US20050072562A1 - Heat exchanger tube assembly - Google Patents
Heat exchanger tube assembly Download PDFInfo
- Publication number
- US20050072562A1 US20050072562A1 US10/955,148 US95514804A US2005072562A1 US 20050072562 A1 US20050072562 A1 US 20050072562A1 US 95514804 A US95514804 A US 95514804A US 2005072562 A1 US2005072562 A1 US 2005072562A1
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- United States
- Prior art keywords
- tube
- heat exchanger
- fins
- fin
- exchanger tube
- 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
Links
- 125000006850 spacer group Chemical group 0.000 claims abstract description 31
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical group [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 18
- 239000011701 zinc Substances 0.000 claims description 16
- 229910052725 zinc Inorganic materials 0.000 claims description 16
- 230000007797 corrosion Effects 0.000 claims description 13
- 238000005260 corrosion Methods 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 13
- 238000000034 method Methods 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 4
- 230000000712 assembly Effects 0.000 claims description 4
- 238000000429 assembly Methods 0.000 claims description 4
- 238000005246 galvanizing Methods 0.000 claims description 2
- 239000012530 fluid Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000007598 dipping method Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000004411 aluminium Substances 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
- 238000004140 cleaning Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000004378 air conditioning Methods 0.000 description 1
- 230000009286 beneficial effect Effects 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
- 230000006866 deterioration Effects 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
- F28F1/32—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/081—Heat exchange elements made from metals or metal alloys
- F28F21/082—Heat exchange elements made from metals or metal alloys from steel or ferrous alloys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2240/00—Spacing means
Definitions
- the present invention relates to a heat exchanger tube suitable to be incorporated into a heat exchanger, as well as a method of manufacturing such a heat exchanger tube.
- Heat exchangers are utilised in a broad range of applications where it is necessary to transfer heat to or from a particular item of equipment, such as an air compressor, air conditioning unit, booster or engine.
- a typical heat exchanger commonly used in air or gas heating and cooling applications such as those identified above is that of the “cross-flow” type.
- Such exchangers generally comprise an arrangement of tubes through which a first fluid is passed and across which a second fluid (often a gas) is passed.
- a particular type of cross-flow exchanger comprises an arrangement of tubes, each of which is provided with a plurality of fins along, and extending generally transverse to, its length.
- a cooler fluid often a gas
- the fins assist in cooling the hot fluid by providing a large heat transfer area. It is desirable that the fins be thin to maximise the surface area available for transfer of heat within the particular space available..
- Cross-flow heat exchangers generally use fins made of aluminium or copper due to the excellent heat conduction characteristics of those metals. However, their use introduces other problems.
- the tubes used are not made of the same metal as they are required to be more robust. Galvanic corrosion tends to occur as a result of the dissimilarity in the metals. Such galvanic corrosion gives rise to oxides which are poor conductors of heat and which thus compromises the heat transfer between the tubes and fins.
- a further disadvantage is the relative softness of those metals and thus the vulnerability of the fins to damage, particularly from impact such as during cleaning with a high pressure hose. Moreover, those metals oxidise and/or perish over time in harsh operating conditions.
- the invention resides in a heat exchanger tube assembly comprising a tube having a plurality of fins mounted thereto at spaced intervals along its length, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin, the spacer being bonded to the tube by a thermally-conductive medium.
- the fins are formed of generally the same material as the tube.
- said material is a steel.
- the thermally conductive medium occupies a region between the external surface of the tube and the inner surface of the spacer to thereby enhance said heat transfer from the tube to the fin.
- each spacer is configured as an annular flange.
- said annular flange is discontinuous around the circumference of said tube.
- said annular flange comprises a plurality of tabs disposed around the circumference of said tube.
- said fins are resistant to permanent deformation under conditions typically encountered by a heat exchanger.
- each spacer is closely adjacent the external surface of said tube.
- said heat exchanger tube assembly is covered with a corrosion-resistant material.
- said corrosion-resistant material is said thermally-conductive medium.
- thermoly-conductive medium is zinc or zinc alloy.
- the invention resides in a heat exchanger comprising a plurality of heat exchanger tube assemblies as previously descibed, said tubes being held in parallel spaced relation, adjacent tubes being interconnected by at least some of said fins, each tube being received through an aperture provided in said fins, each fin having at least two apertures to thereby interconnect adjacent tubes.
- the invention resides in a heat exchanger comprising a plurality of heat exchanger tube assemblies as previously descibed, said tubes being held in parallel spaced relation, each tube being interconnected with at least one adjacent tube by a group of fins, each fin having two apertures to receive said adjacent tubes to thereby interconnect adjacent tubes.
- the invention resides in method of manufacturing a heat exchanger tube assembly, said method comprising the steps of mounting a plurality of fins to a tube and bonding the fins to the tube with a thermally-conductive medium, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin.
- the method further comprises the step of covering the fins and tube with a corrosion-resistant material.
- the methods of bonding the fins to the tube and covering of the fins and tube comprises a hot-dip, zinc or zinc-alloy galvanising procedure.
