EP1055897A1 - Heat exchanger with improved fin-positioning - Google Patents

Heat exchanger with improved fin-positioning Download PDF

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Publication number
EP1055897A1
EP1055897A1 EP00401350A EP00401350A EP1055897A1 EP 1055897 A1 EP1055897 A1 EP 1055897A1 EP 00401350 A EP00401350 A EP 00401350A EP 00401350 A EP00401350 A EP 00401350A EP 1055897 A1 EP1055897 A1 EP 1055897A1
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EP
European Patent Office
Prior art keywords
fins
fin
heat exchanger
exchanger according
tubes
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP00401350A
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German (de)
French (fr)
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EP1055897B1 (en
Inventor
Philippe Lemercier
Guy Lenormand
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.)
Valeo Thermique Moteur SA
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Valeo Thermique Moteur SA
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Publication of EP1055897A1 publication Critical patent/EP1055897A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/24Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
    • F28F1/32Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2240/00Spacing means

Definitions

  • the invention relates to a heat exchanger, in particular for motor vehicle. It relates more particularly to a heat exchanger intended to cooperate with an air flow which crosses it, so as to modify the temperature of this flow.
  • such a heat exchanger comprises a series heat conducting fins, in order to increase its cooperation with the aforementioned air flow.
  • Such fins have a generally planar general shape, and are substantially parallel and spaced apart. Otherwise, they are each provided with openings for the passage of tubes intended to convey a clean fluid to exchange the heat with the air flow.
  • the fins are successively stacked the on top of each other.
  • a sliding of one of the fins relative to the others can happen.
  • the openings of this fin are then, at less partly, obscured by the other fins, which makes the subsequent step of inserting the tubes delicate in the openings.
  • the present invention improves the situation.
  • each fin has at least one protrusion projecting from a first side, and at least one recess on a second side opposite to the first face, so that the protuberance of a fin is able to cooperate by nesting with the recess a consecutive fin, which allows positioning substantially the fins relative to each other of so that the openings for the passage of the tubes substantially coincide between two consecutive fins.
  • the fins are made of a material substantially deformable metal and each have at minus a pin forming both the protuberance and the recess cited above.
  • these pins are of substantially shaped conical, with the top of the cone turned towards a fin consecutive.
  • these pins have substantially a shape of punctured dome with three sides, each forming a substantially angle less than 90 ° with the aforementioned first side of a fin.
  • each fin comprises at least two recesses and at least two protuberances suitable for engaging in the recesses of a consecutive fin, in view substantially immobilize the fins, relative to each other to others.
  • each fin further comprises a plurality spacing stops, intended to rest on one of the first and second faces of a consecutive fin, in view to keep the fins substantially spaced apart by compared to others, and the spacing stops are high substantially less than a height of the protrusions of positioning.
  • the aforementioned tubes are substantially in contact with the openings of the fins, in order to mechanically stiffen the assembly formed by the fins and the tubes.
  • FIG. 1 we first refer to Figure 1 to describe a heat exchanger according to the invention, intended to cool a fluid thanks to an air flow (arrow F) which crosses it.
  • this heat exchanger is part the cooling module of a motor vehicle engine, as a cooling radiator.
  • the exchanger comprises flat tubes 1 arranged in bundles and intended to convey a heat exchange fluid (liquid cooling) of one of the manifolds 4a that includes the heat exchanger, at the other 4b.
  • the extremities tubes are housed, preferably sealed, in openings in the collector plates 3a and 3b, integral with the manifolds 4a and 4b. Tubes 1 which coolant cooperate by exchange thermal with the air flow F, in order to cool said cooling liquid.
  • the heat exchanger has then fins 2, of generally substantially planar shape and substantially parallel to each other. These fins 2 are made of a heat conductive material (comprising aluminum) to increase the surface heat exchange with the air flow F which enters the exchanger, which increases, in general, the cooperation between flow F and the exchanger.
