+

US20060131006A1 - Heat exchanger and ribs - Google Patents

Heat exchanger and ribs Download PDF

Info

Publication number
US20060131006A1
US20060131006A1 US11/303,483 US30348305A US2006131006A1 US 20060131006 A1 US20060131006 A1 US 20060131006A1 US 30348305 A US30348305 A US 30348305A US 2006131006 A1 US2006131006 A1 US 2006131006A1
Authority
US
United States
Prior art keywords
rib
heat exchanger
thickness
ribs
edge 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.)
Abandoned
Application number
US11/303,483
Inventor
Viktor Brost
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.)
Modine Manufacturing Co
Original Assignee
Modine Manufacturing Co
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
Application filed by Modine Manufacturing Co filed Critical Modine Manufacturing Co
Publication of US20060131006A1 publication Critical patent/US20060131006A1/en
Assigned to MODINE MANUFACTURING COMPANY reassignment MODINE MANUFACTURING COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BROST, VIKTOR
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular 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
    • F28F1/126Tubular 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2225/00Reinforcing means

Definitions

  • the present invention is directed toward heat exchanger ribs, and more particularly toward ribs through which a gaseous medium flows in order to exchange heat with another medium.
  • Heat exchangers having ribs through which gas flows to exchange heat with another medium are old.
  • the ribs contact tubes or the like through which the other medium flows, wherein heat is passed from one medium to the other via flow of the media over the tube walls and the ribs.
  • JP-A-60-018240 and also the more recent EP 1 028 303 B1, have provided heat exchanger ribs (e.g., flat, plate or corrugated ribs) in which both opposite edge strips are reinforced by turning in the edges over the narrowest possible section.
  • heat exchanger ribs e.g., flat, plate or corrugated ribs
  • Such reinforcement has increased the stability of the ribs and the heat exchanger since the thickness of the ribs is generally is well below 0.5 mm. That is, while the main function of the ribs is to facilitate efficient heat exchange, they also importantly function to retain the stability of the heat exchanger.
  • the heat exchange performance is better in thicker ribs than in thinner ones, perhaps due to the fact that the amount of heat transported per unit time is smaller in thinner ribs, since resistance to heat conduction rises. At the same time, however, thick ribs may block more surface area, leaving less area for gas flow therethrough. In short, the wall thickness of the heat exchange ribs cannot be arbitrarily reduced
  • the geometry of the heat exchange ribs cannot be arbitrarily altered either.
  • the wavelength could be reduced, but the pressure loss, for example, of the cooling air would be undesirably increased on this account.
  • a longer sheet material would naturally also be required, which could result in additional weight which is undesirable in many applications such as vehicle cooling systems.
  • the present invention is directed toward overcoming one or more of the problems set forth above.
  • a heat exchange rib through which a gaseous medium flows to be in heat exchange with another medium.
  • the rib is a strip adapted to receive flow of the gaseous medium along the surfaces thereof, wherein the strip has a first thickness and an edge portion of the strip has a second thickness greater than the first thickness, with the edge portion extending in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.
  • the gaseous medium flows from front to back of the rib, and the edge portion is the front portion of the rib.
  • the first thickness of the sheet material is generally in the range from 0.04-0.15 mm, and the second thickness is generally double the first thickness.
  • the second thickness is substantially a multiple of the first thickness, and the edge portion is formed by one or more folds of the rib strip.
