EP0827567B1 - Intake manifold with ringed air tubes for internal combustion engines - Google Patents

Intake manifold with ringed air tubes for internal combustion engines Download PDF

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Publication number
EP0827567B1
EP0827567B1 EP96917521A EP96917521A EP0827567B1 EP 0827567 B1 EP0827567 B1 EP 0827567B1 EP 96917521 A EP96917521 A EP 96917521A EP 96917521 A EP96917521 A EP 96917521A EP 0827567 B1 EP0827567 B1 EP 0827567B1
Authority
EP
European Patent Office
Prior art keywords
tube
sleeve
outlet
envelope
cradle
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
EP96917521A
Other languages
German (de)
French (fr)
Other versions
EP0827567A1 (en
Inventor
Micha[L Pontopiddan
Michele Sonori
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Marelli France SAS
Original Assignee
Magneti Marelli France SAS
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 Magneti Marelli France SAS filed Critical Magneti Marelli France SAS
Publication of EP0827567A1 publication Critical patent/EP0827567A1/en
Application granted granted Critical
Publication of EP0827567B1 publication Critical patent/EP0827567B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F02M35/104Intake manifolds
    • F02M35/112Intake manifolds for engines with cylinders all in one line
    • 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
    • F02M35/10091Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements
    • F02M35/10111Substantially V-, C- or U-shaped ducts in direction of the flow path
    • 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
    • F02M35/1034Manufacturing 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
    • F02M35/10078Connections 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
    • F02M35/10209Fluid connections to the air intake system; their arrangement of pipes, valves or the like
    • F02M35/10216Fuel injectors; Fuel pipes or rails; Fuel pumps or pressure regulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2225/00Synthetic polymers, e.g. plastics; Rubber
    • F05C2225/08Thermoplastics

