EP1915519A1 - Exhaust pipe - Google Patents

Exhaust pipe

Info

Publication number
EP1915519A1
EP1915519A1 EP06808051A EP06808051A EP1915519A1 EP 1915519 A1 EP1915519 A1 EP 1915519A1 EP 06808051 A EP06808051 A EP 06808051A EP 06808051 A EP06808051 A EP 06808051A EP 1915519 A1 EP1915519 A1 EP 1915519A1
Authority
EP
European Patent Office
Prior art keywords
fibers
tube
conduit according
holding layer
inner tube
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP06808051A
Other languages
German (de)
French (fr)
Other versions
EP1915519B1 (en
Inventor
Vincent Leroy
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.)
Faurecia Systemes dEchappement SAS
Original Assignee
Faurecia Systemes dEchappement 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 Faurecia Systemes dEchappement SAS filed Critical Faurecia Systemes dEchappement SAS
Publication of EP1915519A1 publication Critical patent/EP1915519A1/en
Application granted granted Critical
Publication of EP1915519B1 publication Critical patent/EP1915519B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08Other arrangements or adaptations of exhaust conduits
    • F01N13/10Other arrangements or adaptations of exhaust conduits of exhaust manifolds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/14Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00 having thermal insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08Other arrangements or adaptations of exhaust conduits
    • F01N13/10Other arrangements or adaptations of exhaust conduits of exhaust manifolds
    • F01N13/102Other arrangements or adaptations of exhaust conduits of exhaust manifolds having thermal insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/16Selection of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2310/00Selection of sound absorbing or insulating material
    • F01N2310/02Mineral wool, e.g. glass wool, rock wool, asbestos or the like

Definitions

  • the present invention relates to an exhaust duct comprising, arranged concentrically:
  • the elements of the exhaust line between the engine outlet and the pollution control members comprise an inner ceramic tube surrounded by an outer tube of metal between which is interposed an insulating material.
  • the ceramic tube because of its low thermal inertia, greatly reduces the heat transfer of the exhaust gas to the ceramic tube.
  • the low thermal expansion of the inner ceramic tube makes it possible to produce single-piece internal pipes even for engines that release exhaust gases at very high temperatures, in particular greater than 1000 ° C. without risk of thermomechanical rupture.
  • Such a structure is used in particular in the exhaust manifolds provided immediately at the output of the engine.
  • a relatively thick, thermally insulating layer of ceramic fibers in contact with the ceramic tube.
  • the thick layer of ceramic fibers has a thickness of between 1 mm and 40 mm and preferably between 2 mm and 20 mm.
  • a so-called thin layer of stress isolation is provided between the thick layer of ceramic fiber and the outer tube of metal. This thin layer of stress isolation is between 0.05 mm and 2 mm and preferably between 0.1 mm and 0.5 mm. This layer of stress insulation is designed to absorb the vibrations of the engine and the road to prevent the destruction of the thick ceramic fiber layer.
  • This layer also attenuates the vibrations, in particular by compensating the differential thermal expansions between the thick ceramic fiber layer and the outer metal tube during heating of the exhaust line. Indeed, when the inner tube is traversed by gases at high temperatures, there are significant differential thermal expansions because the dense inner ceramic tube and the thick layer of ceramic fibers have relatively low expansion coefficients in comparison with the outer tube made of metal.
  • US 6,725,658 thus describes a multilayer structure comprising at least a dense ceramic inner layer, a thermally insulating thick layer of ceramic fibers and a metal layer. This structure is optionally supplemented by a thin layer of stress insulation for protecting the thick layer of ceramic fibers from vibrations.
  • an object of the invention is an exhaust duct for satisfactory heat delivery comprising an inorganic matrix composite inner pipe held in an outer metal structure.
  • the subject of the invention is an exhaust duct of the aforementioned type, characterized in that the thickness of the holding layer is between 2 mm and 10 mm, and preferably between 3 mm and 6 mm, and in that the minimum holding pressure exerted by the retaining layer on the inner tube is between 10 -4 MPa and 10 -1 MPa.
  • the duct below comprises one or more of the characteristics following:
  • the minimum holding pressure exerted by the retaining layer on the inner tube is between 10 3 MPa and 5 ⁇ 10 -2 MPa
  • the outer metal tube has a thickness of between 0.5 mm and 3 mm
  • the outer metal tube is chosen from the group consisting of a steel tube, an aluminum tube and a titanium tube,
  • the outer tube is formed of two half-shells in the form of gutters assembled by longitudinal joints, the inner tube of inorganic matrix composite has a thickness of less than 2 mm,
  • the inorganic matrix composite internal tube comprises a matrix consisting of at least one inorganic polymer
  • the inorganic polymer is a geopolymer based on aluminosilicate
  • the inorganic matrix composite internal tube comprises a matrix reinforced with fibers, in particular based on silicon carbide (SiC), carbon, silica (SiO2), or a stainless wire resistant to temperatures equal to or greater than 600 °,
  • the holding layer comprises a sheet of ceramic fibers
  • the holding layer comprises ceramic fibers and an inorganic binder, the holding layer comprising between 90% to 100% by weight of ceramic fibers
  • the ceramic fibers are fibers selected from the group consisting of silica fibers, alumina fibers, zirconium fibers, alumina-borosilicate fibers, and mixtures thereof,
  • the fibers contained in the holding layer are a mixture of alumina fibers and silica fibers in a ratio of 72 and 28% respectively,
  • the GBD of the material constituting the holding layer is between 0.1 and 0.6
  • the density of the material constituting the holding layer is between 500 g / m 2 and 3000 g / m 2 ,
  • the coefficient of friction of the material forming the holding layer against the surfaces of the inner and outer tubes is between 0.15 and 0.7
