EP1687580B1 - Charge-air/coolant radiator - Google Patents

Charge-air/coolant radiator Download PDF

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Publication number
EP1687580B1
EP1687580B1 EP04818135.8A EP04818135A EP1687580B1 EP 1687580 B1 EP1687580 B1 EP 1687580B1 EP 04818135 A EP04818135 A EP 04818135A EP 1687580 B1 EP1687580 B1 EP 1687580B1
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EP
European Patent Office
Prior art keywords
heat exchanger
coolant
charge
exchanger medium
air
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.)
Not-in-force
Application number
EP04818135.8A
Other languages
German (de)
French (fr)
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EP1687580A1 (en
Inventor
Daniel Hendrix
Florin Moldovan
Jürgen Wegner
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
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Mahle Behr GmbH and Co KG
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Publication of EP1687580A1 publication Critical patent/EP1687580A1/en
Application granted granted Critical
Publication of EP1687580B1 publication Critical patent/EP1687580B1/en
Anticipated expiration legal-status Critical
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/026Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • 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
    • F28D9/0031Heat-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 conduits for one heat-exchange medium being formed by paired plates touching each other
    • F28D9/0043Heat-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 conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another
    • F28D9/005Heat-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 conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another the plates having openings therein for both heat-exchange media
    • 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
    • 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
    • F28D2021/0089Oil coolers

