MICROCHANNEL HEAT EXCHANGER

Information

  • Patent Application
  • 20250052503
  • Publication Number
    20250052503
  • Date Filed
    August 08, 2023
    a year ago
  • Date Published
    February 13, 2025
    6 days ago
  • Inventors
    • Klein; Bradley John
    • Barrowclough; Nicholas
Abstract
A heat exchanger tube includes a tube formed substantially of a heat conducting material, the tube being defined by a length, a height, and a width. The heat exchanger tube also includes at least one conduit formed within the tube and extending the length of the tube, the conduit defining an inlet at one end of the tube and the conduit defining an outlet at the opposite end of the tube, the conduit having a cross-section defined within the height and width of the tube, the cross-section having an oscillating geometry.
Description
BACKGROUND

Conventionally, heat exchangers are widely used in refrigeration applications. The heat exchanger typically consists of multiple tubes, fins and two manifolds. A refrigerant flows inside the tubes while outside air passes over the fins. For efficiency, heat exchangers are designed to maximize the surface area of the wall between the two fluids, while minimizing resistance to fluid flow through the exchanger.


Generally, these refrigeration applications require a considerable amount of energy. Many design improvements and refinements have focused on improving the design of the fins and surfaces for exchanging beat between the cooling air and the refrigerant. It is also advantageous to provide design improvements to the multiple tubes through which the refrigerant flows. To accomplish improved minimization of flow resistance and improved heat exchange, microchannel tubes have been used but often not in the most effective manner. Accordingly, improvements to conventional microchannel designs may be advantageous.


SUMMARY

An exemplary embodiment relates to a heat exchanger tube. The heat exchanger tube includes a tube formed substantially of a heat conducting material, the tube being defined by a length, a height, and a width. The heat exchanger tube also includes at least one conduit formed within the tube and extending the length of the tube, the conduit defining an inlet at one end of the tube and the conduit defining an outlet at the opposite end of the tube, the conduit having a cross-section defined within the height and width of the tube, the cross-section having an oscillating geometry.


Another exemplary embodiment relates to a heat exchanger. The heat exchanger includes more than one tube formed substantially of a heat conducting material, each tube being defined by a length, a height, and a width, each tube having an inlet end and an outlet end. The heat exchanger also includes at least one conduit formed within each tube and extending the length of each tube, the conduit defining an inlet at one end of each tube and the conduit defining an outlet at the opposite end of each tube, the conduit having a cross-section defined within the height and width of each tube, the cross-section having an oscillating geometry. Further, the heat exchanger includes an inlet manifold fluidly coupled to each of the inlet ends of the more than one tubes and configured to receive a fluid. Further still, the heat exchanger includes an outlet manifold fluidly coupled to each of the outlet ends of the more than one tubes. Yet further still, the heat exchanger includes heat conducting structures conductively coupled to the more than one tubes.


In addition to the foregoing, other system aspects are described in the claims, drawings, and text forming a part of the disclosure set forth herein. The foregoing is a summary and thus may contain simplifications, generalizations, inclusions, and/or omissions of detail; consequently, those skilled in the art will appreciate that the summary is illustrative only and is NOT intended to be in any way limiting. Other aspects, features, and advantages of the devices and/or processes and/or other subject matter described herein will become apparent in the disclosures set forth herein.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 2 is an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 3 is an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 4 is an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 5 is an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry in accordance with conventional microchannel design.



FIG. 6 is partial perspective view of an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 7 is partial perspective view of an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 8 is partial perspective view of an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 9 is partial perspective view of an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 10 is partial perspective view of an illustrative embodiment of a cross-section of a heat exchanger tube having an exemplary geometry.



FIG. 11 is a partial perspective view of a heat exchanger having tubes in accordance with an exemplary embodiment.



FIG. 12 is a cutaway view of the heat exchanger of FIG. 12.



