Heat transfer apparatus and method employing active regenerative cycle

Information

  • Patent Grant
  • 6332323
  • Patent Number
    6,332,323
  • Date Filed
    Friday, February 25, 2000
    24 years ago
  • Date Issued
    Tuesday, December 25, 2001
    23 years ago
Abstract
This application relates to a heat transfer apparatus and method employing an active regenerative cycle. The invention employs a working or “active” fluid and a heat transfer fluid which are physically separated. The working fluid is contained in an array of refrigeration elements that are distributed over the temperature gradient of a regenerative bed. The work for the refrigeration cycle is provided by alternative compression and expansion of the working fluid in each of the refrigeration elements at a temperature corresponding to the element's location in the temperature gradient. The compression and expansion strokes may be coupled together for optimum work recovery. The heat transfer fluid is circulated relative to the working fluid between a thermal load and a heat sink to enact a refrigeration cycle having improved energy efficiency.
Description




TECHNICAL FIELD




This application relates to a heat transfer apparatus and method employing an active regenerative cycle. The invention employs a working fluid and a heat transfer fluid which are physically separated. The working fluid is contained in an array of discrete elements that are distributed over the temperature profile of a regenerative bed located between a thermal load and a heat sink. The work for the cycle and temperature differences for heat transfer are provided by alternating compression and expansion of the working fluid. The heat transfer fluid is circulated relative to the working fluid between the thermal load and the heat sink to enact a regenerative cycle having improved energy efficiency.




BACKGROUND




A conventional “vapor-compression” refrigeration cycle employs a single refrigerant that is circulated through a conduit between a heat sink and a thermal load. This cycle relies on the thermodynamic principles of adiabatic compression (temperature increase), isenthalpic expansion (temperature decrease) and latent heat of vaporization or condensation of a fluid.




Refrigerants, such as chlorofluorocarbons, hydrochlorofluorocarbons and hydrofluorocarbons, are typically liquids at ambient temperatures. At one stage in the refrigeration cycle, the refrigerant passes through a compressor that increases its pressure and temperature, causing it to release heat as it condenses from a vapor to a liquid form in a condensing heat exchanger. At another stage in the cycle, the liquid refrigerant passes through an expansion valve to reduce its pressure and temperature, creating a two phase fluid. This reduction in temperature causes the refrigerant to absorb heat and evaporate within the evaporative heat exchanger. In this conventional cycle, the “working fluid”, which is compressed and expanded as it circulates, and the “heat transfer fluid”, which accepts heat from the thermal load and rejects heat to the heat sink, are the same thing, namely the volatile refrigerant. The compressor and expansion valve are physically separated, the compressor being at the “hot end” of the cycle and the expansion valve being at the “cold end” of the cycle. The condensing heat exchanger rejects heat to the heat sink while the evaporative heat exchanger absorbs heat from the thermal load.




Regenerative thermodynamic cycles that use regenerators for periodic heat exchange are known in the prior art. In most cases the regenerator is a material which has a large thermal mass and heat transfer surface. In typical regenerative cycles the regenerator is a passive element that is not capable of doing work and whose purpose is to transfer heat back and forth to a working gas periodically during the cycle to enable larger temperature spans to be achieved. The working gas continues to be compressed at the hot end of the cycle and expanded at the cold end of the cycle. Moreover, the working gas is the same gas which is used to transfer heat from the cooled space to the environment via heat exchangers. Stirling, Gifford-McMahon and Orifice Pulse Tube devices are all examples of prior art refrigeration systems employing passive regeneration.




Stirling cycle devices operate on a regenerative thermodynamic cycle, with cyclic isothermal compression and isothermal expansion of the working fluid at different temperature levels, separated by constant volume flow through regenerators with a temperature span from the two different temperatures of compression and expansion. Stirling cycle devices have been used as heat engines, heat pumps, and refrigerators.




In a Stirling cycle machine operating as a prime mover, the working fluid isothermal compression takes place in the hotter chamber, while most of the isothermal expansion takes place in the colder chamber. Some of the heat introduced at the hot chamber is converted to work in the prime mover and the residual heat is rejected at the cold chamber. As will be appreciated by those skilled in the art, when the Stirling cycle is used in a refrigerating machine rather than a prime mover, the working fluid isothermal expansion that absorbs heat occurs in the cold chamber while the isothermal compression of the working fluid, during which heat is rejected, takes place in the hot chamber. In either type of machine the working fluid is shifted between the two chambers through a passive regenerator which is not itself capable of doing work.




In prior art Stirling cycle machines, the “working fluid” which is alternatively compressed and expanded may either be a gas or liquid. For example, U.S. Pat. No. 5,172,554 dated Dec. 22, 1992, Swift et al., discloses a Stirling thermodynamic cycle refrigerator that utilizes a single phase solution of liquid


3


He as the working fluid. The liquid


3


He may be present in superfluid


4


He. As in conventional Stirling cycles, a passive regenerator is employed as a thermal reservoir that maintains a temperature difference between the compressor and expander and functions as a thermal reservoir that cyclically exchanges heat with the working fluid. Work is applied to the working fluid during the Stirling cycle in the compressor and expander rather than within the passive regenerator itself.




U.S. Pat. No. 4,353,218 dated Oct. 12, 1982, Wheatley et al., relates to a heat pump/refrigerator using working fluid that is continuously in a liquid state. The Wheatley apparatus includes a pair of heat exchangers respectively coupled to a thermal load and a heat sink, a displacer forming a pair of reservoirs coupled to the different heat exchangers, a regenerator connecting the heat exchangers, and means for compressing a working fluid that can pass between the reservoirs by way of the regenerator and a heat exchanger. The working fluid may consist of, for example, compressed polypropylene. As in other similar prior art systems, the regenerator is utilized to transfer heat from the working fluid leaving one heat exchanger into fluid leaving the other heat exchanger and does not input work into or remove work from the system.




“Active regenerators” utilize heat transfer materials that not only have large thermal masses and heat transfer surfaces but are also capable of doing work during a thermodynamic cycle. Heretofore active refrigerants have been solids, such as magnetic materials or elastomers. For example, U.S. Pat. No. 4,704,871, Barclay et al., issued Nov. 10, 1987, relates to magnetic refrigerators employing paramagnetic or ferromagnetic materials. When such materials are adiabatically passed into and out of a magnetic field (such as produced by a superconducting magnet) their temperature alternatively increases and decreases. This is referred to as the magnetocaloric effect. By way of example, if Gadolinium at room temperature is adiabatically subjected to a magnetic field of about 8 Tesla it will increase its temperature by about 12-14 K. A refrigeration cycle may be enacted by passing a heat transfer fluid between hot and cold heat exchangers in a periodic flow as the magnetic material is alternatively adiabatically magnetized and demagnetized.




One significant problem associated with active regenerative systems employing the magnetocaloric effect is the cost of developing adequate adiabatic temperature changes especially for near room temperature use. Magnetic systems require powerful superconducting magnets to achieve magnetic fields large enough to cause modest temperature ratios. Such superconducting magnets are very expensive and not practical for many applications and the energy required to keep the superconducting magnets cold makes the entire cycle inefficient with the exception of very large systems.




Elastomeric materials may also be used as an active heat transfer element in a regenerative system. U.S. Pat. No. 5,339,653 dated Aug. 23, 1994, DeGregoria, describes refrigeration cycles based on the thermoelastic effect in which certain elastomers, such as rubber, warm upon stretching and cool upon contracting. In particular, a regenerative bed may be formed comprising a porous matrix of elastomeric sheets arranged in layers with spacers between the sheets defining fluid flow channels. Work may be inputted into or removed from the system by periodically stretching and contracting the elastomeric sheets to effect temperature changes. A circulator passes a heat transfer fluid through the porous matrix in one direction when the bed is at one temperature or stretch and in the reverse direction when the bed is at a different temperature or stretch.




The significant problems associated with active regenerative systems employing the thermoelastic effect include the large strains (˜4-10) required to achieve modest temperature change (˜20 K), hysteretic effects and crystallization of the elastomer after prolonged use or upon cooling significantly below room temperature.




While the use of solid heat transfer regenerative materials capable of doing work, such as magnetic or elastomeric materials, is known in the prior art, the use of an active or “working” fluid capable of doing work in a regenerative refrigeration cycle has not been previously described as a means of improving thermal efficiency. The need has therefore arisen for an active regenerative refrigerator that comprises a working fluid separate from the heat transfer fluid and which is distributed over the temperature profile of a regenerative bed. The need has also arisen for an active regenerative refrigerator of modular design that may be easily tailored to meet the heat transfer requirements of different applications, thereby achieving optimum versatility.




Since the present invention achieves improved thermodynamic efficiency, it has many potential cryogenic and near room temperature applications. For example, vehicles that operate on liquefied natural gas are particularly attractive as an alternative to gasoline-based vehicles in that they utilize a domestically available fuel, generate less pollution and have significantly lower maintenance costs. The refueling stations needed to service vehicles operating on liquefied natural gas will require relatively inexpensive refrigerators to liquefy the gas delivered through pipelines that operate at ambient temperature.




Numerous high temperature superconductor devices provide the promise of improved electronic performance provided cost-effective refrigeration systems are available to cool the electronics down to near or below liquid nitrogen temperatures. The present cost of cryogenic cooling systems, however, makes circuitry that utilizes superconductors impractical for consumer applications.




