EP0384612A2 - In tank oil cooler - Google Patents
In tank oil cooler Download PDFInfo
- Publication number
- EP0384612A2 EP0384612A2 EP90301265A EP90301265A EP0384612A2 EP 0384612 A2 EP0384612 A2 EP 0384612A2 EP 90301265 A EP90301265 A EP 90301265A EP 90301265 A EP90301265 A EP 90301265A EP 0384612 A2 EP0384612 A2 EP 0384612A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- plate
- plates
- heat exchanger
- dimples
- central portion
- 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.)
- Withdrawn
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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
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated 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
- F28F3/04—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element
- F28F3/042—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of local deformations of the element
- F28F3/044—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being integral with the element in the form of local deformations of the element the deformations being pontual, e.g. dimples
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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
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0031—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
- F28D9/0043—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another
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- 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
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/008—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
- F28D2021/0089—Oil coolers
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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
- F28F2275/00—Fastening; Joining
- F28F2275/04—Fastening; Joining by brazing
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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
- F28F2275/00—Fastening; Joining
- F28F2275/12—Fastening; Joining by methods involving deformation of the elements
- F28F2275/122—Fastening; Joining by methods involving deformation of the elements by crimping, caulking or clinching
Definitions
- This invention relates to heat exchangers, and in particular, to automotive oil coolers which are located inside other heat exchangers, such as automotive radiators.
- the oil coolers of the type in question which have been mounted inside automotive radiators have consisted of concentric tubes closed at both ends to form an internal passage for the oil.
- the engine coolant flows around the outside tube and through the inside tube.
- a difficulty with this type of oil cooler is that it has relatively low heat transfer efficiency. Also, the pressure drop of the oil flowing through the oil cooler is relatively high.
- the present invention is a plate type heat exchanger which has higher efficiency and less pressure drop, and yet is strong enough to withstand the high oil pressures that are frequently encountered in such engine oil or transmission fluid cooling systems.
- a heat exchanger comprising a plurality of stacked plates arranged in pairs, each of the pairs including first and second plates.
- the first plate has a planar central portion, a raised peripheral co-planar edge portion extending above the central portion, and opposed co-planar end bosses extending below the central portion.
- the second plate of each plate pair has a peripheral edge portion joined to the first plate peripheral edge portion and a central portion spaced from the first plate central portion.
- a planar turbulizer is located between the first and second plate central portions in contact therewith.
- the first plate central portion has a plurality of spaced-apart dimples formed therein, the dimples extending below the central portion equidistant with the end bosses.
- the first plates of two plate pairs are located back-to-back with the respective dimples and end bosses joined together. Also, each plate pair defines inlet and outlet openings for the flow of fluid through the plate pair past the turbulizer.
- a method of making a heat exchanger comprising the steps of providing a plurality of plates, each having a planar central portion with spaced-apart dimples formed therein, a raised peripheral edge portion with spaced-apart tabs projecting outwardly therefrom, and opposed bosses defining inlet and outlet openings at respective opposed plate end portions, said dimples and bosses being located in a common plane.
- the plates are arranged face-to-face in pairs having a hollow space therebetween.
- a turbulizer is inserted into the hollow space, the turbulizer being in contact with the planar central portions of each plate of a plate pair.
- the tabs of one plate are crimped over the peripheral edge portion of the other plate of each plate pair.
- a plurality of the crimped plate pairs is stacked so that the inlet and outlet openings are in registration and the bosses and dimples of adjacent plates are in contact. Also, the contacting areas of the plates and turbulizers are joined to form a fluid tight assembly.
- a heat exchanger comprising a plurality of stacked plates arranged in pairs, each of said pairs including first and second plates, the first plate having a planar central portion and a raised peripheral co-planar edge portion extending above the central portion.
- the second plate of each plate pair has a peripheral edge portion joined to the first plate peripheral edge portion and a central portion spaced from the first plate central portion.
- a planar turbulizer is located between the first and second plate central portions in contact therewith.
- the first and second plates each have two tabs, one tab being located at each of respectively diametrically opposed corners of the plate and being crimped over the peripheral edge portion of the respective other plate of each plate pair.
- the tabs on the first and second plates are located such that tabs are positioned at all four corners of the assembled plate pair.
- each plate pair defines inlet and outlet openings for the flow of fluid through the plate pair past the turbulizer.
