WO2019180377A1 - Intake air cooling device for an internal combustion engine - Google Patents

Intake air cooling device for an internal combustion engine Download PDF

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Publication number
WO2019180377A1
WO2019180377A1 PCT/FR2019/050634 FR2019050634W WO2019180377A1 WO 2019180377 A1 WO2019180377 A1 WO 2019180377A1 FR 2019050634 W FR2019050634 W FR 2019050634W WO 2019180377 A1 WO2019180377 A1 WO 2019180377A1
Authority
WO
WIPO (PCT)
Prior art keywords
housing
cooling device
intake air
flange
docking
Prior art date
Application number
PCT/FR2019/050634
Other languages
French (fr)
Inventor
Frédéric WASCAT
Yoann Naudin
Original Assignee
Valeo Systemes Thermiques
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 Valeo Systemes Thermiques filed Critical Valeo Systemes Thermiques
Publication of WO2019180377A1 publication Critical patent/WO2019180377A1/en

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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
    • F28F9/001Casings in the form of plate-like arrangements; Frames enclosing a heat exchange core
    • F28F9/002Casings in the form of plate-like arrangements; Frames enclosing a heat exchange core with fastening means for other structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/045Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
    • F02B29/0462Liquid cooled heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2255/00Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
    • F28F2255/08Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes pressed; stamped; deep-drawn
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the invention relates to a cooling system for an intake air of an internal combustion engine.
  • the invention finds a particularly advantageous, but not exclusive, application with turbocharged engines.
  • the automobile like many other industries, uses heat exchangers to provide the engine with optimum operating conditions.
  • Cooling a heat engine, and more particularly intake air from a turbocharger outlet, requires the use of heat exchangers to cool the air and to increase the density of the mixture. air / fuel.
  • a heat exchanger for cooling a supercharged air consists of a housing that contains a heat exchange beam body between the intake air to be cooled and a heat transfer fluid.
  • the docking flange must meet certain conditions to allow the heat exchanger to be perfectly maintained against the internal combustion engine. Indeed, the latter must withstand significant mechanical stresses resulting from the weight, the cantilever and the method of attachment of the cooling device equipped with such a docking flange
  • the heat exchanger is placed not far from the combustion chambers where the temperature can reach 700 ° C.
  • the exchange bundle is also traversed by a cooling fluid which is at a temperature of the order of 50 ° C. These two temperatures are far apart and generate significant thermal stresses on the docking flange of the cooling device.
  • the docking flange of the prior art is designed from the metal molding technique.
  • the metal molding is known to be an imprecise manufacturing technique, which is a disadvantage in the production of metal parts to ensure airtightness with another component, in this case, the cylinder head of the internal combustion engine.
  • the invention therefore aims to at least partially overcome the disadvantages of the prior art described above by reducing the manufacturing time, reducing manufacturing costs and reducing the energy required for the production of the flange d docking which ensures the attachment of the cooling device to the internal combustion engine.
  • the present invention thus relates to a cooling device of an intake air of an internal combustion engine, the cooling device comprising a housing inside which is housed a beam body consisting of a stack of plates. and dissipation devices, the cooling device comprising a docking flange configured to connect the casing to the internal combustion engine, characterized in that the docking flange is embossed.
  • Stamping is the deformation of the metal raw material into a desired piece of complex shape by the compressive action of a stamping press.
  • This manufacturing technique has many advantages including that of working the metal cold, which avoids spending energy to melt the raw material as requested during a metal molding.
  • the compressive action does not involve the creation of asperities on the stamped part, which avoids the resumption of machining of its surface, which involves in the prior art additional expenses.
  • the docking flange has a more complex shape for fixing the housing against the internal combustion engine, while having a mechanical and thermal resistance at least as good as with the solution of the prior art.
  • the stamped docking flange has the advantage of being secured to the housing via a method called Nocolok brazing. This process consists of brazing without adding material.
  • the material forming the embossed docking flange comprises at least two layers: a core of raw material and a bonding layer for mechanically connecting the docking flange to the housing.
  • This tie layer is characterized by its melting temperature, about 550 ° C, which is lower than the melting temperature of the docking flange core.
  • the bonding layer melts and mixes with the surface against which it is supported, to form a single structure, ensuring the mechanical connection and sealing between the two welded surfaces.
  • the housing and the docking flange, both of which are provided with this bonding layer are welded when passing through a Nocolok brazing furnace. Then follows a cooling step that solidifies the parts thus linked.
  • the manufacturing time of a stamped part is significantly lower than that of a molded part and the rate of production of the stamped parts is greater than that of the molded parts.
  • the beam body is a heat exchange bundle between the intake air flow and a heat transfer fluid. Intake air flow and heat transfer fluid, including a coolant, both pass through the beam body.
  • the docking flange comprises a folded edge against which the housing is supported.
  • the folded edge thus provides a contact surface ensuring a good connection area and a good seal.
  • the housing bears against an inner face of the folded edge.
  • the folded edge thus forms a seat belt of the housing, surrounding the latter.
  • internal face here refers to the face of the folded edge which is in contact with the housing, that is to say the face against which the housing rests and is welded after brazing by the Nocolok process.
  • this folded edge has the advantage of increasing the contact area between the housing and the docking flange, thereby increasing the contact area. and therefore the brazing ability of the housing to the docking flange. Moreover, this folded edge provides a housing holding space against the docking flange visible to the naked eye, which facilitates its verification.
  • the folded edge comprises at least one stop against which the housing bears.
  • the stops which result from a deformation of the surface of the docking flange, are easily achievable on a stamped part, as is the case of the docking flange according to the invention.
  • the introduction of the housing into the docking flange is limited at one end by these stops, thus ensuring a positioning of the housing in the docking flange which does not require additional means to ensure their position relative to the 'other. This guarantees a simple way the respect of an essential dimension of the cooling device according to the invention.
  • the beam body comprises at least one pair of plates between which a heat transfer fluid can circulate.
  • the beam body is configured to be traversed in a sealed manner by a coolant liquid.
  • the beam body comprises at least one pair of dissipation devices disposed on either side of the pair of plates.
  • the beam body which is traversed by the intake air flow, comprises at least a pair of rectangular parallelepiped shaped plates, for example rectangular, between which circulates at least one heat transfer fluid flow.
  • the dissipation devices are placed on either side of the pair of plates. In this way, a dissipation device is located adjacent to a plate and a heat transfer occurs between the intake air stream, which licks the dissipation devices, and the coolant flow that evolves between the two plates. a couple of plates.
  • the docking flange comprises at least one docking edge provided with fastening means configured to secure the docking flange to the internal combustion engine.
  • the fixing means may be orifices enabling the insertion of screws ensuring the attachment of the docking flange on the internal combustion engine.
  • the housing comprises at least four sidewalls surrounding the beam body, at least one of the sidewalls comprising at least one curved edge which is superimposed at least in part on an adjacent sidewall.
  • these flanks are separate parts from each other. After joining, these parts form the housing.
  • This curved edge of a flank, allowing the superposition of a first flank on another side, is obtained by stamping a plate.
  • the superposition of the curved edge of the first sidewall on another side increases the contact surface, which improves the welding between the two superimposed sides and finally improves the sealing of the housing.
  • the soldering is carried out by brazing according to the Nocolok process, during a step simultaneous with the brazing step of the stamped docking flange and the housing.
  • the cooling device comprises a housing holding flange, secured to the housing opposite the docking flange relative to the beam body.
  • This holding flange keeps the housing flanks in place before the soldering operation.
  • This holding flange also forms a docking zone for a pipe that channels the intake flow from the turbocharger.
  • the cooling device of an intake air at least:
  • a simultaneous soldering step at least of the housing, the docking flange and the beam body.
  • the brazing step allows to connect in one operation the beam body, the housing, the docking flange and the holding flange.
  • the brazing step is carried out by a Nocolok process.
  • FIG. 1 is a front perspective view of the cooling device of an intake air of an internal combustion engine according to the invention
  • FIG. 2 is a perspective view of the docking flange operated in the cooling device which is the subject of the invention
  • FIG. 3 is a rear perspective view of the cooling device of an intake air according to the invention.
  • FIG. 1 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine.
  • a cooling device 1 comprises a housing 2, a beam body 3 and a docking flange 4, assembled to each other simultaneously during a brazing step according to a Nocolok method.
