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GB2128258A - Gravity actuated thermal motor - Google Patents

Gravity actuated thermal motor Download PDF

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Publication number
GB2128258A
GB2128258A GB08325696A GB8325696A GB2128258A GB 2128258 A GB2128258 A GB 2128258A GB 08325696 A GB08325696 A GB 08325696A GB 8325696 A GB8325696 A GB 8325696A GB 2128258 A GB2128258 A GB 2128258A
Authority
GB
United Kingdom
Prior art keywords
chamber
chambers
motor
hot
motor according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB08325696A
Other versions
GB8325696D0 (en
Inventor
Salah Djelouah
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sorelec
Original Assignee
Sorelec
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sorelec filed Critical Sorelec
Publication of GB8325696D0 publication Critical patent/GB8325696D0/en
Publication of GB2128258A publication Critical patent/GB2128258A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03GSPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G6/00Devices for producing mechanical power from solar energy
    • F03G6/002Devices for producing mechanical power from solar energy with expansion and contraction elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03GSPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G3/00Other motors, e.g. gravity or inertia motors
    • F03G3/087Gravity or weight motors
    • F03G3/091Gravity or weight motors using unbalanced wheels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03GSPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G6/00Devices for producing mechanical power from solar energy
    • F03G6/003Devices for producing mechanical power from solar energy having a Rankine cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2254/00Heat inputs
    • F02G2254/30Heat inputs using solar radiation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/46Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sustainable Development (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Energy (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Valve Device For Special Equipments (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Permanent Magnet Type Synchronous Machine (AREA)
  • Power Steering Mechanism (AREA)

Abstract

The motor comprises a rotor carrying sealed chambers 2, 3 containing a fluid which vaporises and condenses successively when the chambers pass a hot zone SC and a cold zone SF. Within the chambers are deformable pockets 5, 6 interconnected by a tube 4 and containing a transmission liquid. The vaporisation pressure of the fluid in the chambers passing the hot zone compresses the pockets therein and forces some of the transmission liquid to pass into the pockets in the cold zone and thereby rotate the rotor about its shaft 7. Solar heat may be utilised. The chambers 2, 3 may be provided with blades (18), Fig. 2 (not shown), in order to obtain additional drive from hot and cold gas flows 13-16. <IMAGE>

