EP2183529B1 - Verfahren zum umwandeln thermischer energie niedriger temperatur in thermische energie höherer temperatur mittels mechanischer energie und umgekehrt - Google Patents
Verfahren zum umwandeln thermischer energie niedriger temperatur in thermische energie höherer temperatur mittels mechanischer energie und umgekehrt Download PDFInfo
- Publication number
- EP2183529B1 EP2183529B1 EP08782795.2A EP08782795A EP2183529B1 EP 2183529 B1 EP2183529 B1 EP 2183529B1 EP 08782795 A EP08782795 A EP 08782795A EP 2183529 B1 EP2183529 B1 EP 2183529B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- working medium
- heat
- compressor
- relaxation
- circulation process
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 43
- 230000008569 process Effects 0.000 claims description 25
- 230000006835 compression Effects 0.000 claims description 20
- 238000007906 compression Methods 0.000 claims description 20
- 239000007788 liquid Substances 0.000 claims description 14
- 238000012546 transfer Methods 0.000 claims description 10
- 230000003247 decreasing effect Effects 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 4
- 229910052743 krypton Inorganic materials 0.000 claims description 3
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 claims description 3
- 229910052756 noble gas Inorganic materials 0.000 claims description 3
- 229910052724 xenon Inorganic materials 0.000 claims description 3
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 claims description 3
- 229910052786 argon Inorganic materials 0.000 claims description 2
- 229910052704 radon Inorganic materials 0.000 claims description 2
- SYUHGPGVQRZVTB-UHFFFAOYSA-N radon atom Chemical compound [Rn] SYUHGPGVQRZVTB-UHFFFAOYSA-N 0.000 claims description 2
- 230000000717 retained effect Effects 0.000 claims 2
- 230000002040 relaxant effect Effects 0.000 claims 1
- 239000007789 gas Substances 0.000 description 10
- 239000012530 fluid Substances 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- 230000001133 acceleration Effects 0.000 description 6
- 230000003068 static effect Effects 0.000 description 6
- 230000002829 reductive effect Effects 0.000 description 5
- 230000002441 reversible effect Effects 0.000 description 5
- 230000009467 reduction Effects 0.000 description 4
- 206010016352 Feeling of relaxation Diseases 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000017525 heat dissipation Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 230000002528 anti-freeze Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 125000004122 cyclic group Chemical group 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- LVGUZGTVOIAKKC-UHFFFAOYSA-N 1,1,1,2-tetrafluoroethane Chemical compound FCC(F)(F)F LVGUZGTVOIAKKC-UHFFFAOYSA-N 0.000 description 1
- VHUUQVKOLVNVRT-UHFFFAOYSA-N Ammonium hydroxide Chemical compound [NH4+].[OH-] VHUUQVKOLVNVRT-UHFFFAOYSA-N 0.000 description 1
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 235000011114 ammonium hydroxide Nutrition 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000012267 brine Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 235000020681 well water Nutrition 0.000 description 1
- 239000002349 well water Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B3/00—Self-contained rotary compression machines, i.e. with compressor, condenser and evaporator rotating as a single unit
Definitions
- the invention relates to a device for carrying out a method according to the invention with a compressor, a relaxation unit and in each case a heat exchanger for heat supply or heat dissipation, wherein the compressor and the expansion unit are rotatably mounted about an axis of rotation and the compressor or the expansion unit are configured such in that the working medium in the compressor is guided essentially radially outwardly with respect to the axis of rotation or substantially radially inward in the expansion unit, so that an increase or decrease in pressure is produced by increasing or decreasing the centrifugal force acting on the working medium ,
- thermodynamic cycle vaporizing, compressing, liquefying and expanding at a throttle of the working medium comprises; ie usually the physical state of the working medium changes.
- the refrigerant R134a or a mixture consisting inter alia of R134a is used, which, although having no ozon destroying effect, however, has a 1300 times higher greenhouse-forming effect than the same amount of CO 2 .
- Such processes which are carried out essentially according to the Carnot process, have a theoretical coefficient of performance or COP (Coefficient of Performance), ie a ratio of the heat given off to the electrical energy used of approximately 5.5 (when "pumping" the working medium from 0 to 35 ° C). In practice, however, at best a performance factor of 4.9 has been achieved; As a rule, today's good heat pumps achieve a coefficient of performance of approx. 4.7.
- thermodynamic cycle as ideal as possible to expose a gaseous working fluid to a strong centrifugal force field.
