HEAT EXCHANGER WITH TURBULATING INSERTS

Abstract

A heat exchanger has a turbulating insert arranged between a pair of plates. The turbulating insert is permeable to fluid flow in both a high-pressure-drop direction and a low-pressure drop direction. One portion of the turbulating insert has the high-pressure-drop direction oriented at a non-zero angle to the high-pressure-drop direction of another portion. A method of making the heat exchanger includes forming a turbulating insert, removing a portion of the turbulating insert to create a cavity within the turbulating insert, placing the remaining turbulating insert into a stamped first plate, and placing the removed portion of the turbulating insert into the cavity at a non-zero angle of rotation relative to the remaining turbulating insert.

Claims

1. A heat exchanger comprising: a pair of plates configured to direct a first fluid through a fluid volume between the pair of plates and a second fluid over outer surfaces of the pair of plates; a first turbulating insert arranged in the fluid volume, the first turbulating insert being permeable to fluid flow in a high-pressure-drop direction and in a low-pressure-drop direction, the low-pressure-drop direction of the first turbulating insert being oriented perpendicular to the high-pressure-drop direction of the first turbulating insert; and a second turbulating insert arranged in the fluid volume, the second turbulating insert being permeable to fluid flow in a high-pressure-drop direction and in a low-pressure-drop direction, the low-pressure-drop direction of the second turbulating insert being oriented perpendicular to the high-pressure-drop direction of the second turbulating insert, wherein the low-pressure-drop direction of the second turbulating inserts is arranged at a non-zero angle to the low-pressure drop direction of the first turbulating insert.

2. The heat exchanger of claim 1, wherein the low-pressure-drop direction of the second turbulating insert is aligned with the high-pressure-drop direction of the first turbulating insert.

3. The heat exchanger of claim 1, wherein the second turbulating insert is arranged within a cavity of the first turbulating insert.

4. The heat exchanger of claim 3, further comprising a third turbulating insert arranged within another cavity of the first turbulating insert.

5. The heat exchanger of claim 3, wherein the second turbulating insert exhibits rotational symmetry.

6. The heat exchanger of claim 5, wherein the second turbulating insert is square in shape.

7. The heat exchanger of claim 1, further comprising an inlet manifold for the first fluid and an outlet manifold for the first fluid extending through the pair of plates, the inlet manifold and the outlet manifold being fluidly connected by the fluid volume, the first turbulating insert including an aperture through which the inlet manifold or the outlet manifold extends.

8. The heat exchanger of claim 7, wherein the aperture is a first aperture through which the inlet manifold extends, the first turbulating insert further including a second aperture through which the outlet manifold extends.

9. The heat exchanger of claim 7, wherein the heat exchanger has a longitudinal direction and the inlet manifold and outlet manifold are arranged along a line that extends parallel to the longitudinal direction.

10. The heat exchanger of claim 9, wherein the low-pressure-drop direction of the first turbulating insert is aligned with the longitudinal direction.

11. The heat exchanger of claim 9, wherein the high-pressure-drop direction of the first turbulating insert is aligned with the longitudinal direction.

12. A method of making a heat exchanger, comprising: forming a turbulating insert; removing a portion of the turbulating insert to create an aperture within the remaining turbulating insert; placing the remaining turbulating insert into a stamped first plate; placing the removed portion of the turbulating insert into the aperture of the remaining turbulating insert; and joining a stamped second plate to the stamped first plate to enclose the turbulating insert within a fluid volume created between the stamped first plate and the stamped second plate.

13. The method of claim 12, wherein the removed portion of the turbulating insert is placed into the aperture at a non-zero angle of rotation relative to the remaining turbulating insert.

14. The method of claim 13, wherein the non-zero angle is ninety degrees.

15. The method of claim 12, wherein the removed portion of the turbulating insert exhibits rotational symmetry.

16. The method of claim 15, wherein the removed portion of the turbulating insert has a square shape.

17. The method of claim 12, further comprising: forming a locating hole into the removed portion of the turbulating insert; and using the locating hole to orient the removed portion of the turbulating insert within the aperture at a non-zero angle of rotation relative to the remaining turbulating insert.

18. The method of claim 17, wherein using the locating hole to orient the removed portion of the turbulating insert within the aperture includes receiving a projection formed into the stamped first plate into the locating hole.

