Process and apparatus for transferring heat from a first medium to a second medium

Abstract

A process of transferring heat from a first relatively cold medium to a second relatively hot medium features rotating a contained amount of a compressible fluid about an axis of rotation, thus generating a radial temperature gradient in the fluid, and heating the second medium by the fluid in a section of the fluid relatively far from the axis of rotation. An apparatus for carrying out the process includes a gastight drum rotatably mounted in a frame, and a first heat exchanger mounted inside the drum relatively far from the axis of rotation of the drum.

Claims

1. A method of transferring heat from a first relatively cold medium to a second relatively hot medium and generating work, the method comprising: rotating a contained amount of a compressible fluid in a drum about an axis of rotation, forcibly mixing radial segments of the fluid within the drum by at least one axial ventilator arranged in a tube that is arranged in the drum and coaxial with a longitudinal axis of the drum, generating, based on the rotation of the contained amount of the compressible fluid about the axis of rotation, a radial temperature gradient in the fluid, extracting heat from the first medium by the fluid in a second heat exchanger in a section at or relatively close to the axis of rotation and heating the second medium by the fluid in a first heat exchanger in a section of the fluid relatively far from the axis of rotation, where the radial temperature in the fluid increases, based on the forced mixing of segments of the fluid, from the section at or relatively close to the axis of rotation to the section relatively far from the axis of rotation, wherein the first and second heat exchangers are coupled to a cycle for generating work, the cycle comprising: an evaporator or super-heater that is thermally coupled to the first heat exchanger, a condenser that is thermally coupled to the second heat exchanger, and a heat engine coupled with the evaporator and the condenser, and generating work with the cycle.

2. The method according to claim 1, further comprising circulating the fluid from the section at or relatively close to the axis of rotation to the section relatively far from the axis of rotation and back to the section at or relatively close to the axis of rotation.

3. The method according to claim 1, wherein the compressible fluid is contained in the drum having a diameter of at least 1.5 meter and is rotated at at least 50 RPM.

4. The method according to claim 1, further comprising rotating a contained amount of the compressible fluid about an axis of rotation in at least one of two or more drums and in two or more compartments of the at least one of two or more drums.

5. The method according to claim 1, wherein the compressible fluid contains or consists essentially of a mono-atomic element having an atomic number (Z)≧18.

6. A heat transfer apparatus for transferring heat from a first relatively cold medium to a second relatively hot medium, the apparatus comprising: a gastight drum rotatably mounted in a frame, a first heat exchanger mounted inside the drum relatively far from an axis of rotation of the drum, where the gastight drum is configured to rotate a compressible fluid about the axis of rotation of the drum to generate a radial temperature in the fluid that increases from a section at or relatively close to the axis of rotation to a section relatively far from the axis of rotation, one or more mixers to forcibly mix of segments of the fluid, and a second heat exchanger positioned at or relatively close to the axis of rotation, wherein at least one of the first or second heat exchangers is coupled to a cycle for generating work, the cycle comprising: an evaporator or super-heater, which is thermally coupled to the first heat exchanger, a condenser, thermally coupled to the second heat exchanger, and a heat engine coupled with the evaporator and condenser.

7. The apparatus according to claim 6, comprising one or more at least substantially cylindrical and co-axial walls, separating the inside of the drum into a plurality of compartments.

8. The apparatus according to claim 6, wherein at least one of the first or second heat exchangers comprises a coiled tube coaxial with the axis of rotation.

9. A method of transferring heat from a first relatively cold medium to a second relatively hot medium, the method comprising: rotating a contained amount of a compressible fluid about an axis of rotation, thus generating a radial temperature gradient in the fluid, heating the second medium by fluid in a section of the fluid relatively far from the axis of rotation; allowing an additional liquid to flow away from the axis of rotation, driving a generator with the liquid, evaporating the liquid by the fluid in a section of the fluid relatively far from the axis of rotation, pumping the vapor towards the axis of rotation; and condensing the vapor by the fluid in a section at or relatively close to the axis of rotation.

10. The method according to claim 1, wherein the compressible fluid is at a pressure in excess of 10 bar measured at the axis of rotation.

11. The method according to claim 1, where entropy of the compressible fluid decreases from the section at or relatively close to the axis of rotation to the section relatively far from the axis of rotation.

12. The method according to claim 1, wherein the compressible fluid is at a pressure in excess of 2 bar.

13. The method according to claim 1, wherein the compressible fluid is contained in the drum having a diameter of at least 1.5 meter and is rotated at at least 100 RPM.

