EP3469196B1 - Method for producing a honeycomb structure - Google Patents

Method for producing a honeycomb structure Download PDF

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Publication number
EP3469196B1
EP3469196B1 EP17726272.2A EP17726272A EP3469196B1 EP 3469196 B1 EP3469196 B1 EP 3469196B1 EP 17726272 A EP17726272 A EP 17726272A EP 3469196 B1 EP3469196 B1 EP 3469196B1
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EP
European Patent Office
Prior art keywords
web structure
winding
metal foil
spiral
axial direction
Prior art date
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Active
Application number
EP17726272.2A
Other languages
German (de)
French (fr)
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EP3469196A1 (en
Inventor
Alf NIEDMANN
Emmanuel KRAUS
Alexander MÖSELER
Ferdi Kurth
Harald Kraus
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.)
Vitesco Technologies GmbH
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Vitesco Technologies GmbH
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Publication of EP3469196A1 publication Critical patent/EP3469196A1/en
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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
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust 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
    • F01N3/24Exhaust 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
    • F01N3/28Construction of catalytic reactors
    • F01N3/2803Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
    • F01N3/2807Metal other than sintered metal
    • F01N3/281Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
    • 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
    • F01N13/18Construction facilitating manufacture, assembly, or disassembly
    • 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
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust 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
    • F01N3/18Exhaust 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 methods of operation; Control
    • F01N3/20Exhaust 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 methods of operation; Control specially adapted for catalytic conversion ; Methods of operation or control of catalytic converters
    • F01N3/2006Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating
    • F01N3/2013Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating using electric or magnetic heating means
    • F01N3/2026Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating using electric or magnetic heating means directly electrifying the catalyst substrate, i.e. heating the electrically conductive catalyst substrate by joule effect
    • 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
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust 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
    • F01N3/24Exhaust 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
    • F01N3/28Construction of catalytic reactors
    • F01N3/2839Arrangements for mounting catalyst support in housing, e.g. with means for compensating thermal expansion or vibration
    • F01N3/2842Arrangements for mounting catalyst support in housing, e.g. with means for compensating thermal expansion or vibration specially adapted for monolithic supports, e.g. of honeycomb type
    • 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
    • F01N2330/00Structure of catalyst support or particle filter
    • F01N2330/02Metallic plates or honeycombs, e.g. superposed or rolled-up corrugated or otherwise deformed sheet metal
    • F01N2330/04Methods of manufacturing
    • 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
    • F01N2330/00Structure of catalyst support or particle filter
    • F01N2330/30Honeycomb supports characterised by their structural details
    • F01N2330/40Honeycomb supports characterised by their structural details made of a single sheet, foil or plate
    • 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
    • F01N2330/00Structure of catalyst support or particle filter
    • F01N2330/30Honeycomb supports characterised by their structural details
    • F01N2330/44Honeycomb supports characterised by their structural details made of stacks of sheets, plates or foils that are folded in S-form

