Charles
TRIPLER // Jacob Tripler WAINWRIGHT
Liquid Oxygen Engine
A
self-regenerating liquid O2 / CO2 engine...
http://books.google.com/books?id=isOmR5YkpIEC&pg=PA57&lpg=PA57&dq=Tripler+Nature%27s+Secrets&source=bl&ots=R8ez-58sCf&sig=IOJtWS8C4tGu1A6hVVGCd_N5DpE&hl=en&sa=X&ei=fpoRU7T4GIeo2gXShoCYAw&ved=0CDcQ6AEwAQ#v=onepage&q=Tripler%20Nature%27s%20Secrets&f=false
Doomsday
Men: The Real Dr. Strangelove and the Dream of the
Superweapon
by P.
D. Smith

http://www.gutenberg.org/files/33405/33405-h/33405-h.htm
Nature's
Miracles, Volume 1
by
Elisha
Gray
[ Excerpt ]
Mr. Tripler of New York, who has made liquid air in great
quantities, does it substantially as follows: First, he
compresses air to about 2500 pounds to the square inch. Of
course the air is very hot when it is first compressed because
all the air in the tank has been reduced in bulk about 166
times, and all the heat that was in the whole bulk of air is
concentrated into one-166th of the space it occupied before it
was compressed. It is 166 times hotter. There are two sets of
pipes running from the compressor to a long upright tank
called the liquefier. These pipes pass through running water,
so that the compressed air is quickly cooled down to the
temperature of the water (about 50 degrees Fahrenheit). The
pipes — at least one set of them — run the whole length of the
liquefier, and most likely are coiled. This set of pipes
contains the air to be liquefied. A second set of pipes runs
to the bottom of the liquefier, where there is a valve. By
opening this valve a jet of compressed air is allowed to play
on the other set of pipes, when intense cold is produced by
the sudden[Pg 150] expansion of the air. This cold air rushes
up around the pipe containing the air to be liquefied and
escapes at the top, thus absorbing the heat until the
temperature is reduced to 312 degrees below zero. Then the air
liquefies and runs into a receptacle, where it may be drawn
off at pleasure...
The Fallacy of the Second Law of Thermodynamics
and the Feasibility of Transmuting Terrestrial Heat
Into Available Energy
by
Jacob Tripler WAINWRIGHT
[ PDF
]
An Investigation of the Second Law of
Thermodynamics
by
Jacob Tripler WAINWRIGHT
[ PDF
]
The New Thermodynamics
( The Non-Postulated Rationale of Motive Power of Heat
; Also Comprising an Investigation of the Proposition of
Utilizing Heat of Environment as a Substitute for Fuel )
by
Jacob Tripler WAINWRIGHT
[ PDF
]
Perpetual Motion of the Second Kind
Heat from the Atmosphere a Substitute for Fuel
by
Jacob Tripler WAINWRIGHT
[ PDF
]
Patents
Apparat
til at bringe atmosfärisk Luft i Vädskeform.
DK3539
[ PDF ]

Appareil
pour la liquéfaction de l'air
CH19922
[ PDF ]

Vorrichtungen
zur Verflüssigung atmosphärischer Luft.
AT2777
[ PDF ]


Improvements
in or relating to Fluid Pressure Thermo-dynamic Engines.
GB190003158
[ PDF ]
Abstract -- Vapour engines. Relates to engines in
which the working fluid is liquid air, carbon monoxide, or other
substance having a sufficiently-low critical pressure and
temperature. The invention depends upon a revised statement of
the first and second thermodynamic laws, and consists in a
special cycle or system of working, whereby the heat rejected in
the Carnot cycle is intercepted and returned to the source, thus
rendering it possible to convert into motive power the diffused
heat existing in the atmosphere or elsewhere at ordinary
temperatures. Fig. 8 shows in plan a suitable form of
motivepower apparatus for putting the invention into effect, and
Fig. 8<A> shows on larger scale a diagram to illustrate
the heat exchanges in the cycle. The heat to be converted into
motive power is abstracted by the working fluid in the conduit K
from air flowing through the adjacent conduit H. The working
fluid is conveyed from the conduit K to the cylinders E',
E<2>, E<3> of ordinary fluid-pressure engines, and
is thence exhausted by the pipe V into a conduit where it
receives an admixture of gas evaporated at the trap Z. The
mixture is next compressed in the cylinder C', and in flowing
thence gives heat on the one side to the gases entering the
cylinder C' and on the other to the liquid in the conduit K.
This results in liquefaction at the trap Z. Thence liquid is
drawn by the pump P<3> and delivered into the conduit K,
leakage being made up by the pump.
PROVISIONAL
SPECIFICATION.
I have invented a new and useful art, an apparatus, and a method
of operation, all of which pertain to said new art.
This new and useful art consists in utilizing as a source of
energy heat that is common to terrestrial matter and manifested
as temperature condition. A rationale and description here
follows.
Heat engines which operate by the varying condition of a working
fluid, as regards pressure, volume, and temperature, have
properly been divided into two classes.
1st. Those known as heat motor engines, and which by their
operation transform or convert heat into dynamic energy or work.
2nd. Those known as heat pumps, and which are merely motor
engines with a reversed cycle of operation, .and consequently
transform dynamic energy into heat.
Heretofore, an essential to the operation of such motor engines
has been the maintenance of a refrigerator or medium of heat
reception to receive the accumulation of unconverted heat after
passing through the engine.
Whereas, the object of my invention is to dispense with this
refrigerator, either wholely, or partially.
Also, heat engines heretofore made exemplified the following
principles, first enunciated by Sadi Carnot, and now commonly
known as the second law of thermodynamics.
1. All heat motor engines are similar in that they receive heat
from some source, transform part of it into work, and deliver
the remainder to a refrigerator.
2. In the, thermodynamic sense, a heat motor engine is perfect
only when the cycle is reversible, and the efficiency of such an
engine is expressed by an average ratio of loss of temperature
to initial absolute temperature of the heat applied.
Although these two principles or laws apply with correctness to
heat engines heretofore made, I have discovered or observed that
they are not correct for a broader and more comprehensive
treatment of the subject. In fact, they apply only to a specific
type of engine, have not the broad scope of a general nature,
and do not apply to all heat engines. However, they disclose the
present state of the art.
Also, I have discovered or observed that the two above mentioned
laws should be revised so as to read as follows--
1. All heat motor engines are similar in that they receive heat
from some source; transform this heat into work, wholely, or
partially; and deliver what remains to a refrigerator.
