US20030066635A1 - Turbulator with offset louvers and method of making same - Google Patents
Turbulator with offset louvers and method of making same Download PDFInfo
- Publication number
- US20030066635A1 US20030066635A1 US10/289,047 US28904702A US2003066635A1 US 20030066635 A1 US20030066635 A1 US 20030066635A1 US 28904702 A US28904702 A US 28904702A US 2003066635 A1 US2003066635 A1 US 2003066635A1
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- louvers
- base
- forming
- set forth
- turbulator
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Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 15
- 238000000034 method Methods 0.000 claims description 17
- 239000012530 fluid Substances 0.000 claims description 14
- 238000005219 brazing Methods 0.000 claims description 3
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000005253 cladding Methods 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 229930091051 Arenine Natural products 0.000 description 1
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Images
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
- 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
-
- 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
Definitions
- the present invention relates generally to heat exchangers for motor vehicles and, more specifically, to a turbulator with offset louvers and method of making same for a heat exchanger in a motor vehicle.
- a tube for a heat exchanger such as an oil cooler in a motor vehicle.
- the tube typically carries a first fluid medium in contact with its interior while a second fluid medium contacts its exterior.
- the first fluid medium is oil and the second fluid medium is air.
- corrugated fins or ribs in the interior of the tube to increase the surface area of conductive material available for heat transfer to cause turbulence of the fluid carried in the interior of the tube and to increase the burst strength of the tube.
- One known method of making such a tube is to physically insert a corrugated fin into a generally flattened tube after the tube has been manufactured. This is an extremely difficult process since the corrugated fin to be inserted into the tube is extremely thin and subject to deformation during the insertion process.
- a turbulator for a charged air cooler may be formed by stamping as described above or by roll-forming corrugation, then with a secondary stamping for louvers.
- the present invention is a turbulator with offset louvers for a heat exchanger including a plurality of corrugated fins each having a base extending laterally and longitudinally in a strip.
- the turbulator also includes a plurality of offset louvers spaced along the base and extending longitudinally and generally perpendicular to the base in an alternating manner.
- the offset louvers are rolled in a direction parallel to a longitudinal axis of the strip.
- the present invention is a method of making a turbulator with offset louvers for a heat exchanger.
- the method includes the steps of providing a generally planar strip having a base extending laterally and longitudinally.
- the method also includes the step of forming a plurality of offset louvers spaced along the base and extending generally perpendicular to the base in an alternating manner such that the offset louvers extend in a direction parallel to a longitudinal axis of the strip.
- One advantage of the present invention is that a turbulator with offset louvers is provided for a heat exchanger such as a charge air cooler for a motor vehicle. Another advantage of the present invention is that a method of making a turbulator with offset louvers is provided. Yet another advantage of the present invention is that the method of making the turbulator with off-set louvers uses only roll forming to manufacture the turbulators, which is less costly and increases production through put. Still another advantage of the present invention is that the method of making the turbulator with offset louvers uses roll forming to make turbulator corrugations and cut louvers simultaneously. A further advantage of the present invention is that the method of making the turbulator with offset louvers has the direction of roll forming the same as the strip or fluid direction.
- FIG. 1 is a perspective view of a turbulator with offset louvers, according to the present invention, illustrated in operational relationship with a heat exchanger of a motor vehicle.
- FIG. 2 is a sectional view taken along line 2 - 2 of FIG. 1.
- FIG. 3 is an enlarged partial perspective view of a portion of the turbulator of FIG. 1.
- FIG. 4 is a side elevational view of an apparatus for making the turbulator of FIG. 1.
- FIG. 5 is a front elevational view of the apparatus for making the turbulator of FIG. 1.
- FIG. 6 is a sectional view taken along line 6 - 6 of FIG. 5.
- FIG. 7 is an enlarged view of a portion in circle 7 of FIG. 5.
- FIG. 8 is a perspective view of the turbulator made with the apparatus of FIGS. 4 through 7 before being folded into its final configuration of FIG. 3.
