EP1801378B1 - Process for the manufacture of a precisely shaped honeycomb body - Google Patents
Process for the manufacture of a precisely shaped honeycomb body Download PDFInfo
- Publication number
- EP1801378B1 EP1801378B1 EP06025092A EP06025092A EP1801378B1 EP 1801378 B1 EP1801378 B1 EP 1801378B1 EP 06025092 A EP06025092 A EP 06025092A EP 06025092 A EP06025092 A EP 06025092A EP 1801378 B1 EP1801378 B1 EP 1801378B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- housing
- formed part
- honeycomb body
- honeycomb
- honeycomb structure
- 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.)
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- 238000000034 method Methods 0.000 title claims description 22
- 238000004519 manufacturing process Methods 0.000 title claims description 14
- 239000002184 metal Substances 0.000 claims description 12
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 239000011248 coating agent Substances 0.000 claims description 10
- 238000000576 coating method Methods 0.000 claims description 10
- 238000005219 brazing Methods 0.000 claims description 3
- 238000005260 corrosion Methods 0.000 claims description 2
- 230000007797 corrosion Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims 1
- 241000264877 Hippospongia communis Species 0.000 description 73
- 238000000465 moulding Methods 0.000 description 9
- 239000011888 foil Substances 0.000 description 7
- 239000007789 gas Substances 0.000 description 7
- 238000007669 thermal treatment Methods 0.000 description 5
- 238000011282 treatment Methods 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 239000010970 precious metal Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2807—Metal other than sintered metal
- F01N3/281—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2330/00—Structure of catalyst support or particle filter
- F01N2330/30—Honeycomb supports characterised by their structural details
- F01N2330/44—Honeycomb supports characterised by their structural details made of stacks of sheets, plates or foils that are folded in S-form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2450/00—Methods or apparatus for fitting, inserting or repairing different elements
- F01N2450/02—Fitting monolithic blocks into the housing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2450/00—Methods or apparatus for fitting, inserting or repairing different elements
- F01N2450/22—Methods or apparatus for fitting, inserting or repairing different elements by welding or brazing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/10—Tubes having non-circular cross section
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49345—Catalytic device making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49748—Repairing by shaping, e.g., bending, extruding, turning, etc.
- Y10T29/4975—Repairing by shaping, e.g., bending, extruding, turning, etc. including heating
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49885—Assembling or joining with coating before or during assembling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49908—Joining by deforming
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49908—Joining by deforming
- Y10T29/49925—Inward deformation of aperture or hollow body wall
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49908—Joining by deforming
- Y10T29/49925—Inward deformation of aperture or hollow body wall
- Y10T29/49934—Inward deformation of aperture or hollow body wall by axially applying force
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49945—Assembling or joining by driven force fit
Definitions
- the present invention relates to a method for producing a honeycomb body comprising a honeycomb structure arranged in a housing.
- honeycomb bodies are used in particular for the aftertreatment of exhaust gases.
- honeycomb bodies regularly comprise a metallic housing by arranging a ceramic or metallic honeycomb structure. Part of the manufacturing process is to introduce the honeycomb structure in a suitable manner in the housing and ultimately form a joining connection between the housing and honeycomb structure.
- the contact of the honeycomb structure with the housing is as uniform as possible.
- the honeycomb body is produced with a desired roundness or shape accuracy.
- This is of particular interest, since ultimately an integration of the honeycomb body, for example, in the exhaust system of a mobile internal combustion engine as in a vehicle to be made.
- the housing often offers contact surface for further positive or non-positive connections.
- An inaccuracy in terms of the outer shape means that under certain circumstances sealing compounds for subsequent adjustment of shape tolerances, elaborate reworking steps or other, time-consuming and expensive measures are required.
- the WO-A1-98 / 15354 describes a method for producing metallic honeycomb bodies, wherein structured sheet metal strips are folded and placed in a housing before they are joined together. With the method described there, in particular the durability of honeycomb bodies with folded sheet metal strips is to be improved.
- the EP - A2 - 0 897 749 discloses a method for producing a metallic honeycomb body in which stacks of structured and smooth plates are wound and introduced into a jacket tube. In this case, the stack is pressed with a punch in the jacket tube, so that the diameter of the coiled stack is reduced. This should be accompanied by an improved conditioning of the plates on the jacket tube.
- honeycomb bodies which, for example, have a metallic honeycomb structure which is to be introduced in a non-cylindrical cross section of the housing.
- honeycomb bodies which, for example, have a metallic honeycomb structure which is to be introduced in a non-cylindrical cross section of the housing.
- This can already lead to a small deformation, especially with thin-walled housings.
- this effect is enhanced during later thermal treatments of the honeycomb body. This can lead to a further deformation of the housing and / or to a non-uniform connection of the honeycomb body to the housing.
- the object of the present invention is to at least partially solve the problems described with reference to the prior art.
- a method for producing a dimensionally accurate honeycomb body is to be specified.
- step a) preferably comprises the formation of a metallic honeycomb structure.
- a metallic honeycomb structure For this purpose, at least partially structured metal foils are layered and then wound together. In this case, a spiral, an S-shaped or a similar structure of the honeycomb structure can be achieved.
- the honeycomb structure regularly comprises a multiplicity of channels arranged essentially parallel to one another, through which an exhaust gas can flow.