Definitions

  • the invention relates to a charge air / coolant cooler in disk construction according to the preamble of claim 1.
  • the publication WO 01/67021 A1 discloses a stacked disc radiator of stacked discs with openings for ingress and outflow of the respective medium.
  • a charge air / coolant cooler in disk construction, wherein two adjacent disks define a gap which is traversed by a heat transfer medium, in particular a coolant, preferably a mixture with water and glycol, or a second medium to be cooled or heated, wherein the inlet and / or outflow region of the heat transfer medium and / or second Medium is extended at least off or on the inflow side.
  • a heat transfer medium in particular a coolant, preferably a mixture with water and glycol, or a second medium to be cooled or heated
  • the inlet and / or outflow region of the heat transfer medium and / or second Medium is extended at least off or on the inflow side.
  • the inlet and / or outflow region of a fluid to be cooled for example charge air, which forms the second medium, is widened.
  • charge air / coolant cooler allows a good distribution of the corresponding medium on the relevant for the heat transfer surface of the individual discs, which form the heat exchanger.
  • the uniform flow distribution reduces the boiling problem in heat exchangers used in such critical areas.
  • the area preferably runs at least over one third, in particular over half, of the width of the pane straight.
  • the region extends perpendicularly or substantially over at least part of the slice width, i. at an angle of 80 ° to 100 °, transverse to the mean flow direction of the second medium, in particular a fluid to be cooled.
  • the opening for the second medium in an end region of the disk preferably extends substantially over the entire surface thereof, excluding edge regions and regions in which channels for the heat transfer medium are arranged.
  • At least two heat transfer medium channels per heat transfer medium inlet and / or outlet are provided.
  • Such a trained heat exchanger allows a good distribution of the heat transfer medium on the relevant for the heat transfer surface of the individual discs, which form the heat exchanger.
  • the uniform flow distribution reduces the boiling problem in such a way critical areas used heat overlays.
  • the heat transfer medium channels are thereby formed, as well as the inflow or outflow regions of the medium to be cooled / heated, preferably by in particular aligned apertures in the individual disks.
  • the heat transfer medium distribution is assisted by an embodiment of the disks which is axisymmetric with respect to the heat transfer medium channels with respect to their longitudinal axis. If the disks are furthermore designed to be axially symmetrical with respect to their transverse axis with regard to the heat exchanger medium channels, the assembly is simplified.
  • a single heat transfer medium inlet and / or a single heat transfer medium outlet is provided, which has a branching or merging. This allows a relatively simple structure with improved heat transfer due to the better flow distribution.
  • the branching and / or the merging are preferably circular-arc-shaped, so that a space-saving construction or the like around the individual discs together holding bolts. is possible.
  • a bend of 30 ° to 90 °, as seen in the flow direction, is preferably provided, wherein the forked part of the branching or merging is aligned parallel to the disks.
  • the heat transfer medium inlet entering the two heat transfer medium channels after the branching preferably runs parallel to the heat transfer medium channels, while the two-part part of the branching preferably takes place in a plane lying perpendicular thereto is.
  • the heat transfer medium outlet which merges into the merger from two heat transfer medium channels preferably runs parallel to the heat transfer medium channels, while the two-part part of the branch is preferably arranged in a plane lying perpendicular thereto. This allows a compact and space-saving design of the heat exchanger.
  • the supply can also be effected by means of two individual, separately formed tubes, which are connected to one another via a Y-shaped connecting piece.
  • a charge air / coolant cooler for cooling the charge air is preferred.
  • a mixture with water and glycol is preferably used as the heat transfer medium (coolant).
  • Coolant discs 2 Serving as a heat exchanger between charge air and coolant charge air / coolant radiator 1 has a plurality of stacked coolant discs 2.
  • two inlet openings 3 and two outlet openings 4 are provided in each coolant disc 2, is supplied by the heat transfer medium as coolant to the interstices of the coolant disks 2 and discharged from it.
  • the flow direction is illustrated in the figures by arrows.
  • the coolant spreads after entering through the inlet openings 3 over the entire width of the interstices of the coolant disks 2 and flows uniformly in the direction of the outlet openings 4 (see Fig.
  • the openings 3 and 4 of the stacked coolant disks 2 form coolant channels 5 and 6.
  • the areas of the openings 3 and 4 are formed correspondingly raised, so that there is sufficient space for the charge air to flow through between the coolant disks 2 and can be cooled.
  • the two coolant channels 5 begin - seen in the flow direction of the coolant - at a junction 7, which has a circular arc-shaped bifurcation 8 and a centrally arranged in the arc thereof, arranged parallel to the coolant channels 5 coolant inlet 9.
  • the coolant supplied through the coolant inlet 9 is divided equally between the two coolant channels 5.
  • the exit is formed.
  • the two coolant channels 6 end with a combination 10, which is formed according to the branch 7 and has a coolant outlet 11.
  • the charge air (second medium) is supplied via a charge air inlet 20, via a charge air channel 21, which is formed by openings 22 of the stacked coolant discs 2, the spaces between the flowed through by the coolant spaces of the coolant discs. 2 fed and passes through on the other side of the coolant disks 2 formed openings 23, which form a second charge air channel 24 to the charge air outlet 25th
  • the openings 22 and 23 are, contrary to the prior art (in Fig. 5 shown in dashed lines) are not circular, but have a portion 26 which is substantially straight according to the first embodiment, wherein it is arranged perpendicular to the normal flow direction of the charge air, so that in this region 26 tangentially with respect conventional shape, which corresponds to the inner circle of the openings 22 and 23, is arranged.
  • the openings 22 and 23 each occupy the entire end portion of the coolant disk 2, except for an outer edge 27, the two coolant channels 5 and 6 and each one surrounding the coolant channels edge 28 occupies.
  • the region 26 of the opening 23 is formed such that it extends over the entire end portion of the coolant discs 2, wherein it is arranged perpendicular to the mean flow direction of the charge air.
  • the coolant channels are arranged further offset inwards, so that the shape of a rounded triangle results.
  • the other side of the coolant disc 2 is formed accordingly.
  • coolant disc corresponds to the opening 23 about the opening 23 of the second embodiment, wherein only a coolant channel is provided, which is laterally displaced in the region of the opening 23, so that the opening 23, the end portion of the coolant disc. 2 apart from an outer edge 27, the coolant channel and a coolant channel surrounding edge 28 occupies.
  • the other side of the coolant disc 2 is designed accordingly, in particular axially symmetrical to the central transverse axis or point-symmetrical to the center of the coolant disc.

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

Description

Die Erfindung betrifft einen Ladeluft-/Kühlmittel-Kühler in Scheibenbauweise gemäß dem Oberbegriff von Anspruch 1.The invention relates to a charge air / coolant cooler in disk construction according to the preamble of claim 1.

Bei herkömmlichen Ladeluft-/Kühlmittel-Kühlern in Scheibenbauweise wird die Ladeluft und das Kühlmittel über je einen einzigen Stutzen, der einen kreisförmigen Querschnitt aufweist, in die Scheiben eingebracht. Ein derartiger Ladeluft-/Kühlmittel-Kühler lässt insbesondere in Hinblick auf die Kühlleistung noch Wünsche offen.In conventional disk-type charge / coolant coolers, the charge air and the coolant are introduced into the disks via a single nozzle each having a circular cross-section. Such a charge air / coolant cooler still leaves something to be desired, especially with regard to the cooling performance.