14. The method according to claim 1, wherein the cycle comprises a Carnot or steam cycle.

15. The method according to claim 1, wherein the compressible fluid contains or consists essentially of a mono-atomic element having an atomic number (Z)≧36.

16. A heat transfer apparatus for transferring heat from a first relatively cold medium to a second relatively hot medium, the apparatus comprising: a gastight drum rotatably mounted in a frame, and a first heat exchanger mounted inside the drum relatively far from an axis of rotation of the drum, where the gastight drum is configured to rotate a compressible fluid about the axis of rotation of the drum to generate a radial temperature gradient in the fluid and heat the second medium in the first heat exchanger, a second heat exchanger positioned at or relatively close to the axis of rotation, where at least one of the heat exchangers is coupled to a cycle for generating work, the cycle comprising: an evaporator or super-heater, which is thermally coupled to the first heat exchanger, a condenser thermally coupled to the second heat exchanger, and a heat engine coupled with the evaporator and the condenser.

17. The method according to claim 1, further comprising heating the evaporator or super-heater with heat from the fluid via the first heat exchanger.

18. The method according to claim 1, further comprising cooling the condenser by transferring heat to the fluid via the second heat exchanger.

Description

DESCRIPTION OF DRAWINGS

(1) The invention will now be explained in more detail with reference to the drawings, which schematically show a presently preferred embodiment.

(2) FIGS. 1 and 2 are a perspective view and a side view of a first embodiment of the apparatus.

(3) FIG. 3 is a cross-section of a drum used in the embodiment of FIGS. 1 and 2.

(4) FIG. 4 is a cross-section of a second embodiment of the apparatus.

(5) FIG. 5 is a schematic layout of a power plant comprising the embodiment of FIG. 4.

(6) FIG. 6 illustrates an example embodiment that includes a drum, a radially extending tube for holding an additional liquid (not shown), a generator, a tube where the liquid can be subsequently evaporated by the relatively hot compressible fluid at or near the inner wall of the drum, a radially extending tube for transporting the vapor back to the center of the drum and a tube at or near the center of the drum where the vapor can be condensed by the relatively cold compressible fluid.

(7) Identical parts and parts performing the same or substantially the same function will be denoted by the same numeral.

DETAILED DESCRIPTION

(8) FIG. 1 shows an experimental setup of an artificial gravity apparatus 1. The apparatus 1 comprises a static base frame 2, firmly positioned on a floor, and a rotary table 3, mounted on the base frame 2. Driving means, e.g., an electromotor 4 are mounted in the base frame 2 and are coupled to the rotary table 3. To reduce drag, an annular wall 5 is fastened to the rotary table 3, along its circumference. Further, a cylinder 6 is fastened to the rotary table 3 and extends along a radius thereof.

(9) As shown in FIG. 3, the cylinder 6 comprises a center ring 7, two (Perspex™) outer cylinders 8, two (Perspex™) inner cylinders 9 mounted coaxially inside the outer cylinders 8, two end plates 10, and a plurality of studs 11, with which the end plates 10 are pulled onto the cylinders 8, 9, and the cylinders 8, 9, in turn, onto the center ring 7. The cylinder 6 has a total length of 1.0 meter. FIG. 3 is to scale.

(10) The lumen defined by the center ring 7, the inner cylinders 9, and the end plates 10, is filled with Xenon, at ambient temperature and a pressure of 1.5 bar, and further contains a plurality of mixers or ventilators 12. Finally, a Peltier element (not shown) is mounted on the inner wall of the ring 7 and temperature sensors and pressure gauges (also not shown) are present in both the ring 7 and the end plates 10.

(11) During operation, the rotary table 3 and hence the cylinder 6 is rotated at a speed of approximately 1000 RPM. Radial segments of the fluid are thoroughly mixed by the ventilators 12, to obtain an at least substantially constant entropy in these segments. In view of the fact that the process is reversible and in view of the thermal isolation provided by the inner and outer cylinders 8, 9, which isolation enables conducting substantially adiabatic processes, heat transfer within the cylinder 6, from the axis of rotation to the circumference and vice versa, is substantially isentropic.

(12) Upon rotation, the temperature and the pressure of the Xenon at the end plates 10 increase and the temperature and pressure at the ring 7 drop. When, upon reaching equilibrium, a stepped heat pulse is fed to the gas at the ring 7 by the Peltier element, temperature and pressure at the ring 7 increase and, subsequently, temperature and pressure at the end plates 10 increase, i.e., heat flows from a source having a relatively low temperature (the gas at the ring) to a source having a relatively high temperature (the gas at the end plates).

