US20100108295A1

US20100108295A1 - Process And Apparatus For Transferring Heat From A First Medium to a Second Medium

Info

Publication number: US20100108295A1
Application number: US12/526,734
Authority: US
Inventors: Frank Hoos
Original assignee: HELEOS Tech GmbH
Current assignee: HELEOS Tech GmbH
Priority date: 2007-02-14
Filing date: 2008-02-13
Publication date: 2010-05-06
Also published as: BRPI0807226A2; WO2008098968A1; EP2118586A1; AU2008214605A1; RU2009132192A; CA2677590A1; JP2010533832A; MX2009008657A

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 means of 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 having a lumen for holding a compressible fluid and rotatably mounted in a frame, and a first heat exchanger mounted inside the drum relatively far from the axis of rotation of the drum.

Description

RELATED APPLICATIONS

This application is a 35 U.S.C. § 371 national phase of International Application No. PCT/EP2008/051752, entitled “PROCESS AND APPARATUS FOR TRANSFERRING HEAT FROM A FIRST MEDIUM TO A SECOND MEDIUM” filed on Feb. 13, 2008, which claims priority to European Application Serial Number 07109194.6, filed on May 30, 2007, and European Application Serial Number 07102399.8, filed on Feb. 14, 2007.

TECHNICAL BACKGROUND

The invention relates to a process and an apparatus for transferring heat from a first, relatively cold medium to a second, relatively hot medium.

BACKGROUND

In current power plants, work is typically generated by means of a Carnot cycle or “steam cycle,” employing a high temperature source and a low temperature source (heat sink). In practice, a high temperature medium, typically superheated steam, is fed to a turbine, which generates work, and is subsequently condensed, (super)heated and once more fed to the turbine. In other words, the difference between the amount of heat contained in the high temperature medium and the amount of heat sunk to the low temperature source is converted into work, in accordance with the first law of thermodynamics.
At higher temperature differences between the high and low temperature sources, more heat can be converted into work and the efficiency of the process improves. Typically, the environment (earth) serves as the low temperature source (heat sink) and the high temperature medium is generated by burning fossil fuels or by nuclear fission.
DE 32 38 567 relates to a device for generating temperature differences for heating and cooling. Under the influence of an external force, a temperature difference is established in a gas. By using centrifugal forces and with gases of high molecular weight, this effect is increased to such an extent that it is of interest for technical use.
WO 03/095920 relates to a method for transmitting heat energy, wherein the heat energy is transmitted into an inner chamber (3) of a rotating centrifuge via a first heat exchanger (4, 4a, 4b), in which inner chamber (3) a gaseous energy transfer medium is provided, and wherein the heat is discharged from the centrifuge (2) via a second heat exchanger (5; 5a, 5b). The amount of energy used can be reduced substantially by providing the gaseous energy transmission medium inside the rotor (12) in a state of equilibrium and by radially orienting the heat flow in an outward direction. It is essential to the invention underlying WO 03/095920 that convection be prevented (page 2, last sentence).
U.S. Pat. No. 3,902,549 relates to a rotor mounted for high-speed rotation. At its center is located a source of thermal energy whereas at its periphery there is located a heat exchanger. Chambers are provided, accommodating a gaseous material which, depending upon its position in the chambers, can receive heat from the source of thermal energy or yield heat to the heat exchanger.
For the sake of completeness, it is noted that U.S. Pat. No. 4,107,944 relates to a method and apparatus for generating heating and cooling by circulating a working fluid within passageways carried by rotors, compressing said working fluid therewithin and removing heat from said working fluid in a heat removal heat exchanger and adding heat into said working fluid in a heat addition heat exchanger, all carried by said rotors. The working fluid is sealed within, and may be a suitable gas, such as nitrogen. A working fluid heat exchanger is also provided to exchange heat within the rotor between two streams of said working fluid.
U.S. Pat. No. 4,005,587 relates to a method and apparatus for transport of heat from a low temperature heat source into a higher temperature heated sink, using a compressible working fluid compressed by centrifugal force within a rotating rotor with an accompanying temperature increase. Heat is transferred from the heated working fluid into the heat sink at higher temperature, and heat is added into the working fluid after expansion and cooling from a colder heat source. Cooling is provided within the rotor to control the working fluid density, to assist working fluid circulation.
Similar methods and apparatuses are known from U.S. Pat. No. 3,828,573, U.S. Pat. No. 3,933,008, U.S. Pat. No. 4,060,989, and U.S. Pat. No. 3,931,713.
WO 2006/119946 relates to device (70) and method for transferring heat from a first zone (71) to a second zone (72) using mobile (often gaseous or vaporous) atoms or molecules (4) in which in one embodiment, the chaotic motion of the atoms/molecules which usually frustrates the transfer of heat by simple molecular motion is overcome by using preferably elongated nanosized constraints (33) (such as a carbon nanotube) to align the atoms/molecules and then subjecting them to an accelerating force in the direction in which the heat is to be transferred. The accelerating force is preferably centripetal. In an alternative embodiment, molecules (4c) in a nanosized constraint may be arranged to transfer heat by means of an oscillation transverse of the elongation of an elongated constraint (40).
JP 61165590 and JP 58035388 relate to rotary-type heat pipes. U.S. Pat. No. 4,285,202 relates to industrial processes for energy conversion involving at least one step which consists in acting on the presence of a working fluid in such a manner as to produce either compression or expansion

