(19) |
![](https://data.epo.org/publication-server/img/EPO_BL_WORD.jpg) |
|
(11) |
EP 0 003 355 B1 |
(12) |
EUROPEAN PATENT SPECIFICATION |
(45) |
Mention of the grant of the patent: |
|
26.05.1982 Bulletin 1982/21 |
(22) |
Date of filing: 25.01.1979 |
|
|
(54) |
Unidirectional energy converter engine
Energiewandler mit gleichbleibender Drehrichtung
Moteur unidirectionnel convertisseur d'énergie
|
(84) |
Designated Contracting States: |
|
DE FR GB |
(30) |
Priority: |
27.01.1978 US 872848 11.01.1979 US 2411
|
(43) |
Date of publication of application: |
|
08.08.1979 Bulletin 1979/16 |
(71) |
Applicant: BATTELLE DEVELOPMENT CORPORATION |
|
Columbus
Ohio 43201 (US) |
|
(72) |
Inventors: |
|
- Fawcett, Sherwood L.
Columbus
Ohio 43221 (US)
- Anno, James N.
Cincinnati
Ohio 45244 (US)
|
(74) |
Representative: Rupprecht, Klaus, Dipl.-Ing. |
|
Kastanienstrasse 18 61476 Kronberg 61476 Kronberg (DE) |
|
|
|
Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
|
[0001] As is known, systems have been proposed in the past to convert one type of energy
into another type by using various thermodynamic cycles, such as the Otto, Rankine,
and Brayton cycles. Most of these systems employ reciprocating pistons; although some,
such as those shown in Dutch Patent 65,164 and German Patent 842,845, employ one or
more pistons which are forced to travel in one direction in a continuous closed-loop
by the expansion of a gaseous medium in one region of the closed loop. In the closed-loop
systems of the prior art, each piston is coupled to a mechanical element which moves
with it, the kinetic energy of the moving piston being converted directly into mechanical
energy. These systems, however, require complicated mechanisms for coupling the piston
or pistons to an associated mechanical element.
[0002] In U.S. Patent No. 3,859,789, a method and apparatus are disclosed for converting
one form of energy into another form of energy through the use of a single continuous,
closed-loop passageway containing a plurality of freely-movable, mechanically-unrestrained
bodies which travel around the passageway in one direction only. Acceleration of the
bodies is effected by means of an expanding fluid medium supplied externally to the
closed-loop passageway or by means of internal combustion. The kinetic energy of the
bodies is extracted by a variety of methods including causing the propelled bodies,
when formed from magnetically-permeable material, to pass through an electromagnetic
field to convert some of the kinetic energy into electrical energy. Kinetic energy
is also extracted by compressing the fluid between the bodies to provide energy in
the form of compressed fluid. When the expansion of a gas is used to propel the bodies
in this type of energy converter, the bodies pass through a region where the gas between
them is compressed preparatory to a succeeding cycle of operation. In all such prior
art systems of this type, the closed-loop passageway itself remains stationary.
[0003] It is an object of the present invention to provide an improved unidirectional energy
converter in the form of a rotating engine wherein pistons are accelerated around
a closed-loop passageway mounted on a rotating platform. Energy in the form of an
expanding gas is converted into kinetic energy which is then converted into potential
energy by working the pistons against the centrifugal force of the rotating platform.
Finally, the pistons are moved radially outwardly on the platform under the influence
of centrifugal force; and their energy is converted into rotational energy which is
used to rotate the platform and provide useful work.
[0004] In accordance with one embodiment of the invention, the apparatus for converting
a first form of energy into a second form of energy includes a platform carried by
support means for rotation about a central axis. At least one continuous, closed-loop
passageway is carried by the platform and contains a plurality of freely-movable pistons.
Means are provided for applying a force to successive ones of the pistons in a first
region of the passageway extending along the periphery of the rotating platform to
thereby propel each body in one direction around the passageway and increase its kinetic
energy. In a second region of the passageway which curves inwardly toward the center
of the platform the pistons, after being propelled, are caused to work against centrifugal
force to thereby convert the kinetic energy of the pistons into potential energy as
they approach the center of rotation of the platform. In a third, radially-extending
region of the passageway centrifugal force acts on the pistons causing them to move
radially outwardly back to the first region. In the third region the energy of the
outwardly-moving pistons is converted into rotational energy which is then coupled
to the platform to rotate the same.
[0005] Preferably, in the embodiment of the invention just described, there are two closed-loop
passageways located at diametrically-opposite locations on the rotating platform.
Each passageway includes two arcuate segments, each having a different radius, and
a linear segment interconnecting the two arcuate segments. When the apparatus of the
invention is adapted for operation according to the Rankine cycle, a rotary union
communicates with a duct extending coaxially along a support shaft for the platform;
while conduits extend from the duct to the first region of each passageway to supply
steam or the like as the expansible fluid from a stationary boiler. A second duct
can be connected by conduits to each second region of the passageways for exhausting
steam therefrom. The rotatable means for each passageway includes at least one but
preferably two pocketed wheels disposed at opposite sides of the passageway for receiving
the pistons as they are moved radially outwardly along the linear regions of the passageways
under the influence of centrifugal force. These pocketed wheels also serve to feed
the pistons into the first region where they are propelled by expansion of a fluid.
The pocketed wheels are secured to arbors which are in, turn, rotatably supported
by the platform and coupled by gears in a stationary gear which is coaxial with the
central axis of the platform. The rotational movement of the pocketed wheels is thereby
converted into rotational movement of the platform. Typically, the pocketed wheels
at opposite sides of the linear region of the passageway include circumferentially-spaced
peripheral pockets to pass the pistons between the wheels. Alternatively, the wheels
may have spaced-apart magnets on their peripheries, all of the magnets carried by
one wheel having magnetic south poles and those carried by the other wheel having
magnetic north poles at their respective peripheries.
[0006] When the aforesaid embodiment of the invention is adapted for operation according
to the Brayton cycle, liquid fuel is fed from a stationary tank through a coaxial
pipeline to the rotating platform. An inlet manifold and an exhaust manifold communicate
with only part of opposite sides of the aforesaid second arcuate region of each passageway.
The remaining part of the second region is used to compress between the bodies. The
compressed air is then fed to a combustion chamber where it is heated and used to
propel the pistons in the first region of each passageway.
[0007] In another embodiment of the invention, a single passageway rather than two, is provided
on the rotatable platform. In this case, the passageway has straight portions on opposite
sides of the central axis of rotation of the platform, the straight portions being
interconnected at their ends by curved portions, also on opposite sides of the central
axis of rotation of the platform. Means are provided for applying a force to successive
ones of the pistons in one region in each of said straight portions of the passageway
to propel them inwardly on the rotating platform against centrifugal force, the pistons
being moved radially outwardly in another region of each of the straight portions
under centrifugal force. The means for converting the energy of the pistons into rotational
energy comprises pocketed wheels having their peripheries coinciding with the inner
peripheries of the curved portions of the passageway to convert the energy of the
pistons in the curved portions, which have been moved outwardly under centrifugal
force, into rotational energy. As in the previous embodiment, these pocketed wheels
are coupled through a gear train mounted on the platform which meshes with a stationary
gear carried beneath the platform to cause rotation of the platform about its rotational
axis.
[0008] The above and other objects and features of the invention will become apparent from
the following detailed description taken in connection with the accompanying drawings
which form a part of this specification, and in which:
Fig. 1 is a plan view of the rotating engine according to one embodiment of the present
invention for converting, according to the Rankine cycle, one form of energy into
a second form of energy;
Fig. 2 is an enlarged plan view of the pocketed wheels of the invention for feeding
pistons forming part of the apparatus shown in Fig. 1;
Fig. 3 is a cross-sectional view taken along line III-III of Fig. 2;
Fig. 4 is a sectional view taken along line IV-IV of Fig. 1;
Fig. 5 is a sectional view taken along line V-V of Fig. 4;
Fig. 6 is a plan view similar to Fig. 1 but illustrating the apparatus of the present
invention for operation according to the Brayton cycle;
Fig. 7 is an illustration, in partially broken- away plan view, of another embodiment
of the invention wherein a single loop passageway extends around the axis of rotation
of a platform, there being two regions in the passageway where pistons are propelled
against centrifugal force;
Fig. 8 is a side view of the embodiment of the invention shown in Fig. 7; and
Figs. 9A and 9B illustrate alternative forms of the pistons which can be used in the
two embodiments of the invention.
