EP1331464A2 - Echangeur de chaleur - Google Patents

Echangeur de chaleur Download PDF

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Publication number
EP1331464A2
EP1331464A2 EP03000982A EP03000982A EP1331464A2 EP 1331464 A2 EP1331464 A2 EP 1331464A2 EP 03000982 A EP03000982 A EP 03000982A EP 03000982 A EP03000982 A EP 03000982A EP 1331464 A2 EP1331464 A2 EP 1331464A2
Authority
EP
European Patent Office
Prior art keywords
gill
rib
longitudinal direction
longitudinal
heat exchanger
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.)
Granted
Application number
EP03000982A
Other languages
German (de)
English (en)
Other versions
EP1331464B1 (fr
EP1331464A3 (fr
Inventor
Roland Burk
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mahle Behr GmbH and Co KG
Original Assignee
Behr GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Behr GmbH and Co KG filed Critical Behr GmbH and Co KG
Publication of EP1331464A2 publication Critical patent/EP1331464A2/fr
Publication of EP1331464A3 publication Critical patent/EP1331464A3/fr
Application granted granted Critical
Publication of EP1331464B1 publication Critical patent/EP1331464B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • 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
    • F28F1/126Tubular 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 consisting of zig-zag shaped fins
    • F28F1/128Fins with openings, e.g. louvered fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/053Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
    • F28D1/0535Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
    • F28D1/05366Assemblies of conduits connected to common headers, e.g. core type radiators

