst B is a salt dissolved in the ammonia.
Fig. 14 shows
schematically how heat may be conducted to and from a machine
functioning according to the invention.
Fig. 15 shows a practical realization of a machine
according to the invention in which. heat is conducted to and
from the machine in a manner different from that shown in fig.
14.
Fig. 16 shows a detail of a portion of the device of
figure 15.
Assume that I have a
sealed, vessel or cylinder 1 in fig. 1. A small quantity of
liquid 2 suck as, ammonia lies at the bottom of this vessel. The
space above this liquid in the vessel 1 contains only gaseous
ammonia. Ammonia molecules in the gaseous state are designated
a-molecules. Of course molecules constantly change places
between the gaseous and liquid states, but in the present
consideration this is not a significant phenomenon and it may be
disregarded.
Imagine now that a thin gold foil (for example ) is made to
cover the free surface of the liquid. One then pumps into the
system an inert gas, for example nitrogen. Only a relatively low
nitrogen pressure is required, say 20 atmospheres, but partly in
order that the effect I will describe shall be clearly
discernible and partly for reasons which will arise in
connection with fig. 2, I shall assume a final pressure of the
order of several hundred or circa 1000 atmospheres. The
temperature of the system remains unaltered, i.e. room
temperature. Now imagine that I remove the foil. At once I
observe a fall in pressure within the system as a result of the
evaporation of fluid ammonia into the nitrogen. At this pressure
then, the nitrogen behaves as a solvent for gaseous ammonia.
The volume of fluid ammonia decreases by a certain amount which
we shall call Av, and the gas-occupied volume increases by the
same amount. The nitrogen therefore expands and its pressure
falls. Since the nitrogen pressure is dominant, the pressure in
the whole system falls in spite of a rise in the partial
pressure of the gaseous ammonia. Those ammonia molecules, which
have now found their way into the gaseous state, are designated
B-molecules. The solubility of nitrogen in fluid ammonia can be
assumed to be nil, or alternatively we may assume, that the
remaining quantity of fluid ammonia is infinitesimal.
It is fully in accord with Le Chateliers principle that
evaporation of the fluid ammonia in the nitrogen should be
accompanied by a fall in pressure. This- fall in pressure takes
place so that the total rise in pressure as the nitrogen is
pumped into the system shall remain as little as possible.
If, when the foil has been removed from the surface of the
fluid, the total pressure in the system is maintained at a
constant value by means of (for example) a piston, the volume
will decrease and the specific weight of the system will rise
correspondingly. If in some way the B- molecules are forced back
into the fluid state, the volume will increase and the specific
weight fall.
One should now apply the above to the physical sequence of a
machine whose construction is shown schematically in fig. 2.
Each continuous line in this figure represents a channel. I-I is
an axis about which the machine rotates at high speed. Thus the
contents of the machine lie in an extremely intense force-field.
It shall be assumed that this is of the order of 100,000 g at
the farthest distance from the axis. No energy is required to
keep the machine rotating, if one discounts a small loss through
friction. One may assume that channels 6 and 7 are approximately
the same distance radially from the said axis of rotation, and
channels 8 and 10 also.
The machine contains the said substances A and B.
Assume that A is ammonia and B an inert gas of suitable mean
molecular weight. A mixture of nitrogen and sulphur hexafluoride
will be satisfactory. Also assume (for reasons to be shown
shortly) that the contents of the machine flow in the directions
indicated by the arrows in fig. 2. The pressure near the axis of
rotation is assumed to be about 200 atm., and at the periphery
about 1000 atm. One assumes that the inert gas B plus some
ammonia A passes through channel 4 towards the center of
rotation and that fluid ammonia flows through channel 5 in the
same direction. The gas mixture continues along channel 6 which
is parallel to the axis of rotation. From here it passes into
channel 7
There it meets the fluid ammonia, which has entered channel 7
from channel 5. Here the ammonia evaporates in the inert gas,
wherewith ambient heat is absorbed and cooling occurs. The
contact surface here between liquid and gas is the point u"
mentioned previously.
The inert gas and gaseous ammonia now pass outwards from the
center of rotation through channel 3. accompanied by a rise in
pressure and temperature. The change of state is adiabatic if
channels 3 and 4 are thermally insulated from each other. It
will be assumed for the time bein that they are also insulated.
The gas mixture passes from channel into channel 8. Moving
towards a point 9, the temperature of the gas mixture falls in
consequence of close thermal contact between channel 8 and
channel 10, From point 9 to point 11 the temperature falls in
consequence of heat loss to the surroundings which are at a
lower temperature. At point 9 the ammonia begins to condense.
The heat released by condensation is emitted between said points
9 and 11.
This contact surface between liquid and gas is the point u',
also previously mentioned. At point 11 the fluid ammonia
separates off. Since it is lighter than the inert gas, it flows
towards the axis of rotation I-I through channel 5. The
temperature at point 11 may be assumed to be equal to or
slightly higher than that of the surroundings, while at point 9
it is a good deal higher. The inert gas, now impoverished of
ammonia, continues through channel 10 where it is reheated,
channels 8 and 10 functioning together as a heat-exchanger. The
gas having been reheated, it passes into channel 4 and so moves
in towards- the axis of rotation I-I, cooling adiabatically as
it does so.
It passes thence through channel 6 (as already described) and
comes together with the ammonia once again in channel 7.
Channel 5 can be placed in thermal contact with channels 8 and 3
a 1 also with channel 7, this arrangement winning certain
advantages. This is not relevant to the present consideration,
however, and is merely mentioned in passing.
It shall now show how circulation in the machine, as described,
can occur spontaneously. A number of lines II-II are drawn in
fig. 2, all parallel the axis of rotation I-I and cutting
channels 3 and 5. At the point where the first line II-II cuts
channel 3 (the first line II-11 being nearest the axis of
rotation I-I) we observe a very small, though not infinitesimal
mass q of the gas-mixture, Its volume is v and thus its specific
weight is q/vl, When this mass of gas-mixture passes through
channel 8; fluid ammonia separates off and flows in through
channel 5 towards the axis of rotation. This mass of fluid
ammonia we shall cell q' and the remaining mass of gas-mixture
q". Thus q = q' + q". At points where any of the lines II-II cut
channels 5 and 4 we find masses q' and q" respectively. And at
the points where any of the lines II-II cut channel 3 one finds
masses q which, taken in order outwards from the axis of
rotation, occupy volumes vl, v2, v3, etc. out to the periphery
where we have marked the volume v 10, At the corresponding
points in channel 5 the masses q" occupy volumes v' . v'2,
v'3 etc. out to v"10. at the periphery, and at the corresponding
points in channel 4 the masses q" occupy volumes v" , v'2 , v"
etc. out to
1 v" 10 at the periphery.