[0009] With reference now to Figs. 1 to 5, the rotating engine shown includes a platform
11 in the form of two disc-shaped plates 11 A and 11 B (Figs. 3 and 4) with mutually-engaging
face surfaces maintained in contact by fastening members, not shown. The platform
is adapted to rotate about a central vertical axis 12 (Fig. 4) and is secured by fasteners
to a centrally- arranged shaft 13 extending downwardly from the bottom of plate 11
B of the platform. Bearings 14 support the shaft 13 for rotation within a support
frame 15. A stationary main gear 16 is keyed to a journal surface provided on frame
15. As is perhaps best shown in Figs. 1 and 5, the diameter of gear 16 is selected
so that it meshes with two separate gear trains, each being identical and including
a first idler gear 17 and a second idler gear 18. The gears 17, for example, are supported
by bearings on arbor shafts 19 (Figs. 4 and 5) carried by plate 11 B.
[0010] As shown in Figs. 2, 3 and 5, each idler gear 18 is secured to the lower end of an
arbor shaft 20 which extends through an opening in the platform 11. Above gear 18,
the arbor shaft 20 carries a timing gear 21 located within a recess in plate 11 B.
In this recess, the timing gear 21 meshes with a second timing gear 22 secured to
an arbor shaft 23. Both arbor shafts 20 and 23 rotate in suitable bearings supported
by the platform as shown. The upper ends of arbor shafts 20 and 23 carry pocketed
wheels 24 and 25, respectively. As shown in Figs. 1 and 2, the pocketed wheels have
circular recesses uniformly spaced about their outer periphery which are adapted to
received in succession pistons 27 which are typically spheroids.
[0011] The respective pairs of pocketed wheel assemblies 24, 25 are arranged at generally,
diametrically-opposite locations on the platform 11. Each pair of pocketed wheels
forms part of an independent, unidirectional energy converter loop that includes a
continuous, closed-loop passageway 30. The two loop passageways take the form of machined
slots in each of the mutually-engaging face surfaces of the plates 11A and 11B of
the platform 11. In other words, the passageway 30 is defined by aligned slots having
walls which are preferably smooth and formed from metal. The passageways are located
at mutually-exclusive sectors which lie at opposite sides of a vertical plane passing
through the axis 12. The pistons 27 are freely-movable bodies which pass in succession
through each passageway. The tolerances or clearances between the surfaces of the
pistons 27 and the walls of the passageway 30 are such as to permit the pistons to
move freely therealong. Fluid flow past the pistons within the passageways is substantially
prevented since the pistons have a spherical shape which is substantially complementary
to the cross-sectional shape of the passageways. If desired, a tube can be used as
a liner in each passageway.
[0012] As shown in Fig. 1, each passageway 30 is made up of three regions 32, 33 and 34.
Region 32 extends along the periphery of the platform 11 for a distance of approximately
90°. This region forms an expanding section wherein a fluid medium, such as steam,
is used to freely accelerate the pistons in succession. Region 33 is curved inwardly
toward the center of rotation of the platform 11 and is provided with one or more
ports 31 in the upper plate 11 A to bleed off fluid between successive pistons. It
should be understood, however, that the ports 31 could be replaced by a plenum chamber
which collects the steam, condenses and returns it to a boiler.
[0013] As the pistons 27 move radially inwardly in the region 33, they must work against
centrifugal force; and in this process the kinetic energy of the moving pistons in
region 32 is converted into potential energy as they approach the center of rotation
of the platform. Finally, when the pistons are in region 34 in closely-abutting relationship,
they are urged radially outwardly under the influence of centrifugal force. In this
process, they pass through the pocketed wheels 24 and 25, thereby inducing rotation
which is transmitted through idler gears 18 and 17 to central gear 16, thereby causing
the entire platform 11 and the elements carried thereby to rotate in the direction
indicated by the arrow A in Fig. 1. As the pocketed wheels 24 and 25 rotate, they
feed successive ones of the pistons 27 to the first or expander region 32 where they
again are propelled in the same direction as the direction of rotation of the platform
11.
[0014] In Figs. 1 to 5, steam is used for the operation of the rotary platform according
to a Rankine cycle. The steam is fed from a stationary boiler, not shown, to the rotating
platform 11 by means of a duct 40 (Fig. 4) extending through the support shaft 13.
The steam is delivered by a stationary conduit 41 through a rotary union 42 and into
the duct 40. Duct 40 communicates with a chamber 43 located in the plate 11 B below
the continuous, closed-loop passageways 30. Radially-extending slots 44, machined
into the mutually-engaging face surfaces of plates 11 A and 11 B, deliver the steam
from chamber 43 to supply chambers 45 (see also Figs. 1 and 2). Disposed within the
chambers 45 are bushings 46 with portal openings to deliver steam from the slots 44
into the expander region 32. As shown, the expansible steam is injected into the expander
region at the point of juncture between the expander region 32 and the radially-extending
region 34. The force exerted by the expanding steam propels the pistons along the
expander region to the point where they enter the combined coasting and steam exhaust
section formed by region 33. In region 33, the steam is exhausted through ports 31
to the atmosphere as described above or, if desired, a system of ducts may be used
to conduct the steam and/or condensate from region 33 through a pipe within duct 40
in shaft 13 for return to the boiler.
[0015] In the operation of the invention, the steam injected into the expander region 32
will propel each of the pistons 27 along the periphery of the platform 11, thereby
converting the thermal energy of the steam into kinetic energy of the pistons 27.
As each of the pistons 27 is propelled forwardly, an equal and opposite reaction is
induced tending to rotate the platform in the direction of arrow A. However, as the
pistons 27 enter the region 33, their direction of movement changes, thereby producing
a force on the platform 11 tending to rotate it in a direction opposite to the direction
of arrow A. The two forces thus produced essentially cancel each other so that, as
the pistons are propelled around the passageway 30, the net torque on the platform
11 is essentially zero. As the pistons pass through region 33 and work against centrifugal
force, their kinetic energy is converted into potential energy as they enter the radially-extending
region 34. Now, and assuming that the platform 11 is rotated, the abutting pistons
27 in region 34 will be urged radially outwardly by centrifugal force; and as they
pass through the pocketed wheels 24 and 25, torque will be imparted to the pocketed
wheels which is coupled through gears 21, 17 and 18 to the stationary gear 16. The
energy of the pistons, which are urged radially outwardly by centrifugal force in
region 34, is thus converted into rotational energy used to drive the platform 11
in the direction of arrow A as shown in Fig. 1. It will be appreciated that a starter
motor or some other device to initially rotate the platform may be required to initiate
centrifugal force on the pistons in region 34.
[0016] In addition to converting the energy of the pistons into rotational energy, the gear
system just described has two other functions. The second function is to maintain
the entire rotating system of the rotating energy converter at a desired velocity.
The third function of the gear system is to feed the pistons into the expander region
32 and provide thrust to overcome frictional drag of the pistons in the loop passageway.
[0017] The two unidirectional energy converter loops according to the invention are disposed
at mutually-exclusive sectors which are spaced 180° from each other and supported
by the platform 11. While it is possible to use a single closed-loop passageway, it
is obviously preferable to use at least two diametrically-opposed passageways in order
that the rotating platform 11 will be balanced rotationally. Furthermore, it will
be appreciated that a series of platforms such as that shown herein may be stacked
in spaced-apart relation for rotation about common axis 12.
[0018] A practical engine incorporating the principles of the invention may, for example,
employ a 900 mm diameter platform having a thickness twice the diameter of the pistons
27. The rotating engine may incorporate ten unidirectional energy conversion loops
having pistons with diameters of 28,6 mm (1-1/8 inches). Such an engine will develop
approximately 27 Kilowatt (50 horsepower) while the overall size of the engine will
be about 900 mm (three feet) in diameter and about 300 mm (one foot) long, not including
ducting for the steam and exhaust. Under these circumstances, the frequency of the
pistons in the passageways would be about 100 per second while the platform rotates
at a speed of about 650 revolutions per minute. Such a concept for a rotating engine
has a significant potential for practical low-temperature steam engines based on a
4.5 bar (absolute) (66 psia) at 149°C (300°F) steam inlet pressure and a 0.2 bar (absolute)
(3 psia) at 60°C (140°F) steam outlet pressure.
[0019] Fig. 6 illustrates another embodiment of the invention incorporating the principles
of the Brayton cycle. Because of the similarity between the parts forming the rotating
engine for a Brayton cycle and the parts forming a rotating engine for operation according
to the Rankine cycle as just described, elements of Fig. 6 which correspond to those
of Fig. 5 are identified by like reference numerals. The expander region 32 of each
continuous, closed-loop passageway 30 curves along a 90° circumferential part of the
platform 11. A combined exhaust and intake section 60 receives the pistons from the
expander region 32. An exhaust manifold 51 delivers the exhaust gases carried between
successive pistons. The exhaust gases are replaced by fresh air from an inlet manifold
52. From region 50, the pistons pass into a compression region 53. The gases compressed
between the pistons are delivered by a manifold 54 at an increased pressure through
a check valve 55 and into a combustion chamber 56. The compressed air is heated in
the combustion chamber and introduced into the unidirectional energy conversion loop
by an inlet conduit 57. The heated air accelerates the pistons in succession along
the expander region 32. Liquid fuel is fed from a stationary tank on the rotating
platform through a coaxial pipe in shaft 13 with a rotating shaft seal. The fuel is
then fed by a conduit 58 into the combustion chamber 56.
