GB2383631A - Counter flow shell and coil heat exchanger - Google Patents

Counter flow shell and coil heat exchanger Download PDF

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Publication number
GB2383631A
GB2383631A GB0227074A GB0227074A GB2383631A GB 2383631 A GB2383631 A GB 2383631A GB 0227074 A GB0227074 A GB 0227074A GB 0227074 A GB0227074 A GB 0227074A GB 2383631 A GB2383631 A GB 2383631A
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GB
United Kingdom
Prior art keywords
wall
heat exchanger
tubing
fluid
gap
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB0227074A
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GB0227074D0 (en
Inventor
Haiping Hong
Fred Georg Schroeder
Zhongping Zeng
Chao A Zhang
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Visteon Global Technologies Inc
Original Assignee
Visteon Global Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Visteon Global Technologies Inc filed Critical Visteon Global Technologies Inc
Publication of GB0227074D0 publication Critical patent/GB0227074D0/en
Publication of GB2383631A publication Critical patent/GB2383631A/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B40/00Subcoolers, desuperheaters or superheaters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B43/00Arrangements for separating or purifying gases or liquids; Arrangements for vaporising the residuum of liquid refrigerant, e.g. by heat
    • F25B43/006Accumulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/02Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled
    • F28D7/024Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being helically coiled the conduits of only one medium being helically coiled tubes, the coils having a cylindrical configuration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/06Compression machines, plants or systems characterised by the refrigerant being carbon dioxide
    • F25B2309/061Compression machines, plants or systems characterised by the refrigerant being carbon dioxide with cycle highest pressure above the supercritical pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/05Compression system with heat exchange between particular parts of the system
    • F25B2400/051Compression system with heat exchange between particular parts of the system between the accumulator and another part of the cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/002Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
    • F25B9/008Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being carbon dioxide

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Power Engineering (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A heat exchanger 100 comprises helical tubing 104 disposed in a accumulator heat transfer chamber 108 which is between an outer cylinder wall 102 and a coaxial inner cylinder wall 106. Tubing 104 communicates a fluid from a gas cooler (126, fig 2) or a condenser (128, fig 2) to an evaporator 130 into a chamber housing a J-tube 134 which communicates only a vapour to a compressor 125. Chamber 108 is sealed at one end of the walls 102, 106 by a cover 110 and at the other end by a cover 119 attached to a lower portion of the wall 106. Helical tubing 104 has first and second portions which do not make contact with walls 104, 106 so that an inner gap (114, fig 5) and outer gap (116, fig 5) are formed and allow the passage of fluid over the tubing 104. Walls 102, 106 or tubing 104 may have irregular surfaces on them so that tubes may touch both walls but still have gaps between the tubing 104 and the walls 102, 106 to allow fluid to pass. Gaps (114, 116) may be the same size or varied as a function of the distance between adjacent tubing bends. Wall 102 may be thermally insulated from external influences. The helical tubing 104 may be replaced with double helical tubing. A temperature and/or pressure transducer may be attached in the top of the heat transfer chamber 108.