- the method shown is based on a Carnot cycle. Expansion of the gas is effected by passing the gas against the direction of centrifugal force; in an analogous manner, the gas is compressed as the gas flows in the direction of the centrifugal force.
- thermodynamic method which makes use of the centrifugal force.
- a runner rotatable about a shaft has a compression channel or an expansion channel and a connecting channel, wherein a compression or expansion of a gaseous working medium is effected via the centrifugal action.
- thermodynamic device which basically makes use of the centrifugal force, but here also a throttle point is provided, so that considerable friction losses occur.
- the object of the present invention is to improve the efficiency or the coefficient of performance in the conversion of low-temperature thermal energy into higher-temperature thermal energy by means of mechanical energy and vice versa.
- a noble gas in particular krypton, xenon, argon, or radon or a mixture thereof is preferably used as the working medium.
- the pressure in the closed cycle is at least 50 bar, in particular more than 70 bar, preferably substantially 100 bar, ie the pressure during the entire process is comparatively high. Due to the comparatively high pressure, the pressure loss in the heat exchanger can be kept low because the heat transfer at comparatively low flow rates is relatively high.
- the critical point is present at different pressure or temperature, depending on the working medium used.
- the total power efficiency is maximized by performing the relaxation in an entropy range which is as close as possible to the entropy of the respective critical point.
- the lower relaxation temperature is just above the critical point.
- the critical point can be adjusted by gas mixtures to the desired process temperature.
- the heat exchangers with the compressor and the expansion unit, in which the working medium is passed around the axis of rotation during the closed cycle process are formed co-rotating, so that the flow energy of the working medium is essentially maintained during the closed loop process.
- the heat exchangers each have at least one tube through which a liquid heat transfer medium flows.
- the expansion unit connects directly to the compressor via the heat exchanger.
- the wheels of the compressor and the expansion unit are mounted on a common rotary shaft.
- the pressure increase of the working medium can be achieved via a centrifugal acceleration when a mitcardendes with impellers of the compressor and the expansion unit housing is provided.
- a co-rotating heat exchanger is accommodated in the housing.
- the co-rotating heat exchanger is circumferentially arranged outside.
- a device results in a comparatively low overall weight, since the wall thickness of the working medium leading tubes can be made smaller than those of the working medium receiving housings.
- the pipeline system has linear compression tubes extending in the radial direction.
- the pipeline system has curved expansion tubes against the direction of rotation of the rotary shaft.
- the expansion tubes can be arcuately curved in cross section for the purpose of a structurally simple design.
- the expansion tubes it is also possible for the expansion tubes to have a curvature in cross-section with a radius that constantly reduces towards the center of rotation. This can reduce any turbulence in the piping system.
- a flow of the working medium in the piping system is reliably ensured if, in the piping system, a blade wheel rotating relative to the piping system is included.
- the paddle wheel which is designed as a compressor, expansion turbine or stator, be rotatably disposed, resulting in a relative movement to the rotating piping system due to the rotationally fixed arrangement.
- the impeller is associated with a motor for generating or using a relative movement to the piping system or a generator which converts the shaft power generated by the relative movement of the impeller into electrical energy.
- Fig. 1 schematically a process block diagram of a thermodynamic cycle is shown, as this is basically known in the prior art.
- an isentropic compression of the gaseous working medium is initially carried out with the aid of a compressor 1.
- isobaric heat removal takes place via a heat exchanger 2, so that the thermal energy is delivered at high temperature via a circuit (with water, water / antifreeze or other liquid heat transfer media) to a heating circuit.
- a turbine formed relaxation unit 3 an isentropic relaxation is performed, whereby mechanical energy is recovered.
- an isobaric heat supply is performed via a further heat exchanger 4, whereby thermal energy of low temperature is supplied to the system via a circuit (with water, water / antifreeze, brine or other liquid heat transfer media).
- thermal energy from well water, from so-called deep probes, in which the located in a heat exchanger located up to 200 m in the ground, the heat is removed and the heat pump is supplied or the thermal energy from just under the earth lying large heat exchangers (Piping) or taken from the air.
- an isentropic compression is again effected with the aid of the compressors 1, as described above.
- the cycle described above takes place in the reverse order.
- a motor 5 for driving a rotary shaft 5 ' is provided;
- the engine is replaced by a generator 5 and motor generator 5.
