EP0839273B1 - Intake manifold for internal combustion engine - Google Patents

Intake manifold for internal combustion engine Download PDF

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Publication number
EP0839273B1
EP0839273B1 EP96919876A EP96919876A EP0839273B1 EP 0839273 B1 EP0839273 B1 EP 0839273B1 EP 96919876 A EP96919876 A EP 96919876A EP 96919876 A EP96919876 A EP 96919876A EP 0839273 B1 EP0839273 B1 EP 0839273B1
Authority
EP
European Patent Office
Prior art keywords
tube
cradle
tubes
envelope
outlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP96919876A
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German (de)
French (fr)
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EP0839273A1 (en
Inventor
Michäel PONTOPPIDAN
Georges Evieux
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Marelli France SAS
Original Assignee
Magneti Marelli France SAS
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Publication date
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Publication of EP0839273A1 publication Critical patent/EP0839273A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/1034Manufacturing and assembling intake systems
    • F02M35/10354Joining multiple sections together
    • F02M35/1036Joining multiple sections together by welding, bonding or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10006Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
    • F02M35/10026Plenum chambers
    • F02M35/10039Intake ducts situated partly within or on the plenum chamber housing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10006Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
    • F02M35/10078Connections of intake systems to the engine
    • F02M35/10085Connections of intake systems to the engine having a connecting piece, e.g. a flange, between the engine and the air intake being foreseen with a throttle valve, fuel injector, mixture ducts or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10314Materials for intake systems
    • F02M35/10321Plastics; Composites; Rubbers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/1034Manufacturing and assembling intake systems
    • F02M35/10347Moulding, casting or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/104Intake manifolds
    • F02M35/108Intake manifolds with primary and secondary intake passages

Definitions

  • the invention relates to an intake manifold, for internal combustion engine fitted with an installation fuel supply preferably by injection, particular of the type called "multipoint", comprising, for each engine cylinder, at least one injector which injects fuel in a manifold suction line air intake to the engine, directly upstream of the engine cylinder head and intake valve (s) corresponding cylinder.
  • the outer part, relative to the center of curvature of the bent tubes, of all the air tubes can be formed by hollow molded impression bottoms in each of the two half-shells, and which extend when the half-shells are closed against each other the other.
  • the inner part of all the air tubes can be formed by the bottoms molded imprints in two molded inserts, in general in the same material as the half-shells, for example in polyamide loaded with reinforcing fibers, and each reported in one of the half-shells respectively, so that the imprints of the inserts also extend during the joining of the half-shells one against the other. This process therefore makes it possible to form the tubes by cooperation of surfaces presented by at least four molded parts (two half-shells and two inserts) which are associated.
  • a collector thus produced is suitable for the equipment of a diesel engine, due to the low pressure gradient between the atmosphere and the plenum of the collector, in operation of the motor.
  • each tube air is either in one piece with the desired shape, as already mentioned above, either made by assembling two complementary halves molded into shape. But this assembly, despite the precautions taken, does not generally not allow to obtain an internal surface of each tube which be completely smooth and continuous, without roughness, from its entry to its exit, except to finish this surface by a special machining, when the geometry of the tubes permits.
  • the problem underlying the invention is to propose a collector of an advantageous structure, in particular for the connection of each tube to the manifold fixing flange to the engine cylinder head, the structure being essentially in a thermomouldable, semi-modular plastic, because acoustically adaptable to a whole family of displacement engines different by dimensional adjustment, and capable of being carried out by a more economical manufacturing process.
  • the intake manifold according to the invention is characterized in that the internal surface of each tube is smooth, and continues from its entry to its exit and in that each end piece is made with, on the one hand, a cradle in one piece with said mounting flange, and projecting from the side opposite the cylinder head, in the extension of said corresponding feed opening, the cradle being of substantially semi-cylindrical shape, the end internal to said envelope has an annular bottom forming an inwardly projecting stop of the cradle, and, on the other hand, a jumper for holding said tube in said cradle, the rider having a stop protruding towards the inside of the cradle and opposite the annular bottom of the cradle, a ring being attached and fixed around said tube, near its air outlet, said flexible seal being attached around said tube, between said ring and said air outlet of the tube, the outlet end portion of said tube with said ring and said seal sealing being in place in said corresponding
  • the characteristic that the internal surface of each tube is smooth and continuous from entry to exit should be understood as meaning that this internal surface has no roughness or unevenness, between two adjacent parts of internal surface, which is greater than about 200 ⁇ m.
  • the intake manifold according to the invention is distinguished essentially state-of-the-art collectors by manufacturing air intake tubes and by the connection of each tube to the fixing flange from the manifold to the engine cylinder head.
  • the intake manifold according to the invention is advantageously such that its envelope includes two molded half-shells, of shapes complementary to the shape of the envelope, and arranged one against each other and joined to each other by their peripheral rim, in a joint plane, to form the envelope with the tubes between them, each tube being blow molded, and preferably by suction-blowing, in a material thermally moldable plastic, and said fixing flange being in one piece with one of the half-shells.
  • each tube is made with a section gradually decreasing downstream on at least part of its length and / or with a converging air inlet, shaped tulip; each tube can be made with a section having substantially the same shape from entry to exit air, and which can be a circular section or, advantageously as specified below, an oblong section.
  • the tubes are grouped at least in pairs of tubes attached to at at least part of their length, and the tubes of each group of tubes are fixed in the same half-shell provided a mounting flange with supply openings to which the tubes of said group are connected with sealing, using at least a second jumper which transversely overlaps the joined tubes of said group, in their adjoining part, which is fixed by its ends on said half-shell.
  • each tube is made with an oblong section and parallel flats to the major axis of its section, on its opposite opposite faces, and the tubes are grouped together by being joined by their flats.
  • the half-shells with their bases, on the one hand, and the second jumpers, on the other hand may be molded plastic parts, and the second jumpers can be fixed on a half-shell corresponding by welding or gluing.
  • the tubes can be made curved with a radius of curvature, in the plane containing their axis, lower than that of the envelope, the envelope half-shells being molded of material plastic with clamps on their edges in the joint plane, and the half-shells are secured together to form the envelope by welding, preferably by vibration, at the clamps.
  • this geometry of the tubes bent by relation to the geometry of the envelope, as well as the mode of fixing of the tubes in the half-shells, which avoid contact points, and therefore friction between the tubes and the half-shells allow the half-shells to be joined together economically, by vibration welding at the level of their fastening flanges, a known manner, without risk of rupture of the tubes.
  • each end piece ensures the retaining a corresponding tube on one of the half-shells which each cradle is integral with.
  • seal sealing when the tubes are of section transverse circular, sealing can be ensured between the outlet end portion of each tube and the corresponding end piece by axial compression of said seal sealing, which is cylindrical, by its planar faces end between a flat radial face, facing the tube outlet, tube ring and a radial face flat, facing inward of said envelope, cradle and said flange, said radial faces being substantially perpendicular to the axis of the tube at its exit.
  • each cradle and the corresponding jumper are molded so that the tip formed by the cradle and the rider has a cross section gradually evolving from a shape circular, on the side of the mounting flange and its circular feed opening, oblong in shape, complementary to that of the tubes.
  • the seal between the end part outlet of each tube and the corresponding nozzle is advantageously provided by radial compression of said seal sealing between, on the one hand, the tube, and, on the other hand, the cradle and the corresponding rider.
  • the manifold of Figures 1 and 2 for a motor with four cylinders in line, includes a rigid casing 1, made of moldable and heat-sealable plastic of two half-shells 2 and 3, each molded in this material, having complementary shapes which correspond to the shape of the envelope 1.
  • the two half-shells 2 and 3 close against each other, by their edges peripherals, to reconstruct the shape of envelope 1, and are joined to each other in a joint plane P, defined by fastening flanges 4 and 5, in protruding outwards on their edges, by welding vibrations at these flanges 4 and 5, after assembly in the half-shells 2 and 3 of four suction tubes air (one per engine cylinder), grouped in two pairs of attached tubes, as shown in Figure 2 and described below with reference to Figures 6 to 8.
  • the flange 6 has, for each cylinder of the motor, a feed opening 7, coming from molding, circular cross section, which opens on one side into the flat face 8 for fixing the flange 6 to the cylinder head of the motor and, on the other side, inside the half-shell 3, lower in FIG.
  • the flange 6 also has, for each cylinder, a housing 9 for an injector of fuel, this housing 9 opening in the face 10 of the flange 6 which is opposite to the face 8 for fixing to the cylinder head, and outside the half-shell 3, on the one hand, and, on the other hand, each housing 9 opens into a corresponding feed opening 7.
  • the flange 6 finally has holes 11, also from molding like openings 7 and housings 9, for passage of collector fixing elements on the cylinder head.
  • the collector also includes a curved tube air intake for each cylinder, or, as already mentioned, four air tubes grouped into two pairs of tubes joined together over part of their length.
  • Each tube such as tube 12 in Figure 6, is a curved tube molded in one piece from a material blow molded plastic, or more precisely by the known process of suction-blowing.
  • a light, relatively rigid, thin-walled tube 12 and waterproof with smooth internal and external surfaces.
  • the internal surface of the tube 12 is smooth and continues from entry to exit. By smooth and continuous, it should be understood that this internal surface does not have roughness or unevenness between two adjacent parts with a surface that is greater than about 200 ⁇ m.
  • each tube such as 12 is molded with a volute or tulip shaped air inlet 13 converging downstream, and the cross-sectional area of the tube gradually decreases from its entry 13 to its exit 14, from preferably around 10% of its input cross-section, while that the shape of the section of the tube is constant input 13 to its output 14, and, in this example, is a oblong shape, visible in FIGS. 7 and 8, the wall of each tube having two opposite flats 15 parallel to the major axis 16 of the oblong section of the tube.
  • Each tube as that 12 is bent in an almost complete loop in the plane of Figure 6, over most of its length from its entry 13, and its downstream part is more bent or bent in a direction perpendicular to the plan of Figure 6, as shown in Figures 2 and 7.
  • two tubes such as 12a and 12b, grouped into a pair of tubes to supply each one of two cylinders respectively adjacent, can be joined by their flats 15 on the most of their length from their entrances 13a and 13b (see Figure 8), while their outputs 14a and 14b (see Figure 7) are separated from each other to be each tightly connected to one respectively two adjacent supply openings 7 one of the other in the flange 8 to supply the two cylinders correspondents.
  • each of the tubes 12a and 12b is introduced into a cradle 20a and 20b respectively molded in one piece with the half-shell 3 and the flange 6.
  • This cradle 20a, 20b protrudes from the flange 6 on the side opposite the cylinder head of the engine and substantially in the shape of an open semi-cylinder towards the joint plane P and delimiting a central duct which extends a corresponding opening 7 towards the inside of the half-shell 3.
  • each cradle 20a, 20b has an annular chamber delimited by an annular bottom 21a, 21b projecting radially towards the inside of the cradle 20a, 20b, to form a stop opposing the axial exit of the ring 17 and the seal 18 on the outlet end of the tube 12a, 12b.
  • the seal 18 (such as 18a, 18b or 18c), around the tube is compressed radially between the tube and the cradle 20a, 20b.
  • This jumper 22a, 22b is molded in plastic material and welded by ultrasound on its periphery on the edges of the cradle 20a or 20b. Maintaining the tube and sealing its connection to the corresponding opening 7 are thus ensured thanks to the gasket and a manifold tip, formed by the cradle 20a or 20b and the rider 22a or 22b corresponding, the latter having, as shown on the sections Figures 4 and 5, a recess complementary to that of cradle 20a or 20b to define a section duct progressively variable connecting the oblong outlet 14a or 14b from the tube to the circular section of the opening 7 corresponding, as represented by the section of the figure 3.
  • the cradle 20a, 20b as well as the rider 22a, 22b corresponding are molded so that their recesses present this corresponding section evolution.
  • the two tubes 12a and 12b are also retained in the downstream half-shell 3 by a second jumper 24, also molded from plastic, which overlaps transversely these two tubes 12a and 12b in their part attached, and is preferably fixed by stoppers in plastic material 25, projecting towards the joint plane P in the half-shell 3, and engaged in orifices at ends of the second jumper 24, to then be crushed thermally on the latter.
  • the jumper 24 maintains the tubes 12a and 12b applied against a base 26 of support, formed by an extra thickness of the half-shell 3, projecting towards the interior of the latter.
  • tubes 12a and 12b were molded by blowing with a general radius of curvature which is less at the radius of curvature of the rounded parts of the half-shells 2 and 3 of envelope 1, this avoids contacts and friction between the tubes and the half-shell upstream 2, during vibration welding of the two half-shells 2 and 3 against each other, which imposes small relative alternating displacements of the half-shells 2 and 3 causing friction between the flanges 4 and 5 leading to a heat seal.
  • the contacts between the tubes and the downstream half-shell 3 are limited to contact with the jumper 24 and the base 25 and in contact with the ring 17 of the outlet end of the tubes 12a, 12b with the tubular end piece constituted by the cradle 20a or 20b and the jumper 22a or 22b, so that we avoid any possible source of disruptive friction between tubes and the two parts of the envelope, which can lead to ruptures during the vibration welding phase, which constitutes the final assembly phase of the collector.
  • a collector is thus obtained, the envelope 1 of which delimits an internal chamber 27, called plenum, which is supplied with engine feed air through an opening (not shown) for example formed in the center of a end face of the envelope 2 parallel to the plane of Figure 1, this opening being connected to a body of butterfly.
  • Each tube such as 12a or 12b mounted in the envelope 1 draws air into plenum 27 through its inlet 13a or 13b and transmits this air through its outlet 14a or 14b to a supply opening 7 of the flange 6 for supplying a corresponding cylinder.
  • envelope 1 contains, in its half not shown in Figure 2, two other symmetrical air intake tubes 12a and 12b and mounted in the same way.
  • the tubes 12'a and 12'b are of section transverse circular. However, they are also joined for part of their length and are applied by a jumper 24 'against a support base 26' to inside the downstream half-shell 3 ', the jumper 24' being, as in the previous example, fixed by bolting or heat sealing on pins 25 'of this half-shell 3 '.
  • the outlet ends of the tubes 12'a and 12'b are surrounded by a 17 'ring and a seal flexible 18 'and are each connected so watertight at a corresponding opening 7 'of the flange of fixing 6 'to the cylinder head by a tubular end piece.
  • the latter consists of a cradle 20'a or 20'b of U-shaped cross section and value constant, with an annular bottom forming a radial stop internal 21'a or 21'b, on the side of the half-shell 3 ', thus than a basically flat rider 22'a or 22'b with a 23'a or 23'b arc-shaped abutment projecting inwards of the cradle 20'a or 20'b and opposite the annular bottom 21'a or 21'b of the latter.
  • the manifold tip as well made for each outlet end of a 12'a tube or 12'b is preferably of circular cross-section of diameter constant, with one face, oriented towards the corresponding tube which is flat and perpendicular to the axis of the tube in its outlet end part.
  • the cylindrical seal 18 ' is, in this example, compressed axially by its two radial and planar end faces between, of a side, the planar radial face of the ring 17 'which is turned towards the flange 6 'and, on the other side, a radial face flat, facing inward of the 3 'half-shell, in the bottom of the corresponding cradle 20'a or 20'b, on the flange 6 ', these different radial faces being substantially perpendicular to the axis of the tube 12'a or 12'b at its outlet.
  • the tubes as the half-shells can be made in one plastic material such as polyamide, loaded with fibers reinforcement.