  • the exhaust manifold comprises at least one exhaust duct as defined above.
  • FIG. 1 is a perspective view of an exhaust manifold according to the invention.
  • FIG. 2 is a sectional view of an exhaust pipe of the manifold of FIG. 1.
  • the exhaust manifold 10 illustrated in FIG. 1 is intended to be disposed at the outlet of a heat engine at the inlet. an exhaust system of a motor vehicle.
  • This exhaust line comprises downstream of the collector 10, possibly a supercharging system tion (turbo) and one or more depollution elements capable of operating at high temperature.
  • Turbo supercharging system tion
  • the collector 10 has a plurality of inlets 12 converging towards an outlet flange 14.
  • the inlets 12 are connected to the outlet flange 14 by ducts 20 opening into each other.
  • each conduit 20 comprises an inner tube 22 of inorganic matrix composite, in particular ceramic, and an outer metal tube 24 between which is disposed a holding layer 26 made of a ceramic fibrous material.
  • the conduit consists of only three layers 22, 24 and 26.
  • the outer tube 24 is formed of a metal wall having a thickness of between 0.5 and 3 mm. According to a first embodiment, the outer tube 24 is a cylindrical metal tube including steel, aluminum or titanium.
  • the outer tube 24 is formed of two metal half-shells 27 in the form of gutters joined by opposite longitudinal seals 28.
  • the outer tube 24 is provided with flanges allowing its connection with, upstream, the engine and downstream, the exhaust line of the vehicle.
  • the choice of an outer metal tube is justified by the need to ensure optimum sealing upstream of the pollution control elements, and in particular at the junction of the outer tube with the upstream and downstream metal flanges.
  • the authorized leakage flow rate is 25 liters / hour at 20 ° C. under 1.3 bar.
  • the inner tube 22 is a tube formed from a composite material with an inorganic matrix, in particular a ceramic matrix. Examples of inorganic matrix composite materials that can allow the formation of the inner tube 22 are given in patent applications US6134881 and WO2004106705. These materials are formed by the combination of a matrix consisting of at least one inorganic polymer, preferably of geopolymer type, based on aluminosilicate.
  • the inner tube 22 is formed of a wall having a thickness of less than 2 mm.
  • the holding layer 26 has a thickness of between
  • the holding layer 26 is formed of a layer of ceramic fibers, in particular long ceramic fibers preferably associated with an organic and / or inorganic binder.
  • the organic binder is only useful when placing the holding layer around the inner tube; it is consumed during the first temperature rise of the exhaust duct on the vehicle. This binder represents from 0 to 15% by weight of the new holding layer.
  • the inorganic binder is used when it is necessary to ensure better cohesion between the fibers during operation of the vehicle and must not be burned.
  • This binder represents from 0 to 10% by weight of the organic binder-free holding layer.
  • the ceramic fibers represent 90 to 100% by weight of the holding layer, the remainder being the inorganic binder.
  • the ceramic fibers present in the holding layer 26 are selected from the group consisting of silica fibers, alumina fibers, zirconium fibers, borosilicate alumina fibers and a mixture thereof.
  • the sheets may be needled, which improves their behavior over time.
  • the fibers used are mullite fibers combining alumina and silica in a ratio of 72% and 28%, respectively.
  • the density of the material constituting the holding layer is between 500 g / m 2 and 3000 g / m 2 .
  • This holding layer 26 must maintain the inner tube 22 in the outer tube 24 regardless of the operating conditions.
  • the minimum pressure to be applied to maintain said inner tube in the metal tube is determined. This minimum pressure takes into account, in addition to the above mentioned solicitations, a specific corrective factor of the operating behavior of the inner ceramic tube and the holding layer. A coefficient of friction intervenes in this corrective factor.
  • the material constituting the holding layer is chosen so that the coefficient of friction of the damping layer against the surfaces of the inner and outer tubes is between 0.15 and 0.7.
  • the minimum holding pressure is between 10 "4 and 10" 1 MPa and preferably between 10 "3 MPa and 5.10" 2 MPa.
  • the value of 10 "3 MPa corresponds to an inner tube of 100 grams having a contact area of 40 dm 2 with the holding layer subjected to an acceleration of 10 g and a pressure drop of 100 Pa. This pressure drop is induced by the friction of the gases against the wall of the inner tube
  • the value of 5.10 "2 MPa corresponds to an inner tube of 200 grams having a contact surface of 20 dm 2 with the holding layer and subjected to an acceleration of 40 g and a loss charge of 250Pa.
  • the value of the clearance between the outer and inner tubes is dictated in particular by the shape constraints of the exhaust line element.
  • the usable GBD range is 0.1 to 0.6. The minimum value is given to avoid vibrational deterioration of the fibers, the maximum value is given to avoid deterioration of the fibers by compression.
  • the GBD is 0.3.
  • the holding pressure exerted by the ply on the internal ceramic matrix composite tube is then, for the chosen type of ply, 0.2 MPa.
  • This GBD of 0.3 is well within the recommended GBD range. This pressure is greater than the minimum holding pressure calculated for this application (5.10 "2 MPa) and lower than the mechanical strength of the inner tube.
  • the maximum clearance for this same application is 4.25 mm, corresponding to a GBD of 0.22 and a holding pressure of 6.10 "2 MPa.
  • the GBD remains in the range of use of the web and the induced pressure remains greater than the minimum holding pressure. It is noted that with such an exhaust duct, the holding material correctly ensures the maintenance of the inner tube of inorganic matrix composite in the outer metal tube regardless of the temperature of the exhaust line and the flow conditions. gaseous and acceleration to which the inner tube is subjected without deteriorating or damaging the inner tube.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Valve Device For Special Equipments (AREA)
  • Seal Device For Vehicle (AREA)
  • Steroid Compounds (AREA)