  • the housing 2 comprises four flanks 21, parallel in pairs, for forming a housing 2 of parallelepipedal shape, or cubic.
  • the housing 2 defines an inlet surface 22 and an outlet surface 23 parallel to each other, allowing an intake air flow to pass through the housing 2 in its entirety, that is to say from one side to the other .
  • the beam body 3 consists of a stack of plates 31 and dissipation devices 32.
  • the stack consists of the following: an alternation of a pair of plates 31 and a dissipation device 32. Between the two plates 31 of the pair of plates, a heat transfer fluid flow circulates parallel thereto.
  • a pair of dissipation devices 32 is disposed on either side of the plates 31, flanking them.
  • the flow of intake air passing through the housing 2 passes through the dissipating devices 32, the latter may take the form of fins or spacers.
  • the dissipating devices 32 may take the form of fins or spacers.
  • the docking flange 4 is placed at the exit surface 23 of the casing 2. Like a ring, the docking flange 4 surrounds the casing 2 which rests against a folded edge 41 of the casing flange. 4. Such a folded edge 41 results from a right angle bend of an inner part of the docking flange 4 housing.
  • the casing 2 is inserted inside the docking flange 4 until it is locked against abutments 42 which are formed on the folded edge 4L.
  • a stop 42 takes the form of a tongue made by cutting or deformation of the folded edge 41, which emerges towards the inside of the docking flange 4.
  • a free edge of this stop 42 forms a bearing face against which the housing 2 is brought into contact, during the pre-assembly of the cooling device 1 according to the invention. In this way, the housing 2 is embedded in the docking flange 4.
  • brazing is performed between the housing 2 and the docking flange 4, at the folded edge 41.
  • the inner face 411 of the folded edge 41 of the docking flange 4 is welded to the four flanks 21 of the housing 2 by brazing according to the Nocolok process, ensuring good mechanical strength of the housing 2 against the docking flange 4.
  • the docking flange 4 comprises a docking edge 43 on which fixing means 44 are present to allow the attachment of the docking flange 4 against the internal combustion engine.
  • the fastening means 44 are orifices allowing insertion, for example, of a screw which, once tightened, keeps the docking flange 4 against the internal combustion engine.
  • the fastening means 44 are distributed on the docking edge all around the casing 2.
  • a peripheral reinforcement 45 is formed on the docking flange 4 during the stamping operation.
  • This peripheral reinforcement 45 takes the form of a right-angled folding of the outer peripheral part of the docking flange 4.
  • the docking flange 4 has a "U" -shaped section, observed in accordance with a perpendicular section of the docking flange 4 and passing therethrough. The presence of such a peripheral reinforcement 45 significantly increases the mechanical strength of the docking flange 4.
  • the docking flange 4 also comprises ears where the fastening means 44 are arranged. This is a localized widening of the docking edge 43 which offers the possibility of disposing a nut and a washer therein.
  • the docking flange 4 is stamped because of the rounding and filleting it comprises at the border between the folded edge 41 and the docking edge 43, for example, or between the docking edge 43 and the peripheral reinforcement 45.
  • Figure 2 shows a cross-sectional view of the docking flange 4 according to the side accommodating the housing.
  • the docking flange 4 comprises at its center an open space 46 of surface equivalent to the exit surface of the housing, thus allowing the latter to be inserted into the docking flange 4.
  • the stops 42 coming from the folded edge 41 , act as a limit to the insertion of the housing into the docking flange 4. Once the housing is inserted to the stops 42, its flanks rest against the folded edge 41 so as to create a contact surface 47 between the housing and the docking flange 4. In a later step, a mechanical stirring link according to the Nocolok process is implemented at this contact surface 47, in order to mechanically link the housing to the docking flange 4.
  • the docking edge 43 is provided with fastening means 44.
  • these fastening means 44 may be orifices allowing the insertion of anchoring means of the docking flange 4 against the combustion engine. internal. Unlike the previous connection operation between the housing 2 and the docking flange 4, the latter is fixed against the internal combustion engine by a mechanical compressive action such as, for example, the use of screws and d nuts.
  • the docking flange 4 comprises the peripheral reinforcement 45 placed at the outer periphery of the docking flange 4.
  • This peripheral reinforcement 45 consists of a perpendicular fold of a docking edge 43 of the docking flange 4, such a fold being made in the same direction as the folded edge 41 of the docking flange 4.
  • the docking flange 4 taking the form of a "U”, comprises two right angles 48 which have the major characteristic of being highly resistant to mechanical and thermal deformation.
  • the docking flange 4 is stamped. This docking flange 4 is the result of a deformation of a flat sheet operated by a punch received in a cavity, punch and cavity being a constituent of a stamping press.
  • Figure 3 shows a general view of the rear of the cooling device 1 of an intake air. Here is meant, rear with respect to Figure 1, having a view of the front of the cooling device 1.
  • FIG. 3 illustrates a rear face of the docking edge 43.
  • the fastening means 44 allow the attachment of the docking flange 4 to the internal combustion engine, in particular on the cylinder head of the latter.
  • a fold is made, thereby creating the peripheral reinforcement 45.
  • This reinforcement oriented in the same direction as the folded edge 41, makes the docking flange more resistant to the mechanical forces imposed by the cooling device 1 as such, and not its mounting on the internal combustion engine.
  • the inlet surface 22 of the casing 2 forms the mouth through which the flow of intake air enters inside the casing 2, in order to undergo a heat exchange with the heat transfer liquid circulating in the casing 2.
  • the heat exchange is increased thanks to the presence of dissipation devices 32 which are traversed by the intake air flow. These dissipation devices 32 capture the calories present in the intake air flow and transmit them to the plates 31, and thus to the heat transfer fluid circulating therebetween.
  • the successive stacking of this organization composes the beam body 3.
  • the casing 2 envelops the beam body 3 via four flanks 21, leaving open the inlet surface 22, which allows entry of the intake air flow, and the outlet surface 23 which allows the output of this same flow of intake air.
  • flanks 21 In order to fix the flanks 21 between them, the latter are provided, at their ends in contact with the other sides 21, curved edges 24. These curved edges 24 create a large bonding surface between two flanks 21 adjacent. Thus, it is possible to have two longitudinal flanks 21 each provided with two curved edges 24 which cooperate with side flanks 21 flat at their ends. Alternatively, each of the four flanks 21 may comprise a single curved edge 24 associated with the adjacent flank 21.
  • a stirring weld according to the Nocolok process is carried out at this bonding surface between the curved edges 24 and the sides covered by these curved edges 24, in order to mechanically link the flanks 21 of the housing 2 with each other, making at the same time, the housing 2 completely sealed to the flow of intake air flowing in the beam body 3.
  • FIG. 3 also shows a holding flange 25, one of whose functions is to hold the four flanks 21 together against one another by means of notches 26, placed around the periphery of the holding flange 25. This maintenance is used especially in the pre-assembly phase, before the passage to the brazing furnace provided in the context of the Nocolok process.
  • This holding flange 25 thus ensures the fixing of the four flanks 21 between them, allowing the sealing of the housing 2.
  • This holding flange 25 also serves as a docking edge for receiving a pipe from the air circuit admission
  • the holding flange 25 is a piece of complementary shape to the shape of the housing 2. In sectional view, this holding flange forms a "U" within which each flank 21 of the housing 2 is housed.
  • the holding flange 25 is disposed opposite the docking flange 4, with respect to the 2 of the housing or relative to the beam body 3.
  • the holding flange 25 thus extends in the plane of the inlet surface 22 of the intake air flow, while the embossed docking flange 4 s' extends in the plane of the exit surface 23 of the intake air flow.
  • the stamped docking flange 4 is thus disposed at a first end of the casing 2, along a direction of flow of the intake air stream.
  • the holding flange 25 is in turn disposed at a second end of the housing 2, opposite the first end along a direction of flow of the intake air flow.
  • the present invention provides a cooling member of a flow of air admitted into a heat engine and which passes through a heat exchange beam.
  • This member is intended to be attached to a cylinder head of the heat engine by means of a fastening flange which is made by a stamping process, detectable in that the flange comprises bending and deformation zones which result from this process of stamping.
  • the invention has a certain advantage in the use of a stamped docking flange as it can be associated with the other preassembled parts of the cooling device, prior to the brazing operation performed in a furnace of a Nocolok process.
  • the invention can not be limited to the means and configurations described and illustrated here, and it also extends to any equivalent means or configuration and any technical combination operating such means.