Description

SPECIFICATION Rotary motor This invention relates to a rotary thermodynamic fluid motor comprising a set of units which are integrally connected for rotation and each formed by two rigid constantvolume equidistant chambers containing a thermodynamic fluid which successively vaporizes and condenses depending on whether the chamber is subjected to the effect of the hot source or the cold source, the chambers being rigid constant-volume chambers.
The invention relates more particularly to a solar mill which converts thermodynamic energy into mechanical and electrical energy by means of a thermodynamic fluid in constant equilibrium (liquid vapour) and in a looped circuit, and a second fluid (water, oil, etc.) or a rocking member.
Solar systems of this kind are already known, wherein thermodynamic energy is converted into mechanical energy, either by the vaporization of a fluid or by way of a gas engine using the Carnot cycle.
These two types of installation which are at present available on the market are complex; gas engines require complex installations (collector, evaporator, condenser, expansion motor, reinjection pump, and so on).
Apart from the very high investments they require, these installations also need permanent technical assistance. Their efficiency is also mediocre. Some applications are in the form of gadgets, because they cannot be industrialized.
These gadgets are based on the following principle: A liquid which evaporates, the pressure of the reservoir being increased. This pressure causes a liquid to rise in an equilibrium system, causes the assembly to rock and returns to its initial position.
This is the principle applied in toys of the kind in which a bird repeatedly dips its beak into water.
The object of this invention is to provide a rotary motor of the above type adapted to deliver a relatively high power to drive a load, and the operation of which is not rapidly disturbed by the unbalance of the corresponding chambers.
To this end, the invention relates to a motor characterised in that each module comprises a sealed deformable chamber containing thermodynamic fluid and a heavy transmission means which immediately and integrally transmits any variation in the volume of one of the chambers to the other chamber, the transmission means thus assuming an unbalanced position which produces a torque which is transmitted to the motor shaft.
According to another feature, the transmission means is either a set of two pistons connected by a connecting means provided with a heavy weight, or a column of liquid. The two pistons may also comprise flexible partitions or pockets.
In the inoperative state, when the temperature of the cold source is the same as that of the hot source, the system is in equilibrium: The thermodynamic fluid masses contained in the two chambers are equal and the heavy transmission means is at equilibrium.
A torque is'applied to the motor output shaft only as a result of the unbalance resulting from the movement of the heavy transmission means in response to the pressure difference in the two chambers of the diametrically opposite modules of each unit.
The invention will be described in greater detail with reference to the accompanying drawings wherein: Fig. 1 is a diagram showing the principle of a motor according to the invention.
Fig. 2 is a section on the line Il-Il in Fig. 1.
Fig. 3 is a section on Ill-Ill in Fig. 1.
Fig. 4 is a perspective of another embodiment.
Fig. 5 is a section through a central plane of the embodiment shown in Fig. 4.
Figs. 6 and 7 are diagrams of two embodiments of a tunnel.
Referring to Fig. 1 , the thermodynamic fluid rotary motor comprises a set of modules 1 each formed by two chambers 2, 3 interconnected, for example, by a diametric arm 4 which also forms a connecting tube.
Each chamber 2, 3 contains a pocket 5, 6; the two pockets of the corresponding two chambers communicate via the tube 4. The volume defined respectively between each chamber 2, 3 and the pocket 5, 6 is sealed off and contains a thermodynamic fluid, i.e., a fluid adapted to vaporize at the temperature of the hot source SC and condense at the temperature of the cold source SF. Since the temperatures of the hot and cold sources SC and SF respectively depend on the utilization conditions, the thermodynamic fluid is selected accordingly.
The assembly comprising the two pockets 5, 6 and the tube 4 forms a constant closed volume with two deformable parts formed by the pockets 5, 6. Any reduction in volume of one of the pockets 5, 6 has the effect of increasing the volume of the other pocket 6, 5, since the volume thus closed contains a non-compressible fluid, preferably a liquid, e.g. water, or a liquid of higher density.
All the movable units 2, 3 are integral with an output shaft 7. Since the torque exerted by each movable unit depends on the difference in weight between the two pockets 5, 6, the hot source SC acts on one vertical half of the system and the cold source SF acts on the other vertical half thereof.
In each plane, the shaft 7 contains as many movable units as the size of the chambers 2, 3 allows. A plurality of movable units can be juxtaposed on the same shaft.
According to one embodiment, the hot source SC comprises a toric passage of circular section corresponding to a hemi-torus. Passage 8 is a solar radiation absorber. The cold source SF also comprises a passage 9 of circular section and of toric shape corresponding to a hemi-torus. The cold source and hot source passages 8, 9 correspond to the same torus.
The hot source passage 8 comprises a jacket 10 which forms a heat absorber surrounded by a transparent jacket 11 giving a hothouse effect.
The cold source passage 9 has an outer wall 12, e.g. of felt, on to which water is dropped, said water drawing the heat by evaporation and enabling the passage and hence the chambers to be cooled as they pass through the passage.
The movement can also be accelerated by a chimney effect by the flow of the hot and cold gases in the two passages, with hot and cold air intakes 13, 14 and outlets 15, 16, e.g. Canadian wells which deliver hot or cold air depending upon whether the exterior is the hot or cold source and the Canadian well the cold or hot source.
Finally, the system may be associated with any other natural energy recovery device.
Fig. 2 is a section on the line Il-lI in Fig. 1 and shows the structure of the system at the hot source, whose passage operates by the hothouse effect. This section shows the outer transparent jacket 11 containing a layer of air, and then the absorbent material of the absorber 10 which defines the passage 8 in which the chambers 2, 3 move. The chambers 2, 3 of each unit, which are preferably spheres or quadrilaterals of a highly conductive material such as copper or aluminium, contain the deformable jacket 5, 6, which is preferably a poor conductor in order to limit the exchange of heat or cold to the incompressible fluid.
Fig. 3 shows the structure of the system of Fig.
2 at the cold source SF, showing the opaque liquid-absorbent jacket 12, e.g. felt, defining the passage 9 through which the chambers 2, 3 move.
Referring to Figs. 2 and 3, aprons 1 7 provide the seal between the tubes 4 carrying the chambers 2, 3 and the hot source and cold source passages 8, 9. The seal may be provided in some other way by replacing the radial tubes 4 by a rotor or at least by providing the outer part of the tubes 4 where they pass into the hot and cold source passages 8, 9 with a ring which provides a seal by sliding or rolling contact on counter-acting sealing means provided in the hot and cold source passages 8, 9.
To be able to utilize the rising flow of hot and cold gases in the hot and cold source passages it is advantageous to provide the chambers at least partially with blades 18 to improve the transmission of the movement.
Finally, the hot source may be replaced by a basin which heats up in response to solar radiation or which contains hot recuperation water and into which the chambers are successively immersed for heating, the cold source being formed by the exterior of the basin.
Referring to Figs. 4 and 5, the motor comprises a stator 20 and a rotor 21.
The stator 20 is in the form of a toric tunnel (compare Figs. 6 and 7) comprising an insulating jacket 22 of, for example, rectangular, square or circular section, surrounding a chamber 23 in which a heat-vehicle fluid flows, and a chamber 24 in which a coolant fluid flows. Each chamber 23, 24 corresponds substantially to a semi-circle.
Rotor 21 rotates in the free space defined by the chambers 23, 24.
In a first embodiment (modules 25, 26), rotor 21 comprises a set of modules comprising a flexible partition 27 respectively defining chambers 28, 29 and 30,31.
Chambers 28, 30 contain a thermodynamic fluid adapted to vaporize and condense at the temperatures of the hot and cold sources of the motor.
The chambers 29, 31 are connected by a duct 32 and the whole of the volume thus defined contains a liquid whose boiling temperature is much higher than that of the hot source.
The liquid is thus delivered partially from the chamber (e.g. 29) on the hot source side to the chamber 31 on the cold source side, thus unbalancing the module and producing a driving torque which is applied to the motor output shaft.
Fig. 5 shows the deformation and position of the two partitions 27; in this example, the partitions are deformable but they could be replaced by a partition acting as a piston and enclosing a column of liquid.
According to another variant, which is not illustrated, for the purpose of increasing the motor possibilities the mass displaced during each cycle is increased. To this end, the two pistons can be connected by a piston rod which can be loaded by a weight if required.
Referring to Fig. 5, according to another embodiment, the module comprises two chambers 33, 34 each containing a deformable pocket 35 containing a thermodynamic fluid.
As before, the chambers 33, 34 are connected by a duct 36 via which they communicate. The volume thus defined contains a liquid which is inert at the installation operating temperatures, i.e.
it does not evaporate at the hot source temperature.
Vaporization of the thermodynamic liquid in the chamber 33 on the hot source side causes liquid to be delivered to chamber 34 on the cold source side and thus produces a driving torque.
Advantageously, to improve operation, the chambers of the different modules are insulated from one another.
The inlets and outlet of the heat-vehicle fluids of the hot and cold sources are denoted by references 37, 38; 39, 40.
Figs. 6 and 7 show two examples of tunnels for the hot and cold sources. The tunnels have a passage 41 for the ducts 32, 36 on the side facing the centre of the torus.
Finally, to prevent the partition 27 or pocket 35 from clogging the ducts 32, 36 the latter have a protective means 42 (Fig. 5).
The rotor 21 shown in Fig. 5 can also be applied to a hot source comprising the direct solar radiation. In that case the tunnel of the stator 20 is omitted at least in the part forming the hot source, or is replaced by a hothouse effect tunnel.

