EP2106520B1 - Ailette d'échangeur de chaleur - Google Patents

Ailette d'échangeur de chaleur Download PDF

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Publication number
EP2106520B1
EP2106520B1 EP07853381.7A EP07853381A EP2106520B1 EP 2106520 B1 EP2106520 B1 EP 2106520B1 EP 07853381 A EP07853381 A EP 07853381A EP 2106520 B1 EP2106520 B1 EP 2106520B1
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EP
European Patent Office
Prior art keywords
strip
louvers
louver
metal strip
extending
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.)
Not-in-force
Application number
EP07853381.7A
Other languages
German (de)
English (en)
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EP2106520A1 (fr
EP2106520A4 (fr
Inventor
John A. Kolb
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vista-Pro Automotive LLC
Original Assignee
Vista-Pro Automotive LLC
Vista Pro Automotive LLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US11/622,512 external-priority patent/US7866042B2/en
Priority claimed from US11/770,210 external-priority patent/US8408283B2/en
Application filed by Vista-Pro Automotive LLC, Vista Pro Automotive LLC filed Critical Vista-Pro Automotive LLC
Publication of EP2106520A1 publication Critical patent/EP2106520A1/fr
Publication of EP2106520A4 publication Critical patent/EP2106520A4/fr
Application granted granted Critical
Publication of EP2106520B1 publication Critical patent/EP2106520B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/053—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
    • F28D1/0535—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
    • F28D1/05366—Assemblies of conduits connected to common headers, e.g. core type radiators
    • F28D1/05383—Assemblies of conduits connected to common headers, e.g. core type radiators with multiple rows of conduits or with multi-channel conduits
    • 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
    • B21D13/00—Corrugating sheet metal, rods or profiles; Bending sheet metal, rods or profiles into wave form
    • B21D13/04—Corrugating sheet metal, rods or profiles; Bending sheet metal, rods or profiles into wave form by rolling
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2215/00—Fins
    • F28F2215/02—Arrangements of fins common to different heat exchange sections, the fins being in contact with different heat exchange media

Definitions

  • the present invention relates to the manufacture of heat exchangers and the manufacture of fins for heat exchanger cores primarily used in motor vehicles.
  • serpentine fins formed from thin gauge metal strip such as copper or aluminum are placed between and in contact with the tubes which carry the fluid to be cooled.
  • the heat exchanger core tubes typically extend between the manifolds, or the inlet and outlet tanks, of the heat exchanger.
  • the fins are the chief heat exchange medium between the coolant and the ambient air. The ability of the fins to transfer heat from the tubes to the air passing over the fins greatly relies on the design of the fins, with some including dimples or protrusions to aid in the heat transfer. To increase the heat transfer rate even further, louvers have been incorporated into the fins.
  • the louvers turbulate the air in a manner which has been found to increase the efficiency of the radiator.
  • the louver configuration may be so-called full louvers, where each louver in the row extends over essentially the entire distance between the tubes, or split louvers, where two side-by-side banks of louvers are employed in the row, so that each of the two louvers extends over less than half of the distance between each tube.
  • serpentine fins in which a flat metal strip is folded into convolutions to create the multiple fins between spaced tubes.
  • louvers When louvers are incorporated into fins, the structural integrity of the fin is compromised, particularly where serpentine fins are used.
  • a process known as hard-tool forming is typically used in forming the serpentine fin, wherein the louvers are formed with a pair of dies which have a star configuration for forming the convolutions at the same time.
  • the complexity of the dies and machinery for performing the formation of the fins make the process costly.
  • the rolls only need to have the die formation for the louvers, and the star shape of the roll may be eliminated.
  • backpressure is applied at different locations to the metal strip to force the metal to buckle, create the convolutions in the strip of metal, and form the finished serpentine configuration in the desired fin per inch density.
  • the air-forming process often produces convolutions that are more random in placement with respect to the rows of louvers compared to the use of hard tooling.
  • the use of the air-forming process has been found to distort the full louvers, change the angle of the louvers, and sometimes close the louver opening altogether.
  • serpentine heat exchanger fins have been described in U.S. 5,361,829 to Kreutzer et al and US 6,918,432 to Ozaki . Such reinforcements have been added to serpentine fins for several reasons. The first, as stated by Kreutzer, is to provide support for flat heat exchanger tubes against bulging due to internal pressure. A second reason, as stated by Ozaki, is to prevent distortion of the fins during washing of the core with water at high pressure. Additionally, serpentine fins are subject to compressive forces during the heat exchanger manufacturing operation of stacking the fins and tubes to make a core assembly. The stacked assembly of fins and tubes is held clamped under pressure during the subsequent soldering or brazing of the core.
