EP0672882B1 - Heat exchanger fin - Google Patents

Heat exchanger fin Download PDF

Info

Publication number
EP0672882B1
EP0672882B1 EP94120181A EP94120181A EP0672882B1 EP 0672882 B1 EP0672882 B1 EP 0672882B1 EP 94120181 A EP94120181 A EP 94120181A EP 94120181 A EP94120181 A EP 94120181A EP 0672882 B1 EP0672882 B1 EP 0672882B1
Authority
EP
European Patent Office
Prior art keywords
punched
fin
noses
fins
tubes
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
EP94120181A
Other languages
German (de)
French (fr)
Other versions
EP0672882A1 (en
Inventor
Werner Dipl.-Ing. Helms (Fh)
Roland Hemminger
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.)
Mahle Behr GmbH and Co KG
Original Assignee
Behr GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Behr GmbH and Co KG filed Critical Behr GmbH and Co KG
Publication of EP0672882A1 publication Critical patent/EP0672882A1/en
Application granted granted Critical
Publication of EP0672882B1 publication Critical patent/EP0672882B1/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
    • 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
    • F28F1/325Fins with openings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/12Fastening; Joining by methods involving deformation of the elements
    • F28F2275/125Fastening; Joining by methods involving deformation of the elements by bringing elements together and expanding
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/454Heat exchange having side-by-side conduits structure or conduit section
    • Y10S165/50Side-by-side conduits with fins
    • Y10S165/501Plate fins penetrated by plural conduits
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/454Heat exchange having side-by-side conduits structure or conduit section
    • Y10S165/50Side-by-side conduits with fins
    • Y10S165/501Plate fins penetrated by plural conduits
    • Y10S165/502Lanced
    • Y10S165/503Angled louvers
    • 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

  • the invention relates to a fin for a heat exchanger according to the preamble of claim 1.
  • Such heat exchanger fins were described in DE-A-37 28 969 and also known from DE-C-34 23 746.
  • rib density or so-called rib pitch (Number of ribs per dm) decisive - for reasons
  • This predetermined rib density is therefore of constant quality to adhere exactly to why the positioning of the ribs on the Pipes certain spacers are provided.
  • the latter can either as a flap protruding from the ribbed sheet, which then also act as turbulence generators, are formed, or by angled contact surfaces attached to the ends of the rib passages.
  • these contact surfaces are on the circumference Distributed tongues formed and in the DE-C '746 as on the long sides of the ellipses arranged crescent-shaped contact surfaces. Disadvantageous in these versions, it may be that when expanding the Pipes no longer a complete system compared to the fins between passage and pipe is guaranteed. Otherwise means relocating the contact surfaces after an additional operation pulling through.
  • GB-A 2 088 035 developed a heat exchanger with flat tubes and Known ribs that are soldered to the tubes.
  • the ribs point right-angled openings for receiving the flat tubes, taking off These openings have rectangular flaps in the area of the long sides are cut out and set up. These are flat rags soldered to the flat sides of the flat tubes. For spacing the ribs have these right-angled lobes in the form of noses ( Figures 6 and 7).
  • This kind of Pipe / fin connection is for mechanical production, i.e. without Soldering, not suitable.
  • GB-A 1 075 272 also shows a brazed flat tube system about rectangular openings in the ribs, from which rag in the area the long sides are upright. On this rag bends are provided at the end for spacing. Also this tube / fin connection is for a mechanical bond of Pipes and fins are not suitable.
  • GB-A 1 174 402 established a mechanically joined Pipe / fin system is known, in which the pipes compared to the Passages in the ribs are mechanically widened.
  • the passages have bent tongues at the ends, distributed over the circumference, which serve to hold the ribs apart. Bending the tongues means an additional operation, which is the manufacturing cost elevated.
  • the new spacers in the form of Noses are partially stamped out of the wall of the passage, so that with its upper edge it is a contact surface for the above form arranged rib.
  • the noses are too easy to manufacture because of the additional folding process after pulling through is omitted.
  • the heat transfer is also guaranteed since the noses are only partially provided and thus the heat transfer hardly between inner surface passage and outer surface pipe restrict.
  • the noses also expand upwards is the lower tip of such a nose, e.g.
  • the lugs are embossed in rags, which surpass the remaining draft in terms of its amount and thus the degree of rib division, i.e. the rib spacing.
  • the noses to be arranged against each other this allows the maximum height of the Rags are made. If the rib spacing in relation to Pull width is smaller, the lugs or lobes can also opposite.
  • the invention also relates to a method for pulling through with the noses to make what's in four or three consecutive Operations are done with the imprint of the noses either by a punch stroke in the pulling direction or in the opposite direction he follows.
  • Figure 1 shows a rib 1 in plan view with flat oval passages 2, which are arranged offset in two rows to one another, wherein each gill panels 3 are arranged between the passages 2.
  • the passages 2 accommodate pipes of the same cross section, not shown, which are mechanically widened with respect to these passages and thereby produce the contact necessary for heat conduction or heat transfer.
  • the rib 1 essentially forms a flat surface 4.
  • Each passage 2 has - as will be explained in more detail below - three lugs 8, 9, 10.
  • the rib 1 is preferably made of aluminum or an aluminum alloy and has a thickness of approximately 0.1 mm.
  • Figure 2 shows a section II-II through the rib of Figure 1 in an enlarged form, so that in particular the known inclined gills of the gill panels 3 can be seen. They deflect the air sweeping over the fins, which increases the air-side heat transfer.
  • two passages 2 are shown in the side view, three tabs 5, 6, 7 each being recognizable, into which the lugs 8, 9, 10 are each stamped in the center.
  • the tabs 5, 6, 7 are thus arranged offset from one another, ie the tabs 5 and 7 are located at the front, and the tab 6 is located at the rear, ie on the rear longitudinal side of the passage 2.
  • a passage 2, also enlarged, is shown in FIG. 3 , specifically in plan view a as a flat oval shape, from which the lugs 8, 9, 10 are clearly recognizable as bulges in the form of segments of a circle.
  • a dash-dotted line 11 is drawn in the interior of the flat oval passage 2, which delimits a punched-out section 12, so that the passage surface 2 'can be seen in the flat, not yet solid state.
  • Sections c and b of the passage are shown on the right and left of the passage a , the left illustration b showing the centrally arranged tab 6 with the nose 9 and the right illustration c showing the two off-center tabs 5 and 7 with the lugs 8 and 10.
  • the lugs 8, 9, 10 each have an outwardly sloping upper edge 8 ', 9', 10 ', which determines the distance H' (see FIG. 6) of the ribs. It is clear that the height H of the tabs 5, 6, 7 exceeds the height h of the rest of the passage - however, a continuous area 13 of height h is obtained which bears on all sides on the outer circumference of the tube, so that a closed heat transfer surface between the rib and tube is formed, which also maintains the elastic tension required after expansion.
  • FIGS. 4a, 4b, 4c and 4d now - as already indicated in FIG. 3 by line 11 - show the individual process steps for producing the swipe according to the invention.
  • FIG. 4a shows the ribbed sheet 20 after punching, ie a strip 24 with rounded ends 22, 23 is cut out of the flat ribbed sheet 20 by means of a suitable punch, whereby offset tabs 25, 26, 27 are cut free.
  • FIG. 4b in the subsequent process step, tabs 28, 29, 30 are embossed into these tabs 25, 26, 27 by means of an embossing stamp, which are pyramid-shaped, that is to say are formed from two planar triangular surfaces inclined towards one another.
  • an embossing stamp which are pyramid-shaped, that is to say are formed from two planar triangular surfaces inclined towards one another.
  • the passage is completed, ie the collar 21 is pulled through by means of a stamp, not shown, so that it acquires a cylindrical shape (with a flat oval cross section) and the noses 25 ′′, 26 ′′, 27 ′′ as The triangles protrude outwards, which is made possible by corresponding cutouts 32, 33, 34 in the die.
  • the passages with the molded noses can be produced simply, quickly and with consistent quality.
  • FIG. 5 shows an enlarged section of a tube 40, on which ribs 41 to 45 are “threaded”.
  • This tube 40 is part of a heat exchanger (not shown in more detail), the tube shape and division and fin design of which could correspond to FIG.
  • the ribs 41 to 45 are mechanically joined to the tube 40, ie connected by expanding the tube 40 with respect to the rib passages by means of a metallic press fit. So there is no soldering or gluing, ie material connection is necessary.
  • FIG. 6 shows an enlargement of a section from FIG. 5, namely a part of the tube wall 40 and three rib cutouts 41, 42, 43 which, with their passages 46, 47, 48 of height h, lie closely and circumferentially on the tube 40, while their noses 49, 50 , 51 protrude from the outer wall of the tube 40 and determine the distance H 'between the ribs 41, 42, 43 with its upper edge.
  • the rib spacing H ' is slightly smaller than the height H of the tabs (cf. FIG. 3b, c) because the rib passage has a transition radius on which the lugs are supported.
  • FIGS. 5 and 6 show the finished tube / fin arrangement, ie after the tube 40 has been expanded in the mechanically finished state of the tube and fin passages.
  • Such fins connected with a bundle of parallel tubes are, in turn, taken up in tube sheets from collecting tanks are used in particular in heat exchangers for motor vehicles, e.g. as a coolant / air cooler for the engine or as a heating heat exchanger.
  • Flat oval tube cross-sections work here advantageous in terms of air pressure drop.

Landscapes

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

Description

Die Erfindung bezieht sich auf eine Rippe für einen Wärmetauscher nach dem Oberbegriff des Patentanspruches 1.The invention relates to a fin for a heat exchanger according to the preamble of claim 1.

Derartige Wärmetauscherrippen wurden durch die DE-A-37 28 969 und auch durch die DE-C-34 23 746 bekannt. Für die Leistung eines Wärmetauschers ist unter anderem seine Rippendichte bzw. sogenannte Rippenteilung (Anzahl der Rippen pro dm) maßgebend - aus Gründen gleichbleibender Qualität ist diese vorgegebene Rippendichte daher genau einzuhalten, weshalb für die Positionierung der Rippen auf den Rohren bestimmte Abstandshalter vorgesehen sind. Letztere können entweder als aus dem Rippenblech herausgestellte Lappen, die dann auch als Turbulenzerzeuger wirken, gebildet werden, oder durch an den Enden der Rippendurchzüge angebrachte abgewinkelte Anlageflächen. Bei der DE-A '969 sind diese Anlageflächen als auf den Umfang verteilte Zungen ausgebildet und bei der DE-C '746 als an den Längsseiten der Ellipsen angeordnete sichelförmige Anlageflächen. Nachteilig bei diesen Ausführungen kann es sein, daß beim Aufweiten der Rohre gegenüber den Rippendurchzügen keine vollständige Anlage mehr zwischen Durchzug und Rohr gewährleistet ist. Im übrigen bedeutet das Umlegen der Anlageflächen einen zusätzlichen Arbeitsgang nach dem Durchziehen.Such heat exchanger fins were described in DE-A-37 28 969 and also known from DE-C-34 23 746. For the performance of a heat exchanger is among other things its rib density or so-called rib pitch (Number of ribs per dm) decisive - for reasons This predetermined rib density is therefore of constant quality to adhere exactly to why the positioning of the ribs on the Pipes certain spacers are provided. The latter can either as a flap protruding from the ribbed sheet, which then also act as turbulence generators, are formed, or by angled contact surfaces attached to the ends of the rib passages. In DE-A '969, these contact surfaces are on the circumference Distributed tongues formed and in the DE-C '746 as on the long sides of the ellipses arranged crescent-shaped contact surfaces. Disadvantageous in these versions, it may be that when expanding the Pipes no longer a complete system compared to the fins between passage and pipe is guaranteed. Otherwise means relocating the contact surfaces after an additional operation pulling through.

Durch die GB-A 2 088 035 wurde ein Wärmetauscher mit Flachrohren und Rippen bekannt, die mit den Rohren verlötet sind. Die Rippen weisen rechtwinklige Öffnungen zur Aufnahme der Flachrohre auf, wobei aus diesen Öffnungen rechtwinklige ebene Lappen im Bereich der Längsseiten ausgeschnitten und aufgestellt sind. Diese ebenen Lappen sind mit den ebenen Seiten der Flachrohre verlötet. Zur Abstandshalterung der Rippen weisen diese rechtwinkligen aufgestellten Lappen Ausprägungen in Form von Nasen auf (Figur 6 und 7). Diese Art von Rohr/Rippenverbindung ist für eine mechanische Fertigung, d.h. ohne Löten, nicht geeignet.GB-A 2 088 035 developed a heat exchanger with flat tubes and Known ribs that are soldered to the tubes. The ribs point right-angled openings for receiving the flat tubes, taking off These openings have rectangular flaps in the area of the long sides are cut out and set up. These are flat rags soldered to the flat sides of the flat tubes. For spacing the ribs have these right-angled lobes in the form of noses (Figures 6 and 7). This kind of Pipe / fin connection is for mechanical production, i.e. without Soldering, not suitable.

Die GB-A 1 075 272 zeigt ebenfalls ein gelötetes Flachrohrsystem mit etwa rechteckigen Öffnungen in den Rippen, aus welchen Lappen im Bereich der Längsseiten senkrecht hochgestellt sind. An diesen Lappen sind endseitig Abwinklungen zur Abstandshalterung vorgesehen. Auch diese Rohr/Rippenverbindung ist für einen mechanischen Verbund von Rohren und Rippen nicht geeignet.GB-A 1 075 272 also shows a brazed flat tube system about rectangular openings in the ribs, from which rag in the area the long sides are upright. On this rag bends are provided at the end for spacing. Also this tube / fin connection is for a mechanical bond of Pipes and fins are not suitable.

Durch die GB-A 1 174 402 wurde ein mechanisch gefügtes Rohr/Rippensystem bekannt, bei welchem die Rohre gegenüber den Durchzügen in den Rippen mechanisch aufgeweitet sind. Die Durchzüge weisen endseitig, auf den Umfang verteilt, abgebogene Zungen auf, die der Abstandshalterung der Rippen dienen. Das Abbiegen der Zungen bedeutet einen zusätzlichen Arbeitsgang, was die Herstellungskosten erhöht.GB-A 1 174 402 established a mechanically joined Pipe / fin system is known, in which the pipes compared to the Passages in the ribs are mechanically widened. The passages have bent tongues at the ends, distributed over the circumference, which serve to hold the ribs apart. Bending the tongues means an additional operation, which is the manufacturing cost elevated.

Es ist Aufgabe der vorliegenden Erfindung, eine Rippe der eingangs genannten Art derart zu verbessern, daß einerseits eine sichere Abstandshaltung zwischen den Rippen, andererseits ein guter Wärmeübergang zwischen Rohr und Rippen gewährleistet und darüber hinaus eine einfache Herstellung möglich ist.It is an object of the present invention to provide a rib at the beginning to improve the type mentioned in such a way that, on the one hand, safe spacing between the ribs, on the other hand good heat transfer guaranteed between tube and fins and beyond simple manufacture is possible.

Diese Aufgabe wird durch die kennzeichnenden Merkmale des Patentanspruches 1 gelöst. Die neuartigen Abstandshalter in Form von Nasen werden partiell aus der Wand des Durchzuges nach außen ausgeprägt, so daß sie mit ihrer Oberkante eine Anlagefläche für die darüber angeordnete Rippe bilden. Dadurch, daß mehrere Nasen auf den Umfang des Durchzuges verteilt sind, ergibt sich eine gute und stabile Abstützung für die nächstfolgende Rippe. Die Nasen sind auch einfach herstellbar, da der zusätzliche Arbeitsgang des Umlegens nach dem Durchziehen entfällt. Auch der Wärmeübergang ist gewährleistet, da die Nasen nur partiell vorgesehen sind und somit den Wärmedurchgang zwischen Innenfläche-Durchzug und Außenfläche-Rohr kaum einschränken. Die Nasen erweitern sich ferner nach oben Aufwärts ist die untere Spitze einer solchen Nase, z.B. in Form eines halben Kegels, etwas oberhalb der Rippenebene angeordnet, so daß eine durchgehende umlaufende Kontaktfläche bestimmter Breite zwischen Rohr und Rippendurchzug für einen guten Wärmedurchgang erhalten bleibt. Vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus den Unteransprüchen, wobei die Erfindung sowohl für Rohre mit kreisförmigen als auch ovalen oder elliptischen Querschnitten vorteilhaft anwendbar ist. Die Nasen haben vorteilhafterweise etwa die Form von halben Pyramiden oder halben Kegeln, die in der Senkrechten geteilt sind.This object is achieved by the characterizing features of the claim 1 solved. The new spacers in the form of Noses are partially stamped out of the wall of the passage, so that with its upper edge it is a contact surface for the above form arranged rib. The fact that several noses on the Scope of passage are distributed, there is a good and stable Support for the next rib. The noses are too easy to manufacture because of the additional folding process after pulling through is omitted. The heat transfer is also guaranteed since the noses are only partially provided and thus the heat transfer hardly between inner surface passage and outer surface pipe restrict. The noses also expand upwards is the lower tip of such a nose, e.g. in Shape of a half cone, slightly above the rib plane, so that a continuous circumferential contact surface of a certain width maintained between the tube and the fin passage for good heat transfer remains. Advantageous embodiments of the invention result from the subclaims, the invention being for both tubes with circular as well as oval or elliptical cross sections can be used advantageously is. The lugs advantageously have the shape of half pyramids or half cones divided in the vertical are.

Da insofern aus Wärmeübertragungsgründen eine größere Durchzugshöhe nicht erforderlich ist, sind die Nasen in Lappen geprägt, die den übrigen Durchzug hinsichtlich dessen Höhe überragen und somit das Maß der Rippenteilung, d.h. des Rippenabstandes, bestimmen. Bei ovalen oder elliptischen Durchzugsquerschnitten empfiehlt es sich aus herstellungstechnischen Gründen, die Nasen versetzt gegeneinander anzuordnen - dadurch kann die maximale Höhe der Lappen hergestellt werden. Sofern der Rippenabstand in Relation zur Durchzugsbreite geringer ist, können sich die Nasen bzw. Lappen auch gegenüberliegen.Because a larger one for heat transfer reasons Clearance height is not necessary, the lugs are embossed in rags, which surpass the remaining draft in terms of its amount and thus the degree of rib division, i.e. the rib spacing. Recommended for oval or elliptical cross sections for technical reasons, the noses to be arranged against each other - this allows the maximum height of the Rags are made. If the rib spacing in relation to Pull width is smaller, the lugs or lobes can also opposite.

Schließlich betrifft die Erfindung auch ein Verfahren, um die Durchzüge mit den Nasen herzustellen, was in vier oder drei aufeinanderfolgenden Arbeitsgängen geschieht, wobei die Einprägung der Nasen entweder durch einen Stempelhub in Durchzugsrichtung oder entgegengesetzt erfolgt.Finally, the invention also relates to a method for pulling through with the noses to make what's in four or three consecutive Operations are done with the imprint of the noses either by a punch stroke in the pulling direction or in the opposite direction he follows.

Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt und wird im folgenden näher beschrieben. Es zeigen:

Figur 1
eine Rippe in der Draufsicht,
Figur 2
die Rippe gemäß Figur 1 im Schnitt, vergrößert,
Figur 3
einen Durchzug der Rippe gemäß Figur 1, vergrößert,
Figur 4a, 4b, 4c und 4d
die einzelnen Verfahrensschritte zur Herstellung des Durchzuges mit Nasen,
Figur 5
ein Rohr mit Rippen, vergrößert und
Figur 6
ein Detail aus Figur 5: Rohrwand mit Rippendurchzügen.
An embodiment of the invention is shown in the drawing and will be described in more detail below. Show it:
Figure 1
a rib in top view,
Figure 2
the rib of Figure 1 in section, enlarged,
Figure 3
a passage of the rib according to Figure 1, enlarged,
Figure 4a, 4b, 4c and 4d
the individual process steps for the production of the passage with noses,
Figure 5
a tube with fins, enlarged and
Figure 6
a detail from Figure 5: pipe wall with fins.

Figur 1 zeigt eine Rippe 1 in der Draufsicht mit flachovalen Durchzügen 2, die in zwei Reihen versetzt zueinander angeordnet sind, wobei zwischen den Durchzügen 2 jeweils Kiemenfelder 3 angeordnet sind. Die Durchzüge 2 nehmen nicht dargestellte Rohre gleichen Querschnittes auf, welche gegenüber diesen Durchzügen mechanisch aufgeweitet werden und dadurch den für die Wärmeleitung bzw. den Wärmedurchgang notwendigen Kontakt herstellen. Im Bereich, wo keine Kiemenfelder 3 und keine Durchzüge 2 vorgesehen sind, bildet die Rippe 1 im wesentlichen eine ebene Fläche 4. Jeder Durchzug 2 weist - wie unten näher erläutert wird - drei Nasen 8, 9, 10 auf. Die Rippe 1 ist vorzugsweise aus Aluminium bzw. einer Aluminiumlegierung hergestellt und hat eine Dicke von ca. 0,1 mm. Figure 1 shows a rib 1 in plan view with flat oval passages 2, which are arranged offset in two rows to one another, wherein each gill panels 3 are arranged between the passages 2. The passages 2 accommodate pipes of the same cross section, not shown, which are mechanically widened with respect to these passages and thereby produce the contact necessary for heat conduction or heat transfer. In the area where no gill panels 3 and no passages 2 are provided, the rib 1 essentially forms a flat surface 4. Each passage 2 has - as will be explained in more detail below - three lugs 8, 9, 10. The rib 1 is preferably made of aluminum or an aluminum alloy and has a thickness of approximately 0.1 mm.

Figur 2 zeigt einen Schnitt II-II durch die Rippe gemäß Figur 1 in vergrößerter Form, so daß insbesondere die an sich bekannten schräggestellten Kiemen der Kiemenfelder 3 erkennbar werden. Sie bewirken eine Umlenkung der die Rippen überstreichenden Luft, wodurch der luftseitige Wärmeübergang erhöht wird. In dieser Darstellung sind zwei Durchzüge 2 in der Seitenansicht dargestellt, wobei jeweils drei Lappen 5, 6, 7 erkennbar sind, in welche die Nasen 8, 9, 10 jeweils mittig eingeprägt sind. Die Lappen 5, 6, 7 sind also gegeneinander versetzt angeordnet, d.h. die Lappen 5 und 7 liegen vorne, und der Lappen 6 liegt hinten, d.h. auf der hinteren Längsseite des Durchzuges 2. Figure 2 shows a section II-II through the rib of Figure 1 in an enlarged form, so that in particular the known inclined gills of the gill panels 3 can be seen. They deflect the air sweeping over the fins, which increases the air-side heat transfer. In this illustration, two passages 2 are shown in the side view, three tabs 5, 6, 7 each being recognizable, into which the lugs 8, 9, 10 are each stamped in the center. The tabs 5, 6, 7 are thus arranged offset from one another, ie the tabs 5 and 7 are located at the front, and the tab 6 is located at the rear, ie on the rear longitudinal side of the passage 2.

In Figur 3 ist ein Durchzug 2, ebenfalls vergrößert, dargestellt, und zwar in der Draufsicht a als flachovale Form, aus der die Nasen 8, 9, 10 als kreissegmentförmige Ausbuchtungen deutlich erkennbar sind. Im Inneren des flachovalen Durchzuges 2 ist eine strichpunktierte Linie 11 eingezeichnet, welche einen ausgestanzten Ausschnitt 12 begrenzt, so daß die Durchzugsfläche 2' im ebenen, noch nicht durchgezogenen Zustand erkennbar ist. Rechts und links des Durchzuges a sind Schnitte c und b des Durchzuges dargestellt, wobei die linke Darstellung b den mittig angeordneten Lappen 6 mit der Nase 9 und die rechte Darstellung c die zwei außermittig angeordneten Lappen 5 und 7 mit den Nasen 8 und 10 zeigt. Die Nasen 8, 9, 10 weisen jeweils eine nach außen abfallende Oberkante 8', 9', 10' auf, die den Abstand H' (vgl. Figur 6) der Rippen bestimmt. Deutlich ist, daß die Höhe H der Lappen 5, 6, 7 die Höhe h des übrigen Durchzuges übersteigt - allerdings ist ein durchgehender Bereich 13 der Höhe h erhalten, der sich allseitig an den Außenumfang des Rohres anlegt, so daß eine geschlossene Wärmedurchgangsfläche zwischen Rippe und Rohr gebildet wird, die darüber hinaus auch die nach dem Aufweiten erforderliche elastische Spannung aufrechterhält.A passage 2, also enlarged, is shown in FIG. 3 , specifically in plan view a as a flat oval shape, from which the lugs 8, 9, 10 are clearly recognizable as bulges in the form of segments of a circle. A dash-dotted line 11 is drawn in the interior of the flat oval passage 2, which delimits a punched-out section 12, so that the passage surface 2 'can be seen in the flat, not yet solid state. Sections c and b of the passage are shown on the right and left of the passage a , the left illustration b showing the centrally arranged tab 6 with the nose 9 and the right illustration c showing the two off-center tabs 5 and 7 with the lugs 8 and 10. The lugs 8, 9, 10 each have an outwardly sloping upper edge 8 ', 9', 10 ', which determines the distance H' (see FIG. 6) of the ribs. It is clear that the height H of the tabs 5, 6, 7 exceeds the height h of the rest of the passage - however, a continuous area 13 of height h is obtained which bears on all sides on the outer circumference of the tube, so that a closed heat transfer surface between the rib and tube is formed, which also maintains the elastic tension required after expansion.

Die Figuren 4a, 4b, 4c und 4d zeigen nun - wie bereits in Figur 3 durch die Linie 11 angedeutet - die einzelnen Verfahrensschritte zur Herstellung des erfindungsgemäßen Durchzuges. Figur 4a zeigt das Rippenblech 20 nach dem Lochen, d.h. aus dem ebenen Rippenblech 20 ist mittels eines geeigneten Lochstempels ein Streifen 24 mit endseitigen Ausrundungen 22, 23, herausgeschnitten, wobei versetzt angeordnete Lappen 25, 26, 27 freigeschnitten sind. Gemäß Figur 4b werden im darauffolgenden Verfahrensschritt in diese Lappen 25, 26, 27 mittels eines Prägestempels Nasen 28, 29, 30 eingeprägt, die pyramidenförmig ausgebildet sind, d.h. aus zwei ebenen gegeneinander geneigten Dreiecksflächen gebildet werden. Beim nächsten Verfahrensschritt, der in Figur 4c dargestellt ist, wird der Durchzug 21 gegen eine Matrize 31 mit entsprechender oval geformter Biegekante eingezogen, d.h. nur "angekippt", so daß die Nasen gerade an der Innenwand der Matrize 31 zur Anlage kommen, aber der übrige Durchzug 21 noch konisch ausgebildet ist. In Figur 4c sind daher die Lappen 25', 26', 27' verkürzt gegenüber Figur 4b dargestellt. FIGS. 4a, 4b, 4c and 4d now - as already indicated in FIG. 3 by line 11 - show the individual process steps for producing the swipe according to the invention. FIG. 4a shows the ribbed sheet 20 after punching, ie a strip 24 with rounded ends 22, 23 is cut out of the flat ribbed sheet 20 by means of a suitable punch, whereby offset tabs 25, 26, 27 are cut free. According to FIG. 4b , in the subsequent process step, tabs 28, 29, 30 are embossed into these tabs 25, 26, 27 by means of an embossing stamp, which are pyramid-shaped, that is to say are formed from two planar triangular surfaces inclined towards one another. In the next process step, which is shown in FIG. 4c , the passage 21 is drawn in against a die 31 with a corresponding oval-shaped bending edge, that is to say only “tilted” so that the lugs come to rest against the inner wall of the die 31, but the rest Passage 21 is still conical. In Figure 4c , the tabs 25 ', 26', 27 'are therefore shown shortened compared to Figure 4b.

Im letzten Verfahrensschritt gemäß Figur 4d wird der Durchzug fertiggestellt, d.h. mittels eines nicht dargestellten Stempels wird der Kragen 21 durchgezogen, so daß er eine zylindrische Form (mit flachovalem Querschnitt) erhält und die Nasen 25'', 26'', 27'' als Dreiecke nach außen abstehen, was durch entsprechende Aussparungen 32, 33, 34 in der Matrize ermöglicht wird. Mit dem beschriebenen Verfahren können die Durchzüge mit den angeformten Nasen einfach, schnell und mit gleichbleibender Qualität hergestellt werden.In the last process step according to FIG. 4d , the passage is completed, ie the collar 21 is pulled through by means of a stamp, not shown, so that it acquires a cylindrical shape (with a flat oval cross section) and the noses 25 ″, 26 ″, 27 ″ as The triangles protrude outwards, which is made possible by corresponding cutouts 32, 33, 34 in the die. With the described method, the passages with the molded noses can be produced simply, quickly and with consistent quality.

Es ist auch ein anderes Verfahren möglich, bei dem die Verfahrensschritte gemäß Figur 4b und 4c erst zum Schluß erfolgen, und zwar durch einen Prägestempel, der von oben in den fertigen Durchzug einfährt.Another method is also possible in which the method steps according to Figures 4b and 4c only at the end, namely by means of an embossing stamp that enters the finished passage from above.

Figur 5 zeigt vergrößert ein Rohr 40 im Schnitt, auf welches Rippen 41 bis 45 "aufgefädelt" sind. Dieses Rohr 40 ist Teil eines nicht näher dargestellten Wärmetauschers, dessen Rohrform und Teilung sowie Rippenausführung der Figur 1 entsprechen könnte. Wie bereits erwähnt, sind die Rippen 41 bis 45 mechanisch mit dem Rohr 40 gefügt, d.h. durch Aufweiten des Rohres 40 gegenüber den Rippendurchzügen durch einen metallischen Preßsitz verbunden. Es ist also kein Löten oder Kleben, d.h. stoffliche Verbindung notwenig. FIG. 5 shows an enlarged section of a tube 40, on which ribs 41 to 45 are “threaded”. This tube 40 is part of a heat exchanger (not shown in more detail), the tube shape and division and fin design of which could correspond to FIG. As already mentioned, the ribs 41 to 45 are mechanically joined to the tube 40, ie connected by expanding the tube 40 with respect to the rib passages by means of a metallic press fit. So there is no soldering or gluing, ie material connection is necessary.

Figur 6 zeigt eine Ausschnittvergrößerung aus Figur 5, nämlich einen Teil der Rohrwand 40 und drei Rippenausschnitte 41, 42, 43, die mit ihren Durchzügen 46, 47, 48 der Höhe h eng und umlaufend am Rohr 40 anliegen, während ihre Nasen 49, 50, 51 von der Außenwandung des Rohres 40 abstehen und mit ihrer Oberkante den Abstand H' zwischen den Rippen 41, 42, 43 bestimmen. Der Rippenabstand H' ist geringfügig kleiner als die Höhe H der Lappen (vgl. Figur 3b, c), weil der Rippendurchzug einen Übergangsradius aufweist, an welchem die Abstützung der Nasen erfolgt. Beide Figuren 5 und 6 zeigen die fertige Rohr/Rippenanordnung, d.h. nach dem Aufweiten des Rohres 40 im mechanisch fertiggefügten Zustand von Rohr und Rippendurchzügen. FIG. 6 shows an enlargement of a section from FIG. 5, namely a part of the tube wall 40 and three rib cutouts 41, 42, 43 which, with their passages 46, 47, 48 of height h, lie closely and circumferentially on the tube 40, while their noses 49, 50 , 51 protrude from the outer wall of the tube 40 and determine the distance H 'between the ribs 41, 42, 43 with its upper edge. The rib spacing H 'is slightly smaller than the height H of the tabs (cf. FIG. 3b, c) because the rib passage has a transition radius on which the lugs are supported. Both FIGS. 5 and 6 show the finished tube / fin arrangement, ie after the tube 40 has been expanded in the mechanically finished state of the tube and fin passages.

Derartige Rippen, die mit einem Bündel paralleler Rohre verbunden sind, die wiederum in Rohrböden von Sammelbehältern aufgenommen sind, finden insbesondere bei Wärmetauschern für Kraftfahrzeuge Verwendung, z.B. als Kühlmittel/Luft-Kühler für den Motor oder als Heizungswärmetauscher. Hier wirken sich flachovale Rohrquerschnitte vorteilhaft im Hinblick auf den luftseitigen Druckabfall aus.Such fins connected with a bundle of parallel tubes are, in turn, taken up in tube sheets from collecting tanks are used in particular in heat exchangers for motor vehicles, e.g. as a coolant / air cooler for the engine or as a heating heat exchanger. Flat oval tube cross-sections work here advantageous in terms of air pressure drop.

Claims (10)

  1. A fin for a heat exchanger essentially consisting of a matrix of tubes and fins (1; 41:45) arranged transversely thereto, the fins having punched mountings (2; 46:48) for receiving the tubes to be mechanically joined and a first, preferably liquid medium flows through the tubes and a second, preferably gaseous medium is applied to the fins which are positioned by means of integral spacers in the pitch of the fin, characterised in that the spacers are provided in the form of noses (8, 9, 10; 49, 50, 51) stamped out from the punched mountings (2; 46:48) distributed around the circumference thereof, the noses (8, 9, 10) being wider in the punching direction to form a top abutment edge (8', 9', 10'), and the bottom edge of the noses (8, 9, 10; 49, 50, 51) is arranged more or less at a height h above the plane (4) of the fin thereby leaving a surrounding punched ring (13) lying against all sides of the tube.
  2. A fin as claimed in claim 1, characterised in that the tubes and the punched mountings (2) are circular in cross-section.
  3. A fin as claimed in claim 1, characterised in that the tubes and the punched mountings (2) are oval or elliptical in cross-section, preferably having an axial ratio greater than 3 : 1.
  4. A fin as claimed in claim 1, 2 or 3, characterised in that the noses (8, 9, 10) have, in planes parallel with the fins, a semi-circular, arcuate, semi-ellipsoid or triangular cross-section.
  5. A fin as claimed in one of the preceding claims, characterised in that the noses (8, 9, 10) are stamped out from flaps (5, 6, 7) respectively, the height H of which is greater than the height h of the remainder of the punched mounting (2).
  6. A fin as claimed in one of the preceding claims with the exception of claim 2, characterised in that the noses (8, 9, 10) are arranged on the longitudinal sides of the punched mountings (2).
  7. A fin as claimed in claim 6, characterised in that the noses (8, 9, 10) are arranged offset from one another.
  8. A method of manufacturing punched mountings for fins as claimed in one of the preceding claims, characterised by the following process steps:
    a) punching orifices (12; 22-23-24) are punched into the flat fin plate (4), flaps (25, 26, 27) being cut free,
    b) noses (28, 29, 30) are stamped into the flaps (25, 26, 27) by means of a stamping die pushed in the punching direction,
    c) the flaps (25, 26, 27) together with the outwardly punched noses (28, 29, 30) are pushed in and tilted back by means of a stamp and die and
    d) the entire punched mounting, i.e. collar (21) with flaps (25, 26, 27) is fully punched through.
  9. A method of manufacturing punched mountings for fins as claimed in one of claims 1 to 7, characterised by the following process steps:
    a) punching orifices are punched into the flat fin plate(4) and flaps cut free,
    b) the entire punched mounting, i.e. collar with flaps, is punched into a cylindrical shape,
    c) the noses are punched by means of a punching die which travels from above into the free end of the punched mounting.
  10. A heat exchanger essentially consisting of a matrix of tubes with fins arranged transversely thereto, the fins having punched mountings for receiving the mechanically jointed tubes and a first, preferably liquid medium flows through the tubes and a second, preferably gaseous medium is applied to the fins which are positioned by means of integral spacers in the pitch of the fin, characterised by fins as claimed in one of claims 1 to 7.
EP94120181A 1994-02-16 1994-12-20 Heat exchanger fin Expired - Lifetime EP0672882B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4404837A DE4404837A1 (en) 1994-02-16 1994-02-16 Rib for heat exchangers
DE4404837 1994-02-16

Publications (2)

Publication Number Publication Date
EP0672882A1 EP0672882A1 (en) 1995-09-20
EP0672882B1 true EP0672882B1 (en) 1998-10-07

Family

ID=6510337

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94120181A Expired - Lifetime EP0672882B1 (en) 1994-02-16 1994-12-20 Heat exchanger fin

Country Status (4)

Country Link
US (2) US5582244A (en)
EP (1) EP0672882B1 (en)
DE (2) DE4404837A1 (en)
ES (1) ES2123089T3 (en)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH109787A (en) * 1996-04-25 1998-01-16 Denso Corp Plate fin type heat exchanger
US5752567A (en) * 1996-12-04 1998-05-19 York International Corporation Heat exchanger fin structure
US5975200A (en) * 1997-04-23 1999-11-02 Denso Corporation Plate-fin type heat exchanger
DE19741856A1 (en) * 1997-09-23 1999-03-25 Behr Gmbh & Co Rib for a heat exchanger and method for producing rib openings in such ribs
DE29800739U1 (en) * 1998-01-17 1999-05-12 Robert Bosch Gmbh, 70469 Stuttgart Heat exchanger for fuel-heated water heaters
JP4188475B2 (en) * 1998-12-22 2008-11-26 日高精機株式会社 Manufacturing method of heat exchanger
US6253839B1 (en) * 1999-03-10 2001-07-03 Ti Group Automotive Systems Corp. Refrigeration evaporator
FR2827801B1 (en) * 2001-07-24 2003-10-31 Valeo Thermique Moteur Sa METHOD FOR MANUFACTURING COOLING FINS
DE10227930A1 (en) * 2002-06-21 2004-01-08 Behr Gmbh & Co. Heat exchanger, in particular for a motor vehicle
JP4729840B2 (en) * 2003-08-12 2011-07-20 セイコーエプソン株式会社 Method of manufacturing liquid jet head and liquid jet head obtained thereby
US7004242B2 (en) * 2004-06-14 2006-02-28 Advanced Heat Transfer, Llc Enhanced heat exchanger apparatus and method
US20060218791A1 (en) * 2005-03-29 2006-10-05 John Lamkin Fin-tube heat exchanger collar, and method of making same
US20090044408A1 (en) * 2005-03-29 2009-02-19 John Lamkin Fin-Tube Heat Exchanger Collar, and Method of Making Same
US7273094B2 (en) * 2005-07-27 2007-09-25 Asia Vitag Components Co. Ltd. Cooling fin unit
US10415894B2 (en) * 2006-01-26 2019-09-17 Ingersoll-Rand Company Fin and tube heat exchanger
DE502006005252D1 (en) * 2006-08-08 2009-12-10 Behr Gmbh & Co Kg Rib for a heat exchanger, heat exchanger with such a rib and method for producing the heat exchanger
WO2009018150A1 (en) 2007-07-27 2009-02-05 Johnson Controls Technology Company Multichannel heat exchanger
US20100006276A1 (en) * 2008-07-11 2010-01-14 Johnson Controls Technology Company Multichannel Heat Exchanger
CN101995115B (en) * 2009-08-07 2014-07-23 江森自控科技公司 Multi-channel heat exchanger fins
FR2958027B1 (en) * 2010-03-25 2012-03-23 Valeo Systemes Thermiques AILETTE FOR HEAT EXCHANGER AND HEAT EXCHANGER EQUIPPED WITH SUCH FINS.
DE102011075071A1 (en) * 2011-05-02 2012-11-08 Behr Gmbh & Co. Kg Heat exchangers, in particular intercoolers
CN103105089B (en) * 2011-11-10 2017-03-01 松下电器产业株式会社 Thermofin, fin tube heat exchanger and heat pump assembly
DE102012002234A1 (en) 2012-02-04 2013-08-08 Volkswagen Aktiengesellschaft Heat exchanger, particularly radiator for vehicle, has multiple fins oriented perpendicular to tubing, where adjacent fins surround intermediate space by spacers, and sections of web or spacer are formed on base side or on mold side of fin
WO2014091536A1 (en) * 2012-12-10 2014-06-19 三菱電機株式会社 Flat tube heat exchange apparatus
JP6314106B2 (en) * 2015-03-16 2018-04-18 リンナイ株式会社 Heat transfer fin for heat exchanger and heat exchanger provided with the same
FR3037388B1 (en) * 2015-06-12 2019-07-26 Valeo Systemes Thermiques WING OF A HEAT EXCHANGER, IN PARTICULAR FOR A MOTOR VEHICLE, AND CORRESPONDING HEAT EXCHANGER
FR3038976B1 (en) * 2015-07-17 2019-08-09 Valeo Systemes Thermiques HEAT EXCHANGER WITH FINS COMPRISING IMPROVED PERSIANS
FR3038977B1 (en) * 2015-07-17 2019-08-30 Valeo Systemes Thermiques HEAT EXCHANGER WITH FINS COMPRISING IMPROVED PERSIANS
EP3421919A4 (en) * 2016-02-24 2019-11-06 Mitsubishi Electric Corporation Heat exchanger
CN109312991B (en) * 2016-07-01 2020-11-10 三菱电机株式会社 Heat exchanger and refrigeration cycle device provided with same
WO2019062493A1 (en) * 2017-09-30 2019-04-04 杭州三花微通道换热器有限公司 Heat exchanger and fin
JP6656279B2 (en) * 2018-02-15 2020-03-04 三菱電機株式会社 Heat exchanger
CA3036460A1 (en) * 2018-03-14 2019-09-14 Rheem Manufacturing Company Heat exchanger fin
US11774187B2 (en) * 2018-04-19 2023-10-03 Kyungdong Navien Co., Ltd. Heat transfer fin of fin-tube type heat exchanger
USD906268S1 (en) 2018-09-11 2020-12-29 Rheem Manufacturing Company Heat exchanger fin
US11402163B2 (en) * 2018-11-14 2022-08-02 Cooler Master Co., Ltd. Heat dissipation device and fin structure
EP3686714A1 (en) * 2019-01-25 2020-07-29 Asetek Danmark A/S Cooling system including a heat exchanging unit

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT127067B (en) * 1930-06-02 1932-02-25 E H Hugo Dr Ing Junkers Rib for heat exchangers to be pushed onto pipes
FR1028904A (en) * 1950-10-26 1953-05-28 temperature exchange element for industrial applications
GB775675A (en) * 1954-05-31 1957-05-29 Lawrence Holdings Overseas Ltd Improvements in finned tube core structures for heat exchangers
AT275248B (en) * 1963-06-27 1969-10-10 Chausson Usines Sa Rib in radiator bundles of a tubular cooler
US3245465A (en) * 1964-12-09 1966-04-12 Young Radiator Co Heat-exchanger core-unit construction
GB1174402A (en) * 1966-06-03 1969-12-17 English Electric Co Ltd Heat Exchangers.
US3771595A (en) * 1971-09-22 1973-11-13 Modine Mfg Co Heat exchange device
JPS589358B2 (en) * 1975-10-22 1983-02-21 三洋電機株式会社 Netsukou Kankinoseizouhouhou
JPS5267047A (en) * 1975-11-28 1977-06-03 Hitachi Ltd Method of manufacturing fins for air exchanger
JPS55107897A (en) * 1979-02-09 1980-08-19 Nippon Denso Co Ltd Heat exchanger
GB2047399B (en) * 1979-04-20 1982-12-08 Du Pont Fabrication of finned-tube heat exchangers
GB2088035B (en) * 1980-10-22 1984-05-31 Serck Industries Ltd Finned-tube heat exchanger
JPS58127092A (en) * 1982-01-25 1983-07-28 Nippon Denso Co Ltd Heat exchanger and manufacture thereof
JPS6449892A (en) * 1987-08-20 1989-02-27 Fujitsu General Ltd Heat exchanger
DE3910357A1 (en) * 1989-03-30 1990-10-04 Autokuehler Gmbh & Co Kg GUIDE PLATE FOR A HEAT EXCHANGER AND A HEAT EXCHANGER MADE THEREOF
AT394108B (en) * 1990-07-31 1992-02-10 Vaillant Gmbh SHEET BLOCK HEAT EXCHANGER
DE4129573C2 (en) * 1991-09-06 1997-10-23 Behr Gmbh & Co Heat exchanger

Also Published As

Publication number Publication date
ES2123089T3 (en) 1999-01-01
DE59407053D1 (en) 1998-11-12
DE4404837A1 (en) 1995-08-17
US5582244A (en) 1996-12-10
EP0672882A1 (en) 1995-09-20
US5706695A (en) 1998-01-13

Similar Documents

Publication Publication Date Title
EP0672882B1 (en) Heat exchanger fin
EP1703243B1 (en) Heat exchanger with tubes and fins and process to manufacture it
DE60111469T2 (en) Heat exchanger and method for its production
DE69330803T2 (en) Cooling tubes for heat exchangers
DE60219538T2 (en) heat exchangers
DE60217515T2 (en) METAL PLATE FOR MANUFACTURING A FLAT TUBE, FLAT TUBE AND METHOD FOR PRODUCING THE FLAT TUBE
DE69202964T2 (en) Heat exchanger.
DE69814904T2 (en) RIB FOR ONE-PIECE HEAT EXCHANGER AND METHOD FOR THE PRODUCTION THEREOF
DE4340378C2 (en) Heat exchangers and methods of making the same
DE69210452T2 (en) Heat exchanger with tube bundle, in particular for motor vehicles
DE69708730T2 (en) Heat exchanger and process for its manufacture
EP0389970B1 (en) Fin and heat-exchanger
EP0387678A1 (en) Heat exchanger and process for the watertight fixation of heat exchange elements to an end plate
DE102006002932B4 (en) Heat exchangers and manufacturing processes for heat exchangers
EP1555503A2 (en) Heat exchange flat tube, more especially for condenser
EP1468235B1 (en) Welded multi-chamber tube
DE3834822A1 (en) Heat exchanger
WO2000055561A1 (en) Collector tube for a heat transfer unit and method for producing same
DE602004006728T2 (en) Method and device for producing heat exchanger plates
EP1227291B1 (en) Heat exchanger and method of production
EP1306640A2 (en) End plate for exhaust gas heat exchanger
DE4446754A1 (en) Method for construction of heat exchanger
EP1890101B1 (en) Fin for heat exchanger, heat exchanger with such a fin and method for producing the heat exchanger
DE102006031676A1 (en) Turbulence plate for heat transfer devices has corrugated strips with trailing edges and the leading edges with separation distance greater than null when viewed in x direction
DE69903241T2 (en) HEAT EXCHANGER, ESPECIALLY CONDENSER FOR MOTOR VEHICLE AND METHOD FOR THE PRODUCTION THEREOF

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES FR GB IT SE

17P Request for examination filed

Effective date: 19951004

17Q First examination report despatched

Effective date: 19960913

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE ES FR GB IT SE

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19981014

REF Corresponds to:

Ref document number: 59407053

Country of ref document: DE

Date of ref document: 19981112

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19981120

Year of fee payment: 5

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 19981211

Year of fee payment: 5

ET Fr: translation filed
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2123089

Country of ref document: ES

Kind code of ref document: T3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 19990107

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19991220

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19991220

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20001221

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20030522

Year of fee payment: 9

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20010113

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040831

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20051220

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20060220

Year of fee payment: 12

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070703