US20070246202A1 - Louvered fin for heat exchanger - Google Patents
Louvered fin for heat exchanger Download PDFInfo
- Publication number
- US20070246202A1 US20070246202A1 US11/410,694 US41069406A US2007246202A1 US 20070246202 A1 US20070246202 A1 US 20070246202A1 US 41069406 A US41069406 A US 41069406A US 2007246202 A1 US2007246202 A1 US 2007246202A1
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- US
- United States
- Prior art keywords
- edge
- louvers
- louver
- turnaround
- fin
- 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.)
- Abandoned
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/126—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
- F28F1/128—Fins with openings, e.g. louvered fins
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/02—Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
- F28F3/025—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
- F28F3/027—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements with openings, e.g. louvered corrugated fins; Assemblies of corrugated strips
Definitions
- the invention relates to heat exchangers and more particularly to louvered fins for heat exchangers, wherein a rib is formed on the louvers to maximize a strength and rigidity thereof.
- An air-cooled fin-type heat exchanger is very well known. Heat exchangers are used for changing the temperature of various working fluids, such as an engine coolant, an engine lubricating oil, an air conditioning refrigerant, and an automatic transmission fluid, for example.
- the heat exchanger typically includes a plurality of spaced apart fluid conduits or tubes connected between an inlet tank and an outlet tank, and a plurality of heat exchanging fins disposed between adjacent conduits. Air is directed across the fins of the heat exchanger by a cooling fan or a motion of a vehicle, for example. As the air flows across the fins, heat in a fluid flowing through the tubes is conducted through the walls of the tubes, into the fins, and transferred into the air.
- One of the primary goals in heat exchanger design is to achieve a high fin column strength. It is known that a greater composite thickness of a fin produces a greater strength of the fin. However, increasing the composite thickness of the fin results in a larger amount of material being used to manufacture the fins. The larger amount of material results in additional weight, which is undesirable.
- Various types of fin designs have been disclosed in the prior art with the object of increasing the composite thickness to increase the strength of the fin. It would be desirable to produce a louvered fin for a heat exchanger, wherein a strength associated therewith is maximized, and a material usage is minimized.
- a heat exchanger fin comprises a base wall having a first end, a second end, and a middle portion; a turnaround louver disposed in the middle portion of the base wall, the turnaround louver having a first edge and a second edge; a plurality of spaced apart entrance louvers disposed between the first end of the base wall and the turnaround louver, the spaced entrance louvers having a first edge and a second edge; a plurality of spaced apart exit louvers disposed between the turnaround louver and the second end of the base wall, the exit louvers having a first edge and a second edge; and at least one rib formed on at least one of the turnaround louver, the entrance louvers, and the exit louvers.
- a heat exchanger fin comprises a base wall having a first end, a second end, and a middle portion; at least one turnaround louver disposed in the middle portion of the base wall, the turnaround louver having a laterally extending first edge, a laterally extending second edge and at least one rib formed between the first edge and the second edge; a plurality of spaced apart entrance louvers disposed between the first end of the base wall and the turnaround louver, the entrance louvers having a laterally extending first edge, a laterally extending second edge, and at least one rib formed between the first edge and the second edge; and a plurality of spaced apart exit louvers disposed between the turnaround louver and the second end of the base wall, the exit louvers having a laterally extending first edge, a laterally extending second edge, and at least one rib formed between the first edge and the second edge.
- a method of producing a heat exchanger fin comprises the steps of providing a substantially planar sheet of material; forming a plurality of longitudinally extending ribs in the sheet of material; forming a plurality of laterally extending corrugations in the sheet of material; and forming a plurality of rows of longitudinally extending louvers in the sheet of material, is disclosed.
- FIG. 1 is a perspective view of a heat exchanger fin in accordance with an embodiment of the invention
- FIG. 2 is a top sectional view of a plurality of louvers of the heat exchanger fin illustrated in FIG. 1 taken along line 2 - 2 ;
- FIG. 3 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention.
- FIG. 4 is a top sectional view of a plurality of louvers of the heat exchanger fin illustrated in FIG. 3 taken along a line 4 - 4 ;
- FIG. 5 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention.
- FIG. 6 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention.
- FIG. 7 is an elevational view of an apparatus used for producing a heat exchanger fin in accordance with an embodiment of the invention.
- FIG. 8 is an elevational view of an apparatus used for producing a heat exchanger fin in accordance with another embodiment of the invention.
- FIG. 1 shows a heat exchanger fin 10 having an outer surface 11 , an inner surface 13 , a first end 15 and a second end 17 .
- the heat exchanger fin 10 includes a plurality of base walls 12 . It is understood that more or fewer base walls 12 can be used without departing from the spirit or scope of the invention.
- the base walls 12 have an upper portion 14 , a lower portion 16 , a first end 18 , a second end 20 , and a middle portion 22 .
- the middle portion 22 is disposed intermediate the first end 16 and the second end 18 .