  • JP 2002-147982 discloses a corrugated finned heat exchanger having widthwise ends folded back to form double parts in a fin according to the preamble of claim 9 having full louvers extending over essentially the entire distance of the fin.
  • a further object of the invention is to provide a method for manufacturing louvered serpentine fins which does not decrease the structural integrity of the fin, and optionally adds increased structural integrity against forces created during the manufacturing process.
  • a further object of the invention is to provide a heat exchanger fin which will have exceptional strength against bulging of the core due to internal pressure, against distortion to the fins due to pressure washing, and against damage in service due to road debris.
  • Another object of the invention is to provide a heat exchanger fin which has a ribbed hem, for use in a serpentine or plate-type fin.
  • Yet another object of the invention is to provide an improved method of air forming a serpentine heat exchanger fin using a ribbed hem.
  • the present invention provides a serpentine fin for assembly between tubes in a heat exchanger core comprising a metal strip having a width between opposite strip edges and a length greater than the width.
  • the strip edges have a hem formed thereon comprising a double thickness of the strip material extending a portion of the distance inward from the edge.
  • the metal strip has folds extending across the strip width such that the strip forms a serpentine shape, with the folds being adapted to contact the tubes in the heat exchanger core.
  • the serpentine fin also includes at least one row of louvers between adjacent folds.
  • the at least one row of louvers comprises split louvers having openings extending in the direction of the strip length and formed in adjacent, spaced louver banks extending at least a portion across of the width of the strip.
  • the serpentine fin further includes ribs substantially parallel to the louver openings adjacent the strip edges and in at least one center portion of the strip between the strip edges, the ribs extending across the louver banks.
  • the hem may extend over a portion of the rib, may extend fully into the rib, or may extend fully into the rib and associated louver.
  • the rib may form a V-shaped channel or a U-shaped channel.
  • the louvers are formed at an angle to a plane of the metal strip and the louver angle is between about 26 degrees and about 32 degrees.
  • the metal strip has a thickness and the ribs have a height extending from a plane of the metal strip, and the ratio of the height to the thickness of the metal strip is between about 4 and 5.
  • the ribs are preferably elongated, plastically deformed sections and include at least one angled leg connected to an adjacent louver.
  • the present invention is also directed to a method of manufacturing serpentine fins for assembly between tubes in a heat exchanger core.
  • the method includes providing a flat metal strip for making heat exchanger fins, the strip having a width between opposite strip edges and a length greater than the width and forming in the strip, while the strip is substantially flat, multiple rows of split louvers.
  • Each row of louvers has louvers with openings extending in the direction of the strip length and formed in adjacent, spaced louver banks extending at least a portion across of the width of the strip.
  • Each row includes at least one rib formed in the strip substantially parallel to the louver openings and extending across the pair of louver banks.
  • the metal strip has unformed portions extending across the strip width between rows of split louvers and at least one rib for forming folds across the width of the strip.
  • an initial pressure is applied to the metal strip to cause the substantially flat strip to buckle in the unformed portions and begin to form folds in the strip.
  • At least one row of louvers is between adjacent folds along the length of the strip.
  • further pressure is applied to the metal strip to complete formation of the folds of the strip to form the serpentine fin.
  • the distance between the adjacent folds conforms to the desired spacing distance between the heat exchanger core tubes.
  • the ribs formed in the strip may be along the edges of the strip or the ribs may be in a center portion between the edges.
  • the strip will have ribs formed both in the center portion and along the edges.
  • the ribs are elongated, plastically deformed sections and may include at least one angled leg connected to an adjacent louver.
  • the ribs have a height extending from a plane of the metal strip and the ratio of the height to the thickness of the metal strip is preferably between about 4 and 5.
  • the louvers have ends adjacent the unformed portions of the metal strip and after applying the further pressure to the metal strip, the distance between the louver ends and the folds at the unformed portions may be substantially equal.
  • the louvers are formed at an angle to a plane of the metal strip and the louver angle is preferably between about 26 degrees and about 32 degrees.