- FIG. 1 is a perspective view of a heat exchanger tube according to the first embodiment with part of its coating shown cut-away (for clarity);
- FIG. 2 is a front elevation view of the heat exchanger of FIG. 1 ;
- FIG. 3 is a perspective view of a fin of the type incorporated in the heat exchanger tube of FIG. 1 ;
- FIG. 4 is a perspective view of a heat exchanger tube according to the second embodiment
- FIG. 5 is a perspective view of a fin of the type incorporated in the heat exchanger tube of FIG. 4 ;
- FIG. 6 is a perspective view of a heat exchanger tube assembly according to the third embodiment of the invention and comprising fins of the type depicted in FIG. 5 ;
- FIG. 7 is a front elevation view of a repeating unit of the type incorporated in the heat exchanger tube assembly shown in FIG. 6 ;
- FIG. 8 is a perspective view of a heat exchanger tube assembly according to a fourth embodiment of the invention and comprising fins of the type depicted in FIG. 5 .
- FIGS. 1, 3 and 5 illustrate the first, second and third embodiments respectively.
- Each of those embodiments comprises at least one tube and a plurality of fins mounted thereto.
- Each fin has at least one aperture through which the tube is received.
- the heat exchanger tube assembly 10 according to the first embodiment is shown at FIGS. 1 and 2 and comprises a tube 12 and a plurality of fins 14 mounted to the tube 12 .
- the tube is typically made from steel due to the robust properties provided by that material which enable it to withstand harsh environments. In particular, it has the ability to resist fatigue when subject to vibration, provided the system is designed appropriately. As well, it is able to withstand substantial knocks, impacts and the like.
- Each fin 14 has an aperture 16 through which the tube 12 is received and is also provided with a spacer 20 on an axial face thereof. In other embodiments, such spacers may be provided on both axial faces of each fin.
- the spacers 20 which are located between adjacent fins 14 , maintain a regular spacing between those fins 14 along the tube 12 .
- the fins 14 are formed of generally the same material which, in the case of this embodiment, is steel.
- FIG. 3 A detailed view of a fin 14 of the type used in the first embodiment is shown at FIG. 3 .
- the spacer 20 is integrally formed with the fins 14 and extends from the rim of the aperture 16 generally transversely to the fin 14 . It is thereby positioned so as to be closely adjacent to the external surface of the tube 12 .
- the spacer 20 is configured as an annular flange so as to conform with the external surface of the tube 12 .
- the annular flange is discontinuous around its circumference to provide a plurality of tabs around the rim of the aperture 16 . In this embodiment, the tabs are disposed at regular angular intervals around the rim of the aperture 16 .
- the fin 14 is produced from steel sheeting, the aperture 16 being stamped therein to be of a diameter which is such that the aperture 16 which will snugly receive the tube 12 therethrough.
- the stamping device is suitably formed to produce tabs 20 , initially in the plane of the fin 14 .
- the tabs 20 are then bent out of that plane to extend from the rim of the aperture.
- the tabs are suitably profiled to provide an inner surface to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin.
- each of the fins 14 is discrete though, in alternative embodiments, the fins may be provided as a one-piece assembly such as in the form a helix.
- the fins 14 are bonded to the tube 12 by zinc 11 which is a thermally-conductive and corrosion resistant medium.
- the zinc 11 occupies the regions between the external surface of the tube 12 and the inner radial faces both of the fins 14 and the tabs 20 , giving rise to a substantially continuous bond between the fins 14 and the tube 12 . The manner in which this is achieved is discussed further below.
- the substantially continuous bond provides for efficient heat transfer from the tube to the fins and also creates a relatively robust mounting of the fins 14 to the tube 12 .
- the entire exterior of the heat exchanger tube 10 is also coated in zinc to render it corrosion-resistant.
- the fins 14 which may have been formed in the manner described above, are received over the tube 12 such that the spacer 20 of each fin 14 abuts an adjacent fin 14 (best shown at FIG. 2 ). If it is felt necessary, the fins 14 may then be tack welded to the tube 12 to assist in locating the fins 14 in their desired position on the tube 12 prior to coating with the zinc 11 . Alternatively, they may be of a sufficiently snug fit that no such welding is needed.
- the fins 14 and tube 12 forming the heat exchanger tube 10 are then hot-dipped in molten zinc to galvanise the heat exchanger tube 10 .
- Hot-dipping of the heat exchanger tube 10 in zinc is advantageous in that it not only renders the heat exchanger tube 10 corrosion-resistant but simultaneously bonds the fins 14 to the tube 12 .
- the zinc, as applied by hot-dipping is pervasive and occupies the regions between the external surface of the tube 12 and the inner radial faces both of the fins 14 and the tabs 20 , giving rise to the substantially continuous bond between the fins 14 and the tube 12 and thus providing for efficient heat transfer, as described above.
- the spacer 20 provides two functions: namely it acts to provide a definite, predefined spacing between adjoining fins to simply assembly of the fins as one fin may be pressed along the tube 12 until it contacts the spacer of the previous fin, and more importantly, the inner surface of the spacer 20 provides a broad area of contact with tube 12 to enable better transfer of heat from the tube 12 to the fin 14 .