- a device in which by means of the motor 5 via the rotary shaft 5 ', a compressor 1 is driven with a co-rotating housing 6. With the driven by the electric motor 5 rotating shaft 5 'wheels 1' of the compressor 1 are also driven, so that in the closed, stationary housing 8 recorded noble gas, preferably krypton or xenon, is compressed due to the centrifugal acceleration in the co-rotating housing 6 ,
- noble gas preferably krypton or xenon
- a spiral-shaped pipe 9 of the heat exchanger 2 is accommodated, in which a heat exchange medium, for example water, is accommodated.
- the comparatively cold water is introduced via an inlet 10 in the flow direction 10 'in the spiral pipe 9 and is circumferentially arranged in the co-rotating housing 6 to achieve isobaric heat removal from the working medium at the highest possible pressure of the working medium, so that at the output 11 a comparatively warm water can be removed.
- the working medium then flows without significant flow losses to impellers 3 'of the expansion unit 3, via which mechanical energy is recovered. Subsequently, an isobaric heat supply takes place via a spiral-shaped pipe 12 of the further heat exchanger 4 in the stationary housing 8, before the working medium is again subjected to an adiabatic isentropic compression via the running wheels 1 'of the compressor 1.
- the energy of the working medium which is accommodated in the device forming a closed system, maintains its flow energy during compression in the compressor 1 and / or during expansion in the expansion unit 3 and only via a centrifugal acceleration of the gas molecules of the working medium an increase in pressure or reduction of the working medium is achieved.
- the efficiency or the coefficient of performance in the conversion of thermal energy of lower temperature into thermal energy of higher temperature by means of electrical or mechanical energy and vice versa can be substantially improved.
- Fig. 3 is shown a further embodiment, in which case a stationary inner housing 6 'is provided.
- the design complexity is simplified.
- the stationary surfaces with which the working fluid is in communication formed as smooth as possible and there are no transverse to the flow heat transfer tubes, which would further increase the pressure loss provided .
- the spiral-shaped pipe 9 of the heat exchanger 2 is not exposed, but received in the stationary housing 6 'with a smooth surface 2'.
- an insulation 13 is accommodated in the interior of the stationary housing 6 '.
- Fig. 4 a further embodiment is shown, which is essentially that of Fig. 3 corresponds and only the arrangement of the motor 5 different; Namely, in this embodiment, the motor 5 is accommodated within the fixed housing 6.
- a further embodiment of the device according to the invention is shown, in which case all under the pressure of the working fluid parts are formed as pipes or piping system 17, whereby the total weight of the device is reduced and the wall thickness of the tubes 17 may be made smaller than that of the in the Fig. 2 to 4 shown housing 6, 6 'and 8.
- the working fluid is first compressed in the radially extending compression tubes 18 of the piping system 17 of the compressor unit 1 due to the centrifugal acceleration.
- the heat exchanger 2 in this case has to the outer, extending in the axial direction portion of the tubes 17 coaxially arranged tubes 19 which enclose the respective tube 17, so that the heat of the compressed working medium is discharged in countercurrent to the liquid heat exchange medium of the heat exchanger 2.
- the expansion tubes 20 are in this case curved counter to the direction of rotation 21 of the device, which due to the rearward tube curvature (see. Fig. 7 ) reliably results in a circulation of the working medium.
- the expansion tubes 20 can be bent in a semicircular shape, so that they can be produced in a structurally simple manner. Subsequently, the working medium flows in the axial direction in the piping system 17, in which case the low-pressure heat exchanger 4 in turn has a coaxially arranged tube 19, so that heat from the liquid heat exchange medium to the cold, relaxed working medium is delivered.
- piping system 17 for the working medium, which are arranged offset by 90 ° to each other.
- the piping system 17 may also have a larger number of conduits 20, only the rotational symmetry of the arrangement is to be maintained due to the ease of balancing.
- the coaxial with the axially extending portions of the tubes 17 arranged tubes 19 of the heat exchanger 2 and 4 are connected via lines 22, 23, 24, 25 fluidly connected to each other, said conduit system 22 to 25 is fixedly connected to the other device, so that the lines 22 to 25 are carried out co-rotating.
- the liquid heat transfer medium is supplied to the piping system 17 via an inlet 26 'of a static distributor 26; via a co-rotating manifold 27, the heat exchange medium is then supplied via the line 22 to the heat exchanger 2, in which it is heated by the line 23 in the co-rotating manifold 27 is recycled.