  • the edge portion comprises combined strips having at least two different wall thicknesses.
  • cuts in the ribs are adapted to cause turbulence in the gaseous medium flowing along the rib surfaces.
  • the cuts are in the edge portion.
  • the width of the edge portion in the flow direction is about 5-60% of the total width of the rib. In a further form, the width of the edge portion in the flow direction is about 10-30% of the total width of the rib.
  • the rib is flat. In another form, the rib is corrugated and the height of the corrugations is about 3-10 mm.
  • a heat exchanger is provided with ribs disposed between flat tubes adapted to carry the other medium. Gaseous medium flows through the ribs to be in heat exchange with the other medium.
  • the rib is a strip adapted to receive flow of the gaseous medium along the surfaces thereof, wherein the strip has a first thickness and an edge portion of the strip has a second thickness greater than the first thickness, with the edge portion extending in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.
  • FIG. 1 is a diagram of the temperature trend over the block depth of heat exchangers equipped with three different corrugated ribs, with an edge view of the different ribs graphically illustrated at the top of the Figure;
  • FIG. 2 is a progressive perspective illustration of a metal sheet worked into a corrugated rib according to the present invention with a turned-in edge and cuts over the entire width;
  • FIG. 3 is similar to FIG. 2 , but illustrating a corrugated rib according to the present invention having cuts only in the region not turned in.
  • FIG. 1 illustrates the result of extensive studies conducted by the Applicant, with the temperature trend over the entire width W of three corrugated ribs 10 is plotted (wherein the width W corresponds to the block depth of the heat exchanger):
  • the curve for the third corrugated rib 10 i.e., the curve with stars
  • the curve for the third corrugated rib 10 is almost congruent with the solid curve representing the corrugated rib 10 with 0.12 mm sheet thickness without the wall or edge reinforcement.
  • the curve for the third corrugated rib 10 is therefore well about the dashed curve for the second corrugated rib in that region as well.
  • the edge strip 20 i.e., to the right of the FIG. 1 chart
  • W e.g., block depth of the heat exchanger
  • the solid curves and the curves provided with stars separate somewhat from each other, since the poorer heat transfer of the thinner corrugated rib 10 in that region (0.06 mm for the third rib vs. 0.12 mm for the first rib) comes into play and a lower average temperature is obtained over the entire corrugated rib 10 , which leads to an increased average temperature difference between the media.
  • the inventor hereof has established that the entry region into the heat exchange rib 10 for cooling air, for example, has a relatively low temperature and that the temperature has a comparatively higher value roughly from the center of the width of the heat exchange rib 10 , since the cooling air on its path through the heat exchanger has already absorbed heat. Moreover, this finding means that the temperature difference between air flowing past the ribs 10 and the other medium flowing in the tubes, for example, which influences heat exchange performance, is also different.
  • By increasing the wall thickness most advantageously in the entry region for cooling air flow (see arrow 24 in FIGS.
  • the temperature difference between the entry region and the region of the heat exchange rib lying far along in the air flow direction is somewhat reduced, but overall this means that, over the entire width of the heat exchange rib, the average temperature difference between the two media is increased, so that the improved heat exchange performance relative to a heat exchange rib without wall thickening can be explained.