- the base walls 12 include a leading edge louver 23 , a plurality of entrance louvers 24 , a turnaround louver 26 , a plurality of exit louvers 28 , and a trailing edge louver 29 .
- the leading edge louver 23 and entrance louvers 24 are connected to the upper portion 14 of the base wall 12 at a first end 30 and to the lower portion 16 of the base wall 12 at a second end 32 .
- the leading edge louver 23 and each of the entrance louvers 24 includes a first surface 33 , a second surface 35 , a first edge 34 , a spaced apart second edge 36 , and a rib 38 .
- the rib 38 is formed between the first edge 34 and the second edge 36 and extends laterally outwardly from the second surface 35 .
- a single rib 38 is shown formed on the leading edge louver 23 and each entrance louver 24 .
- the ribs 38 extend from the first end 30 to the second end 32 of the leading edge louver 23 and entrance louvers 24 .
- a gap 39 is formed between adjacent entrance louvers 23 , 24 and between the turnaround louver 26 and the entrance louver 24 adjacent the turnaround louver 26 .
- the turnaround louver 26 is connected to the upper portion 14 of the base wall 12 at a first end 40 and to the lower portion 16 of the base wall 12 at a second end 42 .
- the turnaround louver 26 includes a first surface 43 , a second surface 45 , a first edge 44 , a spaced apart second edge 46 , and a rib 48 .
- the rib 48 is formed between the first edge 44 and the second edge 46 and extends laterally outwardly from the second surface 45 .
- a single rib 48 is shown formed on the turnaround louver 26 . However, it is understood that more or fewer ribs 48 can be formed on the turnaround louver 26 as desired.
- the rib 48 extends from the first end 40 to the second end 42 of the turnaround louver 26 .
- each of the exit louvers 28 and the trailing edge louver 29 is connected to the upper portion 14 of the base wall 12 at a first end 50 and to the lower portion 16 of the base wall 12 at a second end 52 .
- each of the exit louvers 28 and the trailing edge louver 29 includes a first surface 53 , a second surface 55 , a first edge 54 , a spaced apart second edge 56 , and a rib 58 .
- the rib 58 is formed between the first edge 54 and the second edge 56 and extends laterally outwardly from the second surface 55 .
- a single rib 58 is shown formed on each exit louver 28 and the trailing edge louver 29 .
- ribs 58 can be formed on the exit louvers 28 and the trailing edge louver 29 as desired.
- the ribs 58 extend from the first end 50 to the second end 52 of the exit louvers 28 and the trailing edge louver 29 .
- a gap 59 is formed between adjacent louvers 28 , 29 and between the turnaround louver 26 and the exit louver 28 adjacent the turnaround louver 26 .
- air is caused to flow through the gaps 39 between adjacent entrance louvers 24 .
- Heat removed from a fluid (not shown) flowing in flow tubes (not shown) is transferred through the heat exchanger fin 10 and the entrance louvers 24 to the air.
- the air is then caused to change direction at the turnaround louver 26 .
- the air flows through the gaps 59 between adjacent exit louvers 28 where additional heat is transferred from the exit louvers 28 to the air.
- a composite thickness of the louvers 24 , 26 , 28 is increased as a result of the formation of the ribs 38 , 48 , 58 on the louvers 24 , 26 , 28 .
- the increase in the composite thickness of the louvers 24 , 26 , 28 results in an increased strength of the fin 10 .
- an increase in strength of about 18% has been measured.
- An increased strength of the fin 10 allows for the use of a thinner gauged flat stock of material to make the fin 10 . Accordingly, a fin 10 having a strength substantially the same as fin structures of the prior art can be made with less material. Thus, overall weight of the fin 10 is minimized. It has been shown that a fin 10 including louvers 24 , 26 , 28 having ribs 38 , 48 , 58 formed thereon can be made with up to 20% less material than fin structures of the prior art.
- the heat exchanger fin 10 shown in FIGS. 3 and 4 includes ribs 381 , 48 ′, 58 ′. Similar structure to that described above for FIGS. 1 and 2 repeated herein with respect to FIGS. 3 and 4 includes the same reference numeral and a prime (′) symbol.
- the ribs 38 ′, 48 ′, 58 ′ are formed to extend laterally outwardly from respective first surfaces 33 , 43 , 53 . The remaining structure is the same as discussed above for FIGS. 1 and 2 . Air flow through the louvers 24 ′, 26 ′, 28 ′ is the same as described above for FIGS. 1 and 2 .
- FIG. 5 shows a strong heat exchanger fin in accordance with another embodiment of the invention. Similar structure to that described above for FIGS. 1 and 2 repeated herein with respect to FIG. 5 includes the same reference numeral and a double prime (′′) symbol.
- the ribs 38 ′′, 48 ′′, 58 ′′ extend from the first end 15 of the fin 10 ′′ to the second end 17 of the fin 10 ′′.
- the ribs 38 ′′, 48 ′′, 58 ′′ may be formed to extend laterally outwardly from the inner surface 13 of the fin 10 ′′ as shown in FIG. 5 .