- the honeycomb structure is prepared separately from the housing and now inserted by means of step b) in a housing.
- the honeycomb structure is preferably inserted into a housing (in particular in the circumferential direction).
- a housing in particular in the circumferential direction.
- Step c) relates in particular to a coating and / or a bonding process.
- the bonding method those in which sintered, brazed and / or welded joints are formed within the honeycomb structure or between the honeycomb structure and the housing are preferred.
- the molding in particular has the task of substantially maintaining a desired shape of the housing during the manufacturing process.
- the molding is usually made more stable than the housing and partially applied in the circumferential direction of the housing.
- the contact surfaces are arranged in particular where an increased stress of the housing due to the introduced honeycomb structure is to be expected. This concerns in particular the areas which have a smaller distance to the center of the honeycomb body and / or in areas of curvature sections of the housing with a large radius of curvature.
- non-circular is meant in particular oval, “race-track” -like, angular or other non-round cross-sections. These regularly have different radii of curvature, some of which can go to infinity (straight housing section). It is precisely here that the different stress states described above can occur during the thermal treatment of the honeycomb body, so that, in particular, such honeycomb bodies can be produced in a dimensionally accurate manner with the method described here.
- the honeycomb body powdered hard solder is preferably supplied via an end face of the honeycomb body.
- the honeycomb body is previously immersed in the front side of an adhesive liquid to which the brazing material should later adhere defined.
- the z. B. doped with precious metals and then calcined.
- this fixation of the honeycomb body by means of the molding z. B. is maintained between the individual processing stations or for temporary storage.
- a molded part for carrying out a method of the type described above in accordance with the invention is also proposed, a frame having a plurality of inwardly directed abutment surfaces being provided for a desired outer contour of the housing.
- the frame is preferably closed in the circumferential direction, for example in the manner of a frame.
- the frame is stirred in one piece.
- the inner contour of the frame accordingly has a plurality of inwardly directed contact surfaces, that is to say that the contact surfaces comprise the part of the inner contour of the frame that projects furthest inward.
- the contact surfaces are aligned with one another or designed such that they essentially correspond to the desired outer contour of the housing. In other words, this means that the contact surfaces form part of the outer contour of the housing.
- it is possible that a part of the contact surfaces are also beveled, so that, for example, a simplified insertion of the housing is made possible in the frame.
- the molded part is designed so that the relative position of the contact surfaces is adjustable to each other. This allows a particularly flexible use of the molding for different contours of the housing. In addition, there is the advantage that with such movable contact surfaces easier removal of the housing or the honeycomb body, for example, after performing a thermal treatment is possible.
- radially outwardly directed recesses space the inwardly directed abutment surfaces.
- the recesses preferably extend substantially parallel to the contact surfaces and limit these at least partially.
- the contact surfaces of the molded part cover between 50% and 80% of the circumference of the housing. This ensures on the one hand a sufficient fixation of the housing to achieve a dimensional stability and on the other hand allows a safe removal of the housing also as part of a series production.
- the recesses may be designed, for example, suitable for gripping tools.
- the molded part is made of a high-temperature-resistant and corrosion-resistant metal.
- the molding is very particularly preferably made from an at least similar material as the housing in order to ensure a uniform thermal expansion behavior, in particular during a thermal treatment of the honeycomb body.
- the metal should be able to withstand the thermal conditions during a brazing process.
- the contact surfaces are at least partially executed with a coating.
- the contact surfaces can also be provided at least partially with a structured surface.
- These measures are used, for example, to avoid connections between the molded part and the housing, as they may possibly take place at high temperatures (for example, sintered connections).
- the contact surface between the molded part and the housing is further reduced by the structured surface of the contact surface, whereby the Entfemle of the housing is improved according to the manufacturing process of the honeycomb body.
- these measures may be only partially provided in the contact surfaces, the application for all contact surfaces in the same way is preferred.
- an exhaust gas treatment unit comprising a honeycomb body with a housing having a thickness of at most 1.5 mm is preferably realized according to the method described according to the invention.
- Fig. 1 schematically shows in a front view of a honeycomb body 2, which has an inner honeycomb structure 3 and an outer housing 1.
- the housing 1 has a non-circular cross-section 12, in which the honeycomb structure 3 is arranged.
- the cross section 12 is substantially oval, almost in the nature of a so-called "race track”, having a first extent 13 and a second extent 14 different from each other.
- the illustration shows that the honeycomb body 2 is designed at the top and bottom with a larger radius of curvature than left and right.
- the honeycomb structure 3 is constructed with a plurality of structured and smooth metal foils 18 that are wound in an S-shape and that form essentially parallel channels 15.
- different voltages act on the housing 1, which could possibly influence the outer contour 6 of the housing 1.
- the use of a molding is proposed, which in a preferred embodiment for such a honeycomb body in Fig. 2 is shown.
- the molding 4 for the in Fig. 1 illustrated honeycomb body 2 is according to a preferred embodiment in Fig. 2 shown.
- the molded part 4 has a plurality of inwardly directed abutment surfaces 5, which rest against the outer contour of the housing 1, which is schematically illustrated. It is also illustrated that the contact surfaces 5 cover more than half of the circumference 9 of the housing 1. Between the contact surfaces 5, designed in the manner of a frame frame 7 radially outwardly directed recesses 8. In these areas, there is no system between the frame 7 and the housing. 1
- Fig. 3 shows a detail of an arrangement of a honeycomb body 2 in the interior of a molded part 4 according to a further embodiment in cross section.