19. The method of claim 12, wherein joining a stamped second plate to the stamped first plate includes either overlapping an outer perimeter of the first plate with an outer perimeter of the second plate or nesting outer perimeter of the second plate within the outer perimeter of the first plate.

20. The method of claim 12, wherein forming the turbulating insert includes lancing and offsetting a metal sheet at regular intervals and rolling the metal sheet to create corrugations.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0017] FIG. 1 is a perspective view of a heat exchanger according to an embodiment of the invention.

[0018] FIG. 2 is a side view of the heat exchanger of FIG. 1.

[0019] FIG. 3 is a detail view of the portion of FIG. 2.

[0020] FIG. 4 is a sectioned detail view of a heat exchanger showing an alternative embodiment of the invention.

[0021] FIG. 5 is a plan view of a turbulating insert for use in the heat exchanger of FIG. 1.

[0022] FIG. 6 is a partial perspective view of a style of insert that can be particularly useful as the turbulating insert of FIG. 5.

[0023] FIG. 7 is a plan view showing additional details of the turbulating insert of FIG. 5.

[0024] FIG. 8 is a plan view showing alternative additional details of the turbulating insert of FIG. 5.

[0025] FIG. 9 is a plan view showing other alternative additional details of the turbulating insert of FIG. 5.

[0026] FIGS. 10A-C are a series of plan views showing several steps in the construction of the turbulating insert of FIG. 5 according to an embodiment of the invention.

[0027] FIGS. 11A-C are a series of plan views showing several steps in the construction of the turbulating insert of FIG. 5 according to another embodiment of the invention.

DETAILED DESCRIPTION

[0028] Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the accompanying drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of including, comprising, or having and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms mounted, connected, and coupled and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, connected and coupled are not restricted to physical or mechanical connections or couplings.

[0029] A heat exchanger 1 is constructed as a stack formed from stamped plates 2 arranged in pairs. An inlet manifold 7 and an outlet manifold 8 each extend through the stack. A flow of fluid to be heated or cooled within the heat exchanger 1 is directed into the heat exchanger 1 by way of the inlet manifold 7, and is directed to flow through fluid volumes arranged within the plate pairs. After having been heated or cooled, the flow of fluid is removed from the heat exchanger 1 by way of the outlet manifold 8. The inlet manifold 7 and the outlet manifold 8 are arranged at opposing ends of the heat exchanger 1 along a longitudinal direction 10 of the heat exchanger 1.

[0030] As shown in detail in FIG. 3, each of the plate pairs is defined by a stamped plate 2a and a stamped plate 2b that are assembled together to create a fluid volume 3 within the plate pair through which the fluid to be heated or cooled can flow from the inlet manifold 7 to the outlet manifold 8. The plates 2a, 2b have formed outer flanges that cooperate with one another to seal the fluid volume 3 within the plate pair. The outer flange of the plate 2a surrounds and receives the outer flange of the plate 2b to create the sealed fluid volume 3.

[0031] The plates 2 are provided with dimples 12 formed therein to space apart adjacent ones of the plate pairs, so that gaps are provided therebetween to allow for the flow of another fluid over outer surfaces of the plates 2. In this manner the heat exchanger 1 can function to transfer heat between a first fluid that flow through the plate pairs and a second fluid that flows over the outer surfaces of the plate pairs. The heat exchanger 1 can, for example, be mounted within a housing through which the second fluid flows.

[0032] As one non-limiting example, the heat exchanger 1 can be an engine oil cooler. In such an application, engine oil can be circulated through the plate pairs of the heat exchanger 1 as the first fluid, and a flow of coolant can be directed through a housing within which the heat exchanger 1 is mounted in order to cool the engine oil.

[0033] FIG. 4 depicts a construction detail of a heat exchanger 1 having an alternative construction. Similar to the heat exchanger 1, the heat exchanger 1 is constructed as a stack of stamped metal plates. The metal plates of the heat exchanger 1 are arranged as stack of nested shells, so that both the first fluid and the second fluid are enclosed by plates arranged in pairs. Plates 2a and 2b are arranged in alternating sequence, so that the first fluid flows within a fluid volume 3 formed by a pair of plates, each such pair of plates defined by a plate 2a and a plate 2b nested therein. The next plate 2a is likewise nested within that plate 2b to form a plate pair for the second fluid, and so on throughout the stack, so that flow passages for the first and second fluids are alternatingly arranged within the stack in a similar fashion as was the case for the heat exchanger 1. Dimples 12 extending outwardly (i.e. away from the fluid volume 3) from the plates 2a, 2b are also provided.

