WO2019180378A1 - 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
WO2019180378A1
WO2019180378A1 PCT/FR2019/050635 FR2019050635W WO2019180378A1 WO 2019180378 A1 WO2019180378 A1 WO 2019180378A1 FR 2019050635 W FR2019050635 W FR 2019050635W WO 2019180378 A1 WO2019180378 A1 WO 2019180378A1
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WO
WIPO (PCT)
Prior art keywords
docking flange
docking
housing
assembly member
cooling device
Prior art date
Application number
PCT/FR2019/050635
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 WO2019180378A1 publication Critical patent/WO2019180378A1/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
    • 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
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates

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 optimal operating conditions.
  • the cooling of a heat engine requires the use of a heat exchanger to cool this air and to increase the density of the air / fuel mixture.
  • 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 of the cooling device, the attachment mode thereof and the overhang that the docking flange can suffer.
  • the heat exchanger is placed not far from the combustion chambers where the temperature can reach 700 ° C.
  • the heat exchange bundle is also traversed by a cooling fluid which is at a temperature of the order of 50 ° C and by a flow of intake air whose temperature is commonly above 200 ° C. These temperatures are far apart and generate significant thermal stresses on the docking flange of the cooling device.
  • the assembly exposed above suffers from another disadvantage.
  • the use of the Nocolok process requires the use of a material covered with a melting layer which realizes the joining of the parts together, especially at the connection area.
  • This connection area is on one side of the docking interface which also serves as a joint plane, against which rests a seal disposed between the docking flange and the cylinder head.
  • the joint plane of the docking interface is thus covered by the melting layer which, once the Nocolok process has been implemented, generates asperities on the joint plane.
  • Such roughness requires the implementation of an additional step of surfacing, to bring the joint plane to the surface coefficient acceptable for the joint.
  • the present invention corrects the disadvantages mentioned above and 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 cooling device comprises an assembly member, the housing being at least partially interposed between the docking flange and the assembly member.
  • the invention moves the position of the connection zone between the housing and the docking flange, since the housing encircles the folded edge of the docking flange by the outside thereof .
  • This new arrangement allows the installation of the assembly member which compresses the housing against the folded edge, and therefore against the flange docking.
  • the sealing zone of the connection between the casing and the docking flange is improved by adding a compressive force which plates the casing on the docking flange before being secured by the Nocolok process.
  • connection area on an inner face of the docking flange it then becomes unnecessary to use a material that has a melting layer on each of these faces.
  • the outer face of the docking interface may be devoid of this layer of fusion, which eliminates any formation of asperity.
  • the docking flange thus comprises an inner face, which comprises the zone of connection with the casing, and an outer face which comprises the joint plane.
  • the inner face is the leading side of the folded edge of the docking flange against which the housing abuts and extends within a cavity of the docking flange.
  • the outer face is the face intended for the connection between the docking flange and the internal combustion engine, and which is opposite to the inner face relative to the constituent material of the docking flange.
  • the assembly member extends into a cavity delimited by the docking flange. In this way, the assembly member is in permanent contact with the housing which it holds against the docking flange.
  • the cavity is delimited by the internal face of the docking flange.
  • the cavity has a section "U" shape, viewed in a cross section of the docking flange.
  • the assembly member comprises a central section, a first lateral section and a second lateral section as well as a central section connecting the first lateral section to the second lateral section, the first lateral section, the central section and the second lateral section being shaped in "U".
  • the assembly member is thus composed of at least three sections, each extending section disposed substantially at right angles to the immediately adjacent section, viewed in a cross section of the assembly member.
  • the assembly member thus has a U-shape, seen according to this section.
  • the assembly member takes the form of the docking flange.
  • the assembly member is thus housed in the cavity of the docking flange and thus has a profile similar to the profile of the docking flange, seen in section.
  • a dimension of the assembly member, measured between the first lateral section and the second lateral section, is greater than a dimension measured between the housing and a peripheral reinforcement constituting the docking member. Effective plating of the casing against the folded edge is guaranteed.
  • a central section of the assembly member is arranged between two lateral sections, seen in cross-section.
  • the docking flange comprises on its side a flat portion and two folded edges formed on each side of the flat portion.
  • the flat portion and the folded edges delimit the cavity.
  • a dimension of the central section of the assembly member is greater than a dimension of the flat portion deduced from a thickness of the housing, measured in the same plane and along the same direction.
  • a thickness of the assembly member is less than a thickness of the docking flange.
  • the assembly member is thus more flexible and can be deformed to become housed in the cavity of the docking flange, while the docking flange is of a thickness that allows it to withstand the stress of compression generated by the housing in response to the support operated by the assembly member.
  • the assembly member and the docking flange has a similar profile, seen in a cross section at the assembly member and the docking flange.
  • the assembly member thus has a general shape complementary to the shape of the docking flange. It is for this reason that the assembly member can be housed in the docking flange.
  • the assembly member thus has a complementarity of section with the section of the docking flange, seen in a plane perpendicular to the docking flange and the assembly member, and which cuts the docking flange. and the assembly member.
  • the docking flange and the assembly member have a similar shape, seen in a plane in which extends mainly the docking flange. Indeed, whatever the embodiment of the assembly member, it has a rectangular shape when the docking flange has a rectangular shape.
  • the docking flange comprises a folded edge and a peripheral reinforcement connected to one another by a docking edge, the assembly member being in contact with the docking edge of the flange. docking.
  • the docking edge is the area of the docking flange against which a seal is arranged to seal the link between the cooling device according to the invention and the internal combustion engine which carries it.
  • the docking flange comprises at least one fastening means and the assembly member comprises at least one orifice superimposed on at least one fastening means of the docking flange. Thanks to the presence of these holes superimposed on the fastening means of the docking flange, the installation of the assembly member does not interfere with the connection of the docking flange against the internal combustion engine, which is an initial goal of the docking flange. Once secured by brazing, the assembly member becomes a mechanical reinforcement that maintains a good flatness of the docking flange.
  • the assembly member is composed of at least two distinct parts, comprising at least three branches that extend in the same plane, each branch forming an angle with respect to the immediately adjacent branch.
  • the assembly member is composed of two distinct parts, comprising only two branches which extend in the same plane, a main branch forming an angle with respect to the adjacent secondary branch.
  • the assembly member is composed of four distinct parts that have a straight profile. These are four bars that can easily be installed in the cavity of the docking flange.
  • the housing comprises at least one locking means against which the assembly member bears. The position of the assembly member against the housing is thus guaranteed, without the risk of accidentally escaping the assembly member.
  • the docking flange comprises at least one locking device against which the assembly member bears. The position of the assembly member against the docking flange is thus guaranteed, without the risk of accidentally escaping the assembly member.
  • an inner face of the housing is positioned against a folded edge of the docking flange, a second lateral section of the assembly member is blocked against the docking flange,
  • a force is exerted on the assembly member until a first lateral section compresses the casing against the folded edge.
  • the second lateral section is locked against the docking flange by bearing against at least one locking means of which the docking flange is provided.
  • the first lateral section is locked against the housing by bearing against at least one locking means whose housing is provided.
  • the cooling device of an intake air at least:
  • a step of clamping the housing against the docking flange by means of an assembly member advantageously the housing is clamped against an outer face of a folded edge of the docking flange
  • the soldering step makes it possible to connect in one operation the beam body, the housing, the docking flange and the assembly member.
  • the brazing step is carried out by Nocolok process.
  • FIG. 1 is a perspective view of the cooling device of an intake air of an internal combustion engine according to the prior art
  • FIG. 2 is a perspective view of the cooling device of an intake air of an internal combustion engine according to the invention
  • FIG. 3 is a perspective view of the assembly member operated in the cooling device that is the subject of the invention, according to one embodiment, FIG. 4 is a perspective view of the assembly member according to a second embodiment,
  • FIG. 5 is a perspective view of the assembly member according to another embodiment
  • FIG. 6 is a schematic view of the assembly method of the housing against the docking flange, by means of the connecting member according to any one of the embodiments.
  • the term “length” refers to the largest dimension of a component of the cooling device, "thickness” being the smallest dimension measured perpendicularly to the largest dimension, and "width” being the dimension of the component perpendicular to both times. its length and thickness.
  • the use in the following description of the internal or internal terms implies a positioning inwardly of the cooling device, in particular towards an axis passing in the center of the beam body of the cooling device.
  • the use in the following description of external or external terms implies positioning facing the external environment surrounding the cooling device.
  • FIG. 1 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine according to the prior art.
  • the cooling device 1 comprises a housing 2, a beam body 3 and a docking flange 4.
  • the housing 2 comprises four flanks 21, parallel in pairs, for forming the housing 2 parallelepipedal shape, or cubic.
  • the housing 2 delimits an inlet surface 22 and an outlet surface 23, parallel to each other, allowing a flow of intake air to enter and exit the housing 2, thus passing through the housing 2 in its entirety. that is to say, from one side to the other.
  • the beam body 3 is housed inside the casing 2 and consists of a stack of plates 31 and dissipation devices 32.
  • the stack consists of the following manner: an alternation of a pair of plates 31 and a device for dissipation 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. This organization is subsequently repeated along an axis perpendicular to a general plane of extension of the plates 31, to fill the housing 2 in its entirety, thus forming the beam body 3.
  • a dissipation device 32 takes the form of a fin or a spacer.
  • 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.
  • a docking flange 4 is placed at the outlet surface 23 of the casing 2.
  • the docking flange 4 surrounds the casing 2 which rests against the folded edge 41 of the docking flange 4.
  • the casing 2 is inserted inside the docking flange 4. In this way, the casing 2 is recessed on the docking flange 4.
  • the docking flange 4 further 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.
  • FIG. 2 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine according to the invention.
  • the cooling device 1 comprises a housing 2, a beam body 3, a docking flange 4.
  • the cooling device 1 also comprises an assembly member 5. Once pre-assembled, these components are simultaneously secured to one another during a brazing step according to a Nocolok process.
  • the housing 2 and the beam body 3 are made and organized identically to what has been described with respect to FIG. 1. Reference is therefore made to the description of FIG. 1 for their implementation.
  • the docking flange 4 comprises a folded edge 41, the docking edge 43 such that FIG. 1 and a peripheral reinforcement 45.
  • the folded edge 41, the docking edge 43 and the peripheral reinforcement 456 delimit a cavity 10 intended to receive at least one assembly member 5.
  • Such a folded edge 41 results from folding at right angles, or substantially at right angles, an inner band of the docking flange 4.
  • a peripheral reinforcement 45 is formed on the docking flange 4 during a stamping operation.
  • This peripheral reinforcement 45 takes the form of a fold substantially at right angles to an outer peripheral band of the docking flange 4.
  • the docking flange 4 has a section in the form of "U", observed in cross-section at the docking flange 4. The presence of such a peripheral reinforcement 45 significantly increases the mechanical strength of the docking flange 4, in particular when this is achieved by a step d stamping.