The generation of liquid oxygen for use in sewer treatment plants would likewise benefit from more cost-effective refrigeration systems. Oxygen is bubbled through aerobic digestion ponds to increase the speed at which waste products are oxidized. The oxygen is typically generated on site by cryogenic liquefaction of air. It would be advantageous to be able to increase the efficiency of such cryogenic systems, thereby lowering the cost of generating the liquid oxygen.




Prior art cryogenic refrigeration systems with large cooling capacities typically depend upon large compressors that generate a great deal of vibration and have limited lifetimes. The need to isolate the vibration and reduce the noise further increases the cost of the systems. It would be clearly advantageous to avoid cryogenic systems that have moving parts and seals requiring periodic replacement.




With the introduction of the Montreal Protocol the initial objectives of reducing emissions of ozone depleting gases, most of which came from the near room temperature refrigeration industry, have been stated. Its implementation has caused the substitution of the CFC refrigerants with similar compounds with less ozone damaging potential. Unfortunately some of the new ozone friendly refrigerants are inferior to previous refrigerants and have reduced the efficiency of some refrigeration equipment.




The newest environmental challenge is the reduction of greenhouse gas emissions. In the case of the near room temperature refrigeration industry, increasing the efficiency of refrigerating devices will help reduce such emissions.




There are many applications in the near room temperature market including air-conditioners, refrigerators, freezers and heat pumps. Vapor compression technology is used in the vast majority of products for these markets and has been under continuing improvement for approximately 100 years. The efficiency of the current products can be increased slightly but only with an increase in capital cost. A refrigerating system with improved efficiency and similar or reduced capital cost would be highly advantageous.




SUMMARY OF THE INVENTION




In accordance with the invention, a heat transfer apparatus employing an active regenerative cycle for transferring heat from a thermal load to a heat sink is provided. The apparatus comprises a contained working fluid; a heat transfer fluid physically separated from the working fluid and in thermal communication with the thermal load and the heat sink; work input means for periodically compressing and expanding the working fluid to alternatively increase and decrease the temperature thereof; and circulation means for circulating the heat transfer fluid relative to the working to either accept heat from or transfer heat to the working fluid.




Preferably the working fluid is contained within at least one first vessel. The work input means is moveable relative to the first vessel to compress a first sub-volume of the working fluid in a first portion of the first vessel and simultaneously cause expansion of a second sub-volume of the working fluid in a second portion of the first vessel, thus enabling work recovery. In one embodiment of the invention a plurality of separate first vessels are arranged in an ordered array, each of the first vessels having a designated location between the thermal load and the heat sink. Each of the first vessels is thermally isolated from the remainder of the first vessels such that the operating temperature of each of the first vessels depends upon its designated location (i.e. its location in the temperature gradient between the thermal load in the heat sink). In this embodiment the heat transfer fluid flows over the surface of each of the first vessels in the array. In an alternative embodiment, the heat transfer fluid may flow through a second vessel contained within the first vessel(s). In this alternative embodiment the working fluid is compressed and expanded externally to the heat transfer fluid.




A method of enacting an active regenerative refrigeration cycle is also disclosed. The cycle comprises:




(A) providing a contained working fluid;




(B) providing a heat transfer fluid physically separated from the working fluid and movable between a thermal load and a heat sink;




(C) compressing the working fluid to increase the temperature thereof;




(D) moving the heat transfer fluid relative to the working fluid in a flow direction from the thermal load toward the heat sink;




(E) expanding the working fluid to decrease the temperature thereof: and




(F) moving the heat transfer fluid relative to the working fluid in a flow direction from the heat sink toward the thermal load.




A regenerative heat transfer device for transferring heat between a thermal load and a heat sink is also disclosed. The heat transfer device generally comprises (a) an array of discrete refrigeration elements spaced apart at intermediate locations between the thermal load and the heat sink, wherein each of the refrigeration elements contains a working fluid and has a mean operating temperature corresponding to its location between the thermal load and the heat sink; (b) an actuator for periodically compressing and expanding the working fluid to thereby increase or decrease the temperature of the refrigeration elements; and (c) a circulator for circulating a heat transfer fluid in a flow path between the thermal load and the heat sink, wherein the heat transfer fluid passes relative to the array of refrigeration elements to either accept heat from or transfer heat to the refrigeration elements.




Preferably the actuator includes means for varying the volume of the refrigeration elements and the working fluid in each of the refrigeration elements is compressed and expanded in unison. For example, the actuator may comprise a reciprocating piston or a rotary drive for rotating the array of refrigeration elements.




Each individual refrigeration element may comprise (a) a container for holding a working fluid; (b) at least one conduit extending within or surrounding the container for holding a heat transfer fluid separate from the working fluid; and (c) an actuator for periodically compressing and expanding the working fluid to vary the temperature of the working fluid.




A regenerative refrigerator having improved thermal efficiency comprises a plurality of refrigeration elements as described above operatively coupled together such that the heat transfer fluid in adjacent pairs of elements is in fluid communication. The refrigeration elements are otherwise thermally isolated so that a temperature gradient between the thermal load and the heat sink is maintained.











BRIEF DESCRIPTION OF DRAWINGS




In drawings which describe embodiments of the invention but which should not be construed as restricting the spirit or scope of the invention in any way,





FIG. 1



a


is a block diagram illustrating the basic concept of the invention.





FIG. 1



b


is a block diagram of an alternative embodiment of the invention allowing heat transfer between a thermal load and a heat sink without the use of heat exchangers.





FIG. 1



c


is an isometric view of a single refrigeration element containing working fluid located within a vessel containing heat transfer fluid.





FIG. 1



d


is an isometric view of an alternative refrigeration element wherein the working fluid is contained externally to the heat transfer fluid.





FIG. 2



a


is a side view of a first embodiment of the invention comprising an array of variable volume regenerator tubes each having flexible walls.





FIG. 2



b


is a side view of a further first embodiment of the invention comprising an array of variable volume regenerator tubes each having extensible telescopic segments.





FIG. 2



c


is a side view of a variation of the embodiment of

FIG. 2



a


illustrating an open system wherein the heat transfer fluid is air and the heat sink is the environment.





FIG. 3

is a side view of a second embodiment of the invention comprising an array of fixed volume regenerator tubes each containing a reciprocating piston.





FIG. 4

is a fragmented cross-sectional view of a third embodiment of the invention comprising an array of fixed volume regenerator tubes each containing an expandable bladder connected to a common gas compressor and showing the bladders in the expanded configuration.





FIG. 5

is a fragmented cross-sectional view of the embodiment of

FIG. 4

showing the bladders in the contracted configuration.





FIG. 6

is a side view of a fourth embodiment of the invention in a compressed configuration comprising an array of fixed volume regenerator tubes each coupled to a common fluid compressor with individual passive regenerators.





FIG. 7

is a side view of the embodiment of

FIG. 6

in an expanded configuration.





FIG. 8

is a fifth embodiment of the invention similar to the embodiment of

FIGS. 6 and 7

except that each regenerator tube is coupled to the gas compressor by means of a common passive regenerator.





FIG. 9



a


is a cross-sectional view of a sixth embodiment of the invention comprising a vessel having a plurality of compartments for containing working fluid external to heat transfer delivery tubes extending therethrough.





FIG. 9



b


is a partial isometric view of the embodiment of

FIG. 9



a.







FIG. 10



a


is an isometric, partially cut-away view of a seventh embodiment of the invention comprising a modular refrigeration element having a plurality of heat transfer tubes extending therethrough and showing the refrigeration element in a compressed configuration.





FIG. 10



b


is an isometric, partially cut-away view of the modular refrigeration element of

FIG. 10



a


in an expanded configuration.





FIG. 11



a


is an isometric, partially cut-away view of an eighth embodiment of the invention comprising a modular refrigeration element in a compressed configuration similar to the embodiment of

FIG. 10



a


but having a spiral heat transfer tube wound within the interior thereof.





FIG. 11



b


is an isometric, partially cut-away view of the modular refrigeration element of

FIG. 11



a


in an expanded configuration.





FIG. 12



a


is an isometric, partially cut-away view of a regenerative bed comprising a plurality of the modular refrigeration elements of

FIG. 11



a


arranged in a stack and shown in the compressed configuration.





FIG. 12



b


is an isometric, partially cut-away view of the regenerative bed of

FIG. 12



a


showing the modular refrigeration elements in an expanded configuration.





FIG. 13

is a side view of dual regenerative beds of

FIGS. 12



a


/


12




b


coupled together by an axially displaceable piston to enable work recovery.





FIG. 14

is a side view of dual regenerative beds of

FIGS. 12



a


/


12




b


coupled together by a pivoting rocker arm to enable work recovery.





FIG. 15

is an isometric, partially cut-away view of a ninth embodiment of the invention illustrating a regenerative bed similar to the embodiment of

FIG. 12



b


but having a common sidewall.





FIG. 16



a


is a schematic view of a tenth embodiment of the invention wherein the regenerator tubes are rotatable to alternatively contract and expand the working fluid.





FIG. 16



b


is an exploded, isometric view of an exemplary tenth embodiment of the invention wherein the regenerator tubes are disposed on a rotatable carousel mounted on a heat transfer fluid delivery column.





FIG. 16



c


is an isometric view of the embodiment of

FIG. 16



b


in its assembled configuration.