Abstract

The invention relates to an exhaust pipe (20) comprising the following elements which are disposed concentrically, namely: an inner tube which is made from an inorganic matrix composite (22); an outer metal tube (24); and a support layer (26) which is made from a fibrous material. The thickness of the support layer (26) measures between 2 mm and 10 mm and preferably between 3 mm and 6 mm. The maximum support pressure exerted by the support layer (26) on the inner tube (22) is between 10-4 MPa and 10-1 MPa.

Description

Conduit d'échappement Exhaust pipe
La présente invention concerne un conduit d'échappement comportant, disposés de manière concentrique :The present invention relates to an exhaust duct comprising, arranged concentrically:
- un tube interne en composite à matrice inorganique ;an internal tube made of an inorganic matrix composite;
- un tube externe métallique ; etan external metal tube; and
- une couche de maintien d'un matériau fibreux.a layer for holding a fibrous material.
De nos jours, l'implantation d'organes de dépollution dans les lignes d'échappement nécessite une gestion précise des flux thermiques du moteur jusqu'à la sortie d'échappement. En particulier, il convient de permettre que l'essentiel de la chaleur produite par le moteur parvienne aux équipements de dépollution implantés sur la ligne d'échappement. Un tel transfert est exigé notamment lors du démarrage du véhicule afin de permettre une montée rapide en température des éléments catalytiques. En effet, avant une température prédéterminée, ceux-ci ne sont pas actifs.Nowadays, the implementation of pollution control components in the exhaust lines requires precise management of the thermal flows of the engine to the exhaust outlet. In particular, it is necessary to allow most of the heat produced by the engine to reach the pollution control equipment located on the exhaust line. Such a transfer is required especially when starting the vehicle to allow a rapid rise in temperature of the catalytic elements. Indeed, before a predetermined temperature, they are not active.
Afin de permettre une montée rapide en température du catalyseur, il est connu que les éléments de la ligne d'échappement compris entre la sortie du moteur et les organes de dépollution comportent un tube interne en céramique entouré d'un tube externe en métal entre lesquels est interposé un matériau isolant. En effet, le tube céramique, du fait de sa faible inertie thermique, réduit fortement le transfert thermique des gaz d'échappement vers le tube céramique.In order to allow a rapid rise in temperature of the catalyst, it is known that the elements of the exhaust line between the engine outlet and the pollution control members comprise an inner ceramic tube surrounded by an outer tube of metal between which is interposed an insulating material. Indeed, the ceramic tube, because of its low thermal inertia, greatly reduces the heat transfer of the exhaust gas to the ceramic tube.
Par ailleurs, la faible dilatation thermique du tube interne céramique permet de réaliser des conduites internes monobloc même pour des moteurs libérant des gaz d'échappement à très hautes températures, notamment supérieures à 10000C sans risque de rupture thermomécanique.In addition, the low thermal expansion of the inner ceramic tube makes it possible to produce single-piece internal pipes even for engines that release exhaust gases at very high temperatures, in particular greater than 1000 ° C. without risk of thermomechanical rupture.
Une telle structure est utilisée notamment dans les collecteurs d'échappement prévus immédiatement en sortie du moteur.Such a structure is used in particular in the exhaust manifolds provided immediately at the output of the engine.
Un tel collecteur est décrit par exemple dans le document US 6,725,658.Such a collector is described for example in US 6,725,658.
Dans ce document, il est proposé de prévoir entre le tube interne de céramique dense et le tube externe de métal, une couche relativement épaisse, thermiquement isolante, de fibres céramiques en contact avec le tube de céramique. La couche épaisse de fibres céramiques a une épaisseur comprise entre 1 mm et 40 mm et de préférence entre 2 mm et 20 mm. Dans un mode de réalisation particulier, une couche mince dite d'isolation des contraintes est prévue entre la couche épaisse de fibres cé- ramique et le tube externe de métal. Cette couche mince d'isolation des contraintes est comprise entre 0,05 mm et 2 mm et de préférence entre 0,1 mm et 0,5 mm. Cette couche d'isolation des contraintes a vocation à absorber les vibrations du moteur et de la route pour éviter la destruction de la couche de fibres de céramique épaisse. Cette couche atténue aussi les vi- brations, notamment en compensant les expansions thermiques différentielles entre la couche de fibres de céramique épaisse et le tube externe de métal lors de réchauffement de la ligne d'échappement. En effet, lorsque le tube interne est parcouru par des gaz à hautes températures, on constate des expansions thermiques différentielles importantes car le tube interne de céramique dense ainsi que la couche épaisse de fibres céramiques ont des coefficients de dilatation relativement faibles en comparaison du tube externe en métal.In this document, it is proposed to provide between the dense inner ceramic tube and the outer metal tube, a relatively thick, thermally insulating layer of ceramic fibers in contact with the ceramic tube. The thick layer of ceramic fibers has a thickness of between 1 mm and 40 mm and preferably between 2 mm and 20 mm. In a particular embodiment, a so-called thin layer of stress isolation is provided between the thick layer of ceramic fiber and the outer tube of metal. This thin layer of stress isolation is between 0.05 mm and 2 mm and preferably between 0.1 mm and 0.5 mm. This layer of stress insulation is designed to absorb the vibrations of the engine and the road to prevent the destruction of the thick ceramic fiber layer. This layer also attenuates the vibrations, in particular by compensating the differential thermal expansions between the thick ceramic fiber layer and the outer metal tube during heating of the exhaust line. Indeed, when the inner tube is traversed by gases at high temperatures, there are significant differential thermal expansions because the dense inner ceramic tube and the thick layer of ceramic fibers have relatively low expansion coefficients in comparison with the outer tube made of metal.
Cette couche mince d'isolation des contraintes est nécessaire dans le dispositif décrit dans US 6,725,658 car la couche épaisse de fibres céramiques n'a pas les propriétés requises pour compenser le jeu dû à la dilatation différentielle entre le tube interne de céramique dense et le tube externe en métal.This thin layer of stress isolation is necessary in the device described in US 6,725,658 because the thick layer of ceramic fibers does not have the properties required to compensate for the backlash due to the differential expansion between the dense ceramic inner tube and the tube. external metal.
US 6,725,658 décrit donc une structure multicouche comprenant au minimum une couche interne céramique dense, une couche épaisse thermiquement isolante de fibres céramiques et une couche métallique. Cette structure est éventuellement complétée par une couche mince d'isolation des contraintes destinée à protéger la couche épaisse de fibres céramiques des vibrations.US 6,725,658 thus describes a multilayer structure comprising at least a dense ceramic inner layer, a thermally insulating thick layer of ceramic fibers and a metal layer. This structure is optionally supplemented by a thin layer of stress insulation for protecting the thick layer of ceramic fibers from vibrations.