  • the docking flange 4 also comprises ears where the fixing means 44 are arranged. This is a localized widening of the docking edge 43 which offers the possibility of disposing of a screw or a nut and a washer. .
  • the docking flange 4 forms an open strapping at its center.
  • This docking flange 4 comprises, seen in cross-section, a central portion and two lateral portions formed by edges bent substantially at 90 ° with respect to a plane in which the central portion extends.
  • One of the side portions is the folded edge 41 of the docking flange 4, against which the housing 2 bears.
  • the other lateral portion is the peripheral reinforcement 45.
  • the central portion and the docking edge 43 is the central portion and the docking edge 43.
  • the docking flange 4 is placed at the outlet surface 23 of the casing 2.
  • the casing 2 surrounds the docking flange 4, coming to rest against the folded edge 41 of the docking flange 4.
  • the docking flange 4 is housed in the casing 2.
  • the docking flange 4 After insertion of the docking flange 4 in the casing 2, an outer face 411 of the folded edge 41 is in contact with an inner face 213 of the flanks 21 at a connection zone between the casing 2 and the flange of the casing. docking 4, this connection area forming a bonding strip between these two components.
  • the casing 2 is blocked on the docking flange 4 by a widening created by a rounding connecting the folded edge 41 to the docking edge 43 of the docking flange 4. In this way, the docking flange 4 is recessed in the housing 2.
  • 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 docking edge 43 is formed by the central portion of the docking flange, seen according to its cross section.
  • the docking edge 43 comprises a joint plane, that is to say a zone configured to seal with a seal. This seal is disposed between the docking flange 4 and the cylinder head of the internal combustion engine which receives the cooling device 1.
  • the docking flange 4 also comprises ears in the vicinity of which the fastening means 44 are arranged. It is a localized widening of the docking edge 43 and a deformation of the peripheral reinforcement 45 which offer the possibility of arrange a screw head or nut and washer.
  • an assembly member 5 is installed in the cooling device 1 so as to press the housing 2 against the docking flange 4, to the right of the connection zone.
  • This assembly member 5 makes it possible to clamp the housing 2 against the folded edge 41 when the cooling device 1 is in a pre-assembly state.
  • This assembly member 5 takes a shape complementary to the shape of the docking flange 4, that is to say, a "U" shape seen in cross-section to the assembly member 5.
  • the assembly member 5 comprises a central section 51 which rests against the docking edge 43 of the docking flange 4, and two lateral sections which rest, for a first lateral section 58 against an outer face 212 flanks 21 of the housing 2, and for a second lateral section 59, against the peripheral reinforcement 45 of the docking flange 4, in particular against the inner face of this peripheral reinforcement 45.
  • flanks 21 of the housing 2 envelop the outer face 411 of the folded edge 41, the first lateral section 58 of the assembly member 5 being in contact against the outer face 212 of the flanks 21 of the housing 2.
  • the assembly member 5 comprises orifices 57 superimposed on the fastening means 44 of the docking flange 4. In this way, the use of any connecting means, such as screws, nuts or other, will not be disturbed by the presence of the assembly member 5 when placed against the docking flange 4.
  • the assembly member 5 also constitutes a reinforcing element of the docking flange 4, by increasing the thickness of the part resulting from the joining of the assembly member 5 with the docking flange 4. This increases the torsional resistance of the docking flange 4, thereby reducing the number of fastening means 44.
  • the assembly member 5 is of generally rectangular shape. According to various embodiments which are detailed in FIGS. 3 to 5, the assembly member 5 is split up into several distinct pieces. These embodiments are intended to provide an assembly member 5 whose installation on the docking flange is facilitated.
  • FIG. 3 is a perspective view of the connecting member 5 operated in the cooling device 1, according to a first embodiment.
  • the latter consists of two separate parts 54.
  • Each separate part 54 comprises three branches 55 which extend in the same plane each leg 55 forming an angle 56, for example a right angle, with respect to the immediately adjacent leg 55.
  • Each separate piece 54 thus formed thus comprises a central branch at the ends of which two lateral branches extend in a direction perpendicular to a majority extension direction of the central branch.
  • each separate piece 54 forms a "U" where the central branch is of greater length than one and / or the other side branches.
  • each piece 54 takes the form of a "U" and thus comprises the central section 51 lined on one side by the first section 58 and the other by the second lateral section 59.
  • the two separate parts 54 forming the assembly member 5 are provided on their central section 51 with orifices 57 which, when the assembly member 5 is affixed against the docking flange 4, are superimposed on the fastening means of FIGS. the docking flange 4.
  • the assembly member 5 comprises only two separate parts 54 which are arranged opposite each other in the flat general plane.
  • the two separate parts 54 of this first embodiment are identical.
  • FIG. 4 is a perspective view of the assembly member 5 operated in the cooling device 1, according to a second embodiment. As presented in the previous mode, the assembly member 5, produced according to this mode, consists solely of two separate pieces 54.
  • Each separate part 54 comprises only two branches 55 which extend in the same plane, each branch 55 forming an angle 56, for example a right angle, with respect to the immediately adjacent branch 55.
  • Each separate piece 54 thus formed thus comprises a main branch at the end of which a secondary branch extends along a direction perpendicular to a majority extension direction of the main branch. Viewed in the flat general plane, each separate piece 54 forms an "L" where the main branch is of greater length than the secondary branch.
  • These separate parts 54 are instead installed head to tail opposite each other.
  • the two distinct pieces 54 are symmetrical to one another with respect to a plane of symmetry passing through two angles 56 opposite to each other with respect to the beam body.
  • Two spaces 53 are formed between each separate piece 54 and, in this second embodiment, these spaces 53 are made at the corners of the docking flange.
  • the assembly member 5 comprises a slot 60 formed at the angle 56 which connects the main branch to the secondary branch of the separate part 54.
  • This slot 60 is intended to allow some opening the angle 56, thus providing a positional flexibility between the main branch and the secondary branch to facilitate the installation of the separate part 54 on the docking flange.
  • such a slot 60 intersects the first lateral section 58 and the central section 51.
  • the slot 60 does not cut the second lateral section 59.
  • each distinct piece 54 seen in section, is identical to that described in the preceding figures. It is the same for the orifices 57 which are intended to be superimposed on the fastening means of the docking flange. Reference is made to the above description of these technical characteristics to implement them in the context of this second embodiment.
  • Figure 5 is a perspective view of the assembly member 5 operated in the cooling device 1, according to a third embodiment.
  • the assembly member 5 made in this mode consists strictly or at least four separate pieces 54.
  • Each separate piece 54 comprises a single branch 55 of rectilinear shape.
  • Each separate piece 54 is thus formed of four bars arranged all around the housing of the cooling device according to the invention.
  • each separate piece 54 is separated from the immediately adjacent separate piece by a space 53.
  • the assembly member 5 thus has four spaces 53 positioned at the angles 56 formed between the four separate pieces 54 forming the assembly member 5.
  • each distinct piece seen in section, is identical to that described in the preceding figures. It is the same for the orifices 57 which are intended to be superimposed on the fastening means of the docking flange. Reference is made to the above description of these technical characteristics to implement them in the context of this second embodiment.
  • FIG. 6 is a partial cross-sectional view of the docking flange 4, the casing 2 and the assembly member 5, illustrated during the assembly of the assembly member 5.
  • FIG. 6 shows that the peripheral reinforcement 45 comprises at least one locking device 47 intended to hold the assembly member 5 in place during its compression phase towards the docking flange 4.
  • the locking device 47 forms a foot support around which the assembly member 5 during its insertion tilts against the docking flange 4.
  • the locking device 47 takes the form of one or more tongues, made by cutting and / or deformation of the peripheral reinforcement 45.
  • the locking device 47 emerges from the inner face 46 of the docking interface 4, towards the folded edge 41 of the same docking flange 4.
  • This tongue which forms an embodiment of the locking device 47 has an edge 48 against which a first wafer 61 the assembly member 5 bears, when installed in the docking flange 4.
  • FIG. 6 also shows that the outer face 212 of the sidewalls 21 of the casing 2 is provided with at least one locking means 62 intended to hold the assembly member 5 in the cavity 10 of the docking flange 4, once compressed against the housing 2.
  • the locking means 62 takes the form of one or more buttresses that emerge from the outer face 212 of the flank 21 concerned, in the direction of the peripheral reinforcement 45.
  • the buttress is made by cutting and / or deformation of the flank 21 constituting the housing 2.
  • This buttress which forms an embodiment of the locking means 62 has a stop 63 against which a second wafer 64 the assembly member 5 bears, of to lock the position of the assembly member 5 which plates the housing 2 on the docking flange 4.
  • the use of the assembly member 5 ensures optimum retention of the housing 2 against the assembly flange 4. Indeed, the first lateral section 58, resting against the outer face 212 of the flanks 21 of the housing 2, is locked through the locking means 62 on the outer face 212 of the sides of the housing 2, while the second lateral section 59, resting against the peripheral reinforcement 45, is held against the latter through the devices 47. The assembly member 5 is thus locked on the docking flange 4, waiting for the soldering step according to the Nocolok process where these parts will be permanently secured.
  • the assembly member 5 is manufactured by stamping a sheet, for example aluminum or an aluminum alloy compatible with the material that constitutes the docking flange 4 and the housing 2.
  • a dimension L of the assembly member 5, measured between the first lateral section 58 and the second lateral section 59 of the assembly member 5 is greater than a dimension 1 measured between the outer face 212 of the flank 21 concerned and the peripheral reinforcement 45.
  • a thickness of the assembly member 5 is less than a thickness of the docking flange 4. This gives the flexibility required for the insertion of the assembly member 5 in the cavity 10 the docking flange 4.
  • the installation of the assembly member 5 is done after the insertion of the housing 2 on the docking flange 4.
  • the installation of the assembly member 5 is broken down into three successive stages represented by three referenced illustrations. (a), (b) and (c) of the figure
  • the first step comprises a positioning of the first portion 61 of the assembly member 5 against the edge 48 of the locking device 47.
  • the dimension L of the assembly member 5 being greater than the dimension 1 measured between housing 2 and peripheral reinforcement 45, the assembly member 5 is inclined relative to the plane in which extends mainly from the docking flange 4. A non-zero angle is thus formed between the central section 51 of the assembly member 5 and the docking edge 43 of the docking flange 4.
  • the second step, represented by the illustration (b) comprises a compressive action 7 which is exerted on the central section 51 of the assembly member 5 and particularly at the angle formed by the central section 51 and the first lateral section 58.
  • This compressive action 7 is oriented towards the docking flange 4 and aims to drive the central section 51 of the assembly member 5 towards the docking edge 43 of the docking flange 4. In doing so, a support is generated between an inner face 213 of the flank 21 and the inner face 46 of the docking flange 4 at the folded edge 41.
  • the connection zone 65 is the seat of this support.
  • the first lateral section 58 which is initially in unstable contact with the outer face 212 of the flanks 21 of the casing 2, slides along this outer face 212 to the placement of the central section 51 against the inner face 46 of the flange. 4, at the docking edge 43 thereof, as shown in the illustration referenced (c).