  • Such improved heat exchange performance can also be explained by the fact that the increase in temperature in the inlet area caused by the increase in wall thickness comes out smaller than the reduction in temperature in the region distant from it. For example, in the front, at the entry region, if the temperature is 5° C. higher and, at the rear, in the exit region, 10° C. lower, then the average temperature on the air side is 5° C. lower. Therefore, the temperature difference between the air and the coolant in the tubes is increased.
  • corrugated ribs 10 may be formed from a flat metal sheet 30 a having the selected minimum thickness.
  • the sheet 30 b may be folded over along the front edge to form the thickened edge strip 20 , where the edge strip thickness is therefore twice the thickness of the sheet with a single fold. It should be understood, however, that it would be within the scope of the present invention to form the edge strip 20 with multiple folds whereby the edge strip 20 may be several times the sheet thickness in which case correspondingly more favorable values with respect to performance may be achieved.
  • ribs 10 of sheets which are rolled with different sheet thicknesses (i.e., having at least one gradation of wall thickness) along their length, in which case an identical curve trend could also be obtained.
  • the sheet 30 b may then be suitably bent so as to be serpentine or corrugated as shown at 30 c.
  • the width W E of the edge strip 20 according to the present invention should be selected so that the average temperature between the media may be increased.
  • the edge strip width W E may advantageously be about 5% to 60% of the width W of the rib 20 , and most advantageously 10 to 30% of the total width W of the heat exchange rib.
  • the wall thickness of the heat exchange rib according to the present invention may advantageously lie in the range from about 0.04 to 0.12 mm, with a particularly advantageous range being between 0.04 and 0.08 mm.
  • heat exchange ribs 10 formed wave-like as previously described i.e., serpentine or corrugated ribs
  • particularly advantageous results may be achieved with a rib height 34 (see FIG. 3 ) between about 3 and 10 mm.
  • the wall thickening at the edge strip 20 also contributes to the stability of the heat exchange rib and the heat exchanger.
  • Cuts 40 which advantageously add turbulence to the flow of air over the ribs 10 may also be provided in the flanks of the ribs 10 .
  • FIG. 2 shows a corrugated rib 10 which includes cuts 40 over the entire width W of the rib 10 which may be formed, for example, by use of a corresponding design in the rib die (not shown).
  • the cuts 40 facilitate the production of deliberate deflection and multiplication of flow paths.
  • the ribs 10 may also be formed with cuts 40 omitted from the edge strip 20 as shown in FIG. 3 .
  • corrugated ribs 10 refer only to corrugated ribs 10 , it should be appreciated that the advantages of the present invention may also be naturally achieved with flat ribs. It will be appreciated by those skilled in this art that flat ribs usually have openings through which the heat exchanger tubes are inserted. Additional details concerning flat ribs can, however, be taken from EP 1 028 303 B1, the full disclosure of which is hereby incorporated by reference. Moreover, it should be appreciated that corrugated ribs 10 as used herein refer to all heat exchange ribs having any wave-like trend, for example rectangular, or as shown in FIG. 2 .
  • Heat exchangers incorporating ribs 10 according to the present invention as described above may be advantageously manufactured, wherein the ribs 10 are disposed between tubes for the other medium. Headers or collecting tanks may be secured to the tube ends such as is known in the art, whereby controlled flow of the medium through the tubes may be achieved, with heat transfer occurring through the tube walls and ribs 10 between the air passing over the ribs and outside the tubes and the medium inside the tubes. Both the tubes and ribs 10 may advantageously be formed of metal, and suitably connected to each other.