Or, en plus des vibrations susceptibles d'endommager la couche épaisse de fibres céramiques, une structure du type de celle décrite dans US 6,725,658 est encore soumise, au niveau de la paroi interne du tube interne céramique dense, à des sollicitations dues au flux des gaz d'échappement. Ces sollicitations ont tendance à entraîner le tube interne avec le flux de gaz occasionnant un problème du maintien du tube interne céramique dans le tube externe en métal.However, in addition to the vibrations that are liable to damage the thick layer of ceramic fibers, a structure of the type described in US Pat. No. 6,725,658 is still subject, at the level of the inner wall of the dense ceramic inner tube, to stresses due to the flow of the ceramic fibers. exhaust gas. These stresses tend to cause the inner tube with the flow of gas causing a problem of maintaining the inner ceramic tube in the outer metal tube.
Or, l'enseignement de US 6,725,658 ne contient aucun élément susceptible de résoudre le problème du maintien de la couche interne céra- mique dense dans une structure métallique.However, the teaching of US Pat. No. 6,725,658 contains no element capable of solving the problem of maintaining the dense ceramic inner layer in a metal structure.
C'est pourquoi l'invention a pour objet un conduit d'échappement permettant un acheminement satisfaisant de la chaleur comprenant une conduite interne en composite à matrice inorganique maintenue dans une structure métallique externe. A cet effet, l'invention a pour objet un conduit d'échappement du type précité, caractérisé en ce que l'épaisseur de la couche de maintien est comprise entre 2 mm et 10 mm, et de préférence entre 3 mm et 6 mm, et en ce que la pression de maintien minimale exercée par la couche de maintien sur le tube interne est comprise entre 10"4 MPa et 10~1 MPa. Selon des modes particuliers de réalisation, le conduit ci-après comporte une ou plusieurs des caractéristiques suivantes :Therefore, an object of the invention is an exhaust duct for satisfactory heat delivery comprising an inorganic matrix composite inner pipe held in an outer metal structure. For this purpose, the subject of the invention is an exhaust duct of the aforementioned type, characterized in that the thickness of the holding layer is between 2 mm and 10 mm, and preferably between 3 mm and 6 mm, and in that the minimum holding pressure exerted by the retaining layer on the inner tube is between 10 -4 MPa and 10 -1 MPa. According to particular embodiments, the duct below comprises one or more of the characteristics following:
- la pression de maintien minimale exercée par la couche de maintien sur le tube interne est comprise entre 10'3 MPa et 5.10"2 MPa,the minimum holding pressure exerted by the retaining layer on the inner tube is between 10 3 MPa and 5 × 10 -2 MPa,
- le tube externe métallique a une épaisseur comprise entre 0,5 mm et 3 mm,the outer metal tube has a thickness of between 0.5 mm and 3 mm,
- le tube externe métallique est choisi dans le groupe consistant en un tube d'acier, un tube d'aluminium et un tube de titane,the outer metal tube is chosen from the group consisting of a steel tube, an aluminum tube and a titanium tube,
- le tube externe est formé de deux demi-coquilles en forme de gouttières assemblées par des joints longitudinaux, - le tube interne en composite à matrice inorganique a une épaisseur inférieure à 2 mm,the outer tube is formed of two half-shells in the form of gutters assembled by longitudinal joints, the inner tube of inorganic matrix composite has a thickness of less than 2 mm,
- le tube interne composite à matrice inorganique comprend une matrice constituée par au moins un polymère inorganique,the inorganic matrix composite internal tube comprises a matrix consisting of at least one inorganic polymer,
- le polymère inorganique est un géopolymère à base d'aluminosi- licate,the inorganic polymer is a geopolymer based on aluminosilicate,
- le tube interne composite à matrice inorganique comprend une matrice renforcée par des fibres, notamment à base de carbure de silicium (SiC), de carbone, de silice (SiO2), ou d'un fil métallique inoxydable résistant à des températures égales ou supérieures à 600°,the inorganic matrix composite internal tube comprises a matrix reinforced with fibers, in particular based on silicon carbide (SiC), carbon, silica (SiO2), or a stainless wire resistant to temperatures equal to or greater than 600 °,
- la couche de maintien comprend une nappe de fibres de céramique, - la couche de maintien comprend des fibres de céramique et un liant inorganique, la couche de maintien comprenant entre 90 % à 100 % en poids de fibres céramiques,the holding layer comprises a sheet of ceramic fibers, the holding layer comprises ceramic fibers and an inorganic binder, the holding layer comprising between 90% to 100% by weight of ceramic fibers,
- les fibres céramiques sont des fibres sélectionnées dans le groupe consistant en des fibres de silice, de fibres d'alumine, de fibres de zirconium, de fibres d'alumine-borosilicate, et de mélanges de celles-ci,the ceramic fibers are fibers selected from the group consisting of silica fibers, alumina fibers, zirconium fibers, alumina-borosilicate fibers, and mixtures thereof,
- les fibres contenues dans la couche de maintien sont un mélange de fibres d'alumine et de fibres de silice dans un rapport de respectivement 72 et 28 %,the fibers contained in the holding layer are a mixture of alumina fibers and silica fibers in a ratio of 72 and 28% respectively,
- la GBD du matériau constituant la couche de maintien est com- prise entre 0,1 et 0,6,the GBD of the material constituting the holding layer is between 0.1 and 0.6,
- la densité du matériau constituant la couche de maintien est comprise entre 500 g/m2 et 3000 g/m2,the density of the material constituting the holding layer is between 500 g / m 2 and 3000 g / m 2 ,
- le coefficient de frottement du matériau formant la couche de maintien contre les surfaces des tubes interne et externe est compris entre 0,15 et 0,7, etthe coefficient of friction of the material forming the holding layer against the surfaces of the inner and outer tubes is between 0.15 and 0.7, and
- le collecteur d'échappement comporte au moins un conduit d'échappement tel que défini ci-dessus.the exhaust manifold comprises at least one exhaust duct as defined above.
L'invention sera mieux comprise à la lecture de la description qui va suivre, donnée uniquement à titre d'exemple et faite en se réfèrent aux dessins sur lesquels :The invention will be better understood on reading the description which follows, given solely by way of example and with reference to the drawings in which:
- la figure 1 est une vue en perspective d'un collecteur d'échappement selon l'invention ; et- Figure 1 is a perspective view of an exhaust manifold according to the invention; and
- la figure 2 est une vue en section d'un conduit d'échappement du collecteur de la figure 1. Le collecteur d'échappement 10 illustré sur la figure 1 est destiné à être disposé en sortie d'un moteur thermique à l'entrée d'une ligne d'échappement d'un véhicule automobile. Cette ligne d'échappement comporte en aval du collecteur 10, éventuellement un système de suralimenta- tion (turbo) et un ou plusieurs éléments de dépollution propres à fonctionner à température élevée.FIG. 2 is a sectional view of an exhaust pipe of the manifold of FIG. 1. The exhaust manifold 10 illustrated in FIG. 1 is intended to be disposed at the outlet of a heat engine at the inlet. an exhaust system of a motor vehicle. This exhaust line comprises downstream of the collector 10, possibly a supercharging system tion (turbo) and one or more depollution elements capable of operating at high temperature.
Le collecteur 10 comporte plusieurs entrées 12 convergeant vers une bride de sortie 14. Les entrées 12 sont reliées à la bride de sortie 14 par des conduits 20 débouchant les uns dans les autres.The collector 10 has a plurality of inlets 12 converging towards an outlet flange 14. The inlets 12 are connected to the outlet flange 14 by ducts 20 opening into each other.
Comme illustré sur la figure 2, chaque conduit 20 comporte un tube interne 22 en composite à matrice inorganique, notamment céramique, et un tube externe en métal 24 entre lesquels est disposée une couche de maintien 26 constituée d'un matériau fibreux céramique . De préférence, le conduit est constitué seulement des trois couches 22, 24 et 26.As illustrated in Figure 2, each conduit 20 comprises an inner tube 22 of inorganic matrix composite, in particular ceramic, and an outer metal tube 24 between which is disposed a holding layer 26 made of a ceramic fibrous material. Preferably, the conduit consists of only three layers 22, 24 and 26.