- a part of honeycomb body 2 is illustrated, which in turn is formed with a plurality of metal foils 18, so that substantially parallel channels 15 are provided.
- the metal foils 18 bear against the housing 1 on the inside, the housing 1 having a thickness 16, for example in the range of up to 1.5 mm, advantageously even less than 1 mm or even 0.8 mm.
- the molded part 4 abuts, wherein the abutment surface 5 is designed here with a coating 17 and a structured surface 10.
- the provision of the structured surface 10 ensures easy removal of the honeycomb body 2 from the molded part 4, while the coating 17 prevents the formation of sintered connections between the molded part 4 and the housing 1.
- honeycomb bodies The preferred field of use for such honeycomb bodies is the automotive sector. Accordingly, the structure of an exhaust system 21 for a vehicle 19 is schematically shown in FIG Fig. 4 illustrated.
- the exhaust gas generated by the engine 20 is now passed through a plurality of exhaust treatment units 11 until it has been freed of pollutants so far that they are discharged to the environment can.
- the exhaust gas treatment unit 11 is in particular equipped with the honeycomb body described here. With the invention, in particular exhaust gas treatment units with a thin housing can be accurately produced.
Description
Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung eines Wabenkörpers aufweisend eine in einem Gehäuse angeordnete Wabenstruktur. Derartige Wabenkörper werden insbesondere zur Nachbehandlung von Abgasen eingesetzt.The present invention relates to a method for producing a honeycomb body comprising a honeycomb structure arranged in a housing. Such honeycomb bodies are used in particular for the aftertreatment of exhaust gases.
Solche Wabenkörper umfassen regelmäßig ein metallisches Gehäuse, indem eine keramische oder metallische Wabenstruktur angeordnet ist. Teil des Herstellungsverfahrens ist dabei, die Wabenstruktur in geeigneter Weise in das Gehäuse einzubringen und letztendlich eine fügetechnische Verbindung zwischen Gehäuse und Wabenstruktur auszubilden.Such honeycomb bodies regularly comprise a metallic housing by arranging a ceramic or metallic honeycomb structure. Part of the manufacturing process is to introduce the honeycomb structure in a suitable manner in the housing and ultimately form a joining connection between the housing and honeycomb structure.
Dafür ist es nötig, dass ein möglichst gleichmäßiger Kontakt der Wabenstruktur mit dem Gehäuse vorliegt. Darüber hinaus sollte sichergestellt sein, dass der Wabenkörper mit einer gewünschten Rundheit bzw. Formgenauigkeit hergestellt wird. Dies ist insbesondere von Interesse, da letztendlich eine Integration des Wabenkörpers beispielsweise in die Abgasanlage einer mobilen Verbrennungskraftmaschine wie in einem Fahrzeug vorgenommen werden soll. Dabei bietet das Gehäuse häufig Anlagefläche für weitere form- oder kraftschlüssige Verbindungen. Eine Ungenauigkeit hinsichtlich der äußeren Form führt dazu, dass unter Umständen Dichtungsmassen zur nachträglichen Ausgleichung von Formtoleranzen, aufwendige Nachbearbeitungsschritte oder andere, zeit- und kostenintensive Maßnahmen erforderlich sind.For this it is necessary that the contact of the honeycomb structure with the housing is as uniform as possible. In addition, it should be ensured that the honeycomb body is produced with a desired roundness or shape accuracy. This is of particular interest, since ultimately an integration of the honeycomb body, for example, in the exhaust system of a mobile internal combustion engine as in a vehicle to be made. The housing often offers contact surface for further positive or non-positive connections. An inaccuracy in terms of the outer shape means that under certain circumstances sealing compounds for subsequent adjustment of shape tolerances, elaborate reworking steps or other, time-consuming and expensive measures are required.
Die
Die
Aus der
Zudem ist noch auf die
Die Probleme bezüglich einer Formgenauigkeit treten insbesondere bei Wabenkörpern auf, die beispielsweise eine metallische Wabenstruktur aufweisen, die in einem nicht-zylindrischen Querschnitt des Gehäuses einzubringen ist. In diesem Fall kann es vorkommen, dass von der Wabenstruktur in Umfangsrichtung des Gehäuses verschiedene Kräfte bzw. Drücke auf das Gehäuse einwirken. Dies kann, gerade bei dünnwandigen Gehäusen bereits zu einer geringen Verformung führen. Bei einer solchen ungleichen Druckverteilung ist zudem beobachtet worden, dass dieser Effekt während später durchgeführten thermischen Behandlungen des Wabenkörpers verstärkt wird. Das kann zu einer weiteren Verformung des Gehäuses und/oder zu einer nicht gleichmäßigen Verbindung des Wabenkörpers mit dem Gehäuse führen.The problems with regard to a dimensional accuracy occur, in particular, in honeycomb bodies which, for example, have a metallic honeycomb structure which is to be introduced in a non-cylindrical cross section of the housing. In this case, it may happen that act from the honeycomb structure in the circumferential direction of the housing, various forces or pressures on the housing. This can already lead to a small deformation, especially with thin-walled housings. In addition, with such an uneven pressure distribution, it has been observed that this effect is enhanced during later thermal treatments of the honeycomb body. This can lead to a further deformation of the housing and / or to a non-uniform connection of the honeycomb body to the housing.