Landscapes

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

Abstract

A heat exchange rib through which a gaseous medium flows to be in heat exchange with another medium. The rib is a strip adapted to receive flow of the gaseous medium along the surfaces thereof, wherein the strip has a first thickness and an edge portion of the strip has a second thickness greater than the first thickness. The edge portion extends in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.

Description

    CROSS REFERENCE TO RELATED APPLICATION(S)
  • Not applicable.
  • Statement Regarding Federally Sponsored Research or Development
  • Not applicable.
  • Reference to a Microfiche Appendix
  • Not applicable.
  • Technical Field
  • The present invention is directed toward heat exchanger ribs, and more particularly toward ribs through which a gaseous medium flows in order to exchange heat with another medium.
  • BACKGROUND OF THE INVENTION AND TECHNICAL PROBLEMS POSED BY THE PRIOR ART
  • Heat exchangers having ribs through which gas flows to exchange heat with another medium are old. Commonly the ribs contact tubes or the like through which the other medium flows, wherein heat is passed from one medium to the other via flow of the media over the tube walls and the ribs.
  • JP-A-60-018240, and also the more recent EP 1 028 303 B1, have provided heat exchanger ribs (e.g., flat, plate or corrugated ribs) in which both opposite edge strips are reinforced by turning in the edges over the narrowest possible section. Such reinforcement has increased the stability of the ribs and the heat exchanger since the thickness of the ribs is generally is well below 0.5 mm. That is, while the main function of the ribs is to facilitate efficient heat exchange, they also importantly function to retain the stability of the heat exchanger. Further, it is known that the heat exchange performance is better in thicker ribs than in thinner ones, perhaps due to the fact that the amount of heat transported per unit time is smaller in thinner ribs, since resistance to heat conduction rises. At the same time, however, thick ribs may block more surface area, leaving less area for gas flow therethrough. In short, the wall thickness of the heat exchange ribs cannot be arbitrarily reduced.
  • The geometry of the heat exchange ribs, for example corrugated ribs, cannot be arbitrarily altered either. For example, the wavelength could be reduced, but the pressure loss, for example, of the cooling air would be undesirably increased on this account. A longer sheet material would naturally also be required, which could result in additional weight which is undesirable in many applications such as vehicle cooling systems.
  • Consequently, conflicting design requirements exist, with some requirements pointing toward lighter and even more compact heat exchangers, while at the same time desiring higher (or at least not distinctly lower) heat exchange performance. Ideally in many applications such as vehicle cooling systems, design improvements will provide lighter and more compact heat exchangers while maintaining or improving performance characteristics.
  • Proposals have been advanced such as disclosed in GB-B-2 133 525, which provide heat exchanger tubes, especially flat tubes, having wall thicknesses larger in sections. This structure is intended to improve corrosion resistance.
  • The present invention is directed toward overcoming one or more of the problems set forth above.
  • SUMMARY OF THE INVENTION
  • In one aspect of the present invention, a heat exchange rib is provided through which a gaseous medium flows to be in heat exchange with another medium. The rib is a strip adapted to receive flow of the gaseous medium along the surfaces thereof, wherein the strip has a first thickness and an edge portion of the strip has a second thickness greater than the first thickness, with the edge portion extending in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.
  • In one form of this aspect of the present invention, the gaseous medium flows from front to back of the rib, and the edge portion is the front portion of the rib.
  • In another form of this aspect of the present invention, the first thickness of the sheet material is generally in the range from 0.04-0.15 mm, and the second thickness is generally double the first thickness.
  • In a further form of this aspect of the present invention, the second thickness is substantially a multiple of the first thickness, and the edge portion is formed by one or more folds of the rib strip.
  • In still another form of this aspect of the present invention, the edge portion comprises combined strips having at least two different wall thicknesses.
  • In a still further form of this aspect of the present invention, cuts in the ribs are adapted to cause turbulence in the gaseous medium flowing along the rib surfaces. In a further form, the cuts are in the edge portion.
  • In yet another form of this aspect of the present invention, the width of the edge portion in the flow direction is about 5-60% of the total width of the rib. In a further form, the width of the edge portion in the flow direction is about 10-30% of the total width of the rib.
  • In another form of this aspect of the present invention, the rib is flat. In another form, the rib is corrugated and the height of the corrugations is about 3-10 mm.