- the ribs 38 ′′′, 48 ′′′, 58 ′′′ may also be formed to extend laterally outwardly from the outer surface 11 of the fin 10 ′′ as shown in FIG. 6 .
- Similar structure to that described above for FIGS. 1 and 2 repeated herein with respect to FIG. 6 includes the same reference numeral and a triple prime (′′′) symbol.
- the remaining structure and air flow through the louvers 24 ′′, 26 ′′, 28 ′′, 24 ′′′, 26 ′′′, 28 ′′′ is the same as described above for FIGS. 1 and 2 .
- a substantially planar sheet of material 110 is provided, such as aluminum, for example. As shown in FIG. 7 , the sheet of material 110 is fed into a retention roll 111 for height and straightness adjustments and then into a set of rib forming rolls 112 .
- a first one of the rib forming rolls 112 includes of a plurality of spaced annular protuberances (not shown).
- a second one of the rib forming rolls 112 includes a plurality of spaced apart annular channels or indentations.
- the protuberances and indentations of the rib forming rolls 112 cooperate to form a plurality of continuous ribs 38 , 48 , 58 in the sheet of material 110 .
- the sheet of material 110 can then be fed into a second retention roll 111 , as illustrated in FIG. 8 . Thereafter, the sheet 110 is fed into a set of corrugation fin forming rolls 114 . Cutters (not shown) disposed on the corrugation fin forming rolls 114 cut the sheet 110 to form a plurality of rows. Each of the rows includes a leading edge louver 23 , a plurality of entrance louvers 24 , a turnaround louver 26 , a plurality of exit louvers 28 , and a trailing edge louver 29 .
- the corrugation fin forming rolls 114 simultaneously alternately bend the sheet 110 to form corrugations and give the sheet 110 a wave-like shape.
- the corrugation fin forming rolls 114 also cooperate to flatten the sheet 110 between adjacent rows of louvers 23 , 24 , 26 , 28 , 29 .
- the ribs 38 , 48 , 58 formed on the top portion 14 and the bottom portion 16 of the sheet 110 are removed.
- the sheet 110 is fed into a density station 116 where further adjustments to the sheet 110 can be accomplished as desired.
- the sheet 110 is fed into a cutoff station 118 where the sheet 110 is cut to a desired length.
- a flattening of the sheet 110 between adjacent rows of louvers 23 ′′, 24 ′′, 26 ′′, 28 ′′, 29 ′′ is eliminated from the process described.
- the ribs 38 ′′, 48 ′′, 58 ′′ produced by this method extend continuously from the first end 15 of the fin 10 to the second end 17 of the fin 10 , rather than terminating at the first ends 30 , 40 , 50 and the second ends 32 , 42 , 52 of the louvers 24 ′′, 26 ′′, 28 ′′.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Geometry (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
Description
- The invention relates to heat exchangers and more particularly to louvered fins for heat exchangers, wherein a rib is formed on the louvers to maximize a strength and rigidity thereof.
- An air-cooled fin-type heat exchanger is very well known. Heat exchangers are used for changing the temperature of various working fluids, such as an engine coolant, an engine lubricating oil, an air conditioning refrigerant, and an automatic transmission fluid, for example. The heat exchanger typically includes a plurality of spaced apart fluid conduits or tubes connected between an inlet tank and an outlet tank, and a plurality of heat exchanging fins disposed between adjacent conduits. Air is directed across the fins of the heat exchanger by a cooling fan or a motion of a vehicle, for example. As the air flows across the fins, heat in a fluid flowing through the tubes is conducted through the walls of the tubes, into the fins, and transferred into the air.
- One of the primary goals in heat exchanger design is to achieve a high fin column strength. It is known that a greater composite thickness of a fin produces a greater strength of the fin. However, increasing the composite thickness of the fin results in a larger amount of material being used to manufacture the fins. The larger amount of material results in additional weight, which is undesirable. Various types of fin designs have been disclosed in the prior art with the object of increasing the composite thickness to increase the strength of the fin. It would be desirable to produce a louvered fin for a heat exchanger, wherein a strength associated therewith is maximized, and a material usage is minimized.
- Harmonious with the present invention, a louvered fin for a heat exchanger, wherein a strength associated therewith is maximized, and a material usage is minimized, has surprisingly been discovered.
- In one embodiment, a heat exchanger fin comprises a base wall having a first end, a second end, and a middle portion; a turnaround louver disposed in the middle portion of the base wall, the turnaround louver having a first edge and a second edge; a plurality of spaced apart entrance louvers disposed between the first end of the base wall and the turnaround louver, the spaced entrance louvers having a first edge and a second edge; a plurality of spaced apart exit louvers disposed between the turnaround louver and the second end of the base wall, the exit louvers having a first edge and a second edge; and at least one rib formed on at least one of the turnaround louver, the entrance louvers, and the exit louvers.