Aufgabe der vorliegenden Erfindung ist es, die mit Bezug auf den Stand der Technik geschilderten Probleme zumindest teilweise zu lösen. Insbesondere soll ein Verfahren zur Herstellung eines formgenauen Wabenkörpers angegeben werden.The object of the present invention is to at least partially solve the problems described with reference to the prior art. In particular, a method for producing a dimensionally accurate honeycomb body is to be specified.
Diese Aufgaben werden gelöst mit einem Verfahren zur Herstellung eines Wabenkörpers gemäß den Merkmalen des Patentanspruchs 1.Weitere vorteilhafte Ausgestaltungen der Erfindung sind in den abhängig formulierten Patentansprüchen angegeben. Es ist darauf hinzuweisen, dass die in den Patentansprüchen einzeln aufgeführten Merkmale in beliebiger, technologisch sinnvoller, Weise miteinander kombiniert werden können und weitere Ausführungsvarianten der Erfindung aufzeigen.These objects are achieved with a method for producing a honeycomb body according to the features of claim 1.Further advantageous embodiments of the invention are specified in the dependent formulated claims. It should be noted that the features listed individually in the claims can be combined with each other in any technologically meaningful way, and show further embodiments of the invention.
Das erfindungsgemäße Verfahren zur Herstellung eines Wabenkörper aufweisend eine in einem Gehäuse angeordnete Wabenstruktur umfasst zumindest die folgenden Schritte:
- a) Ausbilden einer Wabenstruktur,
- b) Einfügen der Wabenstruktur in ein Gehäuse,
- c) Durchführen einer thermischen Behandlung der Wabenstruktur mit Gehäuse,
- a) forming a honeycomb structure,
- b) inserting the honeycomb structure into a housing,
- c) performing a thermal treatment of the honeycomb structure with housing,
Auch wenn das Verfahren grundsätzlich bei jeder Art von Wabenstrukturen einsetzbar ist, so umfasst Schritt a) bevorzugt das Ausbilden einer metallischen Wabenstruktur. Dazu werden zumindest teilweise strukturierte Metallfolien geschichtet und anschließend miteinander verwunden. Dabei kann ein spiralförmiger, ein S-förmiger oder ein ähnlicher Aufbau der Wabenstruktur erzielt werden. Die Wabenstruktur umfasst regelmäßig eine Vielzahl von im Wesentlichen parallel zueinander angeordneten Kanälen, die für ein Abgas durchströmbar sind. Üblicherweise wird die Wabenstruktur getrennt vom Gehäuse vorbereitet und nun mittels Schritt b) in ein Gehäuse eingefügt.Although the method can basically be used with any type of honeycomb structures, step a) preferably comprises the formation of a metallic honeycomb structure. For this purpose, at least partially structured metal foils are layered and then wound together. In this case, a spiral, an S-shaped or a similar structure of the honeycomb structure can be achieved. The honeycomb structure regularly comprises a multiplicity of channels arranged essentially parallel to one another, through which an exhaust gas can flow. Usually, the honeycomb structure is prepared separately from the housing and now inserted by means of step b) in a housing.
Bezüglich des Schritt b) erfolgt meist ein stimseitiges Einführen der Wabenstruktur in ein (insbesondere in Unfangsrichtung geschlossenes) Gehäuse. Hierfür kann es vorteilhaft sein, einen so genannten Einführkonus vorzusehen, der auf das Gehäuse aufgesetzt und durch den die Wabenstruktur hindurchgeführt wird, wobei die Wabenstruktur durch leichte Kompressionen auf das Innenmaß des Gehäuses reduziert wird.With regard to step b), the honeycomb structure is preferably inserted into a housing (in particular in the circumferential direction). For this purpose, it may be advantageous to provide a so-called insertion cone, which is placed on the housing and through which the honeycomb structure is passed, wherein the honeycomb structure is reduced by slight compressions on the internal dimension of the housing.
Schritt c) betrifft insbesondere ein Beschichtungs- und/oder ein Verbindungsverfahren. Hinsichtlich des Verbindungsverfahrens sind solche bevorzugt, bei denen Sinter-, Hartlot- und/oder Schweißverbindungen innerhalb der Wabenstruktur bzw. zwischen Wabenstruktur und dem Gehäuse ausgebildet werden.Step c) relates in particular to a coating and / or a bonding process. With regard to the bonding method, those in which sintered, brazed and / or welded joints are formed within the honeycomb structure or between the honeycomb structure and the housing are preferred.