Die Druckschrift WO 01/67021 A1 offenbart einen Stapelscheibenkühler aus aufeinander gestapelten Scheiben mit Öffnungen zum Ein- und Ausströmen des jeweiligen Mediums.The publication WO 01/67021 A1 discloses a stacked disc radiator of stacked discs with openings for ingress and outflow of the respective medium.

Es ist Aufgabe der Erfindung, einen verbesserten Ladeluft-/Kühlmittel-Kühler zur Verfügung zu stellen.It is an object of the invention to provide an improved charge air / coolant radiator available.

Diese Aufgabe wird gelöst durch einen Ladeluft-/Kühlmittel-Kühler mit den Merkmalen von Anspruch 1. Vorteilhafte Ausgestaltungen sind Gegenstand der Unteransprüche.This object is achieved by a charge air / coolant radiator with the features of claim 1. Advantageous embodiments are the subject of the dependent claims.

Erfindungsgemäß ist ein Ladeluft-/Kühlmittel-Kühler in Scheibenbauweise vorgesehen, wobei zwei benachbarte Scheiben einen Zwischenraum definieren, der von einem Wärmeübertragermedium, insbesondere ein Kühlmittel, bevorzugt ein Gemisch mit Wasser und Glykol, oder einem zu kühlenden oder zu erwärmenden zweiten Medium durchströmt ist, wobei der Ein- und/oder Ausström-Bereich des Wärmeübertragermediums und/oder zweiten Mediums zumindest ab- bzw. zuströmseitig erweitert ist. Hierbei ist insbesondere der Ein- und/oder Ausström-Bereich eines zu kühlenden Fluids, beispielsweise Ladeluft, welches das zweite Medium bildet, erweitert ausgebildet.According to the invention, a charge air / coolant cooler is provided in disk construction, wherein two adjacent disks define a gap which is traversed by a heat transfer medium, in particular a coolant, preferably a mixture with water and glycol, or a second medium to be cooled or heated, wherein the inlet and / or outflow region of the heat transfer medium and / or second Medium is extended at least off or on the inflow side. In this case, in particular, the inlet and / or outflow region of a fluid to be cooled, for example charge air, which forms the second medium, is widened.

Ein derartiger, erfindungsgemäß ausgebildeter Ladeluft-/Kühlmittel-Kühler ermöglicht eine gute Verteilung des entsprechenden Mediums über die für die Wärmeübertragung relevante Fläche der einzelnen Scheiben, welche den Wärmeübertrager bilden. Durch die gleichmäßige Strömungsverteilung verringert sich die Siedeproblematik bei in derart kritischen Bereichen eingesetzten Wärmeübertragern.Such, designed according to the invention charge air / coolant cooler allows a good distribution of the corresponding medium on the relevant for the heat transfer surface of the individual discs, which form the heat exchanger. The uniform flow distribution reduces the boiling problem in heat exchangers used in such critical areas.

Der Bereich verläuft bevorzugt zumindest über ein Drittel, insbesondere über die Hälfte, der Scheibenbreite gerade.The area preferably runs at least over one third, in particular over half, of the width of the pane straight.

Vorzugsweise verläuft der Bereich zumindest über einen Teil der Scheibenbreite senkrecht oder im Wesentlichen, d.h. in einem Winkel von 80° bis 100°, quer zur mittleren Strömungsrichtung des zweiten Mediums, insbesondere eines zu kühlenden Fluids.Preferably, the region extends perpendicularly or substantially over at least part of the slice width, i. at an angle of 80 ° to 100 °, transverse to the mean flow direction of the second medium, in particular a fluid to be cooled.

Die Öffnung für das zweite Medium in einem Endbereich der Scheibe erstreckt sich vorzugsweise im Wesentlichen über die gesamte Fläche derselben, wobei Randbereiche und Bereiche, in denen Kanäle für das Wärmeübertragermedium angeordnet sind, ausgenommen sind.The opening for the second medium in an end region of the disk preferably extends substantially over the entire surface thereof, excluding edge regions and regions in which channels for the heat transfer medium are arranged.