Description

e-> 2383631 $. - 1 COUNTER-FLOW HEAT EXCHANGER WITH OPTIMaL SECoNDARY
CROSS-E'LOW llaCKGROUND OK' I NVEN T:C ON Field of Invention
The present invention relates to heat exchangers, such as a counter-flow heat exchanger.
10 Discussion of Related Art It is well known in the art that counterflow heat exchangers can be used particularly in air conditioners of motor vehicles, such as CO2 air conditioners, in order to provide an accumulator and an internal heat exchanger of 15 the refrigerant circulating system in an integrated arrangement. Examples of known heat exchangers are disclosed in U.S. Patents Nos. 3,955, 375 and 4,895,203 and German Published Patent Application DE 196 35 454 Al. The entire 20 contents of U.S. Patents Nos. 3,955,375 and 4,895,203 are incorporated herein by reference.
In each of the above-identified patents and patent disclosures, a spiral loop is placed between and is in
direct contact with the inner and outer walls of the heat 25 exchanger unit. High pressure, high temperature fluid flows within the tubing while low pressure, low temperature fluid flows outside the tubing and between the inner and outer walls of the heat exchanger unit. Such a design can have several drawbacks. First, the; fluid 30 outside the spiral tube has areas of higher temperature : 3 7:1gp4vl.
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formed where the spiral tubing contacts the inner and outer walls as shown in the Computational Fluid Dynamics analysis illustrated in FIG. 1. This is believed to be caused by the contact between the spiral tubing and the 5 walls that reduces the velocity of fluid flow and, thus, reduces heat exchange. Thus, uneven heat exchange occurs along different positions of the spiral tubing.
Another drawback of known spiral heat exchanger units is that physical contact between the spiral tubing and the 10 inner and outer walls contracts the flow path along the spiral tubing and, thus, increases the drop in pressure.
SPRY OF THE INVENTION
15 One aspect of the present invention regards a heat exchanger that includes a first wall that extends along a first direction and defines a first perimeter in a plane that is perpendicular to the first direction and a second wall that defines a second perimeter and is positioned 20 within the first perimeter, wherein the first wall and the second wall are spaced from one another so as to define a volume of space therebetween. A lid is attached to a top portion of the first wall and a top portion of the second wall and a bottom attached to a bottom portion of the 25 first wall and a bottom portion of the second wall. A spiral tubing is positioned within the volume of space, wherein at least a portion of the spiral tubing does not contact either the first wall or the second wall so that a first gap is formed between the first wall and a first 30 portion of the spiral tubing positioned nearest the first
- 3 wall and a second gap is formed between the second wall and a second portion of the spiral tubing that is positioned nearest the second wall. A first fluid flows within the spiral tubing and a second fluid flows within 5 the first and second gaps.
A second aspect of the present invention regards a method of exchanging heat that includes flowing a high pressure, high temperature fluid within a tubing generally along a first direction and flowing a low pressure, low 10 temperature fluid within a first gap formed between a first wall and a first portion of the tubing positioned nearest the first wall and a second gap formed between a second wall and a second portion of the tubing that is positioned nearest the second wall.
15 Each aspect of the present invention provides the advantage of enhancing heat exchange and reducing pressure drop. The present invention, together with attendant objects and advantages, will be best understood with 20 reference to the detailed description below in connection
with the attached drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Embodiments of the invention will now be described, by way of example only, with reference to the accompanying 25 drawings, in which, FIG. 1 schematically shows a side cross-sectional view of a temperature distribution, via Computational Fluid Dynamics analysis, of a heat exchanger without gaps
- 4 - formed between a spiral tubing and walls of the heat exchanger; FIG. 2 shows a perspective, partially exposed view of a heat exchanger in accordance with the present invention; 5 FIG. 3 shows a bottom view of the heat exchanger of FIG. 2;
FIG 4 shows a side cross-sectional view of the heat exchanger of FIG. 2 taken along line 4-4 of FIG. 3; FIG. 5 shows an enlarged side crosssectional view of 10 the circled portion A of the heat exchanger of FIG. 4i and FIG. 6 schematically shows a side cross-sectional view of a temperature distribution, via Computational Fluid Dynamics analysis, of the heat exchanger of FIGS. 2-