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 is formed by the 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 are formed by the impression bottoms molded into at least two molded inserts, generally in the same material as the half-shells, for example in moldable synthesis, preferably thermoplastic, such as polyamide, and which can be loaded with reinforcing fibers, and each reported in one half-shells respectively, so that the footprints inserts also extend during the joining half shells against each other.
  • 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.
  • a seal must be made between the inserts and the half-shells by fitting cords of suitable polymerizable material, which is a long and delicate operation, adding to the difficulty of realization with low tolerances of the parts to assemble to precisely define the air tubes.
  • the problem underlying the invention is to propose a collector of an economic achievement, essentially in thermomouldable and semi-modular synthesis, because acoustically adaptable to a whole family of engines of different displacements by dimensional adjustment, in particular of the diameter and the length of the air tubes.
  • each tube is an external face tube corrugated, preferably with parallel rings, and internal face smooth delimiting a central passage of cross section constant in shape and in surface, so that the tube has great flexibility or transverse flexibility, but low flexibility or axial flexibility.
  • Such monoblock air tubes being by nature waterproof, the need to make joint cords sealing along the generators disappears.
  • the rings of the corrugated external face of such tubes keep the shape and surface constant the cross section of the central passage, participating maintaining the acoustic impedance of the tubes, while providing good flexibility or suppleness in direction radial or transverse, allowing bending of the tubes as desired, while their smooth internal surface limits pressure losses and gives the tubes a low flexibility or axial flexibility, necessary to maintain their acoustic impedance.
  • each tube is made of synthesis, preferably moldable, such as thermoplastic, and cut, perpendicular to its longitudinal axis, at the desired length, to give the collector an impedance acoustic tuned to the engine, in an element tubular supplied in great length, and preferably of circular section, so that the tubular element is obtained at a very favorable cost, compared to others possible solutions for making waterproof tubes.
  • the annular conformation of the external face of the tube can be defined by one or more ribs helical wound in the outer face of the tube, its inlet to outlet, the corrugated outer face of each tube is advantageously a surface of cylindrical revolution at corrugated generator before the tube is bent at the desired shape, to simultaneously benefit from a large transverse flexibility but very low flexibility axial.
  • the collector envelope may consist of, known manner, of two half-shells of complementary shapes corresponding to the shape of the envelope and molded, preferably in moldable synthetic material, preferably thermoplastic, with fixing flanges on their peripheral edges in a joint plane, the half-shells being closed and fixed against each other at level of their fastening flanges, for example by welding, preferably by vibration, in which case it is advantageous that each tube is fixed only by its ends with half shells.
  • each tube is advantageously fixed to a half-shell using of a sleeve which is partly force-fitted into the corresponding end of the tube and retained on said half-shell by a part of sleeve external to the tube.
  • the sleeve has, on the external face of its part which is fitted at one end corresponding tube, at least one peripheral redent anchor, which is formed at the axial end, facing the said end of the tube, of a surface substantially frustoconical with small base facing the central part of the tube, several axially offset redents preferably being formed in this way on the sleeve.
  • the latter advantageously comprises at least one projecting stop substantially radial towards the outside to limit its fitting into a corresponding end of the tube.
  • the sleeve or each of the two connecting sleeves of a tube is molded from a material of synthesis, which is preferably a thermosetting material.
  • an air inlet sleeve fitted into an inlet end of a tube, is shaped, in its external part at said inlet end of the tube, in a tulip converging towards the inside of the tube and provided with minus one fixing lug to that of the two half-shells which is not provided with the mounting flange having the feed opening at which said tube is connected by its output, the fixing being for example provided by heat sealing or by rolling at the fixing lug (s).
  • each tube is advantageously connected by an air outlet sleeve, fitted into the end of outlet of the tube, to that of the half-shells which is provided with said fixing flange having said opening to which said tube is so connected waterproof by its outlet, said connection means watertight including a tubular manifold tip, in projection on said flange on the side opposite to the cylinder head, in the extension of said corresponding feed opening, and in which tip part of said sleeve outlet, which is external to the tube, is retained with interposition at least one flexible seal between said external part of the outlet sleeve and said end piece collector.
  • a good seal can be ensured using a single flexible gasket for each tube, if gasket, mounted around the part of the outlet sleeve corresponding which is external to the tube and retained in the nozzle corresponding collector, is molded in shape, preferably made of elastomer, with a cross section corresponding to that of the space available between, on the one hand, said outlet sleeve, and, on the other hand, said cradle and said cover, and so that the seal is compressed radially between these three elements.
  • the corresponding manifold tip advantageously has a substantially cross section of the same shape as that of said feed opening, and the corresponding outlet sleeve has a central passage having a cross section of form evolutionary, varying gradually from the section shape of the manifold tip, in the part of the outlet sleeve which is external to the tube, to the cross-sectional shape of the tube, in the part of the outlet sleeve which is fitted into the outlet end of this tube, so that the sleeve of outlet constitutes an adapter sleeve ensuring the transition between the shapes of the tip sections manifold and air tube.
  • the tubes can be grouped at least in pairs of tubes joined on at least part of their length, and, in order to limit the transverse displacements of tubes or groups of tubes attached to the envelope, housing can be delimited by recesses in the internal face of the envelope, and parts of tubes or joined parts of tubes can be accommodated in these recesses, possibly bordered by protruding ribs on the inner face of at least one of the half-shells constituting the envelope.
  • the manifold of Figures 1 and 2 for a motor with four cylinders in line, includes a rigid casing 1, in moldable and heat-sealable synthetic material such as a polyamide possibly reinforced with reinforcing fibers, and made up of two half-shells 2 and 3, each molded in this material, having complementary shapes which correspond to the shape of envelope 1.
  • a rigid casing 1 in moldable and heat-sealable synthetic material such as a polyamide possibly reinforced with reinforcing fibers, and made up of two half-shells 2 and 3, each molded in this material, having complementary shapes which correspond to the shape of envelope 1.
  • the two half-shells 2 and 3 close against each other, by their peripheral edges, to reconstitute the shape of envelope 1, and are secured to each other in a joint plane P, defined by fastening flanges 4 and 5, projecting outwards on their edges, by vibration welding at these flanges 4 and 5, after mounting in the half-shells 2 and 3 of four tubes air intake (one per engine cylinder), grouped in two pairs of joined tubes, as shown in the figure 2, and their sleeves as described below.
  • the flange 6 has, for each cylinder of the motor, a feed opening 7, coming from molding, circular or oblong cross section, which opens out on one side in the flat face 8 for fixing the flange 6 on the engine cylinder head and, on the other side, inside the half-shell 3, lower in FIG.
  • the flange 6 has also, for each cylinder, a housing 9 for a fuel injector, 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, of a part, 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 12a or 12b of the pair of tubes of FIG. 2, is a curved tube, obtained by cutting, perpendicular to its longitudinal axis, a length determined, to give the tube 12a or 12b an impedance acoustic tuned to the engine, in a large tube length in thermoplastic, having an internal face 13 smooth, delimiting a central passage of cross section of constant shape and surface, for example circular, and a corrugated external face 14, with peripheral rings in planes substantially parallel to each other and perpendicular to the axis of the tube, before the tube section cut is not bent to the desired shape by the closure half-shells 2 and 3, each of which each tube 12a or 12b is fixed only by one respectively of its inlet ends such as 15a and outlet ends 16a or 16b.
  • a light tube 12a or 12b is thus produced, with a thin wall and waterproof, having great flexibility or transverse flexibility or radial, and low flexibility or flexibility axial, so that it can be bent to the desired shape without losing the constant shape and surface of the section transverse of its central passage with smooth wall, and without vary significantly in length, which ensures losses of practically constant load and acoustic impedance.
  • Each tube such as 12a or 12b is bent in a loop almost complete in the plan of figure 1, on a large part of its length substantially from its entrance such as 15a, and its downstream part is further angled or bent in a direction perpendicular to the plane of Figure 1, as shown in Figure 2.
  • two tubes such as 12a and 12b grouped into a pair of tubes to supply each one respectively of two adjacent cylinders, can be joined on much of their length substantially from their inputs such as 15a, while their outputs 16a and 16b (see Figure 2) are spaced from each other to each be tightly connected to one respectively two adjacent supply openings 7 one of the other in the flange 8 to supply the two cylinders corresponding contiguous.
  • each tube 12a or 12b is fixed to the upstream half-shell 2 by a air inlet sleeve such as 17a, while the end outlet 16a or 16b of the tube is connected to the half-shell downstream 3 by an air outlet sleeve 18a or 18b, each of sleeves 17a, 18a or 18b being preferably molded in a synthetic material, preferably thermosetting.
  • the inlet sleeve 17a comprises a tubular part 19a which is forced into the end inlet 15a of the tube 12a, and which extends towards the front, outside this entry 15a, by a shaped part in volute or inlet tulip 20a converging inwards from tube 12a and downstream.
  • This entrance tulip 20a has a fixing lug 21a, by which the sleeve 17a is fixed to the half-shell 2 at at least one point, by example by heat sealing or by a dowel, as shown schematically in 22a.
  • the internal face of the tubular part 19a is smooth, and substantially in line with the smooth internal face 13 of the tube 12a, while to ensure a good fit axial of the sleeve 17a in the inlet 15a of the tube 12a, the face outer of the tubular part 19a has redents peripherals, as described below for the output 18a with reference to Figure 5.
  • Each outlet sleeve 18a or 18b includes, as shown for the sleeve 18a in FIG. 5, a part tubular 23a which is force fitted into outlet 16a of tube 12a, and which extends backwards or towards downstream, outside this exit 16a, by a part tubular 24a external to tube 12a and retained on the half-shell 3 while being connected with sealing at the opening 7 corresponding as described below.
  • the parts 23a and 24a between which the sleeve 18a has an annular stop 25a projecting radially outwards to limit fitting in outlet 16a of the tube 12a, have a smooth internal face, substantially in the extension of the smooth internal face 13 of the tube 12a, while that the external face of the fitted part 23a has two peripheral and axially offset redents 26a, each formed at the axial end, facing the stop 25a, of a substantially frustoconical surface 27a with small turned base towards the end of the innermost part 23a of the tube 12a, so as to facilitate penetration at the fitting and to ensure good anchoring.
  • This cradle 29a 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, with a cross section of substantially constant surface U-shape, defining a central duct which extends a corresponding opening 7 towards the inside of the half-shell 3.
  • the cradle 29a has a chamber annular delimited by a projecting U-shaped bottom 30a radially inward of the cradle 29a to form a stop opposing the axial outlet of the seal 28 on the external part 24a of the sleeve 18a.
  • the seal seal 28 around the sleeve 18a is compressed radially between the sleeve 18a and the cradle 29a.
  • This cover 31a is molded in synthetic material, preferably thermoplastic, and preferably ultrasonically welded to its around the edges of the cradle 29a. Maintaining the sleeve 18a and the tightness of its connection to the opening 7 corresponding are thus ensured thanks to the seal 28 and to a tubular manifold end, formed by the cradle 29a and the corresponding cover 31a.
  • the seal 28 is molded with a sectional shape such that it occupies radially all the space available between the part 24a of the sleeve 18a, in the center, and the cradle 29a and the cover 31a, at the periphery, being compressed radially between these parts.
  • the part 24a of the sleeve 18a is extended by a half-cylinder-shaped end open towards the bottom of the cradle 29a which receives it, and having, as shown in the section of FIG. 3, a recess complementary to that of the cradle 29a for define a duct of progressively variable section connecting the outlet, for example circular, 16a of the tube 12a to the section, for example oblong, of the opening 7 corresponding, as shown in the drawings.
  • the sleeve outlet 18a is molded so that its central passage presents this corresponding section evolution, the section of the end of the sleeve 18a fitted into the tube 12a always having the same shape as the section of the tube 12a, and the section of the end of the sleeve 18a facing opening 7 having, alone or with the section complementary to the bottom of the cradle 29a which receives it, the same forms as the section of the opening 7.
  • the outlet sleeve 18b of the tube 12b is mounted from the same way with a seal such as 28 in one manifold tip consisting of a similar cradle 29b closed by a corresponding analog cover.
  • the two tubes 12a and 12b are also arranged, by their adjoining parts, in a housing delimited in the half-shell downstream 3 by a recess between ribs 33 in projection on the internal face of this half-shell 3.
  • Tubes 12a and 12b can be joined so that the rings of the external face of one are engaged between each other’s rings, and possibly ribs 33 bordering the housings may have protrusions engaging between the outer rings of the tubes 12a, 12b to better position them in the envelope 1.
  • tubes 12a and 12b flexible transversely are fixed to the casing 1 by their only ends, the mounting of the sleeves 17a and 18a is carried out to give the tubes a general radius of curvature which is slightly less at the radius of curvature of the rounded parts of the half-shells 2 and 3 of envelope 1.
  • the transverse flexibility of the tubes allows, during assembling the half-shells 2 and 3, small displacements alternating relative of these in the perpendicular direction to the radius of curvature of the tubes, thus providing the possibility of assembling the half-shells 2 and 3 for example by vibration welding.
  • a collector is thus obtained, the envelope 1 of which delimits an internal chamber 34, called plenum, which is supplied with engine feed air through an opening (not shown) for example formed in an end face of the envelope 1 parallel to the plane of FIG. 1, this opening being connected to a butterfly body.
  • Each tube such as 12a or 12b mounted in the casing 1 sucks from the air in plenum 34 by its entry such as 15a and transmits this air through its outlet 16a or 16b to an opening supply 7 of the flange 6 to supply a cylinder corresponding.
  • the envelope 1 contains, in its half not shown in Figure 2, two other tubes symmetrical air suction tubes 12a and 12b and mounted in the same way.