  • the shape of the docking flange can be modified without harming the invention, insofar as the cooling device, in fine, fulfills the same functionalities as those described in this document.

Abstract

The invention concerns a device for cooling intake air of an internal combustion engine, the cooling device comprising a housing, inside which is housed a bundle body composed of a stack of plates and dissipation devices, the cooling device comprising a docking flange configured to connect the housing to the internal combustion engine, characterised in that the docking flange is swaged.

Description

DISPOSITIF DE REFROIDISSEMENT D’UN AIR D’ADMISSION DE  DEVICE FOR COOLING AN INTAKE AIR OF
MOTEUR A COMBUSTION INTERNE  INTERNAL COMBUSTION ENGINE
L’invention porte sur un système de refroidissement d’un air d’admission de moteur à combustion interne. L'invention trouve une application particulièrement avantageuse, mais non exclusive, avec les moteurs turbocompressés. The invention relates to a cooling system for an intake air of an internal combustion engine. The invention finds a particularly advantageous, but not exclusive, application with turbocharged engines.
L’automobile, comme de nombreux autres domaines industriels, utilise des échangeurs de chaleur pour assurer au moteur des conditions de fonctionnement optimales. The automobile, like many other industries, uses heat exchangers to provide the engine with optimum operating conditions.
Le refroidissement d’un moteur thermique, et plus particulièrement de l’air d’admission provenant d’une sortie d’un turbocompresseur, nécessite l’utilisation d’échangeurs de chaleur pour refroidir cet air et permettre d’augmenter la densité du mélange air / carburant. Cooling a heat engine, and more particularly intake air from a turbocharger outlet, requires the use of heat exchangers to cool the air and to increase the density of the mixture. air / fuel.
De nos jours, un échangeur de chaleur destiné au refroidissement d’un air suralimenté se compose d’un boîtier qui contient un corps de faisceau d’échange de chaleur entre l’air d’admission devant être refroidi et un fluide caloporteur. Nowadays, a heat exchanger for cooling a supercharged air consists of a housing that contains a heat exchange beam body between the intake air to be cooled and a heat transfer fluid.
Il est connu de fixer l’échangeur de chaleur destiné à refroidir l’air d’admission du moteur turbocompressé contre le moteur à combustion interne par l’intermédiaire d’une bride d’accostage. It is known to fix the heat exchanger for cooling the intake air of the turbocharged engine against the internal combustion engine via a docking flange.
La bride d’accostage doit remplir certaines conditions pour permettre à l’échangeur de chaleur d’être parfaitement maintenu contre le moteur à combustion interne. En effet, cette dernière doit résister à des contraintes mécaniques importantes qui résultent du poids, du porte-à- faux et du mode de fixation du dispositif de refroidissement équipé d’une telle bride d’accostage The docking flange must meet certain conditions to allow the heat exchanger to be perfectly maintained against the internal combustion engine. Indeed, the latter must withstand significant mechanical stresses resulting from the weight, the cantilever and the method of attachment of the cooling device equipped with such a docking flange
Par ailleurs, l’échangeur de chaleur est placé non loin des chambres de combustion où la température peut atteindre 700°C. Le faisceau d’échange est également traversé par un fluide de refroidissement qui lui est à une température de l’ordre de 50°C. Ces deux températures sont fort éloignées et génèrent des contraintes thermiques importantes sur la bride d’accostage du dispositif de refroidissement. In addition, the heat exchanger is placed not far from the combustion chambers where the temperature can reach 700 ° C. The exchange bundle is also traversed by a cooling fluid which is at a temperature of the order of 50 ° C. These two temperatures are far apart and generate significant thermal stresses on the docking flange of the cooling device.
Pour résister à ces contraintes, la bride d’accostage de l’art antérieur est conçue à partir de la technique du moulage métallique. To resist these constraints, the docking flange of the prior art is designed from the metal molding technique.
Cependant, cette technique de fabrication comprend plusieurs inconvénients. La fabrication d’une pièce par moulage métallique demande tout d’abord la réalisation d’un moule, qui, avec le temps s’use inévitablement. De plus, cette technique de fabrication est extrêmement énergivore. En effet, pour mouler une pièce, la matière première métallique doit être fondue, ce qui requiert une quantité considérable d’énergie à fournir pour fondre la matière première. However, this manufacturing technique has several disadvantages. The manufacture of a piece by metal molding first requires the realization of a mold, which with time wears inevitably. In addition, this manufacturing technique is extremely energy-intensive. Indeed, to mold a part, the metal raw material must be melted, which requires a considerable amount of energy to provide to melt the raw material.
En outre, le moulage métallique est connu pour être une technique de fabrication peu précise, ce qui représente un inconvénient lors de la production de pièces métalliques destinées à assurer une étanchéité à l’air avec un autre composant, dans le cas présent, la culasse du moteur à combustion interne. In addition, the metal molding is known to be an imprecise manufacturing technique, which is a disadvantage in the production of metal parts to ensure airtightness with another component, in this case, the cylinder head of the internal combustion engine.
Enfin, il est régulier d’opérer une reprise en usinage d’une pièce moulée de manière à éliminer les aspérités sur certaines surfaces de la pièce moulée. Or, il est important que la surface de la bride d’accostage soit dénuée de toute aspérité afin d’assurer un planéité idéale entre la surface de la bride d’accostage et la surface du moteur à combustion interne contre laquelle la bride d’accostage est fixée. Cette retouche sur les pièces moulées implique donc une perte de temps et des coûts plus importants. L’invention a donc pour objectif de remédier au moins partiellement aux inconvénients de l'art antérieur décrits ci-dessus en réduisant le temps de fabrication, en diminuant les coûts de fabrication et en réduisant l’énergie nécessaire à la réalisation de la bride d’accostage qui assure la fixation du dispositif de refroidissement au moteur à combustion interne. Finally, it is regular to perform a machining recovery of a molded part so as to eliminate roughness on certain surfaces of the molded part. However, it is important that the surface of the docking flange is free of any roughness to ensure an ideal flatness between the surface of the docking flange and the surface of the internal combustion engine against which the docking flange is fixed. This retouching on the molded parts therefore involves a loss of time and greater costs. The invention therefore aims to at least partially overcome the disadvantages of the prior art described above by reducing the manufacturing time, reducing manufacturing costs and reducing the energy required for the production of the flange d docking which ensures the attachment of the cooling device to the internal combustion engine.
La présente invention concerne ainsi un dispositif de refroidissement d’un air d’admission d’un moteur à combustion interne, le dispositif de refroidissement comprenant un boîtier à l’intérieur duquel est logé un corps de faisceau se composant d’un empilement de plaques et de dispositifs de dissipation, le dispositif de refroidissement comprenant une bride d’accostage configurée pour relier le boîtier au moteur à combustion interne, caractérisé en ce que la bride d’accostage est emboutie. The present invention thus relates to a cooling device of an intake air of an internal combustion engine, the cooling device comprising a housing inside which is housed a beam body consisting of a stack of plates. and dissipation devices, the cooling device comprising a docking flange configured to connect the casing to the internal combustion engine, characterized in that the docking flange is embossed.
L’emboutissage consiste en la déformation de la matière première métallique en une pièce recherchée de forme complexe par l’action compressive d’une presse à emboutir. Cette technique de fabrication comporte de nombreux avantages dont notamment celui de travailler le métal à froid, ce qui évite de dépenser de l’énergie pour faire fondre la matière première comme il est demandé lors d’un moulage métallique. De plus, l’action compressive n’implique pas la création d’aspérités sur la pièce emboutie, ce qui évite la reprise d’usinage de sa surface, qui implique dans l’art antérieur des dépenses additionnelles. Stamping is the deformation of the metal raw material into a desired piece of complex shape by the compressive action of a stamping press. This manufacturing technique has many advantages including that of working the metal cold, which avoids spending energy to melt the raw material as requested during a metal molding. In addition, the compressive action does not involve the creation of asperities on the stamped part, which avoids the resumption of machining of its surface, which involves in the prior art additional expenses.