FIG. 13 is a graph depicting a comparison of fluid pressure drop between two microchannel designs.



FIG. 14 is a graph depicting a comparison of heat transfer between two microchannel designs.





The use of the same symbols in different drawings typically indicates similar or identical items unless context dictates otherwise.


DETAILED DESCRIPTION

Referring to FIGS. 1-5, cross-sections of a variety of tubes 100, 200, 300, 400, and 500 are configured for carrying refrigerant in a heat exchanger. Each of tubes 100-500 are configured as substantially flat having a width that is substantially greater than the thickness. Each of tubes 100-500 include a variety of cross-sectional geometries of the conduits 110, 210, 310, 410, and 510 of tubes 100, 200, 300, 400, and 500 respectively. Each of the conduits 110-510 may be termed microchannels with geometry 510 being of conventional design and conduits 110, 210, 310, 410 having geometries configured in accordance with exemplary embodiments.


In accordance with exemplary embodiments a heat exchanger may be configured with tubes, such as but not limited to tubes 100-400 having microchannel conduits or channels 110-410. A microchannel heat exchanger is characterized by having fluid conduits or channels with a high aspect ratio, small hydraulic diameter. Such microchannel heat exchangers may be applied in any of a variety of applications including but not limited to cooling integrated circuits, solid-state lasers, computer servers, data centers, and the like. Microchannels have been understood since the early 1980s.


One of the advantages of using the microchannel structures is that turbulent flow within the channels is not necessary to increase heat transfer efficiency. Microchannel structures neither require nor create turbulent flow. Conventional macrochannels require turbulence to increase heat transfer rate, otherwise the fluid acts as an insulator between the channel wall and the center of the fluid flow, which is known as a thermal boundary layer. Turbulent flow within the fluid channel mixes the fluid next to the wall of the channel with the fluid in the middle of the channel, thereby minimizing the thickness of the thermal boundary layer and maximizing the rate of heat transfer between the fluid and the wall. However, such turbulence and mixing require high flow velocities and high pressures. Microchannels, instead, have the advantage that the heat transfer coefficient “h” is inversely proportional to the width of the channel. As “h” increases, efficiency increases. A very narrow channel has a thin thermal boundary layer, because the boundary layer cannot be larger than ½ the channel width. Thus, heat is transferred between the wall and the center of the channel with very little thermal resistance.



FIG. 5 is representative of a cross-section of a conventional heat transfer tubes 500 having microchannel conduits 510. One way to increase the heat transfer efficiency of the heat transfer tubes, such as tube 500 is to increase the effective width of the channel relative to the height of the channels within a given width of tube. FIGS. 1-4 depict exemplary embodiments of microchannel geometries which increase the heat transfer efficiency of tubes 100-400 as compared to conventional geometries such as but not limited to those in FIG. 5.


Referring now to FIG. 6, a perspective view of tube 200 with microchannel conduits 210 of FIG. 2 is depicted. A s can be seen microchannel conduits 210 are configured as having substantially sinusoidally shaped cross-section. As depicted, tube 200 contains four (4) microchannel conduits with a cross-section which is a one and a quarter wavelengths and one microchannel conduit being three-fourths of a wavelength.


Referring now to FIG. 7, a perspective view of tube 300 with microchannel conduits 310 of FIG. 3 is depicted. As can be seen microchannel conduits 310 are configured as having substantially sinusoidally shaped cross-section. As depicted, tube 300 contains three (3) microchannel conduits with a cross-section which is a one and a half wavelengths and one microchannel conduit being one and a quarter of a wavelength.