It clearly follows from the description relating to fig. 1 that
v'10 + v"10 > v10
v"10 in fact contains no 3-molecules at all. These have
separated in liquid state at point 11 and thus comprise the
volume v' 10 . The above expression holds true even if some
a-molecules accompany the condensate, that is to say if there is
a shortage of a-molecules in v" , since the pressure of the
inert gas is of a higher order of magnitude than the independent
pressure of the ammonia. On the other hand, conditions close to
the axis of rotation I-I are quite different. At the temperature
which obtains here, the independent pressure of the inert gas is
of the same order as that of the saturated ammonia vapor. Thus
in the proximity of the axis of rotation 1-1 the shortage of
a-molecules in the channel 4 brings about a substantial decrease
in volume, giving
vi1 + V"1 < vl
Thus a force capable of propelling the gasses through channels
3,8, 10, 4,6 and 7 is generated in the peripheral parts of the
system. This force decreases towards the center and as a general
rule changes sign somewhere between the periphery and the
center. If this takes place, it is a function of the pressure
and molecular weight of the inert gas. Pressure at the periphery
however must not rise above a certain value or the ammonia will
not condense. The system is thus fairly complex. The following
is a simpler exposition.
Let us now suppose the machine in fig. 2 contains only a
convenient quantity of ammonia. As before, the machine rotates
at high speed. We now pump into it an inert gas-mixture of
suitable mean molecular weight. What is meant here by "suitable"
will appear shortly. We pump in a certain quantity of gas until
we observe that the liquid ammonia has climbed up channel 5 as
far as channel 7, when we stop pumping. Now the centrifugal
force on the columns of gas in channels 3 and 4 are equal to or
slightly greater than the centrifugal force on the column of
liquid in channel 5. Since we have chosen a suitable value for
the mean molecular weight of the inert gas-mixture, we will
further note that the centrifugal force on the gas column in
channel 3 is just a trifle greater than that on channel 4. Yet
it is enough to overcome flow resistance in the system. The
difference between the two forces is identical to the propelling
force that overcomes fractional and flow resistance. Thus the
lower the chosen molecular weight, the greater this force will
Be. But since the centrifugal forces are enormous compared to
the flow resistance, the mean molecular weight must be fairly
accurately fixed. By means of the process just described, heat
passes from a lower temperature near the axis of rotation, to a
higher temperature at the periphery.
It may also be of great interest to study what occurs if the
process is carried on isothermally, or to be more precise, at
the ambient temperature. In this case a fine mist of fluid
ammonia will form in channel 3 as the gases come under
increasing pressure on their way out towards the periphery. It
may be assumed that this mist is carried along in the gas stream
beyond the point where the specific weight of the inert gas
equals that of the fluid ammonia. Beyond that point of course
(that is to say nearer the periphery) the specific weight of the
gas-mixture is greater than that of the fluid ammonia. So it may
be further assumed that the fluid ammonia, as before, separates
off at point 11 and flows through channel 5 towards the center.
The ammonia- impoverished inert gas passes through channel 4
towards the center for the same reasons as before. Thus the
events described previously also take place at ambient
temperature. In this instance the only benefit derived from such
a machine is mechanical work. The machine can produce work in
two distinct ways, or in both ways at. once. In one case the
mean molecular weight of the gas mixture is so chosen that the
amount of mechanical work apportioned to the gas is just
sufficient to maintain circulation. The mean density of the gas
is high so that the centrifugal force on the gas columns in
channels 3 and 4 is significantly greater than that on the
liquid column in channel 5. The liquid is thus propelled in
towards the center with great force and therefore, can transmit
work to a piston pump or turbine. In the other case an inert gas
is chosen with the lowest possible mean molecular weight. Its
density, however, must be great enough to enable the liquid in
channel 5 to reach up to channel 7. The gas column in channel 4
will be significantly lighter than that in channel 3, so that
the gas will circulate with great force and can transmit
mechanical work to a pump or turbine.
Suppose the temperature continues, as before, to be the same
throughout the machine. In channel 7 where the pressure of the
inert gas is low, ambient heat is absorbed as the fluid ammonia
evaporates. In channel 3 (channel 8 may be disregarded in this
instance) gaseous ammonia condenses in the presence of inert gas
which is at considerably greater pressure than in channel 7.
With condensation, heat is emitted to the surroundings.
Disregard the absorption and emission of heat taking place in
the inert gas alone, since the process was assumed to be
isothermal, and at ambient temperature. It is expected that
condensation heat emitted in the presence of an inert gas
becomes less, the greater the independent pressure of the gas.
More heat then be absorbed when the ammonia evaporates in
channel 7 , than is emitted when it condenses in channel 3. This
difference is identical with the work done, expressed in units
of heat, by the piston machinery or turbine.
It is now known that condensation heat diminishes as the
pressure of the inert gas increases . This seems to be an
encouraging sign for the value of the hypothesis. Also relevant
to this theme is another isothermal process, which will be
described.
Fig. 3 represents a cylinder 1 closed by a movable piston 15. In
the lower part of the cylinder is a small amount of liquid
ammonia. The cylinder also contains inert gas. So that the
liquid ammonia will remain at the bottom of the cylinder and not
flow upward* when the pressure increases, we assume that the
inert gas is light - say helium. The total pressure in the
cylinder, when the piston is in the position shown in fig. 3,
can be 200 atm. This state is represented by point a in the
PV-graph fig. 4. The gas volume contains both helium molecules
and ammonia molecules, the latter being differentiated as before
into a-molecules- and B-molecules.
Now drive the piston into the cylinder, keeping the temperature
constant. The ensuing ch PV=graph fig. 4 by the curve abc. At c
the mass of fluid ammonia at the bottom of cylinder 1 is greater
than at a, ammonia having condensed out under the increased
pressure.
Imagine now that one can cover the free surface of the liquid
with a gold foil. This done, allow the piston 15 to move out. At
c, of course, B-molecules were also present in the gas, and
since the foil now prevents any evaporation of the liquid, these
B-molecules quickly become a-molecules as expansion takes place.
At d on the curve ?? the B-molecules have been transformed. Here
then, one has the same number of ammonia vapor at the same
temperature. In this state, point d, imagine that one pricks a
small hole in the foil which wi11 permit diffusion of just
sufficient molecules to ensure that the mass per unit volume of
gaseous ammonia remains constant, as the piston continues to
move out. Thus during the change of state d - e in fig. 4 there
is a full complement of a-molecules present in the gaseous state
but no B-molecules at all. As in the case of fig. 1, the total
pressure during the change of state d - a is higher than during
B - a. For the same reason it is also higher during c - d than
during c - b.
When the state has reached e in fig. 4 remove the foil. A
quantity of liquid then evaporates, that is to say gaseous
ammonia dissolves in the helium, i.e. B-molecules find their way
into it. The change of state here will be e - a in fig. 4, i.e.
a fall in pressure at constant total volume. The perpetual
motion work released is then equal to the area a-b-c-d-e-a .