  • the maximum force is then generated between the housing 2 and the docking flange 4, at the connection zone 65, which ensures continuous contact over the entire periphery of the folded edge 41 prior to the soldering step, and thus continuous and leak-free brazing at the connection area 65.
  • a step of locking the assembly member 5 against the docking flange 4 is then implemented with the aid of the locking device 47 and the locking means 62 detailed above.
  • the present invention provides a cooling device of an intake air of an internal combustion engine configured to make its sealing more reliable.
  • This cooling device intended to be integrated in an intake air circuit and a heat transfer fluid circuit of a thermal vehicle, offers an easy solution to implement and at a lower cost to guarantee a contact between the housing and the flange. docking that ensures a perfect seal. This avoids the disposal of finished products, after they have undergone an expensive soldering step.
  • 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 connecting member and / or 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 comprising 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 cooling device comprises an assembly member, the housing being at least partially interposed between the docking flange and the assembly member.

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 thermique des conditions de fonctionnement optimales.  The automobile, like many other industries, uses heat exchangers to provide the engine with optimal operating conditions.
Le refroidissement d’un moteur thermique, et plus particulièrement de l’air d’admission provenant d’une sortie d’un compresseur, nécessite l’utilisation d’un échangeur de chaleur pour refroidir cet air et permettre d’augmenter la densité du mélange air / carburant.  The cooling of a heat engine, and more particularly the intake air coming from an outlet of a compressor, requires the use of a heat exchanger to cool this air and to increase the density of the air / fuel mixture.
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 contre le moteur à combustion interne, par l’intermédiaire d’une bride d’accostage qui relie le boîtier du dispositif de refroidissement à une culasse du moteur thermique.  It is known to fix the heat exchanger for cooling the intake air against the internal combustion engine, via a docking flange which connects the housing of the cooling device to a cylinder head of the engine thermal.
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 dispositif de refroidissement, du mode de fixation de celui-ci et du porte-à-faux que cette bride d’accostage peut subir.  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 of the cooling device, the attachment mode thereof and the overhang that the docking flange can suffer.
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 de chaleur est également traversé par un fluide de refroidissement qui lui est à une température de l’ordre de 50°C et par un flux d’air d’admission dont la température est couramment supérieure à 200°C. Ces 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 heat exchange bundle is also traversed by a cooling fluid which is at a temperature of the order of 50 ° C and by a flow of intake air whose temperature is commonly above 200 ° C. These temperatures are far apart and generate significant thermal stresses on the docking flange of the cooling device.
Il est connu de solidariser la bride d’accostage au boîtier par l’intermédiaire d’un brasage par le procédé Nocolok. Cette solidarisation, qui a pour objectif de braser simultanément un ensemble de pièces constitutives du dispositif de refroidissement, doit assurer une parfaite étanchéité entre le boîtier et la bride d’accostage étanche, au niveau d’une zone de connexion. It is known to secure the docking flange to the housing by means of brazing by the Nocolok process. This solidarity, which aims to braze simultaneously a set of components of the cooling device, must ensure a perfect seal between the housing and the sealed docking flange, at a connection area.
L’inconvénient d’un tel montage réside dans la difficulté à obtenir, de manière fiable et répétitive, une parfaite étanchéité entre le boîtier et la bride d’accostage au droit de la zone de connexion. Lorsque cette solidarisation n’est pas effective tout le long de la zone de connexion entre le boîtier et la bride d’accostage, un défaut d’étanchéité apparaît qui autorise une partie du flux d’air d’admission à s’échapper du circuit d’admission. Une telle situation est inacceptable et hautement préjudiciable car elle oblige à mettre au rebus un dispositif de refroidissement à l’état fini, après avoir été brasé selon le procédé Nocolok.  The disadvantage of such an assembly is the difficulty in obtaining, reliably and repeatedly, a perfect seal between the housing and the docking flange to the right of the connection area. When this connection is not effective all along the connection zone between the housing and the docking flange, a leakage fault appears which allows part of the intake air flow to escape the circuit intake. Such a situation is unacceptable and highly detrimental since it requires the disposal of a cooling device in the finished state, after having been brazed according to the Nocolok process.
Le montage exposé plus haut souffre d’un autre inconvénient. En effet, l’utilisation du procédé Nocolok impose l’emploi d’une matière couverte d’une couche de fusion qui réalise la solidarisation des pièces entre elles, notamment au niveau de la zone de connexion. Cette zone de connexion est sur une face de l’interface d’accostage qui sert également de plan de joint, contre lequel prend appui un joint disposé entre la bride d’accostage et la culasse. Le plan de joint de l’interface d’accostage est ainsi couvert de la couche de fusion qui, une fois le procédé Nocolok mis en œuvre, génère des aspérités sur le plan de joint. De tels aspérités nécessite la mise en œuvre d’une étape supplémentaire de surfaçage, pour ramener le plan de joint au coefficient de surface acceptable pour le joint.  The assembly exposed above suffers from another disadvantage. Indeed, the use of the Nocolok process requires the use of a material covered with a melting layer which realizes the joining of the parts together, especially at the connection area. This connection area is on one side of the docking interface which also serves as a joint plane, against which rests a seal disposed between the docking flange and the cylinder head. The joint plane of the docking interface is thus covered by the melting layer which, once the Nocolok process has been implemented, generates asperities on the joint plane. Such roughness requires the implementation of an additional step of surfacing, to bring the joint plane to the surface coefficient acceptable for the joint.
La présente invention corrige les inconvénients mentionnés ci-dessus et 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 le dispositif de refroidissement comprend un organe d’assemblage, le boîtier étant au moins en partie interposé entre la bride d’accostage et l’organe d’assemblage.  The present invention corrects the disadvantages mentioned above and 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 cooling device comprises an assembly member, the housing being at least partially interposed between the docking flange and the assembly member.
Le placement du boîtier entre la bride d’accostage et l’organe d’assemblage présente les avantages suivants :  The placement of the housing between the docking flange and the assembly member has the following advantages:
- comparé à l’art antérieur, l’invention déplace la position de la zone de connexion entre le boîtier et la bride d’accostage, puisque le boîtier encercle le bord plié de la bride d’accostage par l’extérieur de celui-ci. Cette nouvelle disposition permet l’installation de l’organe d’assemblage qui comprime le boîtier contre le bord plié, et donc contre la bride d’accostage. De cette manière, on améliore l’étanchéité de la zone de connexion entre le boîtier et la bride d’accostage en ajoutant une force de compression qui plaque le boîtier sur la bride d’accostage, avant solidarisation par le procédé Nocolok. Après solidarisation du boîtier et de la bride d’accostage, l’organe d’assemblage est lui-même solidarisé à ces derniers lors de la mise en œuvre du procédé Nocolok, - Compared with the prior art, the invention moves the position of the connection zone between the housing and the docking flange, since the housing encircles the folded edge of the docking flange by the outside thereof . This new arrangement allows the installation of the assembly member which compresses the housing against the folded edge, and therefore against the flange docking. In this way, the sealing zone of the connection between the casing and the docking flange is improved by adding a compressive force which plates the casing on the docking flange before being secured by the Nocolok process. After joining the housing and the docking flange, the assembly member is itself secured to the latter during the implementation of the Nocolok process,
- en déplaçant la zone de connexion sur une face interne de la bride d’accostage, il devient alors inutile d’utiliser une matière qui comporte une couche de fusion sur chacune de ces faces. La face externe de l’interface d’accostage peut être dépourvue de ce couche de fusion, ce qui supprime toute formation d’aspérité. La face externe de l’interface d’accostage, c’est-à-dire le plan de joint, ne nécessite donc pas de reprise d’usinage postérieure à la mise en œuvre du procédé Nocolok.  - By moving the connection area on an inner face of the docking flange, it then becomes unnecessary to use a material that has a melting layer on each of these faces. The outer face of the docking interface may be devoid of this layer of fusion, which eliminates any formation of asperity. The outer face of the docking interface, that is to say the joint plane, therefore does not require post-processing recovery after the implementation of the Nocolok process.
La bride d’accostage comprend ainsi une face interne, qui comprend la zone de connexion avec le boîtier, et une face externe qui comprend le plan de joint. La face interne est la face partant du bord plié de la bride d’accostage contre lequel le boîtier appui et s’étend à l’intérieur d’une cavité de la bride d’accostage. La face externe est la face destinée à la liaison entre la bride d’accostage et le moteur à combustion interne, et qui est opposée à la face interne par rapport à la matière constitutive de la bride d’accostage.  The docking flange thus comprises an inner face, which comprises the zone of connection with the casing, and an outer face which comprises the joint plane. The inner face is the leading side of the folded edge of the docking flange against which the housing abuts and extends within a cavity of the docking flange. The outer face is the face intended for the connection between the docking flange and the internal combustion engine, and which is opposite to the inner face relative to the constituent material of the docking flange.
Selon une caractéristique, l’organe d’assemblage s’étend dans une cavité délimitée par la bride d’accostage. De cette manière, l’organe d’assemblage est en contact permanent avec le boîtier qu’il maintient contre la bride d’accostage. La cavité est délimitée par la face interne de la bride d’accostage. La cavité présente une section forme de « U », vue selon une coupe transversale de la bride d’accostage.  According to one characteristic, the assembly member extends into a cavity delimited by the docking flange. In this way, the assembly member is in permanent contact with the housing which it holds against the docking flange. The cavity is delimited by the internal face of the docking flange. The cavity has a section "U" shape, viewed in a cross section of the docking flange.
Selon une caractéristique, l’organe d’assemblage comprend une section centrale, une première section latérale et une seconde section latérale ainsi qu’une section centrale reliant la première section latérale à la seconde section latérale, la première section latérale, la section centrale et la seconde section latérale étant conformées en « U ». L’organe d’assemblage se compose ainsi au moins de trois sections, chaque section étend disposée sensiblement à angle droit par rapport à la section immédiatement adjacente, vue selon une coupe transversale de l’organe d’assemblage. L’organe d’assemblage présente ainsi une forme en U, vue selon cette coupe.  According to one feature, the assembly member comprises a central section, a first lateral section and a second lateral section as well as a central section connecting the first lateral section to the second lateral section, the first lateral section, the central section and the second lateral section being shaped in "U". The assembly member is thus composed of at least three sections, each extending section disposed substantially at right angles to the immediately adjacent section, viewed in a cross section of the assembly member. The assembly member thus has a U-shape, seen according to this section.
Ainsi, l’organe d’assemblage épouse la forme de la bride d’accostage. L’organe d’assemblage est ainsi logé la cavité de la bride d’accostage et il présente ainsi un profil similaire au profil de la bride d’accostage, vue en coupe. Avantageusement, une dimension de l’organe d’assemblage, mesurée entre la première section latérale et la seconde section latérale, est supérieure à une dimension mesurée entre le boîtier et un renfort périphérique constitutif de l’organe d’accostage. On garantit un plaquage efficace du boîtier contre le bord plié. Thus, the assembly member takes the form of the docking flange. The assembly member is thus housed in the cavity of the docking flange and thus has a profile similar to the profile of the docking flange, seen in section. Advantageously, a dimension of the assembly member, measured between the first lateral section and the second lateral section, is greater than a dimension measured between the housing and a peripheral reinforcement constituting the docking member. Effective plating of the casing against the folded edge is guaranteed.