- the heated heat transfer medium is then fed to the heating circuit via the static distributor 26 or a drain 26 ".
- the cold heat exchange medium of the heat exchanger 4 is passed via an inlet 28 'of a static distributor 28, conveyed with another co-rotating distributor 29 in this co-rotating line 25 to the low-pressure heat exchanger 4, where heat is released to the gaseous working medium. Subsequently, the heat exchange medium is supplied via the co-rotating line 25 to the co-rotating distributor 29 then the static manifold 28, and finally leaves via a drain 28 '' the device.
- a motor 5 For driving compressor 1, heat exchanger 2, 4 and relaxation unit 3, in turn, a motor 5 is provided.
- FIGS. 8 and 9 is an embodiment similar to that of FIGS. 5 to 7 shown, but here are the expansion tubes 20 are not circular arc-shaped in cross-section, but have a continuously decreasing radius to the rotation axis center 30. As a result, a monotonically decreasing delayed movement of the working medium is achieved, whereby any turbulence can be reduced.
- two offset by 60 ° to each other arranged independent piping 17, where per pipe system 17 three densifications, relaxations, etc. take place.
- Fig. 10 a further embodiment is shown, which is largely that according to the FIGS. 5 to 7 corresponds, however, the circulation of the working medium is not achieved due to the direction of rotation curved tubes 20, but with the help of a paddle wheel 31, which acts as a compressor or as a turbine.
- the impeller 31 is arranged stationary, wherein due to the relative rotational movement to the surrounding the impeller 31 tubes 17, a flow of the working medium in the tubes 17 is effected.
- the working medium is expanded in the tubes 17 of the expansion unit 3 and the impeller 31 is fed, wherein the impeller 31 is received in a Schaufelradgephase 32, which is closed by a cover 33.
- the impeller 31 is rotatably supported by bearings 34, however, has permanent magnets 35 which cooperate with non-rotatably mounted outside the Schaufelradgephaseuses 32 permanent magnet 36, so that the impeller 31 is arranged rotationally fixed.
- the magnets 36 are held resting on a static shaft 37 here.
- Fig. 11 is one to the in Fig. 10 shown embodiment very similar trained device shown, but here the relative rotational movement of the paddle wheel 31 to the tubes 17 of the compressor and relaxation unit 1 and 3 by means of a motor 38 is generated.
- the motor 38 is rotatably connected to the co-rotating manifold 27.
- the power supply takes place via lines 39, which are accommodated in a shaft 40.
- the shaft 40 contacts 41.
- the motor 5 in this embodiment only provides power to overcome the aerodynamic drag of the rotating system.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL08782795T PL2183529T3 (pl) | 2007-07-31 | 2008-07-21 | Sposób przemiany energii termalnej niskiej temperatury w energię termalną wyższej temperatury przy pomocy energii mechanicznej i odwrotnie |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT0120307A AT505532B1 (de) | 2007-07-31 | 2007-07-31 | Verfahren zum umwandeln thermischer energie niedriger temperatur in thermische energie höherer temperatur mittels mechanischer energie und umgekehrt |
PCT/AT2008/000265 WO2009015402A1 (de) | 2007-07-31 | 2008-07-21 | Verfahren zum umwandeln thermischer energie niedriger temperatur in thermische energie höherer temperatur mittels mechanischer energie und umgekehrt |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2183529A1 EP2183529A1 (de) | 2010-05-12 |
EP2183529B1 true EP2183529B1 (de) | 2017-05-24 |
Family
ID=40134859