- a spacer comprising a continuous annular flange might well provide the best solution from this point of view.
- the fins 14 are more easily mounted to the tube 12 and it is even less likely that zinc will fail to penetrate between the tube 12 and the inner surface of the spacer 20 during the hot-dip process.
- the heat exchanger tube 10 is relatively robust, owing to the fins 14 being formed of steel, which is resistant to permanent deformation, and also due to the continuity and area, and thus the strength, of the zinc bond between the external surface of the tube 12 and the inner radial faces both of the fins 14 and the tabs 20 .
- the fins 14 and the tube 12 are made of substantially the same material, while the zinc coating provides the well known galvanic protection to the assembly.
- corrosion at the junction between the fins and the tubes is eliminated.
- the zinc coating provides stiffness to the fins and the tubes.
- the steel fins are able to withstand the force of high pressure sprays used for cleaning without permanent deflection thereby better maintaining their cooling effectiveness during the life of the heat exchanger.
- the heat exchanger tube assembly 10 in addition to offering the abovementioned advantages, is relatively economic to manufacture.
- the second embodiment of the invention is illustrated at FIG. 4 .
- the second embodiment is a variation of the first embodiment though the heat exchanger tube 10 comprises a pair of parallel tubes 12 respectively received through a pair of apertures 16 .
- a fin 14 of the type used in the second embodiment is shown at FIG. 5 .
- the fin 14 is manufactured in an identical fashion to that which is incorporated in the first embodiment though it is formed with a pair of apertures 16 each of which is provided with a spacer 20 identical to that described in connection with the first embodiment.
- the advantage offered by the second embodiment, over the first, is that a given number of fins 14 in this embodiment is sufficient for two tubes 12 rather than just one tube. This results in a saving in manufacturing costs because the labour required in cutting and/or stamping a single fin is not significantly greater than that required to produce a fin in accordance with the first embodiment.
- a further advantage is a stiffening effect which is created along the axis between the pair of adjacent tubes 12 as a result of their being tied together by the fins 14 . This can reduce vibration, both of the heat exchanger tube 10 and in the heat exchanger generally, and thus increase the life of the heat exchanger.
- the third embodiment of the invention which is illustrated at FIG. 6 , is a heat exchanger tube assembly 100 based on a variation of the heat exchanger tube 10 according to the second embodiment.
- the heat exchanger tube assembly 100 comprises a plurality of tubes 12 interconnected by fins 14 of the type illustrated in FIG. 5 .
- the heat exchanger tube assembly 100 is comprised of a series of repeating units, one such unit 40 being illustrated at FIG. 7 .
- the unit 40 is similar to the heat exchanger tube 10 depicted at FIG. 4 though alternate fins 14 ′, along the length of one of the tubes 12 ′, do not extend to the other tube 12 ′′ in that unit 40 , the unoccupied apertures 16 ′ of those alternate fins 14 ′ instead being intended to receive another tube 12 ′′ of an identical unit 40 shown in broken lines.
- the assembly 100 is formed from the desired number of units 40 prior to hot-dipping.
- the tubes 12 in that assembly 100 need not be coplanar, thus enabling the configuration of the assembly 100 to be adjusted so as to conform with space restrictions and/or the layout of adjacent equipment.
- FIG. 8 illustrates a fourth embodiment which shows an arrangement 110 providing a group of 8 tubes 12 which are disposed in a octagonal configuration and interlinked with fins 14 .
- such a configuration has a high degree of inherent rigidity requiring little additional support.
- such a configuration allows the cooling fluid to be either supplied or withdrawn from a direction parallel to the tubes 12 , rather than transverse to them, which may be beneficial in certain applications.
- the fins 14 may be tack welded to the respective tubes 12 , prior to hot-dipping, so as to assist in locating the fins 14 in their desired position on the tubes 12 and to maintain the configuration of the assembly 100 .
- An advantage offered by this embodiment, and shared by the second embodiment, is the stiffening effect which is created along the axis between the pairs of adjacent tubes 12 ′ and 12 ′′ as a result of their being tied together by the fins 14 ′.
- Such a stiffening effect is also realised along the axis between the pairs of adjacent tubes 12 ′ and 12 ′′ as a result of their being tied together by the fins 14 ′ and also the fins 14 ′′.
- the fins 14 ′ and 14 ′′ thus offer lateral restraint to tubes 12 ′ and 12 ′′ throughout the assembly 100 , thus possibly reducing vibration, both of the assembly 100 and in the heat exchanger generally and increasing the life of the heat exchanger.
- the tube which is second-from-right in FIG. 5 is, advantageously, laterally restrained in two different axes, those axes extending between that tube and the tubes to its left and right (which are not coplanar) respectively.
- units comprising fins of other profiles and having any number of apertures (i.e. possibly more than two apertures) are possible. It is clear that such units may be tied to other units, whether like or unlike, using suitably-profiled fins having appropriately-spaced apertures, those fins, depending on the arrangement of the apertures, being able to provide stiffening and lateral restraint along several different lateral axes. It should also be appreciated that the arrangement of the fins 14 ′ with respect to the fins 14 ′′ need not be staggered as depicted in FIG. 6 , provided those fins still provide adequate lateral restraint, stiffening and heat transfer characteristics throughout the heat exchanger assembly.