- a heat exchanger 10 for a motor vehicle such as a charge air cooler, oil cooler, evaporator, or condenser
- the heat exchanger 10 includes a plurality of generally parallel tubes 12 extending between oppositely disposed headers 14 , 16 .
- the heat exchanger 10 includes a fluid inlet (not shown) for conducting cooling fluid into the heat exchanger 10 formed in the header 14 and an outlet (not shown) for directing fluid out of the heat exchanger 10 formed in the header 16 .
- the heat exchanger 10 also includes a plurality of convoluted or serpentine fins 18 attached to an exterior of each of the tubes 12 .
- the fins 18 are disposed between each of the tubes 12 .
- the fins 18 serve as a means for conducting heat away from the tubes 12 while providing additional surface area for convective heat transfer by air flowing over the heat exchanger 10 . It should be appreciated that the heat exchanger 10 could be used in other applications besides motor vehicles.
- the tube 12 extends longitudinally and is substantially flat.
- the tube 12 includes a base 20 being generally planar and extending laterally.
- the tube 12 also includes a top 22 spaced from the base 20 a predetermined distance and opposing each other.
- the top 22 is generally planar and extends laterally.
- the tube 12 includes a first side 24 interposed between the base 20 and the top 22 along one side thereof.
- the first side 24 is generally arcuate in shape.
- the tube 12 also includes a second side 26 interposed between the base 20 and the top 22 along the other side and opposing the first side 24 to form a channel 28 .
- the second side 26 is generally arcuate in shape.
- the tube 12 is made of a metal material such as aluminum or an alloy thereof and has a cladding on its inner and outer surfaces for brazing. It should be appreciated that the tube 12 is conventional and known in the art.
- the heat exchanger 10 includes a turbulator, generally indicated at 30 and according to the present invention, disposed within the channel 28 of each of the tubes 12 .
- the turbulator 30 extends laterally and longitudinally in the form of a strip 31 that is folded or corrugated providing a series of fins 32 , between folds or connecting members 33 .
- Each fin 32 of the turbulator 30 has a generally planar base 34 extending laterally a predetermined distance and longitudinally a predetermined distance between the connecting members 33 .
- the base 34 has a predetermined thickness such as between approximately 0.05 millimeters (mm) to approximately 0.25 mm.
- Each fin 32 of the turbulator 30 also has a plurality of louvers 36 spaced laterally along the base 32 and extending longitudinally to turbulate fluid flow through the channel 28 .
- the louvers 36 have generally inverted “U” cross-sectional shape.
- the louvers 36 are offset generally vertically from a plane of the base 32 and extend generally perpendicular to a plane of the base 34 a predetermined distance between approximately 0.3 mm to approximately 1.0 mm.
- the louvers 36 extend longitudinally a predetermined distance such as between approximately 4.0 mm to approximately 11.0 mm in a strip or fluid flow direction.
- the louvers 36 are spaced laterally a predetermined distance between approximately 0.80 mm to approximately 3.0 mm.
- the louvers 36 also extend perpendicular to the plane of the base 34 in an alternating pattern such that one of the louvers 36 extends upwardly and a laterally adjacent louver 36 extends downwardly.
- the louvers 36 are spaced laterally in a row, which is offset from an adjacent longitudinal row of laterally spaced louvers 36 such that in a longitudinal direction one of the louvers 36 extends upwardly and the longitudinally adjacent louver 36 extends downwardly.
- the louvers 36 are formed by roll forming the strip 31 in a direction along its longitudinal length to be described.
- the turbulator 30 is made of a metal material such as aluminum or an alloy thereof and has a cladding on its surfaces for brazing the turbulator 30 to the tube 12 . It should be appreciated that the louvers 36 are brazed to the top 22 and base 20 of the tube 12 . It should also be appreciated that the louvers 36 extend longitudinally generally parallel to the base 34 .
- the apparatus 40 includes a pair of support members 42 spaced longitudinally and extending vertically.
- the support members 42 are secured by suitable means such as fasteners 44 to a support surface 46 .
- the apparatus 40 also includes a first or lower stripper plate 48 disposed adjacent the support members 42 and a second or upper stripper plate 50 disposed adjacent the lower stripper plate 48 .