[0020] As each piston exits from the expander region 32 in succession, the velocity of the
piston is at a maximum relative to the unidirectional energy conversion loop formed
by its passageway 30. The kinetic energy of the piston is thus converted into potential
energy as the pistons approach the center of the rotating platform 11 in passing through
arcuate regions 50 and 53. The kinetic energy of the piston is also expended by compression
of air to form the compressed air supply which is fed into the combustion chamber
and then, when heated, fed into the expander inlet. In the radially-extending region
34 of the passageway, the pistons apply centrifugal force to the pocketed wheels.
The mechanical power formed by the unidirectional energy conversion loop is the net
centrifugal force impart to the platform through the sprocket-gear train.
[0021] The second unidirectional energy conversion loop supported by the platform 11 in
Fig. 6 is identical to the first and positioned diametrically opposite the first loop.
It is again apparent that a series of platforms 11 may be stacked in superimposed
spaced-apart relation along the same axis 12. Thus, the unidirectional energy conversion
engine operating according to the Brayton cycle may consist of multiple unidirectional
energy conversion loops as was the case with the embodiment of Figs. 1 to 5.
[0022] Figs. 7 and 8 illustrate another embodiment of the invention wherein a single passageway
is utilized on a rotating platform rather than two passageways as in the embodiment
of Figs. 1 to 6. Since many of the parts forming the rotating engine of the embodiment
of Figs. 7 and 8 are the same or similar to those of Figs. 1 to 6, certain elements
of Figs. 7 and 8 which correspond to those of Figs. 1 to 6 are identified by like
reference numerals.
[0023] In the rotating unidirectional energy converter shown in Figs. 7 and 8, a platform
100 is provided which rotates about a central axis 102. The platform 100 is elongated
but symmetrical about the axis of rotation 102 and is, therefore, balanced about planes
perpendicular to the axis of rotation. The platform 100 can be formed from upper and
lower halves 1 OOA and 1 OOB as shown in Fig. 8. Formed in the upper and lower halves
100A and 100B is a single continuous, closed-loop passageway 104 having two straight
portions 106 and 108 on opposite sides of the axis of rotation 102. The opposite ends
of the straight portions 106 and 108 are interconnected by curved portions 110 and
112, respectively, the portions 110 and 112 also being on opposite sides of the axis
of rotation 102 of the platform 100. Thus, opposite sides of the passageway 104 are
arranged symmetrically, and balanced, about planes perpendicular to the axis of rotation
102. The platform 100 is generally elliptical in shape, meaning that it is long as
compared to its width, having semicircular end portions connected by straight portions.
Instead of forming the passageway 104 from upper and lower plates 100A and 100B, it
is also possible to form the passageway from a tube which is rigidly mounted on a
rotatable platform, not shown. Other forms of construction will be readily apparent
to those skilled in the art.
[0024] The loop passageway 104 is made up of four regions. These comprise a first expander
region 114, a first thruster region 116, a second expander region 118 and a second
thruster region 120. Rotatable thruster wheels 122 and 124 are mounted for rotation
on the platform at the respective axes of the two curved end portions 110 and 112
of passageway 104. The thruster wheels 122 and 124 are provided with pockets 126,
uniformly spaced about their outer peripheries, which are adapted to engage successive
pistons 27 through the open inner faces of the curved end portions 110 and 112 of
the passageway 104. As the pocket thruster wheels 122 and 124 rotate, they serve to
move successive pistons through the curved end portions 110 and 112 and into the respective
expander regions 114 and 118. The rotating thruster wheels also serve to drive the
rotating platform 100 and the shaft 13 connected thereto through central, stationary
main gear 16 and appropriate idler gears 17 and 17' located beneath the platform 100.
Idler gears 17 and 17', in turn, mesh with gears 18 and 18' connected to the rotatable
pocket wheels 122 and 124, respectively, as best shown in Fig. 8. Thus, as the pocket
wheels 122 and 124 rotate in the direction of the arrows shown in Fig. 7, torque will
be transmitted to the shaft 13 to cause it and the platform 100 connected thereto
to rotate in the direction of arrow 128. The shaft 13 may be conveniently journaled
in bearings 130 and 132 as shown in Fig. 8.
[0025] In the operation of the embodiment shown in Figs. 7 and 8, an ideal diatomic gas
(e.g. air or steam) at a pressure elevated above ambient (i.e. from a compressor,
boiler or the like) is introduced into the passageway 104 via inlet port 45 located
between the second thruster region 120 and the first expander region 114, and via
inlet port 45' located between the first thruster region 116 and second expander region
118. Gas is exhausted from the passageway via a venting port (or ports) 134 located
between the first expander region 114 and the first thruster region 116, or via port
(or ports) 136 located between the second expander region 118 and the second thruster
region 120. The pistons 27 act as porting valves at the inlet and venting ports as
in the embodiment of Figs. 1 to 6.
[0026] Passageways or slots 44 and 44' can be provided to deliver steam or another expansible
fluid from chamber 43, similar to chamber 43 shown in Fig. 4, to the inlet ports 45
and 45'.
[0027] The pressurized gas entering the first expander region 114 through inlet port 45
drives successive pistons 27 through the expander region 114 against the centrifugal
force field generated by rotation of the platform 100. That is, the pistons must work
against centrifugal force as they approach the center of rotation of platform 100.
When the next piston closes off the inlet port 45, the unit cell of gas between the
pistons is closed off from the inlet port 45 and expands adiabatically as the lead
piston moves through the expander region. When the piston ahead of the piston in the
expander region 114 traverses venting port 134, the unit cell of gas ahead of the
piston still in the expander region 114 is exhausted through the venting port. The
piston in the expander region then arrives at the beginning of the thruster region
116 and closes off the venting port 134; while the ensuing piston is driven through
the expander region in accordance with the cycle just described.
[0028] Upon leaving the expander region 114, the piston enters the thruster region 116 which
is filled with pistons. When the pistons are in the thruster region, in closely-abutting
relationship, they are urged toward the curved end portion 112 of the passageway 104
under the influence of centrifugal force. That is, they are urged outwardly in relation
to the axis of rotation 102 of the platform 100 by centrifugal force. In this process,
they engage the pocketed thruster wheel 124 and impart torque thereto, causing it
to rotate with the rotation being transmitted through gears 18' and 17' to central
gear 16, thereby causing the entire platform 100 and the drive shaft 13 to rotate
in the direction indicated by arrow 128 in bearings 130 and 132 (Fig. 8). The energy
of the pistons, which are urged outwardly by centrifugal force in regions 116 and
120, is thus converted into rotational energy of the platform. Instead of using gears
as in the embodiment shown in Figs. 7 and 8, it is, of course, also possible to utilize
drive chains or other suitable means in accordance with well-known techniques.
[0029] As the thruster wheels 122 and 124 rotate, they feed successive ones of the pistons
to the expander regions 114 and 118 where the cycle described above is repeated. In
addition to converting the energy of the pistons 27 into rotational energy, the gear
system described above has two other functions. The second function is to maintain
the entire rotating system of the rotating energy converter at a desired velocity.
The third function of the gear system is to feed the pistons into the expander regions
114 and 118 and to provide thrust to overcome frictional drag of the pistons in the
loop passageway.
[0030] It can thus be seen that the rotating passageway 104 of the embodiment of Figs. 7
and 8 comprises, in series, a first expander region 114, a first thruster region 116,
a second expander region 118 and a second thruster region 120. This is in contrast
to the embodiments shown in Figs. 1 to 6 wherein each passageway comprises only one
expander region and one thruster region. However, except as noted above, this embodiment
functions in a manner generally similar to the embodiments previously discussed. A
starter motor or some other device to initially rotate the platform 100 may be required
to initiate centrifugal force on the pistons in regions 116 and 120.
[0031] In the embodiment shown in Figs. 7 and 8, steam may be used for the operation of
the rotating platform 100 in accordance with the Rankine cycle as in the previously-described
embodiments. When steam is used, the force exerted by the expanding steam, which enters
the passageway 104 through ports 45 and 45', propels the pistons 27 through the expander
regions 114 and 118. The steam is exhausted through venting ports 134 and 136 as the
pistons enter the thruster regions 116 and 120. Venting ports 134 and 136 may be open
to the atmosphere or, if desired, a system of ducts, not shown, may be used to return
the steam and/or condensate to the boiler in a manner similar to that of Fig. 4.