This work implies that there is an absorption of heat from the
surroundings. It is easy to understand how this occurs. When the
volume diminishes, a - b - c, ammonia condenses all the while.
When the volume increases, c - d - e, only some of the ammonia
evaporates. During c - d of course, there is no evaporation at
all and during d - e only so much that the number of a-molecules
per unit volume remains constant. The pressure in the inert gas
is thus greater during condensation than during evaporation and
, therefore, (as we know) the heat lost to the surroundings in
condensation must be less than the heat gained in evaporation.
In fig. 5 the abscissa v shows the volume of liquid 2 in the
cyclic process described with reference to fig. 4 and as before,
the ordinate p is the total pressure, i. e. the liquid pressure.
In fig. S points a', B', c', d', e' correspond to a, b, c, d, e
in fig. 4.
It is worthy to note that a perpetual motion process such as
that indicated by the graph, in fig. 4 could theoretically be
possible at the lowest pressure one cares to choose for the
inert gas. The lower this pressure is, however, the more
difficult it is to make the process function. On the other hand,
the pressure may not exceed a certain value or the ammonia will
not condense. We have, of course, only chosen ammonia as an
example.
The processes represented in figs. 3 and 4 can also be explained
in another, perhaps simpler way.
Begin the process at point e in fig. 4 and have the cylinder 1
and piston 15 (fig. 3). At the Bottom of the cylinder 1 is a
small quantity qx of fluid ammonia 2. Thus the volume between
liquid and piston contains only a-molecules. Lay a thin gold
foil over the surface of the liquid. Then pump helium ( for
example ) into the chamber, the total pressure rising to e.g.
200 atm. Escape of B-molecules into the gaseous state is
prevented by the gold foil. All this takes place at constant -
e.g. room - temperature. Now we remove the gold foil.
B-molecules immediately disperse into the gaseous state. The
quantity of liquid q is so chosen that when equilibrium has been
reached almost all the liquid has evaporated, there remaining
only a vanishingly small though, not infinitesimal quantity at
the bottom of the chamber. The position of the piston has until
now regained unchanged. As instanced previously in connection
with Le Chatelier's principle, when evaporation takes place
total pressure falls. When equilibrium is reached, total volume
having remained constant, total pressure will have fallen from e
to a in fig. 4.
Now drive in piston 15. Note that in accordance with what has
previously been said, this may be done at any total pressure
chosen within wide limits. The ammonia condenses. Point c in
fig. 4 is so chosen that when it is reached, the exact quantity
qx of ammonia has condensed. Now lay the gold foil once more
over the surface of the liquid, and then allow the piston to
return to its original position. Clearly we have now reached
point e where we started the process. Once again remove the
foil, wherewith B-molecules immediately disperse into the
gaseous state. When equilibrium has been reached, and only a
vanishingly small though not infinitesimal quantity of liquid
remains (in accord with what has just been said), we have
arrived at point a.
Perpetual motion work e - a - c - e has been released.
Returning now to fig. 2. If the pressure in this machine is
below a certain value or if the mean molecular weight of the
inert gas is chosen wrongly one may still get perpetual motion
work from the machine if the circulation is maintained by the
sacrifice of external work, i. e. if it is kept going by force.
This will be less than the perpetual motion work than is
obtainable theoretically. In these circumstances then, the
useful work produced is equal to the difference between the
other quantities of work. This conclusion, can only be of
theoretical interest since it is simpler to choose the said
pressure and mean molecular weight so that the process as
described earlier shall occur spontaneously. In saying this of
course, one presupposes that no destructive, entropy increasing
process causes sacrifice work in maintaining the circulation.
Thus in circumstances where losses exceed a certain value, the
final advantage of the invention is only that it enables one to
construct, for example, a refrigerator or heat pump of greater
efficiency than any yet known, but not so great that the second
law, which holds that it is impossible to achieve second order
perpetual motion, should still hold true.
When liquid e. g. fluid ammonia forms in the presence of the
inert gas or gas mixture, a diffusion of the condensing medium A
takes place close to and in the direction of the liquid. The
path of this diffusion through the gas is extremely short, but
exists nevertheless.
In the course of the cyclic thermodynamic process just
described, it is supposed that substance A, which oscillates
between the gas and liquid state, be ammonia. But there are many
other substances to choose from. Propane CC3[18) is one at
these. Its pressure-temperature function, i.e. PT-curve,
approximately coincides with that of ammonia. Its molecular
weight as well as vapour density is higher, and its specific
weight in the liquid state lower than that of ammonia, and these
characteristics contribute to a considerable lowering of total
pressure in the machine. ( Other suitable substances A as well
as other inert gasses B can easily be found with the aid of
physical tables ).
The machine could have many such channels 6, 7, 8 and 10 ( fig 2
) placed about the axis of rotation. Alternatively ( as will be
shown 6 analogy in fig. 2 ) each channel may be a geometrically
circular ring with rectangular cross-section. Each such
geometric ring is defined by or formed from two concentric
circles whose centers lie in the geometry axis I-I. The channels
6, 7, 8 and 10 thus take the form of concentric cylinders.
Channels 3 and 4 may be formed from discs whose center is also
in I-I. All the channels participating in the heat exchange
function, whatever geometric form they may have in
cross-section, should be narrow enough to achieve a high
coefficient of heat transmission between gas - or vapor- stream
and solid wall.
Even if circulation in the system occurs spontaneously ( perhaps
against expectations, according to Clausius' theory ) it may he
useful to control the circulation through two pumps, one each
for liquid and gas. The pumps are built into the hermetically
sealed system and so absorb no work except that lost to
friction. They are conveniently driven by three-phase induction
motors whose armatures are also built in. If circulation does
occur spontaneously "against expectations" we will have (as
mentioned.) a second order perpetual motion in reality, which as
yet the second law does not permit us to believe. In whichever
case, this machine also will be more efficient than any existing
refrigerator or heat pump.
Heat may be taken to and from the hermetically sealed machine
with the aid of another system (presented in greater detail in
connection with fig. 14) which is fixed to the machine and
rotates with it. If these rotate in very, low air-pressure,
unnecessary losses through friction can be avoided. This second
system, whose technology is familiar, need not be hermetically
sealed. A fluid oil is driven or circulates within it.
If heat is to be transferred from the high temperature of the
hermetically sealed system to its low temperature, this may be
done by means of an ordinary steam engine which will release
useful work.
In the entropy-reducing perpetual motion processes described
above, mentioned the path of diffusion of substance A through,
out of and into substance B was very short. Other such processes
were mentioned, in which the path of diffusion was many times
greater.
These we will now describe with reference to figs. 6 - 16.