  • the strip may be continually moving such that the initial pressure is a backpressure applied by contacting the strip at a first location and such that the further pressure is a further backpressure applied by contacting the strip at a second location downstream of the first location with respect to strip movement.
  • the present invention further provides an improved method for manufacturing louvered serpentine fins by air forming.
  • the preferred method comprises providing a flat metal strip for making heat exchanger fins, the strip having a width between opposite strip edges and a length greater than the width.
  • Each of the opposite strip edges is a hemmed edge comprising a double thickness of the flat metal strip and extending a portion of the distance inward from the edges to form a hem.
  • the method includes forming in the strip, while the strip is substantially flat, multiple rows of louvers.
  • Each row of louvers comprises louvers having openings extending in the direction of the strip length and formed in adjacent, spaced louver banks extending at least a portion across of the width of the strip.
  • At least one rib is formed in the strip, which rib is substantially parallel to the louver openings and extends across the louver banks.
  • the metal strip has unformed portions extending across the strip width between rows of strip louvers and ribs for forming folds across the width of the strip.
  • the method includes applying an initial pressure to the metal strip to cause the substantially flat strip to buckle in the unformed portions and begin to form folds in the strip, with at least one row of louvers between adjacent folds along the length of the strip, and thereafter applying further pressure to the metal strip to complete formation of the folds of the strip to form the serpentine fin.
  • the distance between the adjacent folds conforms to the desired spacing distance between the heat exchanger core tubes.
  • the method preferably includes folding each of the opposite strip edges to form the hemmed edge, such that the hem extends over a portion of the rib, the hem extends fully into the rib, or the hem extends fully into the rib and associated louver.
  • the strip is continually moving.
  • the initial pressure is a backpressure applied by contacting the strip at a first location and the further pressure is a further backpressure applied by contacting the strip at a second location downstream of the first location with respect to strip movement.
  • the rib may be formed adjacent the strip edges and/or in a center portion of the strip between the strip edges.
  • the rib is preferably an elongated, plastically deformed section and may include at least one angled leg connected to an adjacent louver.
  • the louvers preferably have ends adjacent the unformed portions of the metal strip and wherein after applying the further pressure to the metal strip, the distance between the louver ends and the folds at the unformed portions is substantially equal.
  • the invention is directed to a serpentine fin for assembly between tubes in a heat exchanger core.
  • the serpentine fin comprises a metal strip having a width between opposite strip edges and a length greater than the width and having multiple rows of louvers.
  • Each row of louvers comprises split louvers having openings extending in the direction of the strip length and formed in a pair of adjacent, spaced louver banks extending at least a portion across of the width of the strip.
  • the strip includes ribs formed in the strip substantially parallel to the louver openings adjacent the strip edges and in a center portion of the strip between the strip edges and extending across the pair of louver banks.
  • the metal strip has unformed portions extending across the strip width between rows of strip louvers and ribs, wherein the strip has folds along the unformed portions extending across the strip width such that the strip forms a serpentine shape with at least one row of split louvers between adjacent folds.
  • the folds are adapted to contact the tubes in the heat exchanger core.
  • Figs. 1-4 depict a split louver fin configuration formed in a flat metal strip in accordance with the present invention, prior to forming the serpentine convolutions.
  • a length of metal strip 12 of aluminum or preferably copper has split louvers 40 extending in rows 25 across the width of the strip, ribs 18a and 18b formed adjacent the louvers 40 within the rows 25, and unformed portions 22 extending across the strip width between rows 25 of the louvers 40.
  • the louvers 40 are formed by cutting the strip 12 and twisting and plastically deforming the cut portions. The opposite ends of each of the louvers 40 maintain connection with the remaining metal strip 12 by a twist portion.
  • Each row 25 of split louvers 40 is made up of a pair of banks 25a, 25b of individual louvers 40, which are separated from each other by unformed portion 24 extending in the direction of the strip width.
  • the adjacent, spaced louver banks 25a, 25b extend across at least a portion of the width of the strip 12, and preferably extend across substantially all of the strip width.
  • the louvers 40, the openings between the louvers 40, and ribs 18a, 18b extend in the direction of the strip length 21.