En d’autres termes, une section centrale de l’organe d’assemblage est disposée entre deux sections latérales, vue selon la coupe transversale. La bride d’accostage comprend de son côté une portion plate et deux bords pliés ménagés de chaque côté de la portion plate. La portion plate et les bords pliés délimite la cavité. Selon un aspect de l’invention, une dimension de la section centrale de l’organe d’assemblage est supérieure à une dimension de la portion plate déduite d’une épaisseur du boîtier, mesurées dans un même plan et le long d’une même direction. Une telle conformation garantit l’existence d’un effort de compression exercé par l’organe d’assemblage contre le boîtier.  In other words, a central section of the assembly member is arranged between two lateral sections, seen in cross-section. The docking flange comprises on its side a flat portion and two folded edges formed on each side of the flat portion. The flat portion and the folded edges delimit the cavity. According to one aspect of the invention, a dimension of the central section of the assembly member is greater than a dimension of the flat portion deduced from a thickness of the housing, measured in the same plane and along the same direction. Such a conformation ensures the existence of a compressive force exerted by the assembly member against the housing.
Selon une caractéristique, une épaisseur de l’organe d’assemblage est inférieure à une épaisseur de la bride d’accostage. L’organe d’assemblage est ainsi plus souple et peut se déformer pour venir se loger dans la cavité de la bride d’accostage, tandis que la bride d’accostage est d’une épaisseur qui lui permet de résister à l’effort de compression généré par le boîtier en réponse à l’appui opéré par l’organe d’assemblage.  According to one characteristic, a thickness of the assembly member is less than a thickness of the docking flange. The assembly member is thus more flexible and can be deformed to become housed in the cavity of the docking flange, while the docking flange is of a thickness that allows it to withstand the stress of compression generated by the housing in response to the support operated by the assembly member.
Selon une caractéristique, l’organe d’assemblage et la bride d’accostage présente un profil similaire, vue dans une coupe transversale à l’organe d’assemblage et à la bride d’accostage. L’organe d’assemblage possède ainsi une forme générale complémentaire à la forme de la bride d’accostage. C’est à ce titre que l’organe d’assemblage peut se loger dans la bride d’accostage. L’organe d’assemblage possède ainsi une complémentarité de section avec la section de la bride d’accostage, vue dans un plan perpendiculaire à la bride d’accostage et à l’organe d’assemblage, et qui coupe la bride d’accostage et l’organe d’assemblage.  According to one characteristic, the assembly member and the docking flange has a similar profile, seen in a cross section at the assembly member and the docking flange. The assembly member thus has a general shape complementary to the shape of the docking flange. It is for this reason that the assembly member can be housed in the docking flange. The assembly member thus has a complementarity of section with the section of the docking flange, seen in a plane perpendicular to the docking flange and the assembly member, and which cuts the docking flange. and the assembly member.
On notera que la bride d’accostage et l’organe d’assemblage présentent une forme similaire, vue dans un plan dans lequel s’étend majoritairement la bride d’accostage. En effet, quel que soit le mode de réalisation de l’organe d’assemblage, celui-ci présente une forme rectangulaire quand la bride d’accostage présente une forme rectangulaire.  Note that the docking flange and the assembly member have a similar shape, seen in a plane in which extends mainly the docking flange. Indeed, whatever the embodiment of the assembly member, it has a rectangular shape when the docking flange has a rectangular shape.
Selon une caractéristique, la bride d’accostage comprend un bord plié et un renfort périphérique reliés l’un à l’autre par un bord d’accostage, l’organe d’assemblage étant en contact avec le bord d’accostage de la bride d’accostage. Le bord d’accostage est la zone de la bride d’accostage contre laquelle un joint est disposé pour étanchéifier la liaison entre le dispositif de refroidissement selon l’invention et le moteur à combustion interne qui le porte. According to one characteristic, the docking flange comprises a folded edge and a peripheral reinforcement connected to one another by a docking edge, the assembly member being in contact with the docking edge of the flange. docking. The docking edge is the area of the docking flange against which a seal is arranged to seal the link between the cooling device according to the invention and the internal combustion engine which carries it.
Selon une caractéristique, la bride d’accostage comprend au moins un moyen de fixation et l’organe d’assemblage comprend au moins un orifice superposé à au moins un moyen de fixation de la bride d’accostage. Grâce à la présence de ces orifices superposés aux moyens de fixation de la bride d’accostage, l’installation de l’organe d’assemblage ne nuit pas à la liaison de la bride d’accostage contre le moteur à combustion interne, qui est un objectif initial de la bride d’accostage. Une fois solidarisé par brasage, l’organe d’assemblage devient un renfort mécanique qui permet de maintenir une bonne planéité de la bride d’accostage.  According to one characteristic, the docking flange comprises at least one fastening means and the assembly member comprises at least one orifice superimposed on at least one fastening means of the docking flange. Thanks to the presence of these holes superimposed on the fastening means of the docking flange, the installation of the assembly member does not interfere with the connection of the docking flange against the internal combustion engine, which is an initial goal of the docking flange. Once secured by brazing, the assembly member becomes a mechanical reinforcement that maintains a good flatness of the docking flange.
Selon une caractéristique, l’organe d’assemblage se compose d’au moins deux pièces distinctes, comprenant au moins trois branches qui s’étendent dans un même plan, chaque branche formant un angle par rapport à la branche immédiatement adjacente.  According to one characteristic, the assembly member is composed of at least two distinct parts, comprising at least three branches that extend in the same plane, each branch forming an angle with respect to the immediately adjacent branch.
Selon une autre caractéristique, l’organe d’assemblage se compose de deux pièces distinctes, comprenant seulement deux branches qui s’étendent dans un même plan, une branche principale formant un angle par rapport à la branche secondaire adjacente.  According to another characteristic, the assembly member is composed of two distinct parts, comprising only two branches which extend in the same plane, a main branch forming an angle with respect to the adjacent secondary branch.
Selon encore une autre caractéristique, l’organe d’assemblage se compose de quatre pièces distinctes qui présentent un profil rectiligne. Il s’agit de quatre barreaux qui peuvent aisément être installés dans la cavité de la bride d’accostage.  According to yet another characteristic, the assembly member is composed of four distinct parts that have a straight profile. These are four bars that can easily be installed in the cavity of the docking flange.
Les dispositions ci-dessus sont des exemples de réalisation de l’organe d’assemblage qui visent à faciliter son installation au sein du dispositif de refroidissement.  The above provisions are embodiments of the assembly member which are intended to facilitate its installation within the cooling device.
Selon une caractéristique, le boîtier comprend au moins un moyen de verrouillage contre lesquels l’organe d’assemblage prend appui. La position de l’organe d’assemblage contre le boîtier est ainsi garantie, sans risque de voir échapper accidentellement l’organe d’assemblage.  According to one characteristic, the housing comprises at least one locking means against which the assembly member bears. The position of the assembly member against the housing is thus guaranteed, without the risk of accidentally escaping the assembly member.
Selon une autre caractéristique, la bride d’accostage comprend au moins dispositif de blocage contre lesquels l’organe d’assemblage prend appui. La position de l’organe d’assemblage contre la bride d’accostage est ainsi garantie, sans risque de voir échapper accidentellement l’organe d’assemblage.  According to another characteristic, the docking flange comprises at least one locking device against which the assembly member bears. The position of the assembly member against the docking flange is thus guaranteed, without the risk of accidentally escaping the assembly member.
Selon un procédé de d’assemblage d’un boîtier et d’une bride d’accostage d’un dispositif de refroidissement, il est prévu au moins les étapes suivantes :  According to a method of assembling a housing and a docking flange of a cooling device, at least the following steps are provided:
- on positionne une face intérieure du boîtier contre un bord plié de la bride d’accostage, - on bloque une seconde section latérale de l’organe d’assemblage contre la bride d’accostage, an inner face of the housing is positioned against a folded edge of the docking flange, a second lateral section of the assembly member is blocked against the docking flange,
- on exerce un effort sur l’organe d’assemblage jusqu’à ce qu’une première section latérale comprime le boîtier contre le bord plié. a force is exerted on the assembly member until a first lateral section compresses the casing against the folded edge.
Avantageusement, la deuxième section latérale est bloquée contre la bride d’accostage par mise en appui contre au moins un moyen de blocage dont la bride d’accostage est pourvue.  Advantageously, the second lateral section is locked against the docking flange by bearing against at least one locking means of which the docking flange is provided.
Avantageusement encore, la première section latérale est verrouillée contre la boîtier par mise en appui contre au moins un moyen de verrouillage dont le boîtier est pourvu.  Advantageously, the first lateral section is locked against the housing by bearing against at least one locking means whose housing is provided.
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 du corps de faisceau,  a step of assembling the beam body,
-une étape de positionnement du corps de faisceau dans le boîtier,  a step of positioning the beam body in the housing,
-une étape d’assemblage du boîtier et de la bride d’accostage, a step of assembling the housing and the docking flange,
-une étape de serrage du boîtier contre la bride d’accostage au moyen d’un organe d’assemblage ; avantageusement le boîtier est serré contre une face externe d’un bord plié de la bride d’accostage, a step of clamping the housing against the docking flange by means of an assembly member; advantageously the housing is clamped against an outer face of a folded edge of the docking flange,
-une étape de brasage simultanée au moins du boîtier, de la bride d’accostage et de l’organe d’assemblage.  a step of simultaneously soldering at least the housing, the docking flange and the assembly member.
Avantageusement, l’étape de brasage permet de relier en une opération le corps de faisceau, le boîtier, la bride d’accostage et l’organe d’assemblage. L’étape de brasage est réalisée par procédé Nocolok.  Advantageously, the soldering step makes it possible to connect in one operation the beam body, the housing, the docking flange and the assembly member. The brazing step is carried out by 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 t est une vue en perspective du dispositif de refroidissement d’un air d’admission de moteur à combustion interne selon l’art antérieur,  FIG. 1 is a perspective view of the cooling device of an intake air of an internal combustion engine according to the prior art,
- la figure 2 est une vue en perspective du dispositif de refroidissement d’un air d’admission de moteur à combustion interne selon l’invention,  FIG. 2 is a perspective view of the cooling device of an intake air of an internal combustion engine according to the invention,
- la figure 3 est une vue en perspective de l’organe d’assemblage exploité dans le dispositif de refroidissement objet de l’invention, selon un mode de réalisation, - la figure 4 est vue en perspective de l’organe d’assemblage selon un deuxième mode de réalisation, FIG. 3 is a perspective view of the assembly member operated in the cooling device that is the subject of the invention, according to one embodiment, FIG. 4 is a perspective view of the assembly member according to a second embodiment,
- la figure 5 est vue en perspective de l’organe d’assemblage selon un autre mode de réalisation,  FIG. 5 is a perspective view of the assembly member according to another embodiment,
- la figure 6 est une vue schématique du procédé d’assemblage du boîtier contre la bride d’accostage, au moyen de l’organe d’assemblage selon l’un quelconque des modes de réalisation.  - Figure 6 is a schematic view of the assembly method of the housing against the docking flange, by means of the connecting member according to any one of the embodiments.