SUMMARY

It is one object of the present disclosure to provide a process for efficiently generating a high temperature medium.
To this end, one aspect of the process includes 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.
Some embodiments further include the step of extracting heat from, i.e., cooling, the first medium by the fluid in a section at or relatively close to the axis of rotation.
The hot and cold media thus obtained in turn can be employed e.g., to heat or cool buildings or to generate electricity by, for example, a Carnot cycle or “steam cycle.”
The efficiency of the process according to the present disclosure can be further increased if segments, defined in radial direction, of the fluid are thoroughly mixed to obtain an at least substantially constant entropy in these segments and thus improved heat conduction within the fluid.
Also, heat conduction and hence efficiency increases with the pressure and density of the fluid. Thus, pressure is preferably in excess of 2 bar (at the axis of rotation), and more preferably in excess of 10 bar (at the axis of rotation). The ratio of pressure at the circumference and pressure at the axis of rotation is preferably in excess of 5, and more preferably in excess of 8.
Instead of transferring heat through conductivity, heat can instead or in addition be transferred through heat capacity and mass flow. To that end, the first medium and/or the second medium flows along at least one radius of the contained amount, generating an at least partially radial circulation in the fluid.
The present disclosure further relates to an apparatus for transferring heat from a first relatively cold medium to a second relatively hot medium, including 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, for instance in the inner wall of the drum.
In one aspect of the present disclosure, the apparatus includes a second heat exchanger positioned at or relatively close to the axis of rotation.
In another aspect, the apparatus includes one or more at least substantially cylindrical and co-axial walls, separating, in radial direction, the inside of the drum into a plurality of compartments.
In a further aspect, at least one of the heat exchangers is coupled to a cycle for generating work. The further cycle can include an evaporator or super-heater, which is thermally coupled to the high temperature heat exchanger, a condenser, thermally coupled to the low temperature heat exchanger, and a heat engine. The environment will typically serve as a heat sink, but may also serve a high temperature source, if the operating temperature of the cycle if sufficiently low.
In yet a further aspect, the compressible fluid is a gas and preferably contains or consists essentially of a mono-atomic element having an atomic number (Z)≧18, such as Argon, and preferably≧36, such as Krypton and Xenon.
The invention is based on the insight that, although heat normally flows from a from a higher to a lower entropy and hence from higher to a lower temperature, in a column of an isentropic, compressible fluid positioned in a field of gravity heat also flows from a lower to a higher entropy. In the atmosphere of the earth, this effect reduces the vertical temperature gradient from a calculated 10° C./km to an actual 6.5° C./km. Hydropower is based on the same principle.
A reduced heat resistance further enhances heat flow from a lower to a higher temperature.
In accordance with at least some aspects of the present disclosure, artificial gravity is employed to reduce the length of the column of the compressible fluid, in comparison with a column subjected merely to the gravity of the earth, and the atmosphere is replaced by a gas allowing a much higher temperature gradient in the fluid. Mixing is employed to improve heat conduction within the fluid.
Within the framework of the present invention the term “gradient” is defined as a continuous or stepwise increase or decrease in the magnitude of a property observed in passing from one point to another, e.g., along a radius of a cylinder.

DESCRIPTION OF DRAWINGS

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

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

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

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

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

FIGS. 6A and 6B are cross-sectional side views of a third embodiment of the apparatus.

FIG. 7 is a cross-section of an exchanger unit for use in the embodiment of FIGS. 6A and 6B.