FIGS. 8-10 depict other various embodiments which may be provided to improve the thermal and hydraulic performance as compared with conventional designs. FIG. 8 depicts a tube 800 having a sinusoidal geometry microchannel conduit 810 extending substantially the width of tube 800. FIG. 9 depicts a tube 900 having a square wave geometry microchannel conduit 910 extending substantially the width of tube 900. FIG. 10 depicts a tube 1000 having a triangle wave or sawtooth wave geometry microchannel conduit 1010 extending substantially the width of tube 1000. FIGS. 8-10 are representative of a variety of geometries of microchannel conduits forming tubes configured for use in heat exchanger designs. Although only specific cross-sectional geometries are depicted, many other geometries may be contemplated without departing from the scope of the disclosure. For example, other oscillating (or corrugated) cross-sectional patterns or waveforms may also be used. Further, the cross-sectional geometries may be a combination of various oscillating patterns or waveforms. Generally, what is shown is that various cross-sectional geometries may be used which allow for a greater effective width of conduit (because of the oscillating design) to be formed within a given tube while still maintaining properties and benefits of microchannels used in cooling (or heating) applications. Such properties, where the very narrow microchannel completely heats a very thin layer of fluid as it travels through the conduits of the heat exchanger tubes. Whether different designs meet such properties and provide such benefits as microchannels can be determined through computational fluid dynamic simulations and through experiment.


Referring again to FIGS. 1-5, the geometries of FIGS. 1-4 are representative of some oscillating designs as described above and FIG. 5 is representative of conventional geometries. For purposes of illustration, thermal and hydraulic performance of the designs of tube 100 (FIG. 1) is analyzed and compared with that of the conventional designs of tube 500 (FIG. 5). As illustrated in FIG. 13, the fluid pressure drops in the design of tube 100 (FIG. 1) is about 4.9 times lower than that of the conventional tube 500 (FIG. 5). Accordingly, the designs of FIG. 1 yields more than double the fluid flow through the channel for the same amount of pump's energy consumption, which thereby increases heat transfer capacity of a heat exchanger by more than two times. As illustrated in FIG. 14, the design of tube 100 (FIG. 1) yield about 17% more heat transfer when compared with the conventional design of tube 500 (FIG. 5). Therefore, the novel corrugated channel designs may have an approximately three-fold advantage over the conventional designs as shown in the example. Such experimental evidence may however vary depending on numerous factors in the experiment including precise dimensions of the various geometries, heat transfer fluid, heat exchanger design, etc. In practical applications, the small size of the holes of the conventional microchannel as illustrated in FIG. 1 makes it susceptible to becoming clogged with impurities in the refrigeration fluid reducing their ability to transfer heat. In contrast, the geometry of tube 100 (FIG. 1) is resistant to clogging due to its larger channel cross sectional area. The example data shown is not seen to be limiting but provided to give a context for potential advantages of the disclosed microchannel designs. Utilizing the designs, as disclosed, may provide any or all of the following benefits when compared with conventional designs: i) less flow resistance that yields less energy consumption for pump and higher energy efficiency of the system, ii) more fluid flow through the channels for the same pump power as conventional one and thereby more heat transfer capacity of a system, and iii) more heat transfer efficiency for the same capacity heat exchanger with less energy consumption for pump.


As illustrated in the FIGS. 1-4 and 6-10, the pattern, size, and number of oscillating cross-sectional geometry channels in a tube may be different, such as sinusoidal wave pattern, triangular wave pattern, square wave pattern, evenly sized and spaced, unevenly sized and spaced and different width of each individual channel without departing from the scope of the disclosure.