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. Sur les différentes figures, les éléments identiques portent les mêmes numéros de référence.  It should first be noted that the figures disclose the invention in detail to implement the invention, said figures can of course be used to better define the invention where appropriate. In the different figures, the identical elements bear the same reference numbers.
Dans la présente description, on désigne par longueur, la dimension la plus importante d’un composant du dispositif de refroidissement, par épaisseur la dimension la plus faible mesurée perpendiculairement à la dimension la plus importante et par largeur, une dimension du composant perpendiculaire à fois de sa longueur et de son épaisseur.  In the present description, the term "length" refers to the largest dimension of a component of the cooling device, "thickness" being the smallest dimension measured perpendicularly to the largest dimension, and "width" being the dimension of the component perpendicular to both times. its length and thickness.
L’utilisation dans la description qui suit des termes intérieur ou interne implique un positionnement tourné vers l’intérieur du dispositif de refroidissement, notamment vers un axe passant au centre du corps de faisceau du dispositif de refroidissement. L’utilisation dans la description qui suit des termes extérieur ou externe implique un positionnement tourné vers l’environnement extérieur qui entoure le dispositif de refroidissement.  The use in the following description of the internal or internal terms implies a positioning inwardly of the cooling device, in particular towards an axis passing in the center of the beam body of the cooling device. The use in the following description of external or external terms implies positioning facing the external environment surrounding the cooling device.
La figure 1 représente une vue générale, en perspective, du dispositif de refroidissement 1 d’un air d’admission d’un moteur à combustion interne selon l’art antérieur. Le dispositif de refroidissement 1 comprend un boîtier 2, un corps de faisceau 3 et une bride d’accostage 4.  FIG. 1 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine according to the prior art. The cooling device 1 comprises a housing 2, a beam body 3 and a docking flange 4.
Le boîtier 2 comprend quatre flancs 21, parallèles deux à deux, permettant de former le 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 d’entrer et de sortie du boîtier 2, traversant ainsi 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 the housing 2 parallelepipedal shape, or cubic. The housing 2 delimits an inlet surface 22 and an outlet surface 23, parallel to each other, allowing a flow of intake air to enter and exit the housing 2, thus passing through the housing 2 in its entirety. that is to say, from one side to the other.
Le corps de faisceau 3 est logé à l’intérieur du boîtier 2 et il 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. Cette organisation est par la suite répétée suivant un axe perpendiculaire à un plan général d’extension des plaques 31, jusqu’à remplir le boîtier 2 dans son intégralité, formant ainsi le corps de faisceau 3. The beam body 3 is housed inside the casing 2 and consists of a stack of plates 31 and dissipation devices 32. The stack consists of the following manner: an alternation of a pair of plates 31 and a device for dissipation 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. This organization is subsequently repeated along an axis perpendicular to a general plane of extension of the plates 31, to fill the housing 2 in its entirety, thus forming the beam body 3.
Le flux d’air d’admission traversant le boîtier 2 passe entre les couples de plaques, le long des dispositifs de dissipation 32 et en léchant ces derniers. Un dispositif de dissipation 32 prend la forme d’une ailette ou d’une intercalaire. 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 between the pairs of plates, along the dissipating devices 32 and licking them. A dissipation device 32 takes the form of a fin or a spacer. 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.
Une bride d’accostage 4 est placée au niveau de la surface de sortie 23 du boîtier 2. La bride d’accostage 4 entoure le boîtier 2 qui repose contre le bord plié 41 de la bride d’accostage 4. Le boîtier 2 est inséré à l’intérieur de la bride d’accostage 4. De cette manière, le boîtier 2 est encastré sur la bride d’accostage 4.  A docking flange 4 is placed at the outlet surface 23 of the casing 2. The docking flange 4 surrounds the casing 2 which rests against the folded edge 41 of the docking flange 4. The casing 2 is inserted inside the docking flange 4. In this way, the casing 2 is recessed on the docking flange 4.
La bride d’accostage 4 comprend encore 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.  The docking flange 4 further 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.
La figure 2 représente une vue générale, en perspective, du dispositif de refroidissement 1 d’un air d’admission d’un moteur à combustion interne selon l’invention. Le dispositif de refroidissement 1 comprend un boîtier 2, un corps de faisceau 3, une bride d’accostage 4. Le dispositif de refroidissement 1 comprend également un organe d’assemblage 5. Une fois préassemblés, ces composants sont solidarisés simultanément les uns aux autres au cours d’une étape de brasage selon un procédé Nocolok.  FIG. 2 represents a general perspective view of the cooling device 1 of an intake air of an internal combustion engine according to the invention. The cooling device 1 comprises a housing 2, a beam body 3, a docking flange 4. The cooling device 1 also comprises an assembly member 5. Once pre-assembled, these components are simultaneously secured to one another during a brazing step according to a Nocolok process.
Le boîtier 2 et le corps de faisceau 3 sont réalisés et organisés de manière identique à ce qui a été décrit eu égard à la figure 1. On se reportera donc à la description de la figure 1 pour leur mise en œuvre.  The housing 2 and the beam body 3 are made and organized identically to what has been described with respect to FIG. 1. Reference is therefore made to the description of FIG. 1 for their implementation.
La bride d’accostage 4 comprend un bord plié 41, le bord d’accostage 43 tel que détaillé à la figure i et un renfort périphérique 45. Le bord plié 41, le bord d’accostage 43 et le renfort périphérique 456 délimitent une cavité 10 destinée à recevoir au moins un organe d’assemblage 5. The docking flange 4 comprises a folded edge 41, the docking edge 43 such that FIG. 1 and a peripheral reinforcement 45. The folded edge 41, the docking edge 43 and the peripheral reinforcement 456 delimit a cavity 10 intended to receive at least one assembly member 5.
Un tel bord plié 41 résulte d’un pliage à angle droit, ou sensiblement à angle droit, d’une bande intérieure de la bride d’accostage 4.  Such a folded edge 41 results from folding at right angles, or substantially at right angles, an inner band of the docking flange 4.
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 d’une opération d’emboutissage. Ce renfort périphérique 45 prend la forme d’un pli sensiblement à angle droit d’une bande périphérique extérieure de la bride d’accostage 4. De cette manière et comme évoqué plus haut, la bride d’accostage 4 présente une section en forme de « U », observée suivant une coupe transversale à la bride d’accostage 4. La présence d’un tel renfort périphérique 45 augmente significativement la résistance mécanique de la bride d’accostage 4, notamment quand celle-ci est réalisée par une étape d’emboutissage.  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 a stamping operation. This peripheral reinforcement 45 takes the form of a fold substantially at right angles to an outer peripheral band of the docking flange 4. In this way and as mentioned above, the docking flange 4 has a section in the form of "U", observed in cross-section at the docking flange 4. The presence of such a peripheral reinforcement 45 significantly increases the mechanical strength of the docking flange 4, in particular when this is achieved by a step d stamping.
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 une vis ou un écrou et une rondelle.  The docking flange 4 also comprises ears where the fixing means 44 are arranged. This is a localized widening of the docking edge 43 which offers the possibility of disposing of a screw or a nut and a washer. .
La bride d’accostage 4 forme un cerclage ouvert en son centre. Cette bride d’accostage 4 comprend, vue selon la coupe transversale, une portion centrale et deux portions latérales formées par des bords pliés sensiblement à 90° par rapport à un plan dans lequel s’étend la portion centrale. L’une des portions latérales est le bord plié 41 de la bride d’accostage 4, contre lequel le boîtier 2 prend appui. L’autre portion latérale est le renfort périphérique 45. La portion centrale et le bord d’accostage 43.  The docking flange 4 forms an open strapping at its center. This docking flange 4 comprises, seen in cross-section, a central portion and two lateral portions formed by edges bent substantially at 90 ° with respect to a plane in which the central portion extends. One of the side portions is the folded edge 41 of the docking flange 4, against which the housing 2 bears. The other lateral portion is the peripheral reinforcement 45. The central portion and the docking edge 43.
La bride d’accostage 4 est placée au niveau de la surface de sortie 23 du boîtier 2. Le boîtier 2 entoure la bride d’accostage 4, en venant prendre appui contre le bord plié 41 de la bride d’accostage 4. En d’autres termes, la bride d’accostage 4 est logé dans le boîtier 2.  The docking flange 4 is placed at the outlet surface 23 of the casing 2. The casing 2 surrounds the docking flange 4, coming to rest against the folded edge 41 of the docking flange 4. In addition, In other words, the docking flange 4 is housed in the casing 2.
Après insertion de la bride d’accostage 4 dans le boîtier 2, une face externe 411 du bord plié 41 est en contact avec une face intérieure 213 des flancs 21 au niveau d’une zone de connexion entre le boîtier 2 et la bride d’accostage 4, cette zone de connexion formant une bande de solidarisation entre ces deux composants. Le boîtier 2 est bloqué sur la bride d’accostage 4 grâce à un élargissement créé par un arrondi reliant le bord plié 41 au bord d’accostage 43 de la bride d’accostage 4. De cette manière, la bride d’accostage 4 est encastrée dans le boîtier 2. 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. Le bord d’accostage 43 est réalisé par la portion centrale de la bride d’accostage, vue selon sa coupe transversale. Le bord d’accostage 43 comprend un plan de joint, c’est-à-dire une zone configurée pour assurer une étanchéité avec un joint. Ce joint est disposé entre la bride d’accostage 4 et la culasse du moteur à combustion interne qui reçoit le dispositif de refroidissement 1. After insertion of the docking flange 4 in the casing 2, an outer face 411 of the folded edge 41 is in contact with an inner face 213 of the flanks 21 at a connection zone between the casing 2 and the flange of the casing. docking 4, this connection area forming a bonding strip between these two components. The casing 2 is blocked on the docking flange 4 by a widening created by a rounding connecting the folded edge 41 to the docking edge 43 of the docking flange 4. In this way, the docking flange 4 is recessed in the housing 2. 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 docking edge 43 is formed by the central portion of the docking flange, seen according to its cross section. The docking edge 43 comprises a joint plane, that is to say a zone configured to seal with a seal. This seal is disposed between the docking flange 4 and the cylinder head of the internal combustion engine which receives the cooling device 1.
La bride d’accostage 4 comprend également des oreilles au voisinage desquelles sont disposés les moyens de fixation 44. Il s’agit d’un élargissement localisé du bord d’accostage 43 et une déformation du renfort périphérique 45 qui offrent la possibilité d’y disposer une tête de vis ou un écrou et une rondelle.  The docking flange 4 also comprises ears in the vicinity of which the fastening means 44 are arranged. It is a localized widening of the docking edge 43 and a deformation of the peripheral reinforcement 45 which offer the possibility of arrange a screw head or nut and washer.