Le tube externe 24 est formé d'une paroi métallique ayant une épaisseur comprise entre 0,5 et 3 mm. Suivant un premier mode de réalisation, le tube externe 24 est un tube cylindrique métallique notamment d'acier, d'aluminium ou de titane.The outer tube 24 is formed of a metal wall having a thickness of between 0.5 and 3 mm. According to a first embodiment, the outer tube 24 is a cylindrical metal tube including steel, aluminum or titanium.
En variante, et comme illustré sur la figure 1 , le tube externe 24 est formé de deux demi coquilles métalliques 27 en forme de gouttières assemblées par des joints longitudinaux opposés 28.In a variant, and as illustrated in FIG. 1, the outer tube 24 is formed of two metal half-shells 27 in the form of gutters joined by opposite longitudinal seals 28.
A chacune de ses extrémités, le tube externe 24 est pourvu de brides permettant sa liaison avec, en amont, le moteur et en aval, la ligne d'échappement du véhicule.At each of its ends, the outer tube 24 is provided with flanges allowing its connection with, upstream, the engine and downstream, the exhaust line of the vehicle.
Le choix d'un tube externe métallique se justifie par la nécessité d'assurer une étanchéité optimale en amont des éléments de dépollution, et notamment au niveau de la jonction du tube externe avec les brides métalli- ques amont et aval. A titre indicatif, le débit de fuite autorisé est de 25 litres/heure, à 200C sous 1 ,3 bars. Le tube interne 22 est un tube formé à partir d'un matériau composite à matrice inorganique notamment céramique. Des exemples de matériaux composites à matrice inorganique pouvant permettre la formation du tube interne 22 sont donnés dans les demandes de brevet US6134881 et WO2004106705. Ces matériaux sont formés par l'association d'une matrice constituée par au moins un polymère inorganique, préférentiellement de type géopolymère, à base d'aluminosilicate. Cette matrice est renforcée par des fibres, notamment à base de carbure de sili- cium (SiC) ou de carbone ou de silice (SiO2), voire d'un fil métallique inoxydable résistant à des températures égales ou supérieures à 6000C (inox, inconel® , ...)- De préférence, le tube interne 22 est formé d'une paroi ayant une épaisseur inférieure à 2 mm. La couche de maintien 26 présente une épaisseur comprise entreThe choice of an outer metal tube is justified by the need to ensure optimum sealing upstream of the pollution control elements, and in particular at the junction of the outer tube with the upstream and downstream metal flanges. As an indication, the authorized leakage flow rate is 25 liters / hour at 20 ° C. under 1.3 bar. The inner tube 22 is a tube formed from a composite material with an inorganic matrix, in particular a ceramic matrix. Examples of inorganic matrix composite materials that can allow the formation of the inner tube 22 are given in patent applications US6134881 and WO2004106705. These materials are formed by the combination of a matrix consisting of at least one inorganic polymer, preferably of geopolymer type, based on aluminosilicate. This matrix is reinforced by fibers, in particular based on silicon carbide cium (SiC) or carbon or silica (SiO2), or even a stainless wire resistant to temperatures equal to or greater than 600 0 C (stainless steel, inconel®, ...) - Preferably, the inner tube 22 is formed of a wall having a thickness of less than 2 mm. The holding layer 26 has a thickness of between
2 et 10 mm. Elle est de préférence comprise entre 3 et 6 mm.2 and 10 mm. It is preferably between 3 and 6 mm.
La couche de maintien 26 est formée d'une nappe de fibres céramiques, notamment de fibres de céramique longues associées préféra- blement à un liant organique et / ou inorganique. Le liant organique est utile uniquement lors de la mise en place de la couche de maintien autour du tube interne ; il se consume lors de la première montée en température du conduit d'échappement sur le véhicule. Ce liant représente de 0 à 15 % en masse de la couche de maintien neuve.The holding layer 26 is formed of a layer of ceramic fibers, in particular long ceramic fibers preferably associated with an organic and / or inorganic binder. The organic binder is only useful when placing the holding layer around the inner tube; it is consumed during the first temperature rise of the exhaust duct on the vehicle. This binder represents from 0 to 15% by weight of the new holding layer.
Le liant inorganique est utilisé lorsqu'il est nécessaire d'assurer une meilleure cohésion entre les fibres lors du fonctionnement du véhicule et ne doit donc pas se consumer. Ce liant représente de 0 à 10 % en masse de la couche de maintien hors liant organique.The inorganic binder is used when it is necessary to ensure better cohesion between the fibers during operation of the vehicle and must not be burned. This binder represents from 0 to 10% by weight of the organic binder-free holding layer.
Ainsi, en configuration de fonctionnement, les fibres céramiques représentent 90 à 100 % en poids de la couche de maintien, le reste éven- tuel étant le liant inorganique.Thus, in the operating configuration, the ceramic fibers represent 90 to 100% by weight of the holding layer, the remainder being the inorganic binder.
Les fibres de céramique présentes dans la couche de maintien 26 sont sélectionnées dans le groupe consistant en des fibres de silice, des fibres d'alumine, des fibres de zirconium, des fibres d'alumine borosilicate et un mélange de celles-ci. Les nappes peuvent être aiguilletées, ce qui permet d'améliorer leur tenue dans le temps.The ceramic fibers present in the holding layer 26 are selected from the group consisting of silica fibers, alumina fibers, zirconium fibers, borosilicate alumina fibers and a mixture thereof. The sheets may be needled, which improves their behavior over time.
De préférence, les fibres utilisées sont des fibres de mullite associant alumine et silice dans un rapport respectivement de 72 % et 28 %.Preferably, the fibers used are mullite fibers combining alumina and silica in a ratio of 72% and 28%, respectively.
La densité du matériau constituant la couche de maintien est comprise entre 500 g/m2 et 3000 g/m2. Cette couche de maintien 26 doit assurer le maintien du tube interne 22 dans le tube externe 24 quelles que soient les conditions de fonctionnement. En fonction des caractéristiques du tube interne en céramique et de la nature de la couche de maintien (masse, surface de contact avec la couche de maintien), de l'accélération maximale à laquelle il est soumise et du flux et de la pression maximaux des gaz d'échappement, la pression mi- nimale à appliquer pour maintenir ledit tube interne dans le tube métallique est déterminée. Cette pression minimale prend en compte, en plus des sollicitations mentionnées ci dessus, un facteur correctif spécifique du comportement en fonctionnement du tube interne céramique et de la couche de maintien. Un coefficient de frottement intervient dans ce facteur correctif. En fonction du matériau constituant les tubes interne et externe, le matériau constituant la couche de maintien est choisi de sorte que le coefficient de frottement de la couche amortisseur contre les surfaces des tubes interne et externe est compris entre 0,15 et 0,7. La pression minimale de maintien est comprise entre 10"4 et 10"1 MPa et de préférence entre 10"3 MPa et 5.10"2 MPa.The density of the material constituting the holding layer is between 500 g / m 2 and 3000 g / m 2 . This holding layer 26 must maintain the inner tube 22 in the outer tube 24 regardless of the operating conditions. Depending on the characteristics of the inner ceramic tube and the nature of the holding layer (mass, contact surface with the holding layer), the maximum acceleration to which it is subjected and the maximum flow and pressure of the exhaust gas, the minimum pressure to be applied to maintain said inner tube in the metal tube is determined. This minimum pressure takes into account, in addition to the above mentioned solicitations, a specific corrective factor of the operating behavior of the inner ceramic tube and the holding layer. A coefficient of friction intervenes in this corrective factor. Depending on the material constituting the inner and outer tubes, the material constituting the holding layer is chosen so that the coefficient of friction of the damping layer against the surfaces of the inner and outer tubes is between 0.15 and 0.7. The minimum holding pressure is between 10 "4 and 10" 1 MPa and preferably between 10 "3 MPa and 5.10" 2 MPa.