Fig. 6 represents a hermetically sealed vessel 21 of convenient
material e. g. steel. The vessel contains a beaker 22 of other
suitable material such as glass which has low thermal
conductivity. We suppose that the bottom 22a of beaker 22 is
porous glass, china clay or other such suitable material. The
beaker stands on a thin porous tile 23 which covers the bottom
of the vessel 21.There is thus contact between bodies 22a and
23. We also suppose that the beaker 22 is filled nearly to the
brim 22b with a suitable liquid 24 substance A. The upper
surface of this liquid 24 is marked y", which also designates a
level. The brim 22b of the beaker and the surface y" lie very
close to the ceiling 21a of vessel 21. The substance A may be
propane (C3H8 ), ammonia (NH3) water, et al. The remaining
volume 25 of vessel 21 contains of course, gas or vapor of
substance A. It also contains substance B in gaseous state. A
mixture of the heavy inert gases sulfur hexafluoride SF6 and
xenon X is suitable. The whole device is at room temperature o
and is subject to a force field expressed as ng, where g is
earth gravity and n a variable factor. Assume that heat Q can
leave the device only through, the porous tile 23 and enter it
only through the liquid surface y". We choose the partial
pressure of B so that the mean specific weight of the gas
mixture in chamber 25 equals the specific weight of the liquid
24. When B is composed of said substances SF and X, the said
partial pressure is of the order of 100 atm.
Suppose that the value of n is between 60,000 and 100,000, which
is easily achieved centrifugally.
Assume for practical purposes that force-field ng is the same
throughout the inner volume of vessel 21. Suppose finally that
substance A is propane ( C3H3 ), which happens to have a fairly
high molecular weight or vapor density and fairly low specific
weight in liquid state.
For reasons which will be clarified shortly, when we consider
fig. 7 and 8 , we have the right to assume that the following
can take place. The propane evaporates under partial pressure p"
from the surface y" , whose temperature in dynamic equilibrium
is T2.
Force field n causes propane vapor to diffuse downward through
the inert gas ( SF and X ) in chamber 25, following which it
condenses under partial pressure p' at the floor 23, whose
temperature in dynamic equilibrium is T1. One then has p'> p"
and T1 > T . In this process, then, heat passes of itself
from a lower to a higher temperature, since no work is requires
to maintain force-field ng if small fractional losses are
discounted.
As has just Been said, this is merely yet an assumption.
But in considering figs. 7 and 8 we will begin to see how great
the possibility is that the assumption accords with reality.
Now designate a fraction of the pressure pl as p'6, and a
fraction of p" as p" . The existence of these fractional
pressures is analogous to conditions already described in
conjunction with figs. 1 to 5, that is to say that B-molecules
of propane are forced from the liquid into the gaseous state by
the inert gas. Clearly p'B>p"B, since the pressure of the
Inert gas due to the action of force-field ng is greater at the
floor 23 than at the surface y". This difference, P'B3 - P"B,
tends to lower the temperature T immediately above the floor 23
or, expressed another way, the propane molecules coming down
from surface y" have difficulty penetrating the zone immediately
above the floor 23 because some of the space is already taken by
the B-molecules that are generating pressure p'. This phenomenon
appears to indicate that the molecular weights of substances A
and B could be chosen relative each other so as to eliminate the
perpetual motion effect attempted to be obtained.
As an example of substance A was named propane was mentioned its
relatively high molecular weight. It is, however, considerably
less than that of sulfur hexafluoride and xenon, which mixture
was named an example of substance 13. Now exchange the latter
mixture for hydrogen, or hydrogen plus nitrogen (H,N2). The
pressure in the device, which was previously of the order of 100
atm, will now of course be several times greater since the
weight of the gas column in chamber 25 must equal that of the
liquid column in Beaker 22.
It is now easier to visualize that the propane vapor diffuses
downwards through the inert gas to the floor 23 and there
condenses at a higher temperature T1 than the temperature T2 at
which it evaporated from surface y".
One can believe this because both hydrogen and nitrogen are
considerably lighter than propane. For analogous reasons one
could visualize diffusion of A against the direction of
force-field ng instead of with it; that the floor 23 and
condensation at higher temperature at the surface y", if one
simply exchanged the propane for ammonia (H3N) which has a low
molecular weight, and used SF 6 and X as previously mentioned
for the inert medium B.
In this case the force engendered by the B-molecules is acting
in the same direction as diffusion.
That said about fig. 6, further detailed explanation is not
possible due to lack of experimental data. A formula exists for
deriving values of p'B and p"B, but it cannot serve, partly
because it is based on the assumption that Clausius' theory is
generally applicable and partly because of lack of data. Fig. 6
will, however, emerge clearly after discussion of fig. 7 and 8,,
partly because it is closely related to them and partly because
a description of then is not hindered by any lack of
experimental and theoretical data in the case where diffusion of
A through B takes place against the direction of the force-field
ng.
The vessel 30 in fig. 7 corresponds to vessel 21 in fig. 6
above. In this vessel 30 is a beaker 31. A partition 34 divides
the interior of the beaker into two parts, 35a and 35b. These
spaces communicate with each other through the opening 36 at the
bottom of partition 34 and through. the opening 37 over the top
of partition 34, which, does not reach, fully to the brim of
Beaker 31. Out of the bottom of beaker 31 runs a short channel
38 reaching almost to the bottom 30' of vessel 30. Chambers or
channels 35a and 35b together with the partition 34 can form a
heat exchanger 35. The interior of the vessel 30 outside beaker
31 is divided by a wall 40 into two parts, an upper chamber 30a
and a lower 30b, which chambers are connected only by the gas
pump or compressor 41. The bottom of beaker 31 is covered by a
porous tile 42 whose upper surface is itself covered by a
semi-permeable coating or membrane 44 which is hermetically
sealed to the interior surface of beaker 31. In this connection
it may be mentioned that it is known that a liquid which is not
or is very little soluble in the liquid with which it is in
contact, can function as a semi-permeable member. However, at
least for the time being one assumes that membrane 44 is a
common membrane of the prior art.
Beaker 31 is almost entirely filled with a suitable liquid whose
free surface y" (which also denotes a level) lies between the
upper edge of partition 34 and the brim of said beaker. This
liquid also occupies the pore of the semi-permeable membrane 44
and the tile 42, channel 38 and, as a thin layer, the bottom of
chamber 30b up to the level y' which may also be described as
the free surface of the liquid in that chamber. One presupposes
that the two said free surfaces of the liquid are maintained by
convenient means at the constant levels y' and y". Apart from
that occupied by the liquid, the entire remaining volume of
vessel 30 contains gas or the liquid vapor. Assume (only for
example) that the liquid is ammonia.
Temperature of the upper part of the vessel 30 may be denoted
T2, of the lower part T1, and of the surroundings T0. The whole
apparatus is subject to a force-field ng .
Assume n =- 1, i. e. the apparatus is subject only to gravity,
with ambient temperature throughout, T1 = T2 = Ta. Now let T1
rise to e.g. 50 C and let T2 sink to e. g. -10 C and in doing so
the force field n must be raised from 1 to a value designated
n0, which is precisely enough to keep the liquid levels y' and
y" unaltered.