- a method of making a heat exchanger comprising the steps of providing a plurality of plates each having a planar central portion, a raised peripheral edge portion with spaced-apart tabs projecting outwardly therefrom and inlet and outlet openings formed therein.
- the plates are arranged face-to-face into pairs having a hollow space therebetween.
- a turbulizer is inserted into the hollow space, the turbulizer being in contact with the planar central portions of each plate of a plate pair.
- the tabs of one plate are crimped over the peripheral edge portion of the other plate of each plate pair.
- a plurality of said crimped plate pairs is stacked so that the inlet and outlet openings are in registration. Also, the contacting areas of the plates and turbulizers are joined to form a fluid tight assembly.
- an oil cooler or heat exchanger 10 is generally represented by reference numeral 10 in Figure 1.
- Heat exchanger 10 is formed of a plurality of plate pairs 12 as described in detail below with reference to Figure 2.
- a top plate pair 14 has a smooth top plate 16 and a bottom plate pair 18 has a smooth bottom plate 20, although top and bottom plates 16, 20 could be dimpled as shown in Figure 2 if desired.
- Heat exchanger 10 also had threaded nipples 22 swaged in place in suitable circular openings in top plate 16.
- One nipple 22 serves as an inlet and the other nipple 22 serves as an outlet for flow of oil, such as engine oil or transmission fluid through heat exchanger 10.
- Plate pair 12 includes a first plate 24 and a second plate 26.
- First plate 24 has a planar central portion 28, a raised peripheral, co-planar edge portion 30 which extends above or is located in a plane above central portion 28.
- First plate 24 also includes opposed, co-planar end bosses 32 extending below or located at a lower level than central portion 28.
- first and second plates 24, 26 are identical, so the terms "below” and “above” with reference to the central portion 28 of first plate 24 would, of course, be reversed with reference to the central portion 28 of second plate 26 as seen in Figure 2.
- the ends of plates 16, 20, 24 and 26 are rounded and end bosses 32 of plates 24, 26 are formed with "D"-shaped openings 34.
- smooth top plate 16 has circular openings to accommodate nipples 22.
- the smooth bottom plate 20 has no openings formed therein.
- First and second plates 24, 26 are formed with a plurality of spaced-apart dimples 36 formed therein. With reference to first plate 24, dimples 36 extend below the central portion 28 equidistant or to the same planar level as end bosses 32, so that when two of the plates 24, 26 are located back-to-back as seen best in Figure 3, the respective dimples 36 and end bosses 32 are joined together along a common plane.
- a turbulizer 38 is located inside each plate pair, including top and bottom plate pairs 14, 18.
- Turbulizer 38 is a strip of expanded metal. The preferred configuration is parallel rows shaped in a sinusoidal configuration, although other configurations could be used as desired.
- the length of turbulizer 38 corresponds with the length of the plate central portions 28, and the width of turbulizer 38 corresponds with the distance between peripheral edge portions 30.
- the thickness of turbulizer 38 is such that after the plate pairs are assembled and heat exchanger 10 is joined together, such as by brazing, the plate central portions 28 are joined to and in good thermal contact with turbulizer 38, as discussed further below.
- Dimples 36 are spaced uniformly over the plate central portions 28.
- One of the primary functions of dimples 36 is to support the plate central portions 28 and prevent these central portions from sagging when the plates are heated to brazing temperatures.
- Central portions 28 must be kept flat and in full contact with turbulizer 38 during the brazing process in order to obtain good thermal contact between the turbulizer and the plates.
- Dimples 36 preferably are large enough to result in flat top surfaces to give a good joint between mating dimples 36. As seen best in Figures 3 and 4, the radius of the shoulders in the dimples should be such that sharp corners should be avoided or the dimples could break out as a result of high pressures in heat exchanger 10.
- Dimples 36 should also not be too large in diameter, because the surface area of central portion 28 occupied by dimples 36 is area that is not in contact with turbulizer 38 and this detracts from the heat transfer efficiency of heat exchanger 10. It will be apparent to those skilled in the art that the number and size of the dimples 36 should be chosen so that sufficient strength and structural support for the plate central portions is provided during the brazing process, and that this must be balanced against loss of heat transfer efficiency by making the dimples too numerous or too large.
- plates 24, 26 are formed with tabs 40 at opposed ends.