Abstract

Between the two half-molds (2, 3) fixed against each other in order to form an envelope (1), one-piece blow-molded air tubes (12a, 12b) are mounted; the outlet (14a, 14b) of the tubes is held in a half-mold (3) by means of a fixing clamp (6) to the cylinder-head of the engine while being sealingly connected to an opening (7) of the clamp (6) for supplying one cylinder by means of a tubular nozzle formed of a cradle (20a, 20b) molded with the clamp (6) and the half-mold (3), and a staple (22a, 22b) fixed to the cradle to hold a ring (17) on the outlet of the tube while compressing a seal (18) between the tubes (12a, 12b) and the nozzle. Application particularly to intake manifolds of engines with multipoint injection and controlled ignition.

Description

L'invention concerne un collecteur d'admission, pour moteur à combustion interne équipé d'une installation d'alimentation en carburant de préférence par injection, en particulier du type dit "multipoint", comportant, pour chaque cylindre du moteur, au moins un injecteur qui injecte du carburant dans un conduit d'aspiration du collecteur d'admission d'air au moteur, directement en amont de la culasse du moteur et de la ou des soupapes d'admission du cylindre correspondant.The invention relates to an intake manifold, for internal combustion engine fitted with an installation fuel supply preferably by injection, particular of the type called "multipoint", comprising, for each engine cylinder, at least one injector which injects fuel in a manifold suction line air intake to the engine, directly upstream of the engine cylinder head and intake valve (s) corresponding cylinder.

Plus précisément, l'invention se rapporte à un tel collecteur d'admission, plus particulièrement destiné à équiper un moteur à allumage commandé, et qui comprend, comme connu par US-A-5,003,933 :

  • une enveloppe, délimitant un plenum destiné à être alimenté en air d'alimentation du moteur par une vanne à débit variable, telle qu'un corps de papillon, et munie d'au moins une bride de fixation à une culasse du moteur, la ou lesdites brides présentant au moins une ouverture d'alimentation de chaque cylindre du moteur, chaque ouverture d'alimentation débouchant, d'une part, dans l'enveloppe et, d'autre part, dans une face de fixation de la bride sur ladite culasse, et
  • des tubes d'aspiration d'air recourbés, chacun d'une seule pièce à la forme voulue, en nombre au moins égal à celui des cylindres du moteur, et montés dans l'enveloppe, de sorte que chaque tube alimente un cylindre correspondant en air que le tube reçoit par son entrée dans le plenum et que le tube transmet à une ouverture correspondante d'une bride par sa sortie reliée à ladite ouverture d'alimentation par des moyens de raccordement étanches comprenant un embout tubulaire dans lequel la partie d'extrémité de sortie dudit tube est retenue dans ladite enveloppe, avec interposition d'au moins un joint d'étanchéité souple entre le tube et l'embout.
More specifically, the invention relates to such an intake manifold, more particularly intended to equip a spark-ignition engine, and which comprises, as known by US-A-5,003,933:
  • an envelope, delimiting a plenum intended to be supplied with air supplying the engine by a variable flow valve, such as a throttle body, and provided with at least one clamp for fixing to a cylinder head of the engine, the or said flanges having at least one supply opening for each cylinder of the engine, each supply opening opening, on the one hand, into the casing and, on the other hand, into a face for fixing the flange to said cylinder head , and
  • curved air suction tubes, each in one piece with the desired shape, in number at least equal to that of the engine cylinders, and mounted in the envelope, so that each tube feeds a corresponding cylinder in air which the tube receives by its entry into the plenum and which the tube transmits to a corresponding opening of a flange by its outlet connected to said supply opening by sealed connection means comprising a tubular end piece in which the part of outlet end of said tube is retained in said envelope, with the interposition of at least one flexible seal between the tube and the end piece.