Conformément à l’invention, un organe d’assemblage 5 est installé dans le dispositif de refroidissement 1 de manière à plaquer le boîtier 2 contre la bride d’accostage 4, au droit de la zone de connexion. Cet organe d’assemblage 5 permet de réaliser un serrage du boîtier 2 contre le bord plié 41 lorsque le dispositif de refroidissement 1 est dans un état de pré-assemblage.  According to the invention, an assembly member 5 is installed in the cooling device 1 so as to press the housing 2 against the docking flange 4, to the right of the connection zone. This assembly member 5 makes it possible to clamp the housing 2 against the folded edge 41 when the cooling device 1 is in a pre-assembly state.
Cet organe d’assemblage 5 prend une forme complémentaire à la forme de la bride d’accostage 4, c’est-à-dire, une forme en « U » vue selon une coupe transversale à l’organe d’assemblage 5. Vue dans cette coupe, l’organe d’assemblage 5 comprend une section centrale 51 qui repose contre le bord d’accostage 43 de la bride d’accostage 4, et deux sections latérales qui reposent, pour une première section latérale 58 contre une face extérieure 212 des flancs 21 du boîtier 2, et pour une seconde section latérale 59, contre le renfort périphérique 45 de la bride d’accostage 4, en particulier contre la face interne de ce renfort périphérique 45.  This assembly member 5 takes a shape complementary to the shape of the docking flange 4, that is to say, a "U" shape seen in cross-section to the assembly member 5. View in this section, the assembly member 5 comprises a central section 51 which rests against the docking edge 43 of the docking flange 4, and two lateral sections which rest, for a first lateral section 58 against an outer face 212 flanks 21 of the housing 2, and for a second lateral section 59, against the peripheral reinforcement 45 of the docking flange 4, in particular against the inner face of this peripheral reinforcement 45.
Cette configuration implique donc que les flancs 21 du boîtier 2 enveloppent la face externe 411 du bord plié 41, la première section latérales 58 de l’organe d’assemblage 5 étant en contact contre la face extérieure 212 des flancs 21 du boîtier 2.  This configuration therefore implies that the flanks 21 of the housing 2 envelop the outer face 411 of the folded edge 41, the first lateral section 58 of the assembly member 5 being in contact against the outer face 212 of the flanks 21 of the housing 2.
Afin de permettre la fixation de la bride d’accostage 4 contre le moteur à combustion interne, l’organe d’assemblage 5 comprend des orifices 57 superposés aux moyens de fixation 44 de la bride d’accostage 4. De cette manière, l’utilisation de quelconques moyens de liaison, comme par exemple des vis, écrous ou autre, ne sera pas perturbée par la présence de l’organe d’assemblage 5 une fois placé contre la bride d’accostage 4. L’organe d’assemblage 5 constitue également un élément de renfort de la bride d’accostage 4, en augmentant l’épaisseur de la pièce résultant de la solidarisation de l’organe d’assemblage 5 avec la bride d’accostage 4. On augmente ainsi la résistance à la torsion de la bride d’accostage 4, permettant ainsi de réduire le nombre de moyen de fixation 44. In order to allow the attachment of the docking flange 4 against the internal combustion engine, the assembly member 5 comprises orifices 57 superimposed on the fastening means 44 of the docking flange 4. In this way, the use of any connecting means, such as screws, nuts or other, will not be disturbed by the presence of the assembly member 5 when placed against the docking flange 4. The assembly member 5 also constitutes a reinforcing element of the docking flange 4, by increasing the thickness of the part resulting from the joining of the assembly member 5 with the docking flange 4. This increases the torsional resistance of the docking flange 4, thereby reducing the number of fastening means 44.
Tout comme la bride d’accostage 4, l’organe d’assemblage 5 est de forme générale rectangulaire. Selon différents modes de réalisation qui sont détaillés en figures 3 à 5, l’organe d’assemblage 5 est scindé en plusieurs pièces distinctes. Ces modes de réalisation ont pour objectif de proposer un organe d’assemblage 5 dont l’installation sur la bride d’accostage est facilitée.  Like the docking flange 4, the assembly member 5 is of generally rectangular shape. According to various embodiments which are detailed in FIGS. 3 to 5, the assembly member 5 is split up into several distinct pieces. These embodiments are intended to provide an assembly member 5 whose installation on the docking flange is facilitated.
La figure 3 est une vue en perspective de l’organe d’assemblage 5 exploité dans le dispositif de refroidissement 1, selon un premier mode de réalisation. De forme rectangulaire, vue selon un plan général plat dans lequel s’étend majoritairement l’organe d’assemblage 5, ce dernier se compose de deux pièces distinctes 54. Chaque pièce distincte 54 comprend trois branches 55 qui s’étendent dans un même plan, chaque branche 55 formant un angle 56, par exemple un angle droit, par rapport à la branche 55 immédiatement adjacente. Chaque pièce distincte 54 ainsi formée comprend donc une branche centrale aux bouts de laquelle deux branches latérales s’étendent dans une direction perpendiculaire à une direction d’extension majoritaire de la branche centrale. Vue dans le plan général plat, chaque pièce distincte 54 forme un « U » où la branche centrale est de longueur supérieure à l’une et/ou l’autre des branches latérales.  Figure 3 is a perspective view of the connecting member 5 operated in the cooling device 1, according to a first embodiment. Of rectangular shape, seen according to a flat general plane in which extends mainly the assembly member 5, the latter consists of two separate parts 54. Each separate part 54 comprises three branches 55 which extend in the same plane each leg 55 forming an angle 56, for example a right angle, with respect to the immediately adjacent leg 55. Each separate piece 54 thus formed thus comprises a central branch at the ends of which two lateral branches extend in a direction perpendicular to a majority extension direction of the central branch. Viewed in the flat general plane, each separate piece 54 forms a "U" where the central branch is of greater length than one and / or the other side branches.
Selon un plan perpendiculaire au plan général plat exposé plus haut et passant par l’organe d’assemblage 5, chaque pièce 54 prend la forme d’un « U » et comporte ainsi la section centrale 51 bordée d’un côté par la première section latérale 58 et de l’autre par la seconde section latérale 59.  In a plane perpendicular to the flat general plane exposed above and passing through the assembly member 5, each piece 54 takes the form of a "U" and thus comprises the central section 51 lined on one side by the first section 58 and the other by the second lateral section 59.
Les deux pièces distinctes 54 formant l’organe d’assemblage 5 sont pourvues sur leur section centrale 51 des orifices 57 qui, lorsque l’organe d’assemblage 5 est apposé contre la bride d’accostage 4, sont superposés aux moyens de fixations de la bride d’accostage 4.  The two separate parts 54 forming the assembly member 5 are provided on their central section 51 with orifices 57 which, when the assembly member 5 is affixed against the docking flange 4, are superimposed on the fastening means of FIGS. the docking flange 4.
Selon ce premier mode de réalisation, l’organe d’assemblage 5 comprend uniquement deux pièces distinctes 54 qui sont disposées l’une en face de l’autre, dans le plan général plat. Les deux pièces distinctes 54 de ce premier mode de réalisation sont identiques.  According to this first embodiment, the assembly member 5 comprises only two separate parts 54 which are arranged opposite each other in the flat general plane. The two separate parts 54 of this first embodiment are identical.
Une fois assemblé sur la bride d’accostage, deux espaces 53 sont apparents entre les deux pièces distinctes 54, chaque espace 53 étant ménagé entre l’une des branches latérales de l’une des pièces distinctes 54 et l’une des branches latérales de l’autre des pièces distinctes 54. La figure 4 est une vue en perspective de l’organe d’assemblage 5 exploité dans le dispositif de refroidissement 1, selon un deuxième mode de réalisation. Comme présenté dans le mode précédent, l’organe d’assemblage 5, réalisé selon ce mode, se compose uniquement de deux pièces distinctes 54. Once assembled on the docking flange, two spaces 53 are apparent between the two distinct pieces 54, each space 53 being formed between one of the lateral branches of one of the separate pieces 54 and one of the lateral branches of the other of the separate rooms 54. Figure 4 is a perspective view of the assembly member 5 operated in the cooling device 1, according to a second embodiment. As presented in the previous mode, the assembly member 5, produced according to this mode, consists solely of two separate pieces 54.
Chaque pièce distincte 54 comprend uniquement deux branches 55 qui s’étendent dans un même plan, chaque branche 55 formant un angle 56, par exemple un angle droit, par rapport à la branche 55 immédiatement adjacente. Chaque pièce distincte 54 ainsi formée comprend donc une branche principale au bout de laquelle une branche secondaire s’étend le long d’une direction perpendiculaire à une direction d’extension majoritaire de la branche principale. Vue dans le plan général plat, chaque pièce distincte 54 forme un « L » où la branche principale est de longueur supérieure la branche secondaire.  Each separate part 54 comprises only two branches 55 which extend in the same plane, each branch 55 forming an angle 56, for example a right angle, with respect to the immediately adjacent branch 55. Each separate piece 54 thus formed thus comprises a main branch at the end of which a secondary branch extends along a direction perpendicular to a majority extension direction of the main branch. Viewed in the flat general plane, each separate piece 54 forms an "L" where the main branch is of greater length than the secondary branch.
Ces pièces distinctes 54 sont en revanche installées tête-bêche l’une en face de l’autre. Les deux pièces distinctes 54 sont symétriques l’un à l’autre par rapport à un plan de symétrie passant par deux angles 56 opposés l’un à l’autre par rapport au corps de faisceau.  These separate parts 54 are instead installed head to tail opposite each other. The two distinct pieces 54 are symmetrical to one another with respect to a plane of symmetry passing through two angles 56 opposite to each other with respect to the beam body.
Deux espaces 53 sont ménagés entre chaque pièce distincte 54 et, dans ce deuxième mode de réalisation, ces espaces 53 sont réalisés aux angles de la bride d’accostage.  Two spaces 53 are formed between each separate piece 54 and, in this second embodiment, these spaces 53 are made at the corners of the docking flange.
Selon ce deuxième mode de réalisation, l’organe d’assemblage 5 comprend une fente 60 ménagée au niveau de l’angle 56 qui relie la branche principale à la branche secondaire de la pièce distincte 54. Cette fente 60 est destinée à autoriser une certaine ouverture de l’angle 56, offrant ainsi une souplesse de position entre la branche principale et la branche secondaire afin de faciliter l’installation de la pièce distincte 54 sur la bride d’accostage. Selon un exemple, une telle fente 60 coupe la première section latérale 58 et la section centrale 51. En revanche, la fente 60 ne coupe pas la seconde section latérale 59.  According to this second embodiment, the assembly member 5 comprises a slot 60 formed at the angle 56 which connects the main branch to the secondary branch of the separate part 54. This slot 60 is intended to allow some opening the angle 56, thus providing a positional flexibility between the main branch and the secondary branch to facilitate the installation of the separate part 54 on the docking flange. In one example, such a slot 60 intersects the first lateral section 58 and the central section 51. On the other hand, the slot 60 does not cut the second lateral section 59.