- the lower and upper stripper plates 48 and 50 are secured to the support members 42 by suitable means such as fasteners 52 .
- the stripper plates 48 and 50 include a recess 54 being generally arcuate in shape with a plurality of channels 56 spaced laterally and extending longitudinally. In the embodiment illustrated, there are nine channels 56 spaced laterally a predetermined distance such as 0.0775 inches.
- the channels 56 have a predetermined width such as 0.025 inches for teeth 62 of rollers 58 , 60 to be described.
- the apparatus 40 includes a pair of rotatable rollers such as an upper roller 58 and a lower roller 60 operatively connected to supporting structure (not shown).
- the upper roller 58 and lower roller 60 are generally circular in shape and have a plurality of teeth 62 extending radially and circumferentially and are spaced circumferentially.
- the upper roller 58 is disposed in the recess 54 of the upper stripper plate 50 such that a portion of the teeth 62 are disposed in the channels 56 of the upper stripper plate 50 .
- the lower roller 60 is disposed in the recess 54 of the lower stripper plate 58 such that a portion of the teeth 62 are disposed in the channels 56 of the lower stripper plate 48 .
- the base 34 of the turbulator 30 is fed into a slot or channel 64 between the upper stripper plate 50 and the lower stripper plate 48 in a longitudinal direction, which is the rolling direction for the upper and lower rollers 58 and 60 .
- the strip 31 is roll-formed to make corrugations similar to that disclosed in U.S. Pat. No. 3,214,954, the disclosure of which is hereby incorporated by reference.
- the teeth 62 of the upper and lower rollers 58 and 60 have a base-forming portion 65 and a protruding or louver-forming portion 66 .
- the louver-forming portion 66 extends axially and radially to form the louvers 36 of the turbulator 30 in one direction.
- the teeth 62 also have a tooth arc 68 and a root tip 70 to form the connecting members 33 between the fins 32 .
- the base-forming portion 65 is disposed laterally between the louver-forming portions 66 to maintain the flat shape of the base 34 of the turbulator 30 .
- the teeth 62 of rollers 58 and 60 engage each other to form the louvers 36 of the turbulator 30 and the flat portion or base 34 between the louvers 36 provide strength and allow a finger (not shown) to strip the turbulator 30 to form a coil or roll. It should also be appreciated that the teeth 62 of the rollers 58 and 60 engage each other to corrugate the fins 32 and form the connecting members 33 between the fins 32 while simultaneously cutting or forming the louvers 36 .
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
A turbulator with offset louvers and method of making the same for a heat exchanger includes a plurality of corrugated fins each having a base extending laterally and longitudinally in a strip. The turbulator also includes a plurality of louvers spaced along the base and extending longitudinally and generally perpendicular to the base in an alternating manner, the louvers being rolled in a direction parallel to a longitudinal axis of the strip.
Description
- The present application is a divisional application of co-pending U.S. patent application Ser. No. 09/739,950, filed Dec. 18, 2000.
- 1. Field of the Invention
- The present invention relates generally to heat exchangers for motor vehicles and, more specifically, to a turbulator with offset louvers and method of making same for a heat exchanger in a motor vehicle.
- 2. Description of the Related Art
- It is known to provide a tube for a heat exchanger such as an oil cooler in a motor vehicle. The tube typically carries a first fluid medium in contact with its interior while a second fluid medium contacts its exterior. Typically, the first fluid medium is oil and the second fluid medium is air. Where a temperature difference exists between the first and second fluid mediums, heat will be transferred between the two via heat conductive walls of the tube.
- It is also known to provide corrugated fins or ribs in the interior of the tube to increase the surface area of conductive material available for heat transfer to cause turbulence of the fluid carried in the interior of the tube and to increase the burst strength of the tube. One known method of making such a tube is to physically insert a corrugated fin into a generally flattened tube after the tube has been manufactured. This is an extremely difficult process since the corrugated fin to be inserted into the tube is extremely thin and subject to deformation during the insertion process.