  • the conductive fins include spacing means so as to create gaps between the fins, which allows to leave penetrate the air flow F into the exchanger and avoid heat accumulation points.
  • the fins 2 are substantially perpendicular to the main axes of the tubes 1, and then comprise openings 21 for the passage of the tubes 1.
  • the fins 2 are stacked on top of each other.
  • the tubes 1, preferably produced in a deformable material are introduced into the openings 21 stacked fins 2, with a chosen mechanical play.
  • a stage of expansion of the tubes 1 is then provided, which mechanically stiffens the fins relative to to the tubes, creating in particular a mechanical contact substantially annular between the outer walls of the tubes and the openings 21 of the fins.
  • these fins remain substantially aligned, so that their openings 21 coincide from one fin to the other, which makes it possible to introduce easily the tubes 1 in the openings 21 of the fins consecutive.
  • the openings 21 of these fins must coincide, moreover, with the openings provided in the header plates 3a and 3b.
  • the fins of the heat exchanger comprise means for positioning the consecutive fins, so that the fins stacked successively remain substantially aligned with each other, which allows their openings to substantially coincide respective 21.
  • Fin 2a has openings, substantially in the form of louvers 221 and 222, so as to allow lateral penetration of a part of the air flow F, in order to increase cooperation of the air flow F with the exchanger.
  • Each fin further comprises spacing means 23 with a fin consecutive. These spacing means are formed, in the example described, of stops 23 provided with two walls 231 and 232, forming an angle close to 90 ° with a main surface S of the fin (first side mentioned above).
  • fins 2 are made of a metallic material deformable, for example aluminum and walls 231 and 232 spacing are obtained by punching on one side of the fins opposite side S (second side mentioned above).
  • the height of walls 231 and 232 defines a general pitch p between consecutive fins (aforementioned interstices).
  • the openings 21 of the fins are substantially oblong, particularly suitable for tubes 1, flat in the example described.
  • the walls of the openings 21 are intended to be substantially in contact with the tubes.
  • the openings 21 of a fin 2b substantially coincide with the openings 21 of a consecutive wing 2a.
  • This coincidence of openings is ensured by means of positioning which comprise the fins of the heat exchanger according to the invention.
  • These positioning means are produced in the form of a substantially conical pin, in particular frustoconical, performed, for example, by punching a bottom face fin 2a.
  • the protuberance formed by punching has a general shape of a punctured dome three sides 241, 242 and 243, these sides forming an angle less than 90 ° with the main surface S of the fin.
  • the spacing walls 231 and 232 are substantially curved laterally at their ends and thus have a shape general of collar. Furthermore, the height h of the spike positioning 24 is greater than the height p of the stop of spacing 23. Thus, the sides 241, 242 and 243 of a fin 2b fit into the recess that forms the punching of positioning of a consecutive fin 2a, while the spacing walls 231 and 232 come into contact with the main surface of the consecutive fin 2a.
  • each fin has two pins positioning 24a and 24b ( Figure 3), which allows substantially immobilize the fins, relative to each other to others.
  • the fins can be substantially immobilized in relation to each other in progress stacking, which facilitates the introduction of the tubes into the openings 21.
  • the two positioning pins 24a and 24b also allow to index the fins, in relation to each other, in the case (not shown) where these do not present any double axial symmetry.
  • positioning means 24 described above can form both means of positioning and spacing means between the fins.
  • These positioning means are produced by punching the fins.
  • these may include a protuberance formed on one side, as well as a recess formed on the other side. If it is particularly desired to train a heat exchanger with tubes inclined at an angle different from 90 ° to the fins, it can be envisaged to shift, in the plane of a fin, the recess of the protuberance it entails.
  • positioning protrusions produced by punching and having three sides (or lips) 241, 242 and 243 is described above by way of example. So general, positioning punches may be provided substantially frustoconical, or even conical, with the top of the cone turned towards a consecutive fin.
  • the invention advantageously applies to an exchanger heat produced by mechanical assembly of flat tubes and substantially planar shaped fins, substantially perpendicular to the tubes.