La forme de chaque pièce distincte 54, vue en coupe, est identique à celle décrite aux figures précédentes. Il en va de même pour les orifices 57 qui sont destinés à se superposer sur les moyens de fixation de la bride d’accostage. On se reportera à la description ci- dessus de ces caractéristiques techniques pour les mettre en œuvre dans le cadre de ce deuxième mode de réalisation.  The shape of each distinct piece 54, seen in section, is identical to that described in the preceding figures. It is the same for the orifices 57 which are intended to be superimposed on the fastening means of the docking flange. Reference is made to the above description of these technical characteristics to implement them in the context of this second embodiment.
La figure 5 est une vue en perspective de l’organe d’assemblage 5 exploité dans le dispositif de refroidissement 1, selon un troisième mode de réalisation. A la différence des modes de réalisation précédents, l’organe d’assemblage 5 réalisé selon ce mode se compose strictement ou au moins de quatre pièces distinctes 54. Chaque pièce distincte 54 comprend une unique branche 55 de forme rectiligne. Chaque pièce distincte 54 est ainsi formée de quatre barreaux disposés tout autour du boîtier du dispositif de refroidissement selon l’invention. Figure 5 is a perspective view of the assembly member 5 operated in the cooling device 1, according to a third embodiment. Unlike the previous embodiments, the assembly member 5 made in this mode consists strictly or at least four separate pieces 54. Each separate piece 54 comprises a single branch 55 of rectilinear shape. Each separate piece 54 is thus formed of four bars arranged all around the housing of the cooling device according to the invention.
Dans ce mode de réalisation, chaque pièce distincte 54 est séparée de la pièce distincte immédiatement adjacente par un espace 53. L’organe d’assemblage 5 possède donc quatre espaces 53 positionnées au niveau des angles 56 formés entre les quatre pièces distinctes 54 formant l’organe d’assemblage 5.  In this embodiment, each separate piece 54 is separated from the immediately adjacent separate piece by a space 53. The assembly member 5 thus has four spaces 53 positioned at the angles 56 formed between the four separate pieces 54 forming the assembly member 5.
La forme de chaque pièce distincte, vue en coupe, est identique à celle décrite aux figures précédentes. Il en va de même pour les orifices 57 qui sont destinés à se superposer sur les moyens de fixation de la bride d’accostage. On se reportera à la description ci- dessus de ces caractéristiques techniques pour les mettre en œuvre dans le cadre de ce deuxième mode de réalisation.  The shape of each distinct piece, seen in section, is identical to that described in the preceding figures. It is the same for the orifices 57 which are intended to be superimposed on the fastening means of the docking flange. Reference is made to the above description of these technical characteristics to implement them in the context of this second embodiment.
La figure 6 est une vue partielle et en coupe transversale de la bride d’accostage 4, du boîtier 2 et de l’organe d’assemblage 5, illustrées pendant le montage de l’organe d’assemblage 5.  FIG. 6 is a partial cross-sectional view of the docking flange 4, the casing 2 and the assembly member 5, illustrated during the assembly of the assembly member 5.
La figure 6 montre que le renfort périphérique 45 comprend au moins un dispositif de blocage 47 destiné à maintenir l’organe d’assemblage 5 en place, pendant sa phase de compression vers la bride d’accostage 4. Le dispositif de blocage 47 forme un pied d’appui autour duquel l’organe d’assemblage 5 bascule, pendant son insertion contre la bride d’accostage 4.  FIG. 6 shows that the peripheral reinforcement 45 comprises at least one locking device 47 intended to hold the assembly member 5 in place during its compression phase towards the docking flange 4. The locking device 47 forms a foot support around which the assembly member 5 during its insertion tilts against the docking flange 4.
Le dispositif de blocage 47 prend la forme d’une ou plusieurs languettes, réalisées par découpe et/ou déformation du renfort périphériques 45. Le dispositif de blocage 47 émerge de la face interne 46 de l’interface d’accostage 4, en direction du bord plié 41 de cette même bride d’accostage 4. Cette languette qui forme un exemple de réalisation du dispositif de blocage 47 présente un bord 48 contre lequel une première tranche 61 l’organe d’assemblage 5 prend appui, lors de son installation dans la bride d’accostage 4.  The locking device 47 takes the form of one or more tongues, made by cutting and / or deformation of the peripheral reinforcement 45. The locking device 47 emerges from the inner face 46 of the docking interface 4, towards the folded edge 41 of the same docking flange 4. This tongue which forms an embodiment of the locking device 47 has an edge 48 against which a first wafer 61 the assembly member 5 bears, when installed in the docking flange 4.
La figure 6 montre aussi que la face extérieure 212 des flancs 21 du boîtier 2 est dotée d’au moins un moyen de verrouillage 62, destiné à contenir l’organe d’assemblage 5 dans la cavité 10 de la bride d’accostage 4, une fois comprimé contre le boîtier 2. Le moyen de verrouillage 62 prend la forme d’un ou plusieurs contreforts qui émergent de la face extérieure 212 du flanc 21 concerné, en direction du renfort périphérique 45. Le contrefort est réalisé par découpe et/ou déformation du flanc 21 constitutif du boîtier 2. Ce contrefort qui forme un exemple de réalisation du moyen de verrouillage 62 présente une arrête 63 contre lequel une seconde tranche 64 l’organe d’assemblage 5 prend appui, de manière à verrouiller la position de l’organe d’assemblage 5 qui plaque le boîtier 2 sur la bride d’accostage 4. FIG. 6 also shows that the outer face 212 of the sidewalls 21 of the casing 2 is provided with at least one locking means 62 intended to hold the assembly member 5 in the cavity 10 of the docking flange 4, once compressed against the housing 2. The locking means 62 takes the form of one or more buttresses that emerge from the outer face 212 of the flank 21 concerned, in the direction of the peripheral reinforcement 45. The buttress is made by cutting and / or deformation of the flank 21 constituting the housing 2. This buttress which forms an embodiment of the locking means 62 has a stop 63 against which a second wafer 64 the assembly member 5 bears, of to lock the position of the assembly member 5 which plates the housing 2 on the docking flange 4.
Ainsi, l’utilisation de l’organe d’assemblage 5 assure un maintien optimal du boîtier 2 contre la bride d’assemblage 4. En effet, la première section latérale 58, reposant contre la face extérieure 212 des flancs 21 du boîtier 2, est verrouillé par l’intermédiaire des moyens de verrouillage 62 se trouvant sur la face extérieure 212 des flancs du boîtier 2, tandis que la seconde section latérale 59, reposant contre le renfort périphérique 45, est maintenue contre ce dernier par l’intermédiaire des dispositifs de blocage 47. L’organe d’assemblage 5 est ainsi verrouillé sur la bride d’accostage 4, en attendant l’étape de brasage selon le procédé Nocolok où ces pièces seront définitivement solidarisées.  Thus, the use of the assembly member 5 ensures optimum retention of the housing 2 against the assembly flange 4. Indeed, the first lateral section 58, resting against the outer face 212 of the flanks 21 of the housing 2, is locked through the locking means 62 on the outer face 212 of the sides of the housing 2, while the second lateral section 59, resting against the peripheral reinforcement 45, is held against the latter through the devices 47. The assembly member 5 is thus locked on the docking flange 4, waiting for the soldering step according to the Nocolok process where these parts will be permanently secured.
L’organe d’assemblage 5 est fabriqué par l’emboutissage d’une tôle, par exemple d’aluminium ou d’un alliage d’aluminium compatible avec le matériau qui constitue la bride d’accostage 4 et le boîtier 2.  The assembly member 5 is manufactured by stamping a sheet, for example aluminum or an aluminum alloy compatible with the material that constitutes the docking flange 4 and the housing 2.
D’un point de vue dimensionnel, une dimension L de l’organe d’assemblage 5, mesurée entre la première section latérale 58 et la seconde section latérale 59 de l’organe d’assemblage 5 est supérieure à une dimension 1 mesurée entre la face extérieure 212 du flanc 21 concerné et le renfort périphérique 45. Une telle comparaison s’effectue avant solidarisation par brasage selon le procédé Nocolok et garantit un effort suffisant pour plaquer le flanc 21 contre le bord plié 41, au niveau de la zone de connexion 65 entre boîtier 2 et bride d’accostage 4.  From a dimensional point of view, a dimension L of the assembly member 5, measured between the first lateral section 58 and the second lateral section 59 of the assembly member 5 is greater than a dimension 1 measured between the outer face 212 of the flank 21 concerned and the peripheral reinforcement 45. Such a comparison is made before joining by brazing according to the Nocolok method and ensures a sufficient effort to press the flank 21 against the folded edge 41, at the connection zone 65 between housing 2 and docking flange 4.
On notera également qu’une épaisseur de l’organe d’assemblage 5 est inférieure à une épaisseur de la bride d’accostage 4. On confère ainsi la souplesse nécessaire à l’insertion de l’organe d’assemblage 5 dans la cavité 10 de la bride d’accostage 4.  Note also that a thickness of the assembly member 5 is less than a thickness of the docking flange 4. This gives the flexibility required for the insertion of the assembly member 5 in the cavity 10 the docking flange 4.
L’installation de l’organe d’assemblage 5 se fait après l’insertion du boîtier 2 sur la bride d’accostage 4. L’installation de l’organe d’assemblage 5 se décompose en trois étapes successives représentées par trois illustrations référencées (a), (b) et (c) de la figure The installation of the assembly member 5 is done after the insertion of the housing 2 on the docking flange 4. The installation of the assembly member 5 is broken down into three successive stages represented by three referenced illustrations. (a), (b) and (c) of the figure
6. 6.
La première étape, représentée par l’illustration (a), comprend un positionnement de la première tranche 61 de l’organe d’assemblage 5 contre le bord 48 du dispositif de blocage 47. La dimension L de l’organe d’assemblage 5 étant supérieure à la dimension 1 mesurée entre boîtier 2 et renfort périphérique 45, l’organe d’assemblage 5 est incliné par rapport au plan dans lequel s’étend majoritairement de la bride d’accostage 4. Un angle non nul est ainsi formé entre la section centrale 51 de l’organe d’assemblage 5 et le bord d’accostage 43 de la bride d’accostage 4. La deuxième étape, représentée par l’illustration (b), comprend une action compressive 7 qui s’exerce sur la section centrale 51 de l’organe d’assemblage 5 et particulièrement au niveau de l’angle formé par la section centrale 51 et la première section latérale 58. Cette action compressive 7 est orientée vers la bride d’accostage 4 et a pour objectif de conduire la section centrale 51 de l’organe d’assemblage 5 vers le bord d’accostage 43 de la bride d’accostage 4. Ce faisant, un appui est généré entre une face intérieure 213 du flanc 21 et la face interne 46 de la bride d’accostage 4 au niveau du bord plié 41. La zone de connexion 65 est le siège de cet appui. The first step, represented by the illustration (a), comprises a positioning of the first portion 61 of the assembly member 5 against the edge 48 of the locking device 47. The dimension L of the assembly member 5 being greater than the dimension 1 measured between housing 2 and peripheral reinforcement 45, the assembly member 5 is inclined relative to the plane in which extends mainly from the docking flange 4. A non-zero angle is thus formed between the central section 51 of the assembly member 5 and the docking edge 43 of the docking flange 4. The second step, represented by the illustration (b), comprises a compressive action 7 which is exerted on the central section 51 of the assembly member 5 and particularly at the angle formed by the central section 51 and the first lateral section 58. This compressive action 7 is oriented towards the docking flange 4 and aims to drive the central section 51 of the assembly member 5 towards the docking edge 43 of the docking flange 4. In doing so, a support is generated between an inner face 213 of the flank 21 and the inner face 46 of the docking flange 4 at the folded edge 41. The connection zone 65 is the seat of this support.