- Tabs 40 are located at respective diametrically opposed “corners” of each plate, so that upon assembly, the tabs 40 on one plate, such as first plate 24, are crimped over the peripheral edge portion 30 of the mating plate, such as second plate 26, as seen best in Figure 1. This prevents the plates of each plate pair from moving longitudinally or transversely relative to each other. The crimped plate pairs thus become sub-assemblies to be stacked to complete heat exchanger 10 as described next below.
- the assembly of heat exchanger 10 starts by arranging the plates face-to-face into pairs, so that the respective peripheral edge portions 30 are in registration.
- a turbulizer 38 is then inserted in the hollow space between the central portions 28 of each plate pair.
- Tabs 40 are then crimped over the peripheral edge portions 30 of the respective mating plate.
- the top plate pair 14 is formed by swaging nipples 22 onto smooth top plate 16 and assembling this to one of the plates as shown in Figure 2, again by crimping over tabs 40.
- Bottom plate pair 18 is then formed using a smooth bottom plate 20 mated to another of the plates as shown in Figure 2 and crimping over the respective tabs 40.
- the entire assembly is then placed in a brazing furnace to simultaneously braze together all mating surfaces.
- Nipples 22 and turbulizer 38 are formed of plain aluminum, and plates 16, 20, 24 and 26 are formed of self-brazing aluminum, which is aluminum that has a lower melting point cladding or aluminum brazing alloy layer on the outer surfaces which on each side is about 10% of the thickness of the plate.
- the thickness of turbulizer 38 is such that as this cladding layer melts during the brazing process, all of high areas of turbulizer 38 are brazed to the plate central portions 28 with good thermal heat transfer and minimum drag or pressure drop as the oil flows through or past turbulizers 38.
- heat exchange 10 can be made from other materials than aluminum, such as stainless steel or brass. In the case of stainless steel, copper would be used as the brazing cladding layer. Obviously, any number of plate pairs could be used.
- the length of the plates can be varied simply by repeating longitudinally the dimple diameter and spacing described above. If both the length and the width of the heat exchanger is to be varied, the diameter and spacing of the dimples may have to be varied slightly in keeping with the parameters discussed above.
- the oil cooler of the present invention is a relatively high efficiency heat exchanger which is structurally strong with relatively low pressure drop.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
Description
- This invention relates to heat exchangers, and in particular, to automotive oil coolers which are located inside other heat exchangers, such as automotive radiators.
- In motor vehicles, it is common to provide heat exchangers for cooling engine oil or transmission fluid. Due to the heat transfer characteristics of oil, liquid cooled heat exchangers are normally used as opposed to air cooled exchangers. The most convenient way to do this is to mount the oil cooler or heat exchanger inside the cooling system of the motor vehicle, and in particular, inside the radiator.
- In the past, the oil coolers of the type in question which have been mounted inside automotive radiators have consisted of concentric tubes closed at both ends to form an internal passage for the oil. The engine coolant flows around the outside tube and through the inside tube. A difficulty with this type of oil cooler, however, is that it has relatively low heat transfer efficiency. Also, the pressure drop of the oil flowing through the oil cooler is relatively high.
- The present invention is a plate type heat exchanger which has higher efficiency and less pressure drop, and yet is strong enough to withstand the high oil pressures that are frequently encountered in such engine oil or transmission fluid cooling systems.
- According to the invention, there is provided a heat exchanger comprising a plurality of stacked plates arranged in pairs, each of the pairs including first and second plates. The first plate has a planar central portion, a raised peripheral co-planar edge portion extending above the central portion, and opposed co-planar end bosses extending below the central portion. The second plate of each plate pair has a peripheral edge portion joined to the first plate peripheral edge portion and a central portion spaced from the first plate central portion. A planar turbulizer is located between the first and second plate central portions in contact therewith. The first plate central portion has a plurality of spaced-apart dimples formed therein, the dimples extending below the central portion equidistant with the end bosses. The first plates of two plate pairs are located back-to-back with the respective dimples and end bosses joined together. Also, each plate pair defines inlet and outlet openings for the flow of fluid through the plate pair past the turbulizer.