Bevorzugt sind mindestens zwei Wärmeübertragermedium-Kanäle je Wärmeübertragermedium-Ein- und/oder -Austritt vorgesehen. Ein derartig ausgebildeter Wärmeübertrager ermöglicht eine gute Verteilung des Wärmeübertragermediums über die für die Wärmeübertragung relevante Fläche der einzelnen Scheiben, welche den Wärmeübertrager bilden. Durch die gleichmäßige Strömungsverteilung verringert sich die Siedeproblematik bei in derart kritischen Bereichen eingesetzten Wärmeüberkragern. Die Wärmeübertragermedium-Kanäle werden dabei genauso wie die Einström- beziehungsweise Ausströmbereiche des zu kühlenden/erwärmenden Mediums vorzugsweise durch insbesondere miteinander fluchtende Durchbrüche in den einzelnen Scheiben gebildet.Preferably, at least two heat transfer medium channels per heat transfer medium inlet and / or outlet are provided. Such a trained heat exchanger allows a good distribution of the heat transfer medium on the relevant for the heat transfer surface of the individual discs, which form the heat exchanger. The uniform flow distribution reduces the boiling problem in such a way critical areas used heat overlays. The heat transfer medium channels are thereby formed, as well as the inflow or outflow regions of the medium to be cooled / heated, preferably by in particular aligned apertures in the individual disks.

Durch eine hinsichtlich der Wärmeübertragermedium-Kanäle achssymmetrische Ausgestaltung der Scheiben bezüglich ihrer Längsachse wird die Wärmeübertragermediumverteilung unterstützt. Sind die Scheiben ferner hinsichtlich der Wärmeübertragermedium-Kanäle achssymmetrisch bezüglich ihrer Querachse ausgebildet, so vereinfacht sich die Montage.The heat transfer medium distribution is assisted by an embodiment of the disks which is axisymmetric with respect to the heat transfer medium channels with respect to their longitudinal axis. If the disks are furthermore designed to be axially symmetrical with respect to their transverse axis with regard to the heat exchanger medium channels, the assembly is simplified.

Bevorzugt ist ein einziger Wärmeübertragermedium-Eintritt und/oder ein einziger Wärmeübertragermedium-Austritt vorgesehen, der eine Verzweigung bzw. Zusammenführung aufweist. Dies ermöglicht einen relativ einfachen Aufbau bei verbessertem Wärmeübergang auf Grund der besseren Strömungsverteilung.Preferably, a single heat transfer medium inlet and / or a single heat transfer medium outlet is provided, which has a branching or merging. This allows a relatively simple structure with improved heat transfer due to the better flow distribution.

Die Verzweigung und/oder die Zusammenführung sind vorzugsweise kreisbogenförmig ausgebildet, so dass ein raumsparender Aufbau um die die einzelnen Scheiben zusammenhaltenden Bolzen o.ä. möglich ist.The branching and / or the merging are preferably circular-arc-shaped, so that a space-saving construction or the like around the individual discs together holding bolts. is possible.

Im Bereich der Verzweigung und/oder der Zusammenführung ist - in Strömungsrichtung gesehen - bevorzugt einen Knick von 30° bis 90° vorgesehen, wobei der gegabelte Teil der Verzweigung bzw. Zusammenführung parallel zu den Scheiben ausgerichtet ist.In the area of the branching and / or the merging, a bend of 30 ° to 90 °, as seen in the flow direction, is preferably provided, wherein the forked part of the branching or merging is aligned parallel to the disks.

Der in zwei Wärmaübertragermedium-Kanäle nach der Verzweigung übergehende Wärmeübertragermedium-Eintritt verläuft bevorzugt parallel zu den Wärmeübertragermedium-Kanälen, während der zweiteilige Teil der Verzweigung bevorzugt in einer senkrecht hierzu liegenden Ebene angeordnet ist. Der aus zwei Wärmeübertragermedium-Kanälen in die Zusammenführung übergehende Wärmeübertragermedium-Austritt verläuft bevorzugt parallel zu den Wärmeübertragermedium-Kanälen, während der zweiteilige Teil der Verzweigung bevorzugt in einer senkrecht hierzu liegenden Ebene angeordnet ist. Dies ermöglicht einen kompakten und raumsparenden Aufbau des Wärmeübertragers. Alternativ kann die Zuführung auch mittels zweier einzelner, getrennt ausgebildeter Rohre erfolgen, die über ein Y-förmiges Verbindungsstück miteinander verbunden sind.The heat transfer medium inlet entering the two heat transfer medium channels after the branching preferably runs parallel to the heat transfer medium channels, while the two-part part of the branching preferably takes place in a plane lying perpendicular thereto is. The heat transfer medium outlet which merges into the merger from two heat transfer medium channels preferably runs parallel to the heat transfer medium channels, while the two-part part of the branch is preferably arranged in a plane lying perpendicular thereto. This allows a compact and space-saving design of the heat exchanger. Alternatively, the supply can also be effected by means of two individual, separately formed tubes, which are connected to one another via a Y-shaped connecting piece.