Definitions

  • the present invention relates to a method for producing a honeycomb structure.
  • the honeycomb structure is in particular formed by at least one, at least partially structured metal foil which is stacked and / or wound and / or wound to produce the honeycomb structure.
  • the honeycomb structure at least partially has flow channels through which a fluid can flow through the honeycomb structure from a first end face to a second end face.
  • Partially structured means that the metal foil is partly smooth, partly with e.g. B. sinusoidal waves, with holes, with deflecting structures or the like.
  • the honeycomb structure is preferably used to treat exhaust gas, in particular exhaust gas from an internal combustion engine in a motor vehicle, e.g. B. a car, a truck, a ship, an aircraft used.
  • the honeycomb structure has one or more air gaps which extend along an axial direction, in particular from one end face to the other end face, metal foils arranged adjacent to one another being arranged in an electrically insulated manner by the air gap.
  • the air gap also extends through the honeycomb structure in a circumferential direction and / or a radial direction.
  • the air gap serves z. B. the electrical insulation in an electrically heated honeycomb body. The course of a current path through the honeycomb body is at least partially predetermined by the air gap.
  • Such electrically heated honeycomb bodies with an air gap are, for. B. from the WO 2013/150066 A1 known.
  • the DE 197 04 521 A1 discloses a method for producing a honeycomb body with a plurality of channels permeable to a fluid from a plurality of at least partially structured sheets, in which at least one stack is layered from a plurality of at least partially structured sheets.
  • the stack is placed in a mold and held in it by a wrapping device in the central region of the stack.
  • the stack is then subjected to a wrapping process until a predetermined degree of wrapping of the stack is reached. At least during the wrapping process, a structure formed in a central area with structures of the structured sheets of the stack lying relative to one another is retained.
  • the EP 0 218 062 A1 discloses a carrier matrix which is wound from a carrier tape profiled in its transverse direction.
  • the carrier matrix has deflections of the carrier tape, the deflections being arranged in planes.
  • the deflections are generated during the winding process by inserting deflection pins between the corresponding winding layers.
  • the deflection pins are inserted depending on the desired cross section of the support matrix between the winding layers, so that after the winding process and after the removal of the deflection pins, the support matrix can be inserted into a jacket which has the cross section of the support matrix.
  • the WO 2013/150066 A1 discloses an electrical connection of a plurality of sheet metal layers of a honeycomb body to a connecting pin, the honeycomb body having a metal jacket with an inner circumference through which the connecting pin is passed in an electrically insulating manner in a bushing.
  • the sheet layers are alternately arranged roughly structured and finely structured or smooth sheets.
  • the CN 105 464 766 A discloses a method for producing an electrically heatable carrier body, the honeycomb body being formed from structured and smooth layers.
  • the carrier has a heating core and an insulation body. Solder is placed on the heater core while none Solder material is placed on the insulation body before the layers are joined together. The insulator is removed after soldering, creating an electrically non-conductive area.
  • the JP H09 174179 A discloses a metallic honeycomb body which is optimized in that the winding tension can be increased when the honeycomb body is produced in order to obtain a stable body.
  • a tension-generating tool and a tension-sensing tool are used in the manufacturing process.
  • oxidized smooth and corrugated foils oxidized, at least partially structured metal foils
  • oxidized, at least partially structured metal foils are used in the honeycomb structure with, which are then removed from the honeycomb structure after the soldering process.
  • a molding plate is therefore proposed here which has a first web structure.
  • the shaping plate and in particular the first web structure are made of a temperature-resistant material, e.g. B. a steel alloy, a ceramic or the like.
  • the web structure preferably forms the air gap to be generated in the finished honeycomb structure (that is, for example, also connected by a soldering process).
  • the first web structure starting from a support surface of the shaping plate, has a height in the axial direction, so that the metal foils to be arranged in the first web structure can plunge far enough into the first web structure a fixed air gap along the axial direction can be generated with a constant width.
  • the first web structure extends in particular in the axial direction with a preferably constant height.
  • the web structure extends in a plane parallel to the support surface, that is to say transversely to the axial direction, in particular in a spiral shape. A current path in the honeycomb structure can thus be predetermined by the web structure.
  • step c. the at least one metal foil is arranged on the support surface and within the first web structure, that is to say between the walls of the first web structure.
  • step d the shaping plate is fed together with the at least one metal foil to a connecting step in which the at least one metal foil is connected to one another for the permanent formation of the honeycomb structure, in a subsequent step e. the molding plate with the first web structure is removed from the honeycomb structure.
  • the connecting step comprises in particular a soldering process, preferably a soldering process, in which a solder material is melted at temperatures of 800 to 1200 ° C. [degrees Celsius] and the adjacent and touching metal foils are connected to one another at positions provided for this purpose.
  • This soldering process is known for the production of the honeycomb bodies described here.
  • the molding plate has a plurality of first openings which extend through the molding plate in the axial direction, a support pin being able to be passed through at least one of the first openings for arrangement in the honeycomb structure after step c.
  • the support pin is used in particular for spacing one, and for fixing the honeycomb structure by a so-called Support honeycomb body, which can be arranged downstream or upstream of the honeycomb structure in a fluid (exhaust gas) line.
  • the support pin is used here in particular only for checking the position of the honeycomb structure produced. In this way, it can be ensured for later process steps that the honeycomb structure can be reproducibly connected to other supporting honeycomb structures.
  • the method additionally uses a winding spiral, which has a spiral-shaped second web structure which corresponds to the first web structure; wherein the second web structure is flush in the axial direction on a first end face facing the molding plate, wherein the second web structure has an incline on the second end side, the second end side continuously extending from the center of the second web structure along the spiral windings to the first end side approximates; and wherein the winding coil has at least two pins that extend further from the center along the axial direction; wherein the at least one metal foil is received between the two pins and is continuously taken up into the second web structure by rotation of the winding spiral and then transferred into the first web structure.
  • the winding spiral enables, in particular, an automated arrangement of the at least one metal foil in the first web structure. This process is explained in detail in the following description of the figures.
  • a second web structure extends spirally, on the one hand along a circumferential direction and in a radial direction from the outside inwards and on the other hand with each turn also in the axial direction.
  • the (complete) second web structure is flush with the first face, with the second web structure extends on the second face with a slope always further along the axial direction, so that a center on the second face of the second web structure is arranged at a greatest distance from the first face.
  • the slope of the spiral second web structure enables the one metal foil (or the stack of metal foils) to be wound up successively spirally from the center as the winding spiral rotates and more and more turns (starting from an innermost turn in the center towards an outermost turn) in of the second web structure.
  • the second web structure also forms the predetermined air gaps in the honeycomb structure.
  • the second web structure corresponds at least essentially to the shape of the first web structure (in a plane transverse to the axial direction).
  • the at least one metal foil can thus be transferred from the winding spiral along the axial direction into the first web structure of the shaping plate and the winding spiral can be used further for the next winding process.
  • the winding spiral has driver pins which extend from the second web structure on the first end face and which extend into second openings in the first web structure and / or in the molding plate and / or into first openings in the molding plate.
  • driver pins ensure in particular an aligned arrangement of the first web structure and the second web structure. Furthermore, the rotary movement of the shaping plate and winding spiral can be coupled to wind up the at least one metal foil.
  • step c. also use a winding plate which has a spirally extending slot which corresponds to the second web structure; wherein during the rotation of the winding spiral, the winding spiral with the second web structure and beginning with the center dips into the slot and so the at least one metal foil arranged between the winding plate and the winding spiral is successively introduced along the axial direction into the winding spiral and finally transferred into the first web structure.
  • the winding plate is, in particular, flat, so that the at least one metal foil is preferably guided in its entire extent along the axial direction.
  • the movement along the axial direction is coupled and / or synchronized with the rotation of the winding plate and the shaping plate.
  • the at least one at least partially structured metal foil forms a multilayer stack before being arranged in the first web structure.
  • a metal foil is folded several times to form a stack.
  • several, in particular differently structured (or at least partially not structured, ie essentially smooth) metal foils can also be arranged on top of one another to form a stack.
  • a winding device for carrying out a method according to the invention is also proposed, at least comprising a shaping plate with a first web structure.
  • the winding device further comprises at least one winding spiral with a second web structure and a winding plate.
  • Fig. 1 shows a stack 24 of metal foils 2 in a perspective view and the method step a.
  • Fig. 2 shows a molding plate 5 in a perspective view and the method step b.
  • the shaping plate 5 has a first web structure 8.
  • the first web structure 8 forms the air gap 4 to be generated in the finished honeycomb structure 1 (see also, for example, connected by a soldering process) (see Fig. 4 ).
  • the first web structure 8, starting from the support surface 6 of the shaping plate 5, has a height in the axial direction 7, so that the metal foils 2 to be arranged in the first web structure 8 can penetrate far enough into the first web structure 8, according to a defined air gap 4 can be generated along the axial direction 7 with a constant width (see Fig. 3 ).
  • the first web structure 8 extends in a plane 9 parallel to the support surface 6, that is to say transversely to the axial direction 7 Web structure 8, a current path in the honeycomb structure 1 can be specified. Furthermore, the molding plate 5 has a plurality of first openings 10 which extend through the molding plate 5 in the axial direction 7, wherein a support pin 11 can be passed through at least one of the first openings 10 for arrangement in the honeycomb structure 1 after step c.
  • Fig. 3 shows a shaped plate 5 and a honeycomb structure 1 arranged thereon in a perspective view and method step c.
  • the first web structure 8 extends here in the axial direction 7 with a constant height.
  • the first honeycomb structure 1 here comprises a plurality of at least partially structured metal foils 2, individual metal foils 2 being arranged in partial regions 3 of the honeycomb structure 1 so as to be electrically insulated from an adjacent metal foil 2 by an air gap 4.
  • step d the molding plate 5, together with the at least one metal foil 2, is fed to a connecting step in which the at least one metal foil 2 is connected to one another for the permanent formation of the honeycomb structure 1.
  • Fig. 4 shows a finished honeycomb structure 1 with an air gap 4 in a perspective view.
  • step e the molding plate 5 with the first web structure 8 has been removed from the honeycomb structure 1.
  • Fig. 5 shows a second mold plate 5 in a perspective view.
  • the comments on Fig. 2 apply accordingly.
  • a plurality of first openings 10 are provided, which extend through the shaping plate 5 in the axial direction 7.
  • the first web structure 8 comprises a plurality of windings 18 and also has second openings 21, into which driver pins 20 of the winding spiral 12 can extend (see Fig. 6 ).
  • Fig. 6 shows a winding device 25 in an exploded view and in a perspective view.
  • the winding device 25 shown here is in step c. of the procedure used.
  • the winding device 25 comprises a receptacle 26 which can be driven in at least one circumferential direction 27.
  • the winding device 25 further comprises a shaping plate 5, a winding spiral 12 and a winding plate 22.
  • the winding spiral 12 has a spiral-shaped second web structure 13 which corresponds to the first web structure 8 on the shaping plate 5; the second web structure 13 ends flush on the first end face 14 facing the shaping plate 5 in the axial direction 7, the second web structure 13 having an incline 16 on the second end face 15.
  • the winding spiral 12 has at least two pins 19 which extend further from the center 17 along the axial direction 7.
  • the stack 24 of metal foils 2 is received between the two pins 19 and continuously taken up into the second web structure 13 by rotating the winding spiral 12 and then transferred into the first web structure 8.
  • the winding spiral 12 thus enables an automated arrangement of the at least one metal foil 2 in the first web structure 8.
  • a second web structure 13 extends in a spiral , on the one hand along a circumferential direction 27 and in a radial direction 28 from the outside inwards and on the other hand with each turn 18 also in the axial direction 7.
  • the complete second web structure 13 is flush with the first end face 14, the second web structure 13 along the second end face 15 with an incline 16 the axial direction 7, so that a center 17 on the second end face 15 of the second web structure is arranged at a greatest distance from the first end face 14.
  • the slope 16 of the spiral second web structure 13 enables the one metal foil 2 (or the stack 24 of metal foils 2) to be wound up successively from the center 17 when the winding spiral 12 rotates and more and more turns 18 (starting from an innermost turn 18 in the center 17 towards an outermost turn 18) in the second web structure 13.
  • the second web structure 13 likewise forms the predetermined air gaps 4 in the honeycomb structure 1.
  • the second web structure 13 corresponds at least substantially to the shape of the first web structure 8 (in a plane 9 transverse to the axial direction 7).
  • the at least one metal foil 2 can thus be transferred from the winding spiral 12 along the axial direction 7 into the first web structure 8 of the shaping plate 5 and the winding spiral 12 can be used further for the next winding process.
  • the winding spiral 12 has driver pins 20 which extend from the second web structure 13 on the first end face 14 in the axial direction 7 and which extend into second openings 21 in the first web structure 8 and / or in the shaping plate 5 and / or in first openings 10 extend into the molding plate 5.
  • driver pins 20 ensure an aligned arrangement of the first web structure 8 and the second web structure 13. Furthermore, the rotary movement of receptacle 26, shaping plate 5 and winding spiral 12 can be coupled in this way for winding up the at least one metal foil 2.
  • a winding plate 22 is further shown, which has a spirally extending slot 23, which corresponds to the second web structure 13.
  • the winding spiral 12 dips during the rotation of the winding spiral 12 with the second web structure 13 and starting with the center 17 into the slot 23 and thus transfers the at least one metal foil 2 arranged between the winding plate 22 and the winding spiral 12 successively along the axial direction 7 into the winding spiral 12 and finally into the first web structure 8.
  • the winding plate 22 is of flat design here, so that the at least one metal foil 2 is guided essentially in its entire extent along the axial direction 7.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Catalysts (AREA)
  • Laminated Bodies (AREA)
  • Exhaust Gas After Treatment (AREA)