(13) FIG. 4 is a cross-section of a second artificial gravity apparatus 1. The apparatus 1 comprises a static base frame 2, firmly positioned on a floor, and a rotary drum 6, mounted, rotatable about its longitudinal axis, in the base frame 2, e.g., by suitable bearings, such as ball bearings 20. The drum 6 suitably has a diameter in a range from 2 to 10 meters, in this example 4 meters. The wall of the drum is thermally isolated in a manner known in itself. The apparatus 1 further comprises a driving means (not shown) to spin the drum at rates in a range from 50 to 500 RPM.

(14) The drum 7 contains (at least) two heat exchangers, a first heat exchanger 22 mounted inside the drum relatively far from the axis of rotation of the drum 7 and a second heat exchanger 23 positioned at or relatively close to said axis. In this example, both heat exchangers 22, 23 comprise a coiled tube coaxial with the axis of rotation and connected, via a first rotatable fluid coupling 24, to a supply and, via a second rotatable fluid coupling 25, to an outlet. In some aspects, the drum 7 may have a diameter of at least 1.5 meter and may be rotated at at least 50 RPM.

(15) The embodiment shown in FIG. 4 further comprises a tube 26, coaxial with the longitudinal axis of the drum 6 and containing an axial ventilator 27 to forcedly circulate the contents of the drum 6. In this example, the drum 6 is filled with Xenon at a pressure of 5 bar (at ambient temperature), whereas the heat exchangers 22, 23 are filled with water.

(16) FIG. 5 is a schematic layout of a power plant comprising the embodiment of FIG. 4, coupled to a cycle for generating work, in this example a so-called “steam cycle.” The cycle comprises an super-heater 30, coupled to the high temperature heat exchanger 22 of the apparatus 1, a heat engine, known in itself and comprising, in this example, a turbine 31, a condenser 32 coupled to the first heat exchanger 23 of the apparatus 1, a pump 33, and an evaporator 34. The steam cycle is also filled with water. Other suitable media are known in the art.

(17) Rotating the drum will generate a radial temperature gradient in the Xenon, with a temperature difference (ΔT) between the heat exchangers in a range from 100° C. to 600° C., depending on the angular velocity of the drum. In this example, the drum is rotated at 350 RPM resulting in a temperature difference (ΔT) of approximately 300° C. Water at 20° C. is fed to both heat exchangers 22, 23. Heated steam (320° C.) from the high temperature heat exchanger 22 is fed to the super-heater 30, whereas cooled water (10° C.) from the low temperature heat exchanger 23 is fed to the condenser 32. The steam cycle generates work in a manner known in itself.

(18) In another embodiment, the apparatus comprises two or more drums coupled in series or in parallel. For instance, in configurations comprising two drums in series, the heated medium from the first drum is fed to the low temperature heat exchanger of the second drum. As a result, heat transfer to the high temperature heat exchanger in the second drum is increased considerably, when compared to heat transfer in the first drum. The cooled medium from the first drum can be used as a coolant, e.g., in a condenser.

(19) In another embodiment, and as an alternative or addition to the aforementioned tube (26), the apparatus comprises a plurality of at least substantially cylindrical and co-axial walls, separating the inside of the drum into a plurality of compartments. The fluid in each of the compartments is thoroughly mixed, e.g., by ventilators or static elements, so as to establish a substantially constant entropy within each of the compartments and thus enhance mass transport within each of the compartments. As a result, an entropy gradient, stepwise and negative in outward radial direction, is achieved which enables heat transfer from the axis of rotation of the drum to the circumference of the drum.

(20) The walls mutually separating the compartments may be solid, thus preventing mass transfer from one compartment to the next, or may be open, e.g., gauze- or mesh-like, thus allowing limited mass transfer. The walls may also be provided with protrusions and/or other features that increase surface area and thus heat transfer between compartments.

(21) In yet another embodiment, an additional liquid flows, e.g., inside radially extending tubes, from the center towards the circumference of the drum, thus gaining potential energy and pressure. The high pressure liquid drives a generator, e.g., a (hydro)turbine, and is subsequently evaporated by the relatively hot compressible fluid (e.g., Xenon) at or near the inner wall of the drum. Vapor thus obtained is transported back to the center of the drum, at least partially by employing its own expansion, and condensed by the relatively cold compressible fluid. This embodiment can be used to directly drive a generator.

(22) The invention is not restricted to the above-described embodiments, which can be varied in a number of ways within the scope of the claims. For instance, other media, such as carbon dioxide, hydrogen, and CF.sub.4, can be used in the heat exchangers in the drum.