En plus d’éviter les dépenses additionnelles évoquées ci-avant, ce type de formage permet d’obtenir une meilleure précision dimensionnelle de la pièce. Ainsi, la bride d’accostage présente une forme plus complexe permettant de fixer le boîtier contre le moteur à combustion interne, tout en ayant une résistance mécanique et thermique au moins aussi bonne qu’avec la solution de l’art antérieur. De plus, la bride d’accostage emboutie présente l’avantage de pouvoir être solidarisée au boîtier par l’intermédiaire d’un procédé nommé brasage Nocolok. Ce procédé consiste à effectuer le brasage sans ajout de matière. En effet, la matière composant la bride d’accostage emboutie comprend au moins deux couches : une âme de matière première et une couche de liaison destiné à relier mécaniquement la bride d’accostage au boîtier. Cette couche de liaison est caractérisée par sa température de fusion, environ 550°C, qui est inférieure à la température de fusion de l’âme de la bride d’accostage. Ainsi, lors du brasage par procédé Nocolok, la couche de liaison fond et se mélange avec la surface contre laquelle elle est en appui, pour ne former qu’une unique structure, assurant la liaison mécanique et l’étanchéité entre les deux surfaces soudées. Ainsi, le boîtier et la bride d’accostage, qui sont tous deux dotés de cette couche de liaison, sont soudés lors du passage dans un four de brasage Nocolok. S’en suit alors une étape de refroidissement qui permet de solidifier les pièces ainsi liées. In addition to avoiding the additional expenses mentioned above, this type of forming makes it possible to obtain a better dimensional accuracy of the part. Thus, the docking flange has a more complex shape for fixing the housing against the internal combustion engine, while having a mechanical and thermal resistance at least as good as with the solution of the prior art. In addition, the stamped docking flange has the advantage of being secured to the housing via a method called Nocolok brazing. This process consists of brazing without adding material. Indeed, the material forming the embossed docking flange comprises at least two layers: a core of raw material and a bonding layer for mechanically connecting the docking flange to the housing. This tie layer is characterized by its melting temperature, about 550 ° C, which is lower than the melting temperature of the docking flange core. Thus, during Nocolok brazing, the bonding layer melts and mixes with the surface against which it is supported, to form a single structure, ensuring the mechanical connection and sealing between the two welded surfaces. Thus, the housing and the docking flange, both of which are provided with this bonding layer, are welded when passing through a Nocolok brazing furnace. Then follows a cooling step that solidifies the parts thus linked.
En outre, le temps de fabrication d’une pièce emboutie est nettement inférieur à celui d’une pièce moulée et la cadence de production des pièces embouties est plus importante que celle des pièces moulées. In addition, the manufacturing time of a stamped part is significantly lower than that of a molded part and the rate of production of the stamped parts is greater than that of the molded parts.
Le corps de faisceau est un faisceau d’échange de chaleur entre le flux d’air d’admission et un fluide caloporteur. Flux d’air d’admission et fluide caloporteur, notamment un liquide caloporteur, traversent tout deux le corps de faisceau. The beam body is a heat exchange bundle between the intake air flow and a heat transfer fluid. Intake air flow and heat transfer fluid, including a coolant, both pass through the beam body.
Selon une caractéristique, la bride d’accostage comprend un bord replié contre lequel le boîtier est en appui. Le bord replié offre ainsi une surface de contact garantissant une bonne zone de liaison et une bonne étanchéité. According to one characteristic, the docking flange comprises a folded edge against which the housing is supported. The folded edge thus provides a contact surface ensuring a good connection area and a good seal.
Selon une caractéristique, le boîtier est en appui contre une face interne du bord replié. Le bord replié forme ainsi une ceinture de maintien du boîtier, en venant entourer ce dernier. According to one characteristic, the housing bears against an inner face of the folded edge. The folded edge thus forms a seat belt of the housing, surrounding the latter.
On entend ici par face interne, la face du bord replié qui est au contact du boîtier, c’est-à- dire, la face contre laquelle le boîtier repose et est soudé après brasage par procédé Nocolok. The term "internal face" here refers to the face of the folded edge which is in contact with the housing, that is to say the face against which the housing rests and is welded after brazing by the Nocolok process.
Le pli de la matière première étant rendu possible par l’opération d’emboutissage, ce bord replié présente l’avantage d’augmenter la surface de contact entre le boîtier et la bride d’accostage, augmentant par la même occasion la zone de contact et par conséquent la capacité de brasage du boîtier à la bride d’accostage. Par ailleurs, ce bord replié offre un espace de maintien du boîtier contre la bride d’accostage visible à l’œil nu, ce qui facilite sa vérification. The fold of the raw material being made possible by the drawing operation, this folded edge has the advantage of increasing the contact area between the housing and the docking flange, thereby increasing the contact area. and therefore the brazing ability of the housing to the docking flange. Moreover, this folded edge provides a housing holding space against the docking flange visible to the naked eye, which facilitates its verification.
Selon une caractéristique, le bord replié comprend au moins une butée contre laquelle le boîtier prend appui. Les butées, qui résultent d’une déformation de la surface de la bride d’accostage, sont aisément réalisables sur une pièce emboutie, comme c’est le cas de la bride d’accostage selon l’invention. L’introduction du boîtier dans la bride d’accostage est limitée en une extrémité par ces butées, garantissant ainsi un positionnement du boîtier dans la bride d’accostage qui ne nécessite pas de moyens additionnels pour assurer leur position l’un par rapport à l’autre. On garantit ainsi par un moyen simple le respect d’une dimension essentielle du dispositif de refroidissement selon l’invention. According to one feature, the folded edge comprises at least one stop against which the housing bears. The stops, which result from a deformation of the surface of the docking flange, are easily achievable on a stamped part, as is the case of the docking flange according to the invention. The introduction of the housing into the docking flange is limited at one end by these stops, thus ensuring a positioning of the housing in the docking flange which does not require additional means to ensure their position relative to the 'other. This guarantees a simple way the respect of an essential dimension of the cooling device according to the invention.
Selon une caractéristique, le corps de faisceau comprend au moins un couple de plaques entre lesquelles un fluide caloporteur peut circuler. De manière avantageuse, le corps de faisceau est configuré pour être parcouru de manière étanche par un liquide caloporteur. According to one characteristic, the beam body comprises at least one pair of plates between which a heat transfer fluid can circulate. Advantageously, the beam body is configured to be traversed in a sealed manner by a coolant liquid.
Selon une caractéristique, le corps de faisceau comprend au moins un couple de dispositifs de dissipation disposé de part et d’autre du couple de plaques. According to one characteristic, the beam body comprises at least one pair of dissipation devices disposed on either side of the pair of plates.
En effet, le corps de faisceau, qui est traversé par le flux d’air d’admission, comprend au moins un couple de plaques de forme parallélépipédique, par exemple rectangulaire, entre lesquels circule au moins un flux de fluide caloporteur. Les dispositifs de dissipation, de forme parallélépipédique, sont placés de part et d’autre du couple de plaques. De cette manière, un dispositif de dissipation se trouve adjacent à une plaque et un transfert de chaleur se produit entre le flux d’air d’admission, qui lèche les dispositifs de dissipation, et le flux de fluide caloporteur qui évolue entre les deux plaques d’un couple de plaques. Indeed, the beam body, which is traversed by the intake air flow, comprises at least a pair of rectangular parallelepiped shaped plates, for example rectangular, between which circulates at least one heat transfer fluid flow. The dissipation devices, of parallelepipedal shape, are placed on either side of the pair of plates. In this way, a dissipation device is located adjacent to a plate and a heat transfer occurs between the intake air stream, which licks the dissipation devices, and the coolant flow that evolves between the two plates. a couple of plates.
Selon une caractéristique, la bride d’accostage comprend au moins un bord d’accostage pourvu de moyens de fixation configurés pour solidariser la bride d’accostage au moteur à combustion interne. According to one characteristic, the docking flange comprises at least one docking edge provided with fastening means configured to secure the docking flange to the internal combustion engine.
A titre d’exemple, les moyens de fixation peuvent être des orifices permettant l’insertion de vis assurant la fixation de la bride d’accostage sur le moteur à combustion interne. By way of example, the fixing means may be orifices enabling the insertion of screws ensuring the attachment of the docking flange on the internal combustion engine.
Selon une caractéristique, le boîtier comprend au moins quatre flancs entourant le corps de faisceau, au moins un des flancs comprenant au moins un bord courbé qui se superpose au moins en partie sur un flanc adjacent. Avant solidarisation du dispositif de refroidissement, ces flancs sont des pièces distinctes les unes des autres. Après solidarisation, ces pièces forment le boîtier. According to one characteristic, the housing comprises at least four sidewalls surrounding the beam body, at least one of the sidewalls comprising at least one curved edge which is superimposed at least in part on an adjacent sidewall. Before joining the cooling device, these flanks are separate parts from each other. After joining, these parts form the housing.