Claims (7)

1. A rotary thermodynamic fluid motor, comprising a set of units which are connected for rotation and each formed by two rigid constantvolume modules situated diametrically opposite one another and containing a thermodynamic fluid which vaporizes and condenses successively depending on whether the module is subjected to the effect of the hot source or the cold source, the said motor being characterised in that each module comprises a sealed deformable chamber (6, 28, 30, 35) containing thermodynamic fluid and a heavy transmission means (4, 32, 36) which immediately and completely transmits any variation in the volume of one of the chambers (6, 28, 30, 35) to the other chamber, the transmission means thus assuming an unbalanced position which produces a torque which is transmitted to the motor shaft (7).
2. A motor according to claim 1, characterised in that the transmission means comprises a set of two pistons interconnected for movement and each piston forms the movable wall of each deformable chamber.
3. A motor according to claim 1, characterised in that the transmission means comprises a column (4) of liquid which is inert at the motor operating temperature and conditions, said column of liquid being contained between two pistons (5, 27, 35) defining the sealed variablevolume chambers each containing thermodynamic fluid.
4. A motor according to claim 3, characterised in that the pistons comprise deformable flexible partitions (27) or pockets (5, 35).
5. A motor according to any one of claims 1 to 4, characterised in that it comprises a stator (20) and a rotor (21), the stator (20) being in the form of a tunnel surrounded by a chamber (23) in which the heat-vehicle fluid of the hot source or of the cold source flows, said chamber in turn being enclosed by an insulating chamber (22) and the rotor (21) comprises different units formed by modules, the rotor moving in the chamber defined by the stator (20).
6. A motor according to claim 5, characterised in that the stator part corresponding to the hot source comprises a chamber which acts as a hothouse and the outer insulating chamber is omitted.
7. A motor according to claim 6, characterised in that the successive chambers of the different modules are thermally insulated from one another.
GB08325696A 1982-10-06 1983-09-26 Gravity actuated thermal motor Withdrawn GB2128258A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8216768A FR2534321B1 (en) 1982-10-06 1982-10-06 ROTARY MOTOR