  • In another aspect of the present invention, a heat exchanger is provided with ribs disposed between flat tubes adapted to carry the other medium. Gaseous medium flows through the ribs to be in heat exchange with the other medium. The rib is a strip adapted to receive flow of the gaseous medium along the surfaces thereof, wherein the strip has a first thickness and an edge portion of the strip has a second thickness greater than the first thickness, with the edge portion extending in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a diagram of the temperature trend over the block depth of heat exchangers equipped with three different corrugated ribs, with an edge view of the different ribs graphically illustrated at the top of the Figure;
  • FIG. 2 is a progressive perspective illustration of a metal sheet worked into a corrugated rib according to the present invention with a turned-in edge and cuts over the entire width;
  • FIG. 3 is similar to FIG. 2, but illustrating a corrugated rib according to the present invention having cuts only in the region not turned in.
  • DETAILED DESCRIPTION OF THE INVENTION
  • FIG. 1 illustrates the result of extensive studies conducted by the Applicant, with the temperature trend over the entire width W of three corrugated ribs 10 is plotted (wherein the width W corresponds to the block depth of the heat exchanger):
    • 1. Study results for a first corrugated rib 10 having a 0.12 mm sheet thickness and without a reinforced edge are illustrated by the solid curve.
    • 2. Study results for a second corrugated rib 10 having a 0.06 mm sheet thickness, and also without a reinforced edge, are illustrated by the dashed line. As contrasted with the first rib design, the second rib design has a weight reduction of 50% and a performance loss of 2.64% occurs. Moreover, the two curves make it clear that the different thicknesses T of the corrugated ribs 10 with increasing block depth and increasing temperature ensure that the temperature difference becomes greater, in which case a performance loss will manifest itself.
    • 3. Study results for a third corrugated rib 10, this one according to the present invention, are illustrated in FIG. 1 by the solid curved line with stars. The third corrugated rib 10 includes an edge strip 20 of greater wall thickness resulting from the metal sheet being turned in once. The thicker edge strip 20 may advantageously run over the entire length of corrugated rib 10 and have a substantially uniform width WE over the entire length of the rib 10 which is about 30% of the total width W of the corrugated rib 10 (or the block depth of the heat exchanger). Like the second rib, the third corrugated rib 10 also has a sheet thickness of 0.06 mm, but because of the turned-in (thicker) edge strip 20, with the same total width W the weight reduction is only 35% but the performance loss is also less pronounced, namely only 1.11%.
  • It should be appreciated that the curve for the third corrugated rib 10 (i.e., the curve with stars) in the region of the edge strip 20 (through width WE) is almost congruent with the solid curve representing the corrugated rib 10 with 0.12 mm sheet thickness without the wall or edge reinforcement. The curve for the third corrugated rib 10 is therefore well about the dashed curve for the second corrugated rib in that region as well.
  • Behind the edge strip 20 (i.e., to the right of the FIG. 1 chart), with increasing total width W (e.g., block depth of the heat exchanger), the solid curves and the curves provided with stars (for the first and third corrugated ribs, respectively) separate somewhat from each other, since the poorer heat transfer of the thinner corrugated rib 10 in that region (0.06 mm for the third rib vs. 0.12 mm for the first rib) comes into play and a lower average temperature is obtained over the entire corrugated rib 10, which leads to an increased average temperature difference between the media.
  • As a result, the inventor hereof has established that the entry region into the heat exchange rib 10 for cooling air, for example, has a relatively low temperature and that the temperature has a comparatively higher value roughly from the center of the width of the heat exchange rib 10, since the cooling air on its path through the heat exchanger has already absorbed heat. Moreover, this finding means that the temperature difference between air flowing past the ribs 10 and the other medium flowing in the tubes, for example, which influences heat exchange performance, is also different. By increasing the wall thickness, most advantageously in the entry region for cooling air flow (see arrow 24 in FIGS. 2-3) past the ribs 10, the temperature difference between the entry region and the region of the heat exchange rib lying far along in the air flow direction is somewhat reduced, but overall this means that, over the entire width of the heat exchange rib, the average temperature difference between the two media is increased, so that the improved heat exchange performance relative to a heat exchange rib without wall thickening can be explained. Such improved heat exchange performance can also be explained by the fact that the increase in temperature in the inlet area caused by the increase in wall thickness comes out smaller than the reduction in temperature in the region distant from it. For example, in the front, at the entry region, if the temperature is 5° C. higher and, at the rear, in the exit region, 10° C. lower, then the average temperature on the air side is 5° C. lower. Therefore, the temperature difference between the air and the coolant in the tubes is increased.