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

Abstract

The heat exchanger has a series of flat parallel fins (2a, 2b) with holes (21) for tubes and spacers (231, 232) to provide t required interval between adjacent fins. The spacers are in the form of projections made by punching holes through the fins, whi are of a suitable heat conducting material, e.g. aluminium. The fins also have louvred slits (221, 222) for enhanced interaction with the air flow.

Description

L'invention concerne un échangeur de chaleur, notamment pour véhicule automobile. Elle concerne plus particulièrement un échangeur de chaleur destiné à coopérer avec un flux d'air qui le traverse, de manière à modifier la température de ce flux.The invention relates to a heat exchanger, in particular for motor vehicle. It relates more particularly to a heat exchanger intended to cooperate with an air flow which crosses it, so as to modify the temperature of this flow.

Un tel échangeur de chaleur comporte, à cet effet, une série d'ailettes conductrices de chaleur, en vue d'augmenter sa coopération avec le flux d'air précité. De telles ailettes présentent une forme générale sensiblement plane, et sont sensiblement parallèles et espacées entre elles. Par ailleurs, elles sont munies chacune d'ouvertures pour le passage de tubes destinés à acheminer un fluide propre à échanger de la chaleur avec le flux d'air.For this purpose, such a heat exchanger comprises a series heat conducting fins, in order to increase its cooperation with the aforementioned air flow. Such fins have a generally planar general shape, and are substantially parallel and spaced apart. Otherwise, they are each provided with openings for the passage of tubes intended to convey a clean fluid to exchange the heat with the air flow.

Généralement, les ailettes sont successivement empilées les unes sur les autres. Au montage d'un tel échangeur de chaleur, un glissement de l'une des ailettes par rapport aux autres peut advenir. Les ouvertures de cette ailette sont alors, au moins en partie, occultées par les autres ailettes, ce qui rend délicate l'étape postérieure d'introduction des tubes dans les ouvertures.Generally, the fins are successively stacked the on top of each other. When mounting such a heat exchanger, a sliding of one of the fins relative to the others can happen. The openings of this fin are then, at less partly, obscured by the other fins, which makes the subsequent step of inserting the tubes delicate in the openings.

La présente invention vient améliorer la situation.The present invention improves the situation.

Selon une définition générale de l'invention, chaque ailette comporte au moins une protubérance faisant saillie sur une première face, et au moins un évidement sur une seconde face opposée à la première face, de sorte que la protubérance d'une ailette est propre à coopérer par emboítement avec l'évidement d'une ailette consécutive, ce qui permet de positionner sensiblement les ailettes les unes par rapport aux autres de manière à ce que les ouvertures pour le passage des tubes coïncident sensiblement entre deux ailettes consécutives. According to a general definition of the invention, each fin has at least one protrusion projecting from a first side, and at least one recess on a second side opposite to the first face, so that the protuberance of a fin is able to cooperate by nesting with the recess a consecutive fin, which allows positioning substantially the fins relative to each other of so that the openings for the passage of the tubes substantially coincide between two consecutive fins.

Avantageusement, les ailettes sont réalisées dans un matériau métallique sensiblement déformable et comportent chacune au moins un picot formant à la fois la protubérance et l'évidement précités.Advantageously, the fins are made of a material substantially deformable metal and each have at minus a pin forming both the protuberance and the recess cited above.

Préférentiellement, ces picots sont de forme sensiblement conique, avec le sommet du cône tourné vers une ailette consécutive.Preferably, these pins are of substantially shaped conical, with the top of the cone turned towards a fin consecutive.

Typiquement, ces picots présentent sensiblement une forme de dôme crevé à trois pans, formant chacun un angle sensiblement inférieur à 90° avec la première face précitée d'une ailette.Typically, these pins have substantially a shape of punctured dome with three sides, each forming a substantially angle less than 90 ° with the aforementioned first side of a fin.

Avantageusement, chaque ailette comporte au moins deux évidements et au moins deux protubérances propres à s'engager dans les évidements d'une ailette consécutive, en vue d'immobiliser sensiblement les ailettes, les unes par rapport aux autres.Advantageously, each fin comprises at least two recesses and at least two protuberances suitable for engaging in the recesses of a consecutive fin, in view substantially immobilize the fins, relative to each other to others.

Selon une autre caractéristique optionnelle avantageuse de l'invention, chaque ailette comporte en outre une pluralité de butées d'espacement, destinées à s'appuyer sur l'une des première et seconde faces d'une ailette consécutive, en vue de maintenir les ailettes sensiblement espacées les unes par rapport aux autres, et les butées d'espacement sont de hauteur sensiblement inférieure à une hauteur des protubérances de positionnement.According to another advantageous optional characteristic of the invention, each fin further comprises a plurality spacing stops, intended to rest on one of the first and second faces of a consecutive fin, in view to keep the fins substantially spaced apart by compared to others, and the spacing stops are high substantially less than a height of the protrusions of positioning.

Dans une forme de réalisation préférée de l'échangeur de chaleur selon l'invention, les tubes précités sont sensiblement en contact avec les ouvertures des ailettes, en vue de rigidifier mécaniquement l'ensemble formé par les ailettes et les tubes.In a preferred embodiment of the heat exchanger heat according to the invention, the aforementioned tubes are substantially in contact with the openings of the fins, in order to mechanically stiffen the assembly formed by the fins and the tubes.