FIG. 16



d


is an enlarged, cross-sectional view of the embodiment of

FIGS. 16



b


and


16




c.







FIG. 17

is a graph showing the temperature profile of the regenerative bed at successive stages in the refrigeration cycle.





FIG. 18



a


is a temperature-entropy graph showing the ideal Brayton cycle of a single refrigeration element of the regenerator to illustrate the work input and heat flows embodied in the refrigeration cycle.





FIG. 18



b


is a temperature-entropy graph showing overlapping Brayton cycles of multiple refrigeration elements.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




This application relates to a heat transfer apparatus and method employing an active regenerative cycle. The invention may be used, for example, to configure a regenerative refrigerator having improved energy efficiency. With reference to

FIG. 1



a


, the invention exhibits some features common to any regenerative refrigerator, namely a means for reciprocally exchanging a heat transfer fluid


10


across a regenerative bed


12


between a cold heat exchanger


14


, coupled to a thermal load


16


, and a hot heat exchanger


18


, coupled to a heat sink


20


. Regenerative bed


12


maintains a temperature gradient between the cold and hot heat exchangers


14


,


18


to enable heat flow from load


16


to sink


20


. In some embodiments of the invention, heat exchangers


14


,


18


may be as simple as piping for passing heat transfer fluid


10


between regenerative bed


12


and load


16


or sink


20


.




A unique feature of applicants' invention is the design of regenerative bed


12


. Bed


12


comprises a plurality of refrigeration elements


22


each containing a working fluid


24


that is alternatively compressed and expanded. As used in this patent application the terms “regenerator” and “regenerative bed” refer to a periodic heat exchanger which transfers heat to and accepts heat from a heat transfer fluid during each cycle of operation.




At least one refrigeration element


22


is required in order to create a cooling effect. The extent of the cooling effect is dependent on several factors including the amount and type of working fluid


24


contained in refrigeration element


22


, the compression/expansion ratio of working fluid


24


, the surface area of element


22


available for heat transfer and the temperature of heat exchangers


14


,


18


. For most applications a plurality of refrigeration elements


22


are required to produce a cooling effect of practical utility. As described further below, regenerative bed


12


preferably comprises an array of elements


22


spaced at intermediate locations between heat exchangers


14


,


18


to achieve a larger temperature gradient and hence lower cooling temperatures.




Refrigeration elements


22


located at different intermediate locations in regenerative bed


12


have different operating temperatures. As explained further below, the temperature differences between each adjacent refrigerator element


22


in the array should be as small as possible and hence a large number of elements


22


are preferably employed to achieve optimal thermodynamic efficiency. At each intermediate location in bed


12


a bank of refrigeration elements


22


may be provided for increasing the overall heat transfer capacity of the system.




Applicants' invention is referred to as an “active” regeneration system since each refrigeration element


22


is capable of doing work. The work necessary to enact a refrigeration cycle is inputted into the system by alternatively compressing and expanding working fluid


24


. This causes the temperature of each refrigeration element


22


to alternatively increase and decrease in an amount that depends upon its position in regenerative bed


12


. Notwithstanding the fluctuations in temperature of elements


22


, the temperature gradient across regenerative bed


12


is maintained. Flow of heat transfer fluid


10


across regenerative bed


12


is synchronized with the strokes of compression and expansion of the working fluid


24


within elements


22


.




As shown schematically in

FIG. 1



b


, since heat transfer fluid


10


and working fluid


24


are physically separated, ambient air may potentially be used as heat transfer fluid


10


in an open cycle (which eliminates the need for heat exchangers


14


,


18


as discussed further below).




As described further below, heat transfer fluid


10


and working fluid


24


are physically separated and do not mix. Heat transfer fluid


10


thermally couples refrigeration elements


22


together by either accepting or depositing heat as it passes relative to elements


22


across regenerative bed


12


. In one embodiment, heat transfer fluid


10


may flow externally to working fluid


24


contained within one or more vessels (

FIG. 1



c


). Alternatively, working fluid


24


may be contained in a vessel externally of the heat transfer fluid (

FIG. 1



d


). For example, as described further below, heat transfer fluid may be circulated through a plurality of parallel tubes surrounded by working fluid contained within a larger vessel.




As used in this patent application the term “working fluid” refers to a fluid that may be compressed and expanded to effect a temperature change. As will be apparent to a person skilled in the art, a large number of different gases may be employed as working fluid


24


. Examples of suitable working fluids


24


include common gases (e.g. helium, air, nitrogen, argon etc.), hydrocarbon gases (e.g. methane, ethane, propane etc.) and conventional refrigerants (e.g. CFC, HCFC, HFC, ammonia, etc.). The choice of working fluid


24


may depend upon the location of a particular refrigeration element


22


in the temperature gradient spanning regenerative bed


12


. That is, the properties of the working fluid


24


at the temperature it is expected to operate in bed


12


is a prime criteria used to select a suitable fluid. In some cases, working fluid


24


could comprise a mixture of different gases in a pre-determined proportion. Tailoring the selection of working fluid


24


in this manner has the potential to improve the thermal efficiency and versatility of the refrigeration cycle. Although working fluid


24


will typically be in a gaseous state, it may also be present in a liquid state or as a gas/liquid mixture (e.g. a gas near its critical point).




Each refrigeration element


22


preferably comprises a dual compressor and expander. That is, compression of working fluid


24


in one chamber of element


22


simultaneously causes expansion of working fluid in a separate chamber of element


22


. Accordingly, a portion of the energy inputted during the compression stroke is simultaneously recovered during a corresponding expansion stroke within the same element


22


(and hence at the same location in the temperature gradient). In other words, there is recovery of some of the compression work during the refrigeration cycle by directly coupling the compression step to an expansion step occurring at nearly the same temperature. This potential for maximum work recovery is an important feature of several embodiments of applicants' invention. By contrast, in conventional vapor-compression refrigerators, gas expansion occurs isenthalpically with no work recovery thereby reducing the thermal efficiency of the cycle.




As indicated above, flow of heat transfer fluid


10


across regenerative bed


12


is synchronized with the cycles of compression and expansion of the working fluid


24


within multiple refrigeration elements


22


. During the expansion step (or very shortly thereafter) a pulse of heat transfer fluid


10


is circulated across bed


12


in a direction toward cold heat exchanger


14


. During this hot blow heat transfer fluid


10


deposits heat to elements


22


. The portion of heat transfer fluid


10


closest to cold heat exchanger


14


is circulated into exchanger


14


thereby cooling thermal load


16


. Conversely, during the compression step (or shortly thereafter) a pulse of heat transfer fluid


10


is circulated across bed


12


in the opposite direction toward hot heat exchanger


18


. During this cold blow heat transfer fluid accepts heat from refrigeration elements


22


. The portion of heat transfer fluid closest to hot heat exchanger


18


is circulated into exchanger


18


thereby causing rejection of heat into heat sink


20


.




Heat transfer fluid


10


may therefore be viewed as oscillating in a direction either toward cold heat exchanger


14


or toward hot heat exchanger


18


during each fluid pulse. The displacement of fluid


10


must be greater than the distance between adjacent elements


22


in the array in order to enable thermal communication therebetween. The optimum displacement distance of heat transfer fluid


10


depends upon a number of factors including the number and spacing of refrigeration elements


22


. In one embodiment of the invention the amplitude of the oscillation may be a fraction of the overall size of regenerative bed


12


(i.e. a fraction of the distance between the uppermost and lowermost refrigeration elements


22


in the array).




Heat transfer fluid


10


may be propelled across regenerative bed


12


by means of a conventional fluid pump (not shown). Valves operating at ambient temperature may also be provided for reversing the direction of fluid flow relative to bed


12


. As is the case for all regenerative systems, the thermal conductance from thermal load


16


to heat sink


20


through regenerative bed


12


should be low for efficient operation of the invention. Further, the pressure drop of heat transfer fluid


10


across regenerative bed


12


should also be low for optimum efficiency.





FIGS. 2



a


and


2




b


illustrate a first embodiment of the invention. In this embodiment refrigeration elements


22


comprise a plurality of elongate regenerator tubes


26


disposed in a parallel array between the hot and cold ends of regenerative bed


12


. Tubes


26


each include an outer wall


27


forming a hermetic shell for containing working fluid


24


. Since the ratio of thermal mass of tubes


26


to working fluid


24


should be small, tube walls


27


are preferably constructed from very thin metal (e.g. <0.1 mm)




In the embodiment of

FIGS. 2



a


and


2




b


each regenerator tube


26


has a variable volume. For example, tube walls


27


may be flexible to permit alternating contraction and extension thereof as shown in

FIG. 2



a


. Preferably each tube


26


is subdivided into a first chamber


29


and a second chamber


31


which are physically separated, such as by a moveable central wall


33


. Wall


33


is reciprocated back and forth by a work input driver to alternatively increase and decrease the volume of chambers


29


,


31


(and thereby compress and expand working fluid


24


contained therein). For example, as working fluid


24


is compressed in each first chamber


29


, working fluid


24


in the corresponding second chamber


31


is simultaneously expanded, and vice versa. As explained above, this dual compression/expansion enables effective work recovery.