On sait déjà fabriquer des collecteurs analogues en moulant deux demi-coquilles de formes complémentaires correspondant à la forme de l'enveloppe et destinées à être solidarisées l'une contre l'autre par leur rebord périphérique, dans un plan de joint, pour former l'enveloppe.We already know how to manufacture similar collectors in molding two half-shells of complementary shapes corresponding to the shape of the envelope and intended to be joined together by their peripheral rim, in a parting line, to form the envelope.

La partie extérieure, par rapport au centre de courbure des tubes recourbés, de l'ensemble des tubes d'air peut être formée par les fonds d'empreintes moulées en creux dans chacune des deux demi-coquilles, et qui se prolongent lorsque les demi-coquilles sont refermées l'une contre l'autre. De manière analogue, la partie intérieure de l'ensemble des tubes d'air peut être formée par les fonds d'empreintes moulées en creux dans deux inserts moulés, en général dans la même matière que les demi-coquilles, par exemple en polyamide chargé de fibres de renfort, et chacun rapporté dans l'une respectivement des demi-coquilles, de sorte que les empreintes des inserts se prolongent également lors de la solidarisation des demi-coquilles l'une contre l'autre. Ce procédé permet donc de former les tubes par coopération de surfaces présentées par au moins quatre pièces moulées (deux demi-coquilles et deux inserts) qui sont associées.The outer part, relative to the center of curvature of the bent tubes, of all the air tubes can be formed by hollow molded impression bottoms in each of the two half-shells, and which extend when the half-shells are closed against each other the other. Similarly, the inner part of all the air tubes can be formed by the bottoms molded imprints in two molded inserts, in general in the same material as the half-shells, for example in polyamide loaded with reinforcing fibers, and each reported in one of the half-shells respectively, so that the imprints of the inserts also extend during the joining of the half-shells one against the other. This process therefore makes it possible to form the tubes by cooperation of surfaces presented by at least four molded parts (two half-shells and two inserts) which are associated.

Un collecteur ainsi réalisé convient à l'équipement d'un moteur diesel, en raison du faible gradient de pression entre l'atmosphère et le plenum du collecteur, en fonctionnement du moteur.A collector thus produced is suitable for the equipment of a diesel engine, due to the low pressure gradient between the atmosphere and the plenum of the collector, in operation of the motor.

Par contre, dans un moteur à allumage commandé, où ce gradient de pression peut atteindre des valeurs moyennes plus importantes, de l'ordre de 70 kPa, en fonctionnement du moteur, la présence de fuites d'air entre les pièces assemblées pour former les tubes d'aspiration d'air contenus à l'intérieur du plenum a pour effet de modifier l'impédance acoustique du collecteur, d'où une baisse du rendement du moteur.On the other hand, in a spark ignition engine, where this pressure gradient can reach average values larger, around 70 kPa, when the engine, the presence of air leaks between the parts assembled to form contained air suction tubes inside the plenum has the effect of modifying the impedance collector acoustics, resulting in a drop in the efficiency of the engine.

Il est donc impératif que, dans un collecteur de ce type, une bonne étanchéité, en particulier au niveau des tubes d'air, soit assurée.It is therefore imperative that in a collector of this type, good tightness, especially at the air tubes, be assured.

A cet effet, on doit réaliser un joint d'étanchéité entre les inserts et les demi-coquilles par la pose de cordons d'un matériau polymérisable approprié, ce qui est une opération longue et délicate, s'ajoutant à la difficulté de réalisation avec de faibles tolérances des quatre pièces à assembler pour définir avec précision les tubes d'air.For this purpose, a seal must be made between the inserts and the half-shells by laying strings of polymerizable material appropriate, which is a long and delicate operation, adding to the difficulty of realization with low tolerances of the four parts to be assembled for precisely define the air tubes.

Dans le cas d'un collecteur selon US-A-5,003,933, chaque tube d'air est soit d'une seule pièce à la forme voulue, comme déjà mentionné ci-dessus, soit réalisé par l'assemblage de deux moitiés complémentaires moulées en forme. Mais cet assemblage, malgré les précautions prises, ne permet généralement pas d'obtenir une surface interne de chaque tube qui soit totalement lisse et continue, sans aspérité, de son entrée à sa sortie, sauf à finir cette surface par un usinage particulier, lorsque la géométrie des tubes le permet.In the case of a collector according to US-A-5,003,933, each tube air is either in one piece with the desired shape, as already mentioned above, either made by assembling two complementary halves molded into shape. But this assembly, despite the precautions taken, does not generally not allow to obtain an internal surface of each tube which be completely smooth and continuous, without roughness, from its entry to its exit, except to finish this surface by a special machining, when the geometry of the tubes permits.

Il en résulte qu'un tel collecteur peut devenir d'une réalisation coûteuse.As a result, such a collector can become an achievement expensive.

Le problème à la base de l'invention est de proposer un collecteur d'une structure avantageuse, en particulier pour la liaison de chaque tube à la bride de fixation du collecteur à la culasse du moteur, la structure étant essentiellement en une matière plastique thermomoulable, et semi-modulable, car acoustiquement adaptable à toute une famille de moteurs de cylindrées différentes par ajustement dimensionnel, et susceptible d'être réalisée par un procédé de fabrication plus économique.The problem underlying the invention is to propose a collector of an advantageous structure, in particular for the connection of each tube to the manifold fixing flange to the engine cylinder head, the structure being essentially in a thermomouldable, semi-modular plastic, because acoustically adaptable to a whole family of displacement engines different by dimensional adjustment, and capable of being carried out by a more economical manufacturing process.

A cet effet, le collecteur d'admission selon l'invention, du type présenté ci-dessus, se caractérise en ce que la surface interne de chaque tube est lisse, et continue de son entrée à sa sortie et en ce que chaque embout est réalisé avec, d'une part, un berceau d'une seule pièce avec ladite bride de fixation, et en saillie du côté opposé à la culasse, dans le prolongement de ladite ouverture d'alimentation correspondante, le berceau étant de forme sensiblement hémi-cylindrique, dont l'extrémité interne à ladite enveloppe présente un fond annulaire formant butée en saillie vers l'intérieur du berceau, et, d'autre part, un cavalier de maintien dudit tube dans ledit berceau, le cavalier présentant une butée en saillie vers l'intérieur du berceau et en regard du fond annulaire du berceau, un anneau étant rapporté et fixé autour dudit tube, à proximité de sa sortie d'air, ledit joint d'étanchéité souple étant rapporté autour dudit tube, entre ledit anneau et ladite sortie d'air du tube, la partie d'extrémité de sortie dudit tube avec ledit anneau et ledit joint d'étanchéité étant en place dans ledit berceau correspondant, de sorte que l'anneau ou le joint est retenu par butée contre ledit fond annulaire du berceau, ledit cavalier étant rapporté sur ledit berceau et la partie du tube logée dans ce dernier, et étant fixé sur les bords du berceau.To this end, the intake manifold according to the invention, of the type presented above, is characterized in that the internal surface of each tube is smooth, and continues from its entry to its exit and in that each end piece is made with, on the one hand, a cradle in one piece with said mounting flange, and projecting from the side opposite the cylinder head, in the extension of said corresponding feed opening, the cradle being of substantially semi-cylindrical shape, the end internal to said envelope has an annular bottom forming an inwardly projecting stop of the cradle, and, on the other hand, a jumper for holding said tube in said cradle, the rider having a stop protruding towards the inside of the cradle and opposite the annular bottom of the cradle, a ring being attached and fixed around said tube, near its air outlet, said flexible seal being attached around said tube, between said ring and said air outlet of the tube, the outlet end portion of said tube with said ring and said seal sealing being in place in said corresponding cradle, so that the ring or the seal is retained by abutment against said annular bottom of the cradle, said rider being attached to said cradle and the part of the tube housed in the latter, and being fixed on the edges of the cradle.

La caractéristique selon laquelle la surface interne de chaque tube est lisse et continue de son entrée à sa sortie doit être comprise comme signifiant que cette surface interne ne présente pas d'aspérité ni de dénivellement, entre deux parties adjacentes de surface interne, qui soit supérieur(e) à environ 200ìm.The characteristic that the internal surface of each tube is smooth and continuous from entry to exit should be understood as meaning that this internal surface has no roughness or unevenness, between two adjacent parts of internal surface, which is greater than about 200ìm.

Les tubes d'air monoblocs étant par nature étanches, la nécessité de réaliser des cordons de joints d'étanchéité ou des soudures de liaison entre deux moitiés complémentaires disparait.Monoblock air tubes being inherently sealed, the need to make seams of joints or welds of connection between two complementary halves disappears.