- It is also known to produce a corrugated fin or turbulator by a stamping process. An example of such a turbulator is disclosed in U.S. Pat. No. 5,560,425. In this patent, the turbulator is made by stamping in a direction parallel to the fluid flow or strip direction of the turbulator and has corrugations in a direction perpendicular to the direction of the flow of the fluid or strip direction.
- It is further known that a turbulator for a charged air cooler (CAC) may be formed by stamping as described above or by roll-forming corrugation, then with a secondary stamping for louvers. Although these methods have worked well, they suffer from the disadvantage that the stamping process does not have a high production through put. Another disadvantage is that the stamping process is relatively expensive. Therefore, there is a need in the art to provide a method of using only roll forming to manufacture tubulators in a relatively less costly manner.
- Accordingly, the present invention is a turbulator with offset louvers for a heat exchanger including a plurality of corrugated fins each having a base extending laterally and longitudinally in a strip. The turbulator also includes a plurality of offset louvers spaced along the base and extending longitudinally and generally perpendicular to the base in an alternating manner. The offset louvers are rolled in a direction parallel to a longitudinal axis of the strip.
- In addition, the present invention is a method of making a turbulator with offset louvers for a heat exchanger. The method includes the steps of providing a generally planar strip having a base extending laterally and longitudinally. The method also includes the step of forming a plurality of offset louvers spaced along the base and extending generally perpendicular to the base in an alternating manner such that the offset louvers extend in a direction parallel to a longitudinal axis of the strip.
- One advantage of the present invention is that a turbulator with offset louvers is provided for a heat exchanger such as a charge air cooler for a motor vehicle. Another advantage of the present invention is that a method of making a turbulator with offset louvers is provided. Yet another advantage of the present invention is that the method of making the turbulator with off-set louvers uses only roll forming to manufacture the turbulators, which is less costly and increases production through put. Still another advantage of the present invention is that the method of making the turbulator with offset louvers uses roll forming to make turbulator corrugations and cut louvers simultaneously. A further advantage of the present invention is that the method of making the turbulator with offset louvers has the direction of roll forming the same as the strip or fluid direction.
- Other features and advantages of the present invention will be readily appreciated, as the same becomes better understood, after reading the subsequent description taken in conjunction with the accompanying drawings.
- FIG. 1 is a perspective view of a turbulator with offset louvers, according to the present invention, illustrated in operational relationship with a heat exchanger of a motor vehicle.
- FIG. 2 is a sectional view taken along line2-2 of FIG. 1.
- FIG. 3 is an enlarged partial perspective view of a portion of the turbulator of FIG. 1.
- FIG. 4 is a side elevational view of an apparatus for making the turbulator of FIG. 1.
- FIG. 5 is a front elevational view of the apparatus for making the turbulator of FIG. 1.
- FIG. 6 is a sectional view taken along line6-6 of FIG. 5.
- FIG. 7 is an enlarged view of a portion in circle7 of FIG. 5.
- FIG. 8 is a perspective view of the turbulator made with the apparatus of FIGS. 4 through 7 before being folded into its final configuration of FIG. 3.