  • Ribs 18a, 18b are plastically deformed in the strip substantially parallel to the louver openings in the direction of the strip length and extend substantially completely across the pair of louver banks 25a, 25b, including across the unformed strip portion 24 between the louver banks. End ribs 18a are located near the strip edges 27 and center ribs 18b are located in center portions of the strip 12 between the strip edges 27. Ribs 18a, 18b extend across the pair of louver banks 25a, 25b, but not beyond the ends of the louvers 40 into the unformed sections 22 separating the rows 25 of louvers 40. End ribs 18a shown in the detailed view of Fig.
  • FIG. 3 have plastically deformed portions and include one angled leg 18'a extending at an angle downward from the plane 30 of the undeformed metal strip and a bent portion 18"a that connects to the adjacent louver 40.
  • the end ribs 18a are ultimately positioned, after assembly of the fin in the core, near the upstream and downstream ends of the fin relative to the direction of cooling airflow.
  • Center ribs 18b shown in the detailed view of Fig. 4 also have plastically deformed portions with angled legs 18'b extending at an angle downward from an undeformed metal strip portion in plane 30 and bent portions 18"b that connect to the adjacent split louvers 40.
  • each split louver 40 has a total height L and is angled at an angle ⁇ from the neutral plane 30 of the undeformed metal strip 12.
  • the strip 12 and louvers 40 have a thickness of about 0.0022 in. (0.056 mm), and the louvers have angle ⁇ of about 30° and height L of about 0.023 in. (0.58 mm).
  • the ribs 18a, 18b have a height distance h in one direction from the neutral plane of about 0.0104 in. (0.26 mm). The ratio of h/s is about 4.7, and signifies that the height of the rib is about 4.7 times the thickness of the fin material.
  • the metal strip 12 may be made with a single thickness edge as shown in Fig. 3 , where edge 27 is of the same thickness as the remainder of the strip material.
  • the metal strip 12 may include a hem 88 along each of the opposite edges along which the end ribs 18a are formed.
  • the hem 88 comprises a double thickness of the metal strip material and extends at least a portion inward from the edge. The distance to which the hem 88 extends inward may vary as shown in the embodiments of Figs. 5-7 .
  • the hem 88 is formed by folding a portion of the original cut metal strip edge 27 ( Figs.
  • the invention having the hemmed edges 80 also includes end ribs 18a having a plastically deformed angled leg 18'a and a bent portion 18"a.
  • the embodiment shown in Fig. 5 has the hem 88 extending only a portion of the distance from the hem edge 80 to the end rib 18a, wherein no portion of the end rib 18a or the associated louver 40' is in the hemmed area.
  • the hem 88' extends from the hem edge 80 to a point partially or fully encompassing the end rib 18a, and more preferably, the hem 88" extends fully into the end rib and partially or fully into the associated louver 40'.
  • the end rib 18a adjacent the edges of the metal strip 12 may comprise a double thickness of the metal strip in part of the rib 18a, in the entire rib 18a or the entire rib 18a along with a portion or the entirety of the associated louver 40'.
  • the associated louver 40' is defined as the louver formed with and attached to the adjacent end rib 18a.
  • the formed hem 88 of double thickness provides structural integrity to the fin, both from forces encountered during use of the heat exchanger, and from compression forces incurred during the manufacturing of the heat exchanger.
  • This structural reinforcement is improved further when the end rib 18a is formed in the hemmed area, either partially embedded in the hem 88 or fully embedded in the hem 88.
  • the hem 88 may extend far enough inward to also incorporate the associated louver 40' either partially or fully, increasing the resistance to external forces even further. This embodiment results in exceptional rigidity and provides superior resistance to fin and core damage.
  • Figs. 8-10 shows examples of a rib 82, 86 embedded in the hemmed area wherein the rib 82, 86 has various cross-sectional patterns.
  • Fig. 8 shows a rib 82 having cross-sectional pattern with a sharp peak formed by angled legs 82', 82" with the tip of the peak positioned upward in the same direction as the open edge 85 of the associated louver 40' with respect to the neutral plane 30 of the unformed metal strip 12.
  • Fig. 9 shows a rib 86 having a curved peak 86' with the crest of the peak 86' downward facing, opposite the direction of the open edge 85 of the associated louver 40' and Fig.
  • the 10 has a curved peak 86' with the crest of the peak 86' facing upward in the same direction as the open edge 85 of the associated louver 40'.
  • the variations in the cross sectional patterns of the rib 82, 86, the distance to which the hem 88 extends to or into the rib 82, 86 and associated louver 40', and the direction the peak of the rib 82, 86 faces may be further combined in a multitude of embodiments not specifically described.