5. 15 DETAILED DESCRIPTION ON THE INVENTION
Referring to the drawings, FIGS. 2-5 show an embodiment of a heat exchanger 100 that combines internal heat exchanging with the functions of a refrigerant accumulator, e.g.: preventing liquid from getting to the 20 compressor, refrigerant storage, oil circulation, desiccation, and sensor attachment. As shown in FIG. 2, the heat exchanger 100 can be used particularly for the refrigerant circulation of a motor vehicle air conditioner, in which CO2, R134a or another conventional 25 refrigerant is used. On the low-pressure side, the collector part of the heat exchanger 100 includes an accumulation chamber 108 that adjoins an evaporator, while, on the high-pressure side, the heat exchanger 100
- 5 is situated between a condenser or gas cooler and an expansion valve.
The heat exchanger 100 includes an overall or outer cylinder wall 102 and a high pressure, high temperature 5 tubing 104 laid inside the outer cylinder wall 102 spirally. Consecutive loops of the spiral tubing 104 are separated from one another by approximately 2mm. The spiral tubing 104 is made of a highly thermally conductive material and creates a large heat exchanging area in a 10 confined volume.
In order to improve the heat exchanging effectiveness of the heat exchanger 100, an inner cylinder wall 106 is positioned inside the outer cylinder 102. The inner cylinder wall 106 and outer cylinder wall 102 are co-axial 15 with respect to one another and define in part an accumulation heat transfer chamber 103 therebetween. The heat exchanger 100 includes a cylinder lid 110 that is attached to the upper edges of the inner and outer walls 106 and 102. Similarly, a bottom 112 is attached to the 20 lower edges of the inner and outer walls 106 and 102. The cylinder lid 110 and bottom 112 each form a seal with the inner and outer walls 106 and 102. The inner cylinder wall 106 has an inner diameter of approximately 60 mm while the outer cylinder wall has an inner diameter of 25 approximately 80 mm. The inner and outer cylinder walls each have a length of approximately 200 mm. The walls 102 and 106 are each made of stainless steel with a thickness of approximately 2 mm.
Note that the inner cylinder wall 106 can be 30 interference fitted, brazed or welded to the cylinder lid
6 - 110 on the top and to the outer cylinder wall 102 on the bottom so as to contain the low pressure, low temperature side refrigerant in the heat transfer chamber 108. The inner cylinder wall 106 separates the low pressure, low 5 temperature refrigerant that is in the heat transfer chamber 108 between the inner wall 106 and the outer wall 102 and that flows along the exterior of the spiral tubing 104 The inner cylinder wall 106 also ensures that the spiral tubing 104, used for counter flow heat exchanging, 10 is compactly packed between the two cylinder walls 102, 106. As shown in FIGS. 4 and 5, the spiral tubing 104 is placed within the heat transfer chamber 108 so that the spiral tubing 104 lies between and does not touch the 15 inner cylinder wall 106 and the outer cylinder wall 102 so that an inner side gap 114 and an outer side gap 116 are formed. The side gaps 114 and 116 are formed along the entire length of the spiral tubing 104. As shown in the cross-sectional view of FIG. 5, for the inner side gap 114 20 the innermost portion 118 of the spiral tubing 104 is located a distance dl from the inner cylinder wall 106 that ranges from 0.2 mm to 0.5 mm, preferably 0.3 mm. For the outer side gap 116, the outermost portion 120 of the spiral tubing 104 is located a distance d2 from the outer 25 cylinder wall 102 that ranges from 0.2 mm to 0.5 mm, preferably 0.3 mm. The distances dl and d2 are chosen so that the inner and outer side gaps 114 and 116 reduce the low side pressure drop without adversely affecting heat exchange performance. The distances dl and d2 can be 30 roughly the same. There exist optimal gap widths dl, d2,
- 7 - such as 0.3 mm, for maximizing heat exchanging. The gaps can always be increased from this optimal value to reduce pressure drop further while the heat exchanging may be affected. However, the reduction in pressure drop is 5 faster than the reduction of the heat exchanging performance if the gap widths are very small.
Note that the widths d1, d2 can be varied as a function of the vertical distance z between two adjacent spiral tubing bends so as to achieve an optimal 10 combination of high heat transfer and low pressure drop.
The optimal value for the widths dl, d2 as a function of the distance z. In particular, the ratio of the widths dl, d2 to the distance z preferably is approximately 0.1.