La valeur de 10"3 MPa correspond à un tube interne de 100 grammes ayant une surface de contact de 40 dm2 avec la couche de maintien soumis à une accélération de 10g et une perte de charge de 100Pa. Cette perte de charge est induite par le frottement des gaz contre la paroi du tube interne. La valeur de 5.10"2 MPa correspond à un tube interne de 200 grammes ayant une surface de contact de 20 dm2 avec la couche de maintien et soumis à une accélération de 40g et une perte de charge de 250Pa.The value of 10 "3 MPa corresponds to an inner tube of 100 grams having a contact area of 40 dm 2 with the holding layer subjected to an acceleration of 10 g and a pressure drop of 100 Pa. This pressure drop is induced by the friction of the gases against the wall of the inner tube The value of 5.10 "2 MPa corresponds to an inner tube of 200 grams having a contact surface of 20 dm 2 with the holding layer and subjected to an acceleration of 40 g and a loss charge of 250Pa.
On a constaté que, en fonction du type de nappe choisi pour constituer la couche de maintien 26, il est nécessaire, d'une part d'empêcher la destruction des fibres constituant la nappe et d'autre part d'éviter d'endommager le tube interne en composite à matrice inorganique. Pour cela, il est primordial de ne pas dépasser une certaine pression exercée sur le tube interne et donc une certaine compression de la nappe: cette pression maximale est comprise entre 0,1 et 1 MPa et de préférence entre 0,3 et 0,7 MPa. La GBD (Gap BuIk Density) est le rapport entre la densité en kilogrammes par mètre carré de la nappe choisie pour constituer la couche de maintien et le jeu en millimètres entre les tubes externe et interne. La densité est une caractéristique propre à la nappe. Dans le cadre de l'invention, la valeur du jeu entre les tubes externe et interne est dictée notamment par les contraintes de forme de l'élément de ligne d'échappement. La plage de GBD utilisable est comprise entre 0,1 et 0,6 . Lia valeur minimale est donnée pour éviter la détérioration des fibres par les vibrations, la valeur maximale est donnée pour éviter la détérioration des fibres par la compression.It has been found that, depending on the type of sheet chosen to constitute the holding layer 26, it is necessary, on the one hand, to prevent the destruction of the fibers constituting the sheet and, on the other hand, to avoid damaging the sheet. inner tube of inorganic matrix composite. For this, it is essential not to exceed a certain pressure exerted on the inner tube and therefore a certain compression of the web: this maximum pressure is between 0.1 and 1 MPa and preferably between 0.3 and 0.7. MPa. GBD (Gap BuIk Density) is the ratio between the density in kilograms per square meter of the chosen layer to form the support layer and the clearance in millimeters between the outer and inner tubes. Density is a characteristic of the tablecloth. In the context of the invention, the value of the clearance between the outer and inner tubes is dictated in particular by the shape constraints of the exhaust line element. The usable GBD range is 0.1 to 0.6. The minimum value is given to avoid vibrational deterioration of the fibers, the maximum value is given to avoid deterioration of the fibers by compression.
La relation entre la GBD et la pression P exercée sur le tube interne par la couche de maintien est donnée, pour une nappe constituée de fibres céramique longues, par une équation du type P = A . (GBD)3 + B . (GBD)2 + C (GBD) + D. Lors du choix d'une nappe de densité donnée destinée à assurer le maintien du tube interne séparé du tube externe par un jeu donné, on s'assure que la pression exercée sera supérieure à la pression minimale de maintien et inférieure à la pression maximale supportée par les fibres et le tube interne. Il faut encore pour cela tenir compte du fait que, en cours d'uti- lisation, le jeu entre le tube interne et le tube externe peut varier de plus ou moins 1 mm en raison de la dilatation différentielle entre le tube interne et le tube externe.The relationship between the GBD and the pressure P exerted on the inner tube by the holding layer is given, for a sheet made of long ceramic fibers, by an equation of the P = A type. (GBD) 3 + B. (GBD) 2 + C (GBD) + D. When choosing a sheet of specific density intended to maintain the inner tube separated from the outer tube by a given clearance, it is ensured that the pressure exerted will be greater than the minimum holding pressure and less than the maximum pressure supported by the fibers and the inner tube. It is necessary to take into account that, during use, the clearance between the inner tube and the outer tube may vary by plus or minus 1 mm due to the differential expansion between the inner tube and the tube. external.
Ainsi, pour une couche de maintien 26 formée à partir d'une nappe constituées de fibres céramiques longues de densité de 900 g/m2, mise en place entre un tube interne (conduite composite de 200 grammes ayant une surface de contact de 20 dm2 avec la nappe de maintien et soumise à une accélération de 40g) et un tube externe séparés par un jeu minimum de 3 mm, la GBD est de 0,3. La pression de maintien exercée par la nappe sur le tube interne en composite à matrice céramique est alors, pour le type de nappe choisi, de 0,2 MPa. Cette GBD de 0,3 est bien située dans la plage de GBD conseillée. Cette pression est supérieure à la pression minimale de maintien calculée pour cette application (5.10"2 MPa) et inférieure à la tenue mécanique du tube interne.Thus, for a holding layer 26 formed from a sheet made of long ceramic fibers with a density of 900 g / m 2 , placed between an inner tube (composite pipe of 200 grams having a contact area of 20 dm 2 with the holding ply and subjected to an acceleration of 40g) and an outer tube separated by a minimum play of 3 mm, the GBD is 0.3. The holding pressure exerted by the ply on the internal ceramic matrix composite tube is then, for the chosen type of ply, 0.2 MPa. This GBD of 0.3 is well within the recommended GBD range. This pressure is greater than the minimum holding pressure calculated for this application (5.10 "2 MPa) and lower than the mechanical strength of the inner tube.
Le jeu maximum pour cette même application est de 4,25 mm, correspondant à une GBD de 0,22 et une pression de maintien de 6.10"2 MPa. La GBD reste dans la plage d'utilisation de la nappe et la pression induite reste supérieure à la pression minimale de maintien. On constate qu'avec un tel conduit d'échappement, le matériau de maintien assure correctement la maintien du tube interne en composite à matrice inorganique dans le tube externe en métal quelle que soit la température de la ligne d'échappement et les conditions de flux gazeux et d'accélération auxquelles est soumis le tube interne sans se détériorer ni endommager le tube interne. The maximum clearance for this same application is 4.25 mm, corresponding to a GBD of 0.22 and a holding pressure of 6.10 "2 MPa.The GBD remains in the range of use of the web and the induced pressure remains greater than the minimum holding pressure. It is noted that with such an exhaust duct, the holding material correctly ensures the maintenance of the inner tube of inorganic matrix composite in the outer metal tube regardless of the temperature of the exhaust line and the flow conditions. gaseous and acceleration to which the inner tube is subjected without deteriorating or damaging the inner tube.