- In another embodiment, a heat exchanger fin comprises a base wall having a first end, a second end, and a middle portion; at least one turnaround louver disposed in the middle portion of the base wall, the turnaround louver having a laterally extending first edge, a laterally extending second edge and at least one rib formed between the first edge and the second edge; a plurality of spaced apart entrance louvers disposed between the first end of the base wall and the turnaround louver, the entrance louvers having a laterally extending first edge, a laterally extending second edge, and at least one rib formed between the first edge and the second edge; and a plurality of spaced apart exit louvers disposed between the turnaround louver and the second end of the base wall, the exit louvers having a laterally extending first edge, a laterally extending second edge, and at least one rib formed between the first edge and the second edge.
- A method of producing a heat exchanger fin, the method comprises the steps of providing a substantially planar sheet of material; forming a plurality of longitudinally extending ribs in the sheet of material; forming a plurality of laterally extending corrugations in the sheet of material; and forming a plurality of rows of longitudinally extending louvers in the sheet of material, is disclosed.
- The above, as well as other advantages of the present invention, will become readily apparent to those skilled in the art from the following detailed description of an embodiment of the invention when considered in the light of the accompanying drawings in which:
-
FIG. 1 is a perspective view of a heat exchanger fin in accordance with an embodiment of the invention; -
FIG. 2 is a top sectional view of a plurality of louvers of the heat exchanger fin illustrated inFIG. 1 taken along line 2-2; -
FIG. 3 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention; -
FIG. 4 is a top sectional view of a plurality of louvers of the heat exchanger fin illustrated inFIG. 3 taken along a line 4-4; -
FIG. 5 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention; -
FIG. 6 is a perspective view of a heat exchanger fin in accordance with another embodiment of the invention; -
FIG. 7 is an elevational view of an apparatus used for producing a heat exchanger fin in accordance with an embodiment of the invention; and -
FIG. 8 is an elevational view of an apparatus used for producing a heat exchanger fin in accordance with another embodiment of the invention. - The following detailed description and appended drawings describe and illustrate various exemplary embodiments of the invention. The description and drawings serve to enable one skilled in the art to make and use the invention, and are not intended to limit the scope of the invention in any manner. In respect of the methods disclosed an illustrated, the steps presented are exemplary in nature, and thus, the order of the steps is not necessary or critical.
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FIG. 1 shows aheat exchanger fin 10 having anouter surface 11, aninner surface 13, afirst end 15 and asecond end 17. Theheat exchanger fin 10 includes a plurality ofbase walls 12. It is understood that more orfewer base walls 12 can be used without departing from the spirit or scope of the invention. Thebase walls 12 have anupper portion 14, alower portion 16, afirst end 18, asecond end 20, and amiddle portion 22. Themiddle portion 22 is disposed intermediate thefirst end 16 and thesecond end 18. - The
base walls 12 include a leadingedge louver 23, a plurality ofentrance louvers 24, aturnaround louver 26, a plurality ofexit louvers 28, and atrailing edge louver 29. The leadingedge louver 23 andentrance louvers 24 are connected to theupper portion 14 of thebase wall 12 at afirst end 30 and to thelower portion 16 of thebase wall 12 at asecond end 32. As more clearly shown inFIG. 2 , the leadingedge louver 23 and each of theentrance louvers 24 includes afirst surface 33, asecond surface 35, afirst edge 34, a spaced apartsecond edge 36, and arib 38. Therib 38 is formed between thefirst edge 34 and thesecond edge 36 and extends laterally outwardly from thesecond surface 35. Asingle rib 38 is shown formed on the leadingedge louver 23 and eachentrance louver 24. However, it is understood that more orfewer ribs 38 can be formed on the leadingedge louver 23 and theentrance louvers 24 as desired without departing from the scope of the invention. In the embodiment shown, theribs 38 extend from thefirst end 30 to thesecond end 32 of the leadingedge louver 23 andentrance louvers 24. Agap 39 is formed between 23, 24 and between theadjacent entrance louvers turnaround louver 26 and theentrance louver 24 adjacent theturnaround louver 26. - The
turnaround louver 26 is connected to theupper portion 14 of thebase wall 12 at afirst end 40 and to thelower portion 16 of thebase wall 12 at asecond end 42. As illustrated inFIG. 2 , theturnaround louver 26 includes afirst surface 43, asecond surface 45, afirst edge 44, a spaced apartsecond edge 46, and arib 48. Therib 48 is formed between thefirst edge 44 and thesecond edge 46 and extends laterally outwardly from thesecond surface 45. Asingle rib 48 is shown formed on theturnaround louver 26. However, it is understood that more orfewer ribs 48 can be formed on theturnaround louver 26 as desired. Therib 48 extends from thefirst end 40 to thesecond end 42 of theturnaround louver 26. - The exit louvers 28 and the