  • It should thus be appreciated that use of the present invention, with a thicker edge portion 20 extending sufficiently along the width of the rib 10 to increase the average temperature differential between the media (with the third rib when compared to the second rib, each having a general [first] thickness of 0.06 mm), may provide a noticeable weight reduction with only slight performance losses that lie within the acceptable range, which slight performance losses can easily be compensated by other expedients, or even tolerated.
  • As illustrated in FIGS. 2 and 3, corrugated ribs 10 according to the present invention may be formed from a flat metal sheet 30 a having the selected minimum thickness. The sheet 30 b may be folded over along the front edge to form the thickened edge strip 20, where the edge strip thickness is therefore twice the thickness of the sheet with a single fold. It should be understood, however, that it would be within the scope of the present invention to form the edge strip 20 with multiple folds whereby the edge strip 20 may be several times the sheet thickness in which case correspondingly more favorable values with respect to performance may be achieved. It should also be understood that it would be within the scope of the present invention to form the ribs 10 of sheets which are rolled with different sheet thicknesses (i.e., having at least one gradation of wall thickness) along their length, in which case an identical curve trend could also be obtained. The sheet 30 b may then be suitably bent so as to be serpentine or corrugated as shown at 30 c.
  • The width WE of the edge strip 20 according to the present invention should be selected so that the average temperature between the media may be increased. In this regard, it has been found that the edge strip width WE may advantageously be about 5% to 60% of the width W of the rib 20, and most advantageously 10 to 30% of the total width W of the heat exchange rib.
  • Further, the wall thickness of the heat exchange rib according to the present invention may advantageously lie in the range from about 0.04 to 0.12 mm, with a particularly advantageous range being between 0.04 and 0.08 mm. In heat exchange ribs 10 formed wave-like as previously described (i.e., serpentine or corrugated ribs), particularly advantageous results may be achieved with a rib height 34 (see FIG. 3) between about 3 and 10 mm.
  • Thus, it should be appreciated that by using an extremely thin sheet material, particularly lightweight construction may be advantageously achieved, while at the same time achieving acceptable heat exchange performance. Moreover, the wall thickening at the edge strip 20 also contributes to the stability of the heat exchange rib and the heat exchanger.
  • Cuts 40 which advantageously add turbulence to the flow of air over the ribs 10 may also be provided in the flanks of the ribs 10. For example, FIG. 2 shows a corrugated rib 10 which includes cuts 40 over the entire width W of the rib 10 which may be formed, for example, by use of a corresponding design in the rib die (not shown). The cuts 40 facilitate the production of deliberate deflection and multiplication of flow paths. The ribs 10 may also be formed with cuts 40 omitted from the edge strip 20 as shown in FIG. 3.
  • Further, although the depicted variants refer only to corrugated ribs 10, it should be appreciated that the advantages of the present invention may also be naturally achieved with flat ribs. It will be appreciated by those skilled in this art that flat ribs usually have openings through which the heat exchanger tubes are inserted. Additional details concerning flat ribs can, however, be taken from EP 1 028 303 B1, the full disclosure of which is hereby incorporated by reference. Moreover, it should be appreciated that corrugated ribs 10 as used herein refer to all heat exchange ribs having any wave-like trend, for example rectangular, or as shown in FIG. 2.
  • Heat exchangers incorporating ribs 10 according to the present invention as described above may be advantageously manufactured, wherein the ribs 10 are disposed between tubes for the other medium. Headers or collecting tanks may be secured to the tube ends such as is known in the art, whereby controlled flow of the medium through the tubes may be achieved, with heat transfer occurring through the tube walls and ribs 10 between the air passing over the ribs and outside the tubes and the medium inside the tubes. Both the tubes and ribs 10 may advantageously be formed of metal, and suitably connected to each other.
  • Still other aspects, objects, and advantages of the present invention can be obtained from a study of the specification, the drawings, and the appended claims. It should be understood, however, that the present invention could be used in alternate forms where less than all of the objects and advantages of the present invention and preferred embodiment as described above would be obtained.