Cet bord courbé d’un flanc, permettant la superposition d’un premier flanc sur un autre flanc, est obtenue par emboutissage d’une plaque. Ainsi, la superposition du bord courbé du premier flanc sur un autre flanc augmente la surface de contact, ce qui améliore la soudure entre les deux flancs superposés et améliore finalement l’étanchéité du boîtier. De la même manière qu’énoncé précédemment, la soudure est effectuée par brasage selon le procédé Nocolok, lors d’une étape simultanée à l’étape de brasage de la bride d’accostage emboutie et du boîtier. This curved edge of a flank, allowing the superposition of a first flank on another side, is obtained by stamping a plate. Thus, the superposition of the curved edge of the first sidewall on another side increases the contact surface, which improves the welding between the two superimposed sides and finally improves the sealing of the housing. In the same way as stated above, the soldering is carried out by brazing according to the Nocolok process, during a step simultaneous with the brazing step of the stamped docking flange and the housing.
Selon une caractéristique, le dispositif de refroidissement comprend une bride de maintien du boîtier, solidarisée au boîtier à l’opposé de la bride d’accostage par rapport au corps de faisceau. According to one characteristic, the cooling device comprises a housing holding flange, secured to the housing opposite the docking flange relative to the beam body.
Cette bride de maintien permet de maintenir les flancs du boîtier en place avant l’opération de brasage. Cette bride maintien forme également une zone d’accostage pour une conduite qui canalise le flux d’admission en provenance du turbocompresseur. This holding flange keeps the housing flanks in place before the soldering operation. This holding flange also forms a docking zone for a pipe that channels the intake flow from the turbocharger.
Selon un procédé de fabrication du dispositif de refroidissement d’un air d’admission, il est prévu au moins : According to a method of manufacturing the cooling device of an intake air, at least:
-une étape d’assemblage d’un corps de faisceau, a step of assembling a beam body,
-une étape de positionnement du corps de faisceau dans un boîtier, a step of positioning the beam body in a housing,
-une étape de positionnement d’une bride d’accostage emboutie à une première extrémité du boîtier, a step of positioning a docking flange embossed at a first end of the casing,
-une étape de positionnement d’une bride de maintien à une deuxième extrémité du boîtier, la deuxième extrémité étant opposée à la première extrémité par rapport au boîtier, et a step of positioning a holding flange at a second end of the housing, the second end being opposite the first end relative to the housing, and
-une étape de brasage simultanée au moins du boîtier, de la bride d’accostage et du corps de faisceau. a simultaneous soldering step at least of the housing, the docking flange and the beam body.
Avantageusement, l’étape de brasage permet de relier en une opération le corps de faisceau, le boîtier, la bride d’accostage et la bride de maintien. L’étape de brasage est réalisée par un procédé Nocolok. Advantageously, the brazing step allows to connect in one operation the beam body, the housing, the docking flange and the holding flange. The brazing step is carried out by a Nocolok process.
D'autres caractéristiques, détails et avantages de l'invention ressortiront plus clairement à la lecture de la description donnée ci-après à titre indicatif en relation avec des dessins dans lesquels Other characteristics, details and advantages of the invention will emerge more clearly on reading the description given below as an indication in relation to drawings in which
- la figure 1 est une vue en perspective avant du dispositif de refroidissement d’un air d’admission de moteur à combustion interne selon l’invention, FIG. 1 is a front perspective view of the cooling device of an intake air of an internal combustion engine according to the invention,
- la figure 2 est une vue en perspective de la bride d’accostage exploité dans le dispositif de refroidissement objet de l’invention, FIG. 2 is a perspective view of the docking flange operated in the cooling device which is the subject of the invention;
- la figure 3 est une vue en perspective arrière du dispositif de refroidissement d’un air d’admission selon l’invention. - Figure 3 is a rear perspective view of the cooling device of an intake air according to the invention.
Il faut tout d’abord noter que les figures exposent l’invention de manière détaillée pour mettre en œuvre l’invention, lesdites figures pouvant bien entendu servir à mieux définir l’invention le cas échéant. It should first be noted that the figures show the invention in detail for implement the invention, said figures can of course be used to better define the invention where appropriate.
Sur les différentes figures, les éléments identiques portent les mêmes numéros de référence. In the different figures, the identical elements bear the same reference numbers.
La figure 1 représente une vue générale, en perspective, du dispositif de refroidissement 1 d’un air d’admission de moteur à combustion interne. Un tel dispositif de refroidissement 1 comprend un boîtier 2, un corps de faisceau 3 et une bride d’accostage 4, assemblés les uns aux autres simultanément au cours d’une étape de brasage selon un procédé Nocolok. FIG. 1 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine. Such a cooling device 1 comprises a housing 2, a beam body 3 and a docking flange 4, assembled to each other simultaneously during a brazing step according to a Nocolok method.
Le boîtier 2 comprend quatre flancs 21, parallèles deux à deux, permettant de former un boîtier 2 de forme parallélépipédique, voire cubique. Le boîtier 2 délimite une surface d’entrée 22 et une surface de sortie 23 parallèles entre elles, permettant à un flux d’air d’admission de traverser le boîtier 2 dans son intégralité, c’est-à-dire de part en part. The housing 2 comprises four flanks 21, parallel in pairs, for forming a housing 2 of parallelepipedal shape, or cubic. The housing 2 defines an inlet surface 22 and an outlet surface 23 parallel to each other, allowing an intake air flow to pass through the housing 2 in its entirety, that is to say from one side to the other .
A l’intérieur du boîtier 2 se trouve le corps de faisceau 3. Le corps de faisceau 3 est constitué d’un empilement de plaques 31 et de dispositifs de dissipation 32. L’empilement de compose de la manière suivante : une alternance d’un couple de plaques 31 et d’un dispositif de dissipation 32. Entre les deux plaques 31 du couple de plaques, un flux de fluide caloporteur circule parallèlement à ces dernières. De plus, un couple de dispositifs de dissipation 32 est disposé de part et d’autre des plaques 31, encadrant ces dernières. Inside the casing 2 is the beam body 3. The beam body 3 consists of a stack of plates 31 and dissipation devices 32. The stack consists of the following: an alternation of a pair of plates 31 and a dissipation device 32. Between the two plates 31 of the pair of plates, a heat transfer fluid flow circulates parallel thereto. In addition, a pair of dissipation devices 32 is disposed on either side of the plates 31, flanking them.
Cette organisation est, par la suite répétée, suivant un axe perpendiculaire aux plaques 31, jusqu’à remplir le boîtier 2 dans son intégralité. This organization is subsequently repeated along an axis perpendicular to the plates 31, to fill the housing 2 in its entirety.
Le flux d’air d’admission traversant le boîtier 2 passe au travers des dispositifs de dissipation 32, ces derniers pouvant prendre la forme d’ailettes ou d’intercalaires. Ainsi, un échange de chaleur s’effectue entre le fluide caloporteur qui circule entre les deux plaques 31 et le flux d’air d’admission qui circule à l’extérieur des deux plaques 31. La surface d’échange de chaleur est augmentée au moyen des dispositifs de dissipation 32. The flow of intake air passing through the housing 2 passes through the dissipating devices 32, the latter may take the form of fins or spacers. Thus, a heat exchange takes place between the coolant flowing between the two plates 31 and the flow of intake air flowing outside the two plates 31. The heat exchange surface is increased at means of dissipation devices 32.
