Fin enhancements for low Reynolds number airflow

Abstract

A heat exchanger including a plurality of parallel fins, and at least one tube passing through the parallel fins, wherein the tube carries a fluid that exchanges heat with air passing through the heat exchanger. The parallel fins each include a plurality of air deflecting members formed therein. Each air deflecting member is bent substantially orthogonally relative to a planar surface of each fin, and each air deflecting member is configured to direct the air passing through the heat exchanger to increase turbulence of the air, and to impinge the air against adjacent parallel fins, and to balance air flow across the heat exchanger and decrease maldistribution of the air flow through the heat exchanger.

Claims

1. A heat exchanger, comprising: a plurality of parallel fins; and at least one tube of a serpentine configuration having a plurality of passes in an airflow path and passing through the parallel fins, the tube carrying a fluid that exchanges heat with air passing through the heat exchanger in the airflow path, wherein the parallel fins each include a plurality of air deflecting members that are tabs stamped therefrom such that each air deflecting member of each individual fin of the plurality of parallel fins is bent in the same direction relative to a planar surface of each fin and an aperture is formed in the fin at a location where a material of a respective parallel fin that forms the air deflecting member was previously located, and each air deflecting member configured to direct the air passing through the heat exchanger; and the air deflecting members of a respective fin are staggered relative to the air deflecting members of immediately adjacent parallel fins that sandwich the respective fin.

2. The heat exchanger according to claim 1, wherein edges of the apertures formed in the respective fin are not arranged in parallel with edges of the respective fin.

3. The heat exchanger according to claim 1, further comprising a fan for drawing or pushing air through the heat exchanger, wherein the tube has a plurality of elongated sections that are connected by a plurality of reverse bend sections, and each air deflecting member is configured to direct the air drawn or pushed through the heat exchanger by the fan.

4. The heat exchanger of claim 3, wherein the air deflecting members are formed between adjacent reverse bend sections of tube.

5. The heat exchanger of claim 3, wherein the air deflecting members are overlapped by the reverse bend sections of tube.

6. The heat exchanger of claim 3, wherein the air deflecting members are formed between adjacent elongated sections of tube.

7. The heat exchanger of claim 1, wherein air flow between adjacent parallel fins travels between the parallel fins in a back and forth manner.

8. The heat exchanger according to claim 1, where at least some of the air deflecting members are twisted.

9. The heat exchanger according to claim 1, wherein a portion of each air deflecting member is removed to provide the air deflecting members with a different shape than that originally formed by stamping.

10. The heat exchanger according to claim 8, wherein at least some of the air deflecting members are helically twisted.

11. The heat exchanger according to claim 2, wherein each aperture includes a first edge, a second edge, a third edge, and a fourth edge, and each of the air deflecting members are connected to a respective aperture at the first edge.

12. The heat exchanger according to claim 2, wherein the air deflecting members are arranged on each of the plurality of fins in a plurality of rows; each aperture includes a first edge, a second edge, a third edge, and a fourth edge; the air deflecting members of a first row of the plurality of rows are each connected to a respective aperture at the first edge; and the air deflecting members of a second row of the plurality of rows are each connected to a respective aperture at the second edge.

13. The heat exchanger according to claim 2, wherein each aperture includes a first edge, a second edge, a third edge, and a fourth edge; and an edge at which the air deflecting member is connected to a respective aperture is randomly selected from one of the first edge, the second edge, the third edge, and the fourth edge.

Description

DRAWINGS

(1) The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.

(2) FIG. 1 is a front-perspective view of a conventional heat exchanger;

(3) FIG. 2 is a side-perspective view of a conventional heat exchanger;

(4) FIG. 3 is a front-perspective view of an example heat exchanger according to a principle of the present disclosure;

(5) FIG. 4 is a front-perspective view of an example heat exchanger according to a principle of the present disclosure;

(6) FIG. 5 is a perspective view of a fin of a heat exchanger including a plurality of air deflecting members having alternating orientations;

(7) FIG. 6 is a perspective view of a fin of a heat exchanger including a plurality of rows of air deflecting members wherein the air deflecting members of one row are oriented in a first direction and the air deflecting members of another row are oriented in second and opposite direction;

(8) FIG. 7 is a perspective view of a fin of a heat exchanger including a plurality of openings that form a plurality of air deflecting members, wherein the edges of the openings are not arranged in parallel with the edges of the fin;