Publications (2)

Publication Number Publication Date
GB8325696D0 GB8325696D0 (en) 1983-10-26
GB2128258A true GB2128258A (en) 1984-04-26

Family

ID=9278029

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08325696A Withdrawn GB2128258A (en) 1982-10-06 1983-09-26 Gravity actuated thermal motor

Country Status (12)

Country Link
JP (1) JPS5987281A (en)
AU (1) AU1990583A (en)
BE (1) BE897859A (en)
BR (1) BR8305518A (en)
CH (1) CH654877A5 (en)
DE (1) DE3336406A1 (en)
ES (1) ES8405897A1 (en)
FR (1) FR2534321B1 (en)
GB (1) GB2128258A (en)
IT (1) IT1194417B (en)
MA (1) MA19922A1 (en)
PT (1) PT77437B (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997027401A1 (en) * 1996-01-22 1997-07-31 Daniel Charles Henri Masse Asymmetrical hydrodynamic energy converter
GB2376722A (en) * 2001-06-20 2002-12-24 Michael John Miles Gravity actuated wheel
WO2003089767A1 (en) * 2002-04-15 2003-10-30 Shimshi, Ezra Buoyant-orbicular-seesaw-system (boss)
US7080509B2 (en) * 2004-12-27 2006-07-25 Ezra Shimshi System for obtaining rotational energy from ambient forces
GB2451660A (en) * 2007-08-08 2009-02-11 Samuel Edmund Livermore Heat to kinetic energy converter
WO2011057402A1 (en) * 2009-11-15 2011-05-19 Dyverga Energy Corporation Low differential temperature rotary engines
WO2012155246A1 (en) * 2011-05-14 2012-11-22 Dyverga Energy Corporation Low differential temperature rotary engines
US20130205768A1 (en) * 2008-08-04 2013-08-15 Seong Woong Kim Engine for energy conversion
WO2013170353A1 (en) * 2012-05-14 2013-11-21 Dyverga Energy Corporation External heat engines
EP2685100A1 (en) * 2012-07-09 2014-01-15 Philipp Rüede Heat engine
CN104454057A (en) * 2014-01-25 2015-03-25 周晓军 Temperature difference engine
ES2635613A1 (en) * 2016-10-28 2017-10-04 Zacarias CALVO MERIDA Gravitational engine (Machine-translation by Google Translate, not legally binding)
WO2019081785A1 (en) * 2017-10-28 2019-05-02 Calvo Merida Zacarias Gravitational engine

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU3851397A (en) * 1996-08-12 1998-03-06 Alfonso Laguens Marquesan Power generator by gravity unbalance of liquid fluid
DE19646887C1 (en) 1996-11-13 1998-06-18 Hasse Hans Helmut Contraction machine
WO2007034701A1 (en) * 2005-09-26 2007-03-29 Shinzo Ito Buoyancy power generating apparatus
JP5330618B1 (en) 2013-03-22 2013-10-30 博康 山本 Drive device
FR3145022A1 (en) 2023-01-18 2024-07-19 Jean-Pierre Gervais Independent Free Engine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3659416A (en) * 1970-07-14 1972-05-02 Harold Brown Vapor driven motors
US4121420A (en) * 1976-12-30 1978-10-24 Schur George O Gravity actuated thermal motor
US4307571A (en) * 1979-07-27 1981-12-29 Jackson Robert E Device driven by heat energy