Das Formteil hat insbesondere die Aufgabe, eine gewünschte Form bzw. Gestalt des Gehäuses während des Herstellungsprozesses im Wesentlichen beizubehalten. Bezüglich der konkreten Ausgestaltung des Formteils sei auf die nachfolgenden Erläuterungen verwiesen. An dieser Stelle sei jedoch schon darauf hingewiesen, dass das Formteil in der Regel stabiler als das Gehäuse ausgeführt ist und in Umfangsrichtung des Gehäuses bereichsweise anliegt. Die Anlageflächen sind insbesondere dort angeordnet, wo eine erhöhte Beanspruchung des Gehäuses in Folge der eingebrachten Wabenstruktur zu erwarten ist. Das betrifft insbesondere die Bereiche, die einen geringeren Abstand zum Mittelpunkt des Wabenkörpers aufweisen und/oder in Bereichen von Krümmungsabschnitten des Gehäuses mit einem großen Krümmungsradius. Grundsätzlich ist auch möglich, mehrere Formteile an einem Gehäuse vorzusehen.The molding in particular has the task of substantially maintaining a desired shape of the housing during the manufacturing process. With regard to the specific embodiment of the molded part, reference is made to the following explanations. At this point, however, it should already be noted that the molding is usually made more stable than the housing and partially applied in the circumferential direction of the housing. The contact surfaces are arranged in particular where an increased stress of the housing due to the introduced honeycomb structure is to be expected. This concerns in particular the areas which have a smaller distance to the center of the honeycomb body and / or in areas of curvature sections of the housing with a large radius of curvature. In principle, it is also possible to provide a plurality of molded parts on a housing.
Besonders vorteilhaft ist das Verfahren, wenn ein Wabenkörper mit einem unrunden Querschnitt des Gehäuses hergestellt wird. Mit "unrund" sind insbesondere ovale, "race-track"-ähnliche, eckige oder weitere nicht-runde Querschnitte gemeint. Diese weisen regelmäßig unterschiedliche Krümmungsradien auf, die teilweise bis ins Unendliche gehen können (gerader Gehäuseabschnitt). Gerade hier kann es zu den eingangs beschriebenen unterschiedlichen Spannungszuständen während der thermischen Behandlung des Wabenkörpers kommen, so dass mit dem hier beschriebenen Verfahren insbesondere solche Wabenkörper formgenau hergestellt werden können.The method is particularly advantageous if a honeycomb body having a non-circular cross-section of the housing is produced. By "non-circular" is meant in particular oval, "race-track" -like, angular or other non-round cross-sections. These regularly have different radii of curvature, some of which can go to infinity (straight housing section). It is precisely here that the different stress states described above can occur during the thermal treatment of the honeycomb body, so that, in particular, such honeycomb bodies can be produced in a dimensionally accurate manner with the method described here.
Deshalb ist es gemäß einer Weiterbildung des Verfahrens besonders vorteilhaft, das Formteil vor Schritt b) außen mit dem Gehäuse in Kontakt zu bringen und nach Schritt c) wieder zu entfernen. Das heißt mit anderen Worten, dass der Verbund aus Wabenstruktur und Gehäuse mittels dem Formteil solange gestützt bzw. formgenau gehalten wird, bis tatsächlich eine fügetechnische Verbindung zwischen Teilkomponenten der Wabenstruktur und dem Gehäuse generiert ist.Therefore, according to a development of the method, it is particularly advantageous to bring the molded part into contact with the housing outside step b) and to remove it again after step c). In other words, that the composite honeycomb structure and housing by means of the molded part as long as supported or retained in shape until a joining technology connection between sub-components of the honeycomb structure and the housing is actually generated.
Weiterhin ist es vorteilhaft, wenn das Formteil auch zumindest während einem der nachstehenden Bearbeitungsprozesse am Gehäuse vorgesehen ist:
- Beloten des Wabenkörpers,
- Beschichten des Wabenkörpers,
- Transport des Wabenkörpers.
- Belote the honeycomb body,
- Coating the honeycomb body,
- Transport of the honeycomb body.
Beim Beloten des Wabenkörpers wird bevorzugt über eine Stirnseite des Wabenkörpers pulverförmiges Hartlot zugeführt. Darüber hinaus ist möglich, dass der Wabenkörper zuvor stirnseitig in eine Haftmittel-Flüssigkeit eingetaucht wird, an der später das Hartlot definiert haften bleiben soll. Beim Beschichten des Wabenkörpers wird insbesondere eine so genannte Washcoat-Beschichtung vorgesehen, die z. B. mit Edelmetallen dotiert und anschließend kalziniert wird. Hinsichtlich des Transportes des Wabenkörpers ist anzumerken, dass diese Fixierung des Wabenkörpers mittels des Formteils z. B. zwischen den einzelnen Bearbeitungsstationen oder zur vorübergehenden Lagerung beibehalten wird.When Belote the honeycomb body powdered hard solder is preferably supplied via an end face of the honeycomb body. In addition, it is possible that the honeycomb body is previously immersed in the front side of an adhesive liquid to which the brazing material should later adhere defined. When coating the honeycomb body in particular a so-called washcoat coating is provided, the z. B. doped with precious metals and then calcined. With regard to the transport of the honeycomb body is to be noted that this fixation of the honeycomb body by means of the molding z. B. is maintained between the individual processing stations or for temporary storage.