trailing edge louver 29 are connected to theupper portion 14 of thebase wall 12 at afirst end 50 and to thelower portion 16 of thebase wall 12 at asecond end 52. As shown inFIG. 2 , each of theexit louvers 28 and thetrailing edge louver 29 includes afirst surface 53, asecond surface 55, afirst edge 54, a spaced apartsecond edge 56, and arib 58. Therib 58 is formed between thefirst edge 54 and thesecond edge 56 and extends laterally outwardly from thesecond surface 55. Asingle rib 58 is shown formed on eachexit louver 28 and thetrailing edge louver 29. However, it is understood that more orfewer ribs 58 can be formed on theexit louvers 28 and thetrailing edge louver 29 as desired. Theribs 58 extend from thefirst end 50 to thesecond end 52 of theexit louvers 28 and thetrailing edge louver 29. Agap 59 is formed between 28, 29 and between theadjacent louvers turnaround louver 26 and theexit louver 28 adjacent theturnaround louver 26. - As is known in the art, air is caused to flow through the
gaps 39 betweenadjacent entrance louvers 24. Heat removed from a fluid (not shown) flowing in flow tubes (not shown) is transferred through theheat exchanger fin 10 and theentrance louvers 24 to the air. The air is then caused to change direction at theturnaround louver 26. The air flows through thegaps 59 betweenadjacent exit louvers 28 where additional heat is transferred from theexit louvers 28 to the air. - A composite thickness of the
24, 26, 28 is increased as a result of the formation of thelouvers 38, 48, 58 on theribs 24, 26, 28. The increase in the composite thickness of thelouvers 24, 26, 28 results in an increased strength of thelouvers fin 10. For the embodiment shown inFIGS. 1 and 2 , an increase in strength of about 18% has been measured. - An increased strength of the
fin 10 allows for the use of a thinner gauged flat stock of material to make thefin 10. Accordingly, afin 10 having a strength substantially the same as fin structures of the prior art can be made with less material. Thus, overall weight of thefin 10 is minimized. It has been shown that afin 10 including 24, 26, 28 havinglouvers 38, 48, 58 formed thereon can be made with up to 20% less material than fin structures of the prior art.ribs - The
heat exchanger fin 10 shown inFIGS. 3 and 4 includesribs 381, 48′, 58′. Similar structure to that described above forFIGS. 1 and 2 repeated herein with respect toFIGS. 3 and 4 includes the same reference numeral and a prime (′) symbol. Theribs 38′, 48′, 58′ are formed to extend laterally outwardly from respective 33, 43, 53. The remaining structure is the same as discussed above forfirst surfaces FIGS. 1 and 2 . Air flow through thelouvers 24′, 26′, 28′ is the same as described above forFIGS. 1 and 2 . -
FIG. 5 shows a strong heat exchanger fin in accordance with another embodiment of the invention. Similar structure to that described above forFIGS. 1 and 2 repeated herein with respect toFIG. 5 includes the same reference numeral and a double prime (″) symbol. In this embodiment, theribs 38″, 48″, 58″ extend from thefirst end 15 of thefin 10″ to thesecond end 17 of thefin 10″. Theribs 38″, 48″, 58″ may be formed to extend laterally outwardly from theinner surface 13 of thefin 10″ as shown inFIG. 5 . Theribs 38′″, 48′″, 58′″ may also be formed to extend laterally outwardly from theouter surface 11 of thefin 10″ as shown inFIG. 6 . Similar structure to that described above forFIGS. 1 and 2 repeated herein with respect toFIG. 6 includes the same reference numeral and a triple prime (′″) symbol. The remaining structure and air flow through thelouvers 24″, 26″, 28″, 24′″, 26′″, 28′″ is the same as described above forFIGS. 1 and 2 . - A method of forming the
heat exchanger fin 10 described inFIGS. 1-2 will now be described. A substantially planar sheet ofmaterial 110 is provided, such as aluminum, for example. As shown inFIG. 7 , the sheet ofmaterial 110 is fed into aretention roll 111 for height and straightness adjustments and then into a set of rib forming rolls 112. A first one of therib forming rolls 112 includes of a plurality of spaced annular protuberances (not shown). A second one of therib forming rolls 112 includes a plurality of spaced apart annular channels or indentations. The protuberances and indentations of therib forming rolls 112 cooperate to form a plurality of 38, 48, 58 in the sheet ofcontinuous ribs material 110. Optionally, the sheet ofmaterial 110 can then be fed into asecond retention roll 111, as illustrated inFIG. 8 . Thereafter, thesheet 110 is fed into a set of corrugation fin forming rolls 114. Cutters (not shown) disposed on the corrugationfin forming rolls 114 cut thesheet 110 to form a plurality of rows. Each of the rows includes aleading edge louver 23, a plurality ofentrance louvers 24, aturnaround louver 26, a plurality ofexit louvers 28, and a trailingedge louver 29. The corrugationfin forming rolls 114 simultaneously alternately bend thesheet 110 to form corrugations and give the sheet 110 a wave-like shape. The corrugationfin forming rolls 114 also cooperate to flatten thesheet 110 between adjacent rows of 23, 24, 26, 28, 29. Thus, thelouvers 38, 48, 58 formed on theribs top portion 14 and thebottom portion 16 of thesheet 110 are removed. Thesheet 110 is fed into adensity station 116 where further adjustments to thesheet 110 can be accomplished as desired. Thesheet 110 is fed into acutoff station 118 where thesheet 110 is cut to a desired length. - To form the
fin 10″ described inFIG. 5 above, a flattening of thesheet 110 between adjacent rows oflouvers 23″, 24″, 26″, 28″, 29″ is eliminated from the process described. Theribs 38″, 48″, 58″ produced by this method extend continuously from thefirst end 15 of thefin 10 to thesecond end 17 of thefin 10, rather than terminating at the first ends 30, 40, 50 and the second ends 32, 42, 52 of thelouvers 24″, 26″, 28″. - From the foregoing description, one ordinarily skilled in the art can easily ascertain the essential characteristics of this invention and, without departing from the spirit and scope thereof, can make various changes and modifications to the invention to adapt it to various usages and conditions.