Heat transfer fluid


10


is periodically circulated over the surface of tubes


26


between the hot and cold heat exchangers


14


,


18


in synchrony with the compression and expansion strokes. In the embodiment of

FIG. 2



a


, heat transfer fluid


10


flows in a direction perpendicular to the longitudinal axes of tubes


26


in two parallel ducts disposed on either side of central wall


33


. In particular, heat transfer fluid


10


is circulated in the direction of the upward arrow in a first duct from the cold heat exchanger


14


to the hot heat exchanger


18


over the relatively hot surfaces of tube chambers


29


containing compressed working fluid


24


. Simultaneously, heat transfer fluid


10


is also circulated in the direction of the downward arrow in a second duct from the hot exchanger


18


to the cold heat exchanger


14


over the relatively cool surfaces of tube chambers


31


containing expanded working fluid


24


. The work is inputted into the refrigeration cycle by the reciprocal motion of the central wall


33


. The direction of flow of heat transfer fluid


10


in the first and second ducts is periodically reversed as wall


33


reciprocates back and forth.




As will be apparent to a person skilled in the art, the flow path of heat transfer fluid


10


between heat exchangers


14


,


18


through the first and second ducts need not be linear. Heat transfer fluid


10


may be piped through radially extending channels, spiral coils or any other suitable geometric arrangement. However, in order to optimally transfer heat to sink


20


, the flow path must not be interrupted.




Since each regenerator tube


26


is a dual compressor and expander in the embodiment of

FIG. 2



a


, the array of parallel tubes


26


effectively defines two parallel regenerative beds


12


on opposite sides of central wall


33


. Both regenerative beds


12


extend between the same heat exchangers


14


,


18


, but contain heat transfer fluid


10


flowing in opposite directions. Other alternative tube arrangements could envisioned defining four or more discrete regenerative beds


12


all functioning simultaneously.





FIG. 2



b


illustrates another example of the first embodiment of the invention having regenerator tubes


26


of variable volume. In this embodiment, each regenerator tube


26


consists of a plurality of telescopic sections


28


which may be axially extended or collapsed to vary the volume of chambers


29


,


31


. Extension and contraction of tube sections


28


is activated by reciprocation of a central wall


30


comprising flexible bellows. Wall


33


is connected to the innermost tube sections


28


and prevents fluid communication between tube chambers


29


,


31


. Reciprocal movement of wall


33


is driven by an actuator


32


. As in the embodiment of

FIG. 2



a


, circulation of heat transfer fluid


10


across tubes


26


is timed to the contraction and expansion strokes.




As will be apparent to a person skilled in the art, similar cycles of expansion and compression could be effected in other ways using flexible bellows coupled to a reciprocating drive. For example, end portions of tubes


26


could be coupled to the moveable bellows rather than a central wall.




One of the advantages of applicants' invention is that a benign gas may be used as the heat transfer fluid


10


rather than a volatile refrigerant. In one embodiment of the invention illustrated in

FIG. 2



c


the heat transfer fluid


10


may be air which is alternatively passed back and forth over the surface of regenerative beds


12


. This embodiment is suitable for applications where the medium to be cooled is air, particularly near room temperature cooling as in refrigerators, freezers, air conditioners and the like. In this embodiment cold and hot heat exchangers


14


,


18


are not required (thereby making this embodiment much simpler and less expensive to manufacture). The removal of heat exchangers


14


,


18


also improves the overall thermal efficiency of the system.




As shown in

FIG. 2



c


, air from a refrigerated space (i.e. thermal load


16


) is circulated over regenerative bed


12


during the compression stroke to accept heat from tubes


26


. Air leaving the hot end of bed


12


is deposited into the surrounding environment (i.e. heat sink


20


). Conversely, during the expansion stroke, fresh room temperature air is drawn into regenerative bed


12


where it deposits heat to tubes


26


. The cooled air leaving the cold end of bed


12


is blown into the refrigerated space to provide cooling. Optionally, the mechanism for compressing the working fluid


24


may also be incorporated to move heat transfer fluid


10


(i.e. to blow air across the surface of each regenerative bed


12


as described above).





FIG. 3

illustrates an alternative embodiment of the invention which functions in a manner similar to the embodiment of

FIG. 2

but employs a different drive mechanism. As in the

FIG. 2

embodiment, refrigeration elements


22


comprise an ordered array of elongate tubes


26


for containing working fluid


24


. However, in this embodiment tubes


26


have a fixed volume. A shuttle


34


is mounted for reciprocal movement in each tube


26


to alternatively compress and expand working fluid


24


. Each shuttle


34


divides a corresponding tube


26


into separate first and second chambers


29


,


31


. An annular seal surrounding each piston prevents the flow of working fluid between chambers


29


,


31


. As shown in

FIG. 3

, shuttles


34


preferably move in unison to ensure that working fluid


24


in all of the chambers


29


is compressed simultaneously while all of the fluid


24


in chambers


31


is expanded simultaneously, or vice versa. Flow of heat transfer fluid


10


relative to tubes


26


is timed to the contraction and expansion strokes as described above.




Each shuttle


34


is preferably electromagnetically driven by a drive coil


40


that operates on a magnet


42


embedded in shuttle


34


. When shuttle


34


is in the central neutral position shown in

FIG. 3

, the pressure of working fluid is the same in chambers


29


and


31


. When shuttle


34


is driven toward chamber


29


, working fluid


24


in chamber


29


is compressed while fluid


24


in chamber


31


is expanded. Conversely, when shuttle


34


is driven toward chamber


31


, working fluid


24


in chamber


31


is compressed while fluid


24


in chamber


29


is expanded. As indicated above, a portion of the energy stored in the compressed working fluid


24


in one chamber


29


,


31


is recovered when that chamber becomes the chamber in the expanded fluid state, since the pressure differential across piston


34


helps to drive shuttle


34


toward the neutral position.




In the specific example of this embodiment illustrated in

FIG. 3

shuttle


34


is approximately one half the length of tube


26


and is supported for reciprocal movement within tube


26


by notched guides (not shown). Magnet


42


may include a plurality of small permanent magnetic bars slightly spaced from one another along the central longitudinal axis of piston


34


. In equilibrium, shuttle


34


is located in the central portion of tube


26


and working fluid


24


contained within chambers


29


,


31


is at its mean pressure. Once drive coil(s)


40


are energized with the correct polarity to impose an attractive/repulsive driving force on shuttle


34


, it reciprocates within tube


26


to alternatively compress or expand working fluid


24


in chambers


29


,


31


as discussed above. The frequency of reciprocation may be controlled via a smart electronic module that drives coils


40


. If the period is longer than the thermal time constant of tube


26


(i.e. fractions of a second), the changes in temperature of the tube wall


27


will not be attenuated or significantly out of phase with the drive frequency of shuttle


34


.




As will be apparent to a person skilled in the art, other means for driving shuttles


34


may be employed. For example, movement of shuttles


34


may be actuated by hydraulics or any other prime moving mechanism (i.e. individual tube compressor elements connected to a larger actuated plate).




In a further alternative embodiment of the invention (not shown), shuttle


34


could comprise a simple piston or rod which is periodically inserted into a central portion of chamber


29


,


31


to decrease its effective volume and increase the pressure of working fluid


24


contained therein. In this embodiment, the rod could reciprocate relative to a stationary central seal subdividing tube


26


into chambers


29


,


31


. One advantage of this embodiment is that working fluid


24


may remain in contact with the entire inner surface area of tube


26


during the compression and expansion cycles (and hence the surface area available for heat transfer is not reduced during the compression step). In other words, reciprocation of the rod would result in radial rather than axial compression of the working fluid.





FIGS. 4 and 5

illustrate a further embodiment of the invention which functions in a manner similar to the embodiments of

FIGS. 2 and 3

but employs an alternative drive mechanism. As in the other embodiments described above, refrigeration elements


22


comprise an ordered array of elongate tubes


26


for containing working fluid


24


. The cycles of compression and expansion are enacted within tubes


26


by means of expandable bladders


44


coupled to a compressor


46


. Operation of compressor


46


either forces a fluid into or withdraws a fluid from a supply conduit


48


in communication with bladders


44


. During the compression stroke fluid from supply conduit


48


is forced into bladders


44


thereby causing bladders


44


to expand to a larger volume within each tube


26


. This in turn causes compression of working fluid


24


contained in tubes


26


(FIG.


4


). During the decompression step fluid is withdrawn from supply conduit


48


causing a contraction in the volume of bladders


44


and a consequential expansion of working fluid


24


within tubes


26


(FIG.


5


). Flow of heat transfer fluid


10


relative to tubes


26


is timed to the contraction and expansion cycles as described above. The fluid in bladders


44


could be a liquid and need not be the same as working fluid


24


.





FIGS. 6 and 7

illustrate a further alternative embodiment of the invention that also employs a compressor


46


which pumps fluid into or withdraws fluid from a supply conduit


48


operatively coupled to tubes


26


. In this embodiment, the fluid pumped by compressor


46


is the working fluid


24


that flows into and out of tubes


26


through individual passive regenerators


50


. Passive regenerators


50


are necessary in this embodiment to maintain an effective temperature gradient across regenerative bed


12


. In this embodiment compressor


46


may operate at room temperature.