[0032] While the rotating engine as shown in Figs. 7 and 8 may operate in accordance with
the thermodynamic principles of the Rankine cycle as described above, this embodiment
of the invention, appropriately modified, may also function in accordance with the
principles of the Brayton, Diesel, or Otto cycles as briefly described below.
[0033] In the operation of the embodiment of Figs. 7 and 8 according to the Brayton cycle,
compressed gas (typically air) is heated in a combustion chamber rotating on the platform
as in Fig. 6, or by a heat exchanger rotating on the platform, with the heat exchanger
being connected to a stationary external heat source via a coaxial duct. The heated,-
compressed gas is then introduced into the expander regions from appropriate conduits
via the inlet ports. After expansion, the gas is exhausted at ambient pressure via
the venting ports 134 and 136 either direct to the atmosphere or through a coaxial
duct. The compressed gas may be obtained via conventional compressor means, either
stationary or rotating in the platform; however, it is preferred to obtain the compressed
gas from a separate unidirectional energy converter loop which is rotating about the
same axis of rotation (i.e. stacked above or below the platform), and which is adapted
to function as a compressor in the manner described in connection with Figs. 7 and
8 hereinafter or as described in U.S. Patent No. 3,859,789, Fawcett et al.
[0034] In the operation of the embodiment of Figs. 7 and 8 in accordance with the principles
of the Diesel cycle, an expanding gas is provided in the expander regions by way of
internal combustion within these regions. Compressed air (typically from one of the
sources described above in reference to the Brayton cycle) is introduced into the
regions via the inlet ports 45 and 45'. Liquid or gaseous fuel is fed into the expander
regions 114 and 118 when the inlet ports are closed off by the pistons leaving the
thruster regions. Combustion takes place in the expander regions and is cycled to
effect expanding gas behind each piston as it enters the expander regions 116 and
120. That is, combustion takes place periodically to propel successive ones of the
pistons through the expander regions. As with the Brayton cycle, the combustion gases
may be exhausted at ambient pressure via the venting port directly to the atmosphere
or through a coaxial duct.
[0035] The operation of the embodiment of Figs. 7 and 8 according to the Otto cycle is similar
to that described above regarding the Diesel cycle. The fuel and air may be separately
introduced into the expander regions, as in the Diesel cycle, or the fuel may be mixed
with the incoming air before or after it is compressed. Ignition of the fuel-air mixture
is effected in the expander regions 114 and 118 by means of a conventional spark system
located in an appropriate recessed area in these regions. As in the Diesel cycle,
combustion is cycled to effect expanding gas successively behind each piston as it
passes so as to propel successive ones of the pistons through the expander regions.
[0036] If the platform 100 shown in Figs. 7 and 8 is rotated by a motor or some other external
power source in a direction opposite that shown, gas at ambient pressure will be taken
into the passageway 104 via ports 134 and 136 and will be exhausted at an elevated
pressure via ports 45 and 45'. In this regard, the system can function as a compressor.
If the platform 100 is rotated by a motor, the system of gears interconnecting the
thruster wheels 122 and 124 to the central shaft 13 will act to rotate the thruster
wheels. The rotating thruster wheels will then move the stacked pistons 25 in the
thruster regions toward the axis of rotation of the platform, so that upon passing
ports 134 and 136, the pistons will travel through the expander regions 114 and 118
under the influence of centrifugal force. The gas between the pistons will be adiabatically
compressed by the moving pistons in the expander regions 116 and 120 which would more
properly be termed "compressor regions" in this mode.
[0037] It will also be appreciated that a series of unidirectional energy converters may
be stacked in superimposed, spaced-apart relation for rotation upon shaft 13 about
the common axis 102. In the embodiment of Figs. 7 and 8 the following general observations
can be made: (1) the change in enthalpy of the gas in the expander regions produces
net work, which is performed on the thruster wheels 122 and 124 via the pistons 27,
and then transmitted to the rotating platform 100 and the shaft 13; (2) the change
in enthalpy of the gas in the expander regions transfers energy via the centrifugal
field (potential) energy stored in the mass of the pistons as they move through the
expander regions from a larger radius of rotation (i.e. about the axes of rotation
of the platform 100) to a smaller radius of rotation (i.e. nearer the axis of rotation);
(3) the initial and final velocities of the pistons traveling in the expander regions
relative to the rotating platform are equal; and (4) the inlet and venting gas port
sizes, the mass of the pistons, the speed of rotation of the thruster wheels and the
platform, and the inlet and exit states of the gas are all interrelated in the operation
of, and the net work produced in, this system. Under some conditions of operation,
the gas pressure in the expander region during part of the operating cycle may be
below ambient.
[0038] In Figs. 9A and 9B, alternative forms of the pistons 27 are shown. In Fig. 9A, the
piston 27A comprises a body having a central annular slot 140 and large diameter end
portions 142 and 144 provided with spherically-beveled edges 146 which can engage
the periphery of the passageway 104 as the pistons 27A pass around the curved portions
110 and 112. The large diameter portions 142 and 144 are hollow as shown. The configuration
shown in Fig. 9A comprises, in effect, two interconnected pistons separated by the
reduced diameter portion 140 which receives the radially, outwardly-projecting prongs
on the pocketed wheels 122 and 124 as the pistons move around the curved portions
110 and 112.
[0039] Lightly-loaded piston rings (not shown) may optionally be located in recesses formed
within the outer surface of the pistons, so as to reduce losses due to leakage of
the fluid medium around the pistons.
[0040] Fig. 9B is similar to that of Fig. 9A except that the piston 27B in this case comprises
two spherical end portions 148 and 150 interconnected by reduced diameter portion
152 which again received the radially, outwardly-projecting prongs on the thruster
wheels 122 and 124.
[0041] A piston such as that shown in Fig. 9A, or some other configuration having a cylindrical
outer periphery (as contrasted to a sphere) may be preferable in order that the cylindrical
surface can more positively close off the ports 134 and 136 as they pass thereby.
In this respect, the ports 134 and 136 should be as small in cross section as possible
while affording the required flow volume therethrough.
[0042] The embodiments of the invention described above utilize an arrangement wherein the
pocketed thruster wheels are mechanically linked (i.e. coupled) to both the rotating
platform and the engine drive shaft via a system of gears or drive chains, etc. In
an alternative preferred embodiment of the invention it may be desirable to decouple
the thruster wheels from the platform, and to provide a separate, external drive motor
which can be utilized to separately drive the rotating platform at a speed of rotation
which is independent from that of the pocketed thruster wheels. It is apparent that
the speed of rotation of the platform is related to the torque produced by the rotating
engine of the present invention, whereas the speed of rotation of the thruster wheels
is proportional to the rate of torque applied to the engine drive shaft (i.e. shaft
power). By providing a separate drive motor to independently drive the platform, the
rotating engine of the present invention can be utilized to produce torque independently
from engine drive shaft speed (i.e. high torque can be produced at low or variable
speed).
[0043] Although the invention has been shown in connection with certain specific embodiments,
it will be readily apparent to those skilled in the art that various changes in form
and arrangement of parts may be made to suit requirements without departing from the
spirit and scope of the invention.
1. Apparatus for converting a first form of energy into a second form of energy characterised
by a platform (11, 100), support means for carrying said platform (11, 100) for rotation
about a central axis (12), at least one continuous, closed-loop passageway (30, 104)
carried by the platform (11, 100) in a plane extending perpendicular to said central
axis (12), a plurality of freely-movable pistons (27) contained within the passageway
(30, 104), at least one region (33) in the passageway (30) in which the pistons (27)
must move inwardly against centrifugal force as said platform (11, 100) rotates, at
least one other region (34) in the passageway (30) where said pistons (27) are moved
outwardly under the influence of centrifugal force, means for imparting a force to
successive ones of the pistons to propel them against centrifugal force in said one
region (33), means for converting the energy of pistons (27) moving outwardly under
the influence of centrifugal force in said other region (34) into rotational energy,
and means coupling said rotational energy to said platform (11) to rotate the same.
2. The apparatus according to claim 1 wherein said means for imparting a force to
successive ones of the pistons includes a conduit (44) directing a fluid for expansion
between said pistons (27) to said one region (33) of the passageway (30, 104).
3. The apparatus according to claim 2 wherein each of said plurality of freely-movable
pistons (27) is of a shape substantially complementary to the cross-sectional shape
of said closed-loop passageway (30, 104) so as to substantially seal the passageway
from fluid flow around said pistons (27) and subdivide said fluid into segments.