Abstract

Between two half-shells (2, 3) molded and fixed to each other in order to form an envelope (1), there are mounted air tubes (12a) with a ringed external face (14) and a smooth internal face (13) which are fixed by means of end sleeves (17a, 18a) to the envelope (1). The outlet sleeve (18a) is held within a half-shell (3) by means of a fixing clamp (6) to the cylinder-head of the engine by being sealingly connected to an opening (7) of the clamp (6) for the supply of one cylinder by a tubular nozzle comprised of a cradle (29a) integrally cast with the clamp (6) and the half-shell (3), and a cover (31a) fixed to the cradle in order to hold a seal (28) to the extremity of the outlet sleeve (18a), the seal being compressed between the sleeve (18a) and the nozzle (29a, 31a). Application particularly to intake manifolds of internal combustion engines, preferably with 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.

Par GB-A-2 238 350, on connait un tel collecteur d'admission, qui comprend :

  • une enveloppe, délimitant un plenum destiné à être alimenté en air d'alimentation du moteur, en général par une vanne à débit variable telle qu'un corps de papillon, et munie d'au moins une bride de fixation à au moins 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, et 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 qu'il reçoit par son entrée dans le plenum et qu'il transmet à l'ouverture correspondante de la bride correspondante par sa sortie reliée par des moyens de raccordement étanches à ladite ouverture d'alimentation.
By GB-A-2 238 350, there is known such an intake manifold, which comprises:
  • an envelope, delimiting a plenum intended to be supplied with air supplying the engine, in general by a variable flow valve such as a throttle body, and provided with at least one flange for fixing to at least one cylinder head of the engine, said flange (s) 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 fixing face of the flange on said cylinder head, and
  • curved air suction tubes, each in one piece, and in a number at least equal to that of the engine cylinders, and mounted in the casing, so that each tube supplies a corresponding cylinder with air that it receives by its entry into the plenum and which it transmits to the corresponding opening of the corresponding flange by its outlet connected by sealed connection means to said supply opening.

On sait déjà fabriquer des collecteurs de ce type 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 make collectors of this type 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 est 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 est formée par les fonds d'empreintes moulées en creux dans au moins deux inserts moulés, en général dans la même matière que les demi-coquilles, par exemple en matière de synthèse moulable, de préférence thermoplastique, telle que du polyamide, et pouvant être chargée 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 is formed by the 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 are formed by the impression bottoms molded into at least two molded inserts, generally in the same material as the half-shells, for example in moldable synthesis, preferably thermoplastic, such as polyamide, and which can be loaded with reinforcing fibers, and each reported in one half-shells respectively, so that the footprints inserts also extend during the joining half shells against each other. This process thus 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 a good seal, 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 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 fitting cords of suitable polymerizable material, which is a long and delicate operation, adding to the difficulty of realization with low tolerances of the parts to assemble to precisely define the air tubes.

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

Le problème à la base de l'invention est de proposer un collecteur d'une réalisation économique, essentiellement en matière de synthèse thermomoulable, et semi-modulable, car acoustiquement adaptable à toute une famille de moteurs de cylindrées différentes par ajustement dimensionnel, en particulier du diamètre et de la longueur des tubes d'air.The problem underlying the invention is to propose a collector of an economic achievement, essentially in thermomouldable and semi-modular synthesis, because acoustically adaptable to a whole family of engines of different displacements by dimensional adjustment, in particular of the diameter and the length of the air tubes.

A cet effet, le collecteur d'admission selon l'invention, du type connu par GB-A-2 238 350, se caractérise en ce que chaque tube est un tube à face externe annelée, de préférence à anneaux parallèles, et face interne lisse délimitant un passage central de section transversale constante en forme et en surface, de sorte que le tube présente une grande souplesse ou flexiblité transversale, mais une faible souplesse ou flexibilité axiale.For this purpose, the intake manifold according to the invention, of the type known from GB-A-2 238 350, is characterized in that each tube is an external face tube corrugated, preferably with parallel rings, and internal face smooth delimiting a central passage of cross section constant in shape and in surface, so that the tube has great flexibility or transverse flexibility, but low flexibility or axial flexibility.

De tels tubes d'air monoblocs étant par nature étanches, la nécessité de réaliser des cordons de joints d'étanchéité le long des génératrices disparaít. De plus, les anneaux de la face externe annelée de tels tubes permettent de maintenir constantes la forme et la surface de la section transversale du passage central, en participant au maintien de l'impédance acoustique des tubes, tout en procurant une bonne flexibilité ou souplesse en direction radiale ou transversale, permettant de recourber les tubes de la manière voulue, tandis que leur surface interne lisse limite les pertes de charge et donne aux tubes une faible souplesse ou flexibilité axiale, nécessaire au maintien de leur impédance acoustique.Such monoblock air tubes being by nature waterproof, the need to make joint cords sealing along the generators disappears. Moreover, the rings of the corrugated external face of such tubes keep the shape and surface constant the cross section of the central passage, participating maintaining the acoustic impedance of the tubes, while providing good flexibility or suppleness in direction radial or transverse, allowing bending of the tubes as desired, while their smooth internal surface limits pressure losses and gives the tubes a low flexibility or axial flexibility, necessary to maintain their acoustic impedance.

Avantageusement, chaque tube est en matière de synthèse, de préférence moulable, telle que du thermoplastique, et découpé, perpendiculairement à son axe longitudinal, à la longueur voulue, pour donner au collecteur une impédance acoustique accordée au moteur, dans un élément tubulaire approvisionné en grande longueur, et de préférence de section circulaire, de sorte que l'élément tubulaire soit obtenu à un coût très favorable, par rapport aux autres solutions possibles pour réaliser des tubes étanches.Advantageously, each tube is made of synthesis, preferably moldable, such as thermoplastic, and cut, perpendicular to its longitudinal axis, at the desired length, to give the collector an impedance acoustic tuned to the engine, in an element tubular supplied in great length, and preferably of circular section, so that the tubular element is obtained at a very favorable cost, compared to others possible solutions for making waterproof tubes.

Bien que la conformation annelée de la face externe du tube puisse être définie par une ou plusieurs nervures hélicoïdales enroulées dans la face externe du tube, de son entrée à sa sortie, la face externe annelée de chaque tube est avantageusement une surface de révolution cylindrique à génératrice ondulée avant que le tube ne soit recourbé à la forme voulue, pour bénéficier simultanément d'une grande flexibilité transversale mais d'une très faible flexibilité axiale.Although the annular conformation of the external face of the tube can be defined by one or more ribs helical wound in the outer face of the tube, its inlet to outlet, the corrugated outer face of each tube is advantageously a surface of cylindrical revolution at corrugated generator before the tube is bent at the desired shape, to simultaneously benefit from a large transverse flexibility but very low flexibility axial.