Claims (20)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/410,694 US20070246202A1 (en) | 2006-04-25 | 2006-04-25 | Louvered fin for heat exchanger |
| DE102007020722A DE102007020722A1 (en) | 2006-04-25 | 2007-04-24 | Laminated rib for a heat exchanger |
| KR1020070040104A KR101441123B1 (en) | 2006-04-25 | 2007-04-25 | Louvered pins for heat exchangers |
| JP2007139690A JP2007292453A (en) | 2006-04-25 | 2007-04-25 | Louvered fin for heat exchanger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/410,694 US20070246202A1 (en) | 2006-04-25 | 2006-04-25 | Louvered fin for heat exchanger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070246202A1 true US20070246202A1 (en) | 2007-10-25 |
Family
ID=38608267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/410,694 Abandoned US20070246202A1 (en) | 2006-04-25 | 2006-04-25 | Louvered fin for heat exchanger |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20070246202A1 (en) |
| JP (1) | JP2007292453A (en) |
| KR (1) | KR101441123B1 (en) |
| DE (1) | DE102007020722A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080169091A1 (en) * | 2007-01-12 | 2008-07-17 | Proliance International Inc. | Method for producing a split louver heat exchanger fin |
| US20180369972A1 (en) * | 2017-06-22 | 2018-12-27 | Hs Marston Aerospace Limited | Method of forming a component for a heat exchanger |
| CN113039405A (en) * | 2018-11-13 | 2021-06-25 | 株式会社电装 | Heat exchanger |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5156773B2 (en) * | 2010-02-25 | 2013-03-06 | 株式会社小松製作所 | Corrugated fin and heat exchanger provided with the same |
| DE102010033468B4 (en) * | 2010-08-05 | 2022-05-12 | GEA MASCHINENKüHLTECHNIK GMBH | heat exchanger |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1453250A (en) * | 1922-08-26 | 1923-04-24 | C G Haubold Aktien Ges | Heat-exchanging apparatus |
| US1553093A (en) * | 1920-05-10 | 1925-09-08 | Arthur B Modine | Radiator |
| US1730470A (en) * | 1925-09-25 | 1929-10-08 | Arthur B Modine | Method of soldering radiator fins |
| US4300629A (en) * | 1978-06-21 | 1981-11-17 | Hitachi, Ltd. | Cross-fin tube type heat exchanger |
| US4365667A (en) * | 1979-02-07 | 1982-12-28 | Hitachi, Ltd. | Heat exchanger |
| US4693307A (en) * | 1985-09-16 | 1987-09-15 | General Motors Corporation | Tube and fin heat exchanger with hybrid heat transfer fin arrangement |
| US4791984A (en) * | 1986-04-25 | 1988-12-20 | Hitachi, Ltd. | Heat transfer fin |
| US4869316A (en) * | 1985-10-14 | 1989-09-26 | Mitsubishi Denki Kabushiki Kaisha | Heat exchanger |
| US4958681A (en) * | 1989-08-14 | 1990-09-25 | General Motors Corporation | Heat exchanger with bypass channel louvered fins |
| US4984626A (en) * | 1989-11-24 | 1991-01-15 | Carrier Corporation | Embossed vortex generator enhanced plate fin |
| US5062475A (en) * | 1989-10-02 | 1991-11-05 | Sundstrand Heat Transfer, Inc. | Chevron lanced fin design with unequal leg lengths for a heat exchanger |
| US5111876A (en) * | 1991-10-31 | 1992-05-12 | Carrier Corporation | Heat exchanger plate fin |
| US5353866A (en) * | 1987-12-04 | 1994-10-11 | Hitachi, Ltd. | Heat transfer fins and heat exchanger |
| US5361829A (en) * | 1991-12-19 | 1994-11-08 | Behr Gmbh & Co. | Corrugated fin for flat-tube heat exchangers |
| US5507270A (en) * | 1994-09-06 | 1996-04-16 | Precision Shooting Equipment, Inc. | Limb pocket and pocket liner for archery bow |
| US5722485A (en) * | 1994-11-17 | 1998-03-03 | Lennox Industries Inc. | Louvered fin heat exchanger |
| US5730214A (en) * | 1997-01-16 | 1998-03-24 | General Motors Corporation | Heat exchanger cooling fin with varying louver angle |
| US5752567A (en) * | 1996-12-04 | 1998-05-19 | York International Corporation | Heat exchanger fin structure |
