US3309763A - Method for making a heat exchanger - Google Patents

Method for making a heat exchanger Download PDF

Info

Publication number
US3309763A
US3309763A US413675A US41367564A US3309763A US 3309763 A US3309763 A US 3309763A US 413675 A US413675 A US 413675A US 41367564 A US41367564 A US 41367564A US 3309763 A US3309763 A US 3309763A
Authority
US
United States
Prior art keywords
fin
section
fin stock
sections
bending
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.)
Expired - Lifetime
Application number
US413675A
Inventor
Edward P Oddy
Klnal Lubomyr
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.)
Borg Warner Corp
Original Assignee
Borg Warner Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US246069A external-priority patent/US3182481A/en
Application filed by Borg Warner Corp filed Critical Borg Warner Corp
Priority to US413675A priority Critical patent/US3309763A/en
Application granted granted Critical
Publication of US3309763A publication Critical patent/US3309763A/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F28F1/24Tubular 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
    • F28F1/32Tubular 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00Making other particular articles
    • B21D53/02Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers
    • B21D53/08Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers of both metal tubes and sheet metal
    • B21D53/085Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers of both metal tubes and sheet metal with fins places on zig-zag tubes or parallel tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/053Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
    • F28D1/0535Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2240/00Spacing means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49377Tube with heat transfer means
    • Y10T29/49378Finned tube
    • Y10T29/4938Common fin traverses plurality of tubes