- Referring to the drawings and in particular FIG. 1, one embodiment of a heat exchanger10 for a motor vehicle (not shown), such as a charge air cooler, oil cooler, evaporator, or condenser, is shown. The heat exchanger 10 includes a plurality of generally
parallel tubes 12 extending between oppositely disposedheaders header 14 and an outlet (not shown) for directing fluid out of the heat exchanger 10 formed in theheader 16. The heat exchanger 10 also includes a plurality of convoluted orserpentine fins 18 attached to an exterior of each of thetubes 12. Thefins 18 are disposed between each of thetubes 12. Thefins 18 serve as a means for conducting heat away from thetubes 12 while providing additional surface area for convective heat transfer by air flowing over the heat exchanger 10. It should be appreciated that the heat exchanger 10 could be used in other applications besides motor vehicles. - Referring to FIGS. 1 and 2, the
tube 12 extends longitudinally and is substantially flat. Thetube 12 includes abase 20 being generally planar and extending laterally. Thetube 12 also includes a top 22 spaced from the base 20 a predetermined distance and opposing each other. The top 22 is generally planar and extends laterally. Thetube 12 includes afirst side 24 interposed between thebase 20 and thetop 22 along one side thereof. Thefirst side 24 is generally arcuate in shape. Thetube 12 also includes a second side 26 interposed between thebase 20 and thetop 22 along the other side and opposing thefirst side 24 to form a channel 28. The second side 26 is generally arcuate in shape. Thetube 12 is made of a metal material such as aluminum or an alloy thereof and has a cladding on its inner and outer surfaces for brazing. It should be appreciated that thetube 12 is conventional and known in the art. - Referring to FIGS. 1 through 3 and8, the heat exchanger 10 includes a turbulator, generally indicated at 30 and according to the present invention, disposed within the channel 28 of each of the
tubes 12. In the embodiment illustrated, theturbulator 30 extends laterally and longitudinally in the form of astrip 31 that is folded or corrugated providing a series offins 32, between folds or connectingmembers 33. Eachfin 32 of theturbulator 30 has a generallyplanar base 34 extending laterally a predetermined distance and longitudinally a predetermined distance between the connectingmembers 33. Thebase 34 has a predetermined thickness such as between approximately 0.05 millimeters (mm) to approximately 0.25 mm. Eachfin 32 of theturbulator 30 also has a plurality oflouvers 36 spaced laterally along thebase 32 and extending longitudinally to turbulate fluid flow through the channel 28. Thelouvers 36 have generally inverted “U” cross-sectional shape. Thelouvers 36 are offset generally vertically from a plane of thebase 32 and extend generally perpendicular to a plane of the base 34 a predetermined distance between approximately 0.3 mm to approximately 1.0 mm. Thelouvers 36 extend longitudinally a predetermined distance such as between approximately 4.0 mm to approximately 11.0 mm in a strip or fluid flow direction. Thelouvers 36 are spaced laterally a predetermined distance between approximately 0.80 mm to approximately 3.0 mm. Thelouvers 36 also extend perpendicular to the plane of the base 34 in an alternating pattern such that one of thelouvers 36 extends upwardly and a laterallyadjacent louver 36 extends downwardly. Thelouvers 36 are spaced laterally in a row, which is offset from an adjacent longitudinal row of laterally spacedlouvers 36 such that in a longitudinal direction one of thelouvers 36 extends upwardly and the longitudinallyadjacent louver 36 extends downwardly. Thelouvers 36 are formed by roll forming thestrip 31 in a direction along its longitudinal length to be described. Theturbulator 30 is made of a metal material such as aluminum or an alloy thereof and has a cladding on its surfaces for brazing theturbulator 30 to thetube 12. It should be appreciated that thelouvers 36 are brazed to the top 22 andbase 20 of thetube 12. It should also be appreciated that thelouvers 36 extend longitudinally generally parallel to thebase 34. - Referring to FIGS. 4 through 6, an apparatus, generally indicated at40, is shown for making the
turbulator 30. Theapparatus 40 includes a pair ofsupport members 42 spaced longitudinally and extending vertically. Thesupport members 42 are secured by suitable means such asfasteners 44 to asupport surface 46. Theapparatus 40 also includes a first orlower stripper plate 48 disposed adjacent thesupport members 42 and a second orupper stripper plate 50 disposed adjacent thelower stripper plate 48. The lower andupper stripper plates support members 42 by suitable means such asfasteners 52. Thestripper plates recess 54 being generally arcuate in shape with a plurality ofchannels 56 spaced laterally and extending longitudinally. In the embodiment illustrated, there are ninechannels 56 spaced laterally a predetermined distance such as 0.0775 inches. Thechannels 56 have a predetermined width such as 0.025 inches forteeth 62 ofrollers - As illustrated in FIGS. 4 through 7, the