L'enveloppe du collecteur peut être constituée, de manière connue, de deux demi-coquilles de formes complémentaires correspondant à la forme de l'enveloppe et moulées, de préférence en matière de synthèse moulable, de préférence du thermoplastique, avec des brides de solidarisation sur leurs rebords périphériques dans un plan de joint, les demi-coquilles étant refermées et fixées l'une contre l'autre au niveau de leurs brides de solidarisation, par exemple par soudage, de préférence par vibrations, auquel cas il est avantageux que chaque tube soit fixé uniquement par ses extrémités aux demi-coquilles.The collector envelope may consist of, known manner, of two half-shells of complementary shapes corresponding to the shape of the envelope and molded, preferably in moldable synthetic material, preferably thermoplastic, with fixing flanges on their peripheral edges in a joint plane, the half-shells being closed and fixed against each other at level of their fastening flanges, for example by welding, preferably by vibration, in which case it is advantageous that each tube is fixed only by its ends with half shells.

A cette fin, l'une au moins des extrémités de chaque tube est avantageusement fixée à une demi-coquille à l'aide d'un manchon qui est en partie emmanché à force dans l'extrémité correspondante du tube et retenu sur ladite demi-coquille par une partie de manchon externe au tube. Pour assurer une excellente retenue axiale du manchon dans le tube, il est avantageux que le manchon présente, sur la face externe de sa partie qui s'emmanche dans une extrémité correspondante du tube, au moins un redent périphérique d'ancrage, qui est formé à l'extrémité axiale, tournée vers ladite extrémité du tube, d'une surface sensiblement tronconique à petite base tournée vers la partie centrale du tube, plusieurs redents décalés axialement étant de préférence formés de la sorte sur le manchon. De plus, ce dernier comporte avantageusement au moins une butée en saillie sensiblement radiale vers l'extérieur pour limiter son emmanchement dans une extrémité correspondante du tube.To this end, at least one of the ends of each tube is advantageously fixed to a half-shell using of a sleeve which is partly force-fitted into the corresponding end of the tube and retained on said half-shell by a part of sleeve external to the tube. To ensure excellent axial retention of the sleeve in the tube, it is advantageous that the sleeve has, on the external face of its part which is fitted at one end corresponding tube, at least one peripheral redent anchor, which is formed at the axial end, facing the said end of the tube, of a surface substantially frustoconical with small base facing the central part of the tube, several axially offset redents preferably being formed in this way on the sleeve. In addition, the latter advantageously comprises at least one projecting stop substantially radial towards the outside to limit its fitting into a corresponding end of the tube.

Avantageusement, le manchon ou chacun des deux manchons de liaison d'un tube, est moulé en une matière de synthèse, qui est de préférence une matière thermodurcissable.Advantageously, the sleeve or each of the two connecting sleeves of a tube, is molded from a material of synthesis, which is preferably a thermosetting material.

Dans un mode préféré de réalisation, pour chaque tube du collecteur, un manchon d'entrée d'air, emmanché dans une extrémité d'entrée d'un tube, est conformé, dans sa partie externe à ladite extrémité d'entrée du tube, en une tulipe convergente vers l'intérieur du tube et munie d'au moins une patte de fixation à celle des deux demi-coquilles qui n'est pas munie de la bride de fixation présentant l'ouverture d'alimentation à laquelle ledit tube est raccordé par sa sortie, la fixation étant par exemple assurée par thermosoudage ou par bouterollage au niveau de la ou des pattes de fixation.In a preferred embodiment, for each manifold tube, an air inlet sleeve, fitted into an inlet end of a tube, is shaped, in its external part at said inlet end of the tube, in a tulip converging towards the inside of the tube and provided with minus one fixing lug to that of the two half-shells which is not provided with the mounting flange having the feed opening at which said tube is connected by its output, the fixing being for example provided by heat sealing or by rolling at the fixing lug (s).

De même, chaque tube est avantageusement relié par un manchon de sortie d'air, emmanché dans l'extémité de sortie du tube, à celle des demi-coquilles qui est munie de ladite bride de fixation présentant ladite ouverture d'alimentation à laquelle ledit tube est relié de manière étanche par sa sortie, lesdits moyens de raccordement étanches comprenant un embout tubulaire de collecteur, en saillie sur ladite bride du côté opposé à la culasse, dans le prolongement de ladite ouverture d'alimentation correspondante, et dans lequel embout une partie dudit manchon de sortie, qui est externe au tube, est retenue avec interposition d'au moins un joint d'étanchéité souple entre ladite partie externe du manchon de sortie et ledit embout de collecteur.Likewise, each tube is advantageously connected by an air outlet sleeve, fitted into the end of outlet of the tube, to that of the half-shells which is provided with said fixing flange having said opening to which said tube is so connected waterproof by its outlet, said connection means watertight including a tubular manifold tip, in projection on said flange on the side opposite to the cylinder head, in the extension of said corresponding feed opening, and in which tip part of said sleeve outlet, which is external to the tube, is retained with interposition at least one flexible seal between said external part of the outlet sleeve and said end piece collector.

Avantageusement, pour faciliter la réalisation des pièces constitutives du collecteur et leur assemblage, chaque embout de collecteur comprend :

  • un berceau, moulé d'une seule pièce avec ladite demi-coquille et ladite bride de fixation correspondante, et de forme sensiblement hémi-cylindrique, dont l'extrémité interne à ladite demi-coquille présente un fond en forme de U formant butée en saillie vers l'intérieur du berceau, et
  • un couvercle rapporté de maintien du manchon de sortie et du ou des joints d'étanchéité montés sur ce dernier dans le berceau, ledit couvercle présentant une butée en saillie vers l'intérieur du berceau et en regard du fond en forme de U du berceau, et étant fixé sur des bords du berceau, de préférence par soudure aux ultrasons.
Advantageously, to facilitate the production of the constituent parts of the collector and their assembly, each collector endpiece comprises:
  • a cradle, molded in one piece with said half-shell and said corresponding fixing flange, and of substantially semi-cylindrical shape, the internal end of said half-shell having a U-shaped bottom forming a projecting stop towards the inside of the cradle, and
  • an attached cover for holding the outlet sleeve and the seal (s) mounted on the latter in the cradle, said cover having a stop projecting towards the inside of the cradle and facing the U-shaped bottom of the cradle, and being fixed on edges of the cradle, preferably by ultrasonic welding.

Une bonne étanchéité peut être assurée à l'aide d'un unique joint d'étanchéité souple pour chaque tube, si ce joint, monté autour de la partie du manchon de sortie correspondant qui est externe au tube et retenue dans l'embout de collecteur correspondant, est moulé en forme, de préférence en élastomère, avec une section transversale correspondant à celle de l'espace disponible entre, d'une part, ledit manchon de sortie, et, d'autre part, ledit berceau et ledit couvercle, et de sorte que le joint est comprimé radialement entre ces trois éléments.A good seal can be ensured using a single flexible gasket for each tube, if gasket, mounted around the part of the outlet sleeve corresponding which is external to the tube and retained in the nozzle corresponding collector, is molded in shape, preferably made of elastomer, with a cross section corresponding to that of the space available between, on the one hand, said outlet sleeve, and, on the other hand, said cradle and said cover, and so that the seal is compressed radially between these three elements.