Le collecteur d'admission selon l'invention se distingue essentiellement des collecteurs de l'état de la technique par la fabrication des tubes d'aspiration d'air et par la liaison de chaque tube à la bride de fixation du collecteur à la culasse du moteur.The intake manifold according to the invention is distinguished essentially state-of-the-art collectors by manufacturing air intake tubes and by the connection of each tube to the fixing flange from the manifold to the engine cylinder head.

Le collecteur d'admission selon l'invention est avantageusement tel que son enveloppe comprend deux demi-coquilles moulées, de formes complémentaires correspondant à la forme de l'enveloppe, et disposées l'une contre l'autre et solidarisées l'une à l'autre par leur rebord périphérique, dans un plan de joint, pour former l'enveloppe avec les tubes entre elles, chaque tube étant moulé par soufflage, et de préférence par aspiration-soufflage, dans une matière plastique thermomoulable, et ladite bride de fixation étant d'une seule pièce avec l'une des demi-coquilles.The intake manifold according to the invention is advantageously such that its envelope includes two molded half-shells, of shapes complementary to the shape of the envelope, and arranged one against each other and joined to each other by their peripheral rim, in a joint plane, to form the envelope with the tubes between them, each tube being blow molded, and preferably by suction-blowing, in a material thermally moldable plastic, and said fixing flange being in one piece with one of the half-shells.

Avantageusement, le collecteur est en outre tel que chaque tube est réalisé avec une section progressivement décroissante vers l'aval sur au moins une partie de sa longueur et/ou avec une entrée d'air convergente, en forme de tulipe ; chaque tube peut être réalisé avec une section ayant sensiblement la même forme de son entrée à sa sortie d'air, et qui peut être une section circulaire ou, avantageusement comme précisé ci-dessous, une section oblongue.Advantageously, the collector is further such that each tube is made with a section gradually decreasing downstream on at least part of its length and / or with a converging air inlet, shaped tulip; each tube can be made with a section having substantially the same shape from entry to exit air, and which can be a circular section or, advantageously as specified below, an oblong section.

Avantageusement, ' en outre, pour faciliter la fixation des tubes d'air dans les demi-coquilles, les tubes sont groupés au moins par paires de tubes accolés sur au moins une partie de leur longueur, et les tubes de chaque groupe de tubes sont fixés dans une même demi-coquille munie d'une bride de fixation avec des ouvertures d'alimentation auxquelles les tubes dudit groupe sont raccordés avec étanchéité, à l'aide d'au moins un second cavalier qui chevauche transversalement les tubes accolés dudit groupe, dans leur partie accolée, et qui est fixé par ses extrémités sur ladite demi-coquille.Advantageously, 'in addition, to facilitate the fixing the air tubes in the half-shells, the tubes are grouped at least in pairs of tubes attached to at at least part of their length, and the tubes of each group of tubes are fixed in the same half-shell provided a mounting flange with supply openings to which the tubes of said group are connected with sealing, using at least a second jumper which transversely overlaps the joined tubes of said group, in their adjoining part, which is fixed by its ends on said half-shell.

A cet effet, il est avantageux que chaque tube soit réalisé avec une section oblongue et des méplats, parallèles au grand axe de sa section, sur ses faces en regard opposées, et les tubes sont groupés en étant accolés par leurs méplats.For this purpose, it is advantageous that each tube is made with an oblong section and parallel flats to the major axis of its section, on its opposite opposite faces, and the tubes are grouped together by being joined by their flats.

De manière simple, les demi-coquilles avec leurs embases, d'une part, et les seconds cavaliers, d'autre part, peuvent être des pièces moulées en matière plastique, et les seconds cavaliers peuvent être fixés sur une demi-coquille correspondante par soudage ou bouterollage.In a simple way, the half-shells with their bases, on the one hand, and the second jumpers, on the other hand, may be molded plastic parts, and the second jumpers can be fixed on a half-shell corresponding by welding or gluing.

Avantageusement de plus, les tubes peuvent être réalisés recourbés avec un rayon de courbure, dans le plan contenant leur axe, inférieur à celui de l'enveloppe, les demi-coquilles de l'enveloppe étant moulées en matière plastique avec des brides de solidarisation sur leurs bords dans le plan de joint, et les demi-coquilles sont solidarisées l'une à l'autre pour former l'enveloppe par soudage, de préférence par vibrations, au niveau des brides de solidarisation. En effet, cette géométrie des tubes recourbés par rapport à la géométrie de l'enveloppe, ainsi que le mode de fixation des tubes dans les demi-coquilles, qui évitent les points de contact, et donc de frottement entre les tubes et les demi-coquilles, permettent de solidariser les demi-coquilles de manière économique, par un soudage par vibrations au niveau de leurs brides de solidarisation, d'une manière connue, sans risque de rupture des tubes.Advantageously, the tubes can be made curved with a radius of curvature, in the plane containing their axis, lower than that of the envelope, the envelope half-shells being molded of material plastic with clamps on their edges in the joint plane, and the half-shells are secured together to form the envelope by welding, preferably by vibration, at the clamps. Indeed, this geometry of the tubes bent by relation to the geometry of the envelope, as well as the mode of fixing of the tubes in the half-shells, which avoid contact points, and therefore friction between the tubes and the half-shells, allow the half-shells to be joined together economically, by vibration welding at the level of their fastening flanges, a known manner, without risk of rupture of the tubes.

Avantageusement, en outre, chaque embout assure la retenue d'un tube correspondant sur l'une des demi-coquilles dont chaque berceau est solidaire.Advantageously, in addition, each end piece ensures the retaining a corresponding tube on one of the half-shells which each cradle is integral with.

En particulier, lorsque les tubes sont de section transversale circulaire, l'étanchéité peut être assurée entre la partie d'extrémité de sortie de chaque tube et l'embout correspondant par compression axiale dudit joint d'étanchéité, qui est cylindrique, par ses faces planes d'extrémité entre une face radiale plane, tournée vers la sortie du tube, de l'anneau du tube et une face radiale plane, tournée vers l'intérieur de ladite enveloppe, du berceau et de ladite bride, lesdites faces radiales étant sensiblement perpendiculaires à l'axe du tube à sa sortie.In particular, when the tubes are of section transverse circular, sealing can be ensured between the outlet end portion of each tube and the corresponding end piece by axial compression of said seal sealing, which is cylindrical, by its planar faces end between a flat radial face, facing the tube outlet, tube ring and a radial face flat, facing inward of said envelope, cradle and said flange, said radial faces being substantially perpendicular to the axis of the tube at its exit.

Par contre, lorsque les tubes d'air présentent avantageusement une section transversale oblongue, comme précisé ci-dessus, il est avantageux que chaque berceau et le cavalier correspondant soient moulés de sorte que l'embout formé par le berceau et le cavalier présente une section transversale évoluant progressivement d'une forme circulaire, du côté de la bride de fixation et de son ouverture d'alimentation circulaire, à une forme oblongue, complémentaire de celle des tubes.However, when the air tubes have advantageously an oblong cross section, as specified above, it is advantageous that each cradle and the corresponding jumper are molded so that the tip formed by the cradle and the rider has a cross section gradually evolving from a shape circular, on the side of the mounting flange and its circular feed opening, oblong in shape, complementary to that of the tubes.

Dans ce cas, l'étanchéité entre la partie d'extrémité de sortie de chaque tube et l'embout correspondant est avantageusement assurée par compression radiale dudit joint d'étanchéité entre, d'une part, le tube, et, d'autre part, le berceau et le cavalier correspondant.In this case, the seal between the end part outlet of each tube and the corresponding nozzle is advantageously provided by radial compression of said seal sealing between, on the one hand, the tube, and, on the other hand, the cradle and the corresponding rider.

D'autres caractéristiques et avantages de l'invention ressortiront de la description donnée ci-dessous, à titre non limitatif, d'exemples de réalisation décrits en référence aux dessins annexés sur lesquels :