apparatus 40 includes a pair of rotatable rollers such as anupper roller 58 and alower roller 60 operatively connected to supporting structure (not shown). Theupper roller 58 andlower roller 60 are generally circular in shape and have a plurality ofteeth 62 extending radially and circumferentially and are spaced circumferentially. Theupper roller 58 is disposed in therecess 54 of theupper stripper plate 50 such that a portion of theteeth 62 are disposed in thechannels 56 of theupper stripper plate 50. Thelower roller 60 is disposed in therecess 54 of thelower stripper plate 58 such that a portion of theteeth 62 are disposed in thechannels 56 of thelower stripper plate 48. Thebase 34 of theturbulator 30 is fed into a slot orchannel 64 between theupper stripper plate 50 and thelower stripper plate 48 in a longitudinal direction, which is the rolling direction for the upper andlower rollers strip 31 is roll-formed to make corrugations similar to that disclosed in U.S. Pat. No. 3,214,954, the disclosure of which is hereby incorporated by reference. - As illustrated in FIGS. 6 and 7, the
teeth 62 of the upper andlower rollers portion 65 and a protruding or louver-formingportion 66. The louver-formingportion 66 extends axially and radially to form thelouvers 36 of theturbulator 30 in one direction. Theteeth 62 also have atooth arc 68 and aroot tip 70 to form the connectingmembers 33 between thefins 32. The base-formingportion 65 is disposed laterally between the louver-formingportions 66 to maintain the flat shape of thebase 34 of theturbulator 30. It should be appreciated that theteeth 62 ofrollers louvers 36 of theturbulator 30 and the flat portion orbase 34 between thelouvers 36 provide strength and allow a finger (not shown) to strip theturbulator 30 to form a coil or roll. It should also be appreciated that theteeth 62 of therollers fins 32 and form the connectingmembers 33 between thefins 32 while simultaneously cutting or forming thelouvers 36. - The present invention has been described in an illustrative manner. It is to be understood that the terminology, which has been used, is intended to be in the nature of words of description rather than of limitation.
- Many modifications and variations of the present invention are possible in light of the above teachings. Therefore, within the scope of the appended claims, the present invention may be practiced other than as specifically described.
Claims (15)
1. A method of making a turbulator with offset louvers for a heat exchanger comprising the steps of:
providing a generally planar strip having a base extending laterally and longitudinally;
forming a plurality of corrugated fins each having having a plurality of offset louvers spaced along the base and extending generally perpendicular to the base in an alternating manner such that the offset louvers extend in a direction parallel to a longitudinal axis of the strip.
2. A method as set forth in claim 1 wherein said step of forming comprises roll forming.
3. A method as set forth in claim 1 including the step of providing a pair of rollers and feeding the strip in a direction of rotation of the rollers to form the louvers.
4. A method as set forth in claim 1 wherein said step of forming comprises forming a planar portion laterally between the louvers.
5. A method as set forth in claim 1 wherein said step of forming comprises forming the louvers with a generally inverted “U” cross-sectional shape.
6. A method of making a heat exchanger comprising the steps of:
providing a plurality of tubes;
providing a generally planar strip having a base extending laterally and longitudinally;
forming a plurality of turbulators each having a plurality of corrugated fins with a plurality of louvers spaced laterally and extending generally perpendicular in an alternating manner such that the louvers extend in a direction parallel to a longitudinal axis of the strip;
disposing the turbulator in the tube; and
brazing the tube and the turbulator together.
7. A method as set forth in claim 6 wherein said step of forming comprises roll forming.
8. A method as set forth in claim 7 including the step of providing a pair of rollers and feeding the strip in a direction of rotation of the rollers to form the louvers.
9. A method as set forth in claim 7 wherein said step of forming comprises forming a planar portion laterally between the louvers.
10. A method as set forth in claim 7 wherein said step of forming comprises forming the louvers with a generally inverted “U” cross-sectional shape.
11. A heat exchanger comprising:
a first manifold;
a second manifold spaced from and opposing said first manifold;
a plurality of tubes extending laterally between and in fluid communication with said first manifold and said second manifold; and
a plurality of turbulators, each of said turbulators having a plurality of louvers spaced laterally and extending longitudinally in an alternating manner, said louvers being rolled in a direction parallel to a longitudinal axis thereof, one of said turbulators being disposed in one of said tubes.