During the compression stroke illustrated in

FIG. 6

, working fluid


24


is pumped into conduit


48


and through individual passive regenerators


50


into corresponding tubes


26


. Flow of working fluid


24


into each tube


26


increases the pressure of fluid


26


therein resulting in an increase in temperature of each tube


26


. Passive regenerators


50


ensure that working fluid


24


in each tube


26


is thermally isolated from working fluid in supply conduit


48


. More particularly, each passive regenerator


50


cools the incoming fluid


24


to approximately the mean temperature of the fluid


24


contained in the corresponding tube


26


(which will vary depending upon the location of the tube


26


in the temperature gradient spanning regenerative bed


12


as discussed above). Passive regenerators may comprise, for example, a plug of porous material having sufficient thermal mass to maintain the temperature difference between each regenerator tube


26


and supply conduit


48


.




During the decompression step illustrated in

FIG. 7

, compressor


46


expands working fluid


24


in conduit


48


causing net flow of working fluid


24


from tubes


26


into conduit


48


through passive regenerators


50


. This results in expansion of working fluid


24


within tubes


26


, resulting in a decrease in the temperature thereof. As in the previously described embodiments of the invention, flow of heat transfer fluid


10


relative to tubes


26


is timed to the alternating contraction and expansion strokes.





FIG. 8

illustrates a further alternative embodiment of the invention which also employs a common compressor


46


for pumping working fluid


24


. In this embodiment compressor


46


is operatively coupled to tubes


26


by means of a common regenerator


52


rather than a plurality of individual passive regenerators


50


. In order to maintain the temperature gradient across regenerative bed


12


, common regenerator


52


must exhibit a similar temperature gradient. Common regenerator


52


may be specifically sized or tapered to account for reduced mass flow rates required along its length (i.e. from hot end to cold end).




During the compression portion of the refrigeration cycle, working fluid


24


is forced by compressor


46


into common regenerator


52


. Working fluid


24


is cooled along the length of regenerator


52


to approximately the temperature of each tube


26


in communication with the corresponding portion of regenerator


52


. Accordingly, working fluid


24


flows from regenerator


52


into each tube


26


at approximately the mean temperature of the respective tube


26


. The net inflow of working fluid


24


causes compression of working fluid


24


and hence an increase in temperature of tubes


26


. Flow of working fluid


24


is reversed during the expansion portion of the refrigeration cycle, causing fluid


24


to flow into regenerator


52


along its length at different temperatures to maintain the temperature gradient.




One advantage of the

FIG. 8

design over the embodiment of

FIGS. 6 and 7

is that only a single regenerator


52


is required to operatively couple compressor


46


to regenerative bed


12


rather than a plurality of individual regenerators


50


. This reduces the complexity of the apparatus and may result in lower manufacturing costs.





FIGS. 9



a


and


9




b


illustrate a further alternative embodiment of the invention wherein working fluid


24


is external to the conduits containing heat transfer fluid


10


rather than vice versa. For example, heat transfer fluid may be circulated through a plurality of parallel tubes


54


surrounded by working fluid


24


contained within a vessel


56


.




In the

FIGS. 9



a


/


9




b


embodiment, each refrigeration element


22


comprises a separate compartment


58


of vessel


56


through which tubes


54


extend. As in other embodiments of the invention described above, heat transfer fluid


10


and working fluid


24


are physically separated. A plurality of compartments


58


are preferably provided to maintain an effective temperature gradient within vessel


56


. Division of vessel


56


into multiple compartments


58


is a function of desired efficiency and may be modified.




As in some previously described embodiments of the invention, vessel


56


is a dual compressor and expander enabling work recovery. Parallel regenerative beds


12


are located at opposite ends


60


and


62


of vessel


56


. Work is inputted into the cycle by reciprocation of a moveable wall


64


coupled to a flexible central wall portion


65


of vessel


56


or some other suitable compression means such as synchronized dual acting pistons mounted for movement within compartments


58


. Wall


64


divides each compartment


58


into a first chamber


66


and a second chamber


68


(

FIG. 9



a


). In the illustrated embodiment, wall


64


is displaced toward end


62


of vessel


56


resulting in expansion of working fluid


24


within chambers


66


and compression of working fluid


24


within chambers


68


. Heat transfer fluid


10


is circulated through tubes


54


at vessel end


60


from hot exchanger


18


to cold heat exchanger


14


; and simultaneously through tubes


54


at vessel end


62


from cold heat exchanger


14


to hot heat exchanger


18


. When wall


64


is displaced in the opposite direction toward vessel end


60


, the flow of heat transfer fluid


10


is reversed.




The

FIGS. 9



a


/


9




b


embodiment of the invention has several inherent advantages. Compartments


58


may be much larger in volume than elongate tubes


26


employed in alternative embodiments of the invention described above. This permits much larger volumes of working fluid


24


to be simultaneously compressed while avoiding the inefficiencies of the “pulse tube effect”. When compressing the working fluid


24


using a common compressor through passive regenerators


50


, such as shown in

FIGS. 6

,


7


and


8


, each tube


26


will exhibit a temperature gradient along its longitudinal length. This pulse tube effect is due to the fact that the fluid entering each tube


26


through the passive regenerator does so at a relatively common temperature due to the large thermal mass of passive regenerators


50


. The first portion of fluid entering tube


26


during the first part of compression stroke of the cycle is compressed by the next portion of fluid entering tube


26


, which is compressed by the next portion of fluid and so on. Therefore the first portion of fluid entering tube


26


is subsequently compressed and displaced towards the closed end of tube


26


. This portion of fluid will also experience the highest temperature change. The last portion of fluid entering tube


26


at the end of the compression stroke will have the lowest temperature change and will be only slightly higher in temperature than the end of the passive regenerator. Therefore a temperature gradient will form along the length of each tube


26


, with the highest temperature at the closed end of tube


26


and the lowest temperature at the open end of tube


26


near the passive regenerator.




Further, since the working fluid


24


is compressed externally to the heat transfer fluid


10


, it is not necessary to use tubes having very thin walls. Rather, regular thin-walled tubes


54


may be employed. Since the working fluid of this embodiment is not confined to the internal volume of tubes


26


, a larger volume of working fluid


24


may be employed thereby increasing the thermal mass ratio of working fluid


24


to heat transfer fluid


10


and the wall material of tubes


54


. The heat transfer coefficient between tubes


54


and working fluid


24


may be further increased by incorporating flow elements that direct working fluid


24


across the banks of tubes


54


during compression and expansion.





FIGS. 10



a


and


10




b


illustrate a further alternative embodiment of the invention which is a variation of the embodiment of

FIG. 9

(i.e. working fluid


24


is compressed and expanded externally of heat transfer fluid


10


). In this embodiment refrigeration element


22


comprises a vessel


70


having annular end plates


72


and a gusseted sidewall


74


which is expandable and compressible in an accordion-like fashion to compress or expand working fluid


24


contained therein. End plates


72


are preferably formed from a thermally non-conductive material so that each element


22


operates at a discrete temperature as discussed further below. Heat transfer fluid


10


flows within vessel


70


through at least one heat transfer tube


54


. In the illustrated embodiment a plurality of heat transfer tubes


54


extending between end plates


72


are shown. Tubes


54


also have flexible gusseted sidewalls to enable compression and expansion of tubes


54


as vessel


70


expands and contracts. Each tube


54


has an inlet


76


on one end plate


72


and an outlet


78


on the other end plate


72


. Preferably a plurality of parallel tubes


54


are provided to maximize the surface available for heat transfer. Vessel


70


has a variable internal volume and is adjustable between a compressed configuration (

FIG. 10



a


) and an expanded configuration (

FIG. 10



b


).





FIGS. 11



a


and


11




b


illustrate a further alternative embodiment of the invention. This embodiment is similar to the embodiment of

FIGS. 10



a


and


10




b


except that only a single heat transfer tube


54


is provided which is wound in a spiral configuration within vessel


70


. As in the

FIG. 10

embodiment, heat transfer tube


54


is compressible and expandable and includes an inlet


76


on one end plate


72


and an outlet


78


on the other end plate


72


. As a result of its spiral configuration, the heat transfer tube


54


of

FIG. 11

has a relatively large surface available for heat transfer in both the compressed (

FIG. 11



a


) and expanded (

FIG. 11



b


) configurations. Accordingly, only one tube


54


per refrigeration element


22


may be required.





FIGS. 12



a


and


12




b


illustrate a plurality of refrigeration elements


22


stacked on top of one another to form a regenerative bed or module


12


. For example, elements


22


may be operatively coupled together between cold heat exchanger


14


and hot heat exchanger


18


(not shown in

FIGS. 12



a


and


12




b


). The heat transfer tubes


54


of adjacent refrigeration elements


22


are connected together to enable flow of heat transfer fluid


10


through the entire regenerative bed


12


. In particular, an outlet


78


of one element


22


is connected to an inlet


76


of the next-in-series element


22


. Working fluid


24


in each refrigeration element


22


in the stack is thermally isolated from working fluid


24


in an adjacent element


22


by end plates


72


to enable the establishment of a temperature gradient across bed


12


. As explained above, refrigeration elements


22


are thermally coupled by connecting the heat transfer fluid outlet


78


of one element


22


to an inlet


76


of the next-in-series element


22


. The first and last elements


22


in the array could be thermally coupled to heat exchangers


14


,


18


as in the embodiments described above.