  • la figure 1 est une vue en coupe transversale d'un collecteur pour moteur à quatre cylindres en ligne, la coupe étant sensiblement perpendiculaire à l'axe du moteur,
  • la figure 2 est une demi-vue en partie en élévation en plan et en partie en coupe de la demi-coquille aval ou inférieure du collecteur de la figure 1, avec une des deux paires de tubes qui sont regroupés et retenus dans cette demi-coquille,
  • les figures 3, 4 et 5 sont des coupes transversales respectivement selon III-III, IV-IV, V-V de la figure 1,
  • la figure 6 est une vue en coupe axiale d'un tube d'air,
  • la figure 7 est une vue en partie en coupe et en partie en élévation verticale de la paire des deux tubes regroupés représentés sur la figure 2, avant son montage dans la demi-coquille correspondante,
  • la figure 8 est une vue schématique de face des entrées d'air des deux tubes de la figure 7, vues selon la flèche de la figure 6,
  • les figures 9, 10 et 11 sont une vue et deux demi-vues schématiques représentant trois exemples de joints d'étanchéité souples comprimés radialement entre un tube et l'embout du collecteur correspondant,
  • les figures 12 et 13 sont des vues correspondant respectivement aux figures 1 et 2 pour un second exemple de réalisation,
  • les figures 14 et 15 sont des coupes transversales respectivement selon XIV-XIV et XV-XV de la figure 12, et
  • la figure 16 est une demi-vue en coupe schématique d'un joint d'étanchéité cylindrique comprimé axialement et monté entre un tube et l'embout du collecteur correspondant.
Other characteristics and advantages of the invention will emerge from the description given below, without implied limitation, of exemplary embodiments described with reference to the appended drawings in which:
  • FIG. 1 is a cross-sectional view of a manifold for an in-line four-cylinder engine, the section being substantially perpendicular to the axis of the engine,
  • Figure 2 is a half-view partly in plan elevation and partly in section of the downstream or lower half-shell of the collector of Figure 1, with one of the two pairs of tubes which are grouped and retained in this half shell,
  • FIGS. 3, 4 and 5 are cross sections respectively along III-III, IV-IV, VV of FIG. 1,
  • FIG. 6 is a view in axial section of an air tube,
  • FIG. 7 is a view partly in section and partly in vertical elevation of the pair of the two grouped tubes represented in FIG. 2, before its mounting in the corresponding half-shell,
  • FIG. 8 is a schematic front view of the air inlets of the two tubes of FIG. 7, seen along the arrow in FIG. 6,
  • FIGS. 9, 10 and 11 are a schematic view and two half-views showing three examples of flexible seals compressed radially between a tube and the end of the corresponding manifold,
  • FIGS. 12 and 13 are views corresponding respectively to FIGS. 1 and 2 for a second example of embodiment,
  • FIGS. 14 and 15 are cross sections respectively along XIV-XIV and XV-XV of FIG. 12, and
  • Figure 16 is a schematic half-sectional view of a cylindrical seal axially compressed and mounted between a tube and the tip of the corresponding manifold.

Le collecteur des figures 1 et 2, pour un moteur à quatre cylindres en ligne, comprend une enveloppe 1 rigide, en matière plastique moulable et thermosoudable, constituée de deux demi-coquilles 2 et 3, chacune moulée dans ce matériau, ayant des formes complémentaires qui correspondent à la forme de l'enveloppe 1. Les deux demi-coquilles 2 et 3 se referment l'une contre l'autre, par leurs rebords périphériques, pour reconstituer la forme de l'enveloppe 1, et sont solidarisées l'une à l'autre dans un plan de joint P, défini par des brides de solidarisation 4 et 5, en saillie vers l'extérieur sur leurs rebords, par soudage aux vibrations au niveau de ces brides 4 et 5, après montage dans les demi-coquilles 2 et 3 de quatre tubes d'aspiration d'air (un par cylindre du moteur), groupés en deux paires de tubes accolés, comme représenté sur la figure 2 et décrit ci-dessous en référence aux figures 6 à 8.The manifold of Figures 1 and 2, for a motor with four cylinders in line, includes a rigid casing 1, made of moldable and heat-sealable plastic of two half-shells 2 and 3, each molded in this material, having complementary shapes which correspond to the shape of the envelope 1. The two half-shells 2 and 3 close against each other, by their edges peripherals, to reconstruct the shape of envelope 1, and are joined to each other in a joint plane P, defined by fastening flanges 4 and 5, in protruding outwards on their edges, by welding vibrations at these flanges 4 and 5, after assembly in the half-shells 2 and 3 of four suction tubes air (one per engine cylinder), grouped in two pairs of attached tubes, as shown in Figure 2 and described below with reference to Figures 6 to 8.

La bride 5 de la demi-coquille 3, venant en regard de la bride 4 de la demi-coquille 2 sur toute la périphérie des demi-coquilles, est supportée, sur un côté de l'enveloppe 1, par la partie supérieure d'une bride 6 de fixation du collecteur à la culasse du moteur, cette bride 6 étant moulée d'une seule pièce avec la demi-coquille 3 et sa bride périphérique 5. La bride 6 présente, pour chaque cylindre du moteur, une ouverture d'alimentation 7, venue de moulage, de section transversale circulaire, qui débouche d'un côté dans la face plane 8 de fixation de la bride 6 sur la culasse du moteur et, de l'autre côté, à l'intérieur de la demi-coquille 3, inférieure sur la figure 1 et dite demi-coquille aval, car destinée à loger les parties aval des tubes d'air, par opposition à la demi-coquille 2 supérieure sur la figure 1, dite demi-coquille amont, car destinée à loger les parties amont des tubes d'air. La bride 6 présente également, pour chaque cylindre, un logement 9 pour un injecteur de carburant, ce logement 9 s'ouvrant dans la face 10 de la bride 6 qui est opposée à la face 8 de fixation à la culasse, et à l'extérieur de la demi-coquille 3, d'une part, et, d'autre part, chaque logement 9 débouche dans une ouverture d'alimentation 7 correspondante. La bride 6 présente enfin des trous 11, également venus de moulage comme les ouvertures 7 et logements 9, pour le passage d'organes de fixation du collecteur sur la culasse.The flange 5 of the half-shell 3, coming opposite of the flange 4 of the half-shell 2 over the entire periphery half-shells, is supported, on one side of the envelope 1, through the upper part of a fixing flange 6 from the manifold to the engine cylinder head, this flange 6 being molded in one piece with the half-shell 3 and its flange peripheral 5. The flange 6 has, for each cylinder of the motor, a feed opening 7, coming from molding, circular cross section, which opens on one side into the flat face 8 for fixing the flange 6 to the cylinder head of the motor and, on the other side, inside the half-shell 3, lower in FIG. 1 and called the half-shell downstream, since it is intended to house the downstream parts of the air tubes, as opposed to the upper half-shell 2 in the figure 1, called the upstream half-shell, since it is intended to house the upstream parts of the air tubes. The flange 6 also has, for each cylinder, a housing 9 for an injector of fuel, this housing 9 opening in the face 10 of the flange 6 which is opposite to the face 8 for fixing to the cylinder head, and outside the half-shell 3, on the one hand, and, on the other hand, each housing 9 opens into a corresponding feed opening 7. The flange 6 finally has holes 11, also from molding like openings 7 and housings 9, for passage of collector fixing elements on the cylinder head.

Le collecteur comprend également un tube recourbé d'aspiration d'air pour chaque cylindre, soit, comme déjà mentionné, quatre tubes d'air groupés en deux paires de tubes accolés sur une partie de leur longueur.The collector also includes a curved tube air intake for each cylinder, or, as already mentioned, four air tubes grouped into two pairs of tubes joined together over part of their length.

Chaque tube, tel que le tube 12 de la figure 6, est un tube recourbé moulé d'une seule pièce en une matière plastique thermomoulable par soufflage, ou plus précisément par le procédé connu d'aspiration-soufflage. On réalise ainsi un tube 12 léger, relativement rigide, à paroi mince et étanche, à surfaces interne et externe lisses. En particulier, la surface interne du tube 12 est lisse et continue de son entrée à sa sortie. Par lisse et continue, il faut comprendre que cette surface interne ne présente pas d'aspérité ni de dénivellement entre deux parties adjacentes de surface qui soit supérieur(e) à environ 200 µm.Each tube, such as tube 12 in Figure 6, is a curved tube molded in one piece from a material blow molded plastic, or more precisely by the known process of suction-blowing. We realize thus a light, relatively rigid, thin-walled tube 12 and waterproof, with smooth internal and external surfaces. In in particular, the internal surface of the tube 12 is smooth and continues from entry to exit. By smooth and continuous, it should be understood that this internal surface does not have roughness or unevenness between two adjacent parts with a surface that is greater than about 200 µm.

Dans cet exemple, chaque tube tel que 12 est moulé avec une entrée d'air 13 en forme de volute ou de tulipe convergente vers l'aval, et la surface de la section du tube diminue progressivement de son entrée 13 à sa sortie 14, de préférence de l'ordre de 10 % de sa section d'entrée, tandis que la forme de la section du tube est constante de son entrée 13 à sa sortie 14, et, dans cet exemple, est une forme oblongue, visible sur les figures 7 et 8, la paroi de chaque tube présentant deux méplats opposés 15 parallèles au grand axe 16 de la section oblongue du tube. Chaque tube tel que 12 est recourbé selon une boucle presque complète dans le plan de la figure 6, sur la majeure partie de sa longueur à partir de son entrée 13, et sa partie aval est de plus coudée ou contrecoudée dans une direction perpendiculaire au plan de la figure 6, comme représenté sur les figures 2 et 7. Grâce aux méplats 15 et à leurs formes recourbées, deux tubes tels que 12a et 12b, groupés en une paire de tubes pour alimenter chacun l'un respectivement de deux cylindres adjacents, peuvent être accolés par leurs méplats 15 sur la majeure partie de leur longueur à partir de leurs entrées 13a et 13b (voir figure 8), tandis que leurs sorties 14a et 14b (voir figure 7) sont écartées l'une de l'autre pour être chacune raccordée de manière étanche à l'une respectivement de deux ouvertures d'alimentation 7 voisines l'une de l'autre dans la bride 8 pour alimenter les deux cylindres correspondants.In this example, each tube such as 12 is molded with a volute or tulip shaped air inlet 13 converging downstream, and the cross-sectional area of the tube gradually decreases from its entry 13 to its exit 14, from preferably around 10% of its input cross-section, while that the shape of the section of the tube is constant input 13 to its output 14, and, in this example, is a oblong shape, visible in FIGS. 7 and 8, the wall of each tube having two opposite flats 15 parallel to the major axis 16 of the oblong section of the tube. Each tube as that 12 is bent in an almost complete loop in the plane of Figure 6, over most of its length from its entry 13, and its downstream part is more bent or bent in a direction perpendicular to the plan of Figure 6, as shown in Figures 2 and 7. Thanks to the 15 flats and their curved shapes, two tubes such as 12a and 12b, grouped into a pair of tubes to supply each one of two cylinders respectively adjacent, can be joined by their flats 15 on the most of their length from their entrances 13a and 13b (see Figure 8), while their outputs 14a and 14b (see Figure 7) are separated from each other to be each tightly connected to one respectively two adjacent supply openings 7 one of the other in the flange 8 to supply the two cylinders correspondents.