- According to another aspect of the invention, there is provided a method of making a heat exchanger comprising the steps of providing a plurality of plates, each having a planar central portion with spaced-apart dimples formed therein, a raised peripheral edge portion with spaced-apart tabs projecting outwardly therefrom, and opposed bosses defining inlet and outlet openings at respective opposed plate end portions, said dimples and bosses being located in a common plane. The plates are arranged face-to-face in pairs having a hollow space therebetween. A turbulizer is inserted into the hollow space, the turbulizer being in contact with the planar central portions of each plate of a plate pair. The tabs of one plate are crimped over the peripheral edge portion of the other plate of each plate pair. A plurality of the crimped plate pairs is stacked so that the inlet and outlet openings are in registration and the bosses and dimples of adjacent plates are in contact. Also, the contacting areas of the plates and turbulizers are joined to form a fluid tight assembly.
- According to yet another aspect of the invention, there is provided a heat exchanger comprising a plurality of stacked plates arranged in pairs, each of said pairs including first and second plates, the first plate having a planar central portion and a raised peripheral co-planar edge portion extending above the central portion. The second plate of each plate pair has a peripheral edge portion joined to the first plate peripheral edge portion and a central portion spaced from the first plate central portion. A planar turbulizer is located between the first and second plate central portions in contact therewith. The first and second plates each have two tabs, one tab being located at each of respectively diametrically opposed corners of the plate and being crimped over the peripheral edge portion of the respective other plate of each plate pair. The tabs on the first and second plates are located such that tabs are positioned at all four corners of the assembled plate pair. Also, each plate pair defines inlet and outlet openings for the flow of fluid through the plate pair past the turbulizer.
- According to yet another aspect of the invention, there is provided a method of making a heat exchanger comprising the steps of providing a plurality of plates each having a planar central portion, a raised peripheral edge portion with spaced-apart tabs projecting outwardly therefrom and inlet and outlet openings formed therein. The plates are arranged face-to-face into pairs having a hollow space therebetween. A turbulizer is inserted into the hollow space, the turbulizer being in contact with the planar central portions of each plate of a plate pair. The tabs of one plate are crimped over the peripheral edge portion of the other plate of each plate pair. A plurality of said crimped plate pairs is stacked so that the inlet and outlet openings are in registration. Also, the contacting areas of the plates and turbulizers are joined to form a fluid tight assembly.
- A preferred embodiment of the invention will now be described, by way of example, with reference to the accompanying drawings, in which:
- Figure 1 is a perspective view of a preferred embodiment of an in tank oil cooler according to the present invention;
- Figure 2 is an exploded perspective view of a plate pair sub-assembly;
- Figure 3 is a sectional view taken along lines 3-3 of Figure 1; and
- Figure 4 is a sectional view taken along lines 4-4 of Figure 1.
- Referring to the drawings, an oil cooler or
heat exchanger 10 is generally represented byreference numeral 10 in Figure 1.Heat exchanger 10 is formed of a plurality ofplate pairs 12 as described in detail below with reference to Figure 2. Atop plate pair 14 has asmooth top plate 16 and abottom plate pair 18 has asmooth bottom plate 20, although top andbottom plates Heat exchanger 10 also had threadednipples 22 swaged in place in suitable circular openings intop plate 16. One nipple 22 serves as an inlet and theother nipple 22 serves as an outlet for flow of oil, such as engine oil or transmission fluid throughheat exchanger 10. - Referring in particular to Figure 2, a
typical plate pair 12 is shown in an exploded perspective view.Plate pair 12 includes afirst plate 24 and asecond plate 26.First plate 24 has a planarcentral portion 28, a raised peripheral,co-planar edge portion 30 which extends above or is located in a plane abovecentral portion 28.First plate 24 also includes opposed,co-planar end bosses 32 extending below or located at a lower level thancentral portion 28. - In the preferred embodiment, the first and
second plates central portion 28 offirst plate 24 would, of course, be reversed with reference to thecentral portion 28 ofsecond plate 26 as seen in Figure 2. - The ends of
plates end bosses 32 ofplates shaped openings 34. As mentioned above,smooth top plate 16 has circular openings to accommodatenipples 22. Thesmooth bottom plate 20 has no openings formed therein. - First and