Definitions

  • the invention relates to a heat exchanger, in particular for a motor vehicle, for heat transfer between a liquid and a gas, with the features of the preamble of claim 1.
  • Such a heat exchanger is known for example from DE-OS 14 51 216 known and has a plurality of tubes which are parallel to each other and spaced are arranged from each other.
  • the tubes are inside in the tube longitudinal direction permeable by the liquid and outside transversely to the tube longitudinal direction flowed around by the gas.
  • Between the tubes are in the gas flow path each arranged a plurality of ribs, the heat-transmitting connected to the pipes.
  • These ribs extend with their Longitudinal direction transverse to the tube longitudinal direction and serve as Spacer for the pipes.
  • all between two adjacent ribs arranged ribs combined into a ribbed band.
  • Each rib has several gills, one behind the other in the rib longitudinal direction and are arranged parallel to each other. These gills extend with its longitudinal direction approximately transversely to the tube longitudinal direction and across the Fin longitudinal direction. Furthermore, the gills are transverse to the gill longitudinal direction inclined relative to the rib longitudinal direction and can thereby at a gas admission of the heat exchanger, the gas flow of one rib side to the other rib side lead. These gills initially cause a constant rebuilding of thermal boundary layers, which are relatively thin on average due to the short start-up lengths and thereby a relatively good heat transfer between the gas and the Allow gills.
  • the gills of each rib are in one first rib longitudinal section inclined in the same direction to each other, while the Gills in a second rib longitudinal section in the same direction to each other and are inclined in opposite directions to the gills of the first rib longitudinal section. Furthermore, all are arranged side by side in the tube longitudinal direction Ribs arranged side by side in the tube longitudinal direction Gills inclined in the same direction. This construction results for the gas with the flow through the heat exchanger, a double deflection transverse to the tube longitudinal direction.
  • the tubes are each provided with a container for Collecting and / or distributing and / or diverting the liquid connected.
  • the deflection of the gas flow through the Gill inclination impeded.
  • the heat transfer performance of Ribs starting from a soldered to the respective tube foot up towards the middle of the rib, resulting in a corresponding on the gas side Temperature gradient forms.
  • the middle portion of the gas flow increases in heat transfer in only a small part.
  • To improve the rib efficiency is it possible to measure the distances between adjacent pipes and thus reducing the gill length or increasing the rib thickness. However, these measures increase the weight and the costs as well as the gas-side flow resistance of the heat exchanger.
  • the present invention deals with the problem, for a Heat exchanger of the type mentioned an improved embodiment specify, in particular, a relatively high heat transfer performance achieved at a relatively small pressure loss.
  • the invention is based on the general idea of designing the gills in such a way that that the inclination of the gill transverse direction relative to the Rib longitudinal direction along the longitudinal gill direction in adjacent Gill longitudinal sections reversed.
  • the gills thereby show respect their longitudinal direction a propeller-like distortion. That means each one Gill in the one gill longitudinal section the gas flow from the first Rib side leads to the second rib side and in the other gill longitudinal section from the second rib side to the first rib side. at a corresponding arrangement and distribution of these gill longitudinal sections may be the cross-flow components of the gas flow be enlarged, thereby increasing the heat transfer between gas and Gill or rib increased.
  • all gills a rib be arranged so that the one another in the rib longitudinal direction following gill longitudinal sections are inclined in the same direction.
  • the trained thereby Rib groups thus have alternating tilt directions or twisting directions in their gills, which is a low pressure loss System generate counter-rotating vortices.
  • This vortex system leads on the one hand to a gas exchange in the tube longitudinal direction and on the other hand in Fin longitudinal direction. This results in an improved turbulence the gas flow in the middle of the ribs. Overall, can thereby increasing the heat transfer between gas flow and ribs become.
  • the number of ribs in the rib groups be chosen so that the rib groups in the tube longitudinal direction extend as far as adjacent tubes transversely to the tube longitudinal direction spaced apart from each other. Due to this design can at the Flow through the heat exchanger essentially cylindrical vortex generated at relatively low pressure losses a particularly ensure favorable heat transfer.
  • a heat exchanger 1 a plurality of tubes 2, the parallel to each other and spaced from each other are.
  • the tubes 2 lie in a plane that in Fig. 1 of the drawing plane equivalent.
  • the tubes 2 are shown at their in Fig. 1 below Longitudinal ends each with a lower container 3 and at their in Fig. 1 above shown upper longitudinal end with an upper container. 4 connected.
  • the tubes 2 are in their interior in their by a double arrow symbolized pipe longitudinal direction 5 can be traversed by a liquid.
  • the containers 3 and 4 serve for collecting and / or distributing and / or Redirecting the fluid flow.
  • the heat exchanger 1 around the heat exchanger 1 of a motor vehicle.
  • the heat exchanger 1 is a so-called “Flat tube heat exchanger", in which the tubes 2 as flat tubes are trained; that is, the tubes 2 are transverse to their longitudinal direction 5 are significantly larger in the rib longitudinal direction 8 than in the rib transverse direction 9.
  • the flat tubes can also be soldered against each other Slices are built, it being on the inner structure of the slices or pipes 2 does not arrive here.
  • the tubes 2 are spaced from each other, they are transverse to the outside Tube longitudinal direction 5 and substantially perpendicular to the heat exchanger plane, ie perpendicular to the plane of the drawing, from a gas, e.g. Air, flow around.
  • a gas e.g. Air
  • Rib bands 6 are arranged, which are zigzag-shaped wavy or folded, wherein the individual folds or corrugations form ribs 7, each with the tubes 2 are heat transfer connected.
  • the Ribs 7 and the rib bands 6 with the tubes 2 soldered.
  • the ribs 7 extend with their in Fig. 3 by a double arrow symbolized longitudinal direction 8 transversely to the tube longitudinal direction 5.