Description

Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung einer Wabenstruktur. Die Wabenstruktur wird insbesondere gebildet durch zumindest eine, wenigstens teilweise strukturierte Metallfolie, die zur Erzeugung der Wabenstruktur gestapelt und/oder gewickelt und/oder gewunden wird. Die Wabenstruktur weist zumindest teilweise Strömungskanäle auf, durch die ein Fluid die Wabenstruktur von einer ersten Stirnseite zu einer zweiten Stirnseite durchströmen kann. Teilweise strukturiert bedeutet, dass die Metallfolie teilweise glatt, teilweise mit z. B. sinusförmigen Wellen, mit Löchern, mit Umlenkstrukturen oder ähnlichem ausgeführt ist. Die Wabenstruktur wird bevorzugt zur Behandlung von Abgas, insbesondere von Abgas einer Verbrennungskraftmaschine in einem Kraftfahrzeug, z. B. ein PKW, ein LKW, ein Schiff, ein Flugzeug, eingesetzt.The present invention relates to a method for producing a honeycomb structure. The honeycomb structure is in particular formed by at least one, at least partially structured metal foil which is stacked and / or wound and / or wound to produce the honeycomb structure. The honeycomb structure at least partially has flow channels through which a fluid can flow through the honeycomb structure from a first end face to a second end face. Partially structured means that the metal foil is partly smooth, partly with e.g. B. sinusoidal waves, with holes, with deflecting structures or the like. The honeycomb structure is preferably used to treat exhaust gas, in particular exhaust gas from an internal combustion engine in a motor vehicle, e.g. B. a car, a truck, a ship, an aircraft used.

Die Wabenstruktur weist einen oder mehrere Luftspalte auf, die sich entlang einer axialen Richtung insbesondere von einer Stirnseite zur anderen Stirnseite erstrecken, wobei benachbart zueinander angeordnete Metallfolien durch den Luftspalt elektrisch isoliert angeordnet sind. Der Luftspalt erstreckt sich zusätzlich auch in einer Umfangsrichtung und/oder einer radialen Richtung durch die Wabenstruktur. Der Luftspalt dient z. B. der elektrischen Isolation in einem elektrisch beheizten Wabenkörper. Durch den Luftspalt wird der Verlauf eines Strompfades durch den Wabenkörper zumindest teilweise vorgegeben. Solche elektrisch beheizten Wabenkörper mit Luftspalt sind z. B. aus der WO 2013/150066 A1 bekannt.The honeycomb structure has one or more air gaps which extend along an axial direction, in particular from one end face to the other end face, metal foils arranged adjacent to one another being arranged in an electrically insulated manner by the air gap. The air gap also extends through the honeycomb structure in a circumferential direction and / or a radial direction. The air gap serves z. B. the electrical insulation in an electrically heated honeycomb body. The course of a current path through the honeycomb body is at least partially predetermined by the air gap. Such electrically heated honeycomb bodies with an air gap are, for. B. from the WO 2013/150066 A1 known.