FIG. 12



a


illustrates a stack of refrigeration elements


22


in a compressed configuration and

FIG. 12



b


show the stack of refrigeration elements


22


in an expanded configuration. As discussed above, the flow direction of heat transfer fluid


10


through heat transfer tubes


54


within regenerative bed


12


preferably alternates with compression and expansion strokes.




The embodiments of

FIGS. 10-12

exhibit the advantages of a modular design. The number of refrigeration elements


22


may vary depending upon the refrigeration specifications (i.e. the temperature gradient) required. Each refrigeration element


22


preferably operates at a discrete mean temperature within the temperature gradient (i.e. corresponding to a separate regenerator tube


26


of the

FIGS. 2-8

embodiments or a separate vessel compartment


58


of the

FIG. 9

embodiment, each tube or compartment operating at a designated temperature). Each refrigeration element


22


could be tailored to operate optimally at its designated temperature, such as by selecting a working fluid


24


near its critical point at the designated temperature.





FIGS. 13 and 14

illustrate a plurality of refrigeration elements


22


arranged in dual regenerative beds


12


that are operatively coupled together. In particular, beds


12


are expanded and contracted in tandem to enable work recovery. In the embodiment of

FIG. 13

, an axially displaceable piston


80


reciprocates back and forth to provide the work input. During a first stroke of piston


80


a first group


82


of refrigeration elements


22


will be compressed and a second group


84


of refrigeration elements


22


will be simultaneously expanded. During the second stroke of piston


70


the first group


82


will be expanded and the second group


84


will be compressed. In each case the working fluid


24


contained within each refrigeration element


22


will change in temperature, thereby causing transfer of heat to, or acceptance of heat from, heat transfer fluid


10


circulated through tubes


54


.




In the embodiment of

FIG. 14

a rocker arm


86


pivots about an axis


88


to alternatively compress and expand dual regenerative beds


12


to enable work recovery in a similar manner to the embodiment of FIG.


13


.





FIG. 15

illustrates a further alternative embodiment of the invention wherein regenerative bed


12


comprises a common, unitary sidewall


89


rather than a gusseted or bellows-type sidewall. In the embodiment of

FIG. 15

, refrigeration elements


22


are separated and thermally isolated by end plates


72


. Plates


72


are sealed and moveable relative to common sidewall


89


to vary the volume of elements


22


, thereby compressing or expanding working fluid


24


contained therein. As in the embodiment of

FIGS. 11



a


and


11




b


, a heat transfer tube


54


is wound within the interior of each individual refrigeration element


22


. Refrigeration elements


22


are thermally coupled by connecting the heat transfer fluid outlet


78


of one element


22


to an inlet


76


of the next-in-series element


22


as described above.





FIG. 16



a


illustrates a further alternative embodiment of the invention which relies on rotary rather than reciprocal movement to effect compression and expansion cycles, but otherwise shares the same functional principles as the embodiments described above. Heat transfer fluid


10


moves in a continuous fashion through the heat transfer loop. In particular, fluid


10


from hot heat exchanger


18


is pumped into the cold end of regenerative bed


12


by means of blower


90


. The cold part of bed


12


(i.e. where heat transfer fluid


10


flows radially inward) comprises a plurality of elongated tubes


26


each containing expanded working fluid


24


. After depositing heat to elongated tubes


26


, the cooled heat transfer fluid


10


enters cold heat exchanger


14


to cool the thermal load and provide the refrigeration effect. Heat transfer fluid


10


is discharged from cold heat exchanger


14


into the hot part of regenerative bed


12


comprising contracted tubes


26


containing compressed working fluid


24


. Here heat transfer fluid


10


accepts heat from tubes


26


as it flows radially outward. The outwardly flowing heat transfer fluid


10


transfers the heat to hot heat exchanger


18


to complete the cycle. Heat transfer fluid


10


may be conveyed in either a closed cycle or an open cycle using room temperature air as described above.




Work is inputted into the system by means of a motor


91


driving the rotary movement. Rotation of regenerative bed


12


causes alternative extension and contraction of tubes


26


, and consequential expansion and contraction of working fluid


24


, depending upon the arc of rotation. As will be apparent to a person skilled in the art, rotary devices have the potential for higher frequency operation than reciprocating devices. This may help reduce the size of the apparatus and potentially reduce capital costs.





FIG. 16



b


illustrates one possible embodiment of a rotary refrigerator comprising a plurality of regenerative beds


12


to enact an active regenerative cycle. This rotary refrigerator includes a rotatable carousel


92


mounted on a column


94


. Carousel


92


has a plurality of circumferentially spaced baffles


95


defining compartments


96


therebetween. Slotted upper and lower plates


98


and


100


are coupled to baffles


95


to define the upper and lower end walls of compartments


96


. Upper plate


98


is disposed at an angle relative to lower plate


100


and is moveable relative to baffles


95


to vary the size of compartments


96


. In particular, upper plate


98


is coupled to a shaft


109


that rotates about an axis which intersects the plane of lower plate


100


a non-perpendicular angle (

FIGS. 16



b


and


16




c


). A plurality of extensible tubes


26


containing working fluid


24


extend within each compartment


96


between plates


98


,


100


. The length of each extensible tube


26


within a compartment


96


(and hence the temperature of the working fluid


24


contained therein) varies depending upon the radial position of such tube


26


. Each compartment


96


therefore essentially constitutes a discrete regenerative bed


12


having a temperature gradient between the outside diameter and the inside diameter of carousel


92


(

FIG. 16



d


)




Carousel


92


is mounted on column


94


as shown in

FIGS. 16



b


and


16




c


. Column


94


consists of a fixed heat transfer fluid supply cylinder


102


sub-divided by a central interior separator wall


104


. Wall


104


subdivides cylinder


102


into a first conduit


105


and a second conduit


107


. Column


94


also includes a rotatable support platform


106


at its upper end and a pair of opposed, upwardly extending support arms


108


. As shown best in

FIG. 16



c


, carousel


92


is adapted to rest on support platform


106


between support arms


108


when carousel


92


and column


94


are assembled together.




In use, rotation of carousel


94


about the axis of shaft


109


causes periodic expansion and contraction of extensible tubes


26


and hence changes in the temperature of working fluid


24


contained therein. At the expanded end of the cycle, heat transfer fluid


10


from hot heat exchanger


18


flows into compartments


96


and past expanded tubes


26


before flowing downwardly into first conduit


105


within cylinder


102


to cold heat exchanger


14


. At the same time, on the opposite side of separator wall


104


, heat transfer fluid


10


from cold heat exchanger


14


flows upwardly through cylinder conduit


107


into carousel compartments


96


at the cold end of the cycle. As shown in the drawings, the heat transfer fluid


10


flows past contracted tubes


26


before passing to hot heat exchanger


18


.




As discussed above, each variable volume compartment


96


essentially constitutes a separate regenerative bed


12


. The mean temperature of each regenerative bed


12


depends upon the position of bed


12


in the rotary cycle (i.e. whether extensible tubes


26


are in a relatively contracted configuration or a relatively expanded configuration, corresponding to the variable volume first and second chambers


29


,


31


of FIG.


3


). As shown best in

FIG. 16



d


, the flow direction of heat transfer fluid


10


through each regenerative bed


12


similarly depends upon the position of such bed


12


in the rotary cycle. As in the other embodiments of the invention described above, a temperature gradient is established within each individual regenerative bed


12


(irrespective of its position in the rotary cycle) since the length of each tube


26


(and hence the temperature of working fluid


24


contained therein) varies depends upon its relative radial position. Of course, the radial position of each individual tube


26


is fixed and does not vary during the rotary cycle.




The rotary embodiment of FIGS.


16


(


a


)-


16


(


d


) differs from other embodiments described above in that the flow direction of heat transfer fluid


10


does not periodically reverse. Rather, the relative position of each regenerative bed


12


changes relative to the flow paths of the heat transfer fluid


10


to enact the regenerative refrigeration cycle.




Other design variations are possible without departing from the applicants' invention. As will be apparent to a person skilled in the art, the heat capacity of a gas changes significantly near its critical point (i.e. the point at which it becomes a fluid). The use of a series of working fluids


24


, each near its respective critical point, will allow a large change in thermal mass of individual tubes


26


(or individual compartments


58


or vessels


70


) upon compression or expansion of working fluid


24


contained therein. This combined variable thermal mass can be arranged to allow a much larger thermal mass in the cold blow of heat transfer fluid


10


(i.e. from cold heat exchanger


14


toward hot heat exchanger


18


across regenerative bed


12


) than in the hot blow of heat transfer fluid


10


(i.e. from hot heat exchanger


18


toward cold heat exchanger


14


across regenerative bed


12


). This imbalance or asymmetry in the amount of heat transfer fluid


10


required for the two reciprocating flows potentially allows excess heat transfer fluid


10


to be cooled during one part of the cycle. This “excess” heat transfer fluid


10


not required for balanced operation of regenerative bed


12


may be diverted to a separate flow path external to bed


12


to perform useful refrigeration. For example, the excess volume of cooled heat transfer fluid


10


may be diverted to an external process heat exchanger (not shown) to cool and liquefy a separate process stream before returning such heat transfer fluid


10


to the hot end of regenerative bed


12


.




Other means for using the changes in thermal mass of tubes


26


(or compartments


58


or vessels


70


) during the compression and expansion strokes may be envisioned when the application is in cryogenic temperatures. One approach is to add a layer of magnetic material to create an imbalanced thermal mass in the regenerator as its temperature increases and decreases. The heat capacity of magnetic materials peaks sharply near an ordering temperature such as the Curie temperature in a ferromagnetic order. The heat capacity is significantly larger below the transition temperature than above the transition temperature.