  • the rib longitudinal direction 8 thus runs substantially parallel to the flow of the the heat exchanger 1 acting gas.
  • the ribs 7 and the Rib bands 6 can simultaneously as spacers for the tubes. 2 serve.
  • Figs. 2 and 4 the detail II of Fig. 1 is shown enlarged, wherein the views in Figs. 2 and 4 by 90 ° with respect to the illustration according to Fig. 1 are rotated.
  • Figs. 2 and 4 the structure of a special Ribbed band 6 shown in more detail.
  • the Folding or corrugation of the ribbed belt 6 designed so that ribs 7, the are arranged adjacent to each other in the tube longitudinal direction 5, so are positioned so that they transversely to the rib longitudinal direction.
  • 8 extending, symbolized in Fig. 2 by a double arrow rib transverse direction 9 parallel to each other.
  • are the rib bands 6 as in Fig. 1 zig-zag-shaped corrugated or folded, so that the ribs 7 inclined relative to the rib transverse direction 9 are and are only substantially parallel to each other:
  • the ribs 7 each have a plurality of gills 10, which are arranged one behind the other in the rib longitudinal direction 8.
  • a Longitudinal direction 11 of the gills 10 extends transversely to the rib longitudinal direction eighth and thus coincides with the rib transverse direction 9.
  • At each rib 7 are the gills 10 with respect to their gill longitudinal direction 11 parallel to each other arranged. Due to the parallel or substantially parallel alignment the ribs 7 are the gills 10 also adjacent Ribs 7 corresponding to FIG. 2 also with respect to their gill longitudinal direction 11 arranged parallel or substantially parallel to each other.
  • each gill 10 has a plurality of gill longitudinal sections 12 and 13.
  • FIGS. 2 to 5 are two different embodiments by way of example shown in terms of the number of gill longitudinal sections 12, 13 each gill 10 differ from each other.
  • each gill 10 has two gill longitudinal sections 12, 13, while in the embodiment according to FIGS. 4 and 5 each gill 10 has three gill longitudinal sections 12, 13.
  • the a gill longitudinal sections 12 are shown in Fig. 2 above and in Fig. 3rd drawn with solid lines.
  • the other gill longitudinal sections 13 shown in Fig. 2 below and in Fig. 3rd drawn with broken lines. 2
  • the two KiemenlCode 12 and 13 formed substantially the same size, resulting in a total symmetrical deflection effect leaves.
  • the gill longitudinal sections 12 and 13 of the gills 10 are with respect to the Kiemenlteilscardi 11 in opposite directions against each other wound, resulting in a propeller-like twist.
  • the gill longitudinal sections at each gill 10 12 symbolized in a in Fig. 3 by corresponding double arrows, transverse to the gill longitudinal direction 11 extending gill transverse direction 14 opposite the rib longitudinal direction 8 inclined.
  • the other gill longitudinal sections 13 with their gill transverse direction 14 is shown by dotted double arrows, also inclined to Rib longitudinal direction 8, however, is the inclination of the other gill longitudinal sections 13 opposite to the inclination of a gill longitudinal sections 12 oriented.
  • each gill 10 is arranged at each rib 7, that in the rib longitudinal direction 8 consecutive Kiemenl Kunststoffsabête 12 and 13 are inclined in the same direction.
  • all the lower ones see FIG (See Fig. 4) Gill longitudinal sections 13 inclined in the same way relative to the rib longitudinal direction 8.
  • each form one in the embodiments shown here certain number of ribs 7, in the tube longitudinal direction 5 side by side are arranged, in each case a rib group 15 or 15 ', in the 3 and 5 are marked by braces.
  • a group of ribs 15 all gills 10th are arranged so that all upper or outer gill longitudinal sections 12 are arranged in the same direction and that all lower or middle Gill longitudinal sections 13 are oriented in the same direction to each other.
  • the means that in the tube longitudinal direction 5, the successive gill longitudinal sections 12 and 13 are inclined in the same direction.
  • the gill longitudinal sections 12,13 of a rib group 15 in opposite directions to the gill longitudinal sections 12, 13 of the other rib group 15 ' are inclined.
  • the gill longitudinal sections 12,13 results for the Gas flow in the flow through the heat exchanger 1 within the Ridges 7 a vortex formation whose helical shape in particular from the Fig. 2 and 4 shows and which are designated in Figs. 2 to 5 with 16.
  • These vortices 16 on the one hand cause a gas exchange in the tube longitudinal direction 5 and on the other hand in the longitudinal direction of the gill 11.
  • This Gas exchange can be the temperature gradient between near-pipe areas the ribs 7 and the tube-distal middle portions of the ribs 7 reduced become. Overall, this improves the heat transfer between gas flow and gills 10 or ribs 7 and thus between Gas flow and tubes 5 and the liquid flow guided therein.
  • each fin group has 15, 15 ' three ribs 7 with the same direction gills 10 and first gill longitudinal sections 12 and second gill longitudinal sections 13.
  • the gills 10 form in the ribs 7 openings, the gills 10th because of their employment or inclination at a gas supply of the Heat exchanger 1, the gas flow from the one rib side to lead to other rib side.
  • the opposing flow deflection at the first gill longitudinal sections 12 and the second gill longitudinal sections 13 as well as due to the chosen arrangement and orientation the gill longitudinal sections 12,13 at adjacent ribs 7 may be form the desired vortex 16.
  • Vortex system By the proposed embodiment of the gills 10 and by the Targeted orientation of the gill longitudinal sections 12 and 13 arise propeller-like twisting over several ribs 7 away interact and there a self-contained vortex system (vortex system) stimulate.
  • This vortex system 16 leads to an intensive gas exchange between tube-near and tube-distant air layers, whereby all Air layers along the gas flow path in the region near the tube with high temperature difference, so that the heat transfer improves is.
  • the ribs 7 in the gill longitudinal direction 11 build relatively large, i. the tubes 2 can be relatively large Have distances from each other. This results in a special cost-effective design for the heat exchanger 1.
  • the training of Whirl 16 only results in a comparatively low pressure loss.
  • the gills 10 with respect to a median plane which extends in the tube longitudinal direction 5 and in the rib longitudinal direction 8 extends between the tubes 2, formed mirror-symmetrically.
  • This symmetry can have manufacturing advantages, in particular with respect to a distortion during continuous rolling of a Ribbed tape 6.