second plates dimples 36 formed therein. With reference tofirst plate 24, dimples 36 extend below thecentral portion 28 equidistant or to the same planar level asend bosses 32, so that when two of theplates respective dimples 36 andend bosses 32 are joined together along a common plane. - A
turbulizer 38 is located inside each plate pair, including top andbottom plate pairs turbulizer 38 corresponds with the length of the platecentral portions 28, and the width ofturbulizer 38 corresponds with the distance betweenperipheral edge portions 30. The thickness ofturbulizer 38 is such that after the plate pairs are assembled andheat exchanger 10 is joined together, such as by brazing, the platecentral portions 28 are joined to and in good thermal contact withturbulizer 38, as discussed further below. -
Dimples 36 are spaced uniformly over the platecentral portions 28. One of the primary functions ofdimples 36 is to support the platecentral portions 28 and prevent these central portions from sagging when the plates are heated to brazing temperatures.Central portions 28 must be kept flat and in full contact withturbulizer 38 during the brazing process in order to obtain good thermal contact between the turbulizer and the plates. -
Dimples 36 preferably are large enough to result in flat top surfaces to give a good joint betweenmating dimples 36. As seen best in Figures 3 and 4, the radius of the shoulders in the dimples should be such that sharp corners should be avoided or the dimples could break out as a result of high pressures inheat exchanger 10. -
Dimples 36 should also not be too large in diameter, because the surface area ofcentral portion 28 occupied bydimples 36 is area that is not in contact withturbulizer 38 and this detracts from the heat transfer efficiency ofheat exchanger 10. It will be apparent to those skilled in the art that the number and size of thedimples 36 should be chosen so that sufficient strength and structural support for the plate central portions is provided during the brazing process, and that this must be balanced against loss of heat transfer efficiency by making the dimples too numerous or too large. It has been found that for plates withcentral portions 28 of approximately four centimetres in width, dimples that are 0.5 centimetres in diameter and spaced-apart longitudinally, about 2.5 centimetres and transversely about 2 centimetres provides a preferred balance where aluminum of 0.08 centimetres thickness is used for the plates. - Referring again to Figure 2,
plates tabs 40 at opposed ends.Tabs 40 are located at respective diametrically opposed "corners" of each plate, so that upon assembly, thetabs 40 on one plate, such asfirst plate 24, are crimped over theperipheral edge portion 30 of the mating plate, such assecond plate 26, as seen best in Figure 1. This prevents the plates of each plate pair from moving longitudinally or transversely relative to each other. The crimped plate pairs thus become sub-assemblies to be stacked to completeheat exchanger 10 as described next below. - The assembly of
heat exchanger 10 starts by arranging the plates face-to-face into pairs, so that the respectiveperipheral edge portions 30 are in registration. Aturbulizer 38 is then inserted in the hollow space between thecentral portions 28 of each plate pair.Tabs 40 are then crimped over theperipheral edge portions 30 of the respective mating plate. Several of these assembled plate pairs are then stacked so that the "D"-shapedopenings 34 are in registration. Thetop plate pair 14 is formed by swagingnipples 22 onto smoothtop plate 16 and assembling this to one of the plates as shown in Figure 2, again by crimping overtabs 40.Bottom plate pair 18 is then formed using asmooth bottom plate 20 mated to another of the plates as shown in Figure 2 and crimping over therespective tabs 40. The entire assembly is then placed in a brazing furnace to simultaneously braze together all mating surfaces. - In the preferred embodiment, aluminum is used for all of the components of
heat exchanger 10.Nipples 22 andturbulizer 38 are formed of plain aluminum, andplates turbulizer 38 is such that as this cladding layer melts during the brazing process, all of high areas ofturbulizer 38 are brazed to the platecentral portions 28 with good thermal heat transfer and minimum drag or pressure drop as the oil flows through orpast turbulizers 38. - Having described preferred embodiments of the invention, it will be appreciated that various modifications may be made to the structures described. For example,
heat exchange 10 can be made from other materials than aluminum, such as stainless steel or brass. In the case of stainless steel, copper would be used as the brazing cladding layer. Obviously, any number of plate pairs could be used. The length of the plates can be varied simply by repeating longitudinally the dimple diameter and spacing described above. If both the length and the width of the heat exchanger is to be varied, the diameter and spacing of the dimples may have to be varied slightly in keeping with the parameters discussed above. - From the above, it will be appreciated that the oil cooler of the present invention is a relatively high efficiency heat exchanger which is structurally strong with relatively low pressure drop.