Referring now to FIGS. 11 and 12, a heat exchanger 1100, such as that schematically illustrated in FIG. 11, typically includes an inlet manifold 1110, an outlet manifold on the opposite side of the heat exchanger and coupled to the opposite end of the plurality of tubes 1120. Coupled between the rows of tubes 1120 are air-cooled fins 1130. In one implementation heated air which is to be cooled may be forced through the fins 1130 where heat transfer occurs providing heat to be conducted to fins 1130 and tubes 1120 and subsequently to the heat exchanger fluid flowing in conduits 1140 within tubes 1120. The heat transferred to the heat exchanger fluid is carried away and rejected from the heat exchanger fluid, at a different location, before being delivered again to inlet 1110 in a closed loop system. Although the type of heat exchanger illustrated in FIG. 11 is a direct heat exchanger, i.e., air is forced or drawn across fluid containing tubes, the disclosed concepts may be used with other types of heat exchangers known to persons of skill in the art. The disclosed concepts may be applied, for example, to indirect heat exchangers in which cooling tubes are cooled by a liquid coolant, such as water, that is separately cooled by yet another air exchanger. In accordance with exemplary embodiments, the heat exchanger fluid or refrigerant may be any of a variety of fluids including single phase refrigerants and two-phase refrigerants such as but not limited to a high-pressure Carbon Dioxide (CO2) refrigerant.


In some instances, one or more components may be referred to herein as “configured to,” “configured by,” “configurable to,” “operable/operative to,” “adapted/adaptable,” “able to,” “conformable/conformed to,” etc. Those skilled in the art will recognize that such terms (e.g., “configured to”) generally encompass active-state components and/or inactive-state components and/or standby-state components, unless context requires otherwise.


While particular aspects of the present subject matter described herein have been shown and described, it will be apparent to those skilled in the art that, based upon the teachings herein, changes and modifications may be made without departing from the subject matter described herein and its broader aspects and, therefore, the appended claims are to encompass within their scope all such changes and modifications as are within the true spirit and scope of the subject matter described herein. It will be understood by those within the art that, in general, terms used herein, and especially in the appended claims (e.g., bodies of the appended claims) are generally intended as “open” terms (e.g., the term “including” should be interpreted as “including but not limited to,” the term “having” should be interpreted as “having at least,” the term “includes” should be interpreted as “includes but is not limited to,” etc.). It will be further understood by those within the art that if a specific number of an introduced claim recitation is intended, such an intent will be explicitly recited in the claim, and in the absence of such recitation no such intent is present. For example, as an aid to understanding, the following appended claims may contain usage of the introductory phrases “at least one” and “one or more” to introduce claim recitations. However, the use of such phrases should not be construed to imply that the introduction of a claim recitation by the indefinite articles “a” or “an” limits any particular claim containing such introduced claim recitation to claims containing only one such recitation, even when the same claim includes the introductory phrases “one or more” or “at least one” and indefinite articles such as “a” or “an” (e.g., “a” and/or “an” should typically be interpreted to mean “at least one” or “one or more”); the same holds true for the use of definite articles used to introduce claim recitations. In addition, even if a specific number of an introduced claim recitation is explicitly recited, those skilled in the art will recognize that such recitation should typically be interpreted to mean at least the recited number (e.g., the bare recitation of “two recitations,” without other modifiers, typically means at least two recitations, or two or more recitations). Furthermore, in those instances where a convention analogous to “at least one of A, B, and C, etc.” is used, in general such a construction is intended in the sense one having skill in the art would understand the convention (e.g. “a system having at least one of A, B, and C” would include but not be limited to systems that have A alone, B alone, C alone, A and B together, A and C together, B and C together, and/or A, B, and C together, etc.). In those instances where a convention analogous to “at least one of A, B, or C, etc.” is used, in general such a construction is intended in the sense one having skill in the art would understand the convention (e.g., “a system having at least one of A, B, or C” would include but not be limited to systems that have A alone, B alone, C alone, A and B together, A and C together. B and C together, and/or A, B, and C together, etc.). It will be further understood by those within the art that typically a disjunctive word and/or phrase presenting two or more alternative terms, whether in the description, claims, or drawings, should be understood to contemplate the possibilities of including one of the terms, either of the terms, or both terms unless context dictates otherwise. For example, the phrase “A or B” will be typically understood to include the possibilities of “A” or “B” or “A and B.”