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08782795.2A Active EP2183529B1 (de) | 2007-07-31 | 2008-07-21 | Verfahren zum umwandeln thermischer energie niedriger temperatur in thermische energie höherer temperatur mittels mechanischer energie und umgekehrt |
Country Status (16)
Country | Link |
---|---|
US (1) | US8316655B2 (ko) |
EP (1) | EP2183529B1 (ko) |
JP (1) | JP5833309B2 (ko) |
KR (1) | KR101539790B1 (ko) |
CN (1) | CN101883958B (ko) |
AT (1) | AT505532B1 (ko) |
AU (1) | AU2008281301B2 (ko) |
BR (1) | BRPI0814333A2 (ko) |
CA (1) | CA2694330C (ko) |
DK (1) | DK2183529T3 (ko) |
ES (1) | ES2635512T3 (ko) |
HU (1) | HUE033411T2 (ko) |
NZ (1) | NZ582993A (ko) |
PL (1) | PL2183529T3 (ko) |
RU (1) | RU2493505C2 (ko) |
WO (1) | WO2009015402A1 (ko) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT509231B1 (de) * | 2010-05-07 | 2011-07-15 | Bernhard Adler | Vorrichtung und verfahren zum umwandeln thermischer energie |
EP2489839A1 (en) * | 2011-02-18 | 2012-08-22 | Heleos Technology Gmbh | Process and apparatus for generating work |
EP2810001B1 (de) * | 2012-02-02 | 2019-04-10 | Magna Powertrain Bad Homburg GmbH | Verdichter-wärmetauscher-einheit für ein heiz-kühl-modul für ein kraftfahrzeug |
AT515210B1 (de) * | 2014-01-09 | 2015-07-15 | Ecop Technologies Gmbh | Vorrichtung zum Umwandeln thermischer Energie |
AT515217B1 (de) * | 2014-04-23 | 2015-07-15 | Ecop Technologies Gmbh | Vorrichtung und Verfahren zum Umwandeln thermischer Energie |
US10578342B1 (en) * | 2018-10-25 | 2020-03-03 | Ricardo Hiyagon Moromisato | Enhanced compression refrigeration cycle with turbo-compressor |
CN109855913A (zh) * | 2019-03-04 | 2019-06-07 | 中国地质科学院水文地质环境地质研究所 | 地下水放射性惰性气体核素测年采样系统及其采样方法 |
DE102019009076A1 (de) * | 2019-12-28 | 2021-07-01 | Ingo Tjards | Kraftwerk zur Erzeugung elektrischer Energie |
Family Cites Families (30)
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US2393338A (en) * | 1941-03-13 | 1946-01-22 | John R Roebuck | Thermodynamic process and apparatus |
US2490064A (en) * | 1945-01-12 | 1949-12-06 | Kollsman Paul | Thermodynamic machine |
US2490065A (en) * | 1945-08-27 | 1949-12-06 | Kollsman Paul | Thermodynamic machine |
US4524587A (en) * | 1967-01-10 | 1985-06-25 | Kantor Frederick W | Rotary thermodynamic apparatus and method |
US3470704A (en) * | 1967-01-10 | 1969-10-07 | Frederick W Kantor | Thermodynamic apparatus and method |
NL7108157A (ko) * | 1971-06-14 | 1972-12-18 | ||
USB316851I5 (ko) * | 1972-02-22 | 1975-01-28 | ||
US3926010A (en) * | 1973-08-31 | 1975-12-16 | Michael Eskeli | Rotary heat exchanger |
NL7607040A (nl) * | 1976-06-28 | 1977-12-30 | Ultra Centrifuge Nederland Nv | Installatie voorzien van een holle rotor. |
JPS5424346A (en) * | 1977-07-25 | 1979-02-23 | Ultra Centrifuge Nederland Nv | Hollow rotor equipped facility |
US4211092A (en) * | 1977-09-22 | 1980-07-08 | Karsten Laing | Space heating installation |
FR2406718A1 (fr) * | 1977-10-20 | 1979-05-18 | Bailly Du Bois Bernard | Procede de conversion thermodynamique de l'energie et dispositif pour sa mise en oeuvre |
DE3018756A1 (de) * | 1980-05-16 | 1982-01-21 | Stolz, Oleg, 5000 Köln | Vorrichtung zur entropieaenderung eines arbeitsmittels |
US4438636A (en) * | 1982-06-21 | 1984-03-27 | Thermo Electron Corporation | Heat-actuated air conditioner/heat pump |
US4420944A (en) * | 1982-09-16 | 1983-12-20 | Centrifugal Piston Expander, Inc. | Air cooling system |
US4433551A (en) * | 1982-10-25 | 1984-02-28 | Centrifugal Piston Expander, Inc. | Method and apparatus for deriving mechanical energy from a heat source |
AU5692586A (en) * | 1985-04-16 | 1986-11-05 | Kongsberg Vapenfabrikk A/S | Heat pump |