2. In the thermodynamic sense, a heat motor engine is perfect
only when the cycle is reversible, and the efficiency of such an
engine is expressed by a ratio of loss of heat to quantity of
heat applied.
An application of my invention consists in combining it. heat
motor engine with a novel apparatus which is merely a part of my
invention and is herein called a potential transformer; in a
manner to intercept the transfer to a refrigerator unconverted
heat that has passed through the motor engine; and return such
intercepted heat to its source, or to the motor engine, by the
expenditure of less dynamic energy than is generated by the
motor engine.
When the heat from a heat motor engine is thus intercepted and
retained, a supply of heat can be utilized at a comparatively
low temperature and from some convenient source such as the
atmosphere, or a body of water, because it is not necessary to
maintain a' refrigerator' for the reception of an accumulation
of ejected heat.
The above rationale of the matter is simple and explicit but
necessitates an explanation in regard to the nature and
properties of the potential transformer.
For a potential transformer ; I have invented a new kind of heat
engine which I term potential transforming engine.
When perfect and reversible in a thermodynamic sense; this kind
of engine can transform a fluid from one potential condition to
an other, without changing the intrinsic or total contained
energy of the fluid ; and consequently at no cost, nor gain, as
regards external work or dynamic energy. Also, its operation can
be regulated so as to transform the potential condition of the
fluid either with cost, or gain, as regards external work; and
consequently with a corresponding changed condition as regards
the intrinsic energy of the fluid.
My invention is based on the feasibility of transmuting or
transforming the fluid from a lesser to a greater potential
condition, accompanied by but a meager increase in intrinsic
energy, for the purpose of affording means to manipulate for a
transmutation of its contained energy into dynamic energy or
work; all in accord with the first law of thermodynamics; and
with the second law, as hereinbefore revised by myself.
In a generic sense; my preferable process or method of operation
for trans- forming a fluid from a lesser to a greater potential
condition; consists in densifying the fluid by abstracting heat
or energy therefrom while maintaining it at conveniently low
pressure, transferring this heat to the thus densified .fluid
while maintaining it at higher pressure, by or through a medium
which is adapted to cause a greater increase in potential
condition than' increase in intrinsic energy considered
proportionately respectively as regards total potential
condition and total contained or intrinsic energy.
A perfect transformation is effected when there results no
change in intrinsic energy. With regard to most fluids ; it may
be remarked that such transformation of the potential condition
results at a corresponding temperature which does not differ
from that corresponding with the initial potential condition,
when the fluid is a perfect gas; and at a changed temperature
when the fluid is in the condition of a mixture of liquid and
saturated gas. With such a mixture, a change in potential
condition corresponding with no change in intrinsic energy
necessitates a change in the relative proportion of liquid to
gas, and consequently a change in its temperature because the
values for specific-heat respectively for the liquid and gas are
not equal.
Referring to the accompanying drawings. For the purpose of
simplicity, these drawings have been made in a conventional
manner, and refinements in matters of detail and scale have been
purposely omitted because the specified parts when taken
separately are well known devices and may be constructed in any
manner that is suitable and known.
Figure 1. shows an elementary type of potential transforming
engine which approximates an ideal in a thermodynamic sense, but
is not so efficient in a mechanical sense. A diaphram capable of
a ready conduction of heat therethrough is shown at A, it
separates the 'Interior of a non-conducting cylinder into the
two .parts B and B B, each of these cylindrical parts are
provided with a non-conducting piston respectively indicated by
C and C C, these pistons are moved to and from the diaphram A by
means of separate racks and pinions respectively shown at D and
D D. For explanatory purposes, crank arms indicated at G and G G
are here shown for operating their respective pinions; and for
the purpose of avoiding prolixity, mechanism for operating these
crank arms has been 'purposely omitted because such explanation
is not essential to a proper understanding of the particular
principles and operation herein involved.



Preparatory to operating; a permanent charge of working fluid is
charged through the conduit E and opened cock F and into the
cylinder B while partially withdrawing the piston C ; the cock F
is then closed to put the engine in condition for operation.
This fluid is only a working fluid and not the fluid to be
treated or transformed. It is preferable that this fluid shall
be the same kind as that which is to be treated. Also, it is
essential that this cylinder shall now be only partially
expanded and thereby permit ample room for subsequent expanding
and contracting of the piston C.
Preferably, a cycle is effected by the following successive
operations.-
1. Starting with the pistons placed as shown in Figure 2.
Through the conduit E E and opened cock F F and while
withdrawing the piston C C to its full extent; a charge of
vaporous, or gaseous fluid to be operated upon or transformed is
receivcd into the cylinder J3 I3. '1'he cock F 1' is then
closed. The pistons have now acquired the positions shown in
Figure 3.
This fluid is thus received in a certain condition as regards
its contained or intrinsic energy, also in a certain potential
condition.
This operation causes the piston C C to effect external work or
dynamic energy by reason of its withdrawal with the fluid
pressure thereon.
2. The piston C C remaining stationary; the working fluid in the
cylinder B is expanded and cooled by a partial withdrawal of the
piston C; at a slow rate of speed so as to make efficient the
accompanying transfer of heat through the diaphram A, from the
fluid in the cylinder B 13 to the fluid in the cylinder B. Tins
operation causes the fluid in the cylinder B B to lessen its
pressure by reason of its loss of heat, while the fluid in the
cylinder B effects work by reason of its expansion and pressure.
The pistons have now acquired the positions shown in Figure 4.
3. With the piston C slowly continuing its course of withdrawal;
the cylinder 13 B is contracted by forcing the piston C C
towards the diaphram A, preferably at constant pressure. The
pistons have now acquired the positions shown in Figure 5. This
operation causes the fluid in the cylinder B to be further
cooled and continue its production of work by reason of its
expansion; while the fluid in the cylinder B B is caused to
contract by reason of the application of external work thereon,
and loss of the heat transferred to the contents of the cylinder
B.
4. With the cylinder B B contracted, and the piston C C
remaining stationary, the cylinder B is contracted by slowly
forcing its piston C back to its initial position. This
operation causes the fluid in the cylinder B B to acquire
temperature and pressure by reason of the compression of fluid
in the cylinder B.
The pistons have now acquired the positions shown in Figure 6.
5. The piston C remaining stationary, the fluid in the cylinder
B B is removed in a transformed condition through the conduit E
E, by opening the cock F F and forcing the piston C C to its
initial position; the pistons have again acquired the positions
shown in Figure 2, and the cycle is completed.