Bevorzugt wird ein Ladeluft-/Kühlmittel-Kühler zur Kühlung der Ladeluft. Hierbei wird vorzugsweise ein Gemisch mit Wasser und Glykol als Wärmeübertragermedium (Kühlmittel) verwendet.A charge air / coolant cooler for cooling the charge air is preferred. In this case, a mixture with water and glycol is preferably used as the heat transfer medium (coolant).

Im Folgenden wird die Erfindung anhand dreier Ausführungsbeispiele unter Bezugnahme auf die Zeichnung im Einzelnen erläutert. In der Zeichnung zeigen:

Fig. 1
eine schematisierte perspektivische Explosionsdarstellung eines Ladeluft-/Kühlmittel-Kühlers in Scheibenbauweise gemäß dem ersten Ausführungsbeispiel,
Fig. 2
eine perspektivische Darstellung des Ladeluft-/Kühlmittel-Kühlers von Fig. 1,
Fig. 3
einen Schnitt durch den Ladeluft-/Kühlmittel-Kühler von Fig. 1 entlang Linie III-III in Fig. 4,
Fig. 4
einen Schnitt durch den Ladeluft-/Kühlmittel-Kühler von Fig. 1 entlang Linie IV-IV in Fig. 3,
Fig. 5
einen vergrößerten Ausschnitt einer Kühlmittel-Scheibe,
Fig. 6
einen vergrößerten Ausschnitt einer nicht erfindungsgemäßen Kühlmittel-Scheibe, und
Fig. 7
einen vergrößerten Ausschnitt einer nicht erfindungsgemäßen Kühlmittel-Scheibe.
In the following the invention with reference to three embodiments with reference to the drawings will be explained in detail. In the drawing show:
Fig. 1
FIG. 2 is a schematic exploded perspective view of a disk-type charge air / coolant cooler according to the first embodiment; FIG.
Fig. 2
a perspective view of the charge air / coolant radiator of Fig. 1 .
Fig. 3
a section through the charge air / coolant radiator of Fig. 1 along line III-III in Fig. 4 .
Fig. 4
a section through the charge air / coolant radiator of Fig. 1 along line IV-IV in Fig. 3 .
Fig. 5
an enlarged section of a coolant disc,
Fig. 6
an enlarged section of a non-inventive coolant disc, and
Fig. 7
an enlarged section of a non-inventive coolant disc.

Ein als Wärmeübertrager zwischen Ladeluft und Kühlmittel dienender Ladeluft-/Kühlmittel-Kühler 1 weist eine Mehrzahl von aufeinandergestapelten Kühlmittel-Scheiben 2 auf. Hierbei sind in jeder Kühlmittel-Scheibe 2 je zwei Eintrittsöffnungen 3 und zwei Austrittsöffnungen 4 vorgesehen, durch die als Wärmeübertragermedium Kühlmittel den Zwischenräumen der Kühlmittel-Scheiben 2 zugeführt bzw. von ihm abgeführt wird. Die Strömungsrichtung ist in den Figuren durch Pfeile verdeutlicht. Dabei verbreitet sich das Kühlmittel nach dem Eintritt durch die Eintrittsöffnungen 3 über die gesamte Breite der Zwischenräume der Kühlmittel-Scheiben 2 und strömt gleichmäßig in Richtung der Austrittsöffnungen 4 (siehe Fig. 3), so dass die gesamte Länge und Breite der Zwischenräume zwischen den Ein- und Austrittsöffnungen 3 und 4 gleichmäßig durchströmt wird und ein optimaler Wärmeübergang von der zu kühlenden Ladeluft, die zwischen den einzelnen Kühlmittel-Scheiben 2 den Ladeluft-/Kühlmittel-Kühler 1 durchströmt, erfolgen kann.Serving as a heat exchanger between charge air and coolant charge air / coolant radiator 1 has a plurality of stacked coolant discs 2. In this case, two inlet openings 3 and two outlet openings 4 are provided in each coolant disc 2, is supplied by the heat transfer medium as coolant to the interstices of the coolant disks 2 and discharged from it. The flow direction is illustrated in the figures by arrows. In this case, the coolant spreads after entering through the inlet openings 3 over the entire width of the interstices of the coolant disks 2 and flows uniformly in the direction of the outlet openings 4 (see Fig. 3 ), so that the entire length and width of the spaces between the inlet and outlet openings 3 and 4 flows through uniformly and optimum heat transfer from the charge air to be cooled, which flows through the charge air / coolant radiator 1 between the individual coolant discs 2 , can be done.