Claims

REVENDICATIONS
1.- Conduit d'échappement (20) comportant, disposés de manière concentrique :1.- Exhaust duct (20) comprising, arranged in a concentric manner:
- un tube interne en composite à matrice inorganique (22) ; - un tube externe métallique (24) ;an inorganic matrix composite internal tube (22); an outer metal tube (24);
- une couche de maintien (26) d'un matériau fibreux , caractérisé en ce que l'épaisseur de la couche de maintien (26) est comprise entre 2 mm et 10 mm, et de préférence entre 3 mm et 6 mm, et en ce que la pression de maintien minimale exercée par la couche de maintien (26) sur le tube interne (22) est comprise entre 10'4 MPa et 10~1 MPa.a holding layer (26) of a fibrous material, characterized in that the thickness of the holding layer (26) is between 2 mm and 10 mm, and preferably between 3 mm and 6 mm, and that the minimum holding pressure exerted by the holding layer (26) on the inner tube (22) is between 10 '4 MPa and 10 ~ 1 MPa.
2.- Conduit selon la revendication 1, caractérisé en ce que la pression de maintien minimale exercée par la couche de maintien (26) sur le tube interne (22) est comprise entre 10"3 MPa et 5.10"2 MPa.2. A conduit according to claim 1, characterized in that the minimum holding pressure exerted by the holding layer (26) on the inner tube (22) is between 10 "3 MPa and 5.10 " 2 MPa.
3.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube externe métallique (24) a une épaisseur comprise entre 0,5 mm et 3 mm.3. Conduit according to any one of the preceding claims, characterized in that the outer metal tube (24) has a thickness of between 0.5 mm and 3 mm.
4.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube externe métallique (24) est choisi dans le groupe consistant en un tube d'acier, un tube d'aluminium et un tube de ti- tane.4. A conduit according to any one of the preceding claims, characterized in that the metal outer tube (24) is selected from the group consisting of a steel tube, an aluminum tube and a titanium tube.
5.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube externe (24) est formé de deux demi-coquilles (27) en forme de gouttières assemblées par des joints longitudinaux (28).5. A conduit according to any one of the preceding claims, characterized in that the outer tube (24) is formed of two half-shells (27) shaped gutters assembled by longitudinal joints (28).
6.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube interne en composite à matrice inorganique (22) a une épaisseur inférieure à 2 mm.6. A conduit according to any one of the preceding claims, characterized in that the inner tube of inorganic matrix composite (22) has a thickness of less than 2 mm.
7.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube interne composite à matrice inorganique (22) comprend une matrice constituée par au moins un polymère inorganique. 7. A conduit according to any one of the preceding claims, characterized in that the inorganic matrix composite inner tube (22) comprises a matrix consisting of at least one inorganic polymer.
8.- Conduit selon la revendication 7, caractérisé en ce que le polymère inorganique est un géopolymère à base d'aluminosilicate.8. Conduit according to claim 7, characterized in that the inorganic polymer is a geopolymer based on aluminosilicate.
9.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le tube interne composite à matrice inorganique (22) comprend une matrice renforcée par des fibres, notamment à base de carbure de silicium (SiC), de carbone, de silice (SiO2), ou d'un fil métallique inoxydable résistant à des températures égales ou supérieures à 600°.9. Conduit according to any one of the preceding claims, characterized in that the inner tube composite inorganic matrix (22) comprises a matrix reinforced with fibers, especially based on silicon carbide (SiC), carbon, silica (SiO2), or a stainless wire resistant to temperatures of 600 ° or more.
10.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que la couche de maintien (26) comprend une nappe de fibres de céramique.10. A conduit according to any one of the preceding claims, characterized in that the holding layer (26) comprises a sheet of ceramic fibers.
11.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que la couche de maintien (26) comprend des fibres de céramique et un liant inorganique, la couche de maintien comprenant entre 90 % à 100 % en poids de fibres céramiques.11. A conduit according to any one of the preceding claims, characterized in that the holding layer (26) comprises ceramic fibers and an inorganic binder, the holding layer comprising between 90% to 100% by weight of ceramic fibers. .
12.- Conduit selon la revendication 11 , caractérisé en ce que les fibres céramiques sont des fibres sélectionnées dans le groupe consistant en des fibres de silice, de fibres d'alumine, de fibres de zirconium, de fibres d'alumine-borosilicate, et de mélanges de celles-ci. 12. Conduit according to claim 11, characterized in that the ceramic fibers are fibers selected from the group consisting of silica fibers, alumina fibers, zirconium fibers, alumina-borosilicate fibers, and mixtures thereof.
13. Conduit selon la revendication 12, caractérisé en ce que les fibres contenues dans la couche de maintien (26) sont un mélange de fibres d'alumine et de fibres de silice dans un rapport de respectivement 72 et 28 %.13. Conduit according to claim 12, characterized in that the fibers contained in the holding layer (26) are a mixture of alumina fibers and silica fibers in a ratio of respectively 72 and 28%.
14.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que la GBD du matériau constituant la couche de maintien (26) est comprise entre 0,1 et 0,6.14. A conduit according to any one of the preceding claims, characterized in that the GBD of the material constituting the holding layer (26) is between 0.1 and 0.6.
15.- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que la densité du matériau constituant la couche de maintien (26) est comprise entre 500 g/m2 et 3000 g/m2. 15. A conduit according to any one of the preceding claims, characterized in that the density of the material constituting the holding layer (26) is between 500 g / m 2 and 3000 g / m 2 .
16- Conduit selon l'une quelconque des revendications précédentes, caractérisé en ce que le coefficient de frottement du matériau formant la couche de maintien (26) contre les surfaces des tubes interne (22) et externe (24) est compris entre 0,15 et 0,7.16- conduit according to any one of the preceding claims, characterized in that the coefficient of friction of the material forming the holding layer (26) against the surfaces of the inner tube (22) and outer (24) is between 0.15 and 0.7.
17.- Collecteur d'échappement (10) comportant au moins un conduit d'échappement (20) selon l'une quelconque des revendications précédentes. 17.- Exhaust manifold (10) having at least one exhaust duct (20) according to any one of the preceding claims.
EP06808051A 2005-08-09 2006-08-03 Exhaust pipe Not-in-force EP1915519B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0508466A FR2889721B1 (en) 2005-08-09 2005-08-09 EXHAUST CONDUIT
PCT/FR2006/001896 WO2007017583A1 (en) 2005-08-09 2006-08-03 Exhaust pipe

Publications (2)

Publication Number Publication Date
EP1915519A1 true EP1915519A1 (en) 2008-04-30
EP1915519B1 EP1915519B1 (en) 2009-02-25

Family

ID=35998559

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06808051A Not-in-force EP1915519B1 (en) 2005-08-09 2006-08-03 Exhaust pipe

Country Status (8)

Country Link
US (1) US20090183502A1 (en)
EP (1) EP1915519B1 (en)
JP (1) JP2009504968A (en)
KR (1) KR20080080980A (en)
AT (1) ATE423896T1 (en)
DE (1) DE602006005375D1 (en)
FR (1) FR2889721B1 (en)
WO (1) WO2007017583A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9790836B2 (en) 2012-11-20 2017-10-17 Tenneco Automotive Operating Company, Inc. Loose-fill insulation exhaust gas treatment device and methods of manufacturing

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2916227B1 (en) * 2007-05-18 2009-08-21 Faurecia Sys Echappement EXHAUST PIPE OF A MOTOR VEHICLE
CN101922590A (en) * 2010-02-09 2010-12-22 徐州胜海机械制造科技有限公司 Wear-resisting heat-resisting corrosion-resisting compound pipe and production method thereof
US10508583B2 (en) 2012-08-30 2019-12-17 Bosal Emission Control Systems Nv Composite exhaust element
DE102014112053A1 (en) * 2014-08-22 2016-02-25 Krones Ag Pipeline for hot gases and process for their production
US11339704B2 (en) * 2016-11-18 2022-05-24 Novo Plastics Inc. Exhaust subsystem with fiber pipe and method of forming fiber pipe
CN107387219A (en) * 2017-07-19 2017-11-24 冠立科技扬州有限公司 A kind of motorcycle exhaust blast pipe
DK3887705T3 (en) * 2018-11-27 2024-04-22 Saint Gobain Performance Plastics Corp FLUID MANIFOLD PIPE
IT202000018757A1 (en) * 2020-07-31 2022-01-31 Aeronautical Service S R L MULTILAYER TUBULAR CONDUIT AND PRODUCTION METHOD.