Die DE 197 04 521 A1 offenbart ein Verfahren zur Herstellung eines Wabenkörpers mit einer Vielzahl von für ein Fluid durchlässigen Kanälen aus einer Vielzahl von zumindest teilweise strukturierten Blechen, bei dem wenigstens ein Stapel aus einer Mehrzahl von zumindest teilweise strukturierten Blechen geschichtet wird. Der Stapel wird in eine Form eingebracht und in dieser von einer Umschlingungsvorrichtung in dem Zentralbereich des Stapels gehalten. Anschließend wird der Stapel einem Umschlingungsvorgang unterzogen, bis ein vorgegebener Umschlingungsgrad des Stapels erreicht ist. Wenigstens während des Umschlingungsvorgangs bleibt ein in einem Zentralbereich ausgebildeter Aufbau mit relativ zueinander liegenden Strukturen der strukturierten Bleche des Stapels erhalten.The DE 197 04 521 A1 discloses a method for producing a honeycomb body with a plurality of channels permeable to a fluid from a plurality of at least partially structured sheets, in which at least one stack is layered from a plurality of at least partially structured sheets. The stack is placed in a mold and held in it by a wrapping device in the central region of the stack. The stack is then subjected to a wrapping process until a predetermined degree of wrapping of the stack is reached. At least during the wrapping process, a structure formed in a central area with structures of the structured sheets of the stack lying relative to one another is retained.

Die EP 0 218 062 A1 offenbart eine Trägermatrix, welche aus einem in seiner Querrichtung profilierten Trägerband gewickelt ist. Die Trägermatrix weist Umlenkungen des Trägerbandes auf, wobei die Umlenkungen in Ebenen angeordnet sind. Erzeugt werden die Umlenkungen während des Wickelvorgangs durch das Einbringen von Umlenkstiften zwischen die entsprechenden Wickellagen. Die Umlenkstifte werden dabei in Abhängigkeit vom gewünschten Querschnitt der Trägermatrix zwischen die Wickellagen eingebracht, so dass nach dem Wickelvorgang und nach dem Entfernen der Umlenkstifte die Trägermatrix in einen Mantel, der den Querschnitt der Trägermatrix besitzt, eingeführt werden kann.The EP 0 218 062 A1 discloses a carrier matrix which is wound from a carrier tape profiled in its transverse direction. The carrier matrix has deflections of the carrier tape, the deflections being arranged in planes. The deflections are generated during the winding process by inserting deflection pins between the corresponding winding layers. The deflection pins are inserted depending on the desired cross section of the support matrix between the winding layers, so that after the winding process and after the removal of the deflection pins, the support matrix can be inserted into a jacket which has the cross section of the support matrix.

Die WO 2013/150066 A1 offenbart einen elektrischen Anschluss von mehreren Blechlagen eines Wabenkörpers an einen Anschlussstift, wobei der Wabenkörper einen Metallmantel mit einem Innenumfang aufweist, durch den der Anschlussstift in einer Durchführung elektrisch isolierend hindurchgeführt ist. Die Blechlagen sind abwechselnd angeordnete grob strukturierte und fein strukturierte oder glatte Bleche.The WO 2013/150066 A1 discloses an electrical connection of a plurality of sheet metal layers of a honeycomb body to a connecting pin, the honeycomb body having a metal jacket with an inner circumference through which the connecting pin is passed in an electrically insulating manner in a bushing. The sheet layers are alternately arranged roughly structured and finely structured or smooth sheets.

Die CN 105 464 766 A offenbart ein Verfahren zur Herstellung eines elektrisch beheizbaren Trägerkörpers, wobei der Wabenkörper aus strukturierten und glatten Lagen gebildet ist. Der Träger weist einen Heizkern auf und einen Isolationskörper. Ein Lotmittel wird an dem Heizkern platziert während kein Lotmaterial am Isolationskörper platziert wird bevor die Lagen miteinander verbunden werden. Der Isolationskörper wird nach der Verlötung entfernt, wodurch ein elektrisch nichtleitender Bereich erzeugt wird.The CN 105 464 766 A. discloses a method for producing an electrically heatable carrier body, the honeycomb body being formed from structured and smooth layers. The carrier has a heating core and an insulation body. Solder is placed on the heater core while none Solder material is placed on the insulation body before the layers are joined together. The insulator is removed after soldering, creating an electrically non-conductive area.

Die JP H09 174179 A offenbart einen metallischen Wabenkörper, der dahingehend optimiert ist, dass die Wickelspannung beim Erzeugen des Wabenkörpers erhöht werden kann, um einen stabilen Körper zu erhalten. Hierzu werden im Herstellungsprozess ein spannungserzeugendes Werkzeug und ein spannungserfassendes Werkzeug eingesetzt.The JP H09 174179 A discloses a metallic honeycomb body which is optimized in that the winding tension can be increased when the honeycomb body is produced in order to obtain a stable body. For this purpose, a tension-generating tool and a tension-sensing tool are used in the manufacturing process.

Zur Einbringung eines Luftspalts in eine Wabenstruktur werden bisher oxidierte Glatt- und Wellfolien (oxidierte, zumindest teilweise strukturierte Metallfolien) in die Wabenstruktur mit eingewickelt, wobei diese dann nach dem Lötprozess wieder aus der Wabenstruktur entfernt werden.To introduce an air gap into a honeycomb structure, previously oxidized smooth and corrugated foils (oxidized, at least partially structured metal foils) are used in the honeycomb structure with, which are then removed from the honeycomb structure after the soldering process.