(9) FIG. 8 illustrates an air defecting member that is twisted;

(10) FIG. 9 illustrates an air deflecting member that includes portions that have been removed to provide the air deflecting member with a shape that is different from that originally stamped from the fin;

(11) FIG. 10 is a side-perspective view of an example heat exchanger according to a principle of the present disclosure;

(12) FIG. 11 is a front-perspective view of another example heat exchanger according to a principle of the present disclosure;

(13) FIG. 12 is a front-perspective view of another example heat exchanger according to a principle of the present disclosure;

(14) FIG. 13 graphically illustrates the amount of heat transfer improvement achieved by the example heat exchanger illustrated in FIGS. 3 and 9 in comparison to that achieved by conventional systems that use louvers or a vortex generator; and

(15) FIG. 14 graphically illustrates the impact on airside pressure drop achieved by the example heat exchanger illustrated in FIGS. 3 and 4 in comparison to that achieved by conventional systems that use louvers or a vortex generator.

(16) Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.

DETAILED DESCRIPTION

(17) Example embodiments will now be described more fully with reference to the accompanying drawings.

(18) Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.

(19) Referring to FIG. 3, a heat exchanger or evaporator system 50 is schematically illustrated. Evaporator system 50 includes a tube 52 having both inlet 54 and an outlet 56 ends. Tube 52 is formed in a serpentine configuration including a plurality of elongate sections 58 that are separated by a plurality of reverse bends or hairpin 60. Elongate sections 58 and hairpins 60 may be unitary to form a continuous tube 52, or elongate sections 58 may be formed separately from hairpins 60 and subsequently brazed, welded, or mechanically fastened together. Preferably, elongate sections 58 are fed through openings in a plurality of fins 62, and then hairpins 60 are brazed to ends of the elongate sections to form a continuous tube 52. Regardless, tube 52 may be formed of any material such as copper, aluminum, stainless steel, titanium, or some other metal or alloy material that provides sufficient heat exchange with the surround air.

(20) Fins 62 are metal plates formed of a material similar to or the same as tube 52. In this regard, fins 62 may be formed of materials such as copper, aluminum, stainless steel, or some other type of metal or alloy material that may be brazed, welded, or mechanically fastened to tube 52. Preferably, for cost purposes, fins 62 are formed of a material such as aluminum. To allow elongate sections 58 of tube 52 to pass through fins 62, fins 62 may include openings 64. As best shown in FIG. 3, fins 62 each include a varying profile capable of dramatically enhancing the mixing of the air flow passing through evaporator system 50 and further capable of enhancing the impingement effect of air contacting each fin 62. In this manner, the maldistribution of air flow through the heat exchanger 50 is corrected to balance air flow through the heat exchanger 50. To assist in the flow of air passing through evaporator system 50, a fan 63 may be used. Notwithstanding the use of fan 63, however, it can be seen in FIG. 3 that the air flow through heat exchanger 50 has been balanced along the entire coil width of the heat exchanger 50 by air deflecting members 66 in comparison to the configuration illustrated in FIG. 1 where the uneven airflow is illustrated. That is, by directing air flow using air deflecting members 66, the flow of air through heat exchanger 50 can be directed from a center of tube 52 where fan 63 is located in a direction outward (i.e., toward opposing ends of elongated sections 58) from fan 63.

(21) More specifically, fins 62 may each be stamped to form openings 64 for elongate sections 58 of tube 52, and to form a plurality of air deflecting members or tabs 66 and apertures 65 where the material that forms air deflecting tabs 66 was previously located. Accordingly, fins 62 include a first surface 68 and an opposite second surface 70. Air deflecting tabs 66 are punched through fins 62 and bent relative to first and second surfaces 68 and 70 to a position that is substantially orthogonal to first and second surfaces 68 and 70. It should be understood, however, that air deflecting tabs 66 may be bent at any angle relative to first and second surfaces 68 and 70 that is desirable for directing air flow through evaporator system 50 in the desired manner. Regardless, as the number and placement of the air deflecting tabs 66 can be specifically tailored for each evaporator system 50 the uneven air flow illustrated in FIG. 1 of the application can be effectively eliminated, or at least substantially minimized. Further, the use of air deflecting tabs 66 only slightly increases the possibility of a pressure drop on the air side of the system 50.