D'autres caractéristiques et avantages de l'invention apparaítront à l'examen de la description détaillée, donnée ci-après à titre d'exemple, et des dessins annexés sur lesquels :

  • la figure 1 représente schématiquement un échangeur de chaleur d'un véhicule automobile, muni d'ailettes d'échange thermique ;
  • la figure 2 est une vue générale d'une ailette d'un échangeur de chaleur selon l'invention ;
  • la figure 3 est une vue de face de l'ailette représentée sur la figure 2 ;
  • la figure 4 est une vue selon la coupe IV-IV de la figure 3 ; et
  • la figure 5 est une vue du détail V de la figure 2.
Other characteristics and advantages of the invention will appear on examining the detailed description, given below by way of example, and the attached drawings in which:
  • Figure 1 schematically shows a heat exchanger of a motor vehicle, provided with heat exchange fins;
  • Figure 2 is a general view of a fin of a heat exchanger according to the invention;
  • Figure 3 is a front view of the fin shown in Figure 2;
  • Figure 4 is a view along section IV-IV of Figure 3; and
  • FIG. 5 is a view of detail V of FIG. 2.

La description détaillée ci-après et les dessins annexés contiennent, pour l'essentiel, des éléments de caractère certain. Ils pourront donc non seulement servir à mieux faire comprendre l'invention, mais aussi contribuer à sa définition, le cas échéant.The detailed description below and the attached drawings mainly contain elements of character certain. They can therefore not only serve to do better understand the invention, but also contribute to its definition, if applicable.

On se réfère tout d'abord à la figure 1 pour décrire un échangeur de chaleur selon l'invention, destiné à refroidir un fluide grâce à un flux d'air (flèche F) qui le traverse. Dans l'exemple décrit, cet échangeur de chaleur fait partie du module de refroidissement d'un moteur de véhicule automobile, en tant que radiateur de refroidissement.We first refer to Figure 1 to describe a heat exchanger according to the invention, intended to cool a fluid thanks to an air flow (arrow F) which crosses it. In the example described, this heat exchanger is part the cooling module of a motor vehicle engine, as a cooling radiator.

L'échangeur comporte des tubes plats 1 arrangés en faisceaux et destinés à acheminer un fluide d'échange thermique (liquide de refroidissement) de l'une des boítes collectrices 4a que comporte l'échangeur de chaleur, à l'autre 4b. Les extrémités des tubes sont logées, de préférence à étanchéité, dans des ouvertures que comportent des plaques collectrices 3a et 3b, solidaires des boites collectrices 4a et 4b. Les tubes 1 qui acheminent le liquide de refroidissement coopèrent par échange thermique avec le flux d'air F, en vue de refroidir ledit liquide de refroidissement. L'échangeur de chaleur comporte alors des ailettes 2, de forme générale sensiblement plane et sensiblement parallèles entre elles. Ces ailettes 2 sont réalisées dans un matériau conducteur de chaleur (comportant par exemple de l'aluminium) en vue d'augmenter la surface d'échange thermique avec le flux d'air F qui pénètre dans l'échangeur, ce qui permet d'accroítre, de manière générale, la coopération entre le flux F et l'échangeur.The exchanger comprises flat tubes 1 arranged in bundles and intended to convey a heat exchange fluid (liquid cooling) of one of the manifolds 4a that includes the heat exchanger, at the other 4b. The extremities tubes are housed, preferably sealed, in openings in the collector plates 3a and 3b, integral with the manifolds 4a and 4b. Tubes 1 which coolant cooperate by exchange thermal with the air flow F, in order to cool said cooling liquid. The heat exchanger has then fins 2, of generally substantially planar shape and substantially parallel to each other. These fins 2 are made of a heat conductive material (comprising aluminum) to increase the surface heat exchange with the air flow F which enters the exchanger, which increases, in general, the cooperation between flow F and the exchanger.

Comme on le verra plus loin, les ailettes conductrices comportent des moyens d'espacement de manière à créer des interstices entre les ailettes, ce qui permet de laisser pénétrer le flux d'air F dans l'échangeur et d'éviter des points d'accumulation de chaleur. Dans l'exemple représenté sur la figure 1, les ailettes 2 sont sensiblement perpendiculaires aux axes principaux des tubes 1, et comportent alors des ouvertures 21 pour le passage des tubes 1.As will be seen below, the conductive fins include spacing means so as to create gaps between the fins, which allows to leave penetrate the air flow F into the exchanger and avoid heat accumulation points. In the example shown in FIG. 1, the fins 2 are substantially perpendicular to the main axes of the tubes 1, and then comprise openings 21 for the passage of the tubes 1.