Dabei kann, aufgrund der elastischen Stapelung der Metallfolien, eine ungleichmäßige Spannungsverteilung in der Wabenstruktur vorliegen, die zu einer negativen Lötqualität führen kann (fehlende Verbindung von benachbart zu einander angeordneten Metallfolien). Weiter kann beim Entfernen dieser den Luftspalt erzeugenden Metallfolien aus der Wabenstruktur nach dem Lötprozess die Wabenstruktur beschädigt werden, so dass Reparaturmaßnahmen oder Neufertigung der Wabenstruktur erforderlich werden. Darüber hinaus ist das Entfernen dieser Metallfolien sehr zeitaufwendig und nicht reproduzierbar durchführbar. Eine Automatisierung des Herstellungsprozesses ist damit nur schwer möglich. Die entfernten Metallfolien sind nicht wieder einsetzbar und werden als Schrott entsorgt.Due to the elastic stacking of the metal foils, there may be an uneven stress distribution in the honeycomb structure, which can lead to a negative soldering quality (lack of connection of metal foils arranged adjacent to one another). Furthermore, when these metal foils producing the air gap are removed from the honeycomb structure after the soldering process, the honeycomb structure can be damaged, so that repair measures or new production of the honeycomb structure are necessary. In addition, the removal of these metal foils is very time-consuming and cannot be reproduced. Automation of the manufacturing process is therefore difficult. The removed metal foils cannot be used again and are disposed of as scrap.

Aufgabe der Erfindung ist es daher, die mit Bezug auf den Stand der Technik geschilderten Probleme zumindest teilweise zu lösen und insbesondere ein Verfahren zur Herstellung einer Wabenstruktur mit Luftspalt bereitzustellen, bei dem eine gleichmäßige Vorspannung in der Wabenstruktur vor und während eines Verbindungsprozesses gewährleistet ist, eine Zerstörung der Mittel zur Erzeugung des Luftspalts vermieden wird, der Prozess automatisierbar wird und eine Wiederverwendung der eingesetzten Mittel zur Erzeugung des Luftspalts ermöglicht wird.It is therefore an object of the invention to at least partially solve the problems described with reference to the prior art and, in particular, to provide a method for producing a honeycomb structure with an air gap, in which a uniform prestressing in the honeycomb structure is ensured before and during a connection process Destruction of the means for generating the air gap is avoided, the process can be automated and reuse of the means used for generating the air gap is made possible.

Diese Aufgaben werden gelöst mit einem Verfahren gemäß den Merkmalen des unabhängigen Patentanspruchs 1. Weitere vorteilhafte Ausgestaltungen der Erfindung sind in den abhängig formulierten Patentansprüchen angegeben. Es ist darauf hinzuweisen, dass die in den abhängig formulierten Patentansprüchen einzeln aufgeführten Merkmale in technologisch sinnvoller Weise miteinander kombiniert werden können und weitere Ausgestaltungen der Erfindung definieren. Darüber hinaus werden die in den Patentansprüchen angegebenen Merkmale in der Beschreibung näher präzisiert und erläutert, wobei weitere bevorzugte Ausgestaltungen der Erfindung dargestellt werden.These objects are achieved with a method according to the features of independent claim 1. Further advantageous configurations of the invention are specified in the dependent claims. It should be pointed out that the features listed individually in the dependent claims can be combined with one another in a technologically sensible manner and define further refinements of the invention. In addition, the features specified in the claims in the Description in more detail and explained, wherein further preferred embodiments of the invention are shown.

Vorgeschlagen wird in diesem Zusammenhang ein Verfahren zur Herstellung einer Wabenstruktur umfassend zumindest eine wenigstens teilweise strukturierte Metallfolie, wobei die Metallfolie in Teilbereichen der Wabenstruktur von einer benachbart angeordneten Metallfolie durch einen Luftspalt elektrisch isoliert beabstandet angeordnet ist, zumindest umfassend die folgenden Schritte:

  1. a. Bereitstellen der zumindest einen Metallfolie;
  2. b. Bereitstellen eines Formtellers mit einer Auflagefläche und mindestens einer sich in einer axialen Richtung von der Auflagefläche erstreckenden ersten Stegstruktur, wobei sich die erste Stegstruktur zudem in einer Ebene parallel zu der Auflagefläche erstreckt und den in der Wabenstruktur zu erzeugenden Luftspalt abbildet;
  3. c. Anordnen der zumindest einen Metallfolie auf der Auflagefläche zwischen der ersten Stegstruktur.
In this context, a method is proposed for producing a honeycomb structure comprising at least one at least partially structured metal foil, the metal foil being arranged in parts of the honeycomb structure so as to be electrically insulated from an adjacent metal foil by an air gap, at least comprising the following steps:
  1. a. Providing the at least one metal foil;
  2. b. Providing a molding plate with a support surface and at least one first web structure extending in an axial direction from the support surface, the first web structure also extending in a plane parallel to the support surface and representing the air gap to be generated in the honeycomb structure;
  3. c. Arranging the at least one metal foil on the support surface between the first web structure.

Hinsichtlich der Funktion und Anordnung eines Luftspalts zur Isolierung von Metallfolien und zur Führung eines Strompfads durch eine Wabenstruktur wird auf die eingangs angeführte WO 2013/150066 A1 verwiesen, die hiermit vollumfänglich in Bezug genommen wird.With regard to the function and arrangement of an air gap for the insulation of metal foils and for guiding a current path through a honeycomb structure, reference is made to the above WO 2013/150066 A1 referenced, which is hereby incorporated by reference in its entirety.

Es wird hier also ein Formteller vorgeschlagen, der eine erste Stegstruktur aufweist. Der Formteller und insbesondere die erste Stegstruktur sind aus einem temperaturfesten Werkstoff, z. B. einer Stahllegierung, einer Keramik oder ähnlichem hergestellt. Die Stegstruktur bildet bevorzugt den zu erzeugenden Luftspalt in der fertig hergestellten (also auch z. B. durch einen Lötprozess verbundenen) Wabenstruktur. Dazu weist die erste Stegstruktur, ausgehend von einer Auflagefläche des Formtellers, in der axialen Richtung eine Höhe auf, so dass die in der ersten Stegstruktur anzuordnenden Metallfolien weit genug in die erste Stegstruktur eintauchen können, so ein festgelegter Luftspalt entlang der axialen Richtung mit konstanter Breite erzeugbar ist. Die erste Stegstruktur erstreckt sich insbesondere in der axialen Richtung mit bevorzugt konstanter Höhe. Weiter erstreckt sich die Stegstruktur in einer Ebene parallel zur Auflagefläche, also quer zur axialen Richtung, insbesondere spiralförmig. So kann durch die Stegstruktur ein Strompfad in der Wabenstruktur vorgegeben werden.A molding plate is therefore proposed here which has a first web structure. The shaping plate and in particular the first web structure are made of a temperature-resistant material, e.g. B. a steel alloy, a ceramic or the like. The web structure preferably forms the air gap to be generated in the finished honeycomb structure (that is, for example, also connected by a soldering process). For this purpose, the first web structure, starting from a support surface of the shaping plate, has a height in the axial direction, so that the metal foils to be arranged in the first web structure can plunge far enough into the first web structure a fixed air gap along the axial direction can be generated with a constant width. The first web structure extends in particular in the axial direction with a preferably constant height. Furthermore, the web structure extends in a plane parallel to the support surface, that is to say transversely to the axial direction, in particular in a spiral shape. A current path in the honeycomb structure can thus be predetermined by the web structure.