  • the ribbing of the hemmed area may also be incorporated into the design and manufacturing of plate-type flat fins.
  • the plate-type fin is hemmed along at least one of the fin edges and includes at least one rib formed in the hemmed area.
  • This embodiment is not formed into a serpentine fin, but remains essentially flat, and gives the plate-type fin resistance to damage during handling of the fins during manufacture and transport and against stresses during use of the heat exchanger core.
  • the fin of the present invention employing a ribbed hem may be made by conventional hard tooling or by air forming.
  • Figs. 11-15 The process of air forming the serpentine split louver fins of the present invention is shown in Figs. 11-15 , and begins by providing a coil of unformed metal strip 12 for continuous feeding through a modified prior art air forming machine 10. If the hemmed edges are to be employed, folding of the unformed metal strip edges 27 to produce hemmed edges 80 may be completed before the metal strip 12 enters the air forming machine 10 or as a step during the process of forming the heat exchanger fin after the metal strip 12 is fed into the air forming machine 10.
  • Fig. 11 shows the partial folding of cut strip edges 27 to a first position 27' and subsequently to the final folded position 27" to form hem 88.
  • the air forming machine 10 comprises a front roller 50 which guides the metal strip 12 through a pair of opposing wiping pads 52, one on each side of the metal strip 12, for cleaning any contamination thereon.
  • a pair of counter rotating fin rolls 60, 62 having a cylindrical shape are positioned downstream from the wiping pads 52 with respect to the metal strip 12. If formation of the hem 88 is to be made in the air forming machine 10, the folding operation may be made immediately after the wiping stage and prior to contact with the fin rolls 60, 62. Fin rolls 60, 62 are sufficiently close to one another to exert a compression force on the surface of the moving metal strip 12 in a direction normal to the strip plane 30, as well as move the strip 12 continuously in direction 21.
  • each of the fin rolls 60, 62 have a plurality of meshing cutter blades and tool patterns 44 which cut and form the split louvers 40 and ribs 18a, 18b in the metal strip, to the configuration shown in Figs. 1-4 .
  • each folding shaft 70, 72 has a plurality of arms extending outward from the axis of rotation, and the ends of the arms are parallel to the strip width. As shown in Fig. 12 , the metal strip contacts arms of the rotating lower folding shaft 72 and upper folding shaft 70, which arms provide an initial backpressure in a direction opposite to the motion of the strip 12 in direction 21.
  • the metal strip 12 contacts one of the lower folding shaft 72 arms forcing an unformed portion 22 into a radius formed between shaft arms, creating the initial backpressure on the metal strip 12 between the backing plate 68 and the lower folding shaft 72.
  • strip 12 begins to buckle along a first unformed portion 22 between backing plate 68 and lower folding shaft 72.
  • the unformed portions 22 of the metal strip 12 have the least amount of structural integrity against forces which tend to make the metal strip 12 bend across its width, while the split louvers 40 and the ribs 18a, 18b inhibit buckling and folding in the louver rows 25.
  • air forming refers to the fact that the folds are made in a controlled fashion in air without the necessity to use male and female tool sections conforming to the desired degree of folding.
  • Fig. 13 shows the result of the initial backpressure causing the metal strip to buckle along the unformed portions creating a fold 22'a in one direction, and to buckle along the unformed portion creating a fold 22'b in the opposite direction.
  • the metal strip 12 moves from backing plate 68 to folding shafts 70, 72, it continues to buckle, and additional folds 22'a, 22'b created along the adjacent unformed portions 22 to create the folds 22', 22' or convolutions in the strip 12 between each row 25 of split louvers 40.
  • the fold angles continue to increase as the strip approaches and passes between the folding shafts 70, 72, as shown in Figs. 14 and 15 , which show the progression of the strip folding.
  • a further backpressure is applied to the convoluted strip 12 by a gathering station downstream of the folding shafts 70, 72, again in a direction opposite to the strip movement direction 21.
  • this gathering station has fingers 96, preferably in the form of a metal brush, mounted on an adjustable lever 98 which sequentially contact the upper folds 22' of the convoluted strip as it passes in direction 21.
  • the force of fingers 96 urges the convoluted strip 12' against a second base portion 48b, and may be adjusted to apply sufficient backpressure to create the desired density of strip convolutions, i.e., the number of straight portions containing split louver fins (between folds 22') in a distance D of formed serpentine fin strip 12'.