US4984432A (en) * | 1989-10-20 | 1991-01-15 | Corey John A | Ericsson cycle machine |
US5274997A (en) * | 1991-10-31 | 1994-01-04 | Honda Giken Kogyo Kabushiki Kaisha | Gas turbine engine |
US5906108A (en) * | 1992-06-12 | 1999-05-25 | Kidwell Environmental, Ltd., Inc. | Centrifugal heat transfer engine and heat transfer system embodying the same |
CN2201628Y (zh) * | 1993-07-01 | 1995-06-21 | 杨建林 | 整体旋转式制冷装置及其动力装置 |
US5355691A (en) * | 1993-08-16 | 1994-10-18 | American Standard Inc. | Control method and apparatus for a centrifugal chiller using a variable speed impeller motor drive |
WO1995017606A1 (en) * | 1993-12-22 | 1995-06-29 | Entropy Systems, Inc. | Device and method for thermal transfer using air as the working medium |
FR2749070B3 (fr) * | 1996-05-24 | 1998-07-17 | Chaouat Louis | Pompe a chaleur sans cfc (chlorofluorocarbone) pour congelateurs domestiques et industriels |
SE511741C2 (sv) * | 1997-01-14 | 1999-11-15 | Nowacki Jan Erik | Motor, kylmaskin eller värmepump |
RU2170890C1 (ru) * | 2000-07-26 | 2001-07-20 | Белгородский государственный университет | Пароротационная холодильная машина |
JP3858744B2 (ja) * | 2002-04-09 | 2006-12-20 | 株式会社デンソー | 遠心式送風機 |
US6679076B1 (en) * | 2003-04-17 | 2004-01-20 | American Standard International Inc. | Centrifugal chiller with high voltage unit-mounted starters |
US8051655B2 (en) * | 2004-10-12 | 2011-11-08 | Guy Silver | Method and system for electrical and mechanical power generation using stirling engine principles |
US7600961B2 (en) * | 2005-12-29 | 2009-10-13 | Macro-Micro Devices, Inc. | Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of rotor blades |
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2007
- 2007-07-31 AT AT0120307A patent/AT505532B1/de not_active IP Right Cessation
-
2008
- 2008-07-21 KR KR1020107002494A patent/KR101539790B1/ko active IP Right Grant
- 2008-07-21 HU HUE08782795A patent/HUE033411T2/hu unknown
- 2008-07-21 US US12/671,314 patent/US8316655B2/en active Active
- 2008-07-21 PL PL08782795T patent/PL2183529T3/pl unknown
- 2008-07-21 EP EP08782795.2A patent/EP2183529B1/de active Active
- 2008-07-21 DK DK08782795.2T patent/DK2183529T3/en active
- 2008-07-21 ES ES08782795.2T patent/ES2635512T3/es active Active
- 2008-07-21 NZ NZ582993A patent/NZ582993A/en unknown
- 2008-07-21 BR BRPI0814333-1A2A patent/BRPI0814333A2/pt not_active Application Discontinuation
- 2008-07-21 AU AU2008281301A patent/AU2008281301B2/en active Active
- 2008-07-21 RU RU2010105705/06A patent/RU2493505C2/ru active
- 2008-07-21 WO PCT/AT2008/000265 patent/WO2009015402A1/de active Application Filing
- 2008-07-21 CN CN2008801013726A patent/CN101883958B/zh active Active
- 2008-07-21 JP JP2010518460A patent/JP5833309B2/ja active Active
- 2008-07-21 CA CA2694330A patent/CA2694330C/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20100199691A1 (en) | 2010-08-12 |
CN101883958A (zh) | 2010-11-10 |
AU2008281301A1 (en) | 2009-02-05 |
PL2183529T3 (pl) | 2017-10-31 |
JP5833309B2 (ja) | 2015-12-16 |
JP2010534822A (ja) | 2010-11-11 |
CN101883958B (zh) | 2013-11-20 |
KR20100051060A (ko) | 2010-05-14 |
HUE033411T2 (hu) | 2017-12-28 |
BRPI0814333A2 (pt) | 2015-01-20 |
RU2010105705A (ru) | 2011-08-27 |
KR101539790B1 (ko) | 2015-07-28 |
AT505532B1 (de) | 2010-08-15 |
ES2635512T3 (es) | 2017-10-04 |
AT505532A1 (de) | 2009-02-15 |
RU2493505C2 (ru) | 2013-09-20 |
US8316655B2 (en) | 2012-11-27 |
DK2183529T3 (en) | 2017-08-28 |
AU2008281301B2 (en) | 2012-12-06 |
CA2694330A1 (en) | 2009-02-05 |
CA2694330C (en) | 2014-07-15 |
NZ582993A (en) | 2011-10-28 |
EP2183529A1 (de) | 2010-05-12 |
WO2009015402A1 (de) | 2009-02-05 |
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