Landscapes

  • 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)
  • Power Steering Mechanism (AREA)
  • Compression-Type Refrigeration Machines With Reversible Cycles (AREA)
  • Separation By Low-Temperature Treatments (AREA)
EP03000982A 2002-01-25 2003-01-17 Echangeur de chaleur Expired - Lifetime EP1331464B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10202768A DE10202768A1 (de) 2002-01-25 2002-01-25 Wärmeübertrager
DE10202768 2002-01-25

Publications (3)

Publication Number Publication Date
EP1331464A2 true EP1331464A2 (fr) 2003-07-30
EP1331464A3 EP1331464A3 (fr) 2003-08-06
EP1331464B1 EP1331464B1 (fr) 2006-05-24

Family

ID=7713005

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03000982A Expired - Lifetime EP1331464B1 (fr) 2002-01-25 2003-01-17 Echangeur de chaleur

Country Status (4)

Country Link
EP (1) EP1331464B1 (fr)
AT (1) ATE327492T1 (fr)
DE (2) DE10202768A1 (fr)
ES (1) ES2263854T3 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10336625A1 (de) * 2003-08-05 2005-03-10 Behr Gmbh & Co Kg Vorrichtung zum Austausch von Wärme und Verfahren zu deren Herstellung
DE102015226577A1 (de) 2015-12-22 2017-06-22 Mahle International Gmbh Blechteil mit einer Kiemen aufweisenden Rippenstruktur eines Wärmeübertragers sowie Herstellungsverfahren
WO2018015051A1 (fr) 2016-07-19 2018-01-25 Mahle International Gmbh Ailette ondulée d'un échangeur de chaleur et échangeur de chaleur

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004013682A1 (de) 2003-03-26 2004-12-16 Behr Industrietechnik Gmbh & Co. Kg Wärmeübertrager, insbesondere Luft/Luft-Kühler
DE202008016603U1 (de) * 2008-12-15 2010-04-29 Autokühler GmbH & Co. KG Wellrippe für Wärmeaustauscher