Au cours de l'étape d'assemblage d'un tel échangeur de chaleur, les ailettes 2 sont empilées les unes sur les autres. Ensuite, les tubes 1, préférentiellement réalisés dans un matériau déformable, sont introduits dans les ouvertures 21 des ailettes empilées 2, avec un jeu mécanique choisi. Dans le procédé de fabrication d'un tel échangeur de chaleur, il est prévu ensuite une étape de dilatation des tubes 1, ce qui permet de rigidifier mécaniquement les ailettes par rapport aux tubes, en créant en particulier un contact mécanique sensiblement annulaire entre les parois externes des tubes et les ouvertures 21 des ailettes.During the assembly step of such a heat exchanger heat, the fins 2 are stacked on top of each other. Then, the tubes 1, preferably produced in a deformable material, are introduced into the openings 21 stacked fins 2, with a chosen mechanical play. In the manufacturing process of such a heat exchanger, it a stage of expansion of the tubes 1 is then provided, which mechanically stiffens the fins relative to to the tubes, creating in particular a mechanical contact substantially annular between the outer walls of the tubes and the openings 21 of the fins.

Il est souhaité en particulier que ces ailettes restent sensiblement alignées, de sorte que leurs ouvertures 21 coïncident d'une ailette à l'autre, ce qui permet d'introduire facilement les tubes 1 dans les ouvertures 21 des ailettes consécutives. Les ouvertures 21 de ces ailettes doivent coïncider, par ailleurs, avec les ouvertures prévues dans les plaques collectrices 3a et 3b.It is particularly desired that these fins remain substantially aligned, so that their openings 21 coincide from one fin to the other, which makes it possible to introduce easily the tubes 1 in the openings 21 of the fins consecutive. The openings 21 of these fins must coincide, moreover, with the openings provided in the header plates 3a and 3b.

Cependant, il peut advenir au cours du montage d'un tel échangeur que l'une des ailettes glisse hors de l'empilement. However, it can happen during the mounting of such exchanger that one of the fins slides out of the stack.

Les ouvertures 21 que cette ailette comporte sont alors occultées, au moins en partie, par les autres ailettes.The openings 21 that this fin has are then obscured, at least in part, by the other fins.

Selon l'invention, les ailettes de l'échangeur de chaleur comportent des moyens de positionnement des ailettes consécutives, de sorte que les ailettes empilées successivement restent sensiblement alignées les unes par rapport aux autres, ce qui permet de faire coïncider sensiblement leurs ouvertures respectives 21.According to the invention, the fins of the heat exchanger comprise means for positioning the consecutive fins, so that the fins stacked successively remain substantially aligned with each other, which allows their openings to substantially coincide respective 21.

On se réfère maintenant à la figure 2 pour décrire une ailette d'un échangeur de chaleur selon l'invention. L'ailette 2a comporte des ouvertures, sensiblement en forme de persiennes 221 et 222, de manière à laisser pénétrer latéralement une partie du flux d'air F, en vue d'augmenter la coopération thermique du flux d'air F avec l'échangeur. Chaque ailette comporte en outre des moyens d'espacement 23 avec une ailette consécutive. Ces moyens d'espacement sont formés, dans l'exemple décrit, de butées 23 munies de deux parois 231 et 232, formant un angle voisin de 90° avec une surface principale S de l'ailette (première face précitée). En pratique, les ailettes 2 sont réalisées dans un matériau métallique déformable, par exemple en aluminium et les parois 231 et 232 d'espacement sont obtenues par poinçonnage sur une face des ailettes opposée à la face S (seconde face précitée). La hauteur des parois 231 et 232 définit un pas général p entre les ailettes consécutives (interstices précités).We now refer to Figure 2 to describe a fin a heat exchanger according to the invention. Fin 2a has openings, substantially in the form of louvers 221 and 222, so as to allow lateral penetration of a part of the air flow F, in order to increase cooperation of the air flow F with the exchanger. Each fin further comprises spacing means 23 with a fin consecutive. These spacing means are formed, in the example described, of stops 23 provided with two walls 231 and 232, forming an angle close to 90 ° with a main surface S of the fin (first side mentioned above). In practice, fins 2 are made of a metallic material deformable, for example aluminum and walls 231 and 232 spacing are obtained by punching on one side of the fins opposite side S (second side mentioned above). The height of walls 231 and 232 defines a general pitch p between consecutive fins (aforementioned interstices).

Les ouvertures 21 des ailettes sont sensiblement oblongues, de forme particulièrement adaptées aux tubes 1, plats dans l'exemple décrit. Les parois des ouvertures 21 sont destinées à être sensiblement en contact avec les tubes.The openings 21 of the fins are substantially oblong, particularly suitable for tubes 1, flat in the example described. The walls of the openings 21 are intended to be substantially in contact with the tubes.