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- Physics & Mathematics (AREA)
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Abstract
A heat exchanger tube assembly 10 comprising a tube 12 having a plurality of fins 14 mounted thereto at spaced intervals along its length, each fin 14 having at least one aperture 16 through which the tube 12 is received, each fin 14 having an integral spacer 20 to define the spaced interval from an adjacent fin, the spacer 20 extending from the rim of the aperture 16 generally transversely to the fin 14 to provide an inner surface profiled to contact and cooperate with the external surface of the tube 12 to enhance heat transfer from the tube 12 to the fin 14, the spacer 20 being bonded to the tube 12 by a thermally-conductive medium.
Description
- The present invention relates to a heat exchanger tube suitable to be incorporated into a heat exchanger, as well as a method of manufacturing such a heat exchanger tube.
- Heat exchangers are utilised in a broad range of applications where it is necessary to transfer heat to or from a particular item of equipment, such as an air compressor, air conditioning unit, booster or engine.
- A typical heat exchanger commonly used in air or gas heating and cooling applications such as those identified above is that of the “cross-flow” type. Such exchangers generally comprise an arrangement of tubes through which a first fluid is passed and across which a second fluid (often a gas) is passed.
- A particular type of cross-flow exchanger comprises an arrangement of tubes, each of which is provided with a plurality of fins along, and extending generally transverse to, its length. Where the heat exchanger is being utilised to cool the equipment concerned, hot fluid from that equipment is passed through the tubes whilst a cooler fluid (often a gas) is passed over the fins and tubes to extract heat therefrom and thus to cool the hot fluid. The fins assist in cooling the hot fluid by providing a large heat transfer area. It is desirable that the fins be thin to maximise the surface area available for transfer of heat within the particular space available..
- In this particular type of cross-flow exchanger, it is often necessary that the fluid be passed through the tubes under relatively high pressures. As a result, it is in many instances also desirable that the tubes be robust.
- Cross-flow heat exchangers generally use fins made of aluminium or copper due to the excellent heat conduction characteristics of those metals. However, their use introduces other problems.
- Generally the tubes used are not made of the same metal as they are required to be more robust. Galvanic corrosion tends to occur as a result of the dissimilarity in the metals. Such galvanic corrosion gives rise to oxides which are poor conductors of heat and which thus compromises the heat transfer between the tubes and fins.
- A further disadvantage, is the relative softness of those metals and thus the vulnerability of the fins to damage, particularly from impact such as during cleaning with a high pressure hose. Moreover, those metals oxidise and/or perish over time in harsh operating conditions.
- Accordingly, the invention resides in a heat exchanger tube assembly comprising a tube having a plurality of fins mounted thereto at spaced intervals along its length, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin, the spacer being bonded to the tube by a thermally-conductive medium.
- According to a preferred feature of the invention, the fins are formed of generally the same material as the tube.
- According to a preferred embodiment, said material is a steel.
- According to a preferred feature of the invention, the thermally conductive medium occupies a region between the external surface of the tube and the inner surface of the spacer to thereby enhance said heat transfer from the tube to the fin.
- According to a preferred feature of the invention, each spacer is configured as an annular flange.
- According to a preferred embodiment, said annular flange is discontinuous around the circumference of said tube.
- According to a preferred embodiment, said annular flange comprises a plurality of tabs disposed around the circumference of said tube.
- According to a preferred feature of the invention, said fins are resistant to permanent deformation under conditions typically encountered by a heat exchanger.
- According to a further preferred feature of the invention, each spacer is closely adjacent the external surface of said tube.
- According to a preferred feature of the invention, said heat exchanger tube assembly is covered with a corrosion-resistant material.
- According to a preferred feature of the invention, said corrosion-resistant material is said thermally-conductive medium.
- A heat exchanger tube assembly as claimed in any one of the preceding claims wherein said thermally-conductive medium is zinc or zinc alloy.
- According to a further aspect the invention resides in a heat exchanger comprising a plurality of heat exchanger tube assemblies as previously descibed, said tubes being held in parallel spaced relation, adjacent tubes being interconnected by at least some of said fins, each tube being received through an aperture provided in said fins, each fin having at least two apertures to thereby interconnect adjacent tubes.
- According to a further aspect the invention resides in a heat exchanger comprising a plurality of heat exchanger tube assemblies as previously descibed, said tubes being held in parallel spaced relation, each tube being interconnected with at least one adjacent tube by a group of fins, each fin having two apertures to receive said adjacent tubes to thereby interconnect adjacent tubes.
- According to a further aspect the invention resides in method of manufacturing a heat exchanger tube assembly, said method comprising the steps of mounting a plurality of fins to a tube and bonding the fins to the tube with a thermally-conductive medium, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin.
- According to a preferred feature of the invention, the method further comprises the step of covering the fins and tube with a corrosion-resistant material.
- According to a preferred embodiment, the methods of bonding the fins to the tube and covering of the fins and tube comprises a hot-dip, zinc or zinc-alloy galvanising procedure.