Des Weiteren wird nun auch ein Formteil zur Durchführung eines Verfahrens der vorstehend erfindungsgemäß beschriebenen Art vorgeschlagen, wobei ein Gestell mit einer Mehrzahl inwärts gerichteter Anlageflächen für eine gewünschte Außenkontur des Gehäuses vorgesehen ist. Das Gestell ist bevorzugt in Umfangsrichtung geschlossen, beispielsweise nach Art eines Rahmens. Ganz besonders bevorzugt ist das Gestell einteilig ausgerührt. Die Innenkontur des Gestells weist demnach eine Mehrzahl von inwärts gerichteten Anlageflächen auf, dass heißt dass die Anlageflächen den am weitesten nach innen hineinragenden Teilbereich der Innenkontur des Gestells umfassen. Die Anlageflächen sind so zueinander ausgerichtet bzw. ausgebildet, dass sie im Wesentlichen der gewünschten Außenkontur des Gehäuses entsprechen. Mit anderen Worten bedeutet dies, dass die Anlageflächen einen Teil der Außenkontur des Gehäuses abbilden. Grundsätzlich ist jedoch möglich, dass ein Teil der Anlageflächen auch angeschrägt sind, so dass beispielsweise ein vereinfachtes Einführen des Gehäuses in das Gestell ermöglicht wird.Furthermore, a molded part for carrying out a method of the type described above in accordance with the invention is also proposed, a frame having a plurality of inwardly directed abutment surfaces being provided for a desired outer contour of the housing. The frame is preferably closed in the circumferential direction, for example in the manner of a frame. Most notably Preferably, the frame is stirred in one piece. The inner contour of the frame accordingly has a plurality of inwardly directed contact surfaces, that is to say that the contact surfaces comprise the part of the inner contour of the frame that projects furthest inward. The contact surfaces are aligned with one another or designed such that they essentially correspond to the desired outer contour of the housing. In other words, this means that the contact surfaces form part of the outer contour of the housing. In principle, however, it is possible that a part of the contact surfaces are also beveled, so that, for example, a simplified insertion of the housing is made possible in the frame.
Grundsätzlich ist auch möglich, dass das Formteil so gestaltet ist, dass die Relativlage der Anlageflächen zueinander einstellbar ist. Damit wird ein besonders flexibler Einsatz des Formteils für unterschiedliche Konturen des Gehäuses ermöglicht. Zudem besteht der Vorteil, dass mit solchen beweglichen Anlageflächen eine leichtere Entnahme des Gehäuses bzw. des Wabenkörpers beispielsweise nach Durchführung einer thermischen Behandlung ermöglicht ist.In principle, it is also possible that the molded part is designed so that the relative position of the contact surfaces is adjustable to each other. This allows a particularly flexible use of the molding for different contours of the housing. In addition, there is the advantage that with such movable contact surfaces easier removal of the housing or the honeycomb body, for example, after performing a thermal treatment is possible.
Weiter wird auch vorgeschlagen, dass radial auswärts gerichtete Ausnehmungen die inwärts gerichteten Anlageflächen beabstanden. Die Ausnehmungen verlaufen bevorzugt im Wesentlichen parallel zu den Anlageflächen und begrenzen diese zumindest teilweise. Mittels solcher Ausnehmungen wird verhindert, dass ein zu großer Anpressdruck des Gehäuses an das Gestell auftritt. Damit ist das Gehäuse nach der Bearbeitung leichter wieder entnehmbar.Further, it is also proposed that radially outwardly directed recesses space the inwardly directed abutment surfaces. The recesses preferably extend substantially parallel to the contact surfaces and limit these at least partially. By means of such recesses prevents excessive pressure of the housing to the frame occurs. This makes the housing easier to remove after processing.
Auch deshalb ist es von besonderem Vorteil, wenn die Anlageflächen des Formteils zwischen 50 % und 80 % des Umfangs des Gehäuses abdecken. Dies gewährleitstet einerseits eine ausreichende Fixierung des Gehäuses zur Erzielung einer Formstabilität und ermöglicht andererseits ein sicheres Entfernen des Gehäuses auch im Rahmen einer Serienfertigung. Dabei können die Ausnehmungen beispielsweise auch für Greifwerkzeuge geeignet gestaltet sein.For this reason too, it is particularly advantageous if the contact surfaces of the molded part cover between 50% and 80% of the circumference of the housing. This ensures on the one hand a sufficient fixation of the housing to achieve a dimensional stability and on the other hand allows a safe removal of the housing also as part of a series production. In this case, the recesses may be designed, for example, suitable for gripping tools.
Besonders vorteilhaft ist es, wenn das Formteil aus einem hochtemperaturfesten und korrosionsbeständigen Metall ist. Ganz besonders bevorzugt ist das Formteil aus einem zumindest ähnlichen Material wie das Gehäuse, um insbesondere während einer thermischen Behandlung des Wabenkörpers ein gleichmäßiges thermisches Ausdehnungsverhalten sicherzustellen. Das Metall sollte zumindest in der Lage sein, dauerhaft den thermischen Bedingungen während einem Hartlöt-Prozess standzuhalten.It is particularly advantageous if the molded part is made of a high-temperature-resistant and corrosion-resistant metal. The molding is very particularly preferably made from an at least similar material as the housing in order to ensure a uniform thermal expansion behavior, in particular during a thermal treatment of the honeycomb body. At a minimum, the metal should be able to withstand the thermal conditions during a brazing process.