In dem Schritt c. wird die zumindest eine Metallfolie auf der Auflagefläche und innerhalb der ersten Stegstruktur, also zwischen den Wänden der ersten Stegstruktur, angeordnet.In step c. the at least one metal foil is arranged on the support surface and within the first web structure, that is to say between the walls of the first web structure.

Weiter wird vorgeschlagen, dass in einem weiteren Schritt d. der Formteller zusammen mit der zumindest einen Metallfolie einem Verbindungsschritt zugeführt wird, in dem die zumindest eine Metallfolie untereinander zur dauerfesten Ausbildung der Wabenstruktur verbunden wird, wobei in einem darauffolgenden Schritt e. der Formteller mit der ersten Stegstruktur aus der Wabenstruktur entfernt wird.It is also proposed that in a further step d. the shaping plate is fed together with the at least one metal foil to a connecting step in which the at least one metal foil is connected to one another for the permanent formation of the honeycomb structure, in a subsequent step e. the molding plate with the first web structure is removed from the honeycomb structure.

Der Verbindungsschritt umfasst insbesondere einen Lötprozess, bevorzugt einen Lötprozess, bei dem bei Temperaturen von 800 bis 1200 °C [Grad Celsius] ein Lotmaterial aufgeschmolzen und die benachbart und einander berührenden Metallfolien an dafür vorgesehenen Positionen miteinander verbunden werden. Dieser Lötprozess ist für die Herstellung der hier beschriebenen Wabenkörper bekannt.The connecting step comprises in particular a soldering process, preferably a soldering process, in which a solder material is melted at temperatures of 800 to 1200 ° C. [degrees Celsius] and the adjacent and touching metal foils are connected to one another at positions provided for this purpose. This soldering process is known for the production of the honeycomb bodies described here.

Gemäß einer bevorzugten Weiterbildung weist der Formteller eine Mehrzahl von ersten Öffnungen auf, die sich in der axialen Richtung durch den Formteller erstrecken, wobei durch zumindest eine der ersten Öffnungen ein Stützstift durchführbar ist zur Anordnung in der Wabenstruktur nach Schritt c..According to a preferred development, the molding plate has a plurality of first openings which extend through the molding plate in the axial direction, a support pin being able to be passed through at least one of the first openings for arrangement in the honeycomb structure after step c.

Der Stützstift dient insbesondere zur Beabstandung von einem, und zur Fixierung der Wabenstruktur durch einen sogenannten Stützwabenkörper, der stromabwärts oder stromaufwärts von der Wabenstruktur in einer Fluid- (Abgas-)Leitung anordenbar ist.The support pin is used in particular for spacing one, and for fixing the honeycomb structure by a so-called Support honeycomb body, which can be arranged downstream or upstream of the honeycomb structure in a fluid (exhaust gas) line.

Der Stützstift wird hier insbesondere nur zur Kontrolle der Lage/der Position der hergestellten Wabenstruktur eingesetzt. So kann für spätere Prozessschritte sichergestellt werden, dass die Wabenstruktur mit anderen Stützwabenstrukturen reproduzierbar verbindbar ist.The support pin is used here in particular only for checking the position of the honeycomb structure produced. In this way, it can be ensured for later process steps that the honeycomb structure can be reproducibly connected to other supporting honeycomb structures.

Insbesondere wird in Schritt c. des Verfahrens zusätzlich eine Wickelspirale eingesetzt, die eine spiralförmige zweite Stegstruktur aufweist, die der ersten Stegstruktur entspricht; wobei die zweite Stegstruktur an einer dem Formteller zugewandten ersten Stirnseite in der axialen Richtung bündig abschließt, wobei die zweite Stegstruktur an der zweiten Stirnseite eine Steigung aufweist, wobei sich die zweite Stirnseite ausgehend von einem Zentrum der zweiten Stegstruktur entlang der spiralförmigen Windungen kontinuierlich der ersten Stirnseite annähert; und wobei die Wickelspirale zumindest zwei Stifte aufweist, die sich ausgehend von dem Zentrum weiter entlang der axialen Richtung erstrecken; wobei die zumindest eine Metallfolie zwischen den zwei Stiften aufgenommen wird und durch Drehung der Wickelspirale kontinuierlich in die zweite Stegstruktur aufgenommen und dann in die erste Stegstruktur überführt wird.In particular, in step c. the method additionally uses a winding spiral, which has a spiral-shaped second web structure which corresponds to the first web structure; wherein the second web structure is flush in the axial direction on a first end face facing the molding plate, wherein the second web structure has an incline on the second end side, the second end side continuously extending from the center of the second web structure along the spiral windings to the first end side approximates; and wherein the winding coil has at least two pins that extend further from the center along the axial direction; wherein the at least one metal foil is received between the two pins and is continuously taken up into the second web structure by rotation of the winding spiral and then transferred into the first web structure.