  • This fin strip density is typically described as number of fins per inch. Increased backpressure at the gathering station produces a higher fin density, while lower backpressure at the gathering station results in a lower fin density.
  • the air forming process continues until the final fold angle is obtained at folded unformed portions 22' to form the desired number of folds into a length of fin strip 12'.
  • the fin strip 12' is subsequently cut to create the desired number of fins corresponding to the length of the tubes 30 in the heat exchanger core 50.
  • Figs. 16, 17 and 18 show the completed serpentine fin strips 12' integrated with tubes 30 to form heat exchanger core 50. As shown in Fig. 18 , incoming air flowing in direction 35 enters core 50 at leading fin edge 31 and exits at trailing fin edge 33. The serpentine fin strips 12' are stacked in an alternating pattern with the tubes 30, and then compressed and brazed to form the completed core 50.
  • Fig. 16 One particular advantage of the use of ribs with the split louver serpentine fin made by air forming is shown in Fig. 16 with respect to the location of the ends of the individual louvers 40 from adjacent tubes 30. It is desirable to ensure that there is sufficient distance x 1 and x 2 between the louver ends and the tubes 30, so that the fold 22' is confined to the unformed area 22 between louver rows 25, and the ends of the louvers 40 are not distorted, closed or crushed, or the louver angle changed, by the folding process.
  • the present invention of air forming a split louver serpentine fin has been shown to provide such distance to avoid damage to the louvers 40, and more importantly, provide a consistent distance x 1 , x 2 between the louver ends and the tubes 30, preferably where x 1 is substantially equal to x 2 , to permit the as-built heat exchanger to come closer to the theoretical performance of the design.
  • the ribs formed within the split louver give the louver banks more integrity in the structure during the air forming of the convolutions as well as in the production of the radiator core 50 when the tubes 30 and fin strips are stacked and brazed.
  • a serpentine fin which has a hemmed leading edge where the air enters the heat exchanger, and preferably hemmed leading and trailing edges, will provide for a heat exchanger which has greater structural integrity during the manufacturing process and during use.
  • the hemmed edges 80, and particularly the hemmed edges 80 having ribs therein allow for greater compression of the stacked fins and tubes 30 without damaging or distorting the fins.
  • the hemmed edges 80 give the fins protection from distortion or damage from the installer and, in use of the final product, the hemmed edges 80 protect the fins from damage due to road debris, power washing, and repair.
  • the hemmed edges also aid in reinforcing the tubes 30 during pressure cycling of the heat exchanger where the tubes 30 have a tendency to expand or bulge from internal pressure of the heat exchanger.
  • the present invention provides an improved method for manufacturing split louvered serpentine fins using an air-forming process, which is cost-effective, yet produces a quality fin having consistently high efficiency and heat transfer rates.
  • the invention also provides a serpentine fin with a hemmed leading edge and preferably, hemmed leading and trailing edges, including split louvers and reinforcement ribs which add increased structural integrity against forces created during the manufacturing process.
  • Preferably at least one of the ribs is formed partially or fully within the hemmed area to provide exceptional rigidity to the leading and trailing edges of the heat exchanger fin, whether it is serpentine or plate-type.
  • the resulting increased rigidity provides superior resistance to fin and core damage resulting from handling, shipping and installation, and from pressure washing and road debris in use in the vehicle. This increased rigidity permits the use of thinner fin materials while preserving the aforementioned fin resistance to core damage.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Claims (13)

  1. Ailette en serpentin pour l'assemblage entre des tubes (30) dans un faisceau d'échangeur de chaleur, comprenant :
    une bande métallique (12, 12') ayant une largeur entre des bords opposés (27, 27", 80) de la bande et une longueur supérieure à la largeur, les bords (27, 27", 80) de la bande ayant un rebord (88, 88") formé sur ceux-ci et présentant une double épaisseur du matériau de la bande, qui s'étend sur une partie de la distance au bord (27, 27", 80) vers l'intérieur, la bande métallique (12, 12') présentant des plis (22') s'étendant sur la largeur de la bande de telle sorte que la bande (12, 12') forme une configuration en serpentin, les plis (22') étant conçus pour venir en contact avec les tubes (30) dans le faisceau de l'échangeur de chaleur,
    au moins une rangée (25) de lamelles (40, 40') situées entre les plis (22') adjacents,
    caractérisée par
    au moins une rangée (25) de lamelles (40, 40') qui comprend des lamelles subdivisées (40, 40') présentant des ouvertures qui s'étendent dans la direction de la longueur de bande (21) et qui sont formées dans des bordures de lamelle (25a, 25b) espacées adjacentes qui s'étendent sur une partie au moins de la largeur de la bande (12, 12'),
    des nervures (18a, 18b) sensiblement parallèles aux ouvertures des lamelles (40, 40') adjacentes aux bords (27, 27", 80) de la bande et dans au moins une partie centrale de la bande (12, 12') entre les bords (27, 27", 80) de la bande,
    les nervures (18a, 18b) s'étendant sur les bordures (25a, 25b) des lamelles.