Without being held to any particular theory, it is 15 believed that the side gaps 114 and 116 create secondary by-pass flow for the low side refrigerant flow, which primarily follows the trajectory path of the spiral tubing 109 and therefore significantly reduces the speed of the flow along the spiral tubing 104. Such secondary by-pass 20 flow involves having a component of the low side refrigerant to flow between the gaps 114 and 116. This secondary by-pass flow can allow a significant reduction in pressure drop. For example, a considerable reduction of low side total pressure drop (about 50%) without having 25 significant reduction in heat transfer is achieved with widths dl, d2 each having a value of approximately 0.3 mm.
In this example, a 2% to 15% increase in heat exchanging is achieved. The percentage of reduction in low side pressure drop along the spiral loop, excluding the effects 30 of the inlet and outlet ports, is much higher.
- 8 It is also believed that the side gaps 114 and 116 also allow the low side to flow more evenly at any position around the circumference of the spiral tubing 104. In FIG. 1, heat exchangers without side gaps have 5 higher temperatures at the positions where the spiral tubing touches the walls, where the flow is very minimal.
On the other hand, in the case of the embodiment of the present invention shown in FIGS. 2-5, there is no higher temperature at the position where the spiral tubing is 10 closest to the wall, where there is cross flow from one spiral loop to the other, taking heat from the high side as shown in FIG. 6. This allows for better heat exchanging at any cross section of the tubing. In addition, the high temperature side refrigerant flows a 15 direction opposite to that of the low temperature side refrigerant, which, aside from the primary flow without high-pressure drop has a secondary cross-flow. The benefit of counter flow heat exchanger is retained allowing high effectiveness of the heat exchanger.
20 Besides providing the advantage of reducing pressure drop without adversely affecting heat exchanging properties, the gaps 114 and 116 allow for more loops of the spiral tubing 104 to be packed per linear length of the walls 102, 106 without incurring a high pressure drop.
25 Accordingly, the gaps 114 and 116 allow for relaxed dimension control, as far as the distance between consecutive loops of the spiral tubing 104 is concerned.
That portion of the heat transfer chamber 108 that is not occupied or displaced by the spiral tubing 104 allows 30 the low pressure, low temperature refrigerant, such as CO2
- 9 - or R134a, to flow along the path of the high pressure, high temperature refrigerant within the spiral tubing 104 but in an opposite direction. Such lay-out provides the opportunity to place heat exchanging tubing compactly and 5 allow for counter-flow heat exchanging.
Please note that the inner cylinder wall 106 can be used as an insulator between the liquid refrigerant and the high pressure, high temperature refrigerant. In addition, the outer cylinder wall 102 can be insulated to 10 prevent the low pressure, low temperature refrigerant from absorbing heat from an engine compartment.
As shown in FIG. 2, the inlet 118 of the spiral tubing 104 extends through the bottom 112 at the step 119 of the outer cylinder wall 102 while the outlet 120 of the 15 spiral tubing 104 extends out of the cylinder lid 110.
The inlet 118 and the outlet 120 form seals with the bottom 112 and the cylinder lid 110, respectively. The high pressure, high temperature fluid flows from the inlet 118, through the spiral portion of the tubing 104 and out 20 of the outlet 120.
The low pressure, low temperature fluid flows in a direction generally opposite than that of the high pressure, high temperature fluid. As shown in FIG. 4, an inlet 122 for the low pressure, low temperature fluid is 25 formed in the cylinder lid 110. An outlet 124 for the low pressure, low temperature fluid is formed in the bottom In operation, a high pressure, high temperature fluid, such as CO2 or R134a, from a gas cooler 126 or 30 condenser 128 flow along the high pressure, high
- 10 temperature inlet 118, runs through the spiral loop portion of the spiral tubing 104 and exits out of the high pressure, high temperature outlet 120 which is connected to an expansion valve and an inlet of an evaporator 130.
5 While the high pressure, high temperature fluid is flowing from inlet 118 to outlet 120, the low pressure, low temperature fluid from the outlet of the evaporator 130 flows along the low pressure inlet 122 and into the heat transfer chamber 108 between the walls 102, 106 and the 10 spiral tubing 104. The fluid portion of the low pressure, low temperature fluid mostly deposits tat the bottom of the accumulator 100 while the vapor portion of the low pressure, low temperature fluid exits the accumulator 100 via the top portion 132 of a J-tube 134. The function of 15 the J-tube 134 is to pick up oil and to prevent liquid refrigerant from reaching the compressor section.