Un anneau 17, par exemple en matière plastique thermosoudable, de section interne correspondant en forme et en surface à la section externe de chaque tube tel que 12 à proximité de sa sortie 14, est rapporté et fixé par thermosoudure, par exemple par le procédé connu de soudure dit "par miroir", autour du tube à proximité de sa sortie 14, pour former un épaulement annulaire en saillie radiale vers l'extérieur. Puis un joint d'étanchéité souple et annulaire 18, qui peut, à titre d'exemples non limitatifs, être le joint à lèvres 18a de la figure 9, le joint à section cruciforme 18b de la figure 10 ou le joint torique 18c de la figure 11, est monté autour de la partie d'extrémité de sortie de chaque tube tel que 12, entre son anneau 17 et sa sortie 14. Les deux tubes 12a et 12b groupés en paire de tubes accolés, comme sur la figure 7, avec leur anneau 17 et leur joint d'étanchéité 18 (non représenté sur la figure 7) sont ensuite disposés dans la demi-coquille aval 3. L'extrémité de sortie, avec l'anneau 17 et le joint d'étanchéité 18, de chacun des tubes 12a et 12b est introduite dans un berceau respectivement 20a et 20b moulé d'une seule pièce avec la demi-coquille 3 et la bride 6. Ce berceau 20a, 20b fait saillie sur la bride 6 du côté opposé à la culasse du moteur et a la forme sensiblement d'un hémi-cylindre ouvert vers le plan de joint P et délimitant un conduit central qui prolonge une ouverture 7 correspondante vers l'intérieur de la demi-coquille 3. A son extrémité dans la demi-coquille 3, chaque berceau 20a, 20b présente une chambre annulaire délimitée par un fond annulaire 21a, 21b en saillie radialement vers l'intérieur du berceau 20a, 20b, pour former une butée s'opposant à la sortie axiale de l'anneau 17 et du joint 18 sur l'extrémité de sortie du tube 12a, 12b. Lors de cette mise en place de l'extrémité de sortie du tube 12a ou 12b dans le berceau 20a ou 20b, le joint d'étanchéité 18 (tel que 18a, 18b ou 18c), autour du tube est comprimé radialement entre le tube et le berceau 20a, 20b. La retenue de chacun des tubes 12a et 12b dans le berceau 20a ou 20b de la demi-coquille 3 et son raccordement étanche à l'ouverture 7 correspondante, grâce au joint d'étanchéité, sont complétés par un cavalier 22a ou 22b rapporté transversalement sur la partie d'extrémité du tube engagée dans le berceau 20a ou 20b, et prenant appui par son pourtour contre les bords de ce berceau, le cavalier 22a, 22b présentant un rebord 23a, 23b en forme de fond annulaire en saillie vers l'intérieur du berceau 20a, 20b, et en regard du rebord 21a, 21b de ce dernier. Ce cavalier 22a, 22b est moulé en matière plastique et soudé par ultrasons sur son pourtour sur les bords du berceau 20a ou 20b. Le maintien du tube et l'étanchéité de sa liaison à l'ouverture 7 correspondante sont ainsi assurés grâce au joint d'étanchéité et à un embout de collecteur, formé par le berceau 20a ou 20b et le cavalier 22a ou 22b correspondant, ce dernier ayant, comme montré sur les coupes des figures 4 et 5, un évidement complémentaire de celui du berceau 20a ou 20b pour définir un conduit de section progressivement variable raccordant la sortie oblongue 14a ou 14b du tube à la section circulaire de l'ouverture 7 correspondante, comme représenté par la coupe de la figure 3. Le berceau 20a, 20b ainsi que le cavalier 22a, 22b correspondant sont moulés de sorte que leurs évidements présentent cette évolution correspondante de section.A ring 17, for example made of plastic heat-sealable, with an internal section corresponding to the shape and on the surface at the external section of each tube such as 12 to near its outlet 14, is attached and fixed by heat sealing, for example by the known method of welding said "by mirror", around the tube near its outlet 14, to form an annular shoulder projecting radially towards outside. Then a flexible and annular seal 18, which may, by way of nonlimiting examples, be lip seal 18a of FIG. 9, the section seal cruciform 18b of Figure 10 or the O-ring 18c of the Figure 11, is mounted around the end portion of outlet of each tube such as 12, between its ring 17 and its outlet 14. The two tubes 12a and 12b grouped in pairs of joined tubes, as in FIG. 7, with their ring 17 and their seal 18 (not shown in Figure 7) are then placed in the downstream half-shell 3. The end outlet, with ring 17 and seal 18, of each of the tubes 12a and 12b is introduced into a cradle 20a and 20b respectively molded in one piece with the half-shell 3 and the flange 6. This cradle 20a, 20b protrudes from the flange 6 on the side opposite the cylinder head of the engine and substantially in the shape of an open semi-cylinder towards the joint plane P and delimiting a central duct which extends a corresponding opening 7 towards the inside of the half-shell 3. At its end in the half-shell 3, each cradle 20a, 20b has an annular chamber delimited by an annular bottom 21a, 21b projecting radially towards the inside of the cradle 20a, 20b, to form a stop opposing the axial exit of the ring 17 and the seal 18 on the outlet end of the tube 12a, 12b. During this positioning of the outlet end of the tube 12a or 12b in the cradle 20a or 20b, the seal 18 (such as 18a, 18b or 18c), around the tube is compressed radially between the tube and the cradle 20a, 20b. Restraint of each of the tubes 12a and 12b in the cradle 20a or 20b of the half-shell 3 and its tight connection at the opening 7 corresponding, thanks to the seal, are completed by a jumper 22a or 22b reported transversely on the end part of the tube engaged in the cradle 20a or 20b, and bearing by its periphery against the edges of this cradle, the rider 22a, 22b having a rim 23a, 23b in the form of an annular bottom projecting inwards of the cradle 20a, 20b, and opposite the flange 21a, 21b of this latest. This jumper 22a, 22b is molded in plastic material and welded by ultrasound on its periphery on the edges of the cradle 20a or 20b. Maintaining the tube and sealing its connection to the corresponding opening 7 are thus ensured thanks to the gasket and a manifold tip, formed by the cradle 20a or 20b and the rider 22a or 22b corresponding, the latter having, as shown on the sections Figures 4 and 5, a recess complementary to that of cradle 20a or 20b to define a section duct progressively variable connecting the oblong outlet 14a or 14b from the tube to the circular section of the opening 7 corresponding, as represented by the section of the figure 3. The cradle 20a, 20b as well as the rider 22a, 22b corresponding are molded so that their recesses present this corresponding section evolution.

Les deux tubes 12a et 12b sont également retenus dans la demi-coquille aval 3 par un second cavalier 24, également moulé en matière plastique, qui chevauche transversalement ces deux tubes 12a et 12b dans leur partie accolée, et est fixé de préférence par des bouterolles en matière plastique 25, en saillie vers le plan de joint P dans la demi-coquille 3, et engagés dans des orifices aux extrémités du second cavalier 24, pour être ensuite écrasés thermiquement sur ce dernier. Ainsi, le cavalier 24 maintient les tubes 12a et 12b appliqués contre une embase 26 de support, formée par une surépaisseur de la demi-coquille 3, en saillie vers l'intérieur de cette dernière.The two tubes 12a and 12b are also retained in the downstream half-shell 3 by a second jumper 24, also molded from plastic, which overlaps transversely these two tubes 12a and 12b in their part attached, and is preferably fixed by stoppers in plastic material 25, projecting towards the joint plane P in the half-shell 3, and engaged in orifices at ends of the second jumper 24, to then be crushed thermally on the latter. Thus, the jumper 24 maintains the tubes 12a and 12b applied against a base 26 of support, formed by an extra thickness of the half-shell 3, projecting towards the interior of the latter.