La première section latérale 58, qui est initialement en contact instable avec la face extérieures 212 des flancs 21 du boîtier 2, glisse le long de cette face extérieure 212 jusqu’au placement de la section centrale 51 contre le face interne 46 de la bride d’accostage 4, au niveau du bord d’accostage 43 de celle-ci, comme cela ressort de l’illustration référencée (c). L’effort maximum est alors généré entre le boîtier 2 et la bride d’accostage 4, au niveau de la zone de connexion 65, ce qui garantit un contact continu sur toute la périphérie du bord plié 41 préalablement à l’étape de brasage, et ainsi un brasage continu et exempt de fuite au niveau de la zone de connexion 65.  The first lateral section 58, which is initially in unstable contact with the outer face 212 of the flanks 21 of the casing 2, slides along this outer face 212 to the placement of the central section 51 against the inner face 46 of the flange. 4, at the docking edge 43 thereof, as shown in the illustration referenced (c). The maximum force is then generated between the housing 2 and the docking flange 4, at the connection zone 65, which ensures continuous contact over the entire periphery of the folded edge 41 prior to the soldering step, and thus continuous and leak-free brazing at the connection area 65.
Une étape de verrouillage de l’organe d’assemblage 5 contre la bride d’accostage 4 est alors mise en œuvre, à l’aide du dispositif de blocage 47 et du moyen de verrouillage 62 détaillés plus haut.  A step of locking the assembly member 5 against the docking flange 4 is then implemented with the aid of the locking device 47 and the locking means 62 detailed above.
On comprend à la lecture de ce qui précède que la présente invention propose un dispositif de refroidissement d’un air d’admission d’un moteur à combustion interne configuré pour fiabiliser son étanchéité. Ce dispositif de refroidissement, destiné à être intégré dans un circuit d’air d’admission et un circuit de fluide caloporteur d’un véhicule thermique, offre une solution facile à mettre en œuvre et à moindre coût pour garantir un contact entre boîtier et bride d’accostage qui assure une parfaite étanchéité. On évite ainsi une mise au rebut de produits finis, après que ceux-ci aient subi une étape de brasage coûteuse.  It is understood from the foregoing that the present invention provides a cooling device of an intake air of an internal combustion engine configured to make its sealing more reliable. This cooling device, intended to be integrated in an intake air circuit and a heat transfer fluid circuit of a thermal vehicle, offers an easy solution to implement and at a lower cost to guarantee a contact between the housing and the flange. docking that ensures a perfect seal. This avoids the disposal of finished products, after they have undergone an expensive soldering step.
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 l’organe d’assemblage et/ou la forme de la bride d’accostage peuvent être modifiées 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 connecting member and / or 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 (i) d’un air d’admission d’un moteur à combustion interne, le dispositif de refroidissement (î) 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 le dispositif de refroidissement (1) comprend un organe d’assemblage (5), le boîtier (2) étant au moins en partie interposé entre la bride d’accostage (4) et l’organe d’assemblage (5). 1. Cooling device (i) of 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 cooling device (1) comprises an assembly member (5), the housing (2) being at least partially interposed between the docking flange (4) and the connecting member (5). ).
2. Dispositif de refroidissement (1) selon la revendication précédente, dans lequel l’organe d’assemblage (5) s’étend dans une cavité (10) délimitée par la bride d’accostage (4).  2. Cooling device (1) according to the preceding claim, wherein the connecting member (5) extends into a cavity (10) defined by the docking flange (4).
3. Dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, caractérisée en ce que la bride d’accostage (4) comprend un bord plié (41) et un renfort périphérique (45) reliés l’un à l’autre par un bord d’accostage (43), l’organe d’assemblage (5) étant en contact avec le bord d’accostage (43) de la bride d’accostage (4).  3. Cooling device (1) according to any one of the preceding claims, characterized in that the docking flange (4) comprises a folded edge (41) and a peripheral reinforcement (45) connected to one another. other by a docking edge (43), the connecting member (5) being in contact with the docking edge (43) of the docking flange (4).
4. Dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, caractérisé en ce que l’organe d’assemblage (5) comprend une section centrale (51), une première section latérale (58) et une seconde section latérale (59) ainsi qu’une section centrale (51) reliant la première section latérale (58) à la seconde section latérale (59), la première section latérale (58), la section centrale (51) et la seconde section latérale (59) étant conformées en « U ».  4. Cooling device (1) according to any one of the preceding claims, characterized in that the assembly member (5) comprises a central section (51), a first lateral section (58) and a second lateral section. (59) and a central section (51) connecting the first lateral section (58) to the second lateral section (59), the first lateral section (58), the central section (51) and the second lateral section (59). ) being shaped in "U".
5. Dispositif de refroidissement (1) selon la revendication précédente en combinaison avec la revendication 3, caractérisé en ce qu’une dimension (L) de l’organe d’assemblage (5), mesurée entre la première section latérale (58) et la seconde section latérale (59), est supérieure à une dimension (1) mesurée entre le boîtier (2) et le renfort périphérique (45).  5. Cooling device (1) according to the preceding claim in combination with claim 3, characterized in that a dimension (L) of the connecting member (5), measured between the first lateral section (58) and the second lateral section (59) is greater than one dimension (1) measured between the housing (2) and the peripheral reinforcement (45).
6. Dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, caractérisé en ce que la bride d’accostage (4) comprend au moins un moyen de fixation (44) et en ce que l’organe d’assemblage (5) comprend au moins un orifice (57) superposé au moyen de fixation (44) de la bride d’accostage (4).  Cooling device (1) according to one of the preceding claims, characterized in that the docking flange (4) comprises at least one fastening means (44) and in that the connecting member (4) 5) comprises at least one orifice (57) superimposed on the attachment means (44) of the docking flange (4).
7. Dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, caractérisée en ce que le boîtier (2) comprend un moyen de verrouillage (62) contre lequel l’organe d’assemblage (5) prend appui. Cooling device (1) according to one of the preceding claims, characterized in that the housing (2) comprises a locking means (62) against which the assembly member (5) bears.
8. Dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, caractérisé en ce que la bride d’accostage (4) comprend un dispositif de blocage (47) contre lequel l’organe d’assemblage (5) prend appui.  8. Cooling device (1) according to any one of the preceding claims, characterized in that the docking flange (4) comprises a locking device (47) against which the connecting member (5) is supported .
9. Procédé d’assemblage d’un boîtier (2) et d’une bride d’accostage (4) d’un dispositif de refroidissement (1) selon l’une quelconque des revendications précédentes, au cours duquel : on positionne une face intérieure (211) du boîtier (2) contre un bord plié (41) de la bride d’accostage (4), - on bloque une seconde section latérale (59) de l’organe d’assemblage (5) contre la bride d’accostage (4), on exerce un effort sur l’organe d’assemblage (5) jusqu’à ce qu’une première section latérale (58) comprime le boîtier (2) contre le bord plié (41).  9. A method of assembling a housing (2) and a docking flange (4) of a cooling device (1) according to any one of the preceding claims, in which: one face is positioned interior (211) of the housing (2) against a folded edge (41) of the docking flange (4), - a second lateral section (59) of the assembly member (5) is locked against the flange of (4), a force is exerted on the assembly member (5) until a first lateral section (58) compresses the casing (2) against the folded edge (41).
10. Procédé de fabrication d’un dispositif de refroidissement (1) d’un air d’admission selon l’une quelconque des revendications 1 à 8, comprenant au moins : 10. A method of manufacturing a cooling device (1) of an intake air according to any one of claims 1 to 8, comprising at least:
-une étape d’assemblage du corps de faisceau (3),  a step of assembling the beam body (3),
-une étape de positionnement du corps de faisceau (3) dans le boîtier (2),  a step of positioning the beam body (3) in the housing (2),
-une étape d’assemblage du boîtier (2) et de la bride d’accostage (4),  a step of assembling the housing (2) and the docking flange (4),
-une étape de serrage du boîtier (2) contre la bride d’accostage (4) au moyen d’un organe d’assemblage (5),  a step of clamping the casing (2) against the docking flange (4) by means of an assembly member (5),
-une étape de brasage simultanée au moins du boîtier (2), de la bride d’accostage (4) et de l’organe d’assemblage (5).  a simultaneous soldering step at least of the housing (2), the docking flange (4) and the assembly member (5).
PCT/FR2019/050635 2018-03-23 2019-03-20 Intake air cooling device for an internal combustion engine WO2019180378A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1852523A FR3079266B1 (en) 2018-03-23 2018-03-23 DEVICE FOR COOLING AN INTAKE AIR OF AN INTERNAL COMBUSTION ENGINE
FR1852523 2018-03-23

Publications (1)

Publication Number Publication Date
WO2019180378A1 true WO2019180378A1 (en) 2019-09-26

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Application Number Title Priority Date Filing Date
PCT/FR2019/050635 WO2019180378A1 (en) 2018-03-23 2019-03-20 Intake air cooling device for an internal combustion engine

Country Status (2)

Country Link
FR (1) FR3079266B1 (en)
WO (1) WO2019180378A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2985186B2 (en) * 1989-08-09 1999-11-29 株式会社デンソー Heat exchanger
EP1736348A2 (en) * 2005-06-21 2006-12-27 AGCO GmbH Radiator module for commercial motor vehicles
EP2295916A2 (en) * 2009-07-29 2011-03-16 Behr GmbH & Co. KG Stacked plate cooler, use of same and combustion engine with a stacked plate cooler

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2985186B2 (en) * 1989-08-09 1999-11-29 株式会社デンソー Heat exchanger
EP1736348A2 (en) * 2005-06-21 2006-12-27 AGCO GmbH Radiator module for commercial motor vehicles
EP2295916A2 (en) * 2009-07-29 2011-03-16 Behr GmbH & Co. KG Stacked plate cooler, use of same and combustion engine with a stacked plate cooler

Also Published As

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FR3079266B1 (en) 2020-03-06
FR3079266A1 (en) 2019-09-27

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