As shown in FIG. 4, an orifice-filter 135 is attached to the J-tube 134. The orifice filter 135 picks a certain amount of liquid from the accumulator 100.
20 One or more oil suction bores (not shown) are provided in the lower area of the accumulator 100. The oil suction bores are dimensioned such that, as a function of the suction effect, the more viscous fluid is sucked to a certain desired extent out of the accumulator 100. In 25 the accumulator 100, the intermediately stored refrigerant is situated in the lower area above the settled oil in the liquid state and in the upper area in the gaseous state.
As a result of the suction effect of the compressor 125, the vapor within the J-tube 134 flows into the space 30 136 defined by the inner cylinder wall 106 and flows out
of the space 136 via an outlet 138 of the J-tube 134 that is located near the top of the inner cylinder wall 106.
The outlet 138 is in fluid communication with the heat transfer chamber 108 that is defined as the space between 5 walls 102 and 106 not displaced by the spiral tubing lO4.
The vapor flows downward in the heat transfer chamber 108 between the coils of the spiral tubing 104 and the spaces between the spiral tubing and inner and outer walls and enters into a withdrawal space, again entraining by way of 10 the suction bores and exits out of the low pressure, low temperature outlet 124 formed in the bottom 112. The outlet 124 is connected via a tube and hose to the compressor 125.
Note that a zero leak joint is only needed on the 15 joints to contain the low pressure, low temperature side refrigerant. Such a zero leak joint includes the lid-outer cylinder joint, which also requires the highest joint strength to contain the pressure, the inlet and outlet fittings. The other internal joints are more 20 tolerable about sealing; brazing satisfies requirements but is not always required.
It is possible to create surface irregularities either on both of the contacting cylinder walls, or on the spiral tubing 104. For example, the inner and outer 25 cylinder walls can have such a profile. Then, the cylinder walls and the spiral tubing 104 are put into position, and the inner cylinder wall 106 is expanded to have the spiral tubing 104 tightly in touch on both sides, with the irregularities creating the optimal side gaps
- 12 between the spiral tubing 104 and the inner and outer cylinder walls.
In another variation of the present invention, the single spiral tubing 104 of FIGS. 2, 4 and 5 is replaced 5 by a double spiral tubing. Thus, more heat exchanging tubing is packed in heat exchanger 100.
Another embodiment of a heat exchanger according to the present invention regards varying the flow pattern of the heat exchanger 100 of FIGS. 2-5. This is accomplished 10 by altering the heat exchanger 100 of FIGS. 2-5 so that the spiral tubing 104 has an inlet formed at the top cylinder lid 110 and an outlet formed at the bottom 112.
A temperature and/or pressure transducer that is required at the heat transfer chamber 108 can be attached at the 15 top of the heat exchanger 100. In this embodiment, the high pressure, high temperature fluid from the gas cooler or condenser flows along the high pressure, high temperature side inlet and runs through the spiral tubing 104 from the top to the bottom of the heat exchanger 100 20 and exits out of the high pressure, high temperature outlet connected to the evaporator. While the high pressure, high temperature flows downward, the low pressure, low temperature fluid flows upward by entering through the bottom 112 via of the inner cylinder wall 106 25 and into the heat transfer chamber 108. The fluid portion of the low pressure, low temperature fluid mostly deposits at the bottom of the accumulator while the vapor portion of the low pressure, low temperature fluid exits the accumulator via the top portion 132 of a J-tube 134. An 30 orifice-filter 135 is attached to the J-tube 134. One or
- 13 more oil suction bores are provided in the lower area of the accumulator. The structures and functions of the J-tube 134 and suction bores are the same as those used in the heat exchanger 100. In this embodiment, the orifice 5 filter 135 performs an additional function besides picking up oil in that it also picks a certain amount of liquid from the accumulator.
The vapor portion of the low pressure, low temperature fluid then flows between the loops of the 10spiral tubing 104 and the inner and outer side gaps 114 and 116, respectively. The vapor portion exits out of the low pressure, low temperature outlet formed in the cylinder lid 110. The outlet is connected via a tube and hose to the compressor.
15The foregoing description is provided to illustrate
the invention, and is not to be construed as a limitation.
Numerous additions, substitutions and other changes can be made to the invention without departing from its scope as set forth in the appended claims.