Claims (12)

1. A heat exchange rib through which a gaseous medium flows to be in heat exchange with another medium, said rib comprising a strip adapted to receive flow of said gaseous medium along the surfaces thereof, wherein said strip has a first thickness and an edge portion of the strip has a second thickness greater than said first thickness, said edge portion extending in the flow direction of the gaseous medium a width sufficient to increase the average temperature difference between the media.
2. The heat exchanger rib of claim 1, wherein said gaseous medium flows from front to back of said rib, and said edge portion is the front portion of the rib.
3. The heat exchanger rib of claim 1, wherein the first thickness of the sheet material is generally in the range from 0.04-0.15 mm, and said second thickness is generally double said first thickness.
4. The heat exchanger rib of claim 1, wherein said second thickness is substantially a multiple of said first thickness, and said edge portion is formed by one or more folds of said rib strip.
5. The heat exchanger rib of claim 1, wherein said edge portion comprises combined strips having at least two different wall thicknesses.
6. The heat exchanger rib of claim 1, further comprising cuts in said ribs adapted to cause turbulence in the gaseous medium flowing along the rib surfaces.
7. The heat exchanger rib of claim 6, wherein said cuts are in said edge portion.
8. The heat exchanger rib of claim 1, wherein the width of the edge portion in the flow direction is about 5-60% of the total width of the rib.
9. The heat exchanger rib of claim 8, wherein the width of the edge portion in the flow direction is about 10-30% of the total width of the rib.
10. The heat exchanger rib of claim 1, wherein said rib is flat.
11. The heat exchanger rib of claim 1, wherein said rib is corrugated and the height of the corrugations is about 3-10 mm.
12. A heat exchanger comprising ribs according to claim 1 and flat tubes adapted to carry said other medium, said ribs being disposed between the flat tubes.
US11/303,483 2004-12-17 2005-12-16 Heat exchanger and ribs Abandoned US20060131006A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004060795A DE102004060795A1 (en) 2004-12-17 2004-12-17 Heat exchanger rib and heat exchanger
DEDE102004060795. 2004-12-17

Publications (1)

Publication Number Publication Date
US20060131006A1 true US20060131006A1 (en) 2006-06-22

Family

ID=35911162

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/303,483 Abandoned US20060131006A1 (en) 2004-12-17 2005-12-16 Heat exchanger and ribs

Country Status (3)

Country Link
US (1) US20060131006A1 (en)
EP (1) EP1672305A1 (en)
DE (1) DE102004060795A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090133860A1 (en) * 2007-11-22 2009-05-28 Denso Corporation Heat exchanger
US20090173477A1 (en) * 2008-01-03 2009-07-09 Denso International America, Inc. Heat exchanger fin
US20120211215A1 (en) * 2009-11-11 2012-08-23 Kabushiki Kaisha Toyota Jidoshokki Vapor cooling heat exchanger
US20140352933A1 (en) * 2013-05-28 2014-12-04 Hamilton Sundstrand Corporation Core assembly for a heat exchanger and method of assembling
WO2024203755A1 (en) * 2023-03-28 2024-10-03 三菱電機株式会社 Heat exchanger and method for manufacturing heat exchanger

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008031612A1 (en) * 2008-07-07 2010-01-14 Behr Gmbh & Co. Kg Corrugation fin for heat exchanger, has flat tubes, rib arches and longitudinal edge reinforced by rebates, which are reinforced on exterior of rib arches
DE102014200680A1 (en) * 2014-01-16 2015-07-16 Mahle International Gmbh Heat exchanger

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2055549A (en) * 1934-05-18 1936-09-29 Modine Mfg Co Heat exchange device
US2376749A (en) * 1942-01-16 1945-05-22 Cyril Terence Delaney And Gall Radiator
US2613065A (en) * 1947-11-21 1952-10-07 Chausson Usines Sa Cooling radiator
US5067562A (en) * 1988-04-25 1991-11-26 Sanden Corporation Heat exchanger having fins which are different from one another in fin thickness
US6354367B1 (en) * 2001-02-12 2002-03-12 Rheem Manufacturing Company Air conditioning unit having coil portion with non-uniform fin arrangement
US20050274501A1 (en) * 2004-06-09 2005-12-15 Agee Keith D Decreased hot side fin density heat exchanger

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1138367A (en) * 1910-12-02 1915-05-04 Briscoe Mfg Company Radiator.
US1752879A (en) * 1928-09-15 1930-04-01 American Blower Corp Radiator
GB1017246A (en) * 1963-09-04 1966-01-19 Ford Motor Co Improvements in or relating to heat exchangers
FR2138417A1 (en) * 1971-05-25 1973-01-05 Hutogepgyar Heat exchanger comprising tubes and finned plates - in which collars at contact points are produced by working the plates comprise tube fin plate collar contact point produce working
US4067384A (en) * 1976-06-17 1978-01-10 Miyakawa Gene K Heat exchanger core assembly for engine cooling system
JPS59129392A (en) 1983-01-10 1984-07-25 Nippon Denso Co Ltd Heat exchanger
JPS6018240A (en) * 1983-07-11 1985-01-30 Mitsubishi Heavy Ind Ltd Production of needlelike fin for heat exchanger
DE4142019A1 (en) * 1991-12-19 1993-06-24 Behr Gmbh & Co SHAFT RIB FOR FLAT TUBE HEAT EXCHANGER
EP1028303B1 (en) * 1999-02-13 2001-01-31 Nederlandse Radiateuren Fabriek B.V. Fin for heat exchanger