Comme les tubes 12a et 12b ont été moulés par soufflage avec un rayon de courbure général qui est inférieur au rayon de courbure des parties arrondies des demi-coquilles 2 et 3 de l'enveloppe 1, on évite ainsi les contacts et frottements entre les tubes et la demi-coquille amont 2, lors du soudage par vibrations des deux demi-coquilles 2 et 3 l'une contre l'autre, qui impose de petits déplacements relatifs alternés des demi-coquilles 2 et 3 provoquant des frottements entre les brides 4 et 5 conduisant à un thermosoudage. On note, d'ailleurs, que les contacts entre les tubes et la demi-coquille aval 3 sont limités aux contacts avec le cavalier 24 et l'embase 25 et au contact de l'anneau 17 de l'extrémité de sortie des tubes 12a, 12b avec l'embout tubulaire constitué par le berceau 20a ou 20b et le cavalier 22a ou 22b, de sorte qu'on évite toute source possible de frottements perturbateurs entre les tubes et les deux parties de l'enveloppe, pouvant conduire à des ruptures pendant la phase de soudure par vibrations, qui constitue la phase finale d'assemblage du collecteur.As tubes 12a and 12b were molded by blowing with a general radius of curvature which is less at the radius of curvature of the rounded parts of the half-shells 2 and 3 of envelope 1, this avoids contacts and friction between the tubes and the half-shell upstream 2, during vibration welding of the two half-shells 2 and 3 against each other, which imposes small relative alternating displacements of the half-shells 2 and 3 causing friction between the flanges 4 and 5 leading to a heat seal. We note, moreover, that the contacts between the tubes and the downstream half-shell 3 are limited to contact with the jumper 24 and the base 25 and in contact with the ring 17 of the outlet end of the tubes 12a, 12b with the tubular end piece constituted by the cradle 20a or 20b and the jumper 22a or 22b, so that we avoid any possible source of disruptive friction between tubes and the two parts of the envelope, which can lead to ruptures during the vibration welding phase, which constitutes the final assembly phase of the collector.

On obtient ainsi un collecteur dont l'enveloppe 1 délimite une chambre interne 27, appelée plenum, qui est alimentée en air d'alimentation du moteur par une ouverture (non représentée) par exemple ménagée dans le centre d'une face d'extrémité de l'enveloppe 2 parallèlement au plan de la figure 1, cette ouverture étant reliée à un corps de papillon. Chaque tube tel que 12a ou 12b monté dans l'enveloppe 1 aspire de l'air dans le plenum 27 par son entrée 13a ou 13b et transmet cet air par sa sortie 14a ou 14b à une ouverture d'alimentation 7 de la bride 6 pour alimenter un cylindre correspondant. On comprend que l'enveloppe 1 contient, dans sa moitié non représentée sur la figure 2, deux autres tubes d'aspiration d'air symétriques des tubes 12a et 12b et montés de la même façon.A collector is thus obtained, the envelope 1 of which delimits an internal chamber 27, called plenum, which is supplied with engine feed air through an opening (not shown) for example formed in the center of a end face of the envelope 2 parallel to the plane of Figure 1, this opening being connected to a body of butterfly. Each tube such as 12a or 12b mounted in the envelope 1 draws air into plenum 27 through its inlet 13a or 13b and transmits this air through its outlet 14a or 14b to a supply opening 7 of the flange 6 for supplying a corresponding cylinder. We understand that envelope 1 contains, in its half not shown in Figure 2, two other symmetrical air intake tubes 12a and 12b and mounted in the same way.

L'exemple de collecteur d'admission des figures 12 et 13 comporte de nombreuses caractéristiques en commun avec celui qui vient d'être décrit, de sorte que les éléments analogues sont repérés par les mêmes références numériques affectées d'un symbole prime, et que l'on se contente ci-après de décrire les différences présentées par ce second exemple par rapport au premier.The example of an intake manifold in Figures 12 and 13 has many features in common with the one just described, so the elements analogs are identified by the same reference numbers assigned a prime symbol, and which we are satisfied with below to describe the differences presented by this second example compared to the first.

Tout d'abord, les tubes 12'a et 12'b sont de section transversale circulaire. Toutefois, ils sont également accolés sur une partie de leur longueur et sont appliqués par un cavalier 24' contre une embase de support 26' à l'intérieur de la demi-coquille aval 3', le cavalier 24' étant, comme dans l'exemple précédent, fixé par bouterollage ou thermosoudure sur des pions 25' de cette demi-coquille 3'.First, the tubes 12'a and 12'b are of section transverse circular. However, they are also joined for part of their length and are applied by a jumper 24 'against a support base 26' to inside the downstream half-shell 3 ', the jumper 24' being, as in the previous example, fixed by bolting or heat sealing on pins 25 'of this half-shell 3 '.

De même, les extrémités de sortie des tubes 12'a et 12'b sont entourées d'un anneau 17' et d'un joint d'étanchéité souple 18' et sont chacune raccordées de manière étanche à une ouverture correspondante 7' de la bride de fixation 6' à la culasse par un embout tubulaire. Mais, dans cet exemple, ce dernier est constitué d'un berceau 20'a ou 20'b de section transversale de forme en U et de valeur constante, avec un fond annulaire formant butée radiale interne 21'a ou 21'b, du côté de la demi-coquille 3', ainsi que d'un cavalier 22'a ou 22'b essentiellement plat avec une butée en arc-de-cercle 23'a ou 23'b en saillie vers l'intérieur du berceau 20'a ou 20'b et en regard du fond annulaire 21'a ou 21'b de ce dernier. L'embout de collecteur ainsi réalisé pour chaque extrémité de sortie d'un tube 12'a ou 12'b est de préférence de section circulaire de diamètre constant, avec une face, orientée vers le tube correspondant qui est plane et perpendiculaire à l'axe du tube dans sa partie d'extrémité de sortie. Le joint d'étanchéité cylindrique 18' est, dans cet exemple, comprimé axialement par ses deux faces d'extrémité radiale et planes entre, d'un côté, la face radiale plane de l'anneau 17' qui est tournée vers la bride 6' et, de l'autre côté, une face radiale plane, tournée vers l'intérieur de la demi-coquille 3', dans le fond du berceau 20'a ou 20'b correspondant, sur la bride 6', ces différentes faces radiales étant sensiblement perpendiculaires à l'axe du tube 12'a ou 12'b à sa sortie.Similarly, the outlet ends of the tubes 12'a and 12'b are surrounded by a 17 'ring and a seal flexible 18 'and are each connected so watertight at a corresponding opening 7 'of the flange of fixing 6 'to the cylinder head by a tubular end piece. But in this example, the latter consists of a cradle 20'a or 20'b of U-shaped cross section and value constant, with an annular bottom forming a radial stop internal 21'a or 21'b, on the side of the half-shell 3 ', thus than a basically flat rider 22'a or 22'b with a 23'a or 23'b arc-shaped abutment projecting inwards of the cradle 20'a or 20'b and opposite the annular bottom 21'a or 21'b of the latter. The manifold tip as well made for each outlet end of a 12'a tube or 12'b is preferably of circular cross-section of diameter constant, with one face, oriented towards the corresponding tube which is flat and perpendicular to the axis of the tube in its outlet end part. The cylindrical seal 18 'is, in this example, compressed axially by its two radial and planar end faces between, of a side, the planar radial face of the ring 17 'which is turned towards the flange 6 'and, on the other side, a radial face flat, facing inward of the 3 'half-shell, in the bottom of the corresponding cradle 20'a or 20'b, on the flange 6 ', these different radial faces being substantially perpendicular to the axis of the tube 12'a or 12'b at its outlet.

Dans les deux exemples décrits ci-dessus, les tubes comme les demi-coquilles peuvent être réalisés en une matière plastique telle que le polyamide, chargé de fibres de renfort.In the two examples described above, the tubes as the half-shells can be made in one plastic material such as polyamide, loaded with fibers reinforcement.

Claims (12)