By adding a layer of appropriately chosen magnetic material to a regenerator tube


26


or other vessel containing working fluid


24


, the effective thermal mass is significantly imbalanced for the two periodic flows of the heat transfer fluid. For example, introduction of more working fluid


24


into a tube


26


causes working fluid to compress and heat up above the ordering temperature. Conversely, as working fluid exits tube


26


it expands and cools. This temperature decrease is such that the temperature of tube


26


is below the Curie temperature and the thermal mass of the magnetic layer balances the reduction in thermal mass from the exiting fluid


24


. The amount of heat transfer fluid in the regenerator from hot to cold is larger than the flow required in the regenerator from cold to hot. The excess heat transfer fluid must be returned via an external path such as via a process heat exchanger where it can cool and liquefy a process stream. The materials can be chosen to have Curie temperatures close to the small operating range of each tube


26


in regenerative bed


12


. Further, the materials can be added in thickness to effect the required temperature swings to be above and below the Curie temperatures at appropriate times during the refrigeration cycle.




As should be apparent from the foregoing description, applicants' active regenerative cycle is unique since each refrigeration element


22


undergoes a unique refrigeration cycle based on its relative position in regenerative bed


12


and hence its absolute operating temperature.

FIG. 17

shows the temperature distribution of refrigeration elements


22


over an operating cycle. If it assumed that each refrigeration element


22


undergoes a Brayton cycle (i.e. adiabatic compression and isentropic expansion processes linked with two passive heat transfer processes), the total work for a regenerator is the sum of each refrigeration element


22


.

FIGS. 18



a


and


18




b


illustrate the work input and heat flows associated with operation of applicants' invention, namely a series of separate thermally coupled elements


22


each undergoing a unique refrigeration cycle.




There are two primary thermodynamic constraints directly relevant to applicants' invention. First, the work input must be sufficient to transfer the cooling load across the temperature span to the heat sink including all entropy generated by irreversible losses, i.e.:






W


net


=W


brayton


+W


irreversible








Secondly, the adiabatic temperature changes at the hot and cold ends of the regenerative bed


12


must be sufficient to pick up and reject the cooling load.




In order to optimize the efficiency of the refrigeration cycle the irreversible losses must be minimized. There are four major entropy generation mechanisms in the cycle that cause irreversible losses, namely:




(1) Thermal washing effects. These losses are caused by the fact that the thermal mass of the refrigeration elements


22


cannot be infinite when compared to the thermal mass of the heat transfer fluid


10


. Accordingly, the heat transfer fluid


10


will “wash” the refrigeration elements


22


of some of their thermal energy and thus lower the possible adiabatic temperature change available (thereby decreasing the work done).




(2) Imperfect heat transfer. The heat transfer rate from the refrigeration elements


22


to the heat transfer fluid


10


will not be infinite. The lower the rate, the greater the temperature approach will be between the heat transfer fluid


10


and elements


22


. The greater the temperature approach, the less adiabatic temperature will be available and the greater work input will be required.




(3) Working fluid conduction/mixing. In an ideal regenerative bed


12


, the working fluid in each refrigeration element


22


undergoes a unique cycle based on its absolute temperature and the absolute temperature gradually changes over the span between the hot and cold ends of bed


12


. In order to work effectively, the working fluid


24


at one temperature must be prevented from mixing with working fluid at different temperatures. Thus a discrete barrier separating each refrigeration element


22


is required. The degree of non-continuity in the temperature profile and conduction across the barrier will cause loss.




(4) Heat transfer between working fluid and tube wall. As the working fluid


24


is compressed or expanded, its temperature will change relative to the tube wall separating it from the heat transfer fluid


10


. This temperature difference will produce entropy which will decrease the efficiency of the device.





FIG. 18



a


is a temperature-entropy graph of an ideal Brayton regenerative cycle of a single refrigeration element


22


of the applicant's invention. Initially, at time


1


, working fluid


24


within the element


22


is at a temperature T


1


. Working fluid


24


is then compressed adiabatically so that its temperature at time


2


has increased to T


1+Δ


T


1


. A cold blow of heat transfer fluid


10


(i.e. from cold heat exchanger


14


toward hot heat exchanger


18


) is then passed through element


22


to accept heat from working fluid


24


, thereby reducing the temperature of working fluid


24


at time


3


to T


2


. Working fluid


24


is then adiabatically expanded to reduce its temperature at time


4


to T


2−Δ


T


2


. Finally, a hot blow of heat transfer fluid


10


(i.e. from hot heat exchanger


18


toward cold heat exchanger


14


) is passed through element


22


to return the temperature of working fluid


22


to temperature T


1


to complete the cycle.




The passive heat input of the cycle, Q


in


, is represented in

FIG. 18



a


by the area under curve


1


-


4


; and the heat output of the cycle, Q


out


, is represented by the area underneath curve


2


-


3


. The difference between Q


out


and Q


in


is determined by the work inputted into the cycle, W


net


, to effect periodic compression and expansion of working fluid


24


.





FIG. 18



b


is temperature-entropy graph of a plurality of refrigeration elements


22


of the applicant's invention having overlapping regenerative cycles. By providing a series of elements


22


each operating at their own mean temperature, the temperature difference which regenerative bed


12


can span is increased accordingly (i.e. a larger temperature gradient is created across regenerative bed


12


). Further, a bank of elements


22


could be provided in parallel at each discrete temperature in the gradient to increase the heat transfer/cooling capacity of the system.




As should also be apparent from the above description, applicants' invention is a heat transfer apparatus and method that may be easily tailored to suit a wide variety of applications. Although the invention has been primarily described with reference to refrigerators, it may have application as an air conditioner, ventilator, heat pump, heat exchanger and the like.




As will be apparent to those skilled in the art in the light of the foregoing disclosure, many alterations and modifications are possible in the practice of this invention without departing from the spirit or scope thereof. Accordingly, the scope of the invention is to be construed in accordance with the substance defined by the following claims.