(22) As shown in FIGS. 3 to 6, air deflecting tabs 66 are substantially rectangular or square members 66 that may be bent in a direction from first surface 68 toward second surface 70, or bent in a direction from second surface 70 toward first surface 68. Preferably, each air deflecting tab 66 of a respective fin 62 may be bent in the same direction for ease of manufacturing (FIGS. 3 and 4). It should be understood, however, that individual air deflecting tabs 66 of each fin 62 can be bent in different directions. For example, as best shown in FIG. 5, adjacent air deflecting tabs 66 may be alternately bent in different directions. That is, some air deflecting tabs 66 of a single fin 62 are bent in a direction outward from first surface 68 and some air deflecting tabs 66 are bent in a direction outward from second surface 70. Alternatively, as shown in FIG. 6, each air deflecting tab 66 in a single row 69 are bent in the same direction (i.e.; in a direction outward from second surface 70) while each air deflecting tab 66 in another single row 71 are bent in the same and opposite direction (i.e., in a direction outward from first surface 68).

(23) It should also be understood that air deflecting tabs may be any shape known to one skilled in the art. For example, rounded or triangular-shaped air deflecting tabs 66 are contemplated. In addition, even if square or rectangular air deflecting tabs 66 are utilized, it should be understood that edges 72 of the apertures 65 are not necessarily required to be parallel with edges 74 of fin 62. Indeed, as can best be seen in FIG. 7, it can be seen that edges 72 of apertures 65 formed in fin 62 are rotated about forty-five degrees relative to edges 74 of fin 62. Although apertures 65 are illustrated as being rotate forty-five degrees relative to edges 74 of fin 62, it should be understood that apertures 65 can be rotated at any angle desired that results in edges 72 of apertures 65 being non-parallel with edges 74 of fin 62.

(24) Moreover, when apertures 65 are rotated such that edges 72 of apertures 65 are no longer parallel with edges 74 of fin 62, it should be understood that air deflecting tabs 66 (not shown) that are formed as a result of forming apertures 65 in fin 62 will also be angled. Thus, the directions at which the air moves through heat exchanger 50 can further be tailored such that any maldistribution of the air flow caused by fan 63 through heat exchanger 50 can be eliminated, or at least substantially minimized.

(25) In addition, air deflecting tabs 66 can be formed by bending the material of the fin 62 along any of the different edges 72a, 72b, 72c, or 72d of apertures 65, as desired. For example, each of the air deflecting tabs 66 can be bent along the same edge (e.g., 72a) or each of the air deflecting tags 66 located in a single row 69 can be bent along the same edge (e.g., 72a), while each of the air deflecting tabs 66 located in another single row 71 are bent along the same and different edge (e.g., 72c). Alternatively, the edge 72 at which the air deflecting tabs 66 are bent can be randomly selected. Regardless, it should be understood that one skilled in the art can pre-select the edge 72 of each aperture 65 from which air deflecting tabs 66 will be bent to further tailor the directions at which air is directed through heat exchanger 50 to optimize the air flow and decrease maldistribution of the air flow case by fan 63.

(26) Further, it should be understood that air deflecting tabs 66 may be initially formed as having one shape (i.e., when initially stamped), and then modified to have a different shape using subsequent processing steps without departing from the scope of the present disclosure. For example, air deflecting tabs 66 may be slightly twisted in a helical or spiral manner to further assist in directing air flow between adjacent fins 62 (FIG. 8), or portions 67 of individual tabs 66 may be removed to provide tabs 66 with a different shape than that originally formed by stamping (FIG. 9), Although the portions 67 removed from air deflecting tab 66 are corners of the tab 66, it should be understood that other portions of the air deflecting tab 66 can be removed (e.g., from the center of tab 66) without departing from the scope of the present disclosure.

(27) A size of the air deflecting tabs 66 is variable, and may be selected based on a number of different factors including the size of the heat exchanger, a spacing between fins 62, a size of fan 63, and the like. In this regard, air deflecting tabs may have a surface area that ranges between 4 mm.sup.2 (e.g., 2 mm×2 mm) to 196 mm.sup.2 (e.g., 14 mm×14 mm). A preferred surface area of air deflecting tabs 66 is 24 mm.sup.2 (6 mm×4 mm), which provides good heat transfer improvement for evaporator system 50, and is easily manufactured.