The relative extent of the successive operations which make up a
cycle can be regulated so as to produce any desired degree of
change in potential condition.
The degree of change in intrinsic energy is dependent upon the
degree of pressure under which the treated fluid is densified,
and is an increasing function of this pressure.
This transforming engine posesses the following objectionable
features --
1st. The process is not continuous. 2nd. The engine is not
highly efficient, in a mechanical and constructive sense.
To overcome these objectionable features; I have invented the
type of transforming engine herein shown by Figures. 7A and 7",
taken together as a whole.
I prefer to operate this engine so as to effect a process or
method of operation that is. less generic than that hereinbefore
mentioned, which consists in liquifying the fluid by abstracting
heat or energy therefrom while maintaining it at a relatively
low pressure, and transferring this energy to the liquified
fluid while maintaining it at a higher pressure. With this
particular apparatus'; this process or method of operation is
effected in the more specific manner which consists in
liquifying the fluid by abstracting heat therefrom, while
maintaining it at a relatively low temperature and pressure by a
regenerative action; and transferring this heat to the liquified
liquid while maintaining it at a higher pressure;
A regenerative action is herein understood to be an action in
which there is an interchange of heat between working fluid that
precedes and working fluid that follows in the same routine.
Referring to Figures 7A and 7". In order to clearly show the
operation of this engine and the principles involved; in a
conventional manner the apparatus is shown by these two figures,
when they are taken together as a whole ; certain conduits shown
in one figure connect with and continue as the same conduit in
the other figure, these conduits are respectively indicated by
the same reference letter m each figure, and are the conduits Z,
Y, X, and W; the direction which the fluid is caused to pass
through the various conduits is indicated by conventional
arrows. Figure 7A is a sectional-elevation and shows that
portion of the apparatus where manipulations are effected) as
regards regeneration .of heat. Figure 7" is a plan and shows the
dynamic mechanism, In a conventional manner, and where
desirable, the conduits and engine cylinders are shown to be
surrounded by suitable insulating material to. prevent thermal
inefficiencies by reason of external radiation
In operation, preferably, the fluid to be treated or transformed
is received in a gaseous condition by the conduit U and, passes
therethrough into the conduit Y which extends from the pressure
reducing-valve V to the compression cylinder Cl.
This fluid enters the conduit Y, therein mixes with the current
of fluid passing therethrough from. the valve V, passes from
this conduit into the compression cylinder Cl, is compressed in
this cylinder and delivered therefrom into the conduit Z and
passes therethrough until the valve V is reached at the end of
this conduit Z, by passing through this opened valve it again
enters the conduit Y to again pass therethrough to the
compressor Cl. Through the conduit X, and as explained later, a
portion of the fluid is withdrawn from this circuit.
A diaphram or siding capable of a ready conduction of heat
therethrough is indicated by D, and: separates the above
mentioned conduits Y and Z. The above mentioned compression
effected by the compression cylinder C1 causes a changed
'condition to the fluid, as regards pressure and temperature;
thereby the fluid pressure is increased and also the temperature
of the fluid is increased.
The above mentioned passage of this fluid through the conduit Z,
in this compressed and heated condition, causes. an efficient
regenerative interchange of heat through the diaphram D, and
with the colder fluid passing in an opposite direction in the
adjoining, conduit Y.
This regenerative interchange of heat effects a
self-intensifying frigerative effect, culminating at the valve
V, and causing the fluid in the thus frigefied end of the
conduit Z to condense to the liquid condition. By reason of
gravitation, this frigefied liquid fluid collects in the trap or
upturn at the bottom of the conduit Z, from whence it is forced
through the upward turn of this trap until it reaches the valve
V at the top of this upturn in the conduit. By passing from
thence through the orifice or opened pressure reducing valve V,
the culminating frigefaction is then effected by reason of the
evaporation of this liquid due to its entry into the conduit Y
wherein a lesser pressure is maintained by the combined action
of the valve V and the compressor C 1.
For the purpose of effecting an efficient regenerative
interchange of heat to condense the hold in the conduit Z; the
irigel1ed end of the conduit Y and the adjoining branch from the
conduit Z are purposely , extended upwards and separated by the
heat conducting diaphram, in order that the released liquid from
the valve V may gravitate along the diaphram and toward the
warmer portion of the. conduit and thus insure a rapid,
evaporation and thus prevent .an accumulation of this liquid
after passing through the valve V.
Through the conduit X, a portion of the liquid fluid is
withdrawn from the conduit Z. This withdrawn liquid passes
through the conduit X and enters the pressure pump P 3 wherein
it is put under pressure and ejected therefrom into and through
the conduit W wherein this increased pressure is maintained. The
conduit W is separated from the conduits Z and Y by the diaphram
or siding F which is capable of a ready conduction of heat
therethrough. for a normal working or the apparatus ; the weight
of the liquid fluid thus withdrawn from the conduit % and forced
through the conduit W, and therefrom from this apparatus, is
equal to the weight of gaseous fluid received into the apparatus
through the conduit U. Through the diaphram F, there is an
efficient interchange of heat between the frigefied liquid
passing through the conduit W and the warmer and gaseous fluid
passing under a lesser pressure and in an opposite direction
through the adjoining conduit Z. Thus; the gaseous fluid to be
treated or transformed is received into the apparatus, through
the conduit U is condensed to the liquid condition when it
reaches the frigefactive end of the conduit Z is kept in a
liquid condition and under a greater pressure after passing
through the pump P 3; and while under this pressure and passing
through the conduit W along the diaphram F, it receives heat
abstracted from the gaseous fluid in the adjoining conduit, for
the purpose of aiding the condensation in the conduit Z.
The circuit through the valve V is maintained for the purpose of
producing the self-intensive frigefactive effect, and should .be
operated with sufficient flow, but with little difference in
pressure through this valve; because the efficiency of a
reducing-valve or orifice for . this purpose, in a-thermodynamic
sense, is affected by this difference in pressure and is a
decreasing function thereof.
The counter shaft '1' is driven by any suitable source of
dynamic-energy. By means of suitable regulating devices such as
the belted sprocket cones shown at R and R 3, the counter shaft
T actuates the compressor C 1 and the pressure pump P 3 by means
of their respective crank shaft and piston shown at S 1 and S 3.
These sprocket cones or an equivalent regulating device afford
suitable means for regulating the relative flow through the
compressor C 1 and the pressure pump' P 3. The pressure reducing
valve -NI is of the type used on self-intensive frigefactive
apparatus, and can be readily adjusted to effect any desired
change of pressure.