12. A heat exchanger as set forth in claim 11 wherein said tube comprises a base, a top spaced from and opposing said base, a first side interposed between said base and said top along one side thereof, and a second side interposed between said base and said top along another side thereof, said base and said top and said first side and said second side forming a channel.
13. A heat exchanger as set forth in claim 12 wherein said turbulator is disposed in said channel.
14. A heat exchanger as set forth in claim 11 wherein said turbulator comprises a plurality of corrugated fins each having a generally planar base extending longitudinally and said louvers spaced laterally and extending longitudinally along said base.
15. A heat exchanger as set forth in claim 14 wherein said louvers extend generally perpendicular to said base a predetermined distance.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US10/289,047 US20030066635A1 (en) | 2000-12-18 | 2002-11-06 | Turbulator with offset louvers and method of making same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/739,950 US20020074109A1 (en) | 2000-12-18 | 2000-12-18 | Turbulator with offset louvers and method of making same |
US10/289,047 US20030066635A1 (en) | 2000-12-18 | 2002-11-06 | Turbulator with offset louvers and method of making same |
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Application Number | Title | Priority Date | Filing Date |
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US09/739,950 Division US20020074109A1 (en) | 2000-12-18 | 2000-12-18 | Turbulator with offset louvers and method of making same |
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US20030066635A1 true US20030066635A1 (en) | 2003-04-10 |
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US09/739,950 Abandoned US20020074109A1 (en) | 2000-12-18 | 2000-12-18 | Turbulator with offset louvers and method of making same |
US10/289,047 Abandoned US20030066635A1 (en) | 2000-12-18 | 2002-11-06 | Turbulator with offset louvers and method of making same |
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US09/739,950 Abandoned US20020074109A1 (en) | 2000-12-18 | 2000-12-18 | Turbulator with offset louvers and method of making same |
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US (2) | US20020074109A1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
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US20050016240A1 (en) * | 2003-06-11 | 2005-01-27 | Peter Zurawel | Method and apparatus for forming a turbulizer |
US20090095456A1 (en) * | 2007-10-04 | 2009-04-16 | Ktm Kuhler Gmbh | Plate heat exchanger |
US7686070B2 (en) | 2005-04-29 | 2010-03-30 | Dana Canada Corporation | Heat exchangers with turbulizers having convolutions of varied height |
US20110232866A1 (en) * | 2010-03-29 | 2011-09-29 | Zaffetti Mark A | Integral cold plate and honeycomb facesheet assembly |
US20160236262A1 (en) * | 2015-02-17 | 2016-08-18 | Denso Corporation | Offset Fin Manufacturing Method And Offset Fin Manufacturing Apparatus |
US11193722B2 (en) * | 2018-05-01 | 2021-12-07 | Dana Canada Corporation | Heat exchanger with multi-zone heat transfer surface |
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SE528278C2 (en) * | 2005-02-17 | 2006-10-10 | Scania Cv Ab | Intercooler |
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US20090242180A1 (en) * | 2008-04-01 | 2009-10-01 | Gonzales Luis A | Tube assembly for heat exchanger |
TWI377333B (en) * | 2009-02-05 | 2012-11-21 | Wistron Corp | Heat dissipation device |
JP6333571B2 (en) * | 2014-02-10 | 2018-05-30 | 三菱重工オートモーティブサーマルシステムズ株式会社 | Offset fin for heat exchanger and refrigerant heat exchanger using the same |
WO2019100170A1 (en) | 2017-11-27 | 2019-05-31 | Dana Canada Corporation | Enhanced heat transfer surface |