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001259438A (en) * 2000-03-22 2001-09-25 Ibiden Co Ltd Catalytic converter
JPS5728837B2 (en) * 1973-10-09 1982-06-18
JPS60187712A (en) * 1984-03-08 1985-09-25 Nissan Motor Co Ltd Exhaust manifold for internal-combustion engine
JPH0255823A (en) * 1988-08-17 1990-02-26 Nippon Steel Corp Exhaust manifold
US5163289A (en) * 1991-10-08 1992-11-17 Manville Corporation Automotive exhaust system
US5419127A (en) * 1993-11-22 1995-05-30 Soundwich Inc Insulated damped exhaust manifold
US5842342A (en) * 1997-02-21 1998-12-01 Northrop Grumman Corporation Fiber reinforced ceramic matrix composite internal combustion engine intake/exhaust port liners
US6349542B1 (en) * 1998-08-17 2002-02-26 Soundwich, Inc. Silicon carbide (SiC) composite exhaust manifold and method of making it
EP0992659B1 (en) * 1998-10-05 2007-05-02 Scambia Industrial Developments Aktiengesellschaft Exhaust pipe element and method for producing an exhaust pipe element
US7399718B2 (en) * 2001-02-26 2008-07-15 Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung E.V. Water-repellent and vapor-permeable multilayer material for outdoor applications
US6725656B2 (en) * 2001-12-07 2004-04-27 Dan T. Moore Company Insulated exhaust manifold
US20040177609A1 (en) * 2001-12-07 2004-09-16 Moore Dan T. Insulated exhaust manifold having ceramic inner layer that is highly resistant to thermal cycling
WO2005091902A2 (en) * 2004-03-03 2005-10-06 Intellectual Property Holdings, Llc Highly insulated exhaust manifold

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2007017583A1 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9790836B2 (en) 2012-11-20 2017-10-17 Tenneco Automotive Operating Company, Inc. Loose-fill insulation exhaust gas treatment device and methods of manufacturing

Also Published As

Publication number Publication date
KR20080080980A (en) 2008-09-05
JP2009504968A (en) 2009-02-05
ATE423896T1 (en) 2009-03-15
FR2889721B1 (en) 2007-11-02
EP1915519B1 (en) 2009-02-25
FR2889721A1 (en) 2007-02-16
WO2007017583A1 (en) 2007-02-15
DE602006005375D1 (en) 2009-04-09
US20090183502A1 (en) 2009-07-23

Similar Documents

Publication Publication Date Title
EP1915519B1 (en) Exhaust pipe
CA2979474C (en) Turbine ring assembly comprising a plurality of ring sectors made from ceramic matrix composite material
EP2129878B1 (en) Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained
EP1780398B1 (en) Intake silencer for a turbo compressed engine
EP2107307A1 (en) Gas turbine combustor with sectorised internal and external walls
WO2008148999A2 (en) Exhaust system for gas turbine
WO2006117468A1 (en) Double-shell manifold
FR2835018A1 (en) IMPROVEMENT TO A DECOUPLING HOSE FOR AN EXHAUST LINE OF A MOTOR VEHICLE ENGINE
WO2008142350A1 (en) Motor vehicle exhaust pipe
FR2549529A1 (en) Vehicle IC engine exhaust manifold
FR2924467A1 (en) Internal combustion engine's exhaust unit, has internal exhaust duct and inner casing connected together as outer envelopes to define intermediate insulation volume between duct and casing and between envelopes
EP2096348B1 (en) Exhaust duct, manufacturing method of this duct and vehicle equipped with this duct
FR2860266A1 (en) EXHAUST PIPE AND MOTOR PROPELLER GROUP COMPRISING IT
FR2924753A1 (en) METHOD FOR MANUFACTURING A MOTOR VEHICLE EXHAUST LINE ELEMENT AND CORRESPONDING EXHAUST ELEMENT
FR2877694A1 (en) EXHAUST PIPE AND METHOD FOR MANUFACTURING EXHAUST PIPE
FR2886338A1 (en) I.c. engine double-walled exhaust manifold has inner liner separated from outer wall in flange zones by insulating plugs
EP2959124B1 (en) Device for treating exhaust gases by catalysis
EP1797296A1 (en) Exhaust conduit
FR2917779A1 (en) Physical and chemical depollution element for e.g. hybrid motor vehicle, has heat insulation unit interposed between depollution unit and casing and designed for providing only thermal insulation of element
FR3129678A1 (en) PART FOR A TURBOMACHINE COMPRISING A THERMAL BARRIER COATING IN GEOPOLYMER
FR2870289A1 (en) Exhaust manifold for e.g. four-cylinder internal combustion engine, has partition in form of austenitic steel plate having better resistance at high temperatures and/or expansion coefficient lower than that of material of manifold body
FR2946086A1 (en) Exhaust manifold for supercharged combustion engine, has two parts connected to groups of cylinders of engine, respectively and forming single outlet, where first part is made of cast iron and second part is made of steel
WO2006117454A1 (en) Exhaust manifold
FR3027959A1 (en) FIRE PROTECTION OF A COMPOSITE MATERIAL PART OF A GAS TURBINE
FR2893353A1 (en) Exhaust manifold for an internal combustion engine produced using a flexible intermediary layer acting as the core for casting the external envelope and for compensating for distortions during use of the manifold

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20080205

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REF Corresponds to:

Ref document number: 602006005375

Country of ref document: DE

Date of ref document: 20090409

Kind code of ref document: P

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090525

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090625

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090812

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090605

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090525

26N No opposition filed

Effective date: 20091126

BERE Be: lapsed

Owner name: FAURECIA SYSTEMES D'ECHAPPEMENT

Effective date: 20090831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090526

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20100803

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090803

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100831

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090826

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100803

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090225

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CZ

Payment date: 20110727

Year of fee payment: 6

Ref country code: DE

Payment date: 20110830

Year of fee payment: 6

Ref country code: FR

Payment date: 20110830

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120803

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20130430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130301

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120831

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602006005375

Country of ref document: DE

Effective date: 20130301