This invention relates to a heat exchanger device comprising corrugated micro tubes.
Heat exchangers transfer energy from one fluid to another. Heat exchangers are typically characterized by heat transfer rates and corresponding pressure drops of the fluid(s) across the heat exchanger. In many cases though, volume constraints are provided and, in these cases, heat exchanger performance may be characterized by heat transfer/flow area and corresponding pressure drops. For example, in the case of a liquid-gas heat exchanger, a typical design challenge is to minimize the face area associated with the gas side duct, while simultaneously meeting given specifications relating to allowable pressure drop of the gas across the heat exchanger, and, of course, heat transfer requirements.
Heat exchangers typically consist of cores and headers. The cores provide two sets of intertwining fluid passages that allow good thermal coupling between the two fluids without actual mixing of the fluids. Upon entering the volume occupied by the intertwining fluid passages, the fluid velocity typically increases because the hardware within the core that defines the two sets of fluid channels and promotes heat transfer between the two fluids necessarily occupies volume and restricts the area available for flow of both fluids.
Pressure drop across the core is a function of the drag associated with the shape of the “heat exchanger hardware” (i. e. tubes, fins, rectangular channels, etc.), the total distance of flow through this hardware, and the specific kinetic energy of the fluid (pV2). Good heat exchanger design is essentially a search for an optimum geometry which provides an excellent ratio of heat transfer/pressure drop within given envelope restraints. A need exists for heat exchangers with small flow areas (small duct size) that provide specified rates of heat transfer and specified low pressure drop.
The present invention provides an efficient, simple, and cost-effective device and/or methodology to provide high heat transfer/pressure drop ratios that are needed by heat exchanger end users.
The present invention addresses a means to simultaneously achieve high heat transfer/unit duct area and low pressure drop by the use of a corrugated or serpentine field of closely packed micro tubes. The width of the corrugated field is much less than the total length of the serpentine. The serpentine provides effectively a frontal area much larger than the duct area for one fluid to pass through the heat exchanger. Because the area is larger, the velocity of the fluid passing over the serpentine tube bank is reduced compared to cases involving the same flow rate, same duct size, but no corrugation. The lower fluid velocity combined with the short flow length (equal to the width of the serpentine) results in low pressure drop of the fluid passing over the outside of the tube bank.
As noted above, the present invention comprises tightly packed micro tubes. Micro channel heat exchangers, in general, provide high heat transfer rates/volume compared to heat exchangers with larger, more conventional scale, heat exchange passageways. Heat transfer/unit area is a function of the product hA, where h is the convection coefficient and A is the area available for heat transfer. Because both h and A increase as the characteristic passageway dimension (width or diameter) decreases, the product of hA/unit volume for micro channel heat exchangers is much greater than heat exchangers with larger scale. Because micro channel heat exchangers need less volume to achieve a given rate of heat exchange, it becomes geometrically feasible to “reshape” this reduced volume into a thin, serpentine shape that affords advantages with respect to reducing pressure drop. The advantages associated with the serpentine shape simply disappear as the characteristic dimensions of the heat exchanger hardware are increased.
It should further be noted that fields of tightly packed micro tubes offer another advantage with respect to corrugated or serpentine hardware that dictate a specific flow direction (such as normal to the local tangent along the serpentine). As the depth of each crease of a serpentine increases for a given crease width, the need for the flow direction through the heat exchanger hardware to be nonspecific becomes more important. Heat exchangers that use a tube bank, which allow flow in any direction, tend to offer substantial advantages in corrugated arrangements over flow passage geometries that do not.
One particular embodiment of the present invention comprises a plurality of substantially parallel tubes, each tube having an outer diameter which is less than or equal to one millimeter. Each parallel tube comprises a first end portion and a second end portion. The device further comprises a first manifold forming an inlet for the first fluid, the first manifold further forming a plurality of first openings, each of the first end portions of the parallel tubes being in sealing relation to the first manifold so that each tube is in fluid communication with a respective one of the first openings. In addition, the device comprises a second manifold spaced from and opposing the first manifold, the second manifold forming an outlet for the first fluid. The second manifold further forms a plurality of second openings, each of the second end portions of the parallel tubes being in sealing relation to the second manifold so that each tube is in fluid communication with a respective one of the second openings. The plurality of substantially parallel tubes are laterally disposed relative to one another so that they form at least one corrugated pattern when viewed in an imaginary plane which intersects and is perpendicular to the longitudinal axes of the tubes, the corrugated pattern having a thickness. The device is adapted so that the first fluid exchanges heat with the second fluid as the first fluid passes through the parallel tubes and the second fluid passes between the first and second manifolds and between but outside of the parallel tubes in a direction of flow which is generally perpendicular to the direction of flow of the first fluid through the tubes.