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2055549A (en) * 1934-05-18 1936-09-29 Modine Mfg Co Heat exchange device
US2376749A (en) * 1942-01-16 1945-05-22 Cyril Terence Delaney And Gall Radiator
US2613065A (en) * 1947-11-21 1952-10-07 Chausson Usines Sa Cooling radiator
US5067562A (en) * 1988-04-25 1991-11-26 Sanden Corporation Heat exchanger having fins which are different from one another in fin thickness
US6354367B1 (en) * 2001-02-12 2002-03-12 Rheem Manufacturing Company Air conditioning unit having coil portion with non-uniform fin arrangement
US20050274501A1 (en) * 2004-06-09 2005-12-15 Agee Keith D Decreased hot side fin density heat exchanger

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090133860A1 (en) * 2007-11-22 2009-05-28 Denso Corporation Heat exchanger
US20090173477A1 (en) * 2008-01-03 2009-07-09 Denso International America, Inc. Heat exchanger fin
US8167028B2 (en) * 2008-01-03 2012-05-01 Denso Corporation Heat exchanger fin with planar crests and troughs having slits
US20120211215A1 (en) * 2009-11-11 2012-08-23 Kabushiki Kaisha Toyota Jidoshokki Vapor cooling heat exchanger
US20140352933A1 (en) * 2013-05-28 2014-12-04 Hamilton Sundstrand Corporation Core assembly for a heat exchanger and method of assembling
WO2024203755A1 (en) * 2023-03-28 2024-10-03 三菱電機株式会社 Heat exchanger and method for manufacturing heat exchanger

Also Published As

Publication number Publication date
EP1672305A1 (en) 2006-06-21
DE102004060795A1 (en) 2006-06-29

Similar Documents

Publication Publication Date Title
JP4898300B2 (en) Evaporator
JP4724594B2 (en) Heat exchanger
US6640886B2 (en) Heat exchanger tube, heat exchanger and method of making the same
US20010004935A1 (en) Refrigerant condenser used for automotive air conditioner
US20060266509A1 (en) Heat exchanger
EP1563240B1 (en) High pressure heat exchanger
US7992401B2 (en) Evaporator
KR940004308A (en) Multilayer Heat Exchanger and Manufacturing Method Thereof
EP1239252B1 (en) Stacked-Type, Multi-Flow Heat Exchangers
US6179050B1 (en) Heat exchangers
US20080314076A1 (en) Heat Exchanger
US20080202153A1 (en) Evaporator
JP2006322699A (en) Heat exchanger
US20070068661A1 (en) Heat exchanger
US20060131006A1 (en) Heat exchanger and ribs
US7174953B2 (en) Stacking-type, multi-flow, heat exchanger
US6942024B2 (en) Corrugated heat exchange element
CN100567876C (en) Heat exchanger
US20070068662A1 (en) Heat exchanger
US20050230093A1 (en) Heat exchanger
JPS6157991B2 (en)
US12209815B2 (en) Flat heat exchanger tube
US20010006105A1 (en) Flat heat exchange tubes
JP2006200881A (en) Heat exchanger
JP2005195318A (en) Evaporator

Legal Events

Date Code Title Description
AS Assignment

Owner name: MODINE MANUFACTURING COMPANY, WISCONSIN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:BROST, VIKTOR;REEL/FRAME:018173/0516

Effective date: 20060111

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION

点击 这是indexloc提供的php浏览器服务,不要输入任何密码和下载