4. The apparatus according to claim 1 wherein said means for imparting a force includes
a duct (44) extending in a generally radial direction from said central axis (12)
about which said platform (11, 100) rotates to said one region (33) of the passageway
(30, 104), and conduit means (43) at said central axis (12) communicating with said
duct (44) to feed an expansible fluid medium into said one region (33) of said passageway.
5. The apparatus according to claim 1 wherein said passageway (30, 104) is provided
with one or more ports (31, 134) positioned to bleed fluid from the passageway (30,
104) to reduce pressure in front of the pistons (27) and promote their acceleration
under the influence of centrifugal force.
6. The apparatus according to claim 1 wherein said means for converting the energy
of the pistons (27) into rotational energy includes a wheel (24, 25, 122, 124) having
circumferentially-spaced peripheral pockets (126) for receiving successive ones of
said pistons (27) at one side of said passageway (30, 104) in said other region (34)
thereof.
7. The apparatus according to claim 6 including idler gear means (17, 17', 18) coupled
to said wheel (24, 25, 122, 124) and in meshing engagement with stationary gear means
(16) mounted coaxially with said central axis (12).
8. The apparatus according to claim 1 wherein the apparatus operates according to
the Rankine cycle.
9. The apparatus according to claim 8 wherein said means for imparting a force to
successive ones of the pistons (27) comprises expanding steam under pressure.
10. The apparatus according to claim 1 wherein the apparatus operates according to
the Brayton cycle, and said means for imparting a force to successive ones of the
pistons (27) comprises an expanding gas produced by combustion of a fuel.
11. The apparatus according to claim 10 including a first manifold (51) in said passageway
(30, 104) for exhausting products of combustion, and a second manifold (52) in said
passageway (30, 104) for supplying air to said passageway which is compressed between
successive ones of said pistons (27).
12. The apparatus according to claim 11 including a combustion chamber (56), means
for supplying compressed air from said passageway (30) to said combustion chamber
(56), means for supplying fuel to said combustion chamber (56) and for burning the
fuel therein, and means for supplying compressed gases comprising the products of
combustion from said combustion chamber (56) to said one region of the passageway
to propel successive ones of the pistons (27) therein.
13. Apparatus for converting a first form of energy into a second form of energy characterised
by a platform, support means for carrying said platform (11) for rotation about a
central axis (12), at least one continuous, closed-loop passageway (30) carried by
the platform (11) in a place extending perpendicular to said central axis (12), a
plurality of freely-movable pistons (27) contained within the passageway (30), means
for applying a force to successive ones of the pistons (27) in a first region (32)
of the passageway (30) extending along the periphery of the rotating platform (11)
to thereby propel each piston (27) in one direction around the passageway (30) and
increase its kinetic energy, a second region (33) of the passageway being shaped to
cause the pistons, after being propelled, to work against centrifugal force to thereby
convert the kinetic energy of the pistons into potential energy as they approach the
center of rotation of the platform (11), a third radially-extending region (34) of
the passageway (11) where said pistons (27) are moved radially outwardly back to said
first region (32) under the influence of centrifugal force, means (24, 25) for converting
the energy of pistons (27) moving radially outwardly in said third region (34) into
rotational energy, and means (16, 17, 18) coupling said rotational energy to said
platform (11) to rotate the same.
14. The apparatus of claim 13 wherein there are two continuous, closed-loop passageways
(30) containing a plurality of freely-movable pistons (27), said passageways (30)
being diametrically opposite each other on the rotating platform (11).
15. The apparatus according to claim 13 wherein said passageway (30) includes at least
two arcuate regions each having different radii.
16. The apparatus according to claims 14 and 15 wherein each of said passageways (30)
includes a radially-extending linear region interconnecting said two arcuate regions.
17. The apparatus according to claim 13 wherein said means for applying a force to
successive ones of the pistons (27) includes a conduit (40) directing a fluid medium
for expansion between said pistons (27) into the first region (32) of said passageway
(30).
18. The apparatus according to claim 13 wherein each of said plurality of freely-movable
pistons (27) is of a shape substantially complementary to the cross-sectional shape
of said closed-loop passageway (30) so as to substantially seal the passageway from
fluid flow around said pistons (27) and subdivide said fluid into segments.
19. The apparatus of claim 13 wherein said platform (11) comprises a disc, and a support
shaft (13) coaxial with said central axis for supporting said disc.
20. The apparatus according to claim 19 wherein said support shaft (13) is secured
to said disc.
21. The apparatus according to claim 19 wherein said means for applying a force includes
a duct (44) extending in a generally radial direction from said central axis (12)
about which said platform (11) rotates to said first region of the passageway (30),
and conduit means (43) communicating with said duct (44) to feed an expansible fluid
medium into the first region of said passageway (30).
22. The apparatus according to claim 13 wherein said passageway is provided with one
or more ports (31) positioned to bleed fluid from the passageway (30) to reduce the
pressure in front of the pistons (27) and promote their acceleration in the second
region thereof.
23. The apparatus according to claim 13 wherein said means for converting potential
energy into rotational energy includes a wheel (24, 25) having circumferentially-spaced
peripheral pockets for receiving successive ones of said pistons (27) at one side
of said passageway (30) in the third region thereof.
24. The apparatus according to claim 23 including idler gear means (17, 17', 18) coupled
to said wheel (24, 25) and in meshing engagement with stationary gear means (16) mounted
coaxially with said central axis (12).
25. The apparatus according to claim 14 wherein, for each passageway (30), said means
for converting potential energy into rotational energy includes spaced-apart wheels
(24, 25) projecting into opposite sides of the path of travel of said pistons (27)
in the third region of said passageway (30), each wheel having circumferentially-spaced
peripheral pockets to advance each piston (27) received therebetween along a passageway
(30).
26. The apparatus according to claim 25 including idler gear means (17, 17', 18) coupled
to each pocketed wheel (24, 25) while drivingly engaging stationary gear means (16)
mounted coaxially with said central axis (12).
27. Apparatus for converting a first form of energy into a second form of energy characterised
in a platform (100), support means for carrying said platform for rotation about a
central axis, a continuous, closed loop passageway (104) carried by the platform in
a plane extending perpendicular to said central axis, a plurality of freely-movable
pistons contained within the passageway (104), said passageway having essentially
straight portions (106, 108) on opposite sides of said central axis, said straight
portions being interconnected at their opposite ends by curved portions (110, 112)
also on opposite sides of said central axis, means for applying a force to successive
ones of the pistons in one region of each of said straight portions (106, 108) to
propel them inwardly on the rotating platform (100) against centrifugal force, said
pistons being moved radially outwardly in another region of each of said straight
portions (106, 108) under centrifugal force, means for converting the energy of pistons
in said curved portions (110, 112) which have been moved outwardly under centrifugal
force into rotational energy, and means for coupling said rotational energy to said
platform (100) to rotate the same.
28. The apparatus of claim 27 wherein said means for converting potential energy into
rotational energy includes a wheel (122, 124) having circumferentially-spaced peripheral
pockets (126) for receiving successive ones of said pistons in a curved portion (110,
112) of said passageway (104).
29. The apparatus according to claim 28 wherein the outer periphery of said wheel
(122, 124) substantially coincides with the inner periphery of a curved portion (110,
112) of said passageway (104).
30. The apparatus according to claim 28 including idler gear means coupled to said
wheel (122, 124) and in meshing engagement with stationary gear means mounted coaxially
with said central axis.
31. The apparatus of claim 30 wherein there are wheels (122, 124) for receiving successive
ones of the pistons in each curved portion (110, 112) of the passageway (104), the
idler gear means coupling both of said wheels to said stationary gear means.
32. The apparatus according to claim 27 including a region in each of said straight
portions (106, 108) of said passageway (104) where pistons are propelled by expansion
of a gas, and another region where pistons are propelled by centrifugal force.
1. Vorrichtung zur Umwandlung einer ersten in eine zweite Energieform, gekennzeichnet
durch eine Plattform (11, 100), mit einer um eine Zentralachse (12) drehbaren Lagerung
für die Plattform (11, 100), wenigstens einen kontinuierlichen, in sich geschlossenen
Bahndurchgang (30, 104), der an der Plattform (11, 100) in einer sich senkrecht zur
Zentralachse (12) erstreckenden Ebene angeordnet ist, einer Anzahl im Bahndurchgang
(30, 104) angeordneter, frei beweglicher Kolben (27), wenigstens einem Bereich (33)
im Bahndurchgang (30), in dem sich die Kolben (27) bei Umlauf der Plattform (11, 100)
gegen die Zentrifugalkraft nach innen bewegen müssen, wenigstens einem weiteren Bereich
(34) im Bahndurchgang (30), in dem die Kolben (27) unter dem Einfluß der Zentrifugalkraft
nach außen bewegt werden, einer Einrichtung zum Aufbringen einer Kraft auf die aufeinanderfolgenden
Kolben, um sie gegen die Zentrifugalkraft im dem Bereich (33) anzutreiben, einer Einrichtung
zur Umwandlung der sich unter dem Einfluß der Zentrifugalkraft im weiteren Bereich
nach außen bewegenden Kolben (27) in Rotationsenergie und einer Einrichtung zur Aufbringung
der Rotationsenergie auf die Plattform (11, 100), um diese in Drehung zu versetzen.
2. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß die Einrichtung zur Aufbringung
einer Kraft auf die aufeinanderfolgenden Kolben (27) eine Leitung (44) aufweist, mit
der ein Fluid zur Expansion zwischen den Kolben (27) auf den Bereich (33) des Bahndurchgangs
(30, 104), richtbar ist.
3. Vorrichtung nach Anspruch 2, dadurch gekennzeichnet, daß jeder der frei beweglichen
Kolben (27) einen Querschnitt aufweist, der im wesentlichen komplementär zum Querschnitt
des Bahndurchgangs (30, 104) ist, um auf diese Weise gegen Fluiddurchtritt zwischen
den Kolben (27) und dem Bahndurchgang abzudichten und das Fluid in Segmente zu unterteilen.
4. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß die Einrichtung zur Aufbringung
einer Kraft eine Leitung (44) aufweist, die sich im wesentlichen radial von der Zentralachse
(12) zum Bereich (33) des Bahndurchgangs (30, 104) erstreckt, sowie Verbindungen (43)
im Bereich der Zentralachse (12) zur Leitung (44), um ein expansionsfähiges Fluid
in den Bereich (33) des Bahndurchgangs zu leiten.
5. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß der Bahndurchgang (30,
104), mit einer oder mehreren Öffnungen (31, 134) versehen ist, die zum Ablassen von
Fluid aus dem Bahndurchgang (30, 104) angeordnet sind, um den Druck vor den Kolben
(27) zu verringern und deren Beschleunigung unter dem Einfluß der Zentrifugalkraft
zu steigern.
6. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß die Einrichtung zur Umwandlung
der Energie der Kolben (27) in Rotationsenergie ein Rad (24, 25, 122, 124) mit am
Umfang mit Abstand zueinander angeordneten Taschen (126) aufweist zur Aufnahme von
aufeinander folgenden Kolben (27) auf einer Seite des Bahndurchgangs (30, 104) in
dem weiteren Bereich (34).
7. Vorrichtung nach Anspruch 6, gekennzeichnet durch ein Zwischenzahnrad (17, 17',
18), das an das Rad (24, 25, 122, 124) angekuppelt ist und mit einem stationären Zahnrad
(16) kämmt, welches koaxial zur Zentralachse (12) angeordnet ist.
8. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß sie einen Rankine-Zyklus
ausführt.
9. Vorrichtung nach Anspruch 8, dadurch gekennzeichnet, daß die Einrichtung zur Aufbringung
einer Kraft auf aufeinander folgende Kolben (27) die Expansion von Dampf unter Druck
beinhaltet.
10. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, daß sie einen Brayton-Zyklus
ausführt und daß die Einrichtung zur Aufbringung einer Kraft auf aufeinander folgende
Kolben (27) ein expandierendes Gas aufweist, das durch Verbrennung eines Brennstoffes
gewonnen wird.
11. Vorrichtung nach Anspruch 10, dadurch gekennzeichnet, daß zum Ausstoß von Verbrennungsprodukten
am Bahndurchgang (30, 104) eine Auspuffleitung (51) sowie zur Zufuhr von Luft zum
Bahndurchgang eine Ansaugleitung (52) vorgesehen sind, wobei die angesaugte Luft zwischen
aufeinander folgenden Kolben (27) komprimierbar ist.
12. Vorrichtung nach Anspruch 11, gekennzeichnet durch eine Verbrennungskammer (56),
eine Einrichtung zur Zufuhr komprimierter Luft vom Bahndurchgang (30) zur Verbrennungskammer
(56), einer Einrichtung zur Zufuhr von Brennstoff zur Verbrennungskammer (56) und
zur dortigen Verbrennung des Brennstoffs und einer Einrichtung zur Zufuhr komprimierten
Gases unter Einschluß der Verbrennungsprodukte von der Verbrennungskammer (56) zum
Bereich (33) des Bahndurchgangs, um aufeinander folgende Kolben (27) dort anzutreiben.
13. Vorrichtung zur Umwandlung einer ersten in eine zweite Energieform, gekennzeichnet
durch eine Plattform (11), eine Einrichtung zur Lagerung der Plattform (11) zwecks
Umlaufs um eine Zentralachse (12), wenigstens einen kontinuierlichen, in sich geschlossenen
Bahndurchgang (30), der an der Plattform (11) an einer Stelle angeordnet ist, die
sich senkrecht zur Zentralachse (12) erstreckt, eine Anzahl im Bahndurchgang (30)
angeordneter, frei beweglicher Kolben (27), einer Einrichtung zur Aufbringung einer
Kraft auf aufeinander folgende Kolben (27) in einem ersten Bereich (32) des Bahndurchgangs
(30), welcher Bereich sich längs des Umfangs der rotierenden Plattform (11) erstreckt,
um hierdurch jeden Kolben (27) in einer Richtung längs des Bahndurchgangs (30) anzutreiben
und seine kinetische Energie zu erhöhen, einen zweiten Bereich (33) des Bahndurchgangs,
welcher Bereich ausgebildet ist, daß die Kolben nach ihrem Antrieb gegen die Zentrifugalkraft
arbeiten, um hierdurch ihre kinetische Energie in Potentialenergie umzuwandeln, wenn
sie sich dem Rotationszentrum der Plattform (11) nähern, einen dritten, sich radial
erstreckenden Bereich (34) des Bahndurchgangs (11) in dem die Kolben (27) radial nach
außen, unter dem Einfluß der Zentrifugalkraft zurück zum ersten Bereich (32) bewegt
werden, um die Energie der sich in diesem dritten Bereich (34) radial nach außen bewegenden
Kolben (27) in Rotationsenergie umzuwandeln und durch eine Einrichtung (16, 17, 18)
um die Rotationsenergie auf die Plattform (11) zu übertragen und diese in Umlauf zu
versetzen.
14. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß zwei kontinuierliche,
in sich geschlossene Bahndurchgänge (30) mit einer Anzahl von frei beweglichen Kolben
(27) vorgesehen sind und daß die Bahndurchgänge (30) diametral einander gegenüber
liegend an der rotierenden Plattform (11) angeordnet sind.
15. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß der Bahndurchgang (30)
wenigstens zwei bogenförmige Bereiche mit unterschiedlichem Radius aufweist.
16. Vorrichtung nach Anspruch 14 und 15, dadurch gekennzeichnet, daß jeder der Bahndurchgänge
(30) einen sich radial nach innen erstreckenden, linearen Bereich aufweist, der die
beiden bogenförmigen Bereiche verbindet.
17. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß die Einrichtung zur
Aufbringung einer Kraft auf aufeinander folgende Kolben (27) eine Leitung (40) zur
Aufbringung von Fluid zwecks Expansion zwischen den Kolben (27) in den ersten Bereich
(32) des Bahndurchgangs (30) aufweist.
18. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß jeder der frei beweglichen
Kolben (27) einen im wesentlichen zum Querschnitt des in sich geschlossenen Bereichs
(30) komplementären Querschnitt aufweist, um so im wesentlichen gegen Fluidströmung
zwischen Bahndurchgang und Kolben abzudichten und das Fluid in Segmente zu unterteilen.
19. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß die Plattform (11) eine
Scheibe aufweist sowie eine Lagerwelle (13), die koaxial zue Zentralachse vorgesehen
ist un die Scheibe lagert.
20. Vorrichtung nach Anspruch 19, dadurch gekennzeichnet, daß die Lagerwelle (13)
fest mit der Scheibe verbunden ist.
21. Vorrichtung nach Anspruch 19, dadurch gekennzeichnet, daß die Einrichtung zur
Aufbringung einer Kraft eine Leitung (44) aufweist, die sich im wesentlichen in radialer
Richtung von der Zentralachse (12) zum ersten Bereich des Bahndurchgangs (30) erstreckt
sowie eine Verbindungsleitung (43) zur Leitung, (44), um eine expandierendes Fluid
in den ersten Bereich des Bahndurchgangs (30) zu leiten.
22. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß der Bahndurchgang mindestens
eine Öffnung (31) aufweist zum Ablassen von Fluid und Reduzierung des Drucks vor den
Kolben (27) sowie zu deren Beschleunigung im zweiten Bereich.
23. Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, daß die Einrichtung zur
Umwandlung der Potentialenergie in Rotationsenergie ein Rad (24, 25) mit am Umfang
mit Abstand zueinander angeordneten Taschen aufweist, um auf einer Seite des Bahndurchgangs
(30) in dessen drittem Bereich aufeinander folgende Kolben (27) aufzunehmen.
24. Vorrichtung nach Anspruch 23, dadurch gekennzeichnet, daß ein Zwischenzahnrad
(17, 17', 18) an das Rad (24, 25) angekoppelt ist und mit einem stationären Zahnrad
(16) kämmt, das koaxial zue Zentralachse (12) vorgesehen ist.
25. Vorrichtung nach Anspruch 14, dadurch gekennzeichnet, daß für jeden Bahndurchgang
(30) die Einrichtung zur Umwandlung der potentiellen in Rotationsenergie mit Abstand
zueinander angeordnete Räder (24, 25) aufweist, die sich in gegenüber liegende Seiten
des Weges der Kolben (27) im dritten Bereich des Bahndurchgangs (30) erstrecken, wobei
jedes Rad am Umfang mit Abstand zueinander angeordnete Tasche aufweist, um die dazwischen
aufgenommenen Kolben längs des Bahndurchganges (30) zu beschleunigen.
26. Vorrichtung nach Anspruch 25, gekennzeichnet durch Zwischenzahnräder (17, 17',
18), die mit jedem mit Taschen versehenen Rad (24, 25) verbunden sind und des weiteren
das stationäre Zahnrad (16) antreiben, das koaxial zur Zentralachse (12) vorgesehen
ist.
27. Vorrichtung zur Umwandlung einer ersten Energieform in eine zweite Energieform,
gekennzeichnet durch eine Plattform (100), eine Einrichtung zur Lagerung der Plattform
zwecks Umlaufs um eine Zentralachse, einen kontinuierlichen, in sich geschlossenen
Bahndurchgang, der an der Plattform in einer sich senkrecht zur Zentralachse erstreckenden
Ebene angeordnet ist, ein Anzahl frei beweglicher, im Bahndurch gang angeordneter
Kolben, wobei der Bahndurchgang im wesentlichen gerade Strecken (106, 108) an gegenüber
liegenden Seiten der Zentralachse aufweist, die an ihren gegenüber liegenden Enden
durch bogenförmige Strecken (110, 112) ebenfalls an gegenüber liegenden Seiten der
Zentralachse, miteinander verbunden sind, eine Einrichtung zur Aufbringung einer Kraft
auf aufeinander folgende Kolben in einem Bereich der geraden Strecken (106, 108),
um die Kolben nach innen auf der rotierenden Plattform gegen die Zentrifugalkraft
anzutreiben, wobei die Kolben in einem anderen Bereich jeder der geraden Strecken
(106, 108) aufgrund der Zentrifugalkraft radial nach außen bewegbar sind, eine Einrichtung
in den bogenförmigen Bereichen (110, 112) zur Umwandlung der Energie der nach außen
unter Einfluß der Zentrifugalkraft bewegten Kolben in Rotationsenergie und eine Einrichtung
zur Aufbringung der Rotationsenergie auf die Plattform (100), um diese in Drehung
zu versetzen.
28. Vorrichtung nach Anspruch 27, wobei die Einrichtung zur Umwandlung der Potential-
in Rotationsenergie ein Rad (122, 124) mit am Umfang mit Abstand zueinander angeordneten
Taschen (126) aufweist, um aufeinander folgende Kolben in einer bogenförmigen Strecke
(110, 112) des Bahndurchgangs (104) aufzunehmen.
29. Vorrichtungs nach Anspruch 28, dadurch gekennzeichnet, daß der Außenumfang des
Rades (122, 124) im wesentlichen mit dem Innenumfang einer bogenförmigen Strecke (110,
112) des Bahndurchgangs (104) zusammenfällt.
30. Vorrichtung nach Anspruch 28, gekennzeichnet durch ein mit dem Rad (122, 124)
gekuppelten Zwischenzahnrad, das mit einem stationären Rad kämmt, welches koaxial
zur Zentralachse angeordnet ist.
31. Vorrichtung nach Anspruch 30, dadurch gekennzeichnet, daß Räder (122, 124) zur
Aufnahme aufeinander folgender Kolben in jeder bogenförmigen Strecke (110, 112) des
Durchgangs (104) vorgesehen sind, wobei eine Zwischenzahnrad beide Räder mit dem stationären
Zahnrad verbindet.
32. Vorrichtung nach Anspruch 27, dadurch gekennzeichnet, daß in jeder der geraden
Strecken (106, 108) des Bahndurchgangs (104) ein Bereich vorgesehen ist, in dem die
Kolben durch Expansion eines Gases antreibbar sind, und ein weiterer Bereich in dem
die Kolben durch Zentrifugalkraft antreibbar sind.
1. Dispositif pour convertir une première forme d'énergie en une seconde forme d'énergie,
caractérisé par un plateau (11, 100), par des moyens-support dudit plateau (11, 100)
en rotation autour d'un axe central (12), par au moins un passage sans fin (30, 104),
solidaire du plateau (11, 110), s'étendant dans un plan perpendiculaire audit axe
central (12), par une pluralité de pistons à déplacement libre (27) placés dans ce
passage (30, 104), par au moins une zone (33) dudit passage (30) dans laquelle les
pistons (27) sont forcés de se mouvoir en sens centripète, à l'encontre de la force
centrifuge, lorsque ledit plateau (11, 100) tourne, par au moins une autre zone (34)
dudit passage (30) dans laquelle lesdits pistons (27) sont mus dans le sens centrifuge,
sous l'effet de la force centrifuge, par des moyens pour appliquer successivement
à chacun des pistons (27) une force de propulsion s'opposant à la force centrifuge
dans ladite zone (33), par des moyens pour convertir l'énergie des pistons (27), qui
se déplacent en direction centrifuge sous l'effet de la force centrifuge dans ladite
autre zone (34), en énergie de rotation, et par des moyens pour transmettre ladite
énergie de rotation audit plateau (11), pour l'entraîner en rotation.
2. Dispositif selon la revendication 1, dans lequel lesdits moyens pour appliquer
une force successivement à chacun des pistons comprennent un conduit (44) dirigeant
un fluide se détendant entre lesdits pistons (27), dans ladite zone (33) du passage
(30, 104).
3. Dispositif selon la revendication 2, dans lequel chaque élément de ladite pluralité
de pistons à déplacement libre (27) a une forme substantiellement complémentaire à
la section droite dudit passage sans fin (30, 104), pour obturer de façon substantielle
le passage à l'écoulement du fluide autour desdits pistons (27) et pour répartir ledit
fluide en segments.
4. Dispositif selon la revendication 1, dans lequel lesdits moyens pour appliquer
une force comprennent un conduit (44) s'étendant dans une direction globalement radiale
entre ledit axe central (12), autour duquel tourne ledit plateau (11, 100), et ladite
zone (33) du passage (30, 104), et un organe d'amenée (43) audit axe central (12)
communicant avec ledit conduit (44) pour pourvoir ladite zone (33) dudit passage en
milieu fluide expansible.
5. Dispositif selon la revendication 1, dans lequel ledit passage (30, 104) et pourvu
d'un ou plusieurs orifices (31, 134) placés de façon à permettre au fluide de sortir
du passage (30, 104), afin du diminuer la pression à l'avant des pistons (27), et
de favoriser leur accélération sous l'influence de la force centrifuge.
6. Dispositif selon la revendication 1, dans lequel lesdits moyens pour convertir
l'énergie des pistons (27) en énergie de rotation comprennent une roue (24, 25, 122,
124) comportant des logements périphériques (126) répartis à sa circonférence pour
accueillir successivement chacun desdits pistons (27) sur un côté dudit passage (30,
104), dans ladite autre zone (34) du passage.
7. Dispositif selon la revendication 6, comportant des moyens intermédiaires d'engrènement
(17, 17', 18), accouplés à ladite roue (24, 25, 122, 124), et en prise avec des moyens
immobiles d'engrènement (16) montés coaxialement audit axe central (12).
8. Dispositif selon la revendication 1, dans lequel le dispositif fonctionne selon
un cycle de Rankine.
9. Dispositif selon la revendication 8, dans lequel lesdits moyens pour appliquer
une force successivement à chacun des pistons (27) sont constitués par une détente
de vapeur sous pression.