- The invention will be more fully understood in the light of the following description of specific embodiments.
- The description is made with reference to the accompanying drawings of which:
-
FIG. 1 is a perspective view of a heat exchanger tube according to the first embodiment with part of its coating shown cut-away (for clarity); -
FIG. 2 is a front elevation view of the heat exchanger ofFIG. 1 ; -
FIG. 3 is a perspective view of a fin of the type incorporated in the heat exchanger tube ofFIG. 1 ; -
FIG. 4 is a perspective view of a heat exchanger tube according to the second embodiment; -
FIG. 5 is a perspective view of a fin of the type incorporated in the heat exchanger tube ofFIG. 4 ; -
FIG. 6 is a perspective view of a heat exchanger tube assembly according to the third embodiment of the invention and comprising fins of the type depicted inFIG. 5 ; -
FIG. 7 is a front elevation view of a repeating unit of the type incorporated in the heat exchanger tube assembly shown inFIG. 6 ; and -
FIG. 8 is a perspective view of a heat exchanger tube assembly according to a fourth embodiment of the invention and comprising fins of the type depicted inFIG. 5 . -
FIGS. 1, 3 and 5 illustrate the first, second and third embodiments respectively. Each of those embodiments comprises at least one tube and a plurality of fins mounted thereto. Each fin has at least one aperture through which the tube is received. - The heat
exchanger tube assembly 10 according to the first embodiment is shown atFIGS. 1 and 2 and comprises atube 12 and a plurality offins 14 mounted to thetube 12. The tube is typically made from steel due to the robust properties provided by that material which enable it to withstand harsh environments. In particular, it has the ability to resist fatigue when subject to vibration, provided the system is designed appropriately. As well, it is able to withstand substantial knocks, impacts and the like. - Each
fin 14 has anaperture 16 through which thetube 12 is received and is also provided with aspacer 20 on an axial face thereof. In other embodiments, such spacers may be provided on both axial faces of each fin. Thespacers 20, which are located betweenadjacent fins 14, maintain a regular spacing between thosefins 14 along thetube 12. Thefins 14 are formed of generally the same material which, in the case of this embodiment, is steel. - A detailed view of a
fin 14 of the type used in the first embodiment is shown atFIG. 3 . - The
spacer 20 is integrally formed with thefins 14 and extends from the rim of theaperture 16 generally transversely to thefin 14. It is thereby positioned so as to be closely adjacent to the external surface of thetube 12. Thespacer 20 is configured as an annular flange so as to conform with the external surface of thetube 12. The annular flange is discontinuous around its circumference to provide a plurality of tabs around the rim of theaperture 16. In this embodiment, the tabs are disposed at regular angular intervals around the rim of theaperture 16. - The
fin 14 is produced from steel sheeting, theaperture 16 being stamped therein to be of a diameter which is such that theaperture 16 which will snugly receive thetube 12 therethrough. The stamping device is suitably formed to producetabs 20, initially in the plane of thefin 14. Thetabs 20 are then bent out of that plane to extend from the rim of the aperture. In the forming process, the tabs are suitably profiled to provide an inner surface to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin. - In the case of the embodiments described herein, each of the
fins 14 is discrete though, in alternative embodiments, the fins may be provided as a one-piece assembly such as in the form a helix. - The
fins 14 are bonded to thetube 12 byzinc 11 which is a thermally-conductive and corrosion resistant medium. Thezinc 11 occupies the regions between the external surface of thetube 12 and the inner radial faces both of thefins 14 and thetabs 20, giving rise to a substantially continuous bond between thefins 14 and thetube 12. The manner in which this is achieved is discussed further below. The substantially continuous bond provides for efficient heat transfer from the tube to the fins and also creates a relatively robust mounting of thefins 14 to thetube 12. The entire exterior of theheat exchanger tube 10 is also coated in zinc to render it corrosion-resistant. - The method of manufacturing the
heat exchanger tube 10 will now be described with reference to the drawings. Firstly, thefins 14, which may have been formed in the manner described above, are received over thetube 12 such that thespacer 20 of eachfin 14 abuts an adjacent fin 14 (best shown atFIG. 2 ). If it is felt necessary, thefins 14 may then be tack welded to thetube 12 to assist in locating thefins 14 in their desired position on thetube 12 prior to coating with thezinc 11. Alternatively, they may be of a sufficiently snug fit that no such welding is needed. - The
fins 14 andtube 12 forming theheat exchanger tube 10 are then hot-dipped in molten zinc to galvanise theheat exchanger tube 10. Hot-dipping of theheat exchanger tube 10 in zinc is advantageous in that it not only renders theheat exchanger tube 10 corrosion-resistant but simultaneously bonds thefins 14 to thetube 12. Moreover, the zinc, as applied by hot-dipping is pervasive and occupies the regions between the external surface of thetube 12 and the inner radial faces both of thefins 14 and thetabs 20, giving rise to the substantially continuous bond between thefins 14 and thetube 12 and thus providing for efficient heat transfer, as described above. - It will thus be appreciated that the
spacer 20 provides two functions: namely it acts to provide a definite, predefined spacing between adjoining fins to simply assembly of the fins as one fin may be pressed along thetube 12 until it contacts the spacer of the previous fin, and more importantly, the inner surface of thespacer 20 provides a broad area of contact withtube 12 to enable better transfer of heat from thetube 12 to thefin 14. In this regard a spacer comprising a continuous annular flange might well provide the best solution from this point of view. However, by segmenting thespacer 20 into tabs thefins 14 are more easily mounted to thetube 12 and it is even less likely that zinc will fail to penetrate between thetube 12 and the inner surface of thespacer 20 during the hot-dip process. - The