Claims (15)
a plurality of stacked plates arranged in pairs (12), each of said pairs including first and second plates (24, 26), the first plate (24) having a planar central portion (28), a raised peripheral co-planar edge portion (30) extending above the central portion, and opposed co-planar end bosses (32) extending below the central portion;
the second plate (26) of each plate pair having a peripheral edge portion (30) joined to said first plate peripheral edge portion and a central portion (28) spaced from the first plate central portion;
a planar turbulizer (38) located between the first and second plate central portions (28) in contact therewith;
the first plate central portion having a plurality of spaced-apart dimples (36) formed therein, the dimples extending below the central portion (28) equidistant with the end bosses (30); the first plates (24) of two plate pairs being located back-to-back with the respective dimples (36) and end bosses (30) joined together; and
each plate pair (12) defining inlet and outlet openings (34) for the flow of fluid through the plate pair past the turbulizer.
a plurality of stacked plates arranged in pairs (12), each of said pairs including first and second plates (24, 26), the first plate (24) having a planar central portion (28) and a raised peripheral co-planar edge portion (30) extending above the central portion;
the second plate (26) of each plate pair having a peripheral edge portion (30) joined to said first plate peripheral edge portion (30) and a central portion (28) spaced from the first plate central portion;
a planar turbulizer (38) located between the first and second plate central portions (28) in contact therewith;
the first and second plates each having two tabs (40), one tab being located at each of respectively diametrically opposed corners of the plate and being crimped over the peripheral edge portion of the respective other plate of each plate pair, the tabs on the first and second plates being located such that tabs are positioned at all four corners of the assembled plate pair; and each plate pair defining inlet and outlet openings (34) for the flow of fluid through the plate pair past the turbulizer.
providing a plurality of plates (24, 26) each having a planar central portion (28), a raised peripheral edge portion (30) with spaced-apart tabs (40) projecting outwardly therefrom and inlet and outlet openings (34) formed therein;
inserting turbulizers (38) into the hollow spaces of between face to face pairs of plates, each turbulizer being in contact with the planar central portions of each plate of a plate pair;
crimping the tabs (40) of one plate over the peripheral edge portion of the other plate of each plate pair;
stacking a plurality of said crimped plate pairs (12) so that said inlet and outlet openings are in registration; and
joining the contacting areas of the plates and turbulizers to form a fluid tight assembly.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA000592041A CA1313182C (en) | 1989-02-24 | 1989-02-24 | In tank oil cooler |
CA592041 | 1989-02-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0384612A2 true EP0384612A2 (en) | 1990-08-29 |
EP0384612A3 EP0384612A3 (en) | 1990-11-07 |
Family
ID=4139688
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19900301265 Withdrawn EP0384612A3 (en) | 1989-02-24 | 1990-02-01 | In tank oil cooler |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0384612A3 (en) |
JP (2) | JPH02242089A (en) |
KR (2) | KR0170392B1 (en) |
CA (1) | CA1313182C (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993010415A1 (en) * | 1991-11-15 | 1993-05-27 | Long Manufacturing Ltd. | In tank oil cooler |
EP0622600A1 (en) * | 1993-04-24 | 1994-11-02 | Knecht Filterwerke Gmbh | Flat plate oil cooler assembly |
EP0666461A1 (en) * | 1994-02-04 | 1995-08-09 | Behr GmbH & Co. | Pipe connection for a water casing of a motor vehicle heat exchanger |
WO1995033967A1 (en) * | 1994-06-06 | 1995-12-14 | Valeo Engine Cooling Ab | Heat exchanger for fitting in a tank which forms part of a vehicle radiator |
DE19624358A1 (en) * | 1996-06-19 | 1998-01-02 | Mann & Hummel Filter | Heat exchanger |