Claims
  • 1. A heat transfer apparatus employing an active regenerative cycle for transferring beat from a thermal load to a heat sink comprising(A) a regenerator comprising working fluid contained in a plurality of separate first vessels arranged in an ordered array, each of said first vessels having a designated location between said thermal load and said heat sink and having a mean operating temperature corresponding to said designated location; (B) a heat transfer fluid physically separated from said working fluid and in thermal communication with said thermal load and said heat sink; (C) work input means for periodically compressing and expanding said working fluid to alternatively increase and decrease the temperature thereof; and (D) circulation means for periodically circulating said heat transfer fluid relative to said working fluid to either accept heat from or transfer heat to said working fluid.
  • 2. The heat transfer apparatus of claim 1, wherein said heat transfer fluid moves between said thermal load and said heat sink in an oscillatory manner.
  • 3. The heat transfer apparatus of claim 1, wherein said work input means is moveable relative to each of said first vessels to compress a first sub-volume of said working fluid in a first portion thereof and simultaneously cause expansion of a second sub-volume of said fluid in a second portion thereof.
  • 4. The heat transfer apparatus of claim 1, wherein each of said first vessels is thermally isolated from the remainder of said first vessels and wherein the operating temperature of each of said first vessels depends upon said designated location.
  • 5. The heat transfer apparatus of claim 4, further comprising at least one heat transfer channel for confining said heat transfer fluid, wherein said at least one heat transfer channel spans a temperature gradient extending across said regenerator.
  • 6. The heat transfer apparatus of claim 5, wherein said first vessels comprise an upper vessel, a lower vessel and a plurality of intermediate vessels spaced between said upper and lower vessels, and wherein said system further comprises:(A) a high temperature heat transfer system for receiving said heat transfer fluid leaving said heat transfer channel after passing said upper vessel and transferring heat therefrom to said heat sink and for returning said heat transfer fluid to said heat transfer channel; and (B) a low temperature heat transfer system for transferring heat from said thermal load to said heat transfer fluid after said heat transfer fluid has passed said lower vessel.
  • 7. The heat transfer system of claim 1, further comprising at least one second vessel for containing said heat transfer fluid.
  • 8. The heat transfer system of claim 7, wherein said plurality of separate first vessels are located within said second vessel.
  • 9. A heat transfer apparatus employing art active regenerative cycle for transferring heat from a thermal load to a heat sink comprising(A) a regenerator comprising working fluid contained within at least one first vessel; (B) a heat transfer fluid contained within at least one second vessel, wherein said heat transfer fluid is physically separated from said working fluid and is in thermal communication with said thermal load and said heat sink; (C) work input weans for periodically compressing and expanding said working fluid to alternatively increase and decrease the temperature thereof; and (D) circulation means for periodically circulating said heat transfer fluid relative to said working fluid to either accept heat from or transfer heat to said working fluid.
  • 10. The heat transfer system of claim 9, wherein said at least one second vessel is located within said first vessel.
  • 11. The heat transfer system of claim 4, wherein said work input means comprises:(A) a third vessel in fluid communication with each of said first vessels for holding said working fluid; and (B) a compressor for periodically compressing and expanding said working fluid in said third vessel to cause corresponding compression and expansion cycles in each of said first vessels, wherein said working fluid in said third vessel is thermally isolated from said working fluid in said first vessels.
  • 12. The heat transfer system of claim 11, further comprising a plurality of passive regenerators for operatively coupling said third vessel to each of said first vessels.
  • 13. The heat transfer system of claim 4, wherein each of said first vessels comprises an elongated tube and wherein said work input means is moveable relative to a longitudinal axis thereof.
  • 14. The heat transfer system of claim 13, wherein said work input means comprises a shuttle mounted for reciprocal movement in said tube.
  • 15. The heat transfer system of claim 13, wherein said tubes are arranged in a parallel array and wherein said longitudinal axis of each of said tubes extends in a direction generally perpendicular to the flow path of said heat transfer fluid.
  • 16. A method of enacting an active regenerative refrigeration cycle for transferring heat from a thermal load to a heat sink comprising:(A) providing a regenerator spanning a temperature gradient between said thermal load and said heat sink, said regenerator comprising a plurality of separate refrigeration elements each containing a working fluid and having a designated position in said temperature gradient; (B) providing a heat transfer fluid physically separated from said working fluid and movable relative to said refrigeration elements across said temperature gradient between said thermal load and said heat sink; (C) compressing said working fluid contained in each of said refrigeration elements to increase the temperature thereof; (D) moving said heat transfer fluid relative to said refrigeration elements in a flow direction from said thermal load toward said heat sink; (E) expanding said working fluid contained in each of said refrigeration elements to decrease the temperature thereof; and (F) moving said heat transfer fluid relative to said refrigeration elements in a flow direction from said heat sink toward said thermal load.
  • 17. The method of claim 16, further comprising repeating steps (C)-(F) successively.
  • 18. The method of claim 16, where said heat transfer fluid moves between said thermal load and said heat sink in an oscillatory manner.
  • 19. The method of claim 16, wherein steps (C) and (D) occur simultaneously, and wherein steps (E) and (F) occur simultaneously.
  • 20. A regenerative heat transfer device for transferring heat between a thermal load and a heat sink comprising:(a) an array of discrete refrigeration elements spaced apart at intermediate locations between said thermal load and said heat sink, wherein each of said refrigeration elements contains a working fluid and has a mean operating temperature corresponding to its relative location between said thermal load and said heat sink; (b) an actuator for periodically compressing and expanding said working fluid to thereby increase or decrease the temperature of said refrigeration elements; and (c) a circulator for circulating a heat transfer fluid in a flow path between said thermal load and said heat sink, wherein said heat transfer fluid passes relative to said array of refrigeration elements to either accept heat from or transfer heat to said refrigeration elements.
  • 21. The device of claim 20, wherein said working fluid in each of said refrigeration elements is sequentially compressed and expanded in alternating working cycles, wherein said working cycles coincide in each of said refrigeration elements.
  • 22. The device of claim 20, wherein each of said refrigeration elements comprises two separate sealed chambers each containing a volume of said working fluid, wherein said actuator is moveable relative to each of said refrigeration elements to compress said working fluid in one of said chambers and simultaneously expand said working fluid in the other of said chambers, thereby enabling work recovery.
  • 23. The device of claim 20, further comprising a cold heat exchanger for exchanging heat from said thermal load to said heat transfer fluid; and a hot heat exchanger for exchanging heat from said heat transfer fluid to said heat sink.
  • 24. The device of claim 20, wherein said working fluid comprises one or more gases or mixtures thereof, wherein the composition of said working fluid contained in each of said refrigeration elements varies depending upon said mean operating temperature.
  • 25. The device of claim 24, wherein said working fluid contained in each of said refrigeration elements is near its critical point.
  • 26. The device of claim 20, wherein said actuator comprises a rotary drive for rotating said array of refrigeration elements to compress and expand said working fluid over the arc of rotation to thereby increase or decrease the temperature of said refrigeration elements.
  • 27. The device of claim 20, wherein said actuator comprises means for varying the volume of said refrigeration elements.
  • 28. The device of claim 20, wherein said actuator comprises a plurality of pistons, wherein each of said pistons is mounted for reciprocating movement in a corresponding one of said refrigeration elements.
  • 29. The device of claim 28, wherein said actuator further comprises a controller for actuating movement of all of said pistons in unison.
  • 30. The device of claim 20, wherein said actuator comprises a compressor for introducing working fluid into, and withdrawing working fluid from, said refrigeration elements.
  • 31. The device of claim 30, further comprising at least one passive regenerator for operatively coupling said compressor to each of said refrigeration elements, wherein said passive regenerator maintains a temperature gradient across said array of discrete refrigeration elements.
  • 32. The device of claim 20, wherein said circulator comprises a duct for confining said heat transfer fluid to said flow path, wherein at least a portion of each of said refrigeration elements extends into said duct.
  • 33. The device of claim 20, wherein each of said refrigeration elements comprises a thin-walled elongate tube having a longitudinal axis extending parallel to the longitudinal axis of each of the other of said refrigeration elements in said array.
  • 34. The device of claim 20, wherein said heat transfer fluid is air and said circulator comprises an air pump.
  • 35. A refrigeration element comprising:(a) a container for holding a working fluid; (b) at least one conduit extending within said container for holding a heat transfer fluid separate from said working fluid; and (c) an actuator for periodically compressing and expanding said working fluid to vary the temperature of said working fluid.
  • 36. The refrigeration element of claim 35, wherein said actuator compresses said container.
  • 37. The refrigeration element of claim 35, wherein said conduit comprises an inlet and an outlet for connecting said conduit to a volume of heat transfer fluid external to said container.
  • 38. The refrigeration element of claim 35, wherein said container comprises at least two separate chambers each containing a volume of said working fluid, wherein said actuator is moveable relative to said container to compress said working fluid in one of said chambers and simultaneously expand said working fluid in the other of said chambers, thereby enabling work recovery.
  • 39. A regenerative refrigerator comprising a plurality of refrigeration elements as defined in claim 35 connected together such that said heat transfer fluid in adjacent pairs of said elements is in fluid communication.
  • 40. A regenerative refrigerator as defined in claim 39, wherein one of said elements receives said heat transfer fluid from a thermal load and another one of said elements transfers said heat transfer fluid to a heat sink.
  • 41. A regenerative refrigerator as defined in claim 39, wherein each of said plurality of refrigeration elements is thermally isolated.
  • 42. A regenerative refrigerator as defined in claim 41, wherein said refrigeration elements are stackable.
  • 43. A refrigeration element as defined in claim 35, wherein said container comprises thermally non-conductive sections.
  • 44. The heat transfer system of claim 10, comprising a plurality of second vessels located within said first vessel each of said second vessels spanning a temperature gradient extending across said regenerator.
  • 45. A heat transfer apparatus employing an active regenerative cycle for transferring heat from a thermal load to a heat sink comprising(A) a regenerator comprising contained working fluid; (B) a heat transfer fluid physically separated from said working fluid and in thermal communication with said thermal load and said heat sink; (C) work input means for periodically compressing and expanding said working fluid to alternatively increase and decrease the temperature thereof; and (D) circulation means for periodically circulating said heat transfer fluid relative to said working fluid to either accept heat from or transfer heat to said working fluid, wherein said heat transfer fluid moves between said thermal load and said heat sink in an oscillatory manner.
  • 46. A regenerative heat transfer device for transferring heat across a temperature gradient between a thermal load and a heat sink comprising:(a) a regenerator comprising an array of discrete refrigeration elements spaced apart at intermediate locations between said thermal load and said heat sink, wherein each of said refrigeration elements contains a working fluid and has a mean operating temperature corresponding to its relative location between said thermal load and said heat sink; (b) an actuator for periodically compressing and expanding said working fluid to thereby increase or decrease the temperature of said refrigeration elements; and (c) a circulator for circulating a heat transfer fluid relative to said array of refrigeration elements to either accept heat from or transfer heat to said refrigeration elements, wherein said heat transfer fluid is moveable in a first flow path within said regenerator between said thermal load and said heat sink and a second flow path between said regenerator and an auxiliary device capable of accepting or rejecting heat located externally of said regenerator, whereby a portion of said heat transfer fluid is divertable to said auxiliary device.
  • 47. The heat transfer device of claim 46, wherein said auxiliary device is a heat exchanger.
  • 48. A method of cooling a thermal load comprising(a) providing a regenerator comprising an array of discrete refrigeration elements spaced apart at intermediate locations across a temperature gradient, wherein each of said refrigeration elements contains a working fluid and has a mean operating temperature corresponding to its relative location in said temperature gradient; (b) periodically compressing and expanding said working fluid to thereby increase or decrease the temperature of said refrigeration elements,; and (c) periodically circulating a heat transfer fluid relative to said array of refrigeration elements to either accept heat from or transfer heat to said refrigeration elements, wherein a portion of said heat transfer fluid is further conveyed to a thermal load located externally of said regenerator to accept heat therefrom.
  • 49. A regenerative heat transfer device comprising a plurality of refrigeration elements, wherein each of said refrigeration elements comprises:(a) a container for holding a working fluid; (b) at least one conduit extending within said container for holding a heat transfer fluid separate from said working fluid; and (c) an actuator for periodically compressing and expanding said working fluid to vary the temperature of said working fluid, wherein said refrigeration elements are connected together such that said heat transfer fluid in adjacent pairs of said elements is in fluid communication.
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