heat exchanger tube 10 is relatively robust, owing to thefins 14 being formed of steel, which is resistant to permanent deformation, and also due to the continuity and area, and thus the strength, of the zinc bond between the external surface of thetube 12 and the inner radial faces both of thefins 14 and thetabs 20. - It has been found that the use of steel fins with the inherently lower heat conductivity as compared with metals such as copper and aluminium results in little deterioration in overall performance of the heat exchanger. It is believed that this is partly due to the high thermal conductivity of the zinc and because the reduction in conductivity is compensated for by the improvement in the bond, and thus in the heat conductivity of the junction, between the
fins 14 and thetube 12. - Furthermore, galvanic corrosion between the
fins 14 and thetube 12 is eliminated because thefins 14 and thetube 12 are made of substantially the same material, while the zinc coating provides the well known galvanic protection to the assembly. In particular, corrosion at the junction between the fins and the tubes is eliminated. At the same time, the zinc coating provides stiffness to the fins and the tubes. In particular, in use, the steel fins are able to withstand the force of high pressure sprays used for cleaning without permanent deflection thereby better maintaining their cooling effectiveness during the life of the heat exchanger. - The heat
exchanger tube assembly 10, in addition to offering the abovementioned advantages, is relatively economic to manufacture. - The second embodiment of the invention is illustrated at
FIG. 4 . The second embodiment is a variation of the first embodiment though theheat exchanger tube 10 comprises a pair ofparallel tubes 12 respectively received through a pair ofapertures 16. - A
fin 14 of the type used in the second embodiment is shown atFIG. 5 . Thefin 14 is manufactured in an identical fashion to that which is incorporated in the first embodiment though it is formed with a pair ofapertures 16 each of which is provided with aspacer 20 identical to that described in connection with the first embodiment. - The advantage offered by the second embodiment, over the first, is that a given number of
fins 14 in this embodiment is sufficient for twotubes 12 rather than just one tube. This results in a saving in manufacturing costs because the labour required in cutting and/or stamping a single fin is not significantly greater than that required to produce a fin in accordance with the first embodiment. - A further advantage is a stiffening effect which is created along the axis between the pair of
adjacent tubes 12 as a result of their being tied together by thefins 14. This can reduce vibration, both of theheat exchanger tube 10 and in the heat exchanger generally, and thus increase the life of the heat exchanger. - The third embodiment of the invention, which is illustrated at
FIG. 6 , is a heatexchanger tube assembly 100 based on a variation of theheat exchanger tube 10 according to the second embodiment. The heatexchanger tube assembly 100 comprises a plurality oftubes 12 interconnected byfins 14 of the type illustrated inFIG. 5 . - The heat
exchanger tube assembly 100 is comprised of a series of repeating units, onesuch unit 40 being illustrated atFIG. 7 . Theunit 40 is similar to theheat exchanger tube 10 depicted atFIG. 4 thoughalternate fins 14′, along the length of one of thetubes 12′, do not extend to theother tube 12″ in thatunit 40, theunoccupied apertures 16′ of thosealternate fins 14′ instead being intended to receive anothertube 12″ of anidentical unit 40 shown in broken lines. - The
assembly 100 is formed from the desired number ofunits 40 prior to hot-dipping. As can be seen atFIG. 6 , thetubes 12 in thatassembly 100 need not be coplanar, thus enabling the configuration of theassembly 100 to be adjusted so as to conform with space restrictions and/or the layout of adjacent equipment. Indeed, the ability to interlink tubes with the fins in this manner enables novel heat exchanger configurations to be devised.FIG. 8 illustrates a fourth embodiment which shows anarrangement 110 providing a group of 8tubes 12 which are disposed in a octagonal configuration and interlinked withfins 14. As there are no end tubes, such a configuration has a high degree of inherent rigidity requiring little additional support. As well, such a configuration allows the cooling fluid to be either supplied or withdrawn from a direction parallel to thetubes 12, rather than transverse to them, which may be beneficial in certain applications. - Once that configuration has been suitably adjusted, the
fins 14 may be tack welded to therespective tubes 12, prior to hot-dipping, so as to assist in locating thefins 14 in their desired position on thetubes 12 and to maintain the configuration of theassembly 100. - An advantage offered by this embodiment, and shared by the second embodiment, is the stiffening effect which is created along the axis between the pairs of
adjacent tubes 12′ and 12″ as a result of their being tied together by thefins 14′. Such a stiffening effect is also realised along the axis between the pairs ofadjacent tubes 12′ and 12″ as a result of their being tied together by thefins 14′ and also thefins 14″. Thefins 14′ and 14″ thus offer lateral restraint totubes 12′ and 12″ throughout theassembly 100, thus possibly reducing vibration, both of theassembly 100 and in the heat exchanger generally and increasing the life of the heat exchanger. Moreover, it can be seen that the tube which is second-from-right inFIG. 5 is, advantageously, laterally restrained in two different axes, those axes extending between that tube and the tubes to its left and right (which are not coplanar) respectively. - As an alternative to the
unit 40 shown inFIG. 7 , units comprising fins of other profiles and having any number of apertures (i.e. possibly more than two apertures) are possible. It is clear that such units may be tied to other units, whether like or unlike, using suitably-profiled fins having appropriately-spaced apertures, those fins, depending on the arrangement of the apertures, being able to provide stiffening and lateral restraint along several different lateral axes. It should also be appreciated that the arrangement of thefins 14′ with respect to thefins 14″ need not be staggered as depicted inFIG. 6 , provided those fins still provide adequate lateral restraint, stiffening and heat transfer characteristics throughout the heat exchanger assembly. - It should be appreciated that the scope of the present invention need not be limited to the particular scope of the embodiments described above.