Pour les cas où la section transversale du tube est circulaire ou oblongue, alors que la section transversale de l'ouverture d'alimentation correspondante est respectivement oblongue ou circulaire, l'embout de collecteur correspondant présente avantageusement une section transversale sensiblement de même forme que celle de ladite ouverture d'alimentation, et le manchon de sortie correspondant présente un passage central ayant une section transversale de forme évolutive, variant progressivement de la forme de section de l'embout de collecteur, dans la partie du manchon de sortie qui est externe au tube, à la forme de section du tube, dans la partie du manchon de sortie qui est emmanchée dans l'extrémité de sortie de ce tube, de sorte que le manchon de sortie constitue un manchon d'adaptation assurant la transition entre les formes des sections de l'embout de collecteur et du tube d'air.For cases where the cross section of the tube is circular or oblong, while the cross section of the corresponding feed opening is respectively oblong or circular, the corresponding manifold tip advantageously has a substantially cross section of the same shape as that of said feed opening, and the corresponding outlet sleeve has a central passage having a cross section of form evolutionary, varying gradually from the section shape of the manifold tip, in the part of the outlet sleeve which is external to the tube, to the cross-sectional shape of the tube, in the part of the outlet sleeve which is fitted into the outlet end of this tube, so that the sleeve of outlet constitutes an adapter sleeve ensuring the transition between the shapes of the tip sections manifold and air tube.

De plus, dans l'enveloppe, les tubes peuvent être groupés au moins par paires de tubes accolés sur au moins une partie de leur longueur, et, afin de limiter les déplacements transversaux des tubes ou groupes de tubes accolés dans l'enveloppe, des logements peuvent être délimités par des évidements dans la face interne de l'enveloppe, et des parties de tubes ou parties accolées de tubes peuvent être logées dans ces évidements, éventuellement bordés par des nervures en saillie sur la face interne de l'une au moins des demi-coquilles constituant l'enveloppe.In addition, in the envelope, the tubes can be grouped at least in pairs of tubes joined on at least part of their length, and, in order to limit the transverse displacements of tubes or groups of tubes attached to the envelope, housing can be delimited by recesses in the internal face of the envelope, and parts of tubes or joined parts of tubes can be accommodated in these recesses, possibly bordered by protruding ribs on the inner face of at least one of the half-shells constituting the envelope.

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 du collecteur de la figure 1, avec une des deux paires de tubes qui sont regroupés et retenus dans cette demi-coquille par leur extrémité de sortie,
  • les figures 3 et 4 sont des coupes transversales respectivement selon III-III et IV-IV de la figure 1, et
  • la figure 5 est une vue partielle en coupe axiale et à plus grande échelle d'un détail de la figure 2.
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 half-shell of the collector of Figure 1, with one of the two pairs of tubes which are grouped together and retained in this half-shell by their outlet end,
  • FIGS. 3 and 4 are cross sections respectively on III-III and IV-IV of FIG. 1, and
  • FIG. 5 is a partial view in axial section and on a larger scale of a detail in FIG. 2.

Le collecteur des figures 1 et 2, pour un moteur à quatre cylindres en ligne, comprend une enveloppe 1 rigide, en matière de synthèse moulable et thermosoudable telle qu'un polyamide éventuellement armé de fibres de renfort, et 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 par 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 de leurs manchons comme décrit ci-dessous.The manifold of Figures 1 and 2, for a motor with four cylinders in line, includes a rigid casing 1, in moldable and heat-sealable synthetic material such as a polyamide possibly reinforced with reinforcing fibers, and made up of two half-shells 2 and 3, each molded in this material, having complementary shapes which correspond to the shape of envelope 1. The two half-shells 2 and 3 close against each other, by their peripheral edges, to reconstitute the shape of envelope 1, and are secured to each other in a joint plane P, defined by fastening flanges 4 and 5, projecting outwards on their edges, by vibration welding at these flanges 4 and 5, after mounting in the half-shells 2 and 3 of four tubes air intake (one per engine cylinder), grouped in two pairs of joined tubes, as shown in the figure 2, and their sleeves as described below.

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 ou oblongue, 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 or oblong cross section, which opens out on one side in the flat face 8 for fixing the flange 6 on the engine cylinder head and, on the other side, inside the half-shell 3, lower in FIG. 1 and called the half-shell downstream, because intended to accommodate the downstream parts of air tubes as opposed to the upper 2 half shell in FIG. 1, called the upstream half-shell, since it is intended to accommodate the upstream parts of the air tubes. The flange 6 has also, for each cylinder, a housing 9 for a fuel injector, 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, of a part, 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 12a ou 12b de la paire de tubes de la figure 2, est un tube recourbé, obtenu en découpant, perpendiculairement à son axe longitudinal, une longueur déterminée, pour donner au tube 12a ou 12b une impédance acoustique accordée au moteur, dans un tube de grande longueur en thermoplastique, ayant une face interne 13 lisse, délimitant un passage central de section transversale de forme et surface constantes, par exemple circulaire, et une face externe annelée 14, avec des anneaux périphériques dans des plans sensiblement parallèles entre eux et perpendiculaires à l'axe du tube, avant que le tronçon de tube découpé ne soit recourbé à la forme voulue par la fermeture des demi-coquilles 2 et 3, à chacune desquelles chaque tube 12a ou 12b n'est fixé que par l'une respectivement de ses extrémités d'entrée telle que 15a et de sortie 16a ou 16b. On réalise ainsi un tube 12a ou 12b léger, à paroi mince et étanche, ayant une grande souplesse ou flexibilité transversale ou radiale, et une faible souplesse ou flexibilité axiale, de sorte qu'il peut être recourbé à la forme voulue sans perdre la forme et la surface constantes de la section transversale de son passage central à paroi lisse, et sans varier sensiblement de longueur, ce qui assure des pertes de charge et une impédance acoustique pratiquement constantes. Chaque tube tel que 12a ou 12b est recourbé selon une boucle presque complète dans le plan de la figure 1, sur une grande partie de sa longueur sensiblement à partir de son entrée telle que 15a, et sa partie aval est de plus coudée ou contrecoudée dans une direction perpendiculaire au plan de la figure 1, comme représenté sur la figure 2. Grâce 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 sur une grande partie de leur longueur sensiblement à partir de leurs entrées telles que 15a, tandis que leurs sorties 16a et 16b (voir figure 2) 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 contigus correspondants.Each tube, such as 12a or 12b of the pair of tubes of FIG. 2, is a curved tube, obtained by cutting, perpendicular to its longitudinal axis, a length determined, to give the tube 12a or 12b an impedance acoustic tuned to the engine, in a large tube length in thermoplastic, having an internal face 13 smooth, delimiting a central passage of cross section of constant shape and surface, for example circular, and a corrugated external face 14, with peripheral rings in planes substantially parallel to each other and perpendicular to the axis of the tube, before the tube section cut is not bent to the desired shape by the closure half-shells 2 and 3, each of which each tube 12a or 12b is fixed only by one respectively of its inlet ends such as 15a and outlet ends 16a or 16b. A light tube 12a or 12b is thus produced, with a thin wall and waterproof, having great flexibility or transverse flexibility or radial, and low flexibility or flexibility axial, so that it can be bent to the desired shape without losing the constant shape and surface of the section transverse of its central passage with smooth wall, and without vary significantly in length, which ensures losses of practically constant load and acoustic impedance. Each tube such as 12a or 12b is bent in a loop almost complete in the plan of figure 1, on a large part of its length substantially from its entrance such as 15a, and its downstream part is further angled or bent in a direction perpendicular to the plane of Figure 1, as shown in Figure 2. Thanks to their curved shapes, two tubes such as 12a and 12b, grouped into a pair of tubes to supply each one respectively of two adjacent cylinders, can be joined on much of their length substantially from their inputs such as 15a, while their outputs 16a and 16b (see Figure 2) are spaced from each other to each be tightly connected to one respectively two adjacent supply openings 7 one of the other in the flange 8 to supply the two cylinders corresponding contiguous.