With respect to the appended claims, those skilled in the art will appreciate that recited operations therein may generally be performed in any order. Also, although various operational flows are presented in a sequence(s), it should be understood that the various operations may be performed in other orders than those which are illustrated or may be performed concurrently. Examples of such alternate orderings may include overlapping, interleaved, interrupted, reordered, incremental, preparatory, supplemental, simultaneous, reverse, or other variant orderings, unless context dictates otherwise. Furthermore, terms like “responsive to,” “related to,” or other past-tense adjectives are generally not intended to exclude such variants, unless context dictates otherwise.

Claims
  • 1. A heat exchanger tube, comprising: a tube formed substantially of a heat conducting material, the tube being defined by a length, a height, and a width; andat least one conduit formed within the tube and extending the length of the tube, the conduit defining an inlet at one end of the tube and the conduit defining an outlet at the opposite end of the tube, the conduit having a cross-section defined within the height and width of the tube, the cross-section having an oscillating geometry.
  • 2. The heat exchanger tube of claim 1, wherein more than one conduit is formed within the tube, wherein the cross-section of the conduit is formed by more than one identical repeating full pattern, each full pattern comprising a non-straight shape with the conduit width exceeding the conduit height, with an end of one full pattern defining a start of an adjacent full pattern.
  • 3. The heat exchanger tube of claim 2, wherein all of the conduits formed within the tube have substantially the same geometry.
  • 4. The heat exchanger tube of claim 2, wherein at least one of the more than one conduits has a different geometry.
  • 5. The heat exchanger tube of claim 1, wherein the oscillating geometry is representative of at least a portion of a sine wave.
  • 6. The heat exchanger tube of claim 1, wherein the oscillating geometry is representative of at least a portion of a square wave.
  • 7. The heat exchanger tube of claim 1, wherein the oscillating geometry is representative of at least a portion of a triangle wave.
  • 8. The heat exchanger tube of claim 1, wherein the oscillating geometry is representative of at least a portion of more than one different waveform.
  • 9. The heat exchanger tube of claim 1, wherein the oscillating geometry is representative of more than one additive waveforms.
  • 10. A heat exchanger, comprising: more than one tube formed substantially of a heat conducting material, each tube being defined by a length, a height, and a width, each tube having an inlet end and an outlet end;at least one conduit formed within each tube and extending the length of each tube, the conduit defining an inlet at one end of each tube and the conduit defining an outlet at the opposite end of each tube, the conduit having a cross-section defined within the height and width of each tube, the cross-section having an oscillating geometry;an inlet manifold fluidly coupled to each of the inlet ends of the more than one tubes and configured to receive a fluid;an outlet manifold fluidly coupled to each of the outlet ends of the more than one tubes; andheat conducting structures conductively coupled to the more than one tubes.
  • 11. The heat exchanger of claim 10, wherein the heat conducting structures include fins.
  • 12. The heat exchanger of claim 10, wherein the heat conducting structures include tubes.
  • 13. The heat exchanger of claim 10, wherein the heat conducting structures include plates.
  • 14. The heat exchanger of claim 10, wherein the oscillating geometry is representative of at least a portion of a sine wave.
  • 15. The heat exchanger of claim 10, wherein each tube comprising a plurality of conduits placed serially along the width of the tube thereof, wherein each conduit has the cross-section comprising more than one identical repeating full pattern, each full pattern comprising a non-straight shape with the conduit width exceeding the conduit height, with an end of one full pattern defining a start of an adjacent full pattern.
  • 16. The heat exchanger of claim 10, wherein the oscillating geometry is representative of at least a portion of a triangle wave.
  • 17. The heat exchanger of claim 10, wherein the fluid includes a single-phase refrigerant.
  • 18. The heat exchanger of claim 10, wherein the fluid includes a two-phase refrigerant.
  • 19. The heat exchanger of claim 10, wherein there are more than one conduit formed within each tube.
  • 20. The heat exchanger of claim 19, wherein at least one of the more than one conduits has a different geometry.