Die Öffnungen 3 und 4 der aufeinandergestapelten Kühlmittel-Scheiben 2 bilden Kühlmittel-Kanäle 5 und 6. Hierfür sind die Bereiche der Öffnungen 3 und 4 entsprechend erhaben ausgebildet, so dass ausreichend Zwischenraum vorhanden ist, damit die Ladeluft zwischen den Kühlmittel-Scheiben 2 durchströmen und gekühlt werden kann.The openings 3 and 4 of the stacked coolant disks 2 form coolant channels 5 and 6. For this purpose, the areas of the openings 3 and 4 are formed correspondingly raised, so that there is sufficient space for the charge air to flow through between the coolant disks 2 and can be cooled.

Die beiden Kühlmittel-Kanäle 5 beginnen - in Strömungsrichtung des Kühlmittels gesehen - an einer Verzweigung 7, die eine kreisbogenförmige Gabelung 8 und einen zentral im Kreisbogen derselben angeordneten, parallel zu den Kühlmittel-Kanälen 5 angeordneten Kühlmittel-Eintritt 9 aufweist. So wird das durch den Kühlmittel-Eintritt 9 zugeführte Kühlmittel gleichmäßig auf die beiden Kühlmittel-Kanäle 5 aufgeteilt.The two coolant channels 5 begin - seen in the flow direction of the coolant - at a junction 7, which has a circular arc-shaped bifurcation 8 and a centrally arranged in the arc thereof, arranged parallel to the coolant channels 5 coolant inlet 9. Thus, the coolant supplied through the coolant inlet 9 is divided equally between the two coolant channels 5.

Entsprechend dem Eintritt ist der Austritt ausgebildet. So enden die beiden Kühlmittel-Kanäle 6 mit einer Zusammenführung 10, die entsprechend der Verzweigung 7 ausgebildet ist und einen Kühlmittel-Austritt 11 aufweist.According to the entry, the exit is formed. Thus, the two coolant channels 6 end with a combination 10, which is formed according to the branch 7 and has a coolant outlet 11.

Die Ladeluft (zweites Medium) wird über einen Ladeluft-Eintritt 20 zugeführt, wird über einen Ladeluft-Kanal 21, welcher durch Öffnungen 22 der aufeinandergestapelten Kühlmittel-Scheiben 2 gebildet wird, den Zwischenräumen zwischen den von dem Kühlmittel durchströmten Zwischenräumen der Kühlmittel-Scheiben 2 zugeführt und gelangt über auf der anderen Seite der Kühlmittel-Scheiben 2 ausgebildete Öffnungen 23, welche einen zweiten Ladeluft-Kanal 24 bilden, zum Ladeluft-Austritt 25.The charge air (second medium) is supplied via a charge air inlet 20, via a charge air channel 21, which is formed by openings 22 of the stacked coolant discs 2, the spaces between the flowed through by the coolant spaces of the coolant discs. 2 fed and passes through on the other side of the coolant disks 2 formed openings 23, which form a second charge air channel 24 to the charge air outlet 25th

Die Öffnungen 22 und 23 sind, entgegen dem Stand der Technik (in Fig. 5 gestrichelt dargestellt) nicht kreisförmig, sondern weisen einen Bereich 26 auf, der gemäß dem ersten Ausführungsbeispiel im Wesentlichen gerade verläuft, wobei er senkrecht zur normalen Strömungsrichtung der Ladeluft angeordnet ist, so dass er in diesem Bereich 26 tangential bezüglich der herkömmlichen Form, welche dem Innenkreis der Öffnungen 22 und 23 entspricht, angeordnet ist.The openings 22 and 23 are, contrary to the prior art (in Fig. 5 shown in dashed lines) are not circular, but have a portion 26 which is substantially straight according to the first embodiment, wherein it is arranged perpendicular to the normal flow direction of the charge air, so that in this region 26 tangentially with respect conventional shape, which corresponds to the inner circle of the openings 22 and 23, is arranged.