La bride d’accostage 4 est placée au niveau de la surface de sortie 23 du boîtier 2. A l’image d’un anneau, la bride d’accostage 4 entoure le boîtier 2 qui repose contre un bord replié 41 de la bride d’accostage 4. Un tel bord replié 41 résulte d’un pliage à angle droit d’une partie intérieure de la bride d’accostage 4boîtier. Le boîtier 2 est inséré à l’intérieur de la bride d’accostage 4 jusqu’à être bloqué contre des butées 42 qui sont ménagées sur le bord replié 4L Une butée 42 prend la forme d’une languette, réalisée par une découpe ou une déformation du bord replié 41, et qui émerge vers l’intérieur de la bride d’accostage 4. Un bord libre de cette butée 42 forme une face d’appui contre laquelle le boîtier 2 est mis en contact, lors du pré-assemblage du dispositif de refroidissement 1 selon l’invention. De cette manière, le boîtier 2 est encastré dans la bride d’accostage 4. The docking flange 4 is placed at the exit surface 23 of the casing 2. Like a ring, the docking flange 4 surrounds the casing 2 which rests against a folded edge 41 of the casing flange. 4. Such a folded edge 41 results from a right angle bend of an inner part of the docking flange 4 housing. The casing 2 is inserted inside the docking flange 4 until it is locked against abutments 42 which are formed on the folded edge 4L. A stop 42 takes the form of a tongue made by cutting or deformation of the folded edge 41, which emerges towards the inside of the docking flange 4. A free edge of this stop 42 forms a bearing face against which the housing 2 is brought into contact, during the pre-assembly of the cooling device 1 according to the invention. In this way, the housing 2 is embedded in the docking flange 4.
Par la suite, un brasage est effectué entre le boîtier 2 et le bride d’accostage 4, au niveau du bord replié 41. En effet, la face interne 411 du bord replié 41 de la bride d’accostage 4 est soudée aux quatre flancs 21 du boîtier 2 par brasage selon le procédé Nocolok, assurant une bonne tenue mécanique du boîtier 2 contre la bride d’accostage 4. Subsequently, brazing is performed between the housing 2 and the docking flange 4, at the folded edge 41. Indeed, the inner face 411 of the folded edge 41 of the docking flange 4 is welded to the four flanks 21 of the housing 2 by brazing according to the Nocolok process, ensuring good mechanical strength of the housing 2 against the docking flange 4.
De plus, la bride d’accostage 4 comprend un bord d’accostage 43 sur lequel des moyens de fixation 44 sont présents pour permettre la fixation de la bride d’accostage 4 contre le moteur à combustion interne. Les moyens de fixation 44 sont des orifices permettant l’insertion, par exemple, d’une vis qui, une fois serrée, maintient la bride d’accostage 4 contre le moteur à combustion interne. Afin de fiabiliser le serrage de la bride d’accostage 4 contre le moteur à combustion interne, les moyens de fixation 44 sont répartis sur le bord d’accostage, tout autour du boîtier 2. In addition, the docking flange 4 comprises a docking edge 43 on which fixing means 44 are present to allow the attachment of the docking flange 4 against the internal combustion engine. The fastening means 44 are orifices allowing insertion, for example, of a screw which, once tightened, keeps the docking flange 4 against the internal combustion engine. In order to make reliable the tightening of the docking flange 4 against the internal combustion engine, the fastening means 44 are distributed on the docking edge all around the casing 2.
Afin de supporter les importants efforts mécaniques engendrés par le serrage du dispositif de refroidissement 1 contre une face du moteur à combustion interne, un renfort périphérique 45 est réalisé sur la bride d’accostage 4, lors de l’opération d’emboutissage. Ce renfort périphérique 45 prend la forme d’un pliage à angle droit de la partie périphérique extérieure de la bride d’accostage 4. De cette manière, la bride d’accostage 4 présente une section en forme de « U », observée suivant une coupe perpendiculaire de la bride d’accostage 4 et traversant cette dernière. La présence d’un tel renfort périphérique 45 augmente significativement la résistance mécanique de la bride d’accostage 4. In order to withstand the large mechanical forces generated by the clamping of the cooling device 1 against a face of the internal combustion engine, a peripheral reinforcement 45 is formed on the docking flange 4 during the stamping operation. This peripheral reinforcement 45 takes the form of a right-angled folding of the outer peripheral part of the docking flange 4. In this way, the docking flange 4 has a "U" -shaped section, observed in accordance with a perpendicular section of the docking flange 4 and passing therethrough. The presence of such a peripheral reinforcement 45 significantly increases the mechanical strength of the docking flange 4.
La bride d’accostage 4 comprend également des oreilles où sont disposés les moyens de fixation 44. Il s’agit d’un élargissement localisé du bord d’accostage 43 qui offre la possibilité d’y disposer un écrou et une rondelle. The docking flange 4 also comprises ears where the fastening means 44 are arranged. This is a localized widening of the docking edge 43 which offers the possibility of disposing a nut and a washer therein.
On constate que la bride d’accostage 4 est emboutie en raison des arrondis et congés qu’elle comporte à la frontière entre le bord replié 41 et le bord d’accostage 43, par exemple, ou entre le bord d’accostage 43 et le renfort périphérique 45. It can be seen that the docking flange 4 is stamped because of the rounding and filleting it comprises at the border between the folded edge 41 and the docking edge 43, for example, or between the docking edge 43 and the peripheral reinforcement 45.
La figure 2 représente une vue de travers de la bride d’accostage 4 selon le côté accueillant le boîtier. Figure 2 shows a cross-sectional view of the docking flange 4 according to the side accommodating the housing.
La bride d’accostage 4 comprend en son centre un espace ouvert 46 de surface équivalente à la surface de sortie du boîtier, permettant ainsi l’insertion de ce dernier dans la bride d’accostage 4. Les butées 42, issues du bord replié 41, agissent comme limite à l’insertion du boîtier dans la bride d’accostage 4.Une fois le boîtier inséré jusqu’aux butées 42, ses flancs reposent contre le bord replié 41 de sorte à créer une surface de contact 47 entre le boîtier et la bride d’accostage 4. Dans une étape postérieure, une liaison mécanique par brassage selon le procédé Nocolok est mise en œuvre au niveau de cette surface de contact 47, afin de lier mécaniquement le boîtier à la bride d’accostage 4. The docking flange 4 comprises at its center an open space 46 of surface equivalent to the exit surface of the housing, thus allowing the latter to be inserted into the docking flange 4. The stops 42, coming from the folded edge 41 , act as a limit to the insertion of the housing into the docking flange 4. Once the housing is inserted to the stops 42, its flanks rest against the folded edge 41 so as to create a contact surface 47 between the housing and the docking flange 4. In a later step, a mechanical stirring link according to the Nocolok process is implemented at this contact surface 47, in order to mechanically link the housing to the docking flange 4.
Le bord d’accostage 43 est muni de moyens de fixation 44. A titre d’exemple, ces moyens de fixation 44 peuvent être des orifices permettant l’insertion de moyen d’ancrage de la bride d’accostage 4 contre le moteur à combustion interne. A l’inverse de la précédente opération de liaison entre le boîtier 2 et la bride d’accostage 4, cette dernière est fixée contre le moteur à combustion interne par une action mécanique compressive telle que, par exemple, l’utilisation de vis et d’écrous. The docking edge 43 is provided with fastening means 44. By way of example, these fastening means 44 may be orifices allowing the insertion of anchoring means of the docking flange 4 against the combustion engine. internal. Unlike the previous connection operation between the housing 2 and the docking flange 4, the latter is fixed against the internal combustion engine by a mechanical compressive action such as, for example, the use of screws and d nuts.
De plus, les contraintes thermiques imposées par le moteur à combustion interne sur la bride d’accostage 4 sont élevées. Celles-ci génèrent une dilatation importante de la bride d’accostage 4. C’est pourquoi la bride d’accostage 4 comprend le renfort périphérique 45 placé à la périphérie externe de la bride d’accostage 4. Ce renfort périphérique 45 consiste en un pli perpendiculaire d’un bord d’accostage 43 de la bride d’accostage 4, un tel pli étant réalisé dans le même sens que le bord replié 41 de la bride d’accostage 4. De cette manière, la bride d’accostage 4, prenant la forme d’un « U », comprend deux angles droits 48 qui ont pour caractéristique majeure d’être hautement résistant à la déformation mécanique et thermique. In addition, the thermal stresses imposed by the internal combustion engine on the docking flange 4 are high. These cause significant expansion of the docking flange 4. This is why the docking flange 4 comprises the peripheral reinforcement 45 placed at the outer periphery of the docking flange 4. This peripheral reinforcement 45 consists of a perpendicular fold of a docking edge 43 of the docking flange 4, such a fold being made in the same direction as the folded edge 41 of the docking flange 4. In this way, the docking flange 4 , taking the form of a "U", comprises two right angles 48 which have the major characteristic of being highly resistant to mechanical and thermal deformation.