Claims (1)

  1. - 14 CLAIMS
    1. A heat exchanger comprising: a first wall that extends along a first direction and defines a first perimeter in a plane that is 5 perpendicular to said first direction; a second wall that defines a second perimeter and is positioned within said first perimeter, wherein said first wall and said second wall are spaced from one another so as to define a volume of space therebetween; 10 a lid attached to a top portion of said first wall and a top portion of said second wall; a bottom attached to a bottom portion of said first wall and a bottom portion of said second wall; a spiral tubing positioned within said volume of 15 space, wherein at least a portion of said spiral tubing does not contact either said first wall or said second wall so that a first gap is formed between said first wall and a first portion of said spiral tubing positioned nearest said first wall and a second gap is formed between 20 said second wall and a second portion of said spiral tubing that is positioned nearest said second wall; and a first fluid that flows within said spiral tubing and a second fluid that flows within said first and second gaps. 2. The heat exchanger of claim 1, wherein said spiral tubing in its entirety fails to contact either said first wall or said second wall.
    - 15 3. The heat exchanger of claim 1, wherein a second portion of said spiral tubing contacts both said first wall and said second wall.
    5 4. The heat exchanger of claim 1, wherein said first gap has a magnitude that ranges from 0.2 mm to 0.5 mm. 5. The heat exchanger of claim 1, wherein said 10 second gap has a magnitude that ranges from 0.2 mm to 0.5 mm. 6. The heat exchanger of claim 4, wherein said second gap has a magnitude that ranges from 0.2 mm to 0.5 15 mm.
    7. The heat exchanger of claim 1, wherein a magnitude of said first gap is the same as a magnitude of said second gap.
    8. The heat exchanger of claim 7, wherein said magnitude of said first gap is approximately 0.3 mm:.
    9. The heat exchanger of claim 1, wherein said 25 magnitudes of said first and second gaps are chosen so as to reduce pressure drop without adversely affecting heat exchange performance.
    - 16 10. The heat exchanger of claim 1, wherein magnitudes of said first and second gaps are chosen so as to maximize heat exchanging.
    5 11. The heat exchanger of claim 1, wherein widths of said first and second gaps are varied as a function of distance between adjacent spiral tubing.
    12. The heat exchanger of claim 11, wherein said 10 widths of said first and second gaps are varied so as to achieve an optimal combination of high heat transfer and low pressure drop.
    13. The heat exchanger of claim 1, wherein said 15 spiral tubing is made of a highly thermally conductive material. 14. The heat exchanger of claim 1, wherein said first wall is cylindrical in shape and said second wall is 20 cylindrical in shape.
    15. The heat exchanger of claim 14, wherein said first wall and said second wall are co-axial with respect to one another.
    16. The heat exchanger of claim 1, wherein said first fluid is at a high temperature and high pressure.
    17. The heat exchanger of claim 1, wherein said 30 second fluid is at a low temperature and a low pressure.
    - 17 18. The heat exchanger of claim 16, wherein said second fluid is at a low temperature and a low pressure.
    5 19. The heat exchanger of claim 1, wherein said first and second fluids generally flow in opposite directions with respect to one another.
    20. The heat exchanger of claim 18, wherein said 10 first and second fluids generally flow in opposite directions with respect to one another.
    21. The heat exchanger of claim 18, wherein said first fluid is selected from the group consisting of CO2 15 and R134a.
    22. The heat exchanger of claim 18, wherein said second fluid is selected from the group consisting of CO2 and R134a.
    23. The heat exchanger of claim 21, wherein said second fluid is selected from the group consisting of CO2 and R134a.
    25 24. The heat exchanger of claim 1, wherein said tubing is connected to a gas cooler.
    25. The heat exchanger of claim 1, wherein said tubing is connected to a condenser.
    - 18 26. The heat exchanger of claim 1, further comprising a J-tube having one end in fluid communication with said volume of space.
    5 27. The heat exchanger of claim 1, wherein a first component of said second fluid flows along an exterior of said tubing and a second component of said second fluid flows within said first and said second gaps.
    10 28. A method of exchanging heat, comprising: flowing a high pressure, high temperature fluid within a tubing generally along a first direction; and flowing a low pressure, low temperature fluid within a first gap formed between a first wall and a first 15 portion of said tubing positioned nearest said first wall and a second gap formed between a second wall and a second portion of said tubing that is positioned nearest said second wall.
    20 29. The method of claim 28, wherein said high pressure, high temperature fluid flows in a helical path within said tube.
    30. The method of claim 28, further comprising 25 accumulating said low pressure, low temperature fluid at a bottom of a volume of space defined at least in part by said first wall and said second wall.
    - 19 31. The method of claim 30, further comprising expelling a vapor portion of said low pressure, low temperature fluid present within said volume of space.
    5 32. The method of claim 28, further comprising flowing a portion of said low pressure, low temperature fluid along an exterior of said tubing.
    33. A heat exchanger substantially as herein 10 described, with reference to Figures 2 to 5.
    34. A method of exchanging heat substantially as herein described, with reference to Figures 2 to 5.
GB0227074A 2001-12-28 2002-11-20 Counter flow shell and coil heat exchanger Withdrawn GB2383631A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/034,333 US20030121648A1 (en) 2001-12-28 2001-12-28 Counter-flow heat exchanger with optimal secondary cross-flow