| US5787972A (en) * | 1997-08-22 | 1998-08-04 | General Motors Corporation | Compression tolerant louvered heat exchanger fin |
| US5927393A (en) * | 1997-12-11 | 1999-07-27 | Heatcraft Inc. | Heat exchanger fin with enhanced corrugations |
| US5975199A (en) * | 1996-12-30 | 1999-11-02 | Samsung Electronics Co., Ltd. | Cooling fin for heat exchanger |
| US20030079868A1 (en) * | 1996-12-18 | 2003-05-01 | Samy Bouzida | Metallic cooling fin for a heat exchanger, especially for a motor vehicle |
| US6598295B1 (en) * | 2002-03-07 | 2003-07-29 | Brazeway, Inc. | Plate-fin and tube heat exchanger with a dog-bone and serpentine tube insertion method |
| US20040251004A1 (en) * | 2003-01-02 | 2004-12-16 | Livernois Engineering Company | Serpentine fin with extended louvers for heat exchanger and roll forming tool for manufacturing same |
| US20050056407A1 (en) * | 2003-09-15 | 2005-03-17 | Oh Sai Kee | Heat exchanger |
| US6889759B2 (en) * | 2003-06-25 | 2005-05-10 | Evapco, Inc. | Fin for heat exchanger coil assembly |
| US6918432B2 (en) * | 2001-06-13 | 2005-07-19 | Denso Corporation | Heat exchanger |
| US20050199378A1 (en) * | 2004-03-13 | 2005-09-15 | Bernhard Lamich | Heat exchanger core and corrugated rib |
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| US20070137840A1 (en) * | 2005-12-16 | 2007-06-21 | Denso Corporation | Corrugated fin and heat exchanger using the same |
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| US20080121385A1 (en) * | 2006-11-28 | 2008-05-29 | Hyundai Mobis Co., Ltd. | Heat dissipation fin for heat exchangers |
| US20080169091A1 (en) * | 2007-01-12 | 2008-07-17 | Proliance International Inc. | Method for producing a split louver heat exchanger fin |
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| KR860008433A (en) * | 1985-04-12 | 1986-11-15 | 월터 이. 파블리이크 | Heat exchanger with S-shaped reinforcement fins |
| JPH0868598A (en) * | 1994-08-31 | 1996-03-12 | Hino Motors Ltd | Fin structure of radiator core |
| JP3942210B2 (en) * | 1996-04-16 | 2007-07-11 | 昭和電工株式会社 | Heat exchanger, room air conditioner and car air conditioner using this heat exchanger |
| JP2004263881A (en) * | 2003-01-23 | 2004-09-24 | Showa Denko Kk | Heat transfer fin, heat exchanger, evaporator and condenser for car air conditioner |
-
2006
- 2006-04-25 US US11/410,694 patent/US20070246202A1/en not_active Abandoned
-
2007
- 2007-04-24 DE DE102007020722A patent/DE102007020722A1/en not_active Withdrawn
- 2007-04-25 JP JP2007139690A patent/JP2007292453A/en active Pending
- 2007-04-25 KR KR1020070040104A patent/KR101441123B1/en not_active Expired - Fee Related
Patent Citations (35)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1553093A (en) * | 1920-05-10 | 1925-09-08 | Arthur B Modine | Radiator |
| US1453250A (en) * | 1922-08-26 | 1923-04-24 | C G Haubold Aktien Ges | Heat-exchanging apparatus |
| US1730470A (en) * | 1925-09-25 | 1929-10-08 | Arthur B Modine | Method of soldering radiator fins |
| US4300629A (en) * | 1978-06-21 | 1981-11-17 | Hitachi, Ltd. | Cross-fin tube type heat exchanger |
| US4365667A (en) * | 1979-02-07 | 1982-12-28 | Hitachi, Ltd. | Heat exchanger |
| US4693307A (en) * | 1985-09-16 | 1987-09-15 | General Motors Corporation | Tube and fin heat exchanger with hybrid heat transfer fin arrangement |
| US4869316A (en) * | 1985-10-14 | 1989-09-26 | Mitsubishi Denki Kabushiki Kaisha | Heat exchanger |
| US4791984A (en) * | 1986-04-25 | 1988-12-20 | Hitachi, Ltd. | Heat transfer fin |
| US5353866A (en) * | 1987-12-04 | 1994-10-11 | Hitachi, Ltd. | Heat transfer fins and heat exchanger |
| US4958681A (en) * | 1989-08-14 | 1990-09-25 | General Motors Corporation | Heat exchanger with bypass channel louvered fins |
| US5062475A (en) * | 1989-10-02 | 1991-11-05 | Sundstrand Heat Transfer, Inc. | Chevron lanced fin design with unequal leg lengths for a heat exchanger |