Gemäß einer Ausgestaltung des Formteils sind die Anlageflächen zumindest teilweise mit einer Beschichtung ausgeführt. Alternativ oder in Kombination dazu können die Anlageflächen auch zumindest teilweise mit einer strukturierten Oberfläche versehen sein. Diese Maßnahmen dienen beispielsweise zur Vermeidung von Verbindungen zwischen dem Formteil und dem Gehäuse, wie sie gegebenenfalls bei hohen Temperaturen stattfinden können (zum Beispiel Sinterverbindungen). Ebenso wird durch die strukturierte Oberfläche der Anlagefläche die Kontaktfläche zwischen Formteil und Gehäuse weiter reduziert, womit die Entfembarkeit des Gehäuses nach dem Herstellungsverfahren des Wabenkörpers verbessert wird. Auch wenn diese Maßnahmen nur teilweise bei den Anlageflächen vorgesehen sein können, wird die Anwendung für alle Anlageflächen in gleicher Weise bevorzugt.According to one embodiment of the molded part, the contact surfaces are at least partially executed with a coating. Alternatively or in combination, the contact surfaces can also be provided at least partially with a structured surface. These measures are used, for example, to avoid connections between the molded part and the housing, as they may possibly take place at high temperatures (for example, sintered connections). Likewise, the contact surface between the molded part and the housing is further reduced by the structured surface of the contact surface, whereby the Entfembarkeit of the housing is improved according to the manufacturing process of the honeycomb body. Although these measures may be only partially provided in the contact surfaces, the application for all contact surfaces in the same way is preferred.
Die Bereitstellung einer Abgasbehandlungseinheit umfassend einen Wabenkörper mit einem Gehäuse einer Dicke von höchstens 1,5 mm wird bevorzugt nach dem erfindungsgemäß beschriebenen Verfahren verwirklicht.The provision of an exhaust gas treatment unit comprising a honeycomb body with a housing having a thickness of at most 1.5 mm is preferably realized according to the method described according to the invention.
Die Erfindung sowie das technische Umfeld werden nachfolgend anhand der Figuren näher erläutert. Die Figuren zeigen auch besonders bevorzugte Ausführungsvarianten der Erfindung, auf die diese jedoch nicht begrenzt ist. Es zeigen:
- Fig. 1:
- Einen nicht-zylindrischen Wabenkörper,
- Fig. 2:
- eine Ausgestaltung eines Formteils,
- Fig. 3:
- ein Detail eines in einem Formteil angeordneten Wabenkörpers, und
- Fig. 4:
- ein Abgassystem für ein Fahrzeug.
- Fig. 1:
- A non-cylindrical honeycomb body,
- Fig. 2:
- an embodiment of a molded part,
- 3:
- a detail of a arranged in a molding honeycomb body, and
- 4:
- an exhaust system for a vehicle.
Die Wabenstruktur 3 ist mit einer Mehrzahl von S-förmig gewundenen strukturierten und glatten Metallfolien 18 aufgebaut, die im Wesentlichen parallel zueinander verlaufende Kanäle 15 bilden. Insbesondere bei dieser Anordnung wirken ausgehend von den Metallfolien 18 unterschiedliche Spannungen auf das Gehäuse 1 ein, die unter Umständen die Außenkontur 6 des Gehäuses 1 beeinflussen könnten. Zur Vermeidung von Abweichungen von der Außenkontur 6 wird der Einsatz eines Formteils vorgeschlagen, welches in einer bevorzugten Ausführungsvariante für einen solchen Wabenkörper in
Das Formteil 4 für den in
Als bevorzugtes Einsatzgebiet für solche Wabenkörper ist der Automobil-Bereich anzuführen. Demgemäß ist schematisch der Aufbau eines Abgassystems 21 für ein Fahrzeug 19 in
- 11
- Gehäusecasing
- 22
- Wabenkörperhoneycombs
- 33
- Wabenstrukturhoneycomb structure
- 44
- Formteilmolding
- 55
- Anlageflächencontact surfaces
- 66
- Außenkonturouter contour
- 77
- Gestellframe
- 88th
- Ausnehmungenrecesses
- 99
- Umfangscope
- 1010
- Oberflächesurface
- 1111
- AbgasbehandlungseinheitExhaust gas treatment unit
- 1212
- Querschnittcross-section
- 1313
- Erste ErstreckungFirst extension
- 1414
- Zweite ErstreckungSecond extension
- 1515
- Kanalchannel
- 1616
- Dickethickness
- 1717
- Beschichtungcoating
- 1818
- Metallfoliemetal foil
- 1919
- Fahrzeugvehicle
- 2020
- Motorengine
- 2121
- Abgassystemexhaust system
Claims (11)
- Method for producing a honeycomb body (2) having a honeycomb structure (3) arranged in a housing (1), which method comprises at least the following steps:a) forming a honeycomb structure (3),b) inserting the honeycomb structure (3) into a housing (1),c) carrying out a heat treatment operation on the honeycomb structure (3) with the housing (1),with a formed part (4), which is in contact in regions at the outside, being provided at least during step b) and step c), the contact faces (5) of said formed part (4) reproduce a desired outer contour (6) of the housing (1).
- Method according to Patent Claim 1, in which a honeycomb body (2) having a non-cylindrical housing cross section (12) is produced.
- Method according to Patent Claim 1 or 2, in which the formed part (4) is placed in contact with the housing (1) at the outside before step b), and is removed again after step c).
- Method according to one of the preceding patent claims, in which the formed part (4) is also provided at least during one of the following machining processes on the housing (1):- brazing the honeycomb body (2),- coating the honeycomb body (2),- transporting the honeycomb body (2).
- Method according to one of the preceding patent claims, in which the formed part (4) is provided with a frame (7) being provided with a plurality of inwardly directed contact faces (5) for a desired outer contour (6) of the housing (1).