[0034] A turbulating flow insert 4 (shown generally in FIG. 5) is arranged within each of the fluid volumes 30. The turbulating insert 4 can be provided as multiple pieces, as will be described in greater detail. Generally speaking, the turbulating insert 4 functions to provide both structural support and flow turbulation for the fluid passing through the fluid volume 3. The outer profile of the turbulating insert 4 is shaped to conform to the shape of the stamped plate 2 into which it is to be inserted, so that generally the entire fluid volume 3 is filled with the turbulating insert 4. By way of example, the outer profile can be cut, punched, or otherwise formed in the turbulating flow insert after first producing the turbulating flow insert as a larger piece. Apertures 9 are additionally cut, punched, or otherwise formed into the turbulating insert 4, so that the fluid manifolds 7, 8 can extend through the plate pairs in order to fluidly communicate with the fluid volumes 3.

[0035] In the construction of the heat exchanger 1 or 1, a turbulating insert 4 is placed into a plate 2b or 2b, and a plate 2a or 2a is subsequently assembled to the plate 2b or 2b to form the completed plate pair. This can be repeated as necessary to form the multiple plate pairs of the heat exchanger stack, after which the completed stack is joined by brazing.

[0036] An exemplary style of a turbulating insert 4 is depicted in FIG. 6. The turbulating insert 4 as shown in FIG. 6 is of a lanced and offset type, and is constructed by rolling or stamping a continuously fed sheet of thin metal material. Lances are formed into the material and the resulting strands of material are offset from the plane of the material in successively opposing directions to form openings 13 through which the fluid can pass. Corrugations 14 are subsequently formed into the material at a height that corresponds to the height of the fluid volume 3, so that crests and troughs of the corrugations 14 can be joined to the stamped plates 2.

[0037] As a result of the forming operations, the insert 4 is permeable to fluid flow in two orthogonal directions, indicated in FIG. 6 by the arrows 21 and 22. The direction indicated as 22, extending along the lengths of the corrugations 14, will be much less resistant to fluid flow than the direction indicated as 21, since fluid flowing in the direction 21 will need to flow perpendicular to the corrugations 14 through the openings 13 that are formed by the lances. The direction 22 is therefore generally referred to as the high-pressure-drop direction of flow, and the direction 21 is generally referred to as the low-pressure-drop direction of flow.

[0038] As shown in FIG. 7, the insert 4 can be constructed of multiple pieces. The exemplary insert 4 of FIG. 7 is constructed of three separate pieces, labeled 4a, 4b, and 4c. The piece 4b is arranged between the pieces 4a and 4c along the longitudinal direction, and the apertures 9 are provided within the outer pieces 4a and 4c so that fluid flowing through the turbulating insert 4 from the inlet manifold 7 to the outlet manifold 8 will necessarily pass through all three pieces.

[0039] The flow turbulation features of the turbulating insert are not depicted in detail in FIGS. 7-11, but lines corresponding to the corrugations 14 are used to generally depict the low-pressure-drop direction. Thus, a fluid flowing through the turbulating inserts from one of the apertures 9 to the other of the apertures 9 will first flow through one of the inserts 4a, 4c in a direction that is generally aligned with the low-pressure-drop direction of that insert piece, then through the insert 4b in a direction that is aligned with the high-pressure-drop direction of that insert piece, and then finally through the other of the inserts 4a, 4c, again in a direction that is generally aligned with the low-pressure-drop direction of that insert piece.

[0040] One advantage of the turbulating insert as embodied in FIG. 7 is that both the uniformity of flow distribution along the width of the fluid volume 3 (i.e. in the direction that is perpendicular to the longitudinal direction 10) and the rate of heat transfer within the central portion of the plate pair can be enhanced without imposing the undesirable large pressure drop that would result from the entirety of the turbulating insert having its high-pressure-drop direction aligned with the longitudinal direction.