Die Öffnungen 22 und 23 nehmen jeweils den gesamten Endbereich der Kühlmittel-Scheibe 2 ein, abgesehen von einem äußeren Rand 27, den beiden Kühlmittel-Kanälen 5 und 6 und je einem die Kühlmittel-Kanäle umgebenden Rand 28 einnimmt.The openings 22 and 23 each occupy the entire end portion of the coolant disk 2, except for an outer edge 27, the two coolant channels 5 and 6 and each one surrounding the coolant channels edge 28 occupies.

Gemäß der in Fig.6 dargestellten nicht erfindungsgemäßen Kühlmittel-Scheibe ist der Bereich 26 der Öffnung 23 derart ausgebildet, dass er sich über den gesamten Endbereich der Kühlmittel-Scheiben 2 erstreckt, wobei er senkrecht zur mittleren Strömungsrichtung der Ladeluft angeordnet ist. Hierbei sind die Kühlmittel-Kanäle weiter nach innen versetzt angeordnet, so dass sich die Form eines abgerundeten Dreiecks ergibt. Die andere Seite der Kühlmittel-Scheibe 2 ist entsprechend ausgebildet.According to the in Figure 6 illustrated non-inventive coolant disc, the region 26 of the opening 23 is formed such that it extends over the entire end portion of the coolant discs 2, wherein it is arranged perpendicular to the mean flow direction of the charge air. Here, the coolant channels are arranged further offset inwards, so that the shape of a rounded triangle results. The other side of the coolant disc 2 is formed accordingly.

Gemäß der in Fig. 7 dargestellten nicht erfindungsgemäßen Kühlmittel-Scheibe entspricht die Öffnung 23 etwa der Öffnung 23 des zweiten Ausführungsbeispiels, wobei nur ein Kühlmittel-Kanal vorgesehen ist, der seitlich in den Bereich der Öffnung 23 verschoben ist, so dass die Öffnung 23 den Endbereich der Kühlmittel-Scheibe 2 abgesehen von einem äußeren Rand 27, dem Kühlmittel-Kanal und einem den Kühlmittel-Kanal umgebenden Rand 28 einnimmt. Die andere Seite der Kühlmittel-Scheibe 2 ist entsprechend ausgebildet, insbesondere achssymmetrisch zur Mittel-Querachse oder punktsymmetrisch zum Mittelpunkt der Kühlmittel-Scheibe.According to the in Fig. 7 illustrated coolant disc corresponds to the opening 23 about the opening 23 of the second embodiment, wherein only a coolant channel is provided, which is laterally displaced in the region of the opening 23, so that the opening 23, the end portion of the coolant disc. 2 apart from an outer edge 27, the coolant channel and a coolant channel surrounding edge 28 occupies. The other side of the coolant disc 2 is designed accordingly, in particular axially symmetrical to the central transverse axis or point-symmetrical to the center of the coolant disc.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Ladeluft-/Kühlmittel-KühlerCharge-air / coolant cooler
22
Kühlmittel-ScheibeCoolant disc
33
Eintrittsöffnunginlet opening
44
Austrittsöffnungoutlet opening
55
Kühlmittel-KanalCoolant channel
66
Kühlmittel-KanalCoolant channel
77
Verzweigungbranch
88th
Gabelungcrotch
99
Kühlmittel-EintrittCoolant inlet
1010
Zusammenführungtogether
1111
Kühlmittel-AustrittCoolant outlet
2020
Ladeluft-EintrittCharge air inlet
2121
Ladeluft-KanalCharge air channel
2222
Öffnungopening
2323
Öffnungopening
2424
zweiter Ladeluft-Kanalsecond charge air duct
2525
Ladeluft-AustrittCharge air outlet
2626
BereichArea
2727
äußerer Randouter edge
2828
Randedge

Claims (11)