Die Wickelspirale ermöglicht insbesondere eine automatisierte Anordnung der mindestens einen Metallfolie in der ersten Stegstruktur. Dieser Vorgang wird in der folgenden Figurenbeschreibung genau erläutert. Ausgehend von einer ersten Stirnseite der Wickelspirale, die dem Formteller und der darauf angeordneten ersten Stegstruktur zugewandt ist, erstreckt sich eine zweite Stegstruktur spiralförmig, zum einen entlang einer Umfangsrichtung und in einer radialen Richtung von außen nach innen und zum anderen mit jeder Windung auch in der axialen Richtung. Die (komplette) zweite Stegstruktur schließt dabei bündig an der ersten Stirnseite ab, wobei die zweite Stegstruktur sich an der zweiten Stirnseite mit einer Steigung immer weiter entlang der axialen Richtung erstreckt, so dass ein Zentrum an der zweiten Stirnseite der zweiten Stegstruktur in einem größten Abstand von der ersten Stirnseite angeordnet ist. Die Steigung der spiraligen zweiten Stegstruktur ermöglicht, dass bei Drehung der Wickelspirale die eine Metallfolie (oder der Stapel von Metallfolien) ausgehend von dem Zentrum sukzessive spiralig aufwickelt wird und immer mehr Windungen (ausgehend von einer innersten Windung im Zentrum hin zu einer äußersten Windung) in der zweiten Stegstruktur aufgenommen werden.The winding spiral enables, in particular, an automated arrangement of the at least one metal foil in the first web structure. This process is explained in detail in the following description of the figures. Starting from a first end face of the winding spiral, which faces the shaping plate and the first web structure arranged thereon, a second web structure extends spirally, on the one hand along a circumferential direction and in a radial direction from the outside inwards and on the other hand with each turn also in the axial direction. The (complete) second web structure is flush with the first face, with the second web structure extends on the second face with a slope always further along the axial direction, so that a center on the second face of the second web structure is arranged at a greatest distance from the first face. The slope of the spiral second web structure enables the one metal foil (or the stack of metal foils) to be wound up successively spirally from the center as the winding spiral rotates and more and more turns (starting from an innermost turn in the center towards an outermost turn) in of the second web structure.

Die zweite Stegstruktur bildet dabei ebenfalls die vorbestimmten Luftspalte in der Wabenstruktur. Die zweite Stegstruktur entspricht zumindest im Wesentlichen der Form der ersten Stegstruktur (in einer Ebene quer zur axialen Richtung). Damit kann die mindestens eine Metallfolie von der Wickelspirale entlang der axialen Richtung in die erste Stegstruktur des Formtellers überführt und die Wickelspirale für den nächsten Wickelvorgang weiterverwendet werden.The second web structure also forms the predetermined air gaps in the honeycomb structure. The second web structure corresponds at least essentially to the shape of the first web structure (in a plane transverse to the axial direction). The at least one metal foil can thus be transferred from the winding spiral along the axial direction into the first web structure of the shaping plate and the winding spiral can be used further for the next winding process.

Insbesondere weist die Wickelspirale sich von der zweiten Stegstruktur an der ersten Stirnseite erstreckende Mitnehmerstifte auf, die sich in zweite Öffnungen in der ersten Stegstruktur und/oder im Formteller und/oder in erste Öffnungen im Formteller hinein erstrecken.In particular, the winding spiral has driver pins which extend from the second web structure on the first end face and which extend into second openings in the first web structure and / or in the molding plate and / or into first openings in the molding plate.

Diese Mitnehmerstifte stellen insbesondere eine fluchtende Anordnung von erster Stegstruktur und zweiter Stegstruktur sicher. Weiterhin kann so die Drehbewegung von Formteller und Wickelspirale zum Aufwickeln der mindestens einen Metallfolie gekoppelt werden.These driver pins ensure in particular an aligned arrangement of the first web structure and the second web structure. Furthermore, the rotary movement of the shaping plate and winding spiral can be coupled to wind up the at least one metal foil.

Weiter wird vorgeschlagen, in Schritt c. zudem ein Wickelteller einzusetzen, der einen sich spiralförmig erstreckenden Schlitz aufweist, der der zweiten Stegstruktur entspricht; wobei während der Drehung der Wickelspirale die Wickelspirale mit der zweiten Stegstruktur und beginnend mit dem Zentrum in den Schlitz eintaucht und so die zwischen dem Wickelteller und der Wickelspirale angeordnete zumindest eine Metallfolie sukzessive entlang der axialen Richtung in die Wickelspirale eingeführt und schließlich in die erste Stegstruktur überführt wird.It is also proposed in step c. also use a winding plate which has a spirally extending slot which corresponds to the second web structure; wherein during the rotation of the winding spiral, the winding spiral with the second web structure and beginning with the center dips into the slot and so the at least one metal foil arranged between the winding plate and the winding spiral is successively introduced along the axial direction into the winding spiral and finally transferred into the first web structure.

Der Wickelteller ist insbesondere eben ausgeführt, so dass die mindestens eine Metallfolie bevorzugt in ihrer gesamten Erstreckung entlang der axialen Richtung geführt wird.The winding plate is, in particular, flat, so that the at least one metal foil is preferably guided in its entire extent along the axial direction.

Insbesondere ist die Bewegung entlang der axialen Richtung mit der Drehung von Wickelteller und Formteller gekoppelt und/oder synchronisiert.In particular, the movement along the axial direction is coupled and / or synchronized with the rotation of the winding plate and the shaping plate.

Gemäß einer bevorzugten Ausgestaltung bildet die zumindest eine wenigstens teilweise strukturierte Metallfolie vor dem Anordnen in der ersten Stegstruktur einen mehrlagigen Stapel. Insbesondere ist eine Metallfolie zur Bildung eines Stapels mehrfach gefaltet. Es können aber auch mehrere, insbesondere unterschiedlich strukturierte (oder zumindest teilweise nicht strukturierte, also im Wesentlichen glatte) Metallfolien aufeinander zu einem Stapel angeordnet werden.According to a preferred embodiment, the at least one at least partially structured metal foil forms a multilayer stack before being arranged in the first web structure. In particular, a metal foil is folded several times to form a stack. However, several, in particular differently structured (or at least partially not structured, ie essentially smooth) metal foils can also be arranged on top of one another to form a stack.

Es wird weiter eine Wickelvorrichtung zur Durchführung eines erfindungsgemäßen Verfahrens vorgeschlagen, zumindest umfassend einen Formteller mit einer ersten Stegstruktur.A winding device for carrying out a method according to the invention is also proposed, at least comprising a shaping plate with a first web structure.

Insbesondere umfasst die Wickelvorrichtung weiter zumindest eine Wickelspirale mit einer zweiten Stegstruktur und einen Wickelteller.In particular, the winding device further comprises at least one winding spiral with a second web structure and a winding plate.