Thus as preeexited a description of a type of potential
transforming engine that receives a continuous, now of gaseous
fluid to be treated ejects the same in a continuous flow, and in
a changed potential condition in the same sense as hereinbefore
mentioned and described in connection with the apparatus shown
by Figure 1.
Figures 8A and 8B, taken together as a whole, show a preferable
manner of combining the type of potential transforming engine
shown in Figures 7A and 7" with an ordinary type of heat motor
engine. In order to clearly show the operation of this
combination and the principles involved; in a conventional
manner the apparatus is shown by these two figures, when they
are taken together .as a whole; certain conduits shown in one
figure connect with and continue as the same conduit in the
other figure, these conduits are respectively indicated by the
same reference letter in each figure, and are the conduits Z, Y,
X, W, U, and L ; the direction ,which the fluid is caused to
pass through the various conduits is indicated by conventional
arrows. Figure 8, is a sectional elevation. and shows that
portion of the apparatus where manipulations arc effected, as
regards regeneration, and interchange of heat. Figure 8" is a
plan and shows the dynamic mechanism. 1'or the purpose of
convenience, the various parts of the transforming engine, where
shown in this combination, arc respectively indicated by the
same reference letters that are used in Figures 7A and 7". In a
conventional manner and where desirable, the conduits and engine
cylinders are shown to be surrounded by suitable insulating
material to prevent thermal inefficiencies by reason of external
radiation.
The object of this combination is to effect an interception of
the ejected low pressure fluid from the heat motor engine,
transform the potential condition of this ejected fluid by
passing same through the potential transforming engine, return
this transformed and high pressured fluid to the heat motor
engine, increase the intrinsic energy of this returned fluid by
raising its temperature to that of available terrestrial
atmosphere, pass this comparatively heated fluid through the
working cylinder of the heat motor engine, and thus complete the
cycle -in accordance with the principles hereinbefore explained
in the rationale oi the matter as regards utilizing heat that is
common to terrestrial matter for the purpose of transmuting same
into dynamic energy.
In operation, the low pressure gaseous fluid is ejected from tho
working cylinder 2 of the heat motor engine, it is also.ejected
from the working cylinders of the auxiliary motor engines E 1
and E 3, which are directly attached respectively to the
compression cylinder C 1 and the pressure pump P 3 for the
purpose of supplying the necessary dynamic energy to operate
same. This ejected low' pressure fluid is received in the
conduit U and therefrom passes into and through tho various
conduits of the transforming engine in identically the same
manner as was described for Figures 7" and 7". The transformed
and comparatively cold fluid, under high pressure, and in liquid
condition, passes from the conduit W into a continuation of this
conduit shown at K which is separated from the conduit H by a
diaphram or siding J capable of a ready conduction of heat
there- through. Through the conduit H; preferably; is forced a
current of air taken directly from the atmosphere, or a current
of water taken from some large body of same, by means of a
suitable fan or circulating device which it is not necessary to
show here, and is purposely omittcd in order to avoid prolixity.
Through the diaphram J, the current of atmosphere passing
through the conduit H effects an exchange of heat with the
current of colder fluid passing in an opposite direction in the
adjoining conduit K; thereby, the high pressured liquid fluid is
heated and evaporated at high pressure and is forced through the
continuation of this conduit shown at L. From thence, this high
pressure gaseous fluid is withdrawn to operate the before
mentioned motor cylinders E 1, E 2, and E 3. From these motor
cylinders, this fluid is ejected at low pressure into the
conduit U, and thus the cycle is completed.
In order to renew ).he working fluid lost. by leakage, and to
maintain a proper quantity of fluid in the conduit system, the
pump P 4 forces a supply through the conduit N and from thence
into the conduit W. '1'he fluid is supplied to this pump in a
liquified condition, and by means of the conduit M which leads
from some suitable reservoir containing a supply thereof. It is
desirable that this liquid shall be volatile, cheap, readily
available; and non-corrosive. Consequently, I prefer to use
liquid carbonic acid, or liquid air.
The current of atmosphere passing through the conduit H is the
source from which heat is supplied for actuating this whole
system of mechanism. If it were possible to construct the
apparatus so that a perfect efficiency would be obtained from
all of its parts; the heat that disappears or is abstracted from
the current of atmosphere would represent the surplus of dynamic
or mechanical energy developed by the whole apparatus; in other
words, all of the heat taken from this current would be
transmuted into dynamic energy available for any purpose. In a
practical apparatus; the difference between the actual available
dynamic energy and the heat abstracted from the current of
atmosphere represents that portion of the abstracted heat that
is not transmuted into dynamic energy but is dissipated;
consequently, it is desirable that the various parts shall be
constructed so as to effect the greatest possible degree of
efficiency, particularly as regards fluid expansion and fluid
compression. From the pulley U on the shaft of the motor engine
E 2, all available dynamic energy can be taken by means of a
belt or other suitable device and applied to any desired
purpose. For the purpose of effecting a suitable regulation of
the relative flow through the various conduits; the various
pistons are connected one to the other by means, of the, counter
shaft T and the several belted sprocket cones connecting this
counter-shaft with the crank shafts that operate with these
pistons, and shown respectively at R 1, R 2, R 3, and R 4.
For convenience in starting. and stopping the apparatus; valves
for stopping the supply of motive fluid from the conduit L to
the engine cylinders E 1, E 2, . and E 3, are shown respectively
at L 1, L 2, and L 3; clutches for disconnecting ''the torsional
action of the shaft T in regard to the several sets of sprocket
cones are shown respectively at T 1, T 2, '1' 3, and T 4. In
like manner the clutch T 5 disconnects the pulley R 5 which is
used only when starting the apparatus, and as a means, for then
connecting some suitable steam engine or other convenient source
of dynamic energy for the purpose of actuating the counter shaft
and thereby actuate the mechanism of the apparatus until a
normal working is effected; when the apparatus has acquired a
normal working condition, this pulley is disconnected from
the shaft T by this clutch T 5, the auxiliary starting engine is
stopped, and the apparatus continues by its self operating
action.
By utilizing the cooled current of atmosphere ejected from the
conduit H, for frigefactive purposes, the apparatus becomes a
self operating frigefactive engine.
In order to make clear the principles involved ; in Figures 7A
and 8A, it was necessary to adopt a conventional manner of
showing the conduit system. In ' practice, it is desirable to
adopt an annular spiral coil system.