En se référant à la figure 2, les ouvertures 21 d'une ailette 2b coïncident sensiblement avec les ouvertures 21 d'une ailette consécutive 2a. Cette coïncidence des ouvertures est assurée grâce à des moyens de positionnement que comportent les ailettes de l'échangeur de chaleur selon l'invention. Ces moyens de positionnement sont réalisés sous la forme d'un picot sensiblement conique, en particulier tronconique, effectué, par exemple, par poinçonnage d'une face inférieure de l'ailette 2a.Referring to Figure 2, the openings 21 of a fin 2b substantially coincide with the openings 21 of a consecutive wing 2a. This coincidence of openings is ensured by means of positioning which comprise the fins of the heat exchanger according to the invention. These positioning means are produced in the form of a substantially conical pin, in particular frustoconical, performed, for example, by punching a bottom face fin 2a.

En se référant à la figure de détail 5, la protubérance formée par poinçonnage présente une forme générale de dôme crevé à trois pans 241, 242 et 243, ces pans formant un angle inférieur à 90° avec la surface principale S de l'ailette.Referring to the detail figure 5, the protuberance formed by punching has a general shape of a punctured dome three sides 241, 242 and 243, these sides forming an angle less than 90 ° with the main surface S of the fin.

En se référant à la figure 4, représentant une vue en coupe transversale de deux ailettes consécutives 2a et 2b, les parois 231 et 232 d'espacement sont sensiblement recourbées latéralement en leurs extrémités et présentent ainsi une forme générale de collet. Par ailleurs, la hauteur h du picot de positionnement 24 est supérieure à la hauteur p de la butée d'espacement 23. Ainsi, les pans 241, 242 et 243 d'une ailette 2b s'emboítent dans l'évidement que forme le poinçonnage de positionnement d'une ailette consécutive 2a, tandis que les parois 231 et 232 d'espacement viennent en contact avec la surface principale de l'ailette consécutive 2a.Referring to Figure 4, showing a sectional view transverse of two consecutive fins 2a and 2b, the spacing walls 231 and 232 are substantially curved laterally at their ends and thus have a shape general of collar. Furthermore, the height h of the spike positioning 24 is greater than the height p of the stop of spacing 23. Thus, the sides 241, 242 and 243 of a fin 2b fit into the recess that forms the punching of positioning of a consecutive fin 2a, while the spacing walls 231 and 232 come into contact with the main surface of the consecutive fin 2a.

Avantageusement, chaque ailette comporte deux picots de positionnement 24a et 24b (figure 3), ce qui permet d'immobiliser sensiblement les ailettes, les unes par rapport aux autres.Advantageously, each fin has two pins positioning 24a and 24b (Figure 3), which allows substantially immobilize the fins, relative to each other to others.

Ainsi, selon l'un des avantages majeurs que procure la présente invention, les ailettes peuvent être sensiblement immobilisées les unes par rapport aux autres en cours d'empilement, ce qui facilite l'introduction des tubes dans les ouvertures 21.Thus, according to one of the major advantages which the present invention, the fins can be substantially immobilized in relation to each other in progress stacking, which facilitates the introduction of the tubes into the openings 21.

Selon un autre avantage que procure l'invention, les deux picots de positionnement 24a et 24b permettent en outre d'indexer les ailettes, les unes par rapport aux autres, dans le cas (non représenté) où celles-ci ne présentent pas de double symétrie axiale. According to another advantage which the invention provides, the two positioning pins 24a and 24b also allow to index the fins, in relation to each other, in the case (not shown) where these do not present any double axial symmetry.

Bien entendu, la présente invention ne se limite pas à la forme de réalisation décrite ci-avant à titre d'exemple. Elle s'étend à d'autres variantes.Of course, the present invention is not limited to the embodiment described above by way of example. She extends to other variants.

On comprendra ainsi que les moyens de positionnement 24 décrits ci-avant peuvent former à la fois des moyens de positionnement et des moyens d'espacement entre les ailettes.It will thus be understood that the positioning means 24 described above can form both means of positioning and spacing means between the fins.