L'extrémité d'entrée telle que 15a de chaque tube 12a ou 12b est fixée à la demi-coquille amont 2 par un manchon d'entrée d'air tel que 17a, tandis que l'extrémité de sortie 16a ou 16b du tube est reliée à la demi-coquille aval 3 par un manchon de sortie d'air 18a ou 18b, chacun des manchons 17a, 18a ou 18b étant moulé de préférence dans une matière de synthèse, de préférence thermodurcissable.The inlet end such as 15a of each tube 12a or 12b is fixed to the upstream half-shell 2 by a air inlet sleeve such as 17a, while the end outlet 16a or 16b of the tube is connected to the half-shell downstream 3 by an air outlet sleeve 18a or 18b, each of sleeves 17a, 18a or 18b being preferably molded in a synthetic material, preferably thermosetting.

Le manchon d'entrée 17a comprend une partie tubulaire 19a qui est emmanchée à force dans l'extrémité d'entrée 15a du tube 12a, et qui se prolonge vers l'avant, à l'extérieur de cette entrée 15a, par une partie conformée en volute ou tulipe d'entrée 20a convergente vers l'intérieur du tube 12a et vers l'aval. Cette tulipe d'entrée 20a présente une patte de fixation 21a, par laquelle le manchon 17a est fixé à la demi-coquille 2 en au moins un point, par exemple par thermosoudure ou par une bouterolle, comme schématisé en 22a. Pour réduire les pertes de charge, la face interne de la partie tubulaire 19a est lisse, et sensiblement dans le prolongement de la face interne lisse 13 du tube 12a, tandis que pour assurer un bon emmanchement axial du manchon 17a dans l'entrée 15a du tube 12a, la face externe de la partie tubulaire 19a présente des redents périphériques, comme décrit ci-dessous pour le manchon de sortie 18a en référence à la figure 5.The inlet sleeve 17a comprises a tubular part 19a which is forced into the end inlet 15a of the tube 12a, and which extends towards the front, outside this entry 15a, by a shaped part in volute or inlet tulip 20a converging inwards from tube 12a and downstream. This entrance tulip 20a has a fixing lug 21a, by which the sleeve 17a is fixed to the half-shell 2 at at least one point, by example by heat sealing or by a dowel, as shown schematically in 22a. To reduce pressure drops, the internal face of the tubular part 19a is smooth, and substantially in line with the smooth internal face 13 of the tube 12a, while to ensure a good fit axial of the sleeve 17a in the inlet 15a of the tube 12a, the face outer of the tubular part 19a has redents peripherals, as described below for the output 18a with reference to Figure 5.

Chaque manchon de sortie 18a ou 18b comprend, comme représenté pour le manchon 18a sur la figure 5, une partie tubulaire 23a qui est emmanchée à force dans la sortie 16a du tube 12a, et qui se prolonge vers l'arrière ou vers l'aval, à l'extérieur de cette sortie 16a, par une partie tubulaire 24a externe au tube 12a et retenue sur la demi-coquille 3 en étant raccordée avec étanchéité à l'ouverture 7 correspondante de la manière décrite ci-dessous. Les parties 23a et 24a, entre lesquelles le manchon 18a présente une butée annulaire 25a en saillie radialement vers l'extérieur pour limiter l'emmanchement dans la sortie 16a du tube 12a, ont une face interne lisse, sensiblement dans le prolongement de la face interne lisse 13 du tube 12a, tandis que la face externe de la partie emmanchée 23a présente deux redents 26a périphériques et axialement décalés, formés chacun à l'extrémité axiale, tournée vers la butée 25a, d'une surface sensiblement tronconique 27a à petite base tournée vers l'extrémité de la partie 23a la plus à l'intérieur du tube 12a, de façon à faciliter la pénétration à l'emmanchement et à assurer un bon ancrage.Each outlet sleeve 18a or 18b includes, as shown for the sleeve 18a in FIG. 5, a part tubular 23a which is force fitted into outlet 16a of tube 12a, and which extends backwards or towards downstream, outside this exit 16a, by a part tubular 24a external to tube 12a and retained on the half-shell 3 while being connected with sealing at the opening 7 corresponding as described below. The parts 23a and 24a, between which the sleeve 18a has an annular stop 25a projecting radially outwards to limit fitting in outlet 16a of the tube 12a, have a smooth internal face, substantially in the extension of the smooth internal face 13 of the tube 12a, while that the external face of the fitted part 23a has two peripheral and axially offset redents 26a, each formed at the axial end, facing the stop 25a, of a substantially frustoconical surface 27a with small turned base towards the end of the innermost part 23a of the tube 12a, so as to facilitate penetration at the fitting and to ensure good anchoring.