Definitions

  • This invention relates to a self-stacking fin structure for tube and fin heat exchangers and methods for manufacturing the same.
  • Self-stacking fins for radiators and the like are known, for example, in Krackowizer, US. Patent No. 2,047,207. Radiators of this type are assembled in a conventional manner by arranging a plurality of cooling fins in generally parallel relation, inserting a series of fluid conducting tube elements through apertures provided in said fins, and then joining opposite ends of the tubes to header assemblies above and below the fin structure. The assembled unit is then soldered or brazed to join the several elements together into a unitary structure.
  • FIGURE 1 is a front elevational view of a heat exchanger constructed in accordance with the principles of the present invention
  • FIGURE 2 is a top plan view of a portion of a heat exchanger fin element used in the heat exchanger illustrated in FIGURE 1;
  • FIGURE 3 is an end view of the portion of a fin element taken along section lines 33 of FIGURE 2;
  • FIGURE 4 illustrates a second embodiment of a fin element
  • FIGURE 5 illustrates a third embodiment of a fin element
  • FIGURE 6 is an isometric View of a punch and die assembly employed to form the single self spacers illustrated in FIGURES 2, 3, and 4;
  • - IGURE 7 is a detailed view of the male punch element used in the assembly of FIGURE 6;
  • FIGURE 8 is a view of a punch assembly used to form the self spacers illustrated in FIGURE 5;
  • FIGURE 9 is a detailed elevational view of the male punch of FIGURE 8.
  • FIGURE 10 is a schematic illustration of a continuous manufacturing procedure for assembly of the fin stock
  • FIGURE 11 is a top plan view, partly schematic, of
  • FIGURE 12 is a detailed top plan view of the fin stock prior to the folding operation
  • FIGURE 13 is the preferred configuration of the spacer lug as viewed along lines 13l13 in FIGURE 3;
  • FIGURES 14, 15, and 16 illustrate alternate embodiments of the spacer elements.
  • a heat exchanger generally indicated by the numeral 1 is shown having supply and receiving headers 2 and 3 interconnected by a plurality of tubes 5.
  • the tubes in a preferred embodiment, are of the flat type to reduce the resistance to air flow through the unit although it should be understood that they may have any cross-sectional configuration desired.
  • a plurality of fin elements 7 Arranged parallel to the headers 2 and 3 are a plurality of fin elements 7 having apertures 8, FIGURE 2, for the reception of the tubes 5.
  • a plurality of spacers or lugs 10 are provided, said spacers being formed from the fin sheets by punching out or extruding a small, rectangular shaped section of said sheet and bending the same to a position perpendicular to the plane of the fin.
  • Each tube aperture 8 includes a surrounding flange to insure a more secure connection between the fins and the tubes.
  • the fins may be connected to the tubes in any well known manner, but it is expeditious to use a soldering or brazing process. 1
  • each fin element includes a series of spaced elongated tube apertures 8 arranged in rows running lengthwise of the fin.
  • the tube apertures in one row are preferably staggered with respect to the other row to increase the effective area of heat exchange.
  • each said spacer is formed by cutting an aperture in a strip of fin stock such that the material in the aperture is not severed completely from the fin stock and by bending or extruding the unsevered aperture material upwardly or downwardly with respect to the strip.
  • the edges of each spacer are curled back or convoluted toward each other so that it provides one edge integrally connected to the fin itself and another edge adapted to contact the fin element immediately above or below it.
  • a very important aspect of the present invention consists in the curling of the outer ends of the spacer element around toward each other. By means of this feature an extremely rigid element is formed which resists deformation.
  • the spacer elements are positioned between adjacent tube apertures in each row so that the spacers are staggered with respect to each other.
  • the resistance to flow caused by the spacer elements is not significantly greater than that caused by the tubes themselves. While not required, it has been found to be desirable to provide turbulizer elements spaced around each fin spacer. These turbulization elements form no part of the present invention and are to be regarded as purely optional.
  • an alternative design may include the spacer elements formed by punching the edge of the fin stock so that the spacer elements are spaced slightly inwardly from the edge.
  • the spacers might be placed at random throughout the available space not taken up by the tube apertures.
  • the spacers moreover, may be oriented longitudinally or transversely with respect to the fin or may be located at any angle with respect to the longitudinal axis of said fin element.
  • the edge spacers (FIGURE 4) may be combined with the centrally disposed spacers (FIGURE 2) and may include various combinations of the randomly oriented spacers.
  • FIGURE 5 illustrates a third embodiment of a spacer element which comprises a double spacer element having lugs arranged in pairs.
  • both lugs are formed by a single punching operation.
  • FIGURES 6 and 7 a punch assembly adapted to form the single lug spacer elements shown in FIGURES 2, 3, and 4 is disclosed.
  • This punch assembly includes a die plate 12 having a rectangular opening 14 extending therethrough, a base plate 16, and a punch 18 carried by said base plate extending perpendicular to said base plate.
  • a conventional stripper plate (not shown) may be provided to facilitate withdrawal of the punch from the fin stock after the spacer element has been formed.
  • the punch 18, shown in greater detail in FIGURE 6, comprises a bifurcated member having a pair of sharp cutting prongs 22 on opposite sides thereof and face 24 sloping downwardly from a transversely extending cutting edge 26.
  • the pair of cutting prongs 22 cut the strip at opposite ends of an imaginary rectangular section in the strip.
  • the transversely extending cutting edge 26 engages the strip cutting the third side from the rectangular element.