  2. Ailette selon la revendication 1, caractérisée en ce que le rebord (88, 88') s'étend sur une partie de la nervure (18a, 18b).
  3. Ailette selon la revendication 1, caractérisée en ce que le rebord (88, 88') s'étend complètement dans la nervure (18a, 18b) et dans la lamelle associée (40, 40').
  4. Ailette selon la revendication 1, caractérisée en ce que les lamelles sont formées sous un angle par rapport à un plan de la bande métallique (12, 12'), et l'angle des lamelles est compris entre environ 26 degrés et environ 32 degrés.
  5. Ailette selon la revendication 1, caractérisée en ce que la bande métallique (12, 12') présente une épaisseur, et les nervures (18a, 18b) présentent une hauteur s'étendant à partir d'un plan de la bande métallique (12, 12'), la relation de la hauteur par rapport à l'épaisseur de la bande métallique (12, 12') étant comprise entre environ 4 et 5.
  6. Procédé de fabrication d'une ailette en serpentin selon l'une des revendications précédentes, comprenant :
    - la mise à disposition d'une bande métallique (12, 12') plate pour réaliser des ailettes d'échangeur de chaleur, la bande (12, 12') ayant une largeur entre des bords opposés (27, 27", 80) de la bande et une longueur supérieure à la largeur, et les bords (27, 27", 80) de la bande ayant un rebord (88, 88") formé sur ceux-ci et présentant une double épaisseur du matériau de la bande, qui s'étend sur une partie de la distance au bord (27, 27", 80) vers l'intérieur;
    - la formation d'une multitude de rangées de lamelles subdivisées (40, 40') dans la bande (12, 12'), la bande (12, 12') étant sensiblement plate, chaque rangée de lamelles (40, 40') comprenant des lamelles présentant des ouvertures qui s'étendent dans la direction de la longueur de bande (21) et qui sont formées dans des bordures de lamelle (25a, 25b) espacées adjacentes qui s'étendent sur une partie au moins de la largeur de la bande (12, 12'), et comprenant au moins une nervure (18a, 18b) formée dans la bande (12, 12") sensiblement parallèlement aux ouvertures des lamelles et s'étendant sur la paire de bordures de lamelle (25a, 25b), la bande métallique (12, 12') ayant des parties non formées s'étendant sur la largeur de la bande entre les rangées de lamelles de bande et au moins une nervure (18a, 18b) pour former des plis (22') sur la largeur de la bande (12, 12') ;
    - suite à la formation des rangées de lamelles subdivisées (40, 40') et pendant le mouvement continu de la bande (12, 12'), l'application d'une contre-pression initiale à la bande métallique (12, 12') par mise en contact de la bande (12, 12') à un premier emplacement (72) pour amener la bande (12, 12') sensiblement plate à se plier dans les parties non formées et à commencer à former des plis (22') dans la bande (12, 12'), avec au moins une rangée de lamelles (40, 40') entre des plis (22') adjacents le long de la longueur de la bande (12, 12') ; et
    - puis l'application d'une contre-pression supplémentaire à la bande métallique (12, 12') par mise en contact de la bande (12, 12') à un second emplacement (96) en aval du premier emplacement par rapport au mouvement de la bande (12, 12'), afin de compléter la formation des plis (22') de la bande (12, 12') pour former l'ailette en serpentin, la distance entre les plis (22') adjacents étant conforme à la distance d'espacement désirée entre les tubes (30) du faisceau de l'échangeur de chaleur.
  7. Procédé selon la revendication 6, caractérisé par la formation de nervures (18a, 18b) adjacentes aux bords (27, 27", 80) de la bande et dans une partie centrale de la bande (12, 12') entre les bords (27, 27", 80) de la bande.