Un joint d'étanchéité souple et annulaire 28, moulé en élastomère avec la forme en coupe représentée sur la figure 4, est monté autour de la partie externe 24a du manchon 18a, et cette partie externe 24a entourée du joint 28 est introduite dans un berceau 29a, moulé d'une seule pièce avec la demi-coquille 3 et la bride 6. Ce berceau 29a 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, avec une section transversale de forme en U de surface sensiblement constante, 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, le berceau 29a présente une chambre annulaire délimitée par un fond en forme de U 30a en saillie radialement vers l'intérieur du berceau 29a pour former une butée s'opposant à la sortie axiale du joint 28 sur la partie externe 24a du manchon 18a. Lors de cette mise en place de la partie externe 24a dans le berceau 29a, le joint d'étanchéité 28 autour du manchon 18a est comprimé radialement entre le manchon 18a et le berceau 29a. La retenue de la partie 24a du manchon 18a dans le berceau 29a de la demi-coquille 3 et son raccordement étanche à l'ouverture 7 correspondante, grâce au joint d'étanchéité 28, sont complétés par un couvercle 31a plat rapporté transversalement sur la partie 24a du manchon 18a engagée dans le berceau 29a, et prenant appui par son pourtour contre les bords de ce berceau 29a, le couvercle 31a présentant un rebord 32a en forme de butée en arc-de-cercle en saillie vers l'intérieur du berceau 29a, et en regard du fond en forme de U 30a de ce dernier, de sorte que le rebord 32a et le fond en forme de U 30a forment ensemble une butée annuulaire. Ce couvercle 31a est moulé en matière de synthèse, de préférence thermoplastique, et de préférence soudé par ultrasons sur son pourtour sur les bords du berceau 29a. Le maintien du manchon 18a et l'étanchéité de sa liaison à l'ouverture 7 correspondante sont ainsi assurés grâce au joint d'étanchéité 28 et à un embout tubulaire de collecteur, formé par le berceau 29a et le couvercle 31a correspondant. Comme montré par la coupe de la figure 4, le joint 28 est moulé avec une forme de section telle qu'il occupe radialement tout l'espace disponible entre la partie 24a du manchon 18a, au centre, et le berceau 29a et le couvercle 31a, à la périphérie, en étant comprimé radialement entre ces pièces. Au delà du joint 28 et vers l'ouverture 7, la partie 24a du manchon 18a se prolonge par une extrémité en forme de demi-cylindre ouvert vers le fond du berceau 29a qui la reçoit, et ayant, comme montré sur la coupe de la figure 3, un évidement complémentaire de celui du berceau 29a pour définir un conduit de section progressivement variable raccordant la sortie, par exemple circulaire, 16a du tube 12a à la section, par exemple oblongue, de l'ouverture 7 correspondante, comme représenté sur les dessins. Le manchon de sortie 18a est moulé de sorte que son passage central présente cette évolution correspondante de section, la section de l'extrémité du manchon 18a emmanchée dans le tube 12a ayant toujours la même forme que la section du tube 12a, et la section de l'extrémité du manchon 18a tournée vers l'ouverture 7 ayant, à elle seule ou avec la section complémentaire du fond du berceau 29a qui la reçoit, la même forme que la section de l'ouverture 7.A flexible, annular seal 28, molded made of elastomer with the sectional shape shown on the Figure 4, is mounted around the outer part 24a of the sleeve 18a, and this external part 24a surrounded by the seal 28 is introduced into a cradle 29a, molded in one part with the half-shell 3 and the flange 6. This cradle 29a 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, with a cross section of substantially constant surface U-shape, defining 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, the cradle 29a has a chamber annular delimited by a projecting U-shaped bottom 30a radially inward of the cradle 29a to form a stop opposing the axial outlet of the seal 28 on the external part 24a of the sleeve 18a. During this implementation place of the external part 24a in the cradle 29a, the seal seal 28 around the sleeve 18a is compressed radially between the sleeve 18a and the cradle 29a. The restraint of the part 24a of the sleeve 18a in the cradle 29a of the half-shell 3 and its tight connection to the opening 7 corresponding, thanks to the gasket 28, are completed by a flat cover 31a attached transversely to the part 24a of the sleeve 18a engaged in the cradle 29a, and leaning by its periphery against the edges of this cradle 29a, the cover 31a having a rim 32a in inwardly projecting arcuate abutment shape of cradle 29a, and opposite the U-shaped bottom 30a of this last, so that the rim 32a and the bottom in the shape of U 30a together form an annular stop. This cover 31a is molded in synthetic material, preferably thermoplastic, and preferably ultrasonically welded to its around the edges of the cradle 29a. Maintaining the sleeve 18a and the tightness of its connection to the opening 7 corresponding are thus ensured thanks to the seal 28 and to a tubular manifold end, formed by the cradle 29a and the corresponding cover 31a. As shown in the section of Figure 4, the seal 28 is molded with a sectional shape such that it occupies radially all the space available between the part 24a of the sleeve 18a, in the center, and the cradle 29a and the cover 31a, at the periphery, being compressed radially between these parts. Beyond the joint 28 and towards the opening 7, the part 24a of the sleeve 18a is extended by a half-cylinder-shaped end open towards the bottom of the cradle 29a which receives it, and having, as shown in the section of FIG. 3, a recess complementary to that of the cradle 29a for define a duct of progressively variable section connecting the outlet, for example circular, 16a of the tube 12a to the section, for example oblong, of the opening 7 corresponding, as shown in the drawings. The sleeve outlet 18a is molded so that its central passage presents this corresponding section evolution, the section of the end of the sleeve 18a fitted into the tube 12a always having the same shape as the section of the tube 12a, and the section of the end of the sleeve 18a facing opening 7 having, alone or with the section complementary to the bottom of the cradle 29a which receives it, the same forms as the section of the opening 7.

Le manchon de sortie 18b du tube 12b est monté de la même manière avec un joint d'étanchéité tel que 28 dans un embout de collecteur constitué d'un berceau 29b analogue fermé par un couvercle analogue correspondant.The outlet sleeve 18b of the tube 12b is mounted from the same way with a seal such as 28 in one manifold tip consisting of a similar cradle 29b closed by a corresponding analog cover.

Pour limiter leurs déplacements transversaux, les deux tubes 12a et 12b sont également disposés, par leurs parties accolées, dans un logement délimité dans la demi-coquille aval 3 par un évidement entre des nervures 33 en saillie sur la face interne de cette demi-coquille 3.To limit their transverse movements, the two tubes 12a and 12b are also arranged, by their adjoining parts, in a housing delimited in the half-shell downstream 3 by a recess between ribs 33 in projection on the internal face of this half-shell 3.

Les tubes 12a et 12b peuvent être accolés de sorte que les anneaux de la face externe de l'un soient engagés entre les anneaux de l'autre, et, éventuellement, les nervures 33 bordant les logements peuvent présenter des saillies s'engageant entre les anneaux externes des tubes 12a,12b pour mieux les positionner dans l'enveloppe 1.Tubes 12a and 12b can be joined so that the rings of the external face of one are engaged between each other’s rings, and possibly ribs 33 bordering the housings may have protrusions engaging between the outer rings of the tubes 12a, 12b to better position them in the envelope 1.

Comme les tubes 12a et 12b souples transversalement sont fixés à l'enveloppe 1 par leurs seules extrémités, le montage des manchons 17a et 18a est effectué pour donner aux tubes un rayon de courbure général qui est légèrement inférieur au rayon de courbure des parties arrondies des demi-coquilles 2 et 3 de l'enveloppe 1.As tubes 12a and 12b flexible transversely are fixed to the casing 1 by their only ends, the mounting of the sleeves 17a and 18a is carried out to give the tubes a general radius of curvature which is slightly less at the radius of curvature of the rounded parts of the half-shells 2 and 3 of envelope 1.

La souplesse transversale des tubes permet, lors de l'assemblage des demi-coquilles 2 et 3, de petits déplacements relatifs alternés de celles-ci dans le sens perpendiculaire au rayon de courbure des tubes, offrant ainsi la possibilité d'effectuer l'assemblage des demi-coquilles 2 et 3 par exemple par soudure par vibrations.The transverse flexibility of the tubes allows, during assembling the half-shells 2 and 3, small displacements alternating relative of these in the perpendicular direction to the radius of curvature of the tubes, thus providing the possibility of assembling the half-shells 2 and 3 for example by vibration welding.

On obtient ainsi un collecteur dont l'enveloppe 1 délimite une chambre interne 34, appelée plenum, qui est alimentée en air d'alimentation du moteur par une ouverture (non représentée) par exemple ménagée dans une face d'extrémité de l'enveloppe 1 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 34 par son entrée telle que 15a et transmet cet air par sa sortie 16a ou 16b 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 34, called plenum, which is supplied with engine feed air through an opening (not shown) for example formed in an end face of the envelope 1 parallel to the plane of FIG. 1, this opening being connected to a butterfly body. Each tube such as 12a or 12b mounted in the casing 1 sucks from the air in plenum 34 by its entry such as 15a and transmits this air through its outlet 16a or 16b to an opening supply 7 of the flange 6 to supply a cylinder corresponding. We understand that the envelope 1 contains, in its half not shown in Figure 2, two other tubes symmetrical air suction tubes 12a and 12b and mounted in the same way.