Ces moyens de positionnement sont réalisés par poinçonnage des ailettes. En variante, celles-ci peuvent comporter une protubérance formée sur une face, ainsi qu'un évidement formé sur l'autre face. S'il est souhaité en particulier de former un échangeur de chaleur avec des tubes inclinés d'un angle différent de 90° par rapport aux ailettes, il peut être envisagé de décaler, dans le plan d'une ailette, l'évidement de la protubérance qu'elle comporte.These positioning means are produced by punching the fins. As a variant, these may include a protuberance formed on one side, as well as a recess formed on the other side. If it is particularly desired to train a heat exchanger with tubes inclined at an angle different from 90 ° to the fins, it can be envisaged to shift, in the plane of a fin, the recess of the protuberance it entails.

La forme des protubérances de positionnement réalisées par poinçonnage et présentant trois pans (ou lèvres) 241, 242 et 243 est décrite ci-avant à titre d'exemple. De manière générale, il peut être prévu des poinçons de positionnement sensiblement de formes tronconiques, ou encore coniques, avec le sommet du cône tourné vers une ailette consécutive.The shape of the positioning protrusions produced by punching and having three sides (or lips) 241, 242 and 243 is described above by way of example. So general, positioning punches may be provided substantially frustoconical, or even conical, with the top of the cone turned towards a consecutive fin.

L'invention s'applique, de façon avantageuse, à un échangeur de chaleur réalisé par assemblage mécanique des tubes plats et d'ailettes de forme sensiblement planes, sensiblement perpendiculaires aux tubes.The invention advantageously applies to an exchanger heat produced by mechanical assembly of flat tubes and substantially planar shaped fins, substantially perpendicular to the tubes.

Claims (8)

Echangeur de chaleur, notamment pour véhicule automobile, du type comprenant une série d'ailettes (2a,2b) sensiblement planes, sensiblement parallèles et espacées entre elles, munies chacune d'ouvertures (21) pour le passage de tubes (1) d'échange thermique,
caractérisé en ce que chaque ailette (2a) comporte au moins une protubérance faisant saillie sur une première face (S), et au moins un évidement sur une seconde face opposée à ladite première face, tandis que la protubérance (24) d'une ailette (2b) est propre à coopérer par emboítement avec l'évidement d'une ailette consécutive (2a), ce qui permet de positionner sensiblement les ailettes les unes par rapport aux autres, de sorte que les ouvertures (21) pour le passage des tubes coïncident sensiblement entre deux ailettes consécutives (2a,2b).
Heat exchanger, in particular for a motor vehicle, of the type comprising a series of fins (2a, 2b) substantially planar, substantially parallel and spaced apart, each provided with openings (21) for the passage of tubes (1) of heat exchange,
characterized in that each fin (2a) has at least one protuberance projecting from a first face (S), and at least one recess on a second face opposite to said first face, while the protuberance (24) of a fin (2b) is adapted to cooperate by fitting with the recess of a consecutive fin (2a), which allows the fins to be positioned substantially in relation to each other, so that the openings (21) for the passage of the tubes substantially coincide between two consecutive fins (2a, 2b).
Echangeur de chaleur selon la revendication 1, caractérisé en ce que les ailettes (2) sont réalisées dans un matériau métallique sensiblement déformable, et en ce que les ailettes comportent chacune un picot (24) pour former à la fois une protubérance sur la première face (S) et un évidement dans la seconde face opposée.Heat exchanger according to claim 1, characterized in that the fins (2) are made of a material substantially deformable metal, and in that the fins each have a pin (24) to form both a protuberance on the first face (S) and a recess in the second opposite side. Echangeur de chaleur selon la revendication 2, caractérisé en ce que lesdits picots (24) sont de forme sensiblement conique.Heat exchanger according to claim 2, characterized in that said pins (24) are substantially shaped conical. Echangeur de chaleur selon la revendication 3, caractérisé en ce que les picots (24) présentent sensiblement une forme de dôme crevé à trois pans (241,242,243).Heat exchanger according to claim 3, characterized in that the pins (24) have substantially a shape three-sided punctured dome (241,242,243). Echangeur de chaleur selon la revendication 4, caractérisé en ce que chaque pan (241,242,243) forme un angle sensiblement inférieur à 90° avec la première face (S) de l'ailette.Heat exchanger according to claim 4, characterized in that each panel (241,242,243) forms an angle substantially less than 90 ° with the first side (S) of the fin. Echangeur de chaleur selon l'une des revendications précédentes, caractérisé en ce que chaque ailette comporte au moins deux évidements et au moins deux protubérances (24a,24b) propres à s'engager dans les évidements d'une ailette consécutive, en vue d'immobiliser sensiblement les ailettes, les unes par rapport aux autres.Heat exchanger according to one of claims previous, characterized in that each fin has at at least two recesses and at least two protrusions (24a, 24b) suitable for engaging in the recesses of a fin consecutive, in order to immobilize the fins appreciably, relative to each other. Echangeur de chaleur selon l'une des revendications précédentes, caractérisé en ce que chaque ailette (2) comporte en outre une pluralité de butées d'espacement (23), destinées à s'appuyer sur l'une des première et seconde faces (S) d'une ailette consécutive, en vue de maintenir les ailettes sensiblement espacées les unes par rapport aux autres, et en ce que les butées d'espacement (23) sont de hauteur (p) sensiblement inférieure à une hauteur (h) des protubérances de positionnement (24).Heat exchanger according to one of claims previous, characterized in that each fin (2) has furthermore a plurality of spacing stops (23), intended to lean on one of the first and second faces (S) of a consecutive fin, in order to maintain the fins substantially spaced from each other, and in that the spacers (23) are of height (p) substantially less than a height (h) of the protrusions positioning (24). Echangeur de chaleur selon l'une des revendications précédentes, caractérisé en ce que les tubes (1) sont sensiblement en contact mécanique avec lesdites ouvertures (21) des ailettes.Heat exchanger according to one of claims previous, characterized in that the tubes (1) are substantially in mechanical contact with said openings (21) fins.
EP20000401350 1999-05-27 2000-05-17 Heat exchanger with improved fin-positioning Expired - Lifetime EP1055897B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9906718A FR2794226B1 (en) 1999-05-27 1999-05-27 HEAT EXCHANGER, PARTICULARLY FOR MOTOR VEHICLE, PROVIDED WITH IMPROVED FIN POSITIONING
FR9906718 1999-05-27

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EP1055897A1 true EP1055897A1 (en) 2000-11-29
EP1055897B1 EP1055897B1 (en) 2004-03-17

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DE (1) DE60008963T2 (en)
ES (1) ES2219276T3 (en)
FR (1) FR2794226B1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003093748A1 (en) * 2002-05-01 2003-11-13 Gregory Christian T Radial flow heat exchanger
FR2866698A1 (en) * 2004-02-24 2005-08-26 Valeo Thermique Moteur Sa Heat exchanger for use as e.g. cooling radiator, has spacing units each projecting from surface of fins and arranged very close to deflectors, and lugs provided in cut and folded portion of fin
US7128136B2 (en) 1998-08-10 2006-10-31 Gregory Christian T Radial flow heat exchanger
CN101995115A (en) * 2009-08-07 2011-03-30 江森自控科技公司 Multi-channel heat exchanger fins

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA3036460A1 (en) 2018-03-14 2019-09-14 Rheem Manufacturing Company Heat exchanger fin
USD906268S1 (en) 2018-09-11 2020-12-29 Rheem Manufacturing Company Heat exchanger fin

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JPS57181917A (en) * 1981-04-30 1982-11-09 Toyota Motor Corp Plate-fin radiator
EP0086559A2 (en) * 1982-02-16 1983-08-24 Unipart Group Limited Improvements relating to heat exchangers
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FR2346660A1 (en) * 1976-03-31 1977-10-28 Volkswagenwerk Ag TUBULAR EXCHANGER
JPS57181917A (en) * 1981-04-30 1982-11-09 Toyota Motor Corp Plate-fin radiator
EP0086559A2 (en) * 1982-02-16 1983-08-24 Unipart Group Limited Improvements relating to heat exchangers
FR2770626A1 (en) * 1997-11-05 1999-05-07 Eichenauer Gmbh & Co Kg F Heating driver's cabin of commercial vehicles rapidly

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7128136B2 (en) 1998-08-10 2006-10-31 Gregory Christian T Radial flow heat exchanger
WO2003093748A1 (en) * 2002-05-01 2003-11-13 Gregory Christian T Radial flow heat exchanger
FR2866698A1 (en) * 2004-02-24 2005-08-26 Valeo Thermique Moteur Sa Heat exchanger for use as e.g. cooling radiator, has spacing units each projecting from surface of fins and arranged very close to deflectors, and lugs provided in cut and folded portion of fin
CN101995115A (en) * 2009-08-07 2011-03-30 江森自控科技公司 Multi-channel heat exchanger fins

Also Published As

Publication number Publication date
DE60008963T2 (en) 2004-08-12
EP1055897B1 (en) 2004-03-17
DE60008963D1 (en) 2004-04-22
FR2794226A1 (en) 2000-12-01
FR2794226B1 (en) 2001-07-27
ES2219276T3 (en) 2004-12-01

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