(28) As air is drawn through fins 62 of evaporator system 50 by fan 63, the air deflecting tabs 66 direct the air in a back and forth manner to create a turbulent flow between adjacent fins 62. This effect is particularly advantageous at wider coil widths. The phrase “coil width” refers to a length of elongate sections 58 of tube 52, as shown in FIG. 3. At greater coil widths, a greater amount of air can be moved by tabs 66 to further increase heat exchange between evaporator system 50 and the air. Thus, as air is drawn through evaporator system 50 the air impinges the cooling fins 62 to increase the cooling effect and efficiency of evaporator system 50. Further, because air deflecting tabs 66 may be formed in the same manufacturing step as forming openings 64, the cost to manufacture fins 62 having air deflecting tabs 66 is reduced.

(29) As best shown in FIG. 10, the air deflecting tabs 66 can be located between respective hairpins 60, behind the hairpins 60, or both. Further, air deflecting tabs 66 formed in different fins 62 can be offset, as shown by the air defecting tabs 66 illustrated in phantom. As shown in FIG. 3, half of the air deflecting tabs 66 can be oriented in one direction, and the remaining half of the air deflecting tabs 66 can be oriented in the opposite direction. In FIG. 3, the air deflecting tabs 66 are oriented in a direction toward the fan 63. It should be understood, however, that the air deflecting tabs 66 on each fin 62 can each be oriented in the same direction (FIG. 4), the air deflecting tabs 66 on each fin 62 can be oriented in a direction away from fan 63 (FIG. 10), or in a manner like FIG. 4 (FIG. 11). Alternatively, air deflecting tabs 66 located near inlet 54 can be oriented in one direction (i.e., to the left in the figure), and air deflecting tabs 66 located near the outlet 56 can be oriented in the opposite direction (i.e., to the right in the figure). Another alternative is to have air deflecting tabs to the left and right of fan 63 be oriented in one direction, while tabs 66 located on fins 62 directly beneath fan 63 are oriented in an opposite direction. It should be understood that any number of combinations of orienting the air defecting tabs 66 can be selected such that specific applications can have specifically tailored configurations for the air defecting tabs 66 to maximize and balance the air flow through heat exchanger 50. In any event, the air defecting tabs 66 reduce the flow area between fins 62, which increases air velocity between fins 62 and around the elongate sections 58 of tube 52 to increase heat transfer between the fluid in tube 52 and the air.

(30) With such a configuration, the Reynolds number of the evaporator system 50 is reduced. While intuitively that would reduce heat transfer, the heat transfer coefficient is function of both Reynolds number and hydraulic diameter:
NuαRe=.sup.˜0.5(ρVD.sub.h/μ).sup.˜0.5  (2)

(31) Where Nu is the Nusselt number, and Nu=h D.sub.h/k (where k is the thermal conductivity and h is the heat transfer coefficient). After substituting and reducing:
hα(ρVD.sub.h/μ).sup.˜0.5K/D.sub.h=(ρV/(D.sub.hμ).sup.˜0.5K  (3).

(32) So, while the Nusselt number does reduce with reduced hydraulic diameter it is only by approximately a half power. Meanwhile, the heat transfer coefficient is proportional to a full inverted power of hydraulic diameter. Hence, reducing hydraulic diameter increases heat transfer coefficient.

Example

(33) A complete evaporator system 50 was tested and the improvement in heat transfer measured. FIG. 13 shows the amount of heat transfer improvement relative to Reynolds Number, and shows the amount of heat transfer improvement when using conventional fin enhancements such as the use of louvers and vortex generators. As can be seen in FIG. 13, the amount of improvement of heat transfer achieved by the use of the air deflecting tabs 66 is better at lower Reynolds Numbers than that achieved using conventional fin enhancements such as louvers and vortex generators.

(34) FIG. 14 illustrates the impact on airside pressure drop that occurs when using air deflecting tabs 66 according to the present disclosure, conventional louvers, and conventional vortex generators. As can be seen in FIG. 14, the use of deflecting tabs 66 is not detrimental to airside pressure drop in comparison to use of conventional louvers, and the amount of airside pressure drop that occurs using air deflecting tabs 66 is similar to that achieved by a conventional vortex generator. Although tabs 66 results in minimal airside pressure drop like the use of a vortex generator, it should be noted that the amount of heat transfer achieved by air defecting tabs 66 is substantially better than that achieved by a vortex generator as shown in FIG. 13.

(35) The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.