  8. Procédé selon la revendication 6, caractérisé en ce que les lamelles (40, 40') ont des extrémités adjacentes aux parties non formées de la bande métallique (12, 12'), et en ce que suite à l'application de la pression supplémentaire à la bande métallique (12, 12') la distance entre les extrémités des lamelles et les plis (22') au niveau des parties non formées est sensiblement égale.
  9. Procédé selon la revendication 6, caractérisé en ce que la bande métallique (12, 12') présente une épaisseur et ladite au moins une nervure (18a, 18b) présente une hauteur s'étendant à partir d'un plan de la bande métallique (12, 12'), la relation de la hauteur par rapport à l'épaisseur de la bande métallique (12, 12') étant comprise entre environ 4 et 5.
  10. Procédé selon la revendication 6, caractérisé en ce que les lamelles (40, 40') sont formées sous un angle par rapport à un plan de la bande métallique (12, 12'), et l'angle des lamelles est compris entre environ 26 degrés et environ 32 degrés.
  11. Procédé selon la revendication 6, caractérisé en ce que dans la bande métallique plate (12, 12'), chacun des bords opposés (27, 27", 80) de la bande est un bord replié comprenant une double épaisseur de la bande métallique plate (12, 12') s'étendant sur une partie de la distance aux bords (27, 27", 80) vers l'intérieur pour former un rebord (88, 88").
  12. Procédé selon la revendication 11, caractérisé en ce que le rebord (88, 88") s'étend sur une partie de la nervure (18a, 18b).
  13. Procédé selon la revendication 11, caractérisé en ce que le rebord (88, 88") s'étend complètement dans la nervure (18a, 18b) et dans la lamelle associée (40, 40').
EP07853381.7A 2007-01-12 2007-12-14 Ailette d'échangeur de chaleur Not-in-force EP2106520B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/622,512 US7866042B2 (en) 2007-01-12 2007-01-12 Method for producing a split louver heat exchanger fin
US11/770,210 US8408283B2 (en) 2007-06-28 2007-06-28 Heat exchanger fin with ribbed hem
PCT/US2007/025559 WO2008085279A1 (fr) 2007-01-12 2007-12-14 Ailette d'échangeur de chaleur

Publications (3)

Publication Number Publication Date
EP2106520A1 EP2106520A1 (fr) 2009-10-07
EP2106520A4 EP2106520A4 (fr) 2012-08-01
EP2106520B1 true EP2106520B1 (fr) 2014-11-19

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EP (1) EP2106520B1 (fr)
CA (1) CA2672218A1 (fr)
MX (1) MX2009005538A (fr)
WO (1) WO2008085279A1 (fr)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2941040B1 (fr) * 2009-01-15 2012-08-31 Valeo Systemes Thermiques Intercalaire d'echange de chaleur pour un dispositif d'echange de chaleur
CN101846479B (zh) * 2009-03-25 2012-02-22 三花丹佛斯（杭州）微通道换热器有限公司 用于换热器的翅片以及采用该翅片的换热器
CN103299150B (zh) * 2011-01-21 2015-09-16 大金工业株式会社 热交换器和空调机
JP2023072100A (ja) * 2020-04-06 2023-05-24 三菱電機株式会社 熱交換器、熱交換器を搭載した空気調和機、及び熱交換器の製造方法

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Publication number Priority date Publication date Assignee Title
JPS6218583U (fr) * 1985-07-18 1987-02-04
DE4142019A1 (de) 1991-12-19 1993-06-24 Behr Gmbh & Co Wellrippe fuer flachrohrwaermetauscher
JPH06180192A (ja) * 1992-12-08 1994-06-28 Nippondenso Co Ltd 熱交換器
JP2000154989A (ja) * 1998-11-18 2000-06-06 Daikin Ind Ltd 空気熱交換器
JP4456750B2 (ja) 2000-11-10 2010-04-28 株式会社ティラド コルゲートフィン型熱交換器およびその製造方法
JP2002372389A (ja) 2001-06-13 2002-12-26 Denso Corp 熱交換器

Also Published As

Publication number Publication date
EP2106520A1 (fr) 2009-10-07
EP2106520A4 (fr) 2012-08-01
CA2672218A1 (fr) 2008-07-17
MX2009005538A (es) 2009-06-08
WO2008085279A1 (fr) 2008-07-17

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