Vapor pressure p' of the ammonia in chamber 30b is that which,
obtains at the exemplary temperature T1, i.e. 50 C, and this
value for p' will remain constant during the argument which
follows. On the other hand, as will soon show, vapor pressure p"
above surface y" will vary.
At this stage of course, p" is the vapor pressure of fluid
ammonia at the exemplary temperature T2, i. e. -10 C.
In order to maintain the value of T and T start up the pump or
compressor 41. Ammonia vapor is pumped from chamber 30a and
pressure p" to chamber 30b and pressure p' .
The ammonia boils away from the liquid surface y", absorbing
heat, and condenses at liquid surface y' emitting heat. The
liquid formed from condensation at temperature T flows against
the force-field ng through channel 38, the porous bodies 42 and
44 and the channels 35a and 35b, finally reaching the low
temperature T where it changes to vapor. The arrangement
functions just like an ordinary compressor refrigerator. It will
be supposed that the cycle takes place without loss and that the
work required, delivered only to compressor 41, has consequently
the minimum value given by Carnot's equation, which work will be
[ illegible ] d Lc . It should be mentioned that, for the cycle
to take place without loss, liquid must pass from
T1 to T by means of a reversible process which, delivers a
little work to compressor 41. This consideration is elementary
and so need not be amplified. The gas compressor 41 could be
exchanged for a liquid pump by which, liquid ammonia in chamber
30b would be pumped into beaker 31, and in this case the gas
pressure p' would be generated solely by the force-field ng
acting on the gas in chamber 30a and, if T2 is constant, T1
would clearly be a function of n.
Now shall be investigated how one may minimize the work
sacrificed, or arrange that it is less than Lc without, of
course, reducing the quantity of heat that is to be transferred
from the lower temperature T2 to the higher T1 . In the fluid
ammonia in beaker 31 now dissolve a substance such as a salt or
a mixture of two salts e.g. LiNO 3 , NaI, KI, NH4N03 ,
KN03 or KNO2. Said substance may of course also be a liquid
which is wholly or partially soluble in the substance A (e.g.
NH3 ). All these substances have considerably greater molecular
weight than ammonia. One must of course take care that the
addition of the salts does not give too great a volume of liquid
in beaker 51. Thus arrange in some way that the liquid
circulates through heat-exchanger 35 in the direction indicated,
and it shall be assumed that no heat losses occur, i.e. that it
is completely efficient.
The dissolved salt has a high osmotic pressure which seeks to
draw liquid from the chamber 30b through the membrane 44.
In order to maintain equilibrium so that the liquid level in
chamber 30b will remain unaltered at y' and similarly the liquid
level in beaker 31 unaltered at y", one must increase the value
of factor n, say from n0 to n .
Now, work will be released in the heat exchanger 35 since the
liquid flowing upwards through channel 35a contains a little
more ammonia and, therefore,, Ray a lower specific weight than
the liquid flowing downwards in channel 356. But theoretically
this work can be retained and passed on to the compressor 41.
For this and other physical reasons which need not be described,
one may disregard this phenomenon; that is, may fairly assume
that the work dissipated by the heat-exchanger is nil or, in the
case of combinations other than ammonia and a salt, that the
work consumed by it is likewise nil. The apparatus described
here functions in , a manner equivalent to an ordinary so-called
resorption refrigerator, and it follows that since no
irreversible losses occur, the work that must be transferred to
the compressor 41 remains constant or equal to Lc. Since the
vapor pressure p' of the pure ammonia above surface y' remains
unaltered, T being constant, and since the work required by the
process according to Carnot also remains unchanged, and the
quantity of heat to be transferred from T to T both likewise
being constant, then the pressure immediately above the
compressor, P , and with it the factor p' - p which is
proportional to the work, must also remain unaltered in spite of
the increase of factor n from no to nl. All these conditions
follow from Carnot's equation, hence a physical-chemical proof
is not required. Further, no perpetual motion process exists in
this case.
Now stop circulation of the liquid in the heat exchanger 35 and
keep factor n unchanged at the value n1. The salt concentration
immediately above the membrane 44 now rises due to diffusion of
the salt downwards under the influence of force-field ng. The
small amount of fluid ammonia at the bottom of chamber 306, in
channel 38 and in the porous tile 42 now drawn up through the
membrane 44 into the beaker 31. Ammonia gas makes contact with
the underside of membrane 44 and the liquid filling each pore in
the membrane acquires a concave surface facing downwards towards
chamber 306. These surfaces are concave since, if menisci were
to form in the downward-facing pores of the membrane 44 in the
absence of diffusion, they would be plane; surface y' being
plane. When diffusion takes place osmotic pressure builds up,
and the menisci must become concave to withstand it. The gas
pressure p' sinks in consequence. Salt concentration in the
upper part of the beaker falls due to diffusion downwards of the
salt under the influence of force-field ng. As a result gas
pressure p" increase? and with it gas pressure Px. Thus the
difference between the pressure p' and px has been reduced and
in consequence less work needs to be supplied to the compressor
for it to move the same quantity of heat from T2 to T .
This work which we will call L is thus less than Lc, which (
according to what has already been stated ) implies
that the process is perpetual motion of the second order.
When Lp is greater than zero but less than Lc ( L c > 1,
>0 ) the process may be described as incomplete second order
perpetual motion. When L is equal to or less than zero ( L<0
) the process may be called complete.
When T2 is equal to T1 , px is greater than p' and the
compressor then functions as a rotor, delivering mechanical
work. This also means that Lp<0 . It will been seen from this
that, at a certain difference between T1 and T2, Lp will equal
zero. This condition will now be illustrated.
Assume that the machine is functioning as a resorption
refrigerator. The liquid is circulating in the heat exchanger
35. Suppose T1 = T2. The machine is pumping heat from T- to T1
but since T1 - T2 and thus Delta T = 0 the work required by the
pump equals zero, in accord with the ordinary laws of
thermodynamics.
Thus px = p'. We now stop the circulation of liquid in the
heat-exchanger 35. Diffusion of the salt causes p' to fall and
p", also px , to rise. Thus px> p' and the compressor 41 now
functions as a motor or steam engine. At a certain value for T1,
Px = p'. The machine then delivers no work, that is, the
compressor 41 no longer functions as a motor, and the machine
becomes merely a refrigerator - a perpetual motion refrigerator.
In a case where there is no circulation in the heat-exchanger
(a, in the preceding paragraph ) the partition 34 can be removed
and the beaker 31 could contain, instead of the ammonia, a
mixture of two liquids of limited solubility. This could be
advantageous in certain circumstances which will not be
described in further detail. Suffice it to say that a perpetual
motion process could also be induced in this case.
In Fig.7 the previously mentioned point u" is formed at the
upper surface of membrane 44 while u' while u' clearly coincides
with surface y".