La bride d’accostage 4 est emboutie. Cette bride d’accostage 4 est le résultat d’une déformation d’une tôle plate opérée par un poinçon reçu dans une empreinte, poinçon et empreinte étant constitutifs d’une presse d’emboutissage. The docking flange 4 is stamped. This docking flange 4 is the result of a deformation of a flat sheet operated by a punch received in a cavity, punch and cavity being a constituent of a stamping press.
La figure 3 représente une vue générale de l’arrière du dispositif de refroidissement 1 d’un air d’admission. On entend ici, arrière par rapport à la figure 1, présentant une vue de l’avant du dispositif de refroidissement 1. Figure 3 shows a general view of the rear of the cooling device 1 of an intake air. Here is meant, rear with respect to Figure 1, having a view of the front of the cooling device 1.
En arrière-plan, il est représenté l’insertion du boîtier 2 à l’intérieur de la bride d’accostage 4, avec la présence de la surface de contact 47 entre le bord replié 41 de la bride d’accostage 4 et une partie des flancs 21 du boîtier 2. In the background, it is shown the insertion of the housing 2 inside the docking flange 4, with the presence of the contact surface 47 between the folded edge 41 of the docking flange 4 and a part flanks 21 of the housing 2.
La figure 3 illustre une face arrière du bord d’accostage 43. FIG. 3 illustrates a rear face of the docking edge 43.
Au niveau du bord d’accostage 43, les moyens de fixation 44 permettent la fixation de la bride d’accostage 4 au moteur à combustion interne, en particulier sur la culasse de ce dernier. A la périphérie du bord d’accostage 43, un pli est effectuée, créant ainsi le renfort périphérique 45. Ce renfort, orienté dans le même sens que le bord replié 41, rend la bride d’accostage plus résistante aux efforts mécaniques imposés par le dispositif de refroidissement 1 en tant que tel, et pas son montage sur le moteur à combustion interne. Au premier plan, la surface d’entrée 22 du boîtier 2 forme la bouche par laquelle le flux d’air d’admission entre à l’intérieur du boîtier 2, pour y subir un échange de chaleur avec le liquide caloporteur qui circule dans le corps de faisceau 3. L’échange de chaleur est augmenté grâce à la présence des dispositifs de dissipation 32 qui sont traversés par le flux d’air d’admission. Ces dispositifs de dissipation 32 captent les calories présentent dans le flux d’air d’admission et les transmettent aux plaques 31, et donc au liquide caloporteur qui circule entre celles-ci. L’empilement successif de cette organisation compose le corps de faisceau 3. At the docking edge 43, the fastening means 44 allow the attachment of the docking flange 4 to the internal combustion engine, in particular on the cylinder head of the latter. At the periphery of the docking edge 43, a fold is made, thereby creating the peripheral reinforcement 45. This reinforcement, oriented in the same direction as the folded edge 41, makes the docking flange more resistant to the mechanical forces imposed by the cooling device 1 as such, and not its mounting on the internal combustion engine. In the foreground, the inlet surface 22 of the casing 2 forms the mouth through which the flow of intake air enters inside the casing 2, in order to undergo a heat exchange with the heat transfer liquid circulating in the casing 2. beam body 3. The heat exchange is increased thanks to the presence of dissipation devices 32 which are traversed by the intake air flow. These dissipation devices 32 capture the calories present in the intake air flow and transmit them to the plates 31, and thus to the heat transfer fluid circulating therebetween. The successive stacking of this organization composes the beam body 3.
Le boîtier 2 enveloppe le corps de faisceau 3 par l’intermédiaire de quatre flancs 21, laissant ouverte la surface d’entrée 22, qui permet l’entrée du flux d’air d’admission, et la surface de sortie 23 qui permet la sortie de ce même flux d’air d’admission. The casing 2 envelops the beam body 3 via four flanks 21, leaving open the inlet surface 22, which allows entry of the intake air flow, and the outlet surface 23 which allows the output of this same flow of intake air.
Afin de fixer les flancs 21 entre eux, ces derniers sont munis, au niveau de leurs extrémités en contact avec les autres flancs 21, de bords courbés 24. Ces bords courbés 24 créent une large surface de liaison entre deux flancs 21 adjacents. Ainsi, il est possible de disposer de deux flancs longitudinaux 21 munis chacun de deux bords courbés 24 qui coopèrent avec des flancs latéraux 21 plats au niveau de leurs extrémités. Alternativement, chacun des quatre flancs 21 peut comprendre un unique bord courbé 24 associé au flanc 21 adjacent. In order to fix the flanks 21 between them, the latter are provided, at their ends in contact with the other sides 21, curved edges 24. These curved edges 24 create a large bonding surface between two flanks 21 adjacent. Thus, it is possible to have two longitudinal flanks 21 each provided with two curved edges 24 which cooperate with side flanks 21 flat at their ends. Alternatively, each of the four flanks 21 may comprise a single curved edge 24 associated with the adjacent flank 21.
Dans une étape postérieure, une soudure par brassage selon le procédé Nocolok est réalisée au niveau de cette surface de liaison entre les bords courbés 24 et les flancs recouverts par ces bords courbés 24, afin de lier mécaniquement les flancs 21 du boîtier 2 entre eux, rendant par la même occasion, le boîtier 2 complètement étanche au flux d’air d’admission qui circule dans le corps de faisceau 3. In a later step, a stirring weld according to the Nocolok process is carried out at this bonding surface between the curved edges 24 and the sides covered by these curved edges 24, in order to mechanically link the flanks 21 of the housing 2 with each other, making at the same time, the housing 2 completely sealed to the flow of intake air flowing in the beam body 3.
La figure 3 montre également une bride de maintien 25 dont une des fonctions est de maintenir ensemble les quatre flancs 21 en appui les uns contre les autres par l’intermédiaire d’encoches 26, placés sur le pourtour de la bride de maintien 25. Ce maintien sert notamment en phase de pré-assemblage, avant le passage au four de brasage prévu dans le cadre du procédé Nocolok. FIG. 3 also shows a holding flange 25, one of whose functions is to hold the four flanks 21 together against one another by means of notches 26, placed around the periphery of the holding flange 25. This maintenance is used especially in the pre-assembly phase, before the passage to the brazing furnace provided in the context of the Nocolok process.
Cette bride de maintien 25 assure donc la fixation des quatre flancs 21 entre eux, permettant l’étanchéité du boîtier 2. Cette bride de maintien 25 sert également de bord d’accostage pour la réception d’une conduite en provenance du circuit d’air d’admission This holding flange 25 thus ensures the fixing of the four flanks 21 between them, allowing the sealing of the housing 2. This holding flange 25 also serves as a docking edge for receiving a pipe from the air circuit admission
La bride de maintien 25 est pièce de forme complémentaire à la forme du boîtier 2. Vue en coupe, cette bride de maintien forme un « U » à l’intérieur duquel se loge chaque flanc 21 du boîtier 2. The holding flange 25 is a piece of complementary shape to the shape of the housing 2. In sectional view, this holding flange forms a "U" within which each flank 21 of the housing 2 is housed.
La bride de maintien 25 est disposée à l’opposé de la bride d’accostage 4, par rapport au boîtier 2 ou par rapport au corps de faisceau 3. La bride de maintien 25 s’étend donc dans le plan de la surface d’entrée 22 du flux d’air d’admission, tandis que la bride d’accostage emboutie 4 s’étend dans le plan de la surface de sortie 23 du flux d’air d’admission. La bride d’accostage emboutie 4 est ainsi disposée à une première extrémité du boîtier 2, le long d’une direction d’écoulement du flux d’air d’admission. La bride de maintien 25 est quant à elle disposée à une deuxième extrémité du boîtier 2, opposée à la première extrémité le long d’une direction d’écoulement du flux d’air d’admission. The holding flange 25 is disposed opposite the docking flange 4, with respect to the 2 of the housing or relative to the beam body 3. The holding flange 25 thus extends in the plane of the inlet surface 22 of the intake air flow, while the embossed docking flange 4 s' extends in the plane of the exit surface 23 of the intake air flow. The stamped docking flange 4 is thus disposed at a first end of the casing 2, along a direction of flow of the intake air stream. The holding flange 25 is in turn disposed at a second end of the housing 2, opposite the first end along a direction of flow of the intake air flow.