  1. A charge-air/coolant radiator (1), of disk-type construction, wherein two adjacent disks (2) define an intermediate space through which a heat exchanger medium or charge air flows, wherein the disks (2) have openings (22, 23) which form passages (21, 24) for charge air and have an entry and an exit region (26), wherein the openings (22, 23) are extended compared to a circle form and the entry and exit regions (26) run rectilinearly at least over a third, in particular over half, of the width of the disk and on the entry side and on the exit side of the heat exchanger medium, respectively two openings (3, 4) for the entry and exit are provided, so that coolant passages (5, 6) are formed which are respectively spaced apart from one another, wherein the openings (22, 23) respectively occupy the complete end region of the disks (2), apart from an outer edge (27), the two coolant passages (5, 6) and an edge (28) respectively surrounding the coolant passages, characterised in that the openings (22, 23) are arranged such that a first distance between the centres of the openings (22, 23) is greater than a shortest second distance between the centre of an inlet opening (3) for the heat exchanger medium and the centre of an outlet opening (4) for the heat exchanger medium and wherein the entry and exit regions (26) protrude between the respective two openings (3, 4) for the entry and exit of the heat exchanger medium.
  2. The charge-air/coolant radiator as claimed in claim 1, characterised in that the region (26) runs at least over part of the width of the disk perpendicularly or essentially transversely to the average flow direction of the second medium.
  3. The charge-air/coolant radiator as claimed in one of the preceding claims, characterised in that the opening (23, 24) for the second medium in an end region of the disk (2) extends essentially over the entire surface of the same, except for edge regions (27, 28) and regions in which passages (5, 6) are arranged.
  4. The charge-air/coolant radiator as claimed in one of the preceding claims, characterised in that a common heat exchanger medium inlet (9) and heat exchanger medium outlet (11) are provided for the disks (2), wherein at least two heat exchanger medium passages (5, 6) are provided per heat exchanger medium inlet and/or outlet (9 and 11).
  5. The charge-air/coolant radiator as claimed in one of the preceding claims, characterised in that the disks (2) are of axially symmetrical design with respect to their longitudinal axis with regard to the heat exchanger medium passages (5, 6).
  6. The charge-air/coolant radiator as claimed in one of the preceding claims, characterised in that the disks (2) are of axially symmetrical design with respect to their transverse axis with regard to the heat exchanger medium passages (5, 6).
  7. The charge-air/coolant radiator as claimed in one of the preceding claims, characterised in that a heat exchanger medium inlet (9) and/or a heat exchanger medium outlet (11) has a branching (7) and/or junction (10).
  8. The charge-air/coolant radiator as claimed in claim 7, characterised in that the branching and/or junction (7 and 10) is designed in the shape of an arc of a circle.
  9. The charge-air/coolant radiator as claimed in one of claims 7 or 8, characterised in that a bend of 30° to 90° is provided, as seen in the direction of flow, in the region of the branching (7) and/or of the junction (10).
  10. The charge-air/coolant radiator as claimed in one of claims 7 to 9, characterised in that the heat exchanger medium inlet (9), which merges into two heat exchanger medium passages (5) after the branching (7), runs parallel to the heat exchanger medium passages (5) while the two-part part of the branching (7) is arranged in a plane lying perpendicularly thereto.
  11. The charge-air/coolant radiator as claimed in one of claims 7 to 10, characterised in that the heat exchanger medium outlet (11), which merges from two heat exchanger medium passages (6) into the junction (10), runs parallel to the heat exchanger medium passages (6) while the two-part part of the branching (7) is arranged in a plane lying perpendicularly thereto.
EP04818135.8A 2003-11-10 2004-11-10 Charge-air/coolant radiator Not-in-force EP1687580B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10352881A DE10352881A1 (en) 2003-11-10 2003-11-10 Heat exchanger, in particular charge air / coolant radiator
PCT/EP2004/012719 WO2005045344A1 (en) 2003-11-10 2004-11-10 Heat exchanger, especially charge-air/coolant radiator

Publications (2)

Publication Number Publication Date
EP1687580A1 EP1687580A1 (en) 2006-08-09
EP1687580B1 true EP1687580B1 (en) 2017-08-02

Family

ID=34559606

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04818135.8A Not-in-force EP1687580B1 (en) 2003-11-10 2004-11-10 Charge-air/coolant radiator

Country Status (7)

Country Link
US (1) US7717165B2 (en)
EP (1) EP1687580B1 (en)
JP (1) JP4653756B2 (en)
CN (1) CN1875235B (en)
BR (1) BRPI0416363B1 (en)
DE (1) DE10352881A1 (en)
WO (1) WO2005045344A1 (en)

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Also Published As

Publication number Publication date
DE10352881A1 (en) 2005-06-09
US7717165B2 (en) 2010-05-18
JP4653756B2 (en) 2011-03-16
US20070084592A1 (en) 2007-04-19
BRPI0416363A (en) 2007-03-13
EP1687580A1 (en) 2006-08-09
WO2005045344A1 (en) 2005-05-19
CN1875235A (en) 2006-12-06
BRPI0416363B1 (en) 2018-10-30
JP2007510883A (en) 2007-04-26
CN1875235B (en) 2010-10-13

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