Fig. 8 differs only slightly from fig. 7. Two channels 52 and 53
lead out of the bottom of beaker 31 down to the bottom of vessel
30. In each is a liquid pump 52a and 53a. One of these, say 52a,
pumps out liquid from beaker 31 while the other pumps liquid
into it so that the liquid is an ammonia-salt solution.
Liquid is circulating in the heat-exchanger 3S, compressor 41 is
functioning and force-field ng is operative.
The ammonia is absorbed at surface y' and is then pumped into
beaker 31 by liquid pump 53a. Heat is emitted at the higher
temperature T1 and absorbed at the lower temperature T2. The
process is assumed to be reversible, and so the work sacrificed
is the same as the value given by Carnot, Lc , i.e. the
difference between work demanded by 53a and work delivered by
52a, plus work demanded by compressor 41. The said difference is
almost exactly equal to the work required (we will call it LA)
to pump the amount of ammonia in question (substance A) in fluid
state, from surface y' to the bottom of beaker 31. It is exactly
equal to LA - Delta'L where Delta'L is a correction term
dependent upon a certain shrinkage of volume which takes place
when the fluid ammonia mixes with the fluid salt solution. The
mean concentration of the latter may be called C' . We now stop
the circulation in heat exchanger 35 and diffusion begins. The
salt concentration of mean value C' now increases at the bottom
of beaker
31 to z", decreases at the zip, and of course also increases to
C" at the bottom of vessel 30 through pump 52a. Suppose now that
one keeps pressure p' unaltered.
Then the difference between work supplied to pump 53a and work
delivered by pump 52a also remains virtually unchanged at LA
since, the force-field being constant uniform, the hydraulic
pressure at the bottom of beaker 31 is independent of diffusion.
In other words (as is self evident) a salt molecule weight the
same whether it is at the top or the bottom of the beaker or,
the weight of liquid in the beaker is not dependent on the
distribution of salt in it. The exact value of the difference
between work, demanded and supplied by the two pumps is LA -
Delta "L". The correction term Delta "L is somewhat larger than
the previous term Delta'L, since C" is larger than C'. The work
required from the pumps is now a little less than before, so it
is fair to take it as constant. This allows us to disregard the
pumps 53a and 52a altogether in the argument which follows.
Now if the gas pressure p' is to remain unaltered as suggested,
in spite of increased salt concentration at the bottom of beaker
31 caused by diffusion, the temperature T1 must be raised, say
to phi T1 where phi > 1.
But if T2 is held constant at, say, ambient temperature, the gas
pressure p" will rise because of the decreased salt
concentration in the upper part of beaker 31 similarly caused by
diffusion. As p" rises, px also rises and it follows that, since
p' remains unaltered, the compressor 41 demands less work.
Before diffusion began the work demanded by the process was that
given by Carnot, Lc . Now the demand is less than Lc, and this
in spite of an increase in temperature T1 to phi T1.
This clearly shows the process to be second-order perpetual
motion. If it does not to lead to a practical useful perpetual
motion machine there must be present, according to Clausius, a
destructive process of sufficient intensity. One such is that
the diffusion resistance in a liquid is so great that in all
probability no difference between T1 and T2 will be discernible,
in which case our experiment becomes merely imaginary. But not
let T1 and T2 equal. On the basis of our imaginary experiment
and the argument presented with fig. 7 it is now seen that the
compressor or machine 41 will deliver a quantity of work.
It should be added that the temperature T1 at the bottom of
vessel 30 ought strictly speaking to be given T1 + Delta T on
the left side and T1 - Delta T on the right side of the vessel,
where Delta T is a very small correction depending on the fact
that salt concentration is a little higher on the left than on
the right. During absorption the salt concentration decreases
from left to right, since it was assumed that liquid was flowing
out of the lower end of channel 52. This variation, however, was
of no concern in the theoretical argument accompanying fig. 8.
In figs. 7 and 8 it was noted that the molecular weight of the
dissolved substance B ( one, or a couple of salts ) was
considerably greater than that of the solvent A, ammonia. The
salt B therefore diffuses downwards in the beaker 31 under the
action of force-field ng and then comes to rest, so that the
salt concentration at the bottom of the beaker remains gleaner
than at the surface y" of the liquid, while at the same time
ammonia diffuses upwards against the force-field ng and
evaporates at the said surface. This is clearly what occurs -
the cycle having its causes in simple and well-known natural
phenomena.
But suppose that the soluble substance B arranged in place of
the salts has a considerably lower molecular weight than the
solvent, substance A. The concentration B will not be greater at
the surface y" than at the bottom of beaker 31. So it is
probable that the process will work in the opposite direction
with A evaporating below at surface y" and condensing or being
absorbed at surface y" at a higher temperature, and therefor
diffusing down in the direction of force-field ng through
substance B in beaker 31.
Considering the similarity between the process illustrated in
fig. 6 and those illustrated Figs. 7 and 8, it is probable that
a perpetual motion process could be achieved in accordance with
the first-named fig. 6. In figs. 10, 11, 12 and 13, which are
closely related to fig. 6, diffusion of A through B occurs in
the direction of the force-field, although ( as mentioned ) it
might be convenient to reverse the direction. One has only to
select the substances A and B according to requirements.
A process according to fig. 7 could be combined with one
according to fig. 6. Suppose for example that the liquid in fig.
7 is ammonia and a salt, and that in chamber 30a there is a
light inert gas such as a mixture of nitrogen and hydrogen.
Suppose also that the wall 40 and compressor 41 are taken away.
Judging from previous considerations, it is probable that the
process now induced in the liquid in beaker 31 will abet the
process induced in the gas mixture in chamber 30a.
It is well known that a gas diffuses through another gas ( as in
fig. 6, it is closely related other figs. and also figs. 1 - 5 )
with vastly less resistance than a liquid or salt through
another liquid ( as in figs. 7 and 8 ). For this reason a
perpetual motion process employing diffusion between gases must
be considered to be technically highly viable.
The theoretical arguments put forward in connection with figs. 7
and 8 appear to be incontrovertible, at least when diffusion of
A occurs in the opposite direction to force-field ng. This
cannot be said, however, for the realization illustrated by fig.
9, probably because here the diffusion of substance A through
substance B occurs in the same direction as the force-field, and
in this case I am not sufficiently familiar with the physical
phenomena involved. Nevertheless, the figure shall be described.
It shows an hermetically sealed vessel 49.
In this vessel is a pillar 5O of e.g. porous active coal,
suitably encased in a gas-tight envelope or skin 50' which,
however, does not reach all the way to the base of the pillar,
nor cover its top surface. Volume 51 in vessel 49 contains (for
example) gaseous ammonia.
As is well known, ammonia is forcefully absorbed by active coal.