Another embodiment of the present invention is a method of exchanging heat between a first fluid and a second fluid. The method comprises providing a housing which defines a passageway through which the second fluid may flow and across which extends a plurality of substantially parallel tubes arranged in a corrugated pattern, when viewed along their longitudinal axes, and spaced apart from one another so that the plurality of tubes is substantially porous from any fluid flow direction nonparallel to the longitudinal axis of the tubes. The method further comprises. feeding the first fluid through the tubes and feeding the second fluid between and through the corrugated bank of parallel tubes, so that heat is transferred between the first fluid and the second fluid. In certain embodiments, the housing comprises a first manifold and second manifold, wherein the parallel tubes are sealingly attached to the first manifold and second manifold.
These and other features of this invention will be still further apparent from the ensuing description, drawings, and appended claims.
Like reference numbers or letters are used in the figures to reference like parts or components amongst the several figures.
The present invention enables the exchange of energy from one fluid to another in a heat exchanger without a significant reduction in pressure across the core while offering high heat transfer to weight ratio and reduced volume of the core. It does so by employing a device and/or methodology which is cost-effective and offers a relative ease of manufacture.
Referring now descriptively to the drawings, the attached figures illustrate one particular embodiment of the invention, in which a heat exchanger device 10 comprises corrugated micro tubes 12. As seen in
First manifold 18 forms an inlet (not shown) for the first fluid A. First manifold 18 further forms a plurality of first openings 20 (See
The plurality of substantially parallel tubes 12 are laterally disposed relative to one another so that they form at least one corrugated pattern 26 when viewed in an imaginary plane which intersects and is perpendicular to the longitudinal axes of the tubes 12. The corrugated pattern 26 has a thickness T (See
Turning now to
The corrugated heat exchanger can be compared to a similar tube-based solid block heat exchanger 34 where the entire volume L1×H×W is occupied by a field of tubes 36 as shown in
In at least some embodiments of the invention, the corrugated pattern may be further defined by a grouping of segments. As shown in
Looking now at
As shown in
Looking now at
In at least one particular embodiment, as illustrated in
Each of the first end portions of the parallel tubes is in sealing relation to the first manifold so that each tube is in fluid communication with a respective one of the first openings. Similarly, each of the second end portions of the parallel tubes is in sealing relation to the second manifold so that each tube is in fluid communication with a respective one of the second openings. The sealing relation between the tube end portions and their respective manifolds may be formed by welding, gluing, braising, or the like between the end portion of the tube and its respective opening in the first or second manifold, as the case may be.
As noted earlier, in some embodiments of the invention, one or more support plates may be disposed between the first and second manifold. Support plate openings may vary in size from the first and second openings. The plurality of substantially parallel tubes may be attached to the support plate openings by gluing, welding, braising, or the like. The plurality of substantially parallel tubes also may be inserted through the support plate openings without being fixably attached to the support plates. The methodology employed to attach the plurality of substantially parallel tubes to the support plates, if any, may vary depending on, for example, the number of support plates disposed between the first manifold and second manifold.
Manifolds and mid plates typically will be made of one or more lamina of thin sheets, for example either metal or polymer, each having the desired opening pattern. These lamina typically are made via lithographic etching, or stamping, and either process can produce the required lamina from a variety of metal alloys including steel, nickel alloy, aluminum, titanium, or from a polymer. Micro tubes typically may also be made from polymer or metal alloys. Such metal alloys may include, e.g., steel, nickel alloy, aluminum, or titanium. The manifold, midplates, and micro tubes of the heat exchanger device can be made from the same material or, for example, the device may comprise manifolds and midplates made out of one material and micro tubes made from a different material. The material used in making the heat exchanger may be selected based on performance standards or physical requirements. For example, the heat exchanger may be composed of stainless steel in high temperature operations or environments requiring high tensile strength. Aluminum may be chosen as a suitable material in order to decrease the weight of the heat exchanger. Such examples are nonlimiting and it should be apparent that one of ordinary skill in the art may choose the heat exchanger materials for a desired result based on the applicable factors.
Except as may be expressly otherwise indicated, the article “a” or “an” if and as used herein is not intended to limit, and should not be construed as limiting, the description or a claim to a single element to which the article refers. Rather, the article “a” or “an” if and as used herein is intended to cover one or more such elements, unless the text expressly indicates otherwise.
This invention is susceptible to considerable variation within the spirit and scope of the appended claims.
This application claims the benefit of U.S. Provisional Application No. 61/019,911, filed Jan. 9, 2008, the disclosure of which is incorporated herein by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2009/030614 | 1/9/2009 | WO | 00 | 12/8/2009 |
Number | Date | Country | |
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61019911 | Jan 2008 | US |