10. Dispositif selon la revendication 1, dans lequel le dispositif fonctionne selon
un cycle de Brayton, et lesdits moyens pour appliquer une force successivement à chacun
des pistons (27) sont constitués par une détente d'un gaz obtenu en brûlant un combustible.
11. Dispositif selon la revendication 10, englobant un premier ensemble de tubes (51
dans ledit passage (30, 104), pour l'évacuation des produits de combustion, et un
second ensemble de tubes (52), dans ledit passage (30, 104), pour fournir à ce passage
l'air comprimé successivement entre chacun desdits pistons.
12. Dispositif selon la revendication 11, englobant une chambre de combustion (56),
des moyens pour alimenter la chambre de combustion (56) en air comprimé à partir dudit
passage (30), des moyens pour alimenter ladit chambre de combustion (56) en combustible
et pour y brûler le combustible, et des moyens pour alimenter ladite zone du passage
en gaz comprimés contenant les produits de combustion à partir de ladite chambre de
combustion (56), pour y propulser successivement chacun des pistons.
13. Dispositif pour convertir une première forme d'énergie en une seconde forme d'énergie,
caractérisé par un plateau, par des moyens-support dudit plateau (11) en rotation
autour de l'axe central (12), par au moins un passage sans fin (30) solidaire du plateau
(11) s'étendant dans un plan perpendiculaire audit axe central (12), par une pluralité
de pistons à déplacement libre placés dans le passage (30), par des moyens pour appliquer
une force successivement à chacun des pistons (27), dans une première zone (32) du
passage (30) s'étendant à la périphérie du plateau tournant (11), pour propulser chaque
piston (27) dans ladite zone (32), dans une direction, autour du passage (30), et
pour accroître son énergie cinétique, par une deuxième zone (33) du passage, formée
pour faire travailler les pistons (27) à l'encontre de la force centrifuge, après
qu'ils aient été propulsés, afin de convertir l'énergie cinétique des pistons en énergie
potentielle, par un rapprochement du centre de rotation du plateau (11), par une troisième
zone (34) du passage (30) s'étendant radialement, dans laquelle lesdits pistons (27)
sont mus radialement, en direction centrifuge, par la force centrifuge, vers ladite
première zone (32), à l'intérieur de ladite troisième zone (34), par des moyens (24,
25) pour convertir l'énergie des pistons (27), animés de mouvements centrifuges radiaux,
dans ladite troisième zone (34), en énergie de rotation, et par des moyens (16, 17,
18) pour transmettre ladite énergie de rotation audit plateau (11) pour l'entraîner
en rotation.
14. Dispositif selon la revendication 13, dans lequel existent deux passages sans
fin (30) contenant une pluralité de pistons à déplacement libre (27), lesdits passages
(30) étant diamétralement opposés l'un à l'autre sur le plateau tournant (11).
15. Dispositif selon la revendication 13, dans lequel ledit passage (30) comprend
au moins deux zones courbes, dont les rayons de courbure sont différents.
16. Dispositif selon les revendications 14 et 15, dans lequel chacun desdits passages
(30) comprend une zone rectiligne, s'étendant radialement, reliant lesdites deux zones
courbes.
17. Dispositif selon la revendication 13, dans lequel lesdits moyens pour appliquer
une force successivement à chacun des pistons (27), comprennent un conduit (40) dirigeant
un milieu fluide entre lesdits pistons (27) dans la première zone (32) dudit passage
(30), pour y être détendu.
18. Dispositif selon la revendication 13, dans lequel chaque piston de ladite pluralité
de pistons à déplacement libre (27) a une forme sensiblement complémentaire à la section
droite dudit passage sans fin (30), pour obturer de façon substantielle le passage
à l'écoulement fluide autour desdits pistons (27), et pour répartir ledit fluide en
segments.
19. Dispositif selon la revendication 13, dans lequel ledit plateau (11) comprend
un disque et un arbre-support (13), coaxial audit axe central, pour soutenir ledit
disque.
20. Dispositif selon la revendication 19, dans lequel ledit arbre-support (13) est
solidaire dudit disque.
21. Dispositif selon la revendication 19, dans lequel lesdits moyens pour appliquer
une force comprennent un conduit (44) s'étendant en direction globalement radiale
à partir dudit axe central (12), autour duquel tourne ledit plateau (11), jusqu'à
ladite première zone du passage (30), et un organe d'amenée (43), communicant avec
ledit conduit (44), pour introduire un fluide expansible dans la première zone dudit
passage (30).
22. Dispositif selon la revendication 13, dans lequel le passage est pourvu d'un ou
de plusieurs orifices (31) placés de façon à permettre au fluide de sortir du passage
(30), afin de diminuer la pression à l'avant des pistons (27) et de favoriser leur
accélération dans la seconde zone.
23. Dispositif selon la revendication 13, dans lequel lesdits moyens pour convertir
l'énergie potentielle en énergie de rotation comprennent une roue (24, 25) comportant
des logements périphériques, répartis à sa circonférence, destinés à accueillir successivement
chacun desdits pistons (27), sur un côté dudit passage (30), dans la troisième zone
de celui-ci.
24. Dispositif selon la revendication 23, comportant des moyens intermédiaires d'engrènement
(17, 17', 18) accouplés à ladite roue (24, 25), et en prise avec des moyens immobiles
d'engrènement (16), montés coaxialement audit axe central (12).
25. Dispositif selon la revendication 14, dans lequel, pour chaque passage (30), lesdits
moyens pour convertir l'énergie potentielle en énergie de rotation comprennent des
roues (24, 25), disposées sur des côtés opposés de la trajectoire desdits pistons
(27), dans la troisième zone dudit passage (30), chaque roue étant pourvue de logements
périphériques répartis à sa circonférence, destinés à faire avancer chaque piston
(27) parvenu entre lesdites roues (24, 25), le long d'un passage (30).
26. Dispositif selon la revendication 25, comprenant des moyens intermédiaires d'engrènement
(17, 17', 18) accouplés à chaque roue à logements (24, 25), et en prise avec des moyens
immobiles (16) d'engrènement montés coaxialement audit axe central (12).
27. Dispositif pour convertir une première forme d'énergie en une seconde forme d'énergie,
caractérisé par un plateau (100), par des moyens-support dudit plateau en rotation
autour d'un axe central, par un passage sans fin (104), solidaire du plateau, situé
dans un plan perpendiculaire audit axe central, par une pluralité de pistons à déplacement
libre, placés dans le passage (104), ledit passage ayant des zones essentiellement
rectilignes (106, 108), de part et d'autre dudit axe central, lesdites zones rectilignes
étant reliées, à leurs extrémités opposées, par des zones courbes (110, 112), également
placées de part et d'autre dudit axe central, par des moyens pour appliquer une force
successivement à chacun des pistons, dans un segment de chacune des zones rectilignes
(106, 108), pour les propulser en direction centripète, sur le plateau tournant (100),
à l'encontre de la force centrifuge, lesdits pistons étant entraînés dans un mouvement
radial centrifuge, dans une autre partie de chacune desdites zones rectilignes (106,
108), sous l'effet de la force centrifuge, par des moyens pour convertir l'énergie
des pistons, mus de manière centrifuge par la force centrifuge, en énergie de rotation,
dans lesdites zones courbes (110, 112) et des moyens pour transmettre cette énergie
de rotation audit plateau (100) afin de la faire tourner.
28. Dispositif selon la revendication 27, dans lequel lesdits moyens pour convertir
l'énergie potentielle en énergie de rotation comprennent une roue (122, 124) comportant
des logements périphériques (126), répartis à sa circonférence, destinés à recevoir
successivement chacun desdits pistons dans une zone courbe (110, 112) dudit passage
(104).
29. Dispositif selon la revendication 28, dans lequel la périphérie extérieure de
ladite roue (122, 124) coincide globalement avec la périphérie interne d'une zone
courbe (110, 112) dudit passage (104).
30. Dispositif selon la revendication 28, comportant des moyens intermédiaires d'engrènement,
couplés à ladite roue (122, 124), en prise avec des moyens immobiles d'engrènement
montés coaxialement audit axe central.
31. Dispositif selon la revendication 30, dans lequel il y a des roues (122, 124)
susceptibles de recevoir successivement chacun des pistons dans chaque zone courbe
(110, 112) du passage (104), et des moyens intermédiaires d'engrénement accouplant
lesdites roues et lesdits moyens immobiles d'engrènement.
32. Dispositif selon la revendication 27, comportant une zone, dans chacune desdites
zones rectilignes (106, 108) dudit passage (104), dans laquelle les pistons sont propulsés
par la détente d'un gaz, et une autre zone, dans laquelle les pistons sont propulsés
par la force centrifuge.