Absorption increases as the temperature falls, which means there
are more ammonia molecules crowded onto a unit surface of coal
at a lower temperature than at a higher. The whole is subject to
force-field ng. Assume first that n - 1, that is to say the
force field is equal to the earths gravity. Temperature
throughout is equal to the ambient temperature T0. The specific
weight per unit volume of ammonia within the coal pillar is
significantly greater than that of the gas in chamber 51. The
ammonia in the coal pillar may be considered as a liquid. When
factor n is increased significantly over the value of 1, we may
suppose that the concentrated ( or perhaps liquid ) ammonia in
the coal pillar travels downwards. Thus equilibrium is disturbed
In the force field. There is reason to believe that evaporation
occurs at the bottom part of the pillar accompanied by a fall in
temperature can be expected at the pillars upper surface, such a
phenomenon has not been observable, however, in spite of a value
for n or over 2000. Undoubtedly the ammonia molecules are too
strongly bound to the coal. It is quite conceivable that ultra
sound could act as a lubricant between the ammonia molecules and
the coal pillar, but this experiment has not yet been performed,
It might be an advantage to replace the coal with fine fibers
such as glass, for example, since the ammonia molecules would
then travel over smooth, surfaces instead of in the mass
surfaces of coal. In the event that this phenomenon could be
induced using combinations of substances other than those named,
it is strikingly similar to the phenomena described in
connection with figs. 6, 7 and 3. The points u" and u' mentioned
previously coincide respectively with the upper and lower ends
of the coal pillar. As well as gas A, chamber 51 may contain
heavy gas of lesser density than liquid A.
Return now to fig. 6. The specific weight of the inert gas in
the lower part of chamber 25, i. e. in the vicinity of tile 23,
is greater than that of the liquid.
There is thus a risk that liquid can gather in a layer at some
level between the ceiling 21a and the tile or floor 23. One
could then arrange, as fig. 10 shows, a porous rod 62 whose
upper tip 62a extends into a tiny chamber 63 which occupies a
very small part of chamber 25.
This part 63 is thermally isolated from the remaining larger
portion of chamber 25 by a screen 64. A small quantity of heat
may be supplied electrically to the tip 62a of rod 62, by which
means the liquid in the said layer 15 taken up in the rod and
eventually evaporates off, the vapor then being carried by the
force-field ng towards the floor 23 where it condenses. It is
simpler, however, to do as shown in principle in fig. 11. The
interior 25 of vessel 21 contains (for example) propane,
sulphur, hexafluoride and xenon. The pressure of the inert gas
mixture is great enough - something up to 100 atm. at room
temperature -- that a thin layer 55 of propane is always at the
ceiling of chamber 25. Under the influence of force-field ng
propane evaporates from this layer at a certain partial
pressure, p and temperature T2. Propane vapor condenses at the
floor of chamber 2 at a certain pressure P1 and temperature T1.
When a drop has formed on the floor and grown large enough for
its buoyancy to overcome adhesion, it floats up and joins the
liquid layer 55. To facilitate heat transfer from condensing
vapor to the floor, the latter may be provided with a large
number of small studs 56 of a heat conducting material. They are
shown as being pointed upwards, in which case the drops will be
fairly small. If the drops are to become larger before detaching
themselves, the studs must be made blunt or given other
appropriate configuration. Of course the ceiling may be
similarly studded to facilitate heat transfer to the liquid
layer 55.
Fig. 12 shows a porous tile 57 of e.g. porcelain covering the
bottom of the vessel 21. Standing out of this tile 57 is a
porous pillar 58 of porcelain or other material having low
thermal conductivity. A layer of fluid propane at the ceiling of
the chamber 25 is marked 55 as in fig. 11. Fluid propane travels
out of tile 57, where plane vapor has condensed, through pillar
58 up to the ceiling where it rejoins the layer of liquid 55.
The movement occurs because the liquid is lighter than the gas.
In figs. 11 and 12 temperature T1 is higher than T2 since
pressure p1 is greater than p2. Heat thus passes of itself from
a lower to a higher temperature, as long as the force-field ng
is operative. We have not yet touched on the destructive
entropy-increasing process which, if Clausius' theory is
generally applicable, must reveal itself if the processes
illustrated in figs. 6, 10, 11 and 12 are not to be second-order
perpetual motion. Suppose that a symptom of such destructive
process is that the pressure and there with the specific weight
of the inert gas (eg. SF6 and X ) may not be great enough to
float the fluid propane all the way up to the ceiling of chamber
25 by itself. The liquid must then be pumped up the last part of
the way by pump 70, shown schematically in fig. 13. Pump 70 is
thus both suction and pressure pump. The liquid, now somewhat
heavier than the gas in the upper part of chamber 25, flows out
of the pipe 71 into the trough 72, of which many such can be
placed at this level. From trough 72 the liquid evaporates at
the lower temperature T2. The vapor diffuses downwards and
condenses on the porous tile 57 at the higher temperature T1. It
is possible that this destructive process could be intense
enough to make Clausius' theory valid in this case also. But it
cannot be so intense, that significantly improved efficiency
over an ordinary compressor refrigerator cannot be won. Because
condensation at the floor takes place in a higher partial
pressure of the gas mixture than evaporation at the ceiling,
less heat is emitted at the higher temperature T1 in the course
of the thermodynamic cycle - it having been stated that heat
released by condensation diminishes under increased pressure of
an inert gas. This carries the inescapable conclusion, according
to the first law, that to keep the process in function now
requires less work.
It may be interesting to note that the inert gas or gas mixture,
substance B, behaves as a semi-permeable body which, transports
substance A when that is a vapor or gas but not when it is a
liquid ( figs. 6, 7, 8, 10, 11, 12 and 13).
In accordance with previous observations, liquid of A ( e.g .
NH3, H2O ) have higher specific weight than gas of B (e.g. SF ,
X ) but lower molecular weight.
Diffusion will then occur in the opposite direction to
force-field ng. In fig. 11 for example, the liquid 55 would lie
at the floor instead of the ceiling in vessel 21. Substances A
and B are chosen to suit requirements. In the following figs. 14
and 15, A and B are assumed to be so chosen that diffusion
occurs in the direction of the force-field.
Fig. 14 shows, in principle, a practical realization of the
invention. Several containers 21-1, 21-2 &c are grouped
together so that the floor of one is the ceiling of the next.
The force-field ng is produced by rotation as before. The
geometric axis of the axis of rotation is marked C-C. Each
container encloses a circular chamber 25 , 25 &c Whose
geometric axis is the same as the above. The chambers contain
propane and inert gas. The force-field ng is proportional to the
mean radius of each chamber and thus the temperature difference
between floor and ceiling, if all the chambers are the same
height, will be least in chamber 251 and greatest in the chamber
on the periphery. 25 in the drawing. The temperature differences
are additive. Heat is supplied to a low temperature T2 by means
of the liquid flowing through channel R2, and drawn off from the
higher temperature T1 through channel R. The channels are shown
only by dotted lines. The inflow and outflow ends of these
channels lie in the immediate proximity of the axis of rotation
C-C. To avoid unnecessary energy losses the whole rotates in a
high-vacuum chamber, whose housing has not bean illustrated.
In fig. 15 the axis of rotation. is marked C-C as before. Only
three chambers are shown, 25-1 - 25-3, though of course the
number may be greater. The geometric axis of each chamber
coincides with said axis C-C. The material of the wall 81
enclosing each chamber is suitably steel of the highest possible
tensile strength.
Parts 81a to left and right of the drawing are suitably joined
to the rest of walls 81 by a seam weld 82 (fig. 16).
The inner wall 81 of chamber 25-1, i.e. that nearest to axis
C-C, rests on or is shrunk onto an axle 83. The inner wall of
25-2 lies against the outer wall of 25-1 etc. To the left and
right in each such chamber is a plug 84 of glass, porcelain or
other material of low thermal conductivity. Each such plug may
be divided in sectors to prevent random breakage and destruction
(not shown in the drawings). The axle 83 is fitted at its ends
83a and 83b in a static housing 85. This consists of a part on
the right with a similar part on the left, 85b and 85a, and a
central part 85c which is hermetically sealed to the said two
parts by soldered seams 86a and 86b. The whole housing is thus
hermetically sealed. It communicates with the surroundings only
by removal of a screw 87. The extremities of the housing to left
and right are marked 85a' and 85b'. The axle 83 contains a
circular chamber 83c whose geometric axis coincides with axis
C-C. The diameter of this chamber increases from the center
outwards towards the ends of the axle, giving conical inner
surfaces to a part to the left and a part to the right in this
chamber. The chamber communicates with its surroundings only by
removal of screw 88. The chamber contains a small quantity of a
liquid and its vapor, which can be ammonia, propane or any other
suitable substance.
That wall 81 having the greatest diameter rests in a cylinder
89. The wall of this cylinder is thicker and stronger than said
wall 81. The ends of axle 83 have a very slightly smaller
diameter than the inner diameter of the ends 85a' and 85b' of
housing 85. 7The gaps 90 are this very narrow, preferably only a
fraction of a millimeter. Similarly the gap between housing 85c
and cylinder 89 is very small. The volume between the static
housing and the body composed of components 83, 81 and 89
rotating about axis C-C, is suitably filled with hydrogen. The
pressure of this gas is low but not so low that its thermal
conductivity is markedly less than at atmospheric pressure. A
fraction of a torr is the right order of magnitude. The chambers
251, 252 &c, contain the same substances A and B as
previously named in connection with figs. 6, 10, 11, 12 and 13.
Substance A can then appropriately be propane and substance B a
mixture of xenon and sulfur hexafluoride at the stated pressure.
These substances are pumped into each chamber through, a short
channel 82' (fig. 16) which is afterwards closed by welding or
soldering. A pillar 58 and pump 70 such as shown in fig. 13 may
be used here but is not shown since it is similar. assume, new,
for the sake of clarity that the thermodynamic process taking
place in a machine such as that in fig. 15, is a complete
second-order perpetual motion. Reinforced by the previous
arguments, and knowing that the general applicability of
Clausius' theory has not been proved, this assumption, which is
in the interests of simplifying the description to follow, may
be made.
The axle 83 and its constituent bodies 31, 84 and 89 may be set
in rotation by the same mean as the rotor in an ordinary
three-phase induction motor. The stator is fixed round part 85a"
or 85b", In every chamber 25-1 25-2 &c. vapor of substance A
( e.g. propane ) condenses on the floor, that is to say the
surface in the chamber furthest from the axis of rotation C-C,
while liquid of the same substance evaporates from the ceiling
of the chamber, or the surface nearest the axis of rotation. If
the centrifugal force in the outer chamber (253 in fig. 15) is
in the region of 10^5 g and the distance between floor and
ceiling is 1 cm, there can be a temperature difference between
them of 5 to 10 C. This value is dependent upon the mean
temperature in the chamber. If it is too little, another
substance other than propane may be chosen for that particular
chamber. Since the mean temperature is higher in the outer
chambers it will often be advisable to have different substances
A in the different chambers.
A quantity of heat, e.g. Q/2, enters through each part 85a' and
85b', passes easily through the hydrogen in gaps 90 and makes
its way in through both ends of the axle 83. here it causes the
liquid of an appropriate substance e.g. ammonia, to boil. The
ammonia condenses on the central parts or the wall of chambers
83c, wherewith heat at, say, temperature T2, is transferred to
the ceiling of the innermost chamber 25-1. Ammonia - the
condensate - flows back under the action of centrifugal force to
the two ends of chamber 83c. These could be appropriately joined
by a channel, preferably straight and so formed that no more
condensate could accumulate in one end of chamber 83c than in
the other. ( Such a channel is not shown in the drawing ). The
quanta of heat 2x Q/2.., i.e. Q, passes from cylinder 89 through
gap 91 to the housing 85c, and on to where it will be used. The
incoming heat has a lower temperature than the outgoing.
Heat conduction from floor to ceiling within each. chamber (251,
252 &c.) is retarded by the presence of bodies 84, whose low
thermal conductivity requires the heat to travel tie long way
round through, the metal parts 81a.
Suppose that work must be sacrificed to pump liquid A from floor
to ceiling in each of the chambers 25. Such a device can be
constructed with known means in several ways, all simple, for
which reason none are shown in the drawing. It should be added
that if work is required it must be introduced into chambers 25
in such a way that they remain hermetically sealed. This could
be done electrically, magnetically or with the aid of an
elastically resilient membrane. As previously shown, if such
work must be sacrificed, the machine at the very best will only
show an incomplete second-order perpetual notion contrary to
Clausius' theory, otherwise it will constitute a refrigeration
plant or heat pump of greater efficiency than any such known,
but not in contravention with the theory.
It may be mentioned that there is advantage to be gained in
choosing substance A so that its critical temperature is not too
much greater than the temperature in which it will be used, but
is of a technically optimum value above the latter. In this way
total pressure in the chambers 25 will be minimized, whereby the
temperature difference between floor and ceiling will be
maximized.
When substance B is an inert gas such as SF6 and X, it is very
slightly soluble in the liquid substance A, and to a small,
extent will share in A 's cycle, oscillating between two states
of matter, but in the main, the state of matter of substance B
is constant.
The temperature difference won by the process can of course be
used to drive a steam engine which delivers work. If the process
takes place at a very low temperature, say -100 C or lower, and
work is delivered at that mean temperature, heat passes to it
from the ambient temperature T0. This transfer of heat can take
place via another steam engine which will thus also deliver
work.
Finally it must be said that as a matter of course losses occur
in the system, such as through vibration in the centrifuge and
friction in its bearings. There are also conduction losses in
the material. These, and perhaps others could be (as suggested)
so great that the second law of thermodynamics still stands, in
spite of the invention being theoretically correct. The
technical usefulness of the invention will then lie only in the
increased efficiency it can bring to an ordinary refrigerator,
heat pump or thermal power machine. Nevertheless the invention
is highly significant.