Publications (2)

Publication Number Publication Date
GB0227074D0 GB0227074D0 (en) 2002-12-24
GB2383631A true GB2383631A (en) 2003-07-02

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GB0227074A Withdrawn GB2383631A (en) 2001-12-28 2002-11-20 Counter flow shell and coil heat exchanger

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DE (1) DE10261886A1 (en)
GB (1) GB2383631A (en)

Cited By (8)

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DE102006017432A1 (en) * 2006-04-06 2007-10-11 Visteon Global Technologies Inc., Van Buren Internal heat exchanger forms unit with accumulator in car air conditioning units and comprises toroidal housing in which helical finned pipe for high-pressure coolant is mounted, fins having circular radial cross-section
CN101730326A (en) * 2008-10-21 2010-06-09 乐金电子(天津)电器有限公司 Induction electric heater
CN104034103A (en) * 2014-07-01 2014-09-10 吉首大学 Novel ammonia refrigeration intercooler
FR3051037A1 (en) * 2016-05-04 2017-11-10 Valeo Systemes Thermiques COMPACT THERMAL EXCHANGER
CN109282672A (en) * 2018-09-26 2019-01-29 房玉山 A method of being quickly cooled down hot fluid
CN109341373A (en) * 2018-09-26 2019-02-15 房玉山 A kind of petrochemical industry heat exchanger
US11573036B2 (en) * 2018-02-24 2023-02-07 Sanhua Holding Group, Co., Ltd. Gas-liquid separator and heat exchange system
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