FIG. 8 is a cross-section of an exchanger tube for use in the unit of FIG. 7.

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

DETAILED DESCRIPTION

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 apparatus, 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.
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.
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 13. 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.
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 means of 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.
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 means of 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).
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 means of 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.
The drum 6 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.
The embodiment shown in FIG. 4 further comprises an tube 26, coaxial with the longitudinal axis of the drum 7 and containing an axial ventilator 27 to forcedly circulate the contents of the drum. In this example, the drum is filled with Xenon at a pressure of 5 bar (at ambient temperature), whereas the heat exchangers 22, 23 are filled with water.
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.
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
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.
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.
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.
Instead of transferring heat through conductivity, as in the embodiments above, heat can instead or in addition be transferred through heat capacity and mass flow. An embodiment of an artificial gravity apparatus 1 based on heat transfer through heat capacity and mass flow is shown in FIGS. 6A to 8. In this embodiment, the first and second heat exchangers comprises a plurality of radially extending exchanger units 22A, 23A evenly distributed, both in axial and in tangential direction, over the surfaces of the inner walls of the drum 6.
As shown in more detail in FIG. 7, each unit comprises a double-walled exchanger tube 40, shown in cross-section in FIG. 8. Each exchanger tube 40 comprises an inlet 41, a central feed tube 42, an outer return tube 43 concentric with the feed tube, and an outlet 44. The outer tube 43 in turn is provided on its outer surface with means for enhancing heat exchange, e.g., features, such as fins 45, increasing the outer surface of the outer tube 43.
Each unit further comprises a siphon 46 positioned concentrically about the exchanger tube 40 and spanning at least 70%, e.g., about 80% of the radial distance between the walls 6A, 6B of the drum 6. To equalize the entropy inside and outside the siphon 46 at least the inner surface of the siphon 46 is provided with features for enhancing heat exchange, e.g., fins 47, increasing the inner surface of the siphon 46.
During operation, a cooling medium, e.g., water, is fed to the exchanger tubes 40 that are positioned relatively far from the axis of rotation of the drum 6, thus locally cooling the fluid in the drum 6 and locally increasing density and decreasing entropy. The dense fluid around the exchangers tubes 22A will be forced outwards by artificial gravity, i.e., co-currently with the water and towards the outer wall 6A of the drum 6, and caused to spread over its inner surface.
A heating medium, e.g., water, is fed to the exchanger tubes 23A that are positioned relatively close to the axis of rotation of the drum 6, thus heating the fluid in the drum 6 and locally decreasing density and increasing entropy. The fluid around the exchangers tubes 40 will be displaced inwards (buoyancy) as a result of artificial gravity, i.e., co-currently with the water and towards the inner wall 6B of the drum 6, and caused to spread over its surface.
These two phenomena together generate a circulation between the heat exchangers, which enhances heat transfer outwards from the heat exchanger 23 relatively close to the axis of rotation of the drum 6 and towards the heat exchanger 22 relatively far from the axis of rotation of the drum 6.
In this embodiment, the length of the exchanger tubes 22A, 23A, is selected such as to prevent these tubes from reaching the zone of the fluid inside the drum where the temperature is about equal to the temperature of an associated heat buffer, such as the surroundings of the apparatus.
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 means of the relatively cold compressible fluid. This embodiment can be used to directly drive a generator.
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 CF₄, can be used in the heat exchangers in the drum. Also, to reduce rotational resistance, the drum can be operated in a low pressure or vacuum environment.

Claims

1-7. (canceled)

8. 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, and

heating the second medium by the fluid in a section of the fluid relatively far from the axis of rotation.

9. The method according to claim 8, further comprising the step of extracting heat from the first medium by the fluid in a section at or relatively close to the axis of rotation.

10. The method according to claim 8, wherein the first medium and/or the second medium flows along at least one radius of the contained amount, generating an at least partially radial circulation in the fluid.

11. 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 having a lumen for holding a compressible fluid and rotatably mounted in a frame, and

a first heat exchanger mounted inside the drum relatively far from the axis of rotation of the drum.

12. The apparatus according to claim 11, comprising a second heat exchanger positioned at or relatively close to the axis of rotation.

13. The apparatus according to claim 11, wherein the first and/or the second heat exchanger comprise a plurality of tubes radially extending into the lumen.

14. The apparatus according to claim 13, wherein a siphon is positioned concentrically about at least some of the tubes.