Preferably; this coil system consists of a continuous series of
flat spirals placed one over the other, separated into
successive layers by horizontal partitions of non-conducting
material; and between these horizontal partitions, a spiral
partition of the same material is arranged to form a flat spiral
conduit in each layer, and so as to continue successively
through the series of layers, and to conduct the current of low
pressure fluid; in and along; this insulated conduit 'containing
the current of low -pressure fluid, are placed conduits or pipes
containing respectively the several high pressure fluid
currents, these pipes are made of material which is capable of a
ready conduction of heat therethrough.
Figures 9 and 10 show a, spiral coil constructed on this system,
Figure 9 is a ~sectional plan, Figure 10 is a sectional
elevation, and the same reference letters are used in both of
these figures .to indicate the same parts. In the interior of
the hermetically closed casing C, the high pressure fluid pipes
or conduits 2 and 3 arc contained in the insulated spiral
conduit 1 and there surrounded by the current of low pressure
fluid contained in this conduit 1.
Thus, is presented a description of an operative and practical
apparatus for effecting the purpose. of my Invention.
It is herein understood that any operation mentioned in
connection with my invention may be performed in any manner that
is suitable and known. Also, my invention is not limited to the
use of any particular material in the construction of the
various parts, nor to the use of any particular working fluid,
Also, the application of a multiplex method of combination,
which consists in effecting the same cycle of operation by means
of interdependent action between two or more apparatus, shall be
considered as a mere equivalent of the simple single apparatus
shown.
COMPLETE
SPECIFICATION.
Improvements in or relating to Fluid Pressure Thermodynamic
Engines.
The purpose of this art consists in utilizing as a source of
energy heat that is cpaimmi to terrestrial matter and manifested
as temperature condition. A rationale and description here
'follows.
Heat engines heretofore made which operate by the varying
condition of a working fluid, as regards pressure, volume, and
temperature; have properly been divided into two classes. 1st.
Those known as heat motor engines; and which by' their operation
transform or convert heat into dynamic energy or work.
2nd. Those known as heat pumps, and which are merely motor
engines with a reversed cycle of operation, and consequently
transform dynamic energy into heat ' 'Heretofore, an essential
to the operation of such motor engines. has been the maintenance
of a refrigerator or medium of heat reception to receive the
accumulation of unconverted heat after passing through the
engine. Whereas, . the purpose of my invention is to dispense
with this refrigerator, either wholly, or partially.
Also, heat' engines heretofore made exemplified the following
principles, first enunciated by Sadi Carnot, and now commonly
known as the second law of thermodynamics.
1. All heat motor engines are similar in that they receive heat
from some source, transform part of it into work, and deliver
the remainder to a refrigerator.
2. In the thermodynamic sense, a heat motor engine is perfect
only when the cycle is reversible; and the efficiency of such
perfect engine is expressed by the difference between the
respective temperatures of heat reception and heat rejection,
divided by the absolute-temperature of heat reception, taken as
an average with respect to the units of heat applied and the
portions of these units which are rejected."
Although these two principles or laws apply with correctness to
heat engines heretofore made, I have observed that they are 'not
correct for a broader and more comprehensive treatment of the
subject. In fact, they have not the broad scope of a general
nature, do not apply to all heat engines, and merely apply to
that particular type in which all portions of the working fluid
progress through the same temperature changes with
cOl1unon-to-aI1 corresponding rates of ' change in potential
condition.
Also, I have observed that the two above mentioned laws should
be revised so, as to read. as follows.-
1. All heat motor engines are similar in that they receive heat
from some source ; transform this heat into work, wholely, or
partially; and deliver what remains to a refrigerator.
2. In the thermodynmnic sense, a heat motor engine is possible
only when the cycle is reversible, and the efficiency of such
perfect engine is expressed by a ratio of loss of heat to
quantity of heat applied.
A preferable application of my Invention consists in combining a
heat motor engine, with a novel apparatus which is merely a part
of my invention and is herein called a potential transformer; in
a manner to intercept, the unconverted heat that has passed
through the motor engine, and prevent the transfer of same to. a
refrigerator; and return such intercepted heat to its source, or
to the motor engine, by the expenditure of less dynamic energy
than is generated by the motor engine. When the heat from a heat
.motor engine is thus intercepted and returned, a. supply of
heat can lie utilized at a comparatively low temperature and
from, some convenient source such as the atmosphere, or a
body of water, because, it is not necessary to maintain a
refrigerator for the reception of an accumulation of ejected
heat..
The above rationale of the matter is simple and explicit but
necessitates an explanation in regard to the nature and
properties of the potential transformer.
For a potential transformer, I have .invented a new kind of heat
engine which.
I term potential transforming engine. Its function, as applied
to my invention in. a preferable manner, is to transform or
transmute the potential condition of the working fluid after
passing through the motor engine, and thus dispense with the
necessity of maintaining an external refrigerator for receiving
the accumulation of such ejected heat. The preferable manner in
which this result is attained consists in reducing the potential
condition of the fluid to be treated, by abstracting heat from
same; when this fluid has thus acquired a. comparatively low
potential condition and consequently is not capable of
developing; much latent beat by. a change in condition as
regards density and pressure, its condition is then caused to be
changed by a meager external application of dynamic energy or
work; the above mentioned 'abstracted heat is then returned to
the thus densified fluid held under an increased pressure and
thereby causes a transmutation to the condition of greater
potential by reason of the returned heat existing in the same
but more densified fluid; and effecting this abstraction and
return of heat by a regenerative action which is made effective
by causing different portions of regenerative fluid to progress
through the same temperature changes with corresponding rates of
change in potential condition that differ.
When perfect and reversible in a thermodynamic sense, this kind
of engine' can transform a fluid from one potential condition to
an other, without changing the total contained energy of the
fluid ; and consequently at no cost, nor gain. as regards
external work or dynamic energy. Also, its operation can be
regulated so as to transform the potential condition of the
fluid either with cost, or with gain, as regards external work;
and consequently with a corresponding. changed condition as
regards the total contained energy of the fluid.
My invention is based on the feasibility of transmuting or
transforming the fluid from a lesser to a greater potential
condition, accompanied by but a meager increase in total
contained energy, for the purpose of affording means to
manipulate for a transmutation of its contained energy into
dynamic energy or work; all in accord with the first law of
thermodynamics; and with the second law of thermodynamics, as
hereinbefore revised by myself.
In a generic sense ; my preferable process for effecting such
transformation consists in lessening the potential condition of
the fluid by abstracting heat from same ; when the fluid has
thus acquired a, lowered potential condition, effecting a
changed condition. by Increasing its density, or fluid pressure,
or both, by an external application of force; returning said
abstracted heat to the thus densified fluid held under increased
pressure ; and effecting this abstraction and return of heat by
a regenerative action in which different portions of
regenerative fluid are caused to progress through some identical
temperature changes with corresponding rates of change in
potential condition that differ.