US11340027B2 (en) * | 2019-07-15 | 2022-05-24 | Modine Manufacturing Company | Tube for a heat exchanger, and method of making the same |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3214954A (en) * | 1963-02-19 | 1965-11-02 | Ford Motor Co | Roll die |
US4050277A (en) * | 1976-05-18 | 1977-09-27 | Leigh Products, Inc. | Method and equipment for roll forming products of complex shape |
US4464920A (en) * | 1982-10-27 | 1984-08-14 | Artos Engineering Company | Machine for roller forming metal louvers |
US4592271A (en) * | 1985-08-16 | 1986-06-03 | Young Lester L | Louvered vent |
US5078207A (en) * | 1989-08-26 | 1992-01-07 | Nippondenso Co., Ltd. | Heat exchanger and fin for the same |
US5107922A (en) * | 1991-03-01 | 1992-04-28 | Long Manufacturing Ltd. | Optimized offset strip fin for use in contact heat exchangers |
US5509288A (en) * | 1993-09-08 | 1996-04-23 | Nippondenso Co., Ltd. | Forming roller for corrugated fin |
US5816320A (en) * | 1997-01-10 | 1998-10-06 | J.I.T. Engineering, Inc. | Radiator fin construction |
US6032503A (en) * | 1998-11-23 | 2000-03-07 | Modine Manufacturing Company | Method and apparatus for roll forming a plurality of heat exchanger fin strips |
US6371201B1 (en) * | 1996-04-03 | 2002-04-16 | Ford Global Technologies, Inc. | Heat exchanger and method of assembly for automotive vehicles |
-
2000
- 2000-12-18 US US09/739,950 patent/US20020074109A1/en not_active Abandoned
-
2002
- 2002-11-06 US US10/289,047 patent/US20030066635A1/en not_active Abandoned
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3214954A (en) * | 1963-02-19 | 1965-11-02 | Ford Motor Co | Roll die |
US4050277A (en) * | 1976-05-18 | 1977-09-27 | Leigh Products, Inc. | Method and equipment for roll forming products of complex shape |
US4464920A (en) * | 1982-10-27 | 1984-08-14 | Artos Engineering Company | Machine for roller forming metal louvers |
US4592271A (en) * | 1985-08-16 | 1986-06-03 | Young Lester L | Louvered vent |
US5078207A (en) * | 1989-08-26 | 1992-01-07 | Nippondenso Co., Ltd. | Heat exchanger and fin for the same |
US5107922A (en) * | 1991-03-01 | 1992-04-28 | Long Manufacturing Ltd. | Optimized offset strip fin for use in contact heat exchangers |
US5509288A (en) * | 1993-09-08 | 1996-04-23 | Nippondenso Co., Ltd. | Forming roller for corrugated fin |
US6371201B1 (en) * | 1996-04-03 | 2002-04-16 | Ford Global Technologies, Inc. | Heat exchanger and method of assembly for automotive vehicles |
US5816320A (en) * | 1997-01-10 | 1998-10-06 | J.I.T. Engineering, Inc. | Radiator fin construction |
US6032503A (en) * | 1998-11-23 | 2000-03-07 | Modine Manufacturing Company | Method and apparatus for roll forming a plurality of heat exchanger fin strips |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050016240A1 (en) * | 2003-06-11 | 2005-01-27 | Peter Zurawel | Method and apparatus for forming a turbulizer |
US7686070B2 (en) | 2005-04-29 | 2010-03-30 | Dana Canada Corporation | Heat exchangers with turbulizers having convolutions of varied height |
US20090095456A1 (en) * | 2007-10-04 | 2009-04-16 | Ktm Kuhler Gmbh | Plate heat exchanger |
US8418752B2 (en) * | 2007-10-04 | 2013-04-16 | Mahle International Gmbh | Plate heat exchanger having a turbulence generator |
US20110232866A1 (en) * | 2010-03-29 | 2011-09-29 | Zaffetti Mark A | Integral cold plate and honeycomb facesheet assembly |
US20160236262A1 (en) * | 2015-02-17 | 2016-08-18 | Denso Corporation | Offset Fin Manufacturing Method And Offset Fin Manufacturing Apparatus |
US10220431B2 (en) * | 2015-02-17 | 2019-03-05 | Denso Corporation | Offset fin manufacturing method and offset fin manufacturing apparatus |
US11193722B2 (en) * | 2018-05-01 | 2021-12-07 | Dana Canada Corporation | Heat exchanger with multi-zone heat transfer surface |
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US20020074109A1 (en) | 2002-06-20 |
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