| US4984626A (en) * | 1989-11-24 | 1991-01-15 | Carrier Corporation | Embossed vortex generator enhanced plate fin |
| US5111876A (en) * | 1991-10-31 | 1992-05-12 | Carrier Corporation | Heat exchanger plate fin |
| US5361829A (en) * | 1991-12-19 | 1994-11-08 | Behr Gmbh & Co. | Corrugated fin for flat-tube heat exchangers |
| US5507270A (en) * | 1994-09-06 | 1996-04-16 | Precision Shooting Equipment, Inc. | Limb pocket and pocket liner for archery bow |
| US5722485A (en) * | 1994-11-17 | 1998-03-03 | Lennox Industries Inc. | Louvered fin heat exchanger |
| US5752567A (en) * | 1996-12-04 | 1998-05-19 | York International Corporation | Heat exchanger fin structure |
| US20030079868A1 (en) * | 1996-12-18 | 2003-05-01 | Samy Bouzida | Metallic cooling fin for a heat exchanger, especially for a motor vehicle |
| US5975199A (en) * | 1996-12-30 | 1999-11-02 | Samsung Electronics Co., Ltd. | Cooling fin for heat exchanger |
| US5730214A (en) * | 1997-01-16 | 1998-03-24 | General Motors Corporation | Heat exchanger cooling fin with varying louver angle |
| US5787972A (en) * | 1997-08-22 | 1998-08-04 | General Motors Corporation | Compression tolerant louvered heat exchanger fin |
| US5927393A (en) * | 1997-12-11 | 1999-07-27 | Heatcraft Inc. | Heat exchanger fin with enhanced corrugations |
| US6918432B2 (en) * | 2001-06-13 | 2005-07-19 | Denso Corporation | Heat exchanger |
| US20060005956A1 (en) * | 2001-06-28 | 2006-01-12 | York International Corporation | High-V plate fin heat exchanger and method of manufacturing |
| US6598295B1 (en) * | 2002-03-07 | 2003-07-29 | Brazeway, Inc. | Plate-fin and tube heat exchanger with a dog-bone and serpentine tube insertion method |
| US20040251004A1 (en) * | 2003-01-02 | 2004-12-16 | Livernois Engineering Company | Serpentine fin with extended louvers for heat exchanger and roll forming tool for manufacturing same |
| US6889759B2 (en) * | 2003-06-25 | 2005-05-10 | Evapco, Inc. | Fin for heat exchanger coil assembly |
| US20050056407A1 (en) * | 2003-09-15 | 2005-03-17 | Oh Sai Kee | Heat exchanger |
| US20050199378A1 (en) * | 2004-03-13 | 2005-09-15 | Bernhard Lamich | Heat exchanger core and corrugated rib |
| US20060157233A1 (en) * | 2005-01-19 | 2006-07-20 | Denso Corporation | Heat exchanger |
| US20070137840A1 (en) * | 2005-12-16 | 2007-06-21 | Denso Corporation | Corrugated fin and heat exchanger using the same |
| US7413002B2 (en) * | 2005-12-16 | 2008-08-19 | Denso Corporation | Corrugated fin and heat exchanger using the same |
| US20070240865A1 (en) * | 2006-04-13 | 2007-10-18 | Zhang Chao A | High performance louvered fin for heat exchanger |
| US20080121385A1 (en) * | 2006-11-28 | 2008-05-29 | Hyundai Mobis Co., Ltd. | Heat dissipation fin for heat exchangers |
| US20080169091A1 (en) * | 2007-01-12 | 2008-07-17 | Proliance International Inc. | Method for producing a split louver heat exchanger fin |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080169091A1 (en) * | 2007-01-12 | 2008-07-17 | Proliance International Inc. | Method for producing a split louver heat exchanger fin |
| US7866042B2 (en) * | 2007-01-12 | 2011-01-11 | Centrum Equities Acquisition, Llc | Method for producing a split louver heat exchanger fin |
| US20180369972A1 (en) * | 2017-06-22 | 2018-12-27 | Hs Marston Aerospace Limited | Method of forming a component for a heat exchanger |
| US10974353B2 (en) * | 2017-06-22 | 2021-04-13 | Hs Marston Aerospace Limited | Method of forming a component for a heat exchanger |
| CN113039405A (en) * | 2018-11-13 | 2021-06-25 | 株式会社电装 | Heat exchanger |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2007292453A (en) | 2007-11-08 |
| KR101441123B1 (en) | 2014-09-17 |
| DE102007020722A1 (en) | 2007-11-22 |
| KR20070105269A (en) | 2007-10-30 |
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