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE17796C (en) * J. L. landis in Lancaster (Pennsylvanien, V. St. a.) Methods and devices for converting heat into work
DE674401C (en) * 1937-07-22 1939-04-15 Dr Emil Vladimir Tuschyckyj Tiltable steam pump
US2513692A (en) * 1947-07-07 1950-07-04 Charles L Tubbs Vapor engine driven by expansion and contraction of vapor
US4051678A (en) * 1975-03-12 1977-10-04 Yates John W Thermal panel powered heat engine
US4074534A (en) * 1977-02-03 1978-02-21 Morgan Wesley W Thermodynamic motor
US4177019A (en) * 1978-03-27 1979-12-04 Utah State University Foundation Heat-powered water pump

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3659416A (en) * 1970-07-14 1972-05-02 Harold Brown Vapor driven motors
US4121420A (en) * 1976-12-30 1978-10-24 Schur George O Gravity actuated thermal motor
US4307571A (en) * 1979-07-27 1981-12-29 Jackson Robert E Device driven by heat energy

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997027401A1 (en) * 1996-01-22 1997-07-31 Daniel Charles Henri Masse Asymmetrical hydrodynamic energy converter
FR2757897A1 (en) * 1996-01-22 1998-07-03 Masse Daniel Charles Henri ASYMMETRIC HYDRODYNAMIC POWER CONVERTERS
GB2376722A (en) * 2001-06-20 2002-12-24 Michael John Miles Gravity actuated wheel
WO2003089767A1 (en) * 2002-04-15 2003-10-30 Shimshi, Ezra Buoyant-orbicular-seesaw-system (boss)
US6644026B2 (en) * 2002-04-15 2003-11-11 Ezra Shimshi Buoyant-orbicular-seesaw-system (BOSS)
GB2401154A (en) * 2002-04-15 2004-11-03 Ezra Shimshi Buoyant-orbicular-seesaw-system (BOSS)
US7080509B2 (en) * 2004-12-27 2006-07-25 Ezra Shimshi System for obtaining rotational energy from ambient forces
GB2451660A (en) * 2007-08-08 2009-02-11 Samuel Edmund Livermore Heat to kinetic energy converter
US20130205768A1 (en) * 2008-08-04 2013-08-15 Seong Woong Kim Engine for energy conversion
US9267489B2 (en) * 2008-08-04 2016-02-23 Seong Woong Kim Engine for conversion of thermal energy to kinetic energy
WO2011057402A1 (en) * 2009-11-15 2011-05-19 Dyverga Energy Corporation Low differential temperature rotary engines
CN102725525A (en) * 2009-11-15 2012-10-10 戴沃格能源公司 Low differential temperature rotary engines
US9140144B2 (en) 2009-11-15 2015-09-22 Dyverga Energy Corporation Rotary gravity engine utilizing volatile material and low temperature heat sources
WO2012155246A1 (en) * 2011-05-14 2012-11-22 Dyverga Energy Corporation Low differential temperature rotary engines
WO2013170353A1 (en) * 2012-05-14 2013-11-21 Dyverga Energy Corporation External heat engines
EP2877744A4 (en) * 2012-05-14 2016-06-22 Dyverga Energy Corp EXTERNAL HEATING ENGINES
WO2014009297A3 (en) * 2012-07-09 2014-04-17 Philipp Rüede Heat engine
EP2685100A1 (en) * 2012-07-09 2014-01-15 Philipp Rüede Heat engine
CN104454057A (en) * 2014-01-25 2015-03-25 周晓军 Temperature difference engine
CN104454057B (en) * 2014-01-25 2017-03-15 周晓军 Temp difference engine
ES2635613A1 (en) * 2016-10-28 2017-10-04 Zacarias CALVO MERIDA Gravitational engine (Machine-translation by Google Translate, not legally binding)
WO2019081785A1 (en) * 2017-10-28 2019-05-02 Calvo Merida Zacarias Gravitational engine

Also Published As

Publication number Publication date
PT77437B (en) 1986-02-13
JPS5987281A (en) 1984-05-19
GB8325696D0 (en) 1983-10-26
DE3336406A1 (en) 1984-04-12
IT1194417B (en) 1988-09-22
IT8323123A0 (en) 1983-10-04
CH654877A5 (en) 1986-03-14
ES526238A0 (en) 1984-06-16
FR2534321B1 (en) 1988-12-16
IT8323123A1 (en) 1985-04-04
MA19922A1 (en) 1984-07-01
DE3336406C2 (en) 1990-05-31
BR8305518A (en) 1984-05-15
FR2534321A1 (en) 1984-04-13
PT77437A (en) 1983-10-01
ES8405897A1 (en) 1984-06-16
AU1990583A (en) 1985-04-18
BE897859A (en) 1984-01-16

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