WO1999046549A1 (en) * | 1998-03-10 | 1999-09-16 | Alfa Laval Ab | A plate heat exchanger with a connection member |
EP1122505A1 (en) * | 1998-10-15 | 2001-08-08 | Ebara Corporation | Plate type heat exchanger |
US7708884B2 (en) | 2005-04-22 | 2010-05-04 | Leonhard Fuchs | Process for aerobic-thermophilic stabilization and disinfection of sludge |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0622770U (en) * | 1992-07-30 | 1994-03-25 | 東洋ラジエーター株式会社 | Multi-plate oil cooler |
JP2006097927A (en) * | 2004-09-28 | 2006-04-13 | Tokyo Roki Co Ltd | Heat exchanger for internal combustion engine |
KR101006597B1 (en) * | 2008-08-12 | 2011-01-07 | 주식회사 경동나비엔 | Heat exchanger |
JP6329756B2 (en) * | 2013-11-26 | 2018-05-23 | 株式会社マーレ フィルターシステムズ | Oil cooler |
JP2022070491A (en) * | 2020-10-27 | 2022-05-13 | 有限会社和氣製作所 | Heat exchanger |
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US4470455A (en) * | 1978-06-19 | 1984-09-11 | General Motors Corporation | Plate type heat exchanger tube pass |
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JPS587071U (en) * | 1981-06-30 | 1983-01-18 | 株式会社 土屋製作所 | Multi-plate oil cooler for automobile gasoline engine |
JPS6184325A (en) * | 1984-09-28 | 1986-04-28 | Aichi Steel Works Ltd | Working heat treatment and its apparatus |
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- 1989-02-24 CA CA000592041A patent/CA1313182C/en not_active Expired - Lifetime
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- 1990-02-01 EP EP19900301265 patent/EP0384612A3/en not_active Withdrawn
- 1990-02-21 JP JP2040844A patent/JPH02242089A/en active Pending
- 1990-02-24 KR KR1019900002359A patent/KR0170392B1/en not_active IP Right Cessation
- 1990-02-24 KR KR1019900002358A patent/KR960005784B1/en not_active IP Right Cessation
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US2287281A (en) * | 1940-07-30 | 1942-06-23 | Servel Inc | Refrigeration |
FR1516735A (en) * | 1966-01-22 | 1968-02-05 | Snecma | Improvements to plate heat exchangers |
FR2280871A1 (en) * | 1974-08-01 | 1976-02-27 | Chausson Usines Sa | Built-up construction heat exchanger - has panels with peripheral support surface and embossed crown sections |
FR2428809A1 (en) * | 1978-06-14 | 1980-01-11 | Piemontese Radiatori | PLATE HEAT EXCHANGER |
US4470455A (en) * | 1978-06-19 | 1984-09-11 | General Motors Corporation | Plate type heat exchanger tube pass |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1993010415A1 (en) * | 1991-11-15 | 1993-05-27 | Long Manufacturing Ltd. | In tank oil cooler |
AU670760B2 (en) * | 1991-11-15 | 1996-08-01 | Long Manufacturing Ltd. | In tank oil cooler |
EP0622600A1 (en) * | 1993-04-24 | 1994-11-02 | Knecht Filterwerke Gmbh | Flat plate oil cooler assembly |
EP0666461A1 (en) * | 1994-02-04 | 1995-08-09 | Behr GmbH & Co. | Pipe connection for a water casing of a motor vehicle heat exchanger |
US5524938A (en) * | 1994-02-04 | 1996-06-11 | Behr Gmbh & Co. | Tube connection for a water box of a motor vehicle heat exchanger |
WO1995033967A1 (en) * | 1994-06-06 | 1995-12-14 | Valeo Engine Cooling Ab | Heat exchanger for fitting in a tank which forms part of a vehicle radiator |
DE19624358A1 (en) * | 1996-06-19 | 1998-01-02 | Mann & Hummel Filter | Heat exchanger |
DE19624358B4 (en) * | 1996-06-19 | 2005-07-14 | Mann + Hummel Gmbh | heat exchangers |
WO1999046549A1 (en) * | 1998-03-10 | 1999-09-16 | Alfa Laval Ab | A plate heat exchanger with a connection member |
EP1122505A1 (en) * | 1998-10-15 | 2001-08-08 | Ebara Corporation | Plate type heat exchanger |
EP1122505A4 (en) * | 1998-10-15 | 2002-07-10 | Ebara Corp | Plate type heat exchanger |
US6681844B1 (en) | 1998-10-15 | 2004-01-27 | Ebara Corporation | Plate type heat exchanger |
US7708884B2 (en) | 2005-04-22 | 2010-05-04 | Leonhard Fuchs | Process for aerobic-thermophilic stabilization and disinfection of sludge |
Also Published As
Publication number | Publication date |
---|---|
JPH081423U (en) | 1996-09-27 |
CA1313182C (en) | 1993-01-26 |
KR900013278A (en) | 1990-09-05 |
KR0170392B1 (en) | 1999-03-20 |
KR900013279A (en) | 1990-09-05 |
JP2590256Y2 (en) | 1999-02-10 |
KR960005784B1 (en) | 1996-05-01 |
JPH02242089A (en) | 1990-09-26 |
EP0384612A3 (en) | 1990-11-07 |
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