- Method according to Patent Claim 5, in which the relative position of the contact faces (5) of the formed part (4) are adjustable relative to one another.
- Method according to Patent Claim 5 or 6, in which radially outwardly directed recesses (8) of the formed part (4) provide space apart the inwardly directed contact faces (5).
- Method according to one of the preceding Patent Claims 5 to 7, in which the contact faces (5) of the formed part (4) cover between 50% and 80% of the periphery (9) of the housing (1).
- Method according to one of the preceding Patent Claims 5 to 8, in which said formed part is made from a high-temperature resistant and corrosion resistant metal.
- Method according to one of the preceding Patent Claims 5 to 9, in which with the contact faces (5) of the formed part (4) are provided at least partially with a coating (17).
- Method according to one of the preceding Patent Claims 5 to 9, in which the contact faces (5) of the formed part (4) are provided at least partially with a structured surface (10).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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DE102005061778A DE102005061778A1 (en) | 2005-12-23 | 2005-12-23 | Process for producing a dimensionally accurate honeycomb body and molded part therefor |
Publications (2)
Publication Number | Publication Date |
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EP1801378A1 EP1801378A1 (en) | 2007-06-27 |
EP1801378B1 true EP1801378B1 (en) | 2008-10-08 |
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Application Number | Title | Priority Date | Filing Date |
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EP06025092A Active EP1801378B1 (en) | 2005-12-23 | 2006-12-05 | Process for the manufacture of a precisely shaped honeycomb body |
Country Status (5)
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US (1) | US8281488B2 (en) |
EP (1) | EP1801378B1 (en) |
JP (1) | JP5235300B2 (en) |
DE (2) | DE102005061778A1 (en) |
ES (1) | ES2315985T3 (en) |
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DE102011115509C5 (en) * | 2011-10-11 | 2020-01-16 | Benteler Automobiltechnik Gmbh | Method for housing a monolith with a storage mat in a housing by plugging |
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JPH0615816B2 (en) * | 1983-01-28 | 1994-03-02 | 本田技研工業株式会社 | Assembling method of catalyst converter |
US5055274A (en) * | 1989-02-06 | 1991-10-08 | Tennessee Gas Pipeline Company | Catalytic converter and substrate support with one piece housing |
TW225491B (en) * | 1992-05-29 | 1994-06-21 | Nippon Yakin Kogyo Co Ltd | |
JP3339933B2 (en) * | 1993-09-28 | 2002-10-28 | 新日本製鐵株式会社 | Honeycomb body press-fitting device |
DE4439685A1 (en) * | 1994-11-07 | 1996-05-09 | Emitec Emissionstechnologie | Method and device for producing a honeycomb body, in particular a catalyst carrier body, with a housing |
JP3585064B2 (en) * | 1995-10-12 | 2004-11-04 | トヨタ自動車株式会社 | Monolithic catalytic converter and method of manufacturing the same |
JPH09174185A (en) * | 1995-12-22 | 1997-07-08 | Usui Internatl Ind Co Ltd | Manufacture of metallic support |
TW396112B (en) * | 1996-10-10 | 2000-07-01 | Engelhard Corp | Honeycomb carrier body for catalytic converters and method for making same |
US5909916A (en) * | 1997-09-17 | 1999-06-08 | General Motors Corporation | Method of making a catalytic converter |
DE19753609A1 (en) * | 1997-12-03 | 1999-06-10 | Leistritz Abgastech | Exhaust gas catalytic converter, in particular for motor vehicles and process for its manufacture |
JPH11197518A (en) * | 1998-01-07 | 1999-07-27 | Yutaka Giken Co Ltd | Production of metallic catalyst carrier |
US6551535B2 (en) * | 2001-01-30 | 2003-04-22 | Acs Industries, Inc. | Extrusion coating process for catalytic monoliths |
DE10217259A1 (en) * | 2002-04-18 | 2003-11-13 | Emitec Emissionstechnologie | Catalyst carrier body with corrugated jacket and process for its production |
DE10226282A1 (en) * | 2002-06-13 | 2003-12-24 | Emitec Emissionstechnologie | Non-cylindrical catalyst carrier body and tool and method for its production |
DE10242283B4 (en) * | 2002-09-12 | 2005-09-08 | J. Eberspächer GmbH & Co. KG | Apparatus and method for pressing a bearing mat to a monolith |
JP2004353549A (en) * | 2003-05-29 | 2004-12-16 | Sango Co Ltd | Method for producing fluid treatment device having honeycomb structure built therein |
DE10329002A1 (en) * | 2003-06-27 | 2005-01-20 | Emitec Gesellschaft Für Emissionstechnologie Mbh | Structure of a metallic honeycomb structure and method for its production |
US20070033803A1 (en) * | 2005-08-09 | 2007-02-15 | Lawrukovich Michael P | Methods for substrate retention |
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2005
- 2005-12-23 DE DE102005061778A patent/DE102005061778A1/en not_active Withdrawn
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JP5235300B2 (en) | 2013-07-10 |
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US20070143999A1 (en) | 2007-06-28 |
US8281488B2 (en) | 2012-10-09 |
DE102005061778A1 (en) | 2007-06-28 |
EP1801378A1 (en) | 2007-06-27 |
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