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1451216A1 (de) 1963-02-19 1969-05-08 Ford Werke Ag Waermeaustauscher,insbesondere Kuehler fuer Kraftfahrzeug-Verbrennungsmotore,mit zwischen Kuehlmittelleitungen desselben angeordneten,als Abstandshalter dienenden Leitblechen zur Fuehrung eines Kuehlluftstromes und Vorrichtung zur Herstellung der Leitbleche

Family Cites Families (13)

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Publication number Priority date Publication date Assignee Title
FR1526316A (fr) * 1967-04-14 1968-05-24 Chausson Usines Sa Perfectionnements aux dissipateurs secondaires pour radiateurs et aérothermes
US3993125A (en) * 1975-11-28 1976-11-23 Ford Motor Company Heat exchange device
DE3050963C3 (de) * 1980-04-30 1995-11-09 Nippon Denso Co Wärmetauscher
GB2169694B (en) * 1985-01-15 1988-01-20 Sanden Corp Serpentine heat exchanger
US4815532A (en) * 1986-02-28 1989-03-28 Showa Aluminum Kabushiki Kaisha Stack type heat exchanger
EP0275813B1 (fr) * 1986-12-29 1991-02-27 United Technologies Corporation Dispositif pour l'accroissement du transfert de chaleur
JP2786702B2 (ja) * 1989-12-07 1998-08-13 昭和アルミニウム株式会社 複式一体型熱交換器
DE9404009U1 (de) * 1994-03-10 1995-07-13 Behr Gmbh & Co, 70469 Stuttgart Wärmetauscher
DE19531383A1 (de) * 1995-08-26 1997-02-27 Martin Dipl Ing Behle Wärmeübertrager
US5992514A (en) * 1995-11-13 1999-11-30 Denso Corporation Heat exchanger having several exchanging portions
US5730214A (en) * 1997-01-16 1998-03-24 General Motors Corporation Heat exchanger cooling fin with varying louver angle
DE19719262C2 (de) * 1997-05-07 2003-01-30 Valeo Klimatech Gmbh & Co Kg Zickzacklamelle als Verrippung von Flachrohrwärmetauschern bei Kraftfahrzeugen
US6170566B1 (en) * 1999-12-22 2001-01-09 Visteon Global Technologies, Inc. High performance louvered fin for a heat exchanger

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1451216A1 (de) 1963-02-19 1969-05-08 Ford Werke Ag Waermeaustauscher,insbesondere Kuehler fuer Kraftfahrzeug-Verbrennungsmotore,mit zwischen Kuehlmittelleitungen desselben angeordneten,als Abstandshalter dienenden Leitblechen zur Fuehrung eines Kuehlluftstromes und Vorrichtung zur Herstellung der Leitbleche

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10336625A1 (de) * 2003-08-05 2005-03-10 Behr Gmbh & Co Kg Vorrichtung zum Austausch von Wärme und Verfahren zu deren Herstellung
DE102015226577A1 (de) 2015-12-22 2017-06-22 Mahle International Gmbh Blechteil mit einer Kiemen aufweisenden Rippenstruktur eines Wärmeübertragers sowie Herstellungsverfahren
EP3184949A2 (fr) 2015-12-22 2017-06-28 Mahle International GmbH Élément de tôle comprenant une structure nervurée présentant une grille d'un caloporteur et procédé de fabrication
WO2018015051A1 (fr) 2016-07-19 2018-01-25 Mahle International Gmbh Ailette ondulée d'un échangeur de chaleur et échangeur de chaleur
DE102016213197A1 (de) 2016-07-19 2018-01-25 Mahle International Gmbh Wellrippe eines Wärmeübertragers und Wärmeübertrager

Also Published As

Publication number Publication date
DE50303414D1 (de) 2006-06-29
ES2263854T3 (es) 2006-12-16
EP1331464B1 (fr) 2006-05-24
ATE327492T1 (de) 2006-06-15
DE10202768A1 (de) 2003-07-31
EP1331464A3 (fr) 2003-08-06

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