  • Further movement of the punch causes the spacer element to be engaged by the sloping face 24 and is bent upwardly from the plane of the strip. Throughout this entire operation, the edges of the spacer element are bent inwardly toward each other to provide the configuration discussed above having improved rigidity characteristics.
  • This punch element results in the spacer element being produced, i.e., pierced and formed with a single tool and with a single stroke of said tool.
  • the punch assembly employed for forming the double lug spacer element (FIGURE 5) is illustrated in FIG- UR'ES 8 and 9.
  • the double lug punch design which may be regarded as a paired set of single lug punches, comprises a punch body 20 having front, rear, and side faces 20a, 20b, and 200 respectively.
  • a slot 21 extending through one end of the punch body 20 from the front face 20a to the rear face 2% divides the end of the punch body into two substantially identical single lug punches each of which includes a bifurcated member 27 having a pair of spaced cutting prongs 22a, a transversely extending cutting edge 26a, and a face 24a sloping downwardly from said cutting edge to the side faces of the punch body.
  • the operation of the punch is substantially the same as that described above in connection with the single lug punch, the only difference being that a slug or blank 27 is formed between the two transversely extending cutting edges 26a as the spacer lugs are bent upwardly from the plane of the strip to positions on opposite sides of the aperture formed by the punch.
  • FIGURES 10 illustrates, in diagrammatic form, a continuous process for manufacturing the fin assemblies of the present invention.
  • FIGURES 11 and 12 which illustrate the strip of fin stock at various stages corresponding to operations performed during the manufacturing process may also be referred to for a complete understanding of the process.
  • a continuous strip of thin metal fin stock is fed from a first station, where it is stored in a roll or any other convenient manner, and delivered to a second station where a plurality of longitudinally spaced groups of slits 30, 31 (FIGURE 11) are formed therein.
  • This operation may be performed by a plurality of reciprocating knives 35, 36.
  • Each group of slits comprises a series of spaced, coaligned individual slits 30a, 31a running transversely from one edge of the strip toward the other so as to provide a series of unsevered portions 30b, 3111 between the ends of the slits.
  • the slit of one group are staggered or offset with respect to the slits of an adjacent group so that the unsevered portions are similarly staggered.
  • the fin stock is fed to a third station which is provided with a die press 40.
  • the operation of the die press is intermittent and in timed relation with respect to the movement of the fin stock so that the die press performs its operations on alternate spaced apart areas A between adjacent groups of slits.
  • the first die press 40 arranged so that the punches and other forming elements move upwardly into the strip, carries out the following operations: (1)
  • the tube apertures 8 are formed so that a narrow flange surrounding each aperture extends upwardly from the plane of the strip; (2)
  • the spacer elements which may be of any previously described design, are formed so that these also extend upwardly from the plane of the strip; and (3)
  • a series of relatively short, longitudinally extending slits are provided, each said slit intersects the terminal portions of the transversely extending slits to Provide a series of integral tie elements joining adjacent sections of the fin stock.
  • These tie elements may be formed by a double pronged punch element similar to that shown in FIGURES 6 and 7 so as to obtain a convoluted reinforcing edge similar to those on the spacing lugs.
  • the same operations performed at the third station are repeated by die press 41, but the die press punching and cutting elements all operate downwardly on the fin stock on the remaining alternate areas A thereof.
  • the spacer elements, the tube aperture flanges, and the tie elements alternately extend downwardly and upwardly from the plane of the strip throughout its length.
  • the strip is bent alternately in opposite directions along the lines coincident with the transversely extending slits to form a corrugated or pleated pattern with the tube apertures in the respective fin plates coaxially arranged. Since alternate areas are provided with oppositely extending tube flanges and spacing lugs, after the strip is folded, the flanges and lugs will all extend in the same direction.
  • the tubes are inserted through the coaxially arranged tube apertures, the headers are connected to the opposite ends of the tube apertures, and then the assembly is bonded together in a unitary construction by brazing, soldering, or some equivalent method.
  • FIGURE 12 a detailed plan view of a section of the Strip just prior to the folding operation, illustrates the optional turbulizer elements 43.
  • the latter merely comprise small polygonal shaped apertures, formed with ragged edges, said edges extending generally perpendicular to the plane of the fin plates. The ragged edges disrupt the flow of air past the fin plates and prevent laminar flow of air past said plates thereby increasing the heat exchange efliciency of the unit.
  • FIGURES 14, 15, and 16 Several alternate embodiments of the spacer elements and tie elements are illustrated in FIGURES 14, 15, and 16.
  • the spacer and tie elements are formed in the same general manner as the spacer and tie elements illustrated in FIGURE 13; the basic difference being in the physical configuration of the punch elements used to form the tie and spacer elements.
  • a method of forming a fin structure from an elongated strip of fin stock comprising the steps of:
  • a method of forming a fin structure from an elongated strip of fin stock comprising the steps of z (a) forming a plurality of co-aligned transverse parallel slits in said fin stock defining integral tie elements between said co-aligned transverse slits and a plurality of first sections and second sections of said stock;
  • a method of forming a fin structure from an elonv gated strip of fin stock comprising the steps of:
  • a method of forming a fin structure from an elongated strip of fin stock comprising the steps of:

Description

March 21, 1957 E. P. ODDY ET AL 3,399,763
METHOD FOR MAKING A HEAT EXCHANGER Original Filed Dec. 20, 1962 3 Sheets-Sheet 1 In venibro and March 21, 1957 Original Filed Dec. 20, 1962 z srAr/alv E. P. ODDY ET AL k E v,
METHOD FOR MAKING A HEAT EXCHANGER 5 Sheets-Sheet 2 In venj'arts' March 21, 1967 p, ODDY ET AL 3,3@9,763
METHOD FOR MAKING A HEAT EXCHANGER Original Filed Dec. 20, 1962 5 Sheets-Sheet 3 4 227672250715" fdwarcifodajy and JO/7:517, ffz'raaz a 2" QUE/f (7 2 United States Patent Ofifice 3,309,763 Patented Mar. 21, 1967 3,309,763 METHOD FOR MAKING A HEAT EXCHANGER Edward P. Oddy and Lubomyr Kinal, Detroit, Mich, as-
signors to Borg-Jamar Corporation, Chicago, Ill., a corporation of Illinois Original application Dec. 20, 1962, Ser. No. 246,069, now Patent No. 3,182,481, dated May 11, 1965. Divided and this application Oct. 29, 1964, Ser. No. 413,675
4 Claims. (1. 29--157.3)
This application is a division of application, Ser. No. 246,069, Edward P. Oddy et al., entitled, Heat Exchanger and Method of Its Manufacture, filed Dec. 20, 1962, and now US Patent No. 3,182,481.
This invention relates to a self-stacking fin structure for tube and fin heat exchangers and methods for manufacturing the same.
Self-stacking fins for radiators and the like are known, for example, in Krackowizer, US. Patent No. 2,047,207. Radiators of this type are assembled in a conventional manner by arranging a plurality of cooling fins in generally parallel relation, inserting a series of fluid conducting tube elements through apertures provided in said fins, and then joining opposite ends of the tubes to header assemblies above and below the fin structure. The assembled unit is then soldered or brazed to join the several elements together into a unitary structure.
One particular problem present in prior art structures is the tendency of the fins to deform under pressure while being handled during assembly or in other stages of manufacture. A principal cause of this problem is that the spacer elements used to separate the fins from one another have not been rigid enough to withstand anything but the most careful handling. This problem is especially present in the production of radiator fins of the type employing a relatively thin metal fin stock on the order of .0025.003 inch. Since the most acceptable fin stock must necessarily have a high coeflicient of thermal conductivity, the choice of materials is usually either copper or aluminum, both of which are easily deformed.
It is another object of the invention to provide an improved method of manufacturing tube and fin heat exchan ers, either in a continuous process or by utilizing individual fin elements.
Gther and more particular objects and advantages of the present invention will be apparent from the following detailed description and the appended drawings, wherein:
FIGURE 1 is a front elevational view of a heat exchanger constructed in accordance with the principles of the present invention;
FIGURE 2 is a top plan view of a portion of a heat exchanger fin element used in the heat exchanger illustrated in FIGURE 1;
FIGURE 3 is an end view of the portion of a fin element taken along section lines 33 of FIGURE 2;
FIGURE 4 illustrates a second embodiment of a fin element;
FIGURE 5 illustrates a third embodiment of a fin element;
FIGURE 6 is an isometric View of a punch and die assembly employed to form the single self spacers illustrated in FIGURES 2, 3, and 4;
- IGURE 7 is a detailed view of the male punch element used in the assembly of FIGURE 6;
FIGURE 8 is a view of a punch assembly used to form the self spacers illustrated in FIGURE 5;
FIGURE 9 is a detailed elevational view of the male punch of FIGURE 8;
FIGURE 10 is a schematic illustration of a continuous manufacturing procedure for assembly of the fin stock;
FIGURE 11 is a top plan view, partly schematic, of
the assembly process, at various stages, and is related to FIGURE 10;
FIGURE 12 is a detailed top plan view of the fin stock prior to the folding operation;
FIGURE 13 is the preferred configuration of the spacer lug as viewed along lines 13l13 in FIGURE 3; and
FIGURES 14, 15, and 16 illustrate alternate embodiments of the spacer elements.
Referring now to FIGURE 1, a heat exchanger generally indicated by the numeral 1 is shown having supply and receiving headers 2 and 3 interconnected by a plurality of tubes 5. The tubes, in a preferred embodiment, are of the flat type to reduce the resistance to air flow through the unit although it should be understood that they may have any cross-sectional configuration desired. Arranged parallel to the headers 2 and 3 are a plurality of fin elements 7 having apertures 8, FIGURE 2, for the reception of the tubes 5. In order to space the fin elements to afford the self-stacking capability a plurality of spacers or lugs 10 are provided, said spacers being formed from the fin sheets by punching out or extruding a small, rectangular shaped section of said sheet and bending the same to a position perpendicular to the plane of the fin. Each tube aperture 8 includes a surrounding flange to insure a more secure connection between the fins and the tubes. The fins may be connected to the tubes in any well known manner, but it is expeditious to use a soldering or brazing process. 1
As shown in FIGURE 2, each fin element includes a series of spaced elongated tube apertures 8 arranged in rows running lengthwise of the fin. The tube apertures in one row are preferably staggered with respect to the other row to increase the effective area of heat exchange.
Referring now in more detail to the tube spacers, each said spacer is formed by cutting an aperture in a strip of fin stock such that the material in the aperture is not severed completely from the fin stock and by bending or extruding the unsevered aperture material upwardly or downwardly with respect to the strip. The edges of each spacer are curled back or convoluted toward each other so that it provides one edge integrally connected to the fin itself and another edge adapted to contact the fin element immediately above or below it. A very important aspect of the present invention consists in the curling of the outer ends of the spacer element around toward each other. By means of this feature an extremely rigid element is formed which resists deformation.
In the embodiment shown in FIGURE 2, the spacer elements are positioned between adjacent tube apertures in each row so that the spacers are staggered with respect to each other. By positioning each spacer element immediately in front of one of the tubes, the resistance to flow caused by the spacer elements is not significantly greater than that caused by the tubes themselves. While not required, it has been found to be desirable to provide turbulizer elements spaced around each fin spacer. These turbulization elements form no part of the present invention and are to be regarded as purely optional.
As shown in FIGURE 4, an alternative design may include the spacer elements formed by punching the edge of the fin stock so that the spacer elements are spaced slightly inwardly from the edge. Various combinations of the edge design and the design shown in FIGURE 2, are contemplated. For example, the spacers might be placed at random throughout the available space not taken up by the tube apertures. The spacers, moreover, may be oriented longitudinally or transversely with respect to the fin or may be located at any angle with respect to the longitudinal axis of said fin element. It is further contemplated that the edge spacers (FIGURE 4) may be combined with the centrally disposed spacers (FIGURE 2) and may include various combinations of the randomly oriented spacers.
FIGURE 5 illustrates a third embodiment of a spacer element which comprises a double spacer element having lugs arranged in pairs. By using a special punch, to be described below, both lugs are formed by a single punching operation.
In FIGURES 6 and 7 a punch assembly adapted to form the single lug spacer elements shown in FIGURES 2, 3, and 4 is disclosed. This punch assembly includes a die plate 12 having a rectangular opening 14 extending therethrough, a base plate 16, and a punch 18 carried by said base plate extending perpendicular to said base plate. A conventional stripper plate (not shown) may be provided to facilitate withdrawal of the punch from the fin stock after the spacer element has been formed. The punch 18, shown in greater detail in FIGURE 6, comprises a bifurcated member having a pair of sharp cutting prongs 22 on opposite sides thereof and face 24 sloping downwardly from a transversely extending cutting edge 26. As the punch element is forced through the fin stock, the pair of cutting prongs 22 cut the strip at opposite ends of an imaginary rectangular section in the strip. As the punch is further extended through the strip, the transversely extending cutting edge 26 engages the strip cutting the third side from the rectangular element. Further movement of the punch causes the spacer element to be engaged by the sloping face 24 and is bent upwardly from the plane of the strip. Throughout this entire operation, the edges of the spacer element are bent inwardly toward each other to provide the configuration discussed above having improved rigidity characteristics. This punch element results in the spacer element being produced, i.e., pierced and formed with a single tool and with a single stroke of said tool.
The punch assembly employed for forming the double lug spacer element (FIGURE 5) is illustrated in FIG- UR'ES 8 and 9. The double lug punch design, which may be regarded as a paired set of single lug punches, comprises a punch body 20 having front, rear, and side faces 20a, 20b, and 200 respectively. A slot 21 extending through one end of the punch body 20 from the front face 20a to the rear face 2% divides the end of the punch body into two substantially identical single lug punches each of which includes a bifurcated member 27 having a pair of spaced cutting prongs 22a, a transversely extending cutting edge 26a, and a face 24a sloping downwardly from said cutting edge to the side faces of the punch body. The operation of the punch is substantially the same as that described above in connection with the single lug punch, the only difference being that a slug or blank 27 is formed between the two transversely extending cutting edges 26a as the spacer lugs are bent upwardly from the plane of the strip to positions on opposite sides of the aperture formed by the punch.
FIGURES 10 illustrates, in diagrammatic form, a continuous process for manufacturing the fin assemblies of the present invention. FIGURES 11 and 12 which illustrate the strip of fin stock at various stages corresponding to operations performed during the manufacturing process may also be referred to for a complete understanding of the process.
Referring first to FIGURE 10, a continuous strip of thin metal fin stock is fed from a first station, where it is stored in a roll or any other convenient manner, and delivered to a second station where a plurality of longitudinally spaced groups of slits 30, 31 (FIGURE 11) are formed therein. This operation may be performed by a plurality of reciprocating knives 35, 36.
Each group of slits comprises a series of spaced, coaligned individual slits 30a, 31a running transversely from one edge of the strip toward the other so as to provide a series of unsevered portions 30b, 3111 between the ends of the slits. In a preferred embodiment, the slit of one group are staggered or offset with respect to the slits of an adjacent group so that the unsevered portions are similarly staggered.
After the slits are formed, the fin stock is fed to a third station which is provided with a die press 40. The operation of the die press is intermittent and in timed relation with respect to the movement of the fin stock so that the die press performs its operations on alternate spaced apart areas A between adjacent groups of slits. The first die press 40, arranged so that the punches and other forming elements move upwardly into the strip, carries out the following operations: (1) The tube apertures 8 are formed so that a narrow flange surrounding each aperture extends upwardly from the plane of the strip; (2) The spacer elements, which may be of any previously described design, are formed so that these also extend upwardly from the plane of the strip; and (3) A series of relatively short, longitudinally extending slits are provided, each said slit intersects the terminal portions of the transversely extending slits to Provide a series of integral tie elements joining adjacent sections of the fin stock. These tie elements may be formed by a double pronged punch element similar to that shown in FIGURES 6 and 7 so as to obtain a convoluted reinforcing edge similar to those on the spacing lugs.
At a fourth station, the same operations performed at the third station are repeated by die press 41, but the die press punching and cutting elements all operate downwardly on the fin stock on the remaining alternate areas A thereof. Thus, the spacer elements, the tube aperture flanges, and the tie elements alternately extend downwardly and upwardly from the plane of the strip throughout its length.
At a fifth station, the strip is bent alternately in opposite directions along the lines coincident with the transversely extending slits to form a corrugated or pleated pattern with the tube apertures in the respective fin plates coaxially arranged. Since alternate areas are provided with oppositely extending tube flanges and spacing lugs, after the strip is folded, the flanges and lugs will all extend in the same direction. After the fin plates have been gathered and formed into the compressed arrangement shown at the left of FIGURE 10, the tubes are inserted through the coaxially arranged tube apertures, the headers are connected to the opposite ends of the tube apertures, and then the assembly is bonded together in a unitary construction by brazing, soldering, or some equivalent method.
FIGURE 12, a detailed plan view of a section of the Strip just prior to the folding operation, illustrates the optional turbulizer elements 43. The latter merely comprise small polygonal shaped apertures, formed with ragged edges, said edges extending generally perpendicular to the plane of the fin plates. The ragged edges disrupt the flow of air past the fin plates and prevent laminar flow of air past said plates thereby increasing the heat exchange efliciency of the unit.
Several alternate embodiments of the spacer elements and tie elements are illustrated in FIGURES 14, 15, and 16. The spacer and tie elements are formed in the same general manner as the spacer and tie elements illustrated in FIGURE 13; the basic difference being in the physical configuration of the punch elements used to form the tie and spacer elements.
What is claimed is:
'1. A method of forming a fin structure from an elongated strip of fin stock comprising the steps of:
(a) forming a plurality of transverse parallel slits in said fin stock defining at least one first section and at least one second section of said stock;
(b) forming a first series of tube apertures in said first section of said fin stock by bending a portion of said fin stock upwardly from said first section and a plurality of spacer elements having convoluted ends bent toward each other in said first section by bending a portion of said fin stock upwardly from said first section and bending said edges toward each other;
(e) forming a second series of tube apertures in said second section of said fin stock by bending a portion of said fin stock downwardly from said second section and a plurality of spacer elements having convoluted edges bent toward each other in said second section by bending a portion of said fin stock downwardly from said second section and bending said edges toward each other;
(d) folding one of said sections toward the other thereof such that said tube apertures are coaligned and said spacer elements of each said sections extend in the same direction with the spacer elements of one of said sections contacting the fin stock of said other of said sections, and v (e) inserting a plurality of tubes in said tube apertures.
2. A method of forming a fin structure from an elongated strip of fin stock comprising the steps of z (a) forming a plurality of co-aligned transverse parallel slits in said fin stock defining integral tie elements between said co-aligned transverse slits and a plurality of first sections and second sections of said stock;
(b) forming a first series of tube apertures in said first sections of said fin stock by bending a portion of said fin stock upwardly from said first sections and a plurality of spacer elements having convoluted ends bent toward each other in said first sections by bending a portion of said fin stock upwardly from said first sections and bending said edges toward each other;
(c) forming a second series of tube apertures in said second sections of said fin stock by bending a portion of said fin stock downwardly from said second sections and a plurality of spacer elements having convoluted edges bent toward each other in said second sections by bending a portion of said fin stock downwardly from said second sections and bending said edges toward each other;
(d) folding said sections such that said tube apertures are co-aligned and said spacer elements of each said sections extend in the same direction with the spacer elements of said sections contacting the fin stock of the next adjacent section and said tie elements extend between said folded fin stock alternately on opposite edges of said fin stock, and
(e) inserting a plurality of tubes in said tube apertures.
3. A method of forming a fin structure from an elonv gated strip of fin stock comprising the steps of:
(a) forming a plurality of transverse parallel slits in said fin stock defining at least one first section and at least one second section of said stock;
(b) forming a first series of tube apertures in said first section of said fin stock by bending a portion of said fin stock upwardly from said first section, a plurality of spacer elements having convoluted ends bent toward each other in said first section by bending a portion of said fin stock upwardly from said first section and bending said edges toward each other; a second series of tube apertures in said second section of said fin stock by bending a portion of said fin stock downwardly from said second section, and a plurality of spacer elements having convoluted edges bent toward each other in said second section by bending a portion of said fin stock downwardly from said second section and bending said edges toward each other;
(c) folding one of said sections toward the other thereof such that said tube apertures are co-aligned and said spacer elements of each said sections extend in the same direction with the space-r elements of one of said sections contacting the fin stock of said other of said sections, and
(d) inserting a plurality of tubes in said tube apertures.
4. A method of forming a fin structure from an elongated strip of fin stock comprising the steps of:
(a) forming a plurality of co-aligned transverse parallel slits in said fin stock defining integral tie elements between said co-aligned transverse slits and a plurality of first sections and second sections of said stock;
(b) bending edge portions of said tie elements toward each other to form re-enforcing edges on said tie elements;
(c) forming -a first series of tube apertures in said first sections of said fin stock by bending a portion of said fin stock upwardly from said first sections and a plurality of spacer elements having convoluted ends bent toward each other in said first sections by bending a portion of said fin stock upwardly from said first sections and bending said edges toward each other;
(d) forming a second series of tube apertures in said second sections of said fin stock by bending a portion of said fin stock downwardly from said second sections and a plurality of spacer elements having convoluted edges bent toward each other in said second sections by bending a portion of said fin stock downwardly from said second sections and bending said edges toward each other;
(e) folding said sections such that said tube apertures are co-aligned and said spacer elements of each said sections extend in the same direction with the spacer elements of said sections contacting the fin stock of the next adjacent section and said tie elements extend between said folded fin stock alternately on opposite edges of said fin stock with said reinforcing sections of said tie elements contacting adjacent sections of said fin stock, and
(t) inserting a plurality of tubes in said tube apertures.
References Cited by the Examiner UNITED STATES PATENTS 2,047,207 7/ 1936 Krackowizer 29157.3 X 2,428,145 9/1947 Cook --15l 2,977,918 4/1961 Kritzer 29-1573 X 3,223,153 12/1965 Simpelaur 165152 3,228,367 1/1966 Donaldson 1l3ll8 JOHN F. CAMPBELL, Primary Examiner.
WHITMORE A. WILTZ, Examiner.
J. D. HOBART, Assistant Examiner,

Claims (1)

1. A METHOD OF FORMING A FIN STRUCTURE FROM AN ELONGATED STRIP OF FIN STOCK COMPRISING THE STEPS OF: (A) FORMING A PLURALITY OF TRANSVERSE PARALLEL SLITS IN SAID FIN STOCK DEFINING AT LEAST ONE FIRST SECTION AND AT LEAST ONE SECOND SECTION OF SAID STOCK; (B) FORMING A FIRST SERIES OF TUBE APERTURES IN SAID FIRST SECTION OF SAID FIN STOCK BY BENDING A PORTION OF SAID FIN STOCK UPWARDLY FROM SAID FIRST SECTION AND A PLURALITY OF SPACER ELEMENTS HAVING CONVOLUTED ENDS BENT TOWARD EACH OTHER IN SAID FIRST SECTION BY BENDING A PORTION OF SAID FIN STOCK UPWARDLY FROM SAID FIRST SECTION AND BENDING SAID EDGES TOWARD EACH OTHER; (C) FORMING A SECOND SERIES OF TUBE APERTURES IN SAID SECOND SECTION OF SAID FIN STOCK BY BENDING A PORTION OF SAID FIN STOCK DOWNWARDLY FROM SAID SECOND SECTION AND A PLURALITY OF SPACER ELEMENTS HAVING CONVOLUTED EDGES BENT TOWARD EACH OTHER IN SAID SECOND SECTION BY BENDING A PORTION OF SAID FIN STOCK DOWNWARDLY FROM SAID SECOND SECTION AND BENDING SAID EDGES TOWARD EACH OTHER; (D) FOLDING ONE OF SAID SECTIONS TOWARD THE OTHER THEREOF SUCH THAT SAID TUBE APERTURES ARE COALIGNED AND SAID SPACER ELEMENTS OF EACH SAID SECTIONS EXTEND IN THE SAME DIRECTION WITH THE SPACER ELEMENTS OF ONE OF SAID SECTIONS CONTACTING THE FIN STOCK OF SAID OTHER OF SAID SECTIONS, AND (E) INSERTING A PLURALITY OF TUBES IN SAID TUBE APERTURES.
US413675A 1962-12-20 1964-10-29 Method for making a heat exchanger Expired - Lifetime US3309763A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US413675A US3309763A (en) 1962-12-20 1964-10-29 Method for making a heat exchanger

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US246069A US3182481A (en) 1962-12-20 1962-12-20 Heat exchanger and method of its manufacture
US413675A US3309763A (en) 1962-12-20 1964-10-29 Method for making a heat exchanger

Publications (1)

Publication Number Publication Date
US3309763A true US3309763A (en) 1967-03-21

Family

ID=26937692

Family Applications (1)

Application Number Title Priority Date Filing Date
US413675A Expired - Lifetime US3309763A (en) 1962-12-20 1964-10-29 Method for making a heat exchanger

Country Status (1)

Country Link
US (1) US3309763A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2832789A1 (en) * 2001-11-27 2003-05-30 Valeo Thermique Moteur Sa Automobile heat exchanger fin module comprise plane metal plate divided into two parts by long slots between which bands of material forming bridges between fin parts extend
EP1586844A1 (en) * 2002-12-25 2005-10-19 T.RAD Co,.Ltd Plate fin for heat exchanger and heat exchanger core
WO2006005594A1 (en) * 2004-07-12 2006-01-19 Behr Gmbh & Co. Kg Heat exchanger, especially for motor vehicles
US20130284416A1 (en) * 2011-01-21 2013-10-31 Daikin Industries, Ltd. Heat exchanger and air conditioner
US20130299141A1 (en) * 2011-01-21 2013-11-14 Daikin Industries, Ltd. Heat exchanger and air conditioner
US20130299152A1 (en) * 2011-01-21 2013-11-14 Daikin Industries, Ltd. Heat exchanger and air conditioner

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2047207A (en) * 1933-05-10 1936-07-14 Oscar Wolff Method of constructing radiator fins
US2428145A (en) * 1944-09-11 1947-09-30 Pacific Metals Company Ltd Heat transfer fin
US2977918A (en) * 1957-07-05 1961-04-04 Richard W Kritzer Method of making heat transfer units
US3223153A (en) * 1962-05-21 1965-12-14 Modine Mfg Co Fin and tube type heat exchanger
US3228367A (en) * 1962-12-20 1966-01-11 Borg Warner Method of manufacturing a heat exchanger

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2047207A (en) * 1933-05-10 1936-07-14 Oscar Wolff Method of constructing radiator fins
US2428145A (en) * 1944-09-11 1947-09-30 Pacific Metals Company Ltd Heat transfer fin
US2977918A (en) * 1957-07-05 1961-04-04 Richard W Kritzer Method of making heat transfer units
US3223153A (en) * 1962-05-21 1965-12-14 Modine Mfg Co Fin and tube type heat exchanger
US3228367A (en) * 1962-12-20 1966-01-11 Borg Warner Method of manufacturing a heat exchanger

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2832789A1 (en) * 2001-11-27 2003-05-30 Valeo Thermique Moteur Sa Automobile heat exchanger fin module comprise plane metal plate divided into two parts by long slots between which bands of material forming bridges between fin parts extend
WO2003046458A1 (en) * 2001-11-27 2003-06-05 Valeo Thermique Moteur Heat exchanger module fin
EP1586844A1 (en) * 2002-12-25 2005-10-19 T.RAD Co,.Ltd Plate fin for heat exchanger and heat exchanger core
EP1586844A4 (en) * 2002-12-25 2009-07-29 T Rad Co Ltd Plate fin for heat exchanger and heat exchanger core
WO2006005594A1 (en) * 2004-07-12 2006-01-19 Behr Gmbh & Co. Kg Heat exchanger, especially for motor vehicles
US20130284416A1 (en) * 2011-01-21 2013-10-31 Daikin Industries, Ltd. Heat exchanger and air conditioner
US20130299141A1 (en) * 2011-01-21 2013-11-14 Daikin Industries, Ltd. Heat exchanger and air conditioner
US20130299152A1 (en) * 2011-01-21 2013-11-14 Daikin Industries, Ltd. Heat exchanger and air conditioner
US9328973B2 (en) 2011-01-21 2016-05-03 Daikin Industries, Ltd. Heat exchanger and air conditioner

Similar Documents

Publication Publication Date Title
US3182481A (en) Heat exchanger and method of its manufacture
US3266567A (en) Heat exchanger
US4778004A (en) Heat exchanger assembly with integral fin unit
KR950014050B1 (en) Method of manufacturing a heat exchanger plate fin and fin so manufactured
US2994123A (en) Method of forming heat transfer units
EP0188314B1 (en) Method of attaching a tube to a fin
KR0161368B1 (en) Heat exchanger and plate fin therefor
JPH05172488A (en) Partition plate assembling structure of header pipe for heat exchanger and assembling method therefor
DE102011078897A1 (en) Temperature control device for controlling the temperature of a battery and method for producing a temperature control device
US10436156B2 (en) Air fin for a heat exchanger, and method of making the same
US3433300A (en) Heat exchangers and the method of making same
US3228367A (en) Method of manufacturing a heat exchanger
US3309763A (en) Method for making a heat exchanger
US4881311A (en) Heat exchanger assembly with integral fin unit
JPH06159985A (en) Heat exchanger and its preparation
US2035403A (en) Heat exchange device
US3211118A (en) Heat exchanger
US2927369A (en) Method of making multiple passage heat exchanger
US3779311A (en) Heat exchanger
JPH06154924A (en) Press working method
US3067994A (en) Apparatus for manufacture of tubetype radiators
US3431973A (en) Heat exchangers
GB1417457A (en) Method of manufacturing a tube panel for a radiator and radiator tube panel manufactured by said method
US2426920A (en) Method of forming and applying cooling fins to tubular members
US3510930A (en) Method of fabricating a heat exchanger