On comprend à la lecture de ce qui précède que la présente invention propose un organe de refroidissement d’un flux d’air admis dans un moteur thermique et qui traverse un faisceau d’échange de chaleur. Cet organe est destiné à être attaché à une culasse du moteur thermique par le biais d’une bride de fixation qui est réalisée par un procédé d’emboutissage, détectable par le fait que la bride comprend des zones de pliage et de déformations qui résultent de ce procédé d’emboutissage. L’invention trouve un avantage certain dans l’emploi d’une bride d’accostage emboutie car elle peut être associée aux autres pièces préassemblées du dispositif de refroidissement, préalablement à l’opération de brasage opérée dans un four d’un procédé Nocolok.  It is understood from the foregoing that the present invention provides a cooling member of a flow of air admitted into a heat engine and which passes through a heat exchange beam. This member is intended to be attached to a cylinder head of the heat engine by means of a fastening flange which is made by a stamping process, detectable in that the flange comprises bending and deformation zones which result from this process of stamping. The invention has a certain advantage in the use of a stamped docking flange as it can be associated with the other preassembled parts of the cooling device, prior to the brazing operation performed in a furnace of a Nocolok process.
L’invention ne saurait toutefois se limiter aux moyens et configurations décrits et illustrés ici, et elle s’étend également à tout moyen ou configuration équivalents et à toute combinaison technique opérant de tels moyens. En particulier, la forme de la bride d’accostage peut être modifiée sans nuire à l’invention, dans la mesure où le dispositif de refroidissement, in fine, remplit les mêmes fonctionnalités que celles décrites dans ce document.  The invention, however, can not be limited to the means and configurations described and illustrated here, and it also extends to any equivalent means or configuration and any technical combination operating such means. In particular, the shape of the docking flange can be modified without harming the invention, insofar as the cooling device, in fine, fulfills the same functionalities as those described in this document.

Claims

REVENDICATIONS
1. Dispositif de refroidissement (1) d’un air d’admission d’un moteur à combustion interne, le dispositif de refroidissement (1) comprenant un boîtier (2) à l’intérieur duquel est logé un corps de faisceau (3) se composant d’un empilement de plaques (31) et de dispositifs de dissipation (32), le dispositif de refroidissement (1) comprenant une bride d’accostage (4) configurée pour relier le boîtier (2) au moteur à combustion interne, caractérisé en ce que la bride d’accostage (4) est emboutie. 1. Cooling device (1) for an intake air of an internal combustion engine, the cooling device (1) comprising a housing (2) inside which is housed a beam body (3) consisting of a stack of plates (31) and dissipation devices (32), the cooling device (1) comprising a docking flange (4) configured to connect the housing (2) to the internal combustion engine, characterized in that the docking flange (4) is embossed.
2. Dispositif de refroidissement (1) d’un air d’admission selon la revendication précédente, caractérisé en ce que la bride d’accostage (4) comprend un bord replié (41) contre lequel le boîtier (2) est en appui. 2. Cooling device (1) for an intake air according to the preceding claim, characterized in that the docking flange (4) comprises a folded edge (41) against which the housing (2) is supported.
3. Dispositif de refroidissement (1) d’un air d’admission selon la revendication précédente, caractérisé en ce que le boîtier (2) est en appui contre une face interne (411) du bord replié (41). 3. Cooling device (1) of an intake air according to the preceding claim, characterized in that the housing (2) bears against an inner face (411) of the folded edge (41).
4. Dispositif de refroidissement (1) d’un air d’admission selon les revendications 2 ou 3, caractérisé en ce que le bord replié (41) comprend au moins une butée (42) contre laquelle le boîtier (2) prend appui. 4. Cooling device (1) of an intake air according to claims 2 or 3, characterized in that the folded edge (41) comprises at least one stop (42) against which the housing (2) bears.
5. Dispositif de refroidissement (1) d’un air d’admission selon l’une quelconque des revendications précédentes, caractérisé en ce que le corps de faisceau (3) comprend au moins un couple de plaques (31) entre lesquelles un fluide caloporteur peut circuler. 5. Cooling device (1) for an intake air according to any one of the preceding claims, characterized in that the beam body (3) comprises at least one pair of plates (31) between which a heat transfer fluid can circulate.
6. Dispositif de refroidissement (1) d’un air d’admission selon la revendication précédente, caractérisé en ce que le corps de faisceau (3) comprend au moins un couple de dispositifs de dissipation (32) disposés de part et d’autre du couple de plaques (31). 6. Cooling device (1) for an intake air according to the preceding claim, characterized in that the beam body (3) comprises at least one pair of dissipation devices (32) arranged on either side the pair of plates (31).
7. Dispositif de refroidissement (1) d’un air d’admission selon l’une quelconque des revendications précédentes, caractérisé en ce que la bride d’accostage (4) comprend au moins un bord d’accostage (43) pourvu de moyens de fixation (44) configurés pour solidariser la bride d’accostage (4) au moteur à combustion interne. Cooling device (1) for an intake air according to one of the preceding claims, characterized in that the docking flange (4) comprises at least one docking edge (43) provided with means fastening means (44) configured to secure the docking flange (4) to the internal combustion engine.
8. Dispositif de refroidissement (1) d’un air d’admission selon l’une quelconque des revendications précédentes, caractérisé en ce que le boîtier (2) comprend au moins quatre flancs (21) entourant le corps de faisceau (3), au moins un des flancs (21) comprenant au moins un bord courbé (24) qui se superpose au moins en partie sur un flanc (21) adjacent.  Cooling device (1) for an intake air according to one of the preceding claims, characterized in that the housing (2) comprises at least four sidewalls (21) surrounding the beam body (3), at least one of the flanks (21) comprising at least one curved edge (24) which is superimposed at least in part on an adjacent flank (21).
9. Dispositif de refroidissement (1) d’un air d’admission selon la revendication 1, caractérisé en ce qu’il comprend une bride de maintien (25) du boîtier (2) solidarisée au boîtier (2) à l’opposé de la bride d’accostage (4) par rapport au corps de faisceau (3). 9. Cooling device (1) of an intake air according to claim 1, characterized in that it comprises a holding flange (25) of the housing (2) secured to the housing (2) opposite the docking flange (4) with respect to the beam body (3).
10. Procédé de fabrication d’un dispositif de refroidissement (1) d’un air d’admission, comprenant au moins :  10. A method of manufacturing a cooling device (1) for an intake air, comprising at least:
-une étape d’assemblage d’un corps de faisceau (3),  a step of assembling a beam body (3),
-une étape de positionnement du corps de faisceau (3) dans un boîtier (2),  a step of positioning the beam body (3) in a housing (2),
-une étape de positionnement d’une bride d’accostage (4) emboutie à une première extrémité du boîtier (2),  a step of positioning a docking flange (4) embossed at a first end of the casing (2),
-une étape de positionnement d’une bride de maintien (25) à une deuxième extrémité du boîtier (2), la deuxième extrémité étant opposée à la première extrémité par rapport au boîtier (2),  a step of positioning a holding flange (25) at a second end of the casing (2), the second end being opposite the first end relative to the casing (2),
-une étape de brasage simultanée au moins du boîtier (2), de la bride d’accostage (4) et du corps de faisceau (3).  a simultaneous brazing step at least of the housing (2), the docking flange (4) and the beam body (3).
PCT/FR2019/050634 2018-03-23 2019-03-20 Intake air cooling device for an internal combustion engine WO2019180377A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1852524 2018-03-23
FR1852524A FR3079267B1 (en) 2018-03-23 2018-03-23 INTERNAL COMBUSTION ENGINE INTAKE AIR COOLING SYSTEM

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WO2019180377A1 true WO2019180377A1 (en) 2019-09-26

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WO (1) WO2019180377A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013001017A1 (en) * 2011-06-30 2013-01-03 Valeo Systemes Thermiques Stacked plate exchanger casing and exchanger comprising such a casing.
EP3088834A1 (en) * 2015-03-26 2016-11-02 Mahle International GmbH Heat exchanger
WO2017155802A1 (en) * 2016-03-07 2017-09-14 Modine Manufacturing Company Multifunctional base plate of a heat exchanger

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013001017A1 (en) * 2011-06-30 2013-01-03 Valeo Systemes Thermiques Stacked plate exchanger casing and exchanger comprising such a casing.
EP3088834A1 (en) * 2015-03-26 2016-11-02 Mahle International GmbH Heat exchanger
WO2017155802A1 (en) * 2016-03-07 2017-09-14 Modine Manufacturing Company Multifunctional base plate of a heat exchanger

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FR3079267A1 (en) 2019-09-27

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