  1. Inlet manifold for an internal combustion engine, preferably a fuel-injected engine, particularly one with multipoint injection, the manifold comprising:
    an envelope (1, 1') delimiting a plenum chamber (27, 27') intended to be supplied with air for supplying the engine via a variable-delivery valve, such as a butterfly valve, and equipped with at least one flange (6, 6') for attaching it to a cylinder head of the engine, said flange or flanges having at least one opening (7, 7') for supplying each cylinder of the engine, each supply opening (7, 7') opening, on the one hand, into the envelope (1, 1') and, on the other hand, into a face (8, 8') for attaching the flange (6, 6') to said cylinder head, and
    curved air-induction tubes (12a, 12b, 12'a, 12'b) each made as a single piece with the desired shape, and of which there are at least as many as there are cylinders in the engine, and which are mounted in the envelope (1, 1') so that each tube supplies a corresponding cylinder with air which the tube receives via its inlet (13a, 13b, 13'a, 13'b) in the plenum chamber (27, 27') and which the tube transmits to a corresponding opening (7, 7') in a flange (6, 6') via its outlet (14a, 14b, 14'a, 14'b) connected to said supply opening (7, 7') by leaktight connection means comprising a tubular end piece (20a-22a, 20b-22b, 20'a-22'a, 20'b-22'b) in which the outlet end part of said tube is held in said envelope (1, 1') with the insertion of at least one flexible seal (18a, 18b, 18c, 18') between the tube and the end piece,
    characterized in that the internal surface of each tube (12a, 12b, 12'a, 12'b) is smooth and continuous from its inlet (13a, 13b, 13'a, 13'b) to its outlet (14a, 14b, 14'a, 14'b), and in that each end piece is made with, on the one hand, a cradle (20a, 20'a) integral with said attachment flange (6, 6') and projecting from the opposite side to the cylinder head, in line with said corresponding supply opening (7, 7'), the cradle being of a more or less semi-cylindrical shape, of which the end inside said envelope (1, 1') has an annular end wall (21a, 21'a) forming a stop projecting toward the inside of the cradle (20a, 20'a) and, on the other hand, a stirrup piece (22a, 22'a) for holding said tube (12a, 12'a) in said cradle (20a, 20'a), said stirrup piece (22a, 22'a) having a stop (23a, 23'a) projecting toward the inside of the cradle (20a, 20'a) and facing the annular end wall (21a, 21'a) of the cradle, a ring (17, 17') being attached and fixed around said tube (12a, 12'a) close to its air outlet (14a, 14'a), said flexible seal (18a, 18b, 18c, 18') being attached around said tube (12a, 12'a) between said ring (17, 17') and said air outlet (14a, 14'a) of the tube (12a, 12'a), the outlet end part of said tube (12a, 12'a) with said ring (17, 17') and said seal being in place in said corresponding cradle (20a, 20'a) in such a way that the ring (17, 17') or the seal (18, 18') is retained by butting against said annular end wall (21a, 21'a) of the cradle (20a, 20'a), said stirrup piece (22a, 22'a) being attached to said cradle (20a, 20'a) and that part of the tube (12a, 12'a) which is held therein, and being fixed to the edges of the cradle (20a, 20'a).
  2. Inlet manifold according to Claim 1 characterized in that the envelope (1, 1') comprises two molded half shells (2, 3; 2', 3') with complementary shapes corresponding to the shape of the envelope (1, 1') and arranged one against the other and secured together via their peripheral edges (4, 5; 4', 5') in a parting plane (P), to form the envelope with the tubes (12a, 12b, 12'a, 12'b) between them, each tube being blow molded, and preferably suction blow-molded, from a thermomoldable plastic, and said attachment flange (6, 6') being integral with one of said half shells (3, 3').
  3. Inlet manifold according to one of Claims 1 and 2, characterized in that each tube (12) is made with a section that decreases progressively in the downstream direction over at least part of its length and/or with a convergent bell-socket-shaped air inlet (13).
  4. Inlet manifold according to one of Claims 1 to 3, characterized in that each tube (12) is made with a section that has more or less the same shape from its air inlet (13) to its air outlet (14).
  5. Inlet manifold according to one of Claims 2 to 4, characterized in that the tubes are grouped at least in pairs of tubes (12a-12b; 12'a-12'b) that touch over at least part of their length, and the tubes of each group of tubes (12a-12b; 12'a-12'b) are fixed into one and the same half shell (3, 3') which has an attachment flange (6, 6') with supply openings (7, 7') to which the tubes of said group are connected in leaktight manner, using at least one second stirrup piece (24, 24') which transversely straddles the touching tubes (12a, 12b; 12'a, 12'b) of said group, in their touching part, and which is attached via its ends to said half shell (3, 3').
  6. Inlet manifold according to Claim 5, characterized in that each tube (12) is made with an oval section and flats (15), parallel to the major axis (16) of its section, on its opposed facing faces, and the tubes (12a-12b) are grouped together, touching along their flats (15).
  7. Inlet manifold according to either of Claims 5 and 6, characterized in that the half shells (2, 3; 2', 3') with their bases (26, 26'), on the one hand, and the stirrup pieces (24, 24'), on the other hand, are components molded from plastic, and the second stirrup pieces (24, 24') are fixed to the corresponding half shells (2, 3; 2', 3') by welding or snap riveting.
  8. Inlet manifold according to one of Claims 2 to 7, characterized in that the tubes (12) are made curved with a radius of curvature, in the plane containing their axis, smaller than that of the envelope (1), the half shells (2, 3) of the envelope (1) are molded of plastic with securing flanges (4, 5) along their edges in the parting plane (P), and the half shells (2, 3) are secured together to form the envelope (1) by welding, preferably vibration welding, at the securing flanges (4, 5).
  9. Inlet manifold according to any one of Claims 2 to 8, characterized in that each end piece (20a-22a) holds a corresponding tube (12a) on one of the half shells (3) to which each cradle (20a, 20'a) is secured.
  10. Inlet manifold according to one of Claims 1 to 9, characterized in that the seal between the outlet end part (14a) of each tube (12a) and the corresponding end piece (20'a-22'a) is provided by axially compressing said seal (18), which is cylindrical, via its flat end faces between a flat radial face, pointing toward the outlet (14'a) of the tube (12'a), of the ring (17') of the tube (12'a) and a flat radial face, pointing toward the inside of said envelope (1'), of the cradle (20'a) and of said flange (6'), said radial faces being more or less perpendicular to the axis of the tube (12'a) at its outlet (14'a).
  11. Inlet manifold according to one of Claims 1 to 9, characterized in that each cradle (20a) and the corresponding stirrup piece (22a) are molded in such a way that the end piece formed by the cradle and the stirrup piece has a cross section that changes progressively from a circular shape, on the same side as the attachment flange (6) and its circular supply opening (7), to an oval shape which complements that of the tubes (12a).
  12. Inlet manifold according to Claim 11, characterized in that the seal between the outlet end part (14a) of each tube (12a) and the corresponding end piece (20a-22a) is provided by radially compressing said seal (18a, 18b, 18c) between, on the one hand, the tube (12a) and, on the other hand, the cradle (20a) and the corresponding stirrup piece (22a).
EP96919876A 1995-05-10 1996-05-07 Intake manifold for internal combustion engine Expired - Lifetime EP0839273B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9505534 1995-05-10
FR9505534A FR2734026B1 (en) 1995-05-10 1995-05-10 INTAKE MANIFOLD FOR INTERNAL COMBUSTION ENGINE AND MANUFACTURING METHOD THEREOF
PCT/FR1996/000689 WO1996035869A1 (en) 1995-05-10 1996-05-07 Intake manifold for internal combustion engine

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EP0839273A1 EP0839273A1 (en) 1998-05-06
EP0839273B1 true EP0839273B1 (en) 2001-11-21

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US (1) US5896838A (en)
EP (1) EP0839273B1 (en)
DE (1) DE69617244T2 (en)
ES (1) ES2168486T3 (en)
FR (1) FR2734026B1 (en)
WO (1) WO1996035869A1 (en)

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DE19647184A1 (en) * 1996-11-14 1998-05-20 Mann & Hummel Filter Intake module for an internal combustion engine
CZ2002612A3 (en) * 1999-08-24 2002-06-12 Siemens Aktiengesellschaft Intake system of internal combustion engine
DE60029809T2 (en) * 1999-10-14 2007-10-25 Siemens Vdo Automotive Inc., Chatham SHAPED INTAKE MANIFOLD WITH SEPARATE INTAKE TUBES
US6234129B1 (en) 1999-12-30 2001-05-22 Hayes Lemmerz International, Inc. Composite intake manifold assembly for an internal combustion engine and method for producing same
US6199530B1 (en) 1999-12-30 2001-03-13 Hayes Lemmerz International, Inc. Composite intake manifold assembly for an internal combustion engine and method for producing same
US6234131B1 (en) 1999-12-30 2001-05-22 Hayes Lemmerz International, Inc. Composite intake manifold assembly for an internal combustion engine and method for producing same
US6234130B1 (en) 1999-12-30 2001-05-22 Hayes Lemmerz International, Inc. Composite intake manifold assembly for an internal combustion engine and method for producing same
EP1277947B1 (en) * 2001-07-20 2007-02-28 Mann + Hummel GmbH Fixing device for an inlet collector
US6598581B2 (en) * 2001-12-13 2003-07-29 Visteon Global Technologies, Inc. Metallic coating on a component of an internal combustion engine
US7246593B2 (en) * 2002-08-29 2007-07-24 Siemens Canada Limited Intake module assembly
US6755897B2 (en) * 2002-10-23 2004-06-29 Siemens Vdo Automotive Inc. Constant velocity radial inflow particle separator
JP2008184939A (en) * 2007-01-29 2008-08-14 Daikyo Nishikawa Kk Resin-made intake manifold
US8181620B2 (en) * 2008-08-11 2012-05-22 Mark IV Systems Moteurs USA, Inc. Modular intake manifold
JP5064537B2 (en) * 2010-07-27 2012-10-31 株式会社サンダンスエンタープライズ Flange for intake manifold
FR2967215B1 (en) * 2010-11-08 2016-01-01 Valeo Systemes Thermiques GAS DISTRIBUTION COLLECTOR AND CORRESPONDING GAS ADMISSION MODULE

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DE2457155A1 (en) * 1974-01-23 1975-07-24 Bayerische Motoren Werke Ag IC engine air intake system - has curved partial sections of suction pipes within distributor housing
DE2501305A1 (en) * 1975-01-15 1976-07-22 Bayerische Motoren Werke Ag AIR INTAKE SYSTEM FOR COMBUSTION MACHINES
US4175504A (en) * 1975-01-15 1979-11-27 Bayerische Motoren Werke Ag Air induction system for an internal combustion engine
JP2892700B2 (en) * 1989-08-18 1999-05-17 ヤマハ発動機株式会社 V-type engine intake system
US5003933A (en) * 1989-11-06 1991-04-02 General Motors Corporation Integrated induction system
US5150669A (en) * 1989-11-06 1992-09-29 General Motors Corporation Pressure relief means for integrated induction system

Also Published As

Publication number Publication date
DE69617244T2 (en) 2002-08-22
WO1996035869A1 (en) 1996-11-14
US5896838A (en) 1999-04-27
EP0839273A1 (en) 1998-05-06
FR2734026B1 (en) 1997-07-18
DE69617244D1 (en) 2002-01-03
ES2168486T3 (en) 2002-06-16
FR2734026A1 (en) 1996-11-15

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