Die Erfindung sowie das technische Umfeld werden nachfolgend anhand der Figuren näher erläutert. Es ist darauf hinzuweisen, dass die Figuren besonders bevorzugte Ausführungsvarianten der Erfindung zeigen, diese jedoch nicht darauf beschränkt ist. Dabei sind gleiche Bauteile in den Figuren mit denselben Bezugszeichen versehen. Es zeigen schematisch:

Fig. 1:
einen Stapel Metallfolien in perspektivischer Ansicht;
Fig. 2:
einen Formteller in perspektivischer Ansicht;
Fig. 3:
eine Wabenstruktur und einen Formteller in perspektivischer Ansicht;
Fig. 4:
eine fertig hergestellte Wabenstruktur mit Luftspalt in perspektivischer Ansicht;
Fig. 5:
einen zweiten Formteller in perspektivischer Ansicht; und
Fig. 6:
eine Wickelvorrichtung in Explosionsdarstellung und in perspektivischer Ansicht.
The invention and the technical environment are explained in more detail below with reference to the figures. It should be pointed out that the figures show particularly preferred embodiment variants of the invention, but these are not restricted thereto is. The same components are provided with the same reference numerals in the figures. They show schematically:
Fig. 1:
a stack of metal foils in a perspective view;
Fig. 2:
a shaped plate in a perspective view;
Fig. 3:
a honeycomb structure and a mold plate in a perspective view;
Fig. 4:
a finished honeycomb structure with an air gap in a perspective view;
Fig. 5:
a second mold plate in a perspective view; and
Fig. 6:
a winding device in an exploded view and in a perspective view.

Fig. 1 zeigt einen Stapel 24 Metallfolien 2 in perspektivischer Ansicht und den Verfahrensschritt a. Fig. 1 shows a stack 24 of metal foils 2 in a perspective view and the method step a.

Fig. 2 zeigt einen Formteller 5 in perspektivischer Ansicht und den Verfahrensschritt b. Der Formteller 5 weist eine erste Stegstruktur 8 auf. Die erste Stegstruktur 8 bildet den zu erzeugenden Luftspalt 4 in der fertig hergestellten (also auch z. B. durch einen Lötprozess verbundenen) Wabenstruktur 1 (siehe Fig. 4). Dazu weist die erste Stegstruktur 8, ausgehend von der Auflagefläche 6 des Formtellers 5, in der axialen Richtung 7 eine Höhe auf, so dass die in der ersten Stegstruktur 8 anzuordnenden Metallfolien 2 weit genug in die erste Stegstruktur 8 eintauchen können, so ein festgelegter Luftspalt 4 entlang der axialen Richtung 7 mit konstanter Breite erzeugbar ist (siehe Fig. 3). Die erste Stegstruktur 8 erstreckt sich in einer Ebene 9 parallel zur Auflagefläche 6, also quer zur axialen Richtung 7. So kann durch die erste Stegstruktur 8 ein Strompfad in der Wabenstruktur 1 vorgegeben werden. Weiter weist der Formteller 5 eine Mehrzahl von ersten Öffnungen 10 auf, die sich in der axialen Richtung 7 durch den Formteller 5 erstrecken, wobei durch zumindest eine der ersten Öffnungen 10 ein Stützstift 11 durchführbar ist zur Anordnung in der Wabenstruktur 1 nach Schritt c. Fig. 2 shows a molding plate 5 in a perspective view and the method step b. The shaping plate 5 has a first web structure 8. The first web structure 8 forms the air gap 4 to be generated in the finished honeycomb structure 1 (see also, for example, connected by a soldering process) (see Fig. 4 ). For this purpose, the first web structure 8, starting from the support surface 6 of the shaping plate 5, has a height in the axial direction 7, so that the metal foils 2 to be arranged in the first web structure 8 can penetrate far enough into the first web structure 8, according to a defined air gap 4 can be generated along the axial direction 7 with a constant width (see Fig. 3 ). The first web structure 8 extends in a plane 9 parallel to the support surface 6, that is to say transversely to the axial direction 7 Web structure 8, a current path in the honeycomb structure 1 can be specified. Furthermore, the molding plate 5 has a plurality of first openings 10 which extend through the molding plate 5 in the axial direction 7, wherein a support pin 11 can be passed through at least one of the first openings 10 for arrangement in the honeycomb structure 1 after step c.

Fig. 3 zeigt einen Formteller 5 und eine darauf angeordnete Wabenstruktur 1 in perspektivischer Ansicht und Verfahrensschritt c. Die erste Stegstruktur 8 erstreckt sich hier in der axialen Richtung 7 mit konstanter Höhe. Die erste Wabenstruktur 1 umfasst hier eine Mehrzahl von wenigstens teilweise strukturierten Metallfolien 2, wobei einzelne Metallfolien 2 in Teilbereichen 3 der Wabenstruktur 1 von einer benachbart angeordneten Metallfolie 2 durch einen Luftspalt 4 elektrisch isoliert beabstandet angeordnet sind. Fig. 3 shows a shaped plate 5 and a honeycomb structure 1 arranged thereon in a perspective view and method step c. The first web structure 8 extends here in the axial direction 7 with a constant height. The first honeycomb structure 1 here comprises a plurality of at least partially structured metal foils 2, individual metal foils 2 being arranged in partial regions 3 of the honeycomb structure 1 so as to be electrically insulated from an adjacent metal foil 2 by an air gap 4.

In diesem Zustand werden in einem weiteren Schritt d. der Formteller 5 zusammen mit der zumindest einen Metallfolie 2 einem Verbindungsschritt zugeführt, in dem die zumindest eine Metallfolie 2 untereinander zur dauerfesten Ausbildung der Wabenstruktur 1 verbunden wird.In a further step d. the molding plate 5, together with the at least one metal foil 2, is fed to a connecting step in which the at least one metal foil 2 is connected to one another for the permanent formation of the honeycomb structure 1.

Fig. 4 zeigt eine fertig hergestellte Wabenstruktur 1 mit Luftspalt 4 in perspektivischer Ansicht. In Schritt e. ist der Formteller 5 mit der ersten Stegstruktur 8 aus der Wabenstruktur 1 entfernt worden. Fig. 4 shows a finished honeycomb structure 1 with an air gap 4 in a perspective view. In step e. the molding plate 5 with the first web structure 8 has been removed from the honeycomb structure 1.

Fig. 5 zeigt einen zweiten Formteller 5 in perspektivischer Ansicht. Die Ausführungen zu Fig. 2 gelten entsprechend. Hier ist ebenfalls eine