- Throughout the specification, unless the context requires otherwise, the word “comprise” or variations such as “comprises” or “comprising”, will be understood to imply the inclusion of a stated integer or group of integers but not the exclusion of any other integer or group of integers.
Claims (15)
1. A heat exchanger tube assembly comprising a tube having a plurality of fins mounted thereto at spaced intervals along its length, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin, the spacer being bonded to the tube by a thermally-conductive medium.
2. A heat exchanger tube assembly as claimed at claim 1 wherein the fins are formed of generally the same material as the tube.
3. A heat exchanger tube assembly as claimed at claim 2 wherein said material is a steel.
4. A heat exchanger tube assembly as claimed at claim 1 wherein the thermally conductive medium occupies a region between the external surface of the tube and the inner surface of the spacer to thereby enhance said heat transfer from the tube to the fin.
5. A heat exchanger tube assembly as claimed at claim 1 wherein each spacer is configured as an annular flange.
6. A heat exchanger tube assembly as claimed at claim 5 wherein said annular flange is discontinuous around the circumference of said tube.
7. A heat exchanger tube assembly as claimed at claim 5 wherein said annular flange comprises a plurality of tabs disposed around the circumference of said tube.
8. A heat exchanger tube assembly as claimed at claim 1 wherein said heat exchanger tube assembly is covered with a corrosion-resistant material.
9. A heat exchanger tube assembly as claimed at claim 8 wherein said corrosion-resistant material is said thermally-conductive medium.
10. A heat exchanger tube assembly as claimed at claim 1 wherein said thermally-conductive medium is zinc or zinc alloy.
11. A heat exchanger comprising a plurality of heat exchanger tube assemblies as claimed at claim 1 , said tubes being held in parallel spaced relation, adjacent tubes being interconnected by at least some of said fins, each tube being received through an aperture provided in said fins, each fin having at least two apertures to thereby interconnect adjacent tubes.
12. A heat exchanger comprising a plurality of heat exchanger tube assemblies as claimed at claim 1 , said tubes being held in parallel spaced relation, each tube being interconnected with at least one adjacent tube by a group of fins, each fin having two apertures to receive said adjacent tubes to thereby interconnect adjacent tubes.
13. A method of manufacturing a heat exchanger tube assembly, said method comprising the steps of mounting a plurality of fins to a tube and bonding the fins to the tube with a thermally-conductive medium, each fin having at least one aperture through which the tube is received, each fin having an integral spacer to define the spaced interval from an adjacent fin, the spacer extending from the rim of the aperture generally transversely to the fin to provide an inner surface profiled to contact and cooperate with the external surface of the tube to enhance heat transfer from the tube to the fin.
14. A method of manufacturing a heat exchanger tube assembly as claimed at claim 13 further comprising the step of covering the fins and tube with a corrosion-resistant material.