A perfect transformation of the potential condition is effected
when there results no change in the total contained energy. With
regard to most fluids ; it may be remarked that such
transformation results at a temperature which does not differ
from that corresponding with the initial potential condition,
when the fluid is a perfect gas; and at a changed temperature
when the fluid is in the condition of a mixture of liquid and
saturated gas. With such a mixture, a change in potential
condition corresponding with no change in total contained energy
necessitates a change in the relative proportion of liquid to
gas, and consequently a change in its temperature because the
values for specific-heat respectively for the liquid and gas are
not equal.
The drawings filed with my Provisional Specification are herein
referred' to. in all cases. For the purpose of simplicity/these
drawings have been made in: a conventional manner, and
refinements in matters of detail and scale have been purposely
omitted because the. specified parts when taken separately are
well known devices and may be constructed in any manner that is
suitable and known.
Figure 1 shows an elementary type of potential transforming
engine which approximates an ideal in a. thermodynamic sense,
but is not so efficient in a' mechanical sense. Figures 2; 3, 4,
5, and 6, are merely of the nature of a diagram, and are for the
purpose of explaining the successive operations that make up a
cycle. A diaphram capable of a ready conduction of heat
therethrough is shown at A, it separates the interior of a
non-conducting cylinder into the two parts B and 13 B, each of
these cylindrical parts are provided with a non-conducting
piston respectively indicated by C and C C, these pistons are
moved' to and from the diaphram A by means of separate racks and
pinions respectively shown at D and D D. For explanatory
purposes, crank arms indicated at G and G G are here shown for
operating their respective pinions ; and for the purpose of
avoiding prolixity, mechanism for operating these crank arms has
been purposely omitted because such explanation is not essential
to a proper understanding of the particular principles and
operation herein involved.
Preparatory to operating, a permanent charge of working fluid is
charged' through the conduit E and opened cock F and into the
cylinder B while partially withdrawing the piston C; the cock F
is, then closed to put the engine in condition for operation.
This fluid is manipulated as a portion of the working fluid and
is not the fluid to be treated or transformed. It is preferable
that this fluid shall be the same kind as that which is to be
treated, but in more densified condition. It is essential
that this cylinder shall now be only partially expanded and
thereby permit ample room for subsequent expanding 'and
contracting by means of the 'piston C.
Preferably, a cycle is ejected by the following successive
operations.-
1. Starting with the pistons placed as shown in Figure 2.
Through the conduit E E and opened, cock F and while withdrawing
the piston C C to its full extent ; a charge of vaporous, or
gaseous fluid to be operated upon or transformed, -is received
into the cylinder B B. The cock F F is then- closed. The pistons
have now acquired the positions shown in Figure 3. This
operation causes an interchange of heat through the diaphram A
until a common temperature is acquired in both cylinders, and
also causes the piston C C to effect external work or dynamic
energy by reason of its withdrawal with the fluid pressure
thereon..
2. The piston C C remaining stationary; the working fluid in the
cylinder B is expanded and cooled by a partial withdrawal of the
piston C ; at a slow rate of speed' so as to make efficient the'
accompanying transfer of heat through the diaphram A, from the
fluid in the cylinder B B to the fluid in the cylinder B.
This operation causes the-fluid in the cylinder B 13 to lessen
its pressure,by reason of its loss of heat, while the fluid in
the cylinder B effects work by reason of its expansion and
pressure. The pistons have now acquired the positions shown in
Figure 4.
3. With the piston C slowly continuing its course of withdrawal,
the cylinder , B B is contracted by forcing the piston C C
towards the diaphram A, preferably at constant pressure. The
pistons have now acquired the. positions' shown in . Figure 5.
This operation causes the fluid in the cylinder B to be further
cooled and continue its production of work by reason of its
expansion; while the fluid in the cylinder B B is caused to
contract by reason of the application of external work thereon,
and loss of the heat transferred to the contents of the cylinder
B.,
4. With the cylinder B B contracted, and the piston C C
remaining stationary; the cylinder B is contracted by slowly
forcing its piston C back to its initial position. This
operation causes the fluid in the cylinder B B to acquire
temperature and pressure by reason of the compression of fluid
in the cylinder B.
The pistons have . now acquired the positions shown in Figure 6.
5. The piston C remaining stationary, the fluid in the cylinder
B B is removed in a transformed condition through the conduit E
E, by opening the cock F F and forcing the piston C C to its
initial position; the pistons have again acquired the positions
shown in-Figure 2, and the cycle is completed.
The relative extent of the successive operations which make up
this single cycle can, be regulated so as to produce any desired
degree of change in potential condition. The degree of increase
in total contained energy is dependent upon the degree of
pressure under which the treated fluid is densified, and is an
increasing function of this pressure.
A more controllable result can be attained by a cycle which
consists in one or more repetitions of such single cycle
modified by retaining the fluid in the cylinder 13 B for the
repeated treatment. '1'he relative extent of the successive.
operations can be regulated to produce any desired change in
potential condition, and any desired change In total contained
energy.
This transforming engine possesses the following objectionable
features
1. The process is not continuous.
2nd. the engine is not highly efficient, in a mechanical and
constructive sense.
To overcome these objectionable features; I have invented the
type of transforming engine herein shown by Figures 7 any 7",
taken together as a whole. I prefer to operate this engine so as
to effect a process or method of operation that is less generic
than that hereinbefore mentioned, which definiteness consists in
liquifying the fluid by abstracting heat or energy therefrom
while maintaining it at a relatively low pressure, and
transferring this heat to the thus liquified fluid while
maintaining this liquified fluid at a greater pressure. With
this particular apparatus; this process or method of operation
is effected in, the more specific manner having definiteness as
regards the liquifaction of the fluid by abstracting heat or
energy therefrom while maintaining it at a relatively low
temperature and pressure by a regenerative action, and
transferring this heat to the thus liquified fluid while
maintaining this liquified fluid at a greater pressure.
Referring to Figures 7A and 7B. In order to clearly show the
operation of this engine and the principles involved; - in a
conventional manner the apparatus. is shown by these two
figures, when they are taken together as a whole; certain.
conduits shown in one figure connect with and continue as the
same conduit. in the other figure, these conduits are
respectively indicated by the same reference letter in each
figure, and are the conduits Z, Y, X, and W; the direction which
the fluid is caused to pass through the various conduits is
indicated by conventional arrows. Figure 7A is a
sectional-elevation and shows that portion of the apparatus
where manipulations are effected as regards interchange of heat.
Figure 7" is a plan and shows the dynamic mechanism. In a
conventional manner, and where desirable, the conduits and
engine cylinders are. shown to be surrounded by suitable
insulating material to prevent thermal inefficiencies by reason
of external radiation.
In operation, preferably, the fluid to be treated or transformed
is received in. a gaseous condition by the conduit U and passes
therethrough into. the conduit Y which extends from the pressure
reducing-valve V to the compression cylinder.Cl.
This fluid enters the conduit Y, therein mixes with- the
current, of, fluid -passing therethrough from the valve V,
passes from this conduit into the compression cylinder Cl, is
compressed in this cylinder and delivered therefrom, into the
conduit Z and passes therethrough until the valve .Y is reached
at the end of this conduit Z, by passing through this opened
valve it again enters the conduit Y to again pass therethrough
to the compressor Cl. Through the conduit X, and as explained
later, a portion of the fluid is withdrawn from this circuit.
A diaphram or siding capable of a ready conduction of heat
therethrough is indicated by D, and separates the above
mentioned conduits Y and Z. The above mentioned compression
ejected by the compression cylinder C causes a changed condition
to the fluid, as regards pressure and temperature; thereby the
fluid pressure is increased and also the temperature of the
fluid is increased.
The above mentioned passage of this fluid through the conduit Z,
in this compressed and heated condition, causes an efficient
regenerative interchange of heat through the diaphram D, with
the colder fluid passing in an opposite direction in the
adjoining conduit Y.
This regenerative interchange of heat effects a,
self-intensifying frigefactive effect, culminating at the valve
V, and causing the fluid in the thus frigefied end of the
conduit Z to condense to the liquid condition. By reason of
gravitation, this frigefied liquid fluid collects in the trap or
upturn at the bottom of the conduit Z, from whence it is forced
through the upward turn of this trap until it reaches the valve
V at the top of this upturn in the conduit. By passing from
thence through the orifice or opened pressure reducing valve V,
the culminating frigefaction is then effected by reason of the
evaporation of this liquid due to its entry into the conduit Y
wherein a lesser pressure is maintained by the combined action
of the valve V and the compressor C 1.
Through the conduit X, a portion of the liquid fluid is
withdrawn from the conduit Z. This withdrawn liquid passes
through the conduit X and enters the pressure pump P 3 wherein
it is put under pressure and ejected therefrom into and through
the conduit W wherein this increased pressure is maintained. The
conduit it' is separated from the conduits and Y by the diaphram
or siding 1' which. is capable of a ready conduction of heat
therethrough.
For a normal working of the apparatus; the weight of the liquid
fluid thus withdrawn from the conduit Z and forced into the
conduit W, is equal to the weight of gaseous fluid received into
the apparatus through the conduit U.
Through the diaphram F, there is an efficient interchange of
heat between the frigefied liquid passing through the conduit W
and the warmer and gaseous fluid passing under a lessor pressure
and in an opposite direction through the adjoining conduit Z.
Thus; the gaseous fluid to be treated or transformed is received
into the apparatus, through the conduit U ; is condensed to the
liquid condition when it reaches the frigefactive end of the
conduit Z;is kept in a. liquid condition and under a greater
pressure after passing through the pump P 3 and while under this
pressure and passing through the conduit W along the diaphram
if, it receives heat abstracted from the gaseous fluid in the
adjoining conduit, thereby aiding the condensation in the
conduit Z.
The circuit through the valve Y is maintained for the purpose of
producing the self-intensive frigefactive effect, and should be
operated with sufficient flow, but with little difference in
pressure through this valve; because the efficiency of a
reducing valve or orifice for this purpose, in a thermodynamic
sense, is affected by this difference in pressure and is a.
decreasing function thereof.
The counter shaft T is driven by any suitable source of dynamic
energy. By means of suitable regulating devices such as the
belted sprocket cones shown at R 1 and R 3, the counter shaft T
actuates the compressor C 1 and the pressure pump P 3 by means
of their respective crank shaft and piston shown at S 1 nnd S 3.
These sprocket cones or an equivalent regulating device afford
suitable means for regulating the relative flow through the
compressor C 1 and the pressure pump P 3. The pressure reducing
valve V is of the type used on self-intensive frigefactive
apparatus, and can be readily adjusted to effect any desired
change of pressure.
Thus is presented a description of a type of potential
transforming engine that receives a continuous flow of gaseous
fluid to be treated; ejects the same in a continuous now, and in
a changed potential condition in the same sense as hereinbefore
mentioned and described in connection with the apparatus shown
by Figure 1. Also, it may be remarked that with each of these
devices it is desirable to densify the treated fluid at a degree
of pressure that is below but somewhat near its
critical-pressure.
Figures 8A and 8B, taken together as a whole, show a preferable
manner of combining the type of potential transforming engine
shown in Figures 7A and 7D, with an ordinary type of heat motor
engine. In order to clearly show the operation of this
combination and the principles involved ; in a conventional
manner the apparatus is shown by these two figures, when they
are taken together as a whole; certain conduits shown in one
figure connect with and continue as the same conduit in the
other figure, these conduits are respectively indicated by the
same reference letter in each figure, and are the conduits Z, Y,
X, W, U, and L; the direction which the fluid is caused to pass
through the various condiii4g is indicated by conventional
arrows. Figure S' is a sectional elevation and shows that
portion of the apparatus where manipulations are effected as
regards interchange of heat. Figure 8B is a. plan and shows the
dynamic mechanism. For the purpose of convenience, the various
parts of the transforming engine, where shown in this
combination, are respectively indicated by the same reference
letters that are used in Figures 7A and 7B. In a conventional
manner and where desirable, the conduits and engine cylinders
are shown to be surrounded by suitable insulating material to
prevent thermal inefficiencies by reason of external radiation.
The object of this combination is to effect an interception of
the ejected low pressure fluid from tho heat motor engine,
transform the potential condition of this ejected fluid by
passing same through the potential transforming engine, return
this transferred and high-pressured fluid to the heat motor
engine, increase the total contained energy of this returned
fluid by applying heat taken from available terrestrial
atmosphere, pass this comparatively heated fluid through the
working cylinder of the heat motor engine, and thus complete the
cycle in accordance with the principles hereinbefore explained
in the rationale of the matter as regards utilizing heat that is
common to terrestrial matter for the purpose of transmuting same
into dynamic energy.
In operation, the low pressure gaseous fluid is ejected from the
working cylinder E 2 of the heat motor engine, it is also
ejected from the working cylinders of the auxiliary motor
engines E I and E 3 which are directly attached respectively to
the compression cylinder 0 1 and the pressure pump P 3 for the
purpose , of supplying the necessary dynamic energy to operate
same. This ejected low pressure fluid is received in the conduit
U and therefrom passes into and through the various conduits of
the transforming engine in identically the same manner as was
described for Figures 7A and 7B. The transformed and
comparatively cold fluid, under high pressure, and preferably in
liquid condition. -passes from the conduit W into a continuation
of this conduit shown at K which is separated from the conduit H
bv a diaphram or siding J capable of a ready conduction of heat
therethrough. Through the conduit H; preferably: is forced a
current of air taken directly from the atmosphere, or a current
of water taken from some large body of same, by means of a.
suitable fan or circulating device which it is not necessary to
show here and is purposely -omitted in order to avoid prolixity.
Through the diaphram T the current of atmosphere passing-
through the conduit H effects an exchange of heat with the
current of colder fluid passing in an opposite direction in the
adioining conduit K; thereby, the hijyh pressured fluid is
heated and expanded, or evaporated, at high pressure, and is
forced through the continuation of this conduit shown at L. From
thence, this high pressured Pa.aeous ftniel is withdrawn to
operate the before mentioned motor cylinders E 1. E 2, and E 3.
From the motor cylinders, this fluid is ejected at low pressure
into the conduit TT, nnll thus the cycle is completed. In order
to, rencw the working fluid lost by leakage, and to maintain a
proper quantity of fluid in the conduit system, the pump P 4
forces a supply through the conduit N and from thence into the
conduit W. The fluid is supplied to this pump in a liquified
condition, and by means of. the conduit M which leads from some
suitable reservoir containing a supply thereof. It .is desirable
that this liquid shall be non-corrosive, cheap, readily
obtained, and .possess a critical temperature and a
critical-pressure that are conveniently low. Consequently, I
prefer to use liquid air, or liquid carbon monoxide.
The current of atmosphere passing through the conduit H is the
source from which heat is supplied for actuating this whole
system of mechanism. If .it were possible to construct the
apparatus so that a perfect efficiency would be obtained from
all of its parts; the heat that disappears or is abstracted from
the current of atmosphere would represent the surplus of dynamic
or mechanical energy developed by the whole apparatus; in other
words, all of the heat taken from this current would be
transmuted into dynamic energy available for any purpose. In a
practical apparatus; the difference between the actual,
available dynamic energy and the heat abstracted from.the
current of atmosphere represents that portion of the abstracted
heat that is not transmuted into dynamic energy but is
dissipated; consequently, it is desirable that-the various parts
shall be con- 8li'uctqd so .as to . effect the greatest possible
degree of efficiency, particularly as regards fluid expansion
and fluid compression. From the. pulley O on the shaft of the
motor engine E 2, all available dynamic energy can be taken by.
means of a belt or other suitable device and applied to any
desired purpose. For the purpose of effecting a suitable
regulation of the relative flow through the.various conduits;
the various pistons are connected one to the other by means of
the counter shaft T and the several belted sprocket cones
connecting this counter shaft with the crank shafts that operate
with these pistons, and shown respectively at R, R 2, R 3, and R
4.
For convenience in starting and stopping the apparatus; valves
for stopping the supply of motive fluid from the conduit L to
the engine cylinders E 1, E 2, and E 3, are shown respectively
at, L 1, L 2, and L 3 ; clutches for disconnecting the torsional
action of tile shaft '1' in regard to the several sets of
sprocket cones are shown. respectively at T l, '1' 2, '1' 3,'
and '1' 4. In like manner the clutch '1" disconnects the pulley
R 5 which is used only when starting the apparatus, and as a
means for then connecting some suitable steam engine or. other
convenient source of dynamic, energy for the purpose of
actuating the counter shaft and thereby actuate the mechanism of
the apparatus until a .normal working is effected ; when the
apparatus has acquired a normal working condition, this pulley
is disconnected from the shaft T by this clutch T 5, the
auxiliary starting engine is stopped, and the apparatus
continues its action by reason of the self operating feature...
By utilizing the cooled current of atmosphere ejected from the
conduit H, for frigefactive purposes, the apparatus becomes a
self operating frigefactive engine.
In order to make clear the principles involved, in Figures 7A
and 8A it was necessary to adopt a conventional manner of
showing the conduit system. In .practice it is desirable to
adopt an annular spiral coil system.
Preferably; this coil system consists of a continuous series of
flat spirals placed one over the other, separated into
successive layers by horizontal partitions of non-conducting
material; and between these horizontal partitions, a spiral
partition of the same material is arranged to form a flat spiral
conduit in each layer, so as to continue successively through
the series of layers, and to conduct the current of low pressure
flu14, In and along this insulated conduit the current of
lower pressured fluid are placed conduits or pipes containing
respectively the several higher pressured fluid currents, these
pipes are made of material which is capable of a ready
conduction of heat therethrough.
Figures 9 and 10 show a spiral coil cont1'lcted on this system,
Figure 9 is a sectional plan, Figure 10 is a sectional
elevation, and the same reference letters are used in both of
these figures to indicate same parts. In the interior of the
hermetically closed casing C the higher pressured fluid pipes or
conduits 2 and 3 are contained in the insulated spiral conduit 1
and there surrounded by the current of lower pressured fluid
contained in this conduit 1.
Thus, is presented a description of an operative and practical
apparatus for effecting the purpose of my invention. ' A
self-intensifying heat engine is herein understood to be a heat
engine in which the action of the cycle tends to intensify or
extend the limit of the working range of temperatures, when
interchange of heat with external sources is dispensed with. A
regenerative action is herein understood to be an interchange of
heat between fluid tha,t precedes and fluid tha,t follows in the
same routine, or the abstraction and subsequent return of heat
to and from the same fluid.
Also, it is understood that any operation herein mentioned in
connection with my invention may be performed in any manner that
is suitable and known.
Also; my invention is not limited to the use of any particular
material in the construction of the various parts; any
particular working fluid; nor any particular type of engine or
device for converting fluid pressure and expansion into dynamic
energy, particularly as regards the application of fluid jets
and turbines to such purposes. Also, the application of a
multiples method of combination, which consists in effecting the
same cycle of operation by means of inter-dependent action
between two or more apparatus, shall be considered as a mere
equivalent of the simple single apparatus shown.