[0041] The design of FIG. 7 allows for the use of differing geometries of the detailed turbulating inserts features for the three pieces. For example, the pitch and width of the corrugations or the strand width of the offset features can be different for the piece 4b than it is for the pieces 4a and 4c, thereby allowing the heat exchanger designer to optimize the balance between heat transfer and pressure drop to be most desirable. Such a variation between the insert details can provide disadvantages as well, however, in that it complicates the manufacturing of the heat exchanger 1 by requiring additional machine setup and operation for the different insert geometries.

[0042] In light of the foregoing, it can be especially advantageous to produce the turbulating insert as a single piece, then removing a portion of that piece and reinserting it with the low-pressure-drop direction oriented at an angle to its original orientation. FIG. 8 depicts an embodiment of the turbulating insert with a two-part turbulating insert having a first piece 4d and a second piece 4e, with the piece 4e arranged within the piece 4d. As again indicated by the lines within each of the pieces, the low-pressure-drop direction of the piece 4e is oriented to be perpendicular to the low-pressure-drop direction of the piece 4d, so that the high-pressure-drop direction of the piece 4e is aligned with the low-pressure-drop direction 4d in the longitudinal direction.

[0043] The piece 4e is advantageously shaped as a square, so that it has rotational symmetry. This allows for the turbulating insert to be first manufactured as a single part. A portion of the manufacturing sequence for the turbulating insert of FIG. 8 is depicted in FIGS. 10A-C. After having first produced the turbulating insert as a sheet (for example, as depicted in FIG. 6), the outer profile of the turbulating insert and the apertures 9 are formed into the sheet by, for example, a punching operation. In the same or a subsequent operation, the piece 4e can be punched out of the turbulating insert, leaving the piece 4d with a cavity 6 the same size as the piece 4e. The piece 4d is recovered and is rotated by the angle of rotational symmetry (in this case, ninety degrees) or a multiple thereof, and is subsequently re-inserted into the cavity 6 to form the completed turbulating insert, with essentially no gaps between the insert pieces.

[0044] FIG. 9 depicts an alternative embodiment with a different angle of rotational symmetry. In that embodiment, a hexagonally shaped turbulating insert piece 4g is inserted into the hexagonally shaped cavity of a turbulating insert piece 4f at a sixty degree angle of rotation. It should be understood that the embodiments of FIG. 8 and FIG. 9 depict just two of the many shapes of insert pieces that can be used. Rotationally symmetrical insert pieces with more or fewer sides (e.g. three, five, seven, or more sides) can be used in a similar manner to that shown and described. It should also be understood that multiple pieces of the turbulating insert can be removed and reinserted to adjust the pattern of fluid flow through the turbulating insert.

[0045] The turbulating insert can be assembled into the plate pair in parts. For example, the piece 4d can be first inserted into one of the plates 2 of the plate pair (for example, the plate 2b or 2b), and the second piece 4e can then be inserted into the cavity 6 before the other plate 2 of the plate pair (for example, the plate 2a or 2a) is assembled to form the completed plate pair.

[0046] In order to aid in the assembly, and to ensure that the flow directions of the turbulating insert pieces are appropriately aligned, an alignment feature can be incorporated into one or more of the pieces of the turbulating insert. FIGS. 11A-C depict a variation of the embodiment depicted in FIGS. 10A-C that includes forming a locating hole 11 into the piece 4e at a location offset from the center of the piece 4e. A locating projection such as a dimple (not shown) can be formed in the plate 2 into which the turbulating insert is to be assembled, at a location corresponding to the location where the locating hole 11 will be when the piece 4e is properly oriented. Although the piece 4e could be reinserted into the cavity 6 in four possible orientations, the locating projection of the plate 2 would prevent the insertion of the piece 4e in any orientation except the desired one, thus ensuring that the low-pressure-drop directions and high-pressure-drop directions of the turbulating insert pieces are properly oriented.

[0047] Various alternatives to the certain features and elements of the present invention are described with reference to specific embodiments of the present invention. With the exception of features, elements, and manners of operation that are mutually exclusive of or are inconsistent with each embodiment described above, it should be noted that the alternative features, elements, and manners of operation described with reference to one particular embodiment are applicable to the other embodiments.

[0048] The embodiments described above and illustrated in the figures are presented by way of example only and are not intended as a limitation upon the concepts and principles of the present invention. As such, it will be appreciated by one having ordinary skill in the art that various changes in the elements and their configuration and arrangement are possible without departing from the spirit and scope of the present invention.