15. A method of manufacturing a heat exchanger tube assembly as claimed at claim 14 wherein the methods of bonding the fins to the tube and covering of the fins and tube comprises a hot-dip, zinc or zinc-alloy galvanising procedure.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2003905374 | 2003-10-02 | ||
| AU2003905374A AU2003905374A0 (en) | 2003-10-02 | Heat Exchanger Tube and Method of Manufacturing Same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050072562A1 true US20050072562A1 (en) | 2005-04-07 |
Family
ID=34382678
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/955,148 Abandoned US20050072562A1 (en) | 2003-10-02 | 2004-09-30 | Heat exchanger tube assembly |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20050072562A1 (en) |
| AU (2) | AU2004216619A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100307718A1 (en) * | 2009-06-05 | 2010-12-09 | Hon Fu Jin Precision Industry (Shenzhen) Co., Ltd. | Heat sink |
| US20110000254A1 (en) * | 2008-04-24 | 2011-01-06 | Mitsubishi Electric Corporation | Heat exchanger and air conditioner using the same |
| US9109844B2 (en) | 2012-03-01 | 2015-08-18 | Rheem Manufacturing Company | Nested helical fin tube coil and associated manufacturing methods |
| US10247481B2 (en) | 2013-01-28 | 2019-04-02 | Carrier Corporation | Multiple tube bank heat exchange unit with manifold assembly |
| US10337799B2 (en) | 2013-11-25 | 2019-07-02 | Carrier Corporation | Dual duty microchannel heat exchanger |
| US11346587B2 (en) * | 2019-08-09 | 2022-05-31 | Heatcraft Refrigeration Products Llc | Refrigeration heat exchangers with embedded fins |
| WO2024071025A1 (en) * | 2022-09-30 | 2024-04-04 | ダイキン工業株式会社 | Heat exchanger |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120199328A1 (en) | 2011-02-04 | 2012-08-09 | Ying Gong | Heat Exchanger Comprising a Tubular Element and a Heat Transfer Element |
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| US399493A (en) * | 1889-03-12 | I-eat-absorbing plate for cooling-coils | ||
| US2089340A (en) * | 1932-01-19 | 1937-08-10 | Moore Dry Kiln Co | Extended fin surface for conduits |
| US2184345A (en) * | 1938-12-31 | 1939-12-26 | United Aircraft Corp | Finned cylinder |
| US2426536A (en) * | 1944-07-07 | 1947-08-26 | Chase Brass & Copper Co | Laminated heat-exchange fin |
| US2475604A (en) * | 1943-11-02 | 1949-07-12 | Foster Wheeler Corp | Heat exchange apparatus |
| US2737370A (en) * | 1949-07-09 | 1956-03-06 | Frisch Martin | Extended surface element for heat exchanger |
| US4082869A (en) * | 1976-07-08 | 1978-04-04 | Raymond Anthony J | Semi-hot metallic extrusion-coating method |
| US5425414A (en) * | 1993-09-17 | 1995-06-20 | Evapco International, Inc. | Heat exchanger coil assembly |
-
2004
- 2004-09-30 AU AU2004216619A patent/AU2004216619A1/en not_active Abandoned
- 2004-09-30 US US10/955,148 patent/US20050072562A1/en not_active Abandoned
-
2010
- 2010-10-14 AU AU2010233051A patent/AU2010233051A1/en not_active Abandoned
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US399493A (en) * | 1889-03-12 | I-eat-absorbing plate for cooling-coils | ||
| US2089340A (en) * | 1932-01-19 | 1937-08-10 | Moore Dry Kiln Co | Extended fin surface for conduits |
| US2184345A (en) * | 1938-12-31 | 1939-12-26 | United Aircraft Corp | Finned cylinder |
| US2475604A (en) * | 1943-11-02 | 1949-07-12 | Foster Wheeler Corp | Heat exchange apparatus |
| US2426536A (en) * | 1944-07-07 | 1947-08-26 | Chase Brass & Copper Co | Laminated heat-exchange fin |
| US2737370A (en) * | 1949-07-09 | 1956-03-06 | Frisch Martin | Extended surface element for heat exchanger |
| US4082869A (en) * | 1976-07-08 | 1978-04-04 | Raymond Anthony J | Semi-hot metallic extrusion-coating method |
| US5425414A (en) * | 1993-09-17 | 1995-06-20 | Evapco International, Inc. | Heat exchanger coil assembly |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110000254A1 (en) * | 2008-04-24 | 2011-01-06 | Mitsubishi Electric Corporation | Heat exchanger and air conditioner using the same |
| US8037699B2 (en) * | 2008-04-24 | 2011-10-18 | Mitsubishi Electric Corporation | Heat exchanger and air conditioner using the same |
| US20100307718A1 (en) * | 2009-06-05 | 2010-12-09 | Hon Fu Jin Precision Industry (Shenzhen) Co., Ltd. | Heat sink |
| US9109844B2 (en) | 2012-03-01 | 2015-08-18 | Rheem Manufacturing Company | Nested helical fin tube coil and associated manufacturing methods |
| US10247481B2 (en) | 2013-01-28 | 2019-04-02 | Carrier Corporation | Multiple tube bank heat exchange unit with manifold assembly |
| US10337799B2 (en) | 2013-11-25 | 2019-07-02 | Carrier Corporation | Dual duty microchannel heat exchanger |
| US11346587B2 (en) * | 2019-08-09 | 2022-05-31 | Heatcraft Refrigeration Products Llc | Refrigeration heat exchangers with embedded fins |
| WO2024071025A1 (en) * | 2022-09-30 | 2024-04-04 | ダイキン工業株式会社 | Heat exchanger |
| JP7464872B1 (en) | 2022-09-30 | 2024-04-10 | ダイキン工業株式会社 | Heat exchanger |
| JP2024054878A (en) * | 2022-09-30 | 2024-04-18 | ダイキン工業株式会社 | Heat exchanger |
Also Published As
| Publication number | Publication date |
|---|---|
| AU2010233051A1 (en) | 2010-11-04 |
| AU2004216619A1 (en) | 2005-04-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: GLENTEN PTY LTD., AUSTRALIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HALL, PETER DAVID;REEL/FRAME:015372/0798 Effective date: 20040930 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |