EP2601474A2 - Plate-shaped heat exchanger for a cooling device comprising at least one heat exchanger package - Google Patents

Plate-shaped heat exchanger for a cooling device comprising at least one heat exchanger package

Info

Publication number
EP2601474A2
EP2601474A2 EP11741208.0A EP11741208A EP2601474A2 EP 2601474 A2 EP2601474 A2 EP 2601474A2 EP 11741208 A EP11741208 A EP 11741208A EP 2601474 A2 EP2601474 A2 EP 2601474A2
Authority
EP
European Patent Office
Prior art keywords
heat exchanger
passage
exhibition
exhibitions
radiation
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.)
Ceased
Application number
EP11741208.0A
Other languages
German (de)
French (fr)
Inventor
Boris Kerler
Steffen GRÖZINGER
Mehmet Tosun
Christian Schnepf
Florian Schmidt
Hans-Joachim Krauss
Vinko Lukcin
Stéphanie LARPENT
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 International GmbH
Mahle Behr GmbH and Co KG
Original Assignee
Behr GmbH and Co KG
Mahle 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, Mahle Behr GmbH and Co KG filed Critical Behr GmbH and Co KG
Publication of EP2601474A2 publication Critical patent/EP2601474A2/en
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/08Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
    • 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
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/02Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the heat-exchange media travelling at an angle to one another
    • 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
    • F28F1/30Tubular 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 being attachable to the element
    • 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
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • 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
    • 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
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/008Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
    • F28D2021/0082Charged air coolers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2215/00Fins
    • F28F2215/08Fins with openings, e.g. louvers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2225/00Reinforcing means
    • F28F2225/06Reinforcing means for fins

Definitions

  • the invention relates to a plate-shaped heat exchanger for a, at least one heat exchanger package having cooling device, in particular for a motor vehicle consisting of a plurality of openings for receiving a, a coolant-carrying tube, each opening is surrounded by a passage and between the passages several exhibitions to Heat exchange are distributed with the medium to be cooled.
  • FIG. 1 There are known intercooler in round tube design, which are shown in Figure 1 are provided.
  • a charge air cooler from a package of plate-shaped heat exchangers 2, which are also referred to as corrugated fins.
  • Each plate-shaped heat exchanger 2 in this case has a plurality of openings 7, in each of which a round tube 3 is fitted and is connected to the plate-shaped heat exchanger 2 via a mechanical widening of the passages 4 surrounding the opening.
  • a coolant 5 while coming from a not shown internal combustion engine, to be cooled charge air 6 flows perpendicular to the round tubes 3 in the, consisting of many plate-shaped heat exchangers 2 heat exchanger package, which is perpendicular to the Rundroh- 3.
  • FIG. 2b shows a cross section through the plate-shaped heat exchanger 2
  • FIG. 2c shows a perspective view of a passage 4.
  • the passages 4 ensure contact with the round tubes 3, which derive the heat from the charge air cooler 1 via the coolant 5.
  • Turbuiatoren or spacers 8 are arranged, see symmetrically between the see, the openings 7 enclosing passages 4 are distributed.
  • the turbulators or spacers 8 receive the plate-shaped heat exchanger 2 arranged above them, wherein there is sufficient space between the two plate-shaped heat exchangers 2 so that the charge air 6 coming from the internal combustion engine can flow between these heat exchangers 2.
  • the turbulators or spacers 8 can also cause a transformation of the laminar flow of the Ladeiuft 6 in a turbulent flow, so that the heat distribution over the entire plate-shaped heat exchanger 2 can be better ensured.
  • FIG. 3 shows a further known embodiment of a plate-shaped heat exchanger 2, in which a gill field 9 is arranged between the passages 4.
  • This gill field 9 has the task of causing turbulence in the air flow of the charge air 6 and to ensure an improved transverse noise of the charge air 6 between the individual, superimposed plate-shaped heat exchangers 2.
  • turbulators or spacers 8 are provided, which serve as a support for the next, plate-shaped heat exchanger 2.
  • the passage 4 so-called crowns 4 a, which are arranged at the passage 4 at its periphery spaced around.
  • This Krontulpen 4a serve as a spacer for the plate-lying heat exchanger lying on it 2, which is why it is possible to dispense with separate Abstandhaiter 8.
  • each passage 4 and the opening 4 surrounded by the passage 4 is surrounded by a gill feeder 9.
  • the plate-shaped heat exchanger 2 must have a high mechanical stability to vibration and vibration during operation in order to avoid fractures of the heat exchanger 2.
  • the invention is therefore based on the object anzzüwe a plate-shaped heat exchanger, which allows a high heat transfer from the charge air to the coolant, wherein the pressure drop of the charge air is to be kept as low as possible.
  • the object is achieved in that several exhibitions are arranged around a passage, the Aussannonen have a shape which ensure a targeted heat conduction from the exhibitions on the passage.
  • Such a form of the exhibition ensures that although the turbulence required for the heat exchange through the exhibitions on the plate-shaped heat exchanger are generated and the turbulent air mass is fed to the passage, but only a slight increase in pressure loss of the charge air occurs.
  • the stiffeners are arranged approximately circularly around the passage. Such a circular arrangement ensures that the turbulent air, which is caused by the exhibitions, directly to the passage and thus when installed in a cooling device is fed to the surrounding of the passage round tube. This improves the heat exchange ofméei device,
  • the exhibition is niksegmentähntich trained. This circular segment-like form of the exhibition supports the new approaches of the flow of the charge air to generate turbulence and ensures a cross-exchange between the various plate-like heat exchangers
  • the width and / or the length and / or the height of the circular segment-like exhibition and / or the distance between two adjacent circular segment-like exhibitions and / or the distance of the circular segment-like exhibition depends on a passage of the heat to be achieved by the circular segment-like exhibition the passage.
  • the design of the plate-shaped heat exchanger can always be adapted concretely to the desired performance requirements of the cooling device.
  • the circular segment-like distributions are arranged in two or more rows around the passage.
  • the air flow is amplified in the direction of the passage, which also improves the heat conduction.
  • the exhibitions are radstrahlenähniich arranged around the passage. This has the advantage that flow recirculation of the charge air to generate turbulence very well, at the same time a short direct path for the heat conduction to the passages and thus to the round tubes of the cooling device is present.
  • the pointing in the direction of the passage ends of the beam-like exhibitions are arranged approximately circularly around the passage, along the longitudinal extension of at least one radiation-like exhibition, a first material overhang runs, which releases the air exchange in the direction of passage and in particular the width of the strahtenähnfichen exhibition and / or the height of the radiation-like exhibition and / or the depth of the radiation-like exhibition depends on the heat conduction to be achieved by the radiation-like exhibition on the passage.
  • the Materiaiüber the air currents are channeled, and improves the cross-exchange between the overlying plate-shaped heat exchangers. This cross-exchange leads to a more homogeneous flow through the charge air.
  • the radiation-like exhibitions are subdivided into at least two groups, which are arranged around the passage such that each group is positioned at a distance from a line extending approximately centrally through the passage and perpendicular to an edge of the heat exchanger. Since the heat exchanger is designed as a band-shaped stamped sheet metal part, it is necessary to separate it into the desired size of the individual plate-shaped heat exchangers. So that the structure of the heat exchanger is not disturbed by the singulation process, the invention advantageously provides for the distance between these groups.
  • the passage at a distance from the surface of the heat exchanger has a second material overhang for receiving an overlying heat exchanger.
  • the passage itself serves as a spacer to the overlying heat exchanger. Additional spacers can therefore be dispensed with. This simplifies the process of making the heat exchanger.
  • the edge region has a corrugation and / or at least one bead and / or at least one turbulator and / or at least one spacer are arranged in the edge region and / or the width of the edge region is up to one reduced first row of passages.
  • Figure 3 a second plate-shaped heat exchanger according to the prior
  • FIG. 6 a plate-shaped heat exchanger with radiation-like displays
  • FIG. 7 shows a cross section through an exhibition made as a gill
  • FIG. 8 shows a plate-shaped heat exchanger with gills made as gills
  • FIG. 9 is a plan view of a plate-shaped heat exchanger with radiation-like gills in the form of gills;
  • FIG. 10 a second plate-shaped heat exchanger with radiation-like gills designed as gills,
  • FIG. 11 edge region of the plate-shaped heat exchanger
  • Figure 5 shows a section of a plate-shaped heat exchanger 2 with circular segment-like exhibitions 10, which surround the opening 7.
  • the circle-segment-like exhibitions 10 thereby form a circle around the opening 7.
  • Figure 5a discloses circular segment-like exhibitions 10, where each circular segment-like Exhibition 10 approximately covers an angle of 90 °.
  • FIG. 5c shows circular segment-like partitions 10, which are considerably shorter than the circular segment-like exhibitions according to FIGS. 5a and 5b.
  • the circular segment-like exhibitions 10 can also be arranged in several rows around the opening 7.
  • Each circular segment-like exhibition 10 represents an expression which is arranged around the opening 7, wherein each opening 7 is surrounded by a circular passage 4.
  • the plate-shaped heat exchanger 2 which are stacked over each other and form a package, performed charge air 6, which originates from an internal combustion engine, the heat contained in the charge air 6 is delivered to the niksegmentähniichen exhibitions 10.
  • the circular segment-like exhibitions TO serve not only as a heat exchanger but also at the same time as a turbulence generator, wherein the laminar air flow of the charge air 6 is converted into a turbulent air flow. This conversion has the advantage that a good supply of heat to all niksegmentähniichen exhibitions 10 takes place.
  • the circular arrangement of the niksegmentähniichen exhibitions 10 to the passage 4 and thus the opening 7 is a restart of the flow of the charge air 6 for generating the turbulence at each niksegmentähniichen exhibition 10, which improves the heat transfer from the niksegmentähniichen exhibition 10 to the opening 7. Due to the shape of the circular segment-like exhibitions 10, their area is enlarged, which results in increased heat absorption from the charge air 6. Since the Vietnamesesegmentähniichen exhibitions 10 not shown openings, for example in the form of slots, a cross-exchange of the charge air 6 between the various plate-shaped heat exchangers 2, which are arranged above each other, guaranteed. As a result, despite inhomogeneous flow, the plate-shaped heat exchanger 2 in the direction of cooling improves heat exchange Charge air and coolant, which flows through circular pipes, not shown, which are inserted into the openings 7, realized.
  • FIG. 6 shows a plate-shaped heat exchanger 2 which has radiation-like displays 11.
  • these radiation-like displays 11 are also arranged in a circle around the passage 4 and thus around the opening 7.
  • the radiation-similar exhibitions 11 are elongated, the narrow ends 12 of the radiation-like exhibition 11 are arranged opposite the passage 4 and are guided directly to the passage 4.
  • the radiation-like exhibitions 11 have slots in their longitudinal direction, material overhangs 13 protruding from the radial displays 11.
  • the radiation-like exhibitions are designed as so-called gills 15.
  • the number of exhibitions 11 in Figure 6a and the gills 15 in Figure 5b is different depending on the size of the strahienähnlichen exhibitions 11 and the gills 15th
  • the radiation-like displays 16 are not straight as in FIG. 6a, but have a slight curvature.
  • the radiation-like exhibitions 11, 15 and 16 serve as heat exchangers, by absorbing the heat supplied by the charge air 6 and transporting in the direction of the passage 4, whereby the round tube (not shown) flows through the passage 4 with the coolant.
  • These exhibitions 11, 15 and 16 arranged in the manner of a beam have the particular advantage that the heat conduction directly to the opening 7 and thus the Round tube is directed, with no interruptions in the heat conduction is provided by intermediate structural components.
  • FIG. 7 shows a cross section through a gill 15, as it has been worked out of the plate-shaped heat exchanger 2.
  • the gill 15 projects beyond the upper side of the plate-shaped heat exchanger 2 with its first material overhang 13, while the second material overhang 14 of the gill 15 is directed in the direction below the plate-shaped heat exchanger 2. Due to this simple design, a very good transverse exchange of the charge air between the various plate-shaped heat exchangers 2 is possible.
  • these straightening-like stiffeners in the form of gills 15 can be structurally varied in their design. This concerns the width (arrow A in FIG. 8 a) as well as the depth (arrow B in FIG. 8 b) and also the height. which is indicated by the arrow C in Figure 8c. These variations improve the flow conditions at the wire-like displays 11, 15 and 16, resulting in better heat conduction and thus improved cooling equipment performance.
  • the angle of the gills 15 also contributes to better heat transfer. The planteieitung is guaranteed all the better, the greater the number of exhibitions 11, 16 and the gills 15 per passage 4.
  • FIG. 9 a shows a detail of a plan view of a plate-shaped heat exchanger 2, which has openings 7 arranged in rows, wherein each opening 7 is surrounded by a passage 4. While the centrally arranged passages 4 are completely surrounded with radiation-like exhibitions 11, in the edge region 17, the passages 4 are provided only approximately halfway with the radiation-like exhibitions 11, in the edge region 17 are located between the passages 4 on the Radar-like exhibitions 11 opposite side spacers 8. These spacers 8 have the task of stabilizing the edge region 17 against mechanical stresses.
  • FIG. 9b again shows a section around an opening 7 with a passage 4, which are surrounded by the radiation-like exhibitions 11; The radiation-like exhibitions 11 are all arranged at the same distance on a circle around the opening 7.
  • FIG. 10 shows a second illustration of a plate-shaped heat exchanger 2, in which, as can be seen in FIG. 10b, the radiation-like displays 11 are divided into two groups 18a, 18b.
  • the radiation-like exhibitions 11 have a similar distance below each other, wherein the distance AB of the two groups 18a, 18b is greater than the distance of the radiation-like exhibitions 11 within a group 18a, 18b.
  • a gap 19 thus extends between the groups 18a, 18b, which gap is used for cutting the plate-shaped heat exchanger 2 out of a strip, the structure of the plate-shaped heat exchanger 2 remaining unaffected during the cutting process.
  • FIGS. 11a to 11d show various measures for increasing the strength of the edge region 17 of the plate-shaped heat exchangers 2. Due to the charge air 6 supplied heat resulting in the edge region of the plate-shaped heat exchanger 2 vibrations, which lead to cracks and consequently to instabilities of the edge region 17 can. Such instabilities can be prevented if, as shown in Figure 11a, the edge region is reduced to the first row of passages 4 (arrow F). A second measure for improving the stability of the edge region 17 is that near the edge region 17 between two adjacent passages 4, a bead 20 is introduced ⁇ Figure 11b).
  • edge region 17 Another improvement in the stability of the edge region 17 is achieved when the entire edge region 17 has a corrugation, which ensures a stability against cracks, which is indicated in Figure 11c.
  • a turbulator or a spacer 8 which is arranged between two adjacent passages 4 (as shown in Figure 11d) * contributes to improving the strength of the Randberetch 17 at.
  • the material for the plate-shaped heat exchangers 2 aluminum, stainless steel, copper or the like is used as the material for the plate-shaped heat exchangers 2.
  • the density of the plate-shaped heat exchanger 2 in a package is to make variable, just as the longitudinal and transverse dividing arrangement of the passages 4 of the plate-shaped heat exchanger 2 is variable.
  • a use of the described plate-shaped heat exchanger 2 is not only possible in a charge air cooler, but also in Abgaskühiern, in evaporators or radiators conceivable.

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

Abstract

The invention relates to a plate-shaped heat exchanger for a cooling device comprising at least one heat exchanger package, in particular for a motor vehicle, consisting of a plurality of openings (7) for accommodating a pipe conducting a coolant, wherein each opening (7) is surrounded by an passage (4) and a plurality of projections (10, 11, 15, 16) are distributed between the passages (4) for the heat exchange with the medium to be cooled. In order to allow a high performance increase of a cooling device, yet a low increase in pressure loss of the charge air, a plurality of projections (10, 11, 15, 16) are arranged around an passage (4), wherein the projections (10, 11, 15, 16) have a shape that assures deliberate heat conduction from the projections (10, 11, 15, 16) to the passage (4).

Description

Plattenförmiger Wärmeübertrager für eine, mindestens ein Wärmeübertragerpaket aufweisende Kühleinrichtung  Plate-shaped heat exchanger for a, at least one heat exchanger package having cooling device
Die Erfindung betrifft einen plattenförmigen Wärmeübertrager für eine, mindestens ein Wärmeübertragerpaket aufweisende Kühleinrichtung, insbesondere für ein Kraftfahrzeug, bestehend aus mehreren Öffnungen zur Aufnah- me eines, ein Kühlmittel führenden Rohres, wobei jede Öffnung von einem Durchzug umgeben ist und zwischen den Durchzügen mehrere Ausstellungen zum Wärmeaustausch mit dem zu kühlenden Medium verteilt sind. The invention relates to a plate-shaped heat exchanger for a, at least one heat exchanger package having cooling device, in particular for a motor vehicle consisting of a plurality of openings for receiving a, a coolant-carrying tube, each opening is surrounded by a passage and between the passages several exhibitions to Heat exchange are distributed with the medium to be cooled.
Es sind Ladeluftkühler in Rundrohrbauweise bekannt, welche in Figur 1 dar- gestellt sind. Dabei besteht ein solcher Ladeluftkühler aus einem Paket von plattenförmigen Wärmeübertragern 2, welche auch als Wellrippen bezeichnet werden. Jeder plättenformige Wärmeübertrager 2 weist dabei mehrere Öffnungen 7 auf, in welche jeweils ein Rundrohr 3 eingepasst ist und über ein mechanisches Aufweiten der die Öffnung umgebenden Durchzüge 4 mit dem plattenförmigen Wärmeübertrager 2 verbunden ist. Durch die Rundroh- re 3 strömt ein Kühlmittel 5, während die von einem nicht weiter dargestellten Verbrennungsmotor kommende, zu kühlende Ladeluft 6 senkrecht zu den Rundrohren 3 in das, aus vielen plattenförmigen Wärmeübertragern 2 bestehende Wärmeübertragerpaket einströmt, was senkrecht zu den Rundroh- ren 3 erfolgt. There are known intercooler in round tube design, which are shown in Figure 1 are provided. In this case, there is such a charge air cooler from a package of plate-shaped heat exchangers 2, which are also referred to as corrugated fins. Each plate-shaped heat exchanger 2 in this case has a plurality of openings 7, in each of which a round tube 3 is fitted and is connected to the plate-shaped heat exchanger 2 via a mechanical widening of the passages 4 surrounding the opening. Through the round re 3 flows a coolant 5, while coming from a not shown internal combustion engine, to be cooled charge air 6 flows perpendicular to the round tubes 3 in the, consisting of many plate-shaped heat exchangers 2 heat exchanger package, which is perpendicular to the Rundroh- 3.
Ein einzelner plattenförmiger Wärmeübertrager 2 ist in Figur 2 dargestellt wobei die die Öffnungen 7 umschließenden Durchzüge 4 in mehreren Reihen angeordnet sind (Figur 2a). Figur 2b zeigt einen Querschnitt durch den plattenförmigen Wärmeübertrager 2, während Figur 2c eine perspektivische Darstellung eines Durchzuges 4 darstellt Die Durchzüge 4 stellen dabei den Kontakt zu den Rundrohren 3 sicher, welche über das Kühlmittel 5 die Wärme aus dem Ladeluftkühler 1 ableiten. Zwischen den Durchzügen 4 sind Turbuiatoren oder Abstandshalter 8 angeordnet, weiche symmetrisch zwi- sehen den, die Öffnungen 7 umschließenden Durchzügen 4 verteilt sind. Die Turbuiatoren bzw. Abstandshalter 8 nehmen den, über ihnen angeordneten plattenförmigen Wärmeübertrager 2 auf, wobei ausreichend Abstand zwischen den beiden plattenförmigen Wärmeübertragern 2 vorhanden ist, damit die vom Verbrennungsmotor kommende Ladeluft 6 zwischen diesen Wärmeübertragern 2 hindurch strömen kann. Die Turbuiatoren oder Abstandshalter 8 können außerdem eine Umwandlung der laminaren Strömung der Ladeiuft 6 in eine turbulente Strömung veranlassen, damit die Wärme- Verteilung über den gesamten plattenförmigen Wärmeübertrager 2 besser gewährleistet werden kann. A single plate-shaped heat exchanger 2 is shown in Figure 2 wherein the passages 4 enclosing the openings 7 are arranged in a plurality of rows (Figure 2a). FIG. 2b shows a cross section through the plate-shaped heat exchanger 2, while FIG. 2c shows a perspective view of a passage 4. The passages 4 ensure contact with the round tubes 3, which derive the heat from the charge air cooler 1 via the coolant 5. Between the passages 4 Turbuiatoren or spacers 8 are arranged, see symmetrically between the see, the openings 7 enclosing passages 4 are distributed. The turbulators or spacers 8 receive the plate-shaped heat exchanger 2 arranged above them, wherein there is sufficient space between the two plate-shaped heat exchangers 2 so that the charge air 6 coming from the internal combustion engine can flow between these heat exchangers 2. The turbulators or spacers 8 can also cause a transformation of the laminar flow of the Ladeiuft 6 in a turbulent flow, so that the heat distribution over the entire plate-shaped heat exchanger 2 can be better ensured.
In Figur 3 ist eine weitere, bekannte Ausführung eines plattenförmigen Wärmeübertragers 2 dargestellt, bei welchem zwischen den Durchzügen 4 ein Kiemenfeld 9 angeordnet ist. Dieses Kiemenfeld 9 hat die Aufgabe, Turbulenzen in der Luftströmung der Ladeluft 6 hervorzurufen und einen ver- besserten Queraustäusch der Ladeluft 6 zwischen den einzelnen, übereinander liegenden plattenförmigen Wärmeübertragern 2 sicherzustellen. Zu- sätzlich zu dem Kiemenfeld 9 sind Turbulatoren oder Abstandshalter 8 vorhanden, welche als Auflage für den nächsten, plattenförmigen Wärmeübertrager 2 dienen. Bei einer bekannten Ausgestaltung nach Figur 4 weist der Durchzug 4 sogenannte Krontutpen 4a auf, welche an dem Durchzug 4 an dessen Umfang herum beabstandet angeordnet sind. Diese Krontulpen 4a dienen als Abstandshalter für den darauf liegenden plattenfärmigen Wärmeübertrager 2, weshalb auf separate Abstandshaiter 8 verzichtet werden kann. Auch hierbei ist jeder Durchzug 4 und die von dem Durchzug 4 umgebene Öffnung 7 von einem Kiemenfeid 9 umgeben. FIG. 3 shows a further known embodiment of a plate-shaped heat exchanger 2, in which a gill field 9 is arranged between the passages 4. This gill field 9 has the task of causing turbulence in the air flow of the charge air 6 and to ensure an improved transverse noise of the charge air 6 between the individual, superimposed plate-shaped heat exchangers 2. To- In addition to the gill box 9 turbulators or spacers 8 are provided, which serve as a support for the next, plate-shaped heat exchanger 2. In a known embodiment of Figure 4, the passage 4 so-called crowns 4 a, which are arranged at the passage 4 at its periphery spaced around. This Krontulpen 4a serve as a spacer for the plate-lying heat exchanger lying on it 2, which is why it is possible to dispense with separate Abstandhaiter 8. Here, too, each passage 4 and the opening 4 surrounded by the passage 4 is surrounded by a gill feeder 9.
Aufgrund der oft inhomogenen Anströmung der Ladeluft 6 an dem Ladeluftkühler 1 mit hohen Ladeluftmassenströmen müssen die plattenförmigen Wärmeübertrager 2 im Betrieb eine hohe mechanische Stabilität gegenüber Vibrationen und Schwingungen aufweisen, um Brüche der Wärmeübertrager 2 zu vermeiden. Due to the often inhomogeneous flow of the charge air 6 to the intercooler 1 with high charge air mass flows, the plate-shaped heat exchanger 2 must have a high mechanical stability to vibration and vibration during operation in order to avoid fractures of the heat exchanger 2.
Der Erfindung liegt somit die Aufgabe zu Grunde, einen plattenförmigen Wärmeübertrager anzügeben, welcher eine hohe Wärmeübertragung von der Ladeluft auf das Kühlmittel ermöglicht, wobei der Druckverlust der Ladeluft so gering wie möglich zu halten ist.  The invention is therefore based on the object anzzügeben a plate-shaped heat exchanger, which allows a high heat transfer from the charge air to the coolant, wherein the pressure drop of the charge air is to be kept as low as possible.
Effindungsgemäß ist die Aufgabe dadurch gelöst, dass mehrere Ausstellungen um einen Durchzug angeordnet sind, wobei die Aussteilungen eine Form aufweisen, welche eine gezielte Wärmeleitung von den Ausstellungen auf den Durchzug gewährleisten. Durch eine solche Form der Ausstellung wird sichergestellt, dass zwar die benötigten Turbulenzen für den Wärmeaustausch durch die Ausstellungen auf dem plattenförmigen Wärmeübertrager erzeugt werden und die turbulente Luftmasse dem Durchzug zugeleitet wird, wobei aber nur ein geringer Druckverlustanstieg der Ladeluft eintritt. Vorteilhafterweise sind die Aussteifungen annähernd kreisförmig um den Durchzug angeordnet. Eine solche kreisförmige Anordnung gewährleistet, dass die turbulente Luft, welche durch die Ausstellungen hervorgerufen wird, unmittelbar dem Durchzug und somit beim Einbau in eine Kühleinrichtung dem von dem Durchzug umgebenden Rundrohr zugeleitet wird. Dadurch verbessert sich der Wärmeaustausch der Kühlei nrichtung, Effindungsgemäß the object is achieved in that several exhibitions are arranged around a passage, the Aussteilungen have a shape which ensure a targeted heat conduction from the exhibitions on the passage. Such a form of the exhibition ensures that although the turbulence required for the heat exchange through the exhibitions on the plate-shaped heat exchanger are generated and the turbulent air mass is fed to the passage, but only a slight increase in pressure loss of the charge air occurs. Advantageously, the stiffeners are arranged approximately circularly around the passage. Such a circular arrangement ensures that the turbulent air, which is caused by the exhibitions, directly to the passage and thus when installed in a cooling device is fed to the surrounding of the passage round tube. This improves the heat exchange of Kühlei device,
In einer Ausgestaltung ist die Ausstellung kreissegmentähntich ausgebildet. Durch diese kreissegmentähnliche Form der Ausstellung werden die Neuan- läufe der Strömung der Ladeiuft zur Erzeugung von Turbulenzen unterstützt und ein Queraustausch zwischen den verschiedenen plattenähnlichen Wärmeübertragern gewährleistet In one embodiment, the exhibition is kreissegmentähntich trained. This circular segment-like form of the exhibition supports the new approaches of the flow of the charge air to generate turbulence and ensures a cross-exchange between the various plate-like heat exchangers
In einer Variante hängt die Breite und/oder die Länge und/oder die Höhe der kreissegmentähnlichen Ausstellung und/oder der Abstand zwischen zwei benachbarten kreissegmentähnlichen Ausstellungen und/oder der Abstand der kreissegmentähnlichen Ausstellung zu einem Durchzug von der zu erzielenden Wärmeleitung von der kreissegmentähnlichen Ausstellung auf den Durchzug ab. Somit lässt sich die Gestaltung des plattenförmigen Wärmeübertragers immer konkret an die gewünschten Leistungsanforderungen der Kühleinrichtung anpassen. In one variant, the width and / or the length and / or the height of the circular segment-like exhibition and / or the distance between two adjacent circular segment-like exhibitions and / or the distance of the circular segment-like exhibition depends on a passage of the heat to be achieved by the circular segment-like exhibition the passage. Thus, the design of the plate-shaped heat exchanger can always be adapted concretely to the desired performance requirements of the cooling device.
In einer Weiterbildung sind die kreissegmentähnlichen Aussteilungen zwei- oder mehrreihig um den Durchzug angeordnet. Damit wird die Luftströmung in Richtung des Durchzuges verstärkt, wobei sich auch die Wärmeleitung verbessert. In a further development, the circular segment-like distributions are arranged in two or more rows around the passage. Thus, the air flow is amplified in the direction of the passage, which also improves the heat conduction.
Vorteilhafterweise sind die Ausstellungen strahlenähniich um den Durchzug angeordnet. Dies hat den Vorteil, dass sich Strömungsneuanläufe der Lade- luft zur Erzeugung von Turbulenzen sehr gut ausbilden, wobei gleichzeitig ein kurzer direkter Weg für die Wärmeleitung zu den Durchzügen und somit zu den Rundrohren der Kühleinrichtung vorhanden ist. Advantageously, the exhibitions are radstrahlenähniich arranged around the passage. This has the advantage that flow recirculation of the charge air to generate turbulence very well, at the same time a short direct path for the heat conduction to the passages and thus to the round tubes of the cooling device is present.
In einer Ausgestaltung sind die in Richtung des Durchzuges weisenden Enden der strahlenähnlichen Ausstellungen annähernd kreisförmig um den Durchzug angeordnet, wobei entlang der Längserstreckung mindestens einer strahlenähnlichen Ausstellung ein erster Materialüberhang verläuft, welcher den Luftaustausch in Richtung Durchzug frei gibt und insbesondere die Breite der strahtenähnfichen Ausstellung und/oder die Höhe der strahlenähnlichen Ausstellung und/oder die Tiefe der strahlenähnlichen Ausstellung von der zu erzielenden Wärmeleitung von der strahlenähnlichen Ausstellung auf den Durchzug abhängt. Durch die Materiaiüberhänge werden die Luftströmungen kanalisiert, und der Queraustausch zwischen den über einander liegenden plattenförmigen Wärmeübertragern verbessert. Durch diesen Queraustausch kommt es zu einer homogeneren Anströmung durch die Ladeluft. Auf Grund der Gestaltung der Materiaiüberhänge wird die gezielte Wärmeleitung auf den Durchzug auf konstruktiv einfache Art und Weise realisiert. In einer Weiterbildung sind die strahlenähnlichen Ausstellungen in wenigstens zwei Gruppen unterteilt, welche derart um den Durchzug angeordnet sind, dass jede Gruppe beabstandet zu einer, annähernd mittig durch den Durchzug verlaufenden, sich senkrecht zu einem Rand des Wärmeübertragers erstreckenden Linie positioniert ist. Da der Wärmeübert- rager als bandförmiges Stanzblechteil ausgebildet wird, ist es notwendig, diesen in die gewünschte Größe der einzelnen plattenförmigen Wärmeübertragern zu vereinzeln. Damit die Struktur des Wärmeübertragers durch den Vereinzelungsvorgang nicht gestört wird, sieht die Erfindung vor- teilhafterweise den Abstand zwischen diesen Gruppen vor. ln einer weiteren Variante weist der Durchzug im Abstand zu der Oberfläche des Wärmeübertragers einen zweiten Materialüberhang zur Aufnahme eines darüber liegenden Wärmeübertragers auf. Somit dient der Durchzug selbst als Abstandshalter zu dem darüber liegenden Wärmeübertrager. Auf zusätz- liehe Abstandshalter kann daher verzichtet werden. Dadurch wird der Her- steilungsprozess des Wärmeübertragers vereinfacht. In one embodiment, the pointing in the direction of the passage ends of the beam-like exhibitions are arranged approximately circularly around the passage, along the longitudinal extension of at least one radiation-like exhibition, a first material overhang runs, which releases the air exchange in the direction of passage and in particular the width of the strahtenähnfichen exhibition and / or the height of the radiation-like exhibition and / or the depth of the radiation-like exhibition depends on the heat conduction to be achieved by the radiation-like exhibition on the passage. Through the Materiaiüberhänge the air currents are channeled, and improves the cross-exchange between the overlying plate-shaped heat exchangers. This cross-exchange leads to a more homogeneous flow through the charge air. Due to the design of Materiaiüberhänge the targeted heat conduction is realized on the passage in a structurally simple manner. In a further development, the radiation-like exhibitions are subdivided into at least two groups, which are arranged around the passage such that each group is positioned at a distance from a line extending approximately centrally through the passage and perpendicular to an edge of the heat exchanger. Since the heat exchanger is designed as a band-shaped stamped sheet metal part, it is necessary to separate it into the desired size of the individual plate-shaped heat exchangers. So that the structure of the heat exchanger is not disturbed by the singulation process, the invention advantageously provides for the distance between these groups. In a further variant, the passage at a distance from the surface of the heat exchanger has a second material overhang for receiving an overlying heat exchanger. Thus, the passage itself serves as a spacer to the overlying heat exchanger. Additional spacers can therefore be dispensed with. This simplifies the process of making the heat exchanger.
Vorteilhafterweise weist zur Erhöhung der Festigkeit des Randbereiches des Wärmeübertragers der Randbereich eine Wellung auf und/oder im Randbe- reich sind mindestens eine Sicke und/oder mindestens ein Turbulator und/oder mindestens ein Abstandshalter angeordnet und/oder ist die Breite des Randbereiches bis zu einer ersten Reihe von Durchzügen reduziert. Durch diese Maßnahmen, welche selbständig oder in Kombination ausgeführt werden können, wird die Festigkeit des Randbereiches des plattenför- migen Wärmeübertragers mechanisch stabilisiert, wodurch Risse in diesem Bereich zuverlässig vermieden werden, Advantageously, to increase the strength of the edge region of the heat exchanger, the edge region has a corrugation and / or at least one bead and / or at least one turbulator and / or at least one spacer are arranged in the edge region and / or the width of the edge region is up to one reduced first row of passages. By means of these measures, which can be carried out independently or in combination, the strength of the edge region of the plate-shaped heat exchanger is mechanically stabilized, whereby cracks in this region are reliably avoided,
Die Erfindung iässt zahlreiche Ausführungsformen zu. Einige davon sollen anhand der in der Zeichnung dargestellten Figuren näher erläutert werden. The invention is susceptible to numerous embodiments. Some of these will be explained in more detail with reference to the figures shown in the drawing.
Es zeigt: It shows:
Figur 1 : Ladeluftkühler nach dem Stand der Technik, Figur 2: ein erster plattenförmiger Wärmeübertrager nach dem Stand der 1: intercooler according to the prior art, Figure 2: a first plate-shaped heat exchanger according to the prior
Technik,  Technology,
Figur 3: ein zweiter plattenförmiger Wärmeübertrager nach dem Stand der Figure 3: a second plate-shaped heat exchanger according to the prior
Technik, Figur 4: ein dritter plattenförmiger Wärmeübertrager nach dem Stand der Technik, Technology, 4 shows a third plate-shaped heat exchanger according to the prior art,
Figur 5; ein plattenförmiger Wärmeübertrager mit kreissegmentähnlichen Figure 5; a plate-shaped heat exchanger with circular segment-like
Ausstellungen  exhibitions
Figur 6: ein plattenförmiger Wärmeübertrager mit strahlenähnlichen Ausstellungen, FIG. 6: a plate-shaped heat exchanger with radiation-like displays,
Figur 7: ein Querschnitt durch eine als Kieme ausgefertigte Ausstellung, FIG. 7 shows a cross section through an exhibition made as a gill,
Figur 8: ein plattenförmiger Wärmeübertrager mit als Kiemen ausgefertigten FIG. 8 shows a plate-shaped heat exchanger with gills made as gills
Aussteifungen  stiffeners
Figur 9: Draufsicht auf einen plattenförmigen Wärmeübertrager mit strahlenähnlichen, als Kiemen ausgeführten Ausstellungen, FIG. 9 is a plan view of a plate-shaped heat exchanger with radiation-like gills in the form of gills;
Figur 10: ein zweiter plattenförmiger Wärmeübertrager mit strahlenähnlichen, als Kiemen ausgeführten Ausstellungen, FIG. 10: a second plate-shaped heat exchanger with radiation-like gills designed as gills,
Figur 11: Randbereich des plattenförmigen Wärmeübertragers, FIG. 11: edge region of the plate-shaped heat exchanger,
Gleiche Merkmale sind mit gleichen Bezugszeichen gekennzeichnet. Identical features are identified by the same reference numerals.
Figur 5 zeigt einen Ausschnitt aus einem plattenförmigen Wärmetauscher 2 mit kreissegmentähnlichen Ausstellungen 10, welche die Öffnung 7 umschließen. Die kreissegmentähnlichen Ausstellungen 10 bilden dabei um die Öffnung 7 einen Kreis, Wie aus den verschiedenen Figuren 5a, 5b und 5c ersichtlich, können dabei die Abmessungen der kreissegmentähnlichen Ausstellungen 10 sehr unterschiedlich gewählt werden. Figur 5a offenbart kreissegmentähnlichen Ausstellungen 10, wo jede kreissegmentähnliche Ausstellung 10 annähernd einen Winkel von 90° überstreicht. Figur 5c zeigt dabei kreissegmentähniichen Aussteilungen 10, die wesentlich kürzer sind als die kreissegmentähnlichen Ausstellungen nach Figuren 5a und 5b. Wie in Figur 5b dargestellt, können die kreissegmentähnlichen Ausstellungen 10 auch mehrreihig um die Öffnung 7 angeordnet sein. Jede kreissegmentähnliche Ausstellung 10 stellt dabei eine Ausprägung dar, welche um die Öffnung 7 angeordnet ist, wobei jede Öffnung 7 von einem kreisförmigen Durchzug 4 umgeben ist. Durch die durch die piattenförmigen Wärmeübertrager 2, welche über einander gestapelt sind und ein Paket bilden, durchgeführte Ladeluft 6, welche von einem Verbrennungsmotor herrührt, wird die in der Ladeluft 6 enthaltene Wärme an die kreissegmentähniichen Ausstellungen 10 abgegeben. Die kreissegmentähnlichen Ausstellungen TO dienen dabei nicht nur als Wärme- Übertrager sondern auch gleichzeig als Turbulenzerzeuger, wobei die laminare Luftströmung der Ladeluft 6 in eine turbulente Luftströmung umgewandelt wird. Diese Umwandlung hat den Vorteil, dass eine gute Wärmezufuhr an alle kreissegmentähniichen Ausstellungen 10 erfolgt. Durch die kreisförmige Anordnung der kreissegmentähniichen Ausstellungen 10 um den Durchzug 4 und somit die Öffnung 7 erfolgt ein Neuanlauf der Strömung der Ladeluft 6 zur Erzeugung der Turbulenzen an jeder kreissegmentähniichen Ausstellung 10, was die Wärmeübertragung von der kreissegmentähniichen Ausstellung 10 an die Öffnung 7 verbessert. Durch die Form der kreissegmentähniichen Ausstellungen 10 erfolgt eine Vergrößerung von deren Flä- che, was eine erhöhte Wärmeaufnahme aus der Ladeluft 6 nach sich zieht. Da auch die kreissegmentähniichen Ausstellungen 10 nicht weiter dargestellte Öffnungen aufweisen, beispielsweise in Form von Schlitzen, ist ein Queraustausch der Ladeluft 6 zwischen den verschiedenen piattenförmigen Wärmeübertragern 2, die über einander angeordnet sind, gewährleistet. Da- durch wird trotz inhomogener Anströmung der piattenförmigen Wärmeübertrager 2 in der Kühlein richtung ein verbesserter Wärmeaustausch zwischen Ladeluft und Kühlmittel, welches durch nicht weiter dargestellte Rundrohre fließt, die in die Öffnungen 7 eingelegt werden, realisiert. Figure 5 shows a section of a plate-shaped heat exchanger 2 with circular segment-like exhibitions 10, which surround the opening 7. The circle-segment-like exhibitions 10 thereby form a circle around the opening 7. As can be seen from the various FIGS. 5a, 5b and 5c, the dimensions of the circular segment-like exhibitions 10 can be chosen very differently. Figure 5a discloses circular segment-like exhibitions 10, where each circular segment-like Exhibition 10 approximately covers an angle of 90 °. FIG. 5c shows circular segment-like partitions 10, which are considerably shorter than the circular segment-like exhibitions according to FIGS. 5a and 5b. As shown in Figure 5b, the circular segment-like exhibitions 10 can also be arranged in several rows around the opening 7. Each circular segment-like exhibition 10 represents an expression which is arranged around the opening 7, wherein each opening 7 is surrounded by a circular passage 4. By through the plate-shaped heat exchanger 2, which are stacked over each other and form a package, performed charge air 6, which originates from an internal combustion engine, the heat contained in the charge air 6 is delivered to the kreissegmentähniichen exhibitions 10. The circular segment-like exhibitions TO serve not only as a heat exchanger but also at the same time as a turbulence generator, wherein the laminar air flow of the charge air 6 is converted into a turbulent air flow. This conversion has the advantage that a good supply of heat to all kreissegmentähniichen exhibitions 10 takes place. The circular arrangement of the kreissegmentähniichen exhibitions 10 to the passage 4 and thus the opening 7 is a restart of the flow of the charge air 6 for generating the turbulence at each kreissegmentähniichen exhibition 10, which improves the heat transfer from the kreissegmentähniichen exhibition 10 to the opening 7. Due to the shape of the circular segment-like exhibitions 10, their area is enlarged, which results in increased heat absorption from the charge air 6. Since the kreissegmentähniichen exhibitions 10 not shown openings, for example in the form of slots, a cross-exchange of the charge air 6 between the various plate-shaped heat exchangers 2, which are arranged above each other, guaranteed. As a result, despite inhomogeneous flow, the plate-shaped heat exchanger 2 in the direction of cooling improves heat exchange Charge air and coolant, which flows through circular pipes, not shown, which are inserted into the openings 7, realized.
Anstelle der kreissegmentähnlichen Ausstellungen 10 sind auch andere Ausprägungen, zum Beispiel in Form von Ellipsen, um die Durchzüge 4 möglich. Instead of the circular segment-like exhibitions 10, other forms, for example in the form of ellipses, around the passages 4 are possible.
In Figur 6 ist ein plattenförmiger Wärmeübertrager 2 dargestellt, welcher strahlenähnliche Ausstellungen 11 aufweist. Wie aus den Figuren 6a bis 6c ersichtlich, sind auch diese strahlenähnlichen Ausstellungen 11 kreisförmig um den Durchzug 4 und somit um die Öffnung 7 angeordnet. Die strahlen- ähnüchen Ausstellungen 11 sind länglich ausgebildet, wobei die schmalen Enden 12 der strahlenähnfichen Ausstellung 11 gegenüber dem Durchzug 4 angeordnet sind und bis unmittelbar an den Durchzug 4 geführt sind. Die strahlenähnlichen Ausstellungen 11 weisen dabei in ihrer Längsrichtung Schlitze auf, wobei Materialüberhänge 13 aus den strahlenförmigen Ausstellungen 11 herausragen. In Figur 5b sind die strahlenähnlichen Ausstellungen als sogenannte Kiemen 15 ausgebildet. Die Anzahl der Ausstellungen 11 in Figur 6a und der Kiemen 15 in Figur 5b ist dabei unterschiedlich je nach der Größe der strahienähnlichen Ausstellungen 11 bzw. der Kiemen 15. FIG. 6 shows a plate-shaped heat exchanger 2 which has radiation-like displays 11. As can be seen from FIGS. 6a to 6c, these radiation-like displays 11 are also arranged in a circle around the passage 4 and thus around the opening 7. The radiation-similar exhibitions 11 are elongated, the narrow ends 12 of the radiation-like exhibition 11 are arranged opposite the passage 4 and are guided directly to the passage 4. The radiation-like exhibitions 11 have slots in their longitudinal direction, material overhangs 13 protruding from the radial displays 11. In Figure 5b, the radiation-like exhibitions are designed as so-called gills 15. The number of exhibitions 11 in Figure 6a and the gills 15 in Figure 5b is different depending on the size of the strahienähnlichen exhibitions 11 and the gills 15th
In Figur 6c sind die strahlenähnlichen Ausstellungen 16 nicht wie in Figur 6a gerade ausgebildet, sondern weisen eine leichte Krümmung auf. Die strah- lenähniichen Ausstellungen 11, 15 bzw. 16 dienen als Wärmetauscher, indem sie die von der Ladeluft 6 zugeführte Wärme aufnehmen und in Richtung des Durchzuges 4 transportieren, wobei durch den Durchzug 4 das nicht weiter dargestellte Rundrohr mit dem Kühlmittel fließt. Diese strahlenähnlich angeordneten Ausstellungen 11, 15 und 16 haben dabei den beson - deren Vorteil, dass die Wärmeleitung direkt auf die Öffnung 7 und somit das Rundrohr gerichtet ist, wobei keine Unterbrechungen bei der Wärmeleitung durch dazwischen liegende konstruktive Bauteile vorhanden ist. In FIG. 6c, the radiation-like displays 16 are not straight as in FIG. 6a, but have a slight curvature. The radiation-like exhibitions 11, 15 and 16 serve as heat exchangers, by absorbing the heat supplied by the charge air 6 and transporting in the direction of the passage 4, whereby the round tube (not shown) flows through the passage 4 with the coolant. These exhibitions 11, 15 and 16 arranged in the manner of a beam have the particular advantage that the heat conduction directly to the opening 7 and thus the Round tube is directed, with no interruptions in the heat conduction is provided by intermediate structural components.
In Figur 7 ist ein Querschnitt durch eine Kieme 15 dargestellt, wie sie aus dem plattenförmigen Wärmeübertrager 2 ausgearbeitet ist. Dabei überragt die Kieme 15 mit ihrem ersten Materialüberhang 13 die Oberseite des plattenförmigen Wärmeübertragers 2, während der zweite Materialüberhang 14 der Kieme 15 in Richtung unterhalb des plattenförmigen Wärmeübertragers 2 gerichtet ist. Aufgrund dieser einfachen Gestaltung ist ein sehr guter Quer- austausch der Ladeluft zwischen den verschiedenen plattenförmigen Wärmeübertragern 2 möglich. FIG. 7 shows a cross section through a gill 15, as it has been worked out of the plate-shaped heat exchanger 2. In this case, the gill 15 projects beyond the upper side of the plate-shaped heat exchanger 2 with its first material overhang 13, while the second material overhang 14 of the gill 15 is directed in the direction below the plate-shaped heat exchanger 2. Due to this simple design, a very good transverse exchange of the charge air between the various plate-shaped heat exchangers 2 is possible.
Wie aus Figur 8 ersichtlich, lassen sich diese strahfenähnlichen Aussteifungen in Form von Kiemen 15 konstruktiv einfach in ihrer Gestaltung variieren, Dies betrifft die Breite (Pfeil A in Figur 8a) genauso wie die Tiefe (Pfeil B in Figur 8b) und auch die Höhe, was durch den Pfeil C in Figur 8c gekennzeichnet ist. Durch diese Variationen verbessern sich die Strömungsbedingungen an den strahfenähnlichen Ausstellungen 11, 15 und 16, was zu einer besseren Wärmeleitung und somit zu einer verbesserten Leistungsfähigkeit der Kühleinrichtung führt. Auch der Winkel der Kiemen 15 trägt zur besseren Wärmeübertragung bei. Die Wärmeieitung ist dabei umso besser gewährleistet, je größer die Anzahl der Ausstellungen 11, 16 bzw. der Kiemen 15 pro Durchzug 4 ist. In Figur 9a ist ein Ausschnitt auf eine Draufsicht auf einen plattenförmigen Wärmeübertrager 2 dargestellt, welcher in Reihen angeordnete Öffnungen 7 aufweist, wobei jede Öffnung 7 von einem Durchzug 4 umgeben ist. Während die mittig angeordneten Durchzüge 4 vollständig mit strahlenähnlichen Ausstellungen 11 umgeben sind, sind im Randbereich 17 die Durchzüge 4 nur etwa hälftig mit den strahlenähnlichen Ausstellungen 11 versehen, im Randbereich 17 befinden sich zwischen den Durchzügen 4 auf der den strahlenähnlichen Ausstellungen 11 entgegen gesetzten Seite Abstandshalter 8. Diese Abstandshalter 8 haben die Aufgabe, den Randbereich 17 gegenüber mechanischen Spannungen zu stabilisieren. In Figur 9b ist noch einmal ein Ausschnitt um eine Öffnung 7 mit einem Durchzug 4 dargestellt, die von den strahienähnlichen Ausstellungen 11 umgeben sind; Dabei sind die strahlenähnlichen Ausstellungen 11 alle im gleichen Abstand auf einem Kreis um die Öffnung 7 angeordnet. As can be seen from FIG. 8, these straightening-like stiffeners in the form of gills 15 can be structurally varied in their design. This concerns the width (arrow A in FIG. 8 a) as well as the depth (arrow B in FIG. 8 b) and also the height. which is indicated by the arrow C in Figure 8c. These variations improve the flow conditions at the wire-like displays 11, 15 and 16, resulting in better heat conduction and thus improved cooling equipment performance. The angle of the gills 15 also contributes to better heat transfer. The Wärmeieitung is guaranteed all the better, the greater the number of exhibitions 11, 16 and the gills 15 per passage 4. FIG. 9 a shows a detail of a plan view of a plate-shaped heat exchanger 2, which has openings 7 arranged in rows, wherein each opening 7 is surrounded by a passage 4. While the centrally arranged passages 4 are completely surrounded with radiation-like exhibitions 11, in the edge region 17, the passages 4 are provided only approximately halfway with the radiation-like exhibitions 11, in the edge region 17 are located between the passages 4 on the Radar-like exhibitions 11 opposite side spacers 8. These spacers 8 have the task of stabilizing the edge region 17 against mechanical stresses. FIG. 9b again shows a section around an opening 7 with a passage 4, which are surrounded by the radiation-like exhibitions 11; The radiation-like exhibitions 11 are all arranged at the same distance on a circle around the opening 7.
Figur 10 zeigt eine zweite Darstellung eines plattenförmigen Wärmeübertragers 2, bei welchem, wie aus Figur 10b ersichtlich, die strahlenähnlichen Ausstellungen 11 ih zwei Gruppen 18a, 18b unterteilt sind. In jeder Gruppe 18a, 18b weisen die strahlenähnlichen Ausstellungen 11 dabei einen gleichartigen Abstand unter einander auf, wobei der Abstand AB der beiden Gruppen 18a, 18b unter einander größer ist als der Abstand der strahienähnlichen Ausstellungen 11 innerhalb einer Gruppe 18a, 18b. Wie aus Figur 10a ersichtlich, erstreckt sich somit zwischen den Gruppen 18a, 18b ein Spalt 19, welcher zum Zuschneiden der plattenförmigen Wärmeübertrager 2 aus einem Band genutzt wird, wobei beim Zuschneidprozess die Struktur der plattenförmigen Wärmeübertrager 2 unbeeinfiusst bleibt. FIG. 10 shows a second illustration of a plate-shaped heat exchanger 2, in which, as can be seen in FIG. 10b, the radiation-like displays 11 are divided into two groups 18a, 18b. In each group 18a, 18b, the radiation-like exhibitions 11 have a similar distance below each other, wherein the distance AB of the two groups 18a, 18b is greater than the distance of the radiation-like exhibitions 11 within a group 18a, 18b. As can be seen from FIG. 10a, a gap 19 thus extends between the groups 18a, 18b, which gap is used for cutting the plate-shaped heat exchanger 2 out of a strip, the structure of the plate-shaped heat exchanger 2 remaining unaffected during the cutting process.
Bei den im Zusammenhang mit Figur 9 und 10 erläuterten Varianten ist eine Leistungssteigerung der Wärmeübertragung von etwa 10% bei einem Druck- veriustanstieg von etwa < 50% der Ladeluft 6 gewährleistet. Somit werden die wachsenden Leistungsanförderungen bei Kühleinrichtungen gewährleis- tet. In the variants explained in connection with FIGS. 9 and 10, a performance increase of the heat transfer of approximately 10% is ensured with a pressure increase of approximately <50% of the charge air 6. Thus, the growing power deliveries in cooling devices are guaranteed.
In den Figuren 11a bis 11d sind verschiedene Maßnahmen zur Erhöhung der Festigkeit des Randbereiches 17 der plattenförmigen Wärmeübertrager 2 dargestellt. Aufgrund der mit der Ladeluft 6 zugeführten Wärme ergeben sich im Randbereich der plattenförmigen Wärmeübertrager 2 Vibrationen, welche zu Rissen und demzufolge zu Instabilitäten des Randbereichs 17 führen können. Solche Instabilitäten können verhindert werden, wenn, wie in Figur 11a dargestellt, der Randbereich bis zur ersten Reihe der Durchzüge 4 verringert wird (Pfeil F). Eine zweite Maßnahme zur Verbesserung der Stabilität des Randbereiches 17 besteht darin, dass nahe des Rändbereiches 17 zwischen zwei nebeneinander liegenden Durchzüge 4 eine Sicke 20 eingebracht wird {Figur 11b). FIGS. 11a to 11d show various measures for increasing the strength of the edge region 17 of the plate-shaped heat exchangers 2. Due to the charge air 6 supplied heat resulting in the edge region of the plate-shaped heat exchanger 2 vibrations, which lead to cracks and consequently to instabilities of the edge region 17 can. Such instabilities can be prevented if, as shown in Figure 11a, the edge region is reduced to the first row of passages 4 (arrow F). A second measure for improving the stability of the edge region 17 is that near the edge region 17 between two adjacent passages 4, a bead 20 is introduced {Figure 11b).
Eine andere Verbesserung der Stabilität des Randbereiches 17 wird erzielt, wenn der gesamte Randbereich 17 eine Wellung aufweist, was eine Stabilität gegen Risse gewährleistet, was in Figur 11c angedeutet ist. Another improvement in the stability of the edge region 17 is achieved when the entire edge region 17 has a corrugation, which ensures a stability against cracks, which is indicated in Figure 11c.
Auch ein Turbulator oder ein Abstandshalter 8, welcher zwischen zwei neben einander liegenden Durchzügen 4 angeordnet ist (wie in Figur 11d darge- stellt)* trägt zur Verbesserung der Festigkeit des Randberetches 17 bei. Also, a turbulator or a spacer 8, which is arranged between two adjacent passages 4 (as shown in Figure 11d) * contributes to improving the strength of the Randberetch 17 at.
Für alle erläuterten Varianten gilt, dass als Material für die plattenförmigen Wärmeübertrager 2 Aluminium, Edelstahl, Kupfer oder Ähnliches eingesetzt wird. Die Dichte der plattenförmigen Wärmeübertrager 2 in einem Paket ist dabei variabel zu gestalten, genauso wie die längs- und querteilende Anordnung der Durchzüge 4 der plattenförmigen Wärmeübertrager 2 variabel ist. Ein Einsatz der beschriebenen plattenförmigen Wärmeübertrager 2 ist dabei nicht nur in einem Ladeluftkühler möglich, sondern auch in Abgaskühiern, in Verdampfern oder Heizkörpern denkbar. For all the variants explained, aluminum, stainless steel, copper or the like is used as the material for the plate-shaped heat exchangers 2. The density of the plate-shaped heat exchanger 2 in a package is to make variable, just as the longitudinal and transverse dividing arrangement of the passages 4 of the plate-shaped heat exchanger 2 is variable. A use of the described plate-shaped heat exchanger 2 is not only possible in a charge air cooler, but also in Abgaskühiern, in evaporators or radiators conceivable.
Durch die beschriebene Vorrichtung ist eine hohe Leistungssteigerung bei dem Wärmeaustausch der Kühleinrichtung möglich. Dabei ist ein verringerter Druckverlustanstieg der Ladetuft gewährleistet und eine mechanische Stabilität des Randbereiches gegen Vibrationen gegeben, By the device described a high performance increase in the heat exchange of the cooling device is possible. In this case, a reduced increase in pressure loss of the charge air is ensured and given a mechanical stability of the edge region against vibrations,

Claims

P a t e n ta n s p r ü c h e P aht ta pspr o
1. Plattenförmiger Wärmeübertrager für eine, mindestens ein Wärmeübertragerpaket aufweisende Kühleinrichtung, insbesondere für ein Kraftfahrzeug, bestehend aus mehreren Öffnungen (7) zur Aufnahme eines, ein Kühlmittel führenden Rohres, wobei jede Öff- nung (7) von einem Durchzug (4) umgeben ist und zwischen den1. Plate-shaped heat exchanger for a, at least one heat exchanger package having cooling device, in particular for a motor vehicle, comprising a plurality of openings (7) for receiving a, a coolant-carrying tube, each opening (7) of a passage (4) is surrounded and between the
Durchzügen (4) mehrere Aussteltungen (10, 11, 15, 16) zum Wärmeaustausch mit dem zu kühlenden Medium verteilt sind, dadurch gekennzeichnet, dass mehrere Ausstellungen (10,11 , 15, 16) um einen Durchzug (4) angeordnet sind., wobei die Ausstellungen (10, 11, 15, 16) eine Form aufweisen, welche eine gezielte Wärmeleitung von derPassages (4) several Aussteltungen (10, 11, 15, 16) are distributed for heat exchange with the medium to be cooled, characterized in that a plurality of exhibitions (10,11, 15, 16) are arranged around a passage (4) . , wherein the exhibitions (10, 11, 15, 16) have a shape which a targeted heat conduction of the
Ausstellung (10, 11 , 15, 16) auf den Durchzug (4) gewährleistet. Exhibition (10, 11, 15, 16) on the passage (4) guaranteed.
2. Wärmeübertrager nach Anspruch 1, dadurch gekennzeichnet, dass die Ausstellungen (11 , 15, 16) annähernd kreisförmig um den Durch- zug (4) angeordnet sind, 2. Heat exchanger according to claim 1, characterized in that the exhibitions (11, 15, 16) are arranged approximately in a circle around the passage (4),
3. Wärmeübertrager nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Aussteifung (10) kreissegmentähnlich ausgebildet ist. 3. Heat exchanger according to claim 1 or 2, characterized in that the stiffener (10) is formed kreissegmentähnlich.
4. Wärmeübertrager nach Anspruch 3, dadurch gekennzeichnet, dass die Breite und/oder die Länge und/öder die Höhe der kreissegment- ähniichen Ausstellung (10) und/oder der Abstand zwischen zwei benachbarten kreissegmentähniichen Ausstellungen (10) ühd/oder der Abstand der kreissegmentähnlichen Ausstellung (10) zu einem Durchzug (4) von der zu erzielenden Wärmeleitung von der kreissegmentähniichen Ausstellung (10) auf den Durchzug (4) abhängt. 4. Heat exchanger according to claim 3, characterized in that the width and / or the length and / or the height of the kreissegment- similar exhibition (10) and / or the distance between two adjacent kreissegmentähniichen exhibitions (10) ühd / or the distance of circular segment-like exhibition (10) to a passage (4) depends on the heat to be achieved by the kreissegmentähniichen exhibition (10) on the passage (4).
5. Wärmeübertrager nach Anspruch 3 oder 4, dadurch gekennzeichnet, dass die kreissegmentähnlichen Aussteilungen (10) zwei- oder mehrreihig um den Durchzug (4) angeordnet sind. 5. Heat exchanger according to claim 3 or 4, characterized in that the circular segment-like Aussteilungen (10) two or more rows around the passage (4) are arranged.
6. Wärmeübertrager nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Aussteilungen (11, 15, 16) strahienähnlich um den Durchzug (4) angeordnet sind. 6. Heat exchanger according to claim 1 or 2, characterized in that the Aussteilungen (11, 15, 16) are arranged like a beam around the passage (4).
7. Wärmeübertrager nach Anspruch 6, dadurch gekennzeichnet, dass die in Richtung des Durchzuges (4) weisenden Enden (12) der strah- fenähniichen Ausstellungen (11, 15., 16) annähernd kreisförmig um den Durchzug (4) angeordnet sind* wobei entlang der Längserstreckung mindestens einer strahlenähnlichen Ausstellung (11, 15, 16) ein erster Materialüberhang (13) verläuft, welcher den Luftaustausch in7. The heat exchanger according to claim 6, characterized in that in the direction of the rim (4) facing ends (12) of the radiation-fenähniichen exhibitions (11, 15th, 16) approximately in a circle around the passage (4) are arranged * along with the longitudinal extent of at least one radiation-like exhibition (11, 15, 16), a first material overhang (13) extends, which the air exchange in
Richtung Durchzug (4) freigibt und insbesondere die Breite der strahlenähnlichen Ausstellung (11 , 15, 16) und/oder die Höhe der strahlenähnlichen Ausstellung (11, 15, 16) und/oder die Tiefe der strahlenähnlichen Ausstellung (11, 15, 16) von der zu erzielenden Wärmeleitung von der strahlenähnlichen Ausstellung (11 , 15, 16) auf den DurchzugDirection of passage (4) releases and in particular the width of the radiation-like exhibition (11, 15, 16) and / or the height of the radiation-like exhibition (11, 15, 16) and / or the depth of the radiation-like exhibition (11, 15, 16) of the thermal conduction to be achieved by the radiation-like exhibition (11, 15, 16) on the passage
(4) abhängt. (4) depends.
8. Wärmeübertrager nach Anspruch 6 oder 7, dadurch gekennzeichnet, dass die strahlenähnlichen Ausstellungen (11 , 15, 16) in wenigstens zwei Gruppen (18a, 18b) unterteilt sind, welche derart um den Durchzug (4) angeordnet sind, dass jede Gruppe (18a, 18b) beabstandet zu einer, annähernd mittig durch den Durchzug (4) verlaufenden, sich senkrecht zu einem Rand (17) des Wärmeüberträgers (2) erstreckenden Linie positioniert ist 9. Wärmeübertrager nach mindestens einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Durchzug (4) im Abstand zu der Oberfläche des Wärmeübertragers (2) einen zweiten Material- Überhang zur Aufnahme eines darüber liegenden Wärmeübertragers (2) aufweist. 10. Wärmeübertrager nach mindestens einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass zu Erhöhung der Festigkeit des Randbereiches (17) des Wärmeübertragers (2) der Randbereich (17) eine Weifung aufweist und/oder Im Randbereich (17) mindestens eine Sicke (20) und/oder mindestens einen Turbulator und/oder mindestens ein Abstandshalter (8) angeordnet ist und/oder die Breite des Randbereiches (17) bis zu einer ersten Reihe von Durchzügen (4) reduziert ist. 8. Heat exchanger according to claim 6 or 7, characterized in that the beam-like exhibitions (11, 15, 16) are subdivided into at least two groups (18a, 18b) which are arranged around the passage (4) such that each group ( A heat exchanger according to at least one of the preceding claims, characterized in that the Passage (4) at a distance from the surface of the heat exchanger (2) a second material Overhang for receiving an overlying heat exchanger (2). 10. Heat exchanger according to at least one of the preceding claims, characterized in that to increase the strength of the edge region (17) of the heat exchanger (2) of the edge region (17) has a Weifung and / or in the edge region (17) at least one bead (20) and / or at least one turbulator and / or at least one spacer (8) is arranged and / or the width of the edge region (17) is reduced to a first series of passages (4).
EP11741208.0A 2010-08-05 2011-08-04 Plate-shaped heat exchanger for a cooling device comprising at least one heat exchanger package Ceased EP2601474A2 (en)

Applications Claiming Priority (2)

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DE102010038945A DE102010038945A1 (en) 2010-08-05 2010-08-05 Plate-shaped heat exchanger for a, at least one heat exchanger package having cooling device
PCT/EP2011/063469 WO2012017044A2 (en) 2010-08-05 2011-08-04 Plate-shaped heat exchanger for a cooling device comprising at least one heat exchanger package

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US (1) US9638476B2 (en)
EP (1) EP2601474A2 (en)
KR (1) KR20130096264A (en)
CN (1) CN203550720U (en)
DE (1) DE102010038945A1 (en)
WO (1) WO2012017044A2 (en)

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US9638476B2 (en) 2017-05-02
DE102010038945A1 (en) 2012-02-09
US20130264038A1 (en) 2013-10-10
CN203550720U (en) 2014-04-16
WO2012017044A2 (en) 2012-02-09
KR20130096264A (en) 2013-08-29
WO2012017044A3 (en) 2012-04-05

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