Claims (14)

  1. Inlet manifold for an internal combustion engine and comprising:
    an envelope (1), delimiting a plenum chamber (34) intended to be supplied with air for supplying the engine, and equipped with at least one flange (6) for attaching it to at least one cylinder head of the engine, the said flange or flanges having at least one opening (7) for supplying each cylinder of the engine, each supply opening (7) opening, on the one hand, into the envelope (1) and, on the other hand, into a face (8) for attaching the flange (6) to the said cylinder head, and
    curved air-induction tubes (12a, 12b) each made as a single piece, and of which there are at least as many as there are cylinders in the engine, and which are mounted in the envelope (1) so that each tube supplies a corresponding cylinder with air which it receives via its inlet (15a) in the plenum chamber (34) and which it transmits to the corresponding opening (7) in the corresponding flange (6) via its outlet (16a, 16b) connected by leaktight connecting means to the said supply opening (7), characterized in that each tube (12a, 12b) is a tube with a ringed external face (14) and a smooth internal face (13) delimiting a central passage with a cross section which is constant in terms of shape and in terms of surface-area, so that the tube (12a, 12b) has great transverse suppleness or flexibility but low axial suppleness or flexibility.
  2. Inlet manifold according to Claim 1, characterized in that each tube (12a, 12b) is made of a synthetic material, preferably a moldable one, such as a thermoplastic, and is preferably of circular section.
  3. Inlet manifold according to either of Claims 1 and 2, characterized in that the ringed external face (14) of each tube (12a, 12b) is a cylindrical surface of revolution with a wavy generatrix before the tube is bent into the desired shape.
  4. Inlet manifold according to any one of Claims 1 to 3, characterized in that the envelope (1) consists of two half shells (2, 3) of complementary shapes corresponding to the shape of the envelope (1) and which are molded, preferably of a moldable synthetic material, preferably thermoplastic, with attachment flanges (4, 5) on their peripheral edges in a parting plane (P), the half shells (2, 3) being closed and fixed together at their attachment flanges (4, 5), for example by welding, preferably vibration welding, and each tube (12a, 12b) is fixed to the half shells (2, 3) only by its ends (15a, 16a, 16b).
  5. Inlet manifold according to Claim 4, characterized in that at least one of the ends (15a, 16a) of each tube (12a) is fixed to a half shell (2, 3) using a sleeve (17a, 18a) which is partly (19a, 23a) force-fitted into the corresponding end (15a, 16a) of the tube and held on the said half shell (2, 3) by a sleeve part (20a, 24a) external to the tube (12a).
  6. Inlet manifold according to Claim 5, characterized in that on the external face of its part (23a) that is pushed into a corresponding end (16a) of the tube (12a), the sleeve (18a) has at least one peripheral anchoring tooth (26a) which is formed at the axial end pointing toward the said end (16a) of the tube (12a), with a more or less frustoconical surface (27a) with the small base pointing toward the central part of the tube (12a).
  7. Inlet manifold according to either of Claims 5 and 6, characterized in that the sleeve (18a) has at least one stop (25a) projecting more or less radially outward to limit the extent to which it can be pushed into a corresponding end (16a) of the tube (12a).
  8. Inlet manifold according to one of Claims 5 to 7, characterized in that the sleeve (17a, 18a, 18b) is molded of a synthetic material, preferably a thermoset.
  9. Inlet manifold according to any one of Claims 5 to 8, characterized in that at least one air inlet sleeve (17a) pushed (19a) into an inlet end (15a) of a tube (12a) is shaped, in its part external to the said inlet end (15a) of the tube (12a) as a bell housing (20a) that converges toward the inside of the tube (12a) and is equipped with at least one lug (21a) for attaching it to that one (2) of the two half shells (2, 3) which does not have the attachment flange (6) with the supply opening (7) to which the said tube (12a) is connected by its outlet (16a).
  10. Inlet manifold according to any one of Claims 5 to 9, characterized in that each tube (12a) is connected by an air outlet sleeve (18a) pushed (23a) into the outlet end (16a) of the tube (12a) to that one (3) of the half shells (2, 3) which has the said attachment flange (6) with the said supply opening (7) to which the said tube (12a) is connected in leaktight fashion by its outlet (16a), the said leaktight connection means comprising a tubular manifold end piece (29a - 31a) projecting from the said flange (6) on the opposite side to the cylinder head, in line with the said corresponding supply opening (7) and in which end piece part (24a) of the said outlet sleeve (18a), external to the tube (12a), is held with the insertion of at least one flexible seal (28) between the said external part (24a) of the outlet sleeve (18a) and the said manifold end piece (29a - 31a).
  11. Inlet manifold according to Claim 10, characterized in that the said manifold end piece comprises:
    a cradle (29a) molded as a single piece with the said half shell (3) and the said corresponding attachment flange (6), and of a more or less semicylindrical shape, of which the end internal to the said half shell (3) has a U-shaped bottom (30a) forming a stop projecting toward the inside of the cradle (29a), and
    an attached cover (31a) for holding the outlet sleeve (18a) and the seal or seals (28) which are mounted on the latter in the cradle (29a), the said cover (31a) having a stop (32a) projecting toward the inside of the cradle (29a) opposite the U-shaped bottom (30a) of the cradle (29a) and being fixed to the edges of the cradle (29a) preferably by ultrasound welding.
  12. Inlet manifold according to Claim 11, characterized in that it comprises, for each tube (12a), a single flexible seal (28) mounted around that part (24a) of the corresponding outlet sleeve (18a) which is external to the tube (12a) and held in the corresponding manifold end piece (29a - 31a) and molded into a shape, preferably from elastomer, with a cross section that corresponds to that of the space available between, on the one hand, the said outlet sleeve (18a) and, on the other hand, the said cradle (29a) and the said cover (31a) and so that the seal (28) is compressed radially between these three components.
  13. Inlet manifold according to any one of Claims 10 to 12, characterized in that each manifold end piece (29a - 31a) has a cross section which is more or less the same shape as the corresponding supply opening (7) and in that the corresponding outlet sleeve (18a) has a central passage which has a cross section of changeable shape, this shape varying progressively from the cross-sectional shape of the manifold end piece (29a - 31a), in that part (24a) of the outlet sleeve (18a) which is external to the tube (12a), to the cross-sectional shape of the tube (12a), in that part (23a) of the outlet sleeve (18a) which is pushed into the outlet end (16a) of the tube (12a).
  14. Inlet manifold according to any one of Claims 1 to 13, characterized in that in the envelope (1) the tubes (12a, 12b) are grouped at least in pairs of tubes that touch over at least part of their length, and the transverse displacements of the groups of touching tubes in the envelope (1) are limited by housings delimited by recesses in the internal face of the envelope (1) and in which touching parts of the tubes (12a, 12b) are housed.
EP96917521A 1995-05-23 1996-05-20 Intake manifold with ringed air tubes for internal combustion engines Expired - Lifetime EP0827567B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9506119A FR2734603B1 (en) 1995-05-23 1995-05-23 INTAKE MANIFOLD WITH ANNULATED AIR TUBES, FOR INTERNAL COMBUSTION ENGINE
FR9506119 1995-05-23
PCT/FR1996/000750 WO1996037696A1 (en) 1995-05-23 1996-05-20 Intake manifold with ringed air tubes for internal combustion engines

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EP0827567A1 EP0827567A1 (en) 1998-03-11
EP0827567B1 true EP0827567B1 (en) 2000-04-12

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US (1) US5964194A (en)
EP (1) EP0827567B1 (en)
DE (1) DE69607752T2 (en)
FR (1) FR2734603B1 (en)
WO (1) WO1996037696A1 (en)

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US5651338A (en) * 1996-03-26 1997-07-29 Pacheco; Allan A. Adjustable induction manifold system

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DE69607752D1 (en) 2000-05-18
FR2734603A1 (en) 1996-11-29
US5964194A (en) 1999-10-12
FR2734603B1 (en) 1997-07-25
WO1996037696A1 (en) 1996-11-28
DE69607752T2 (en) 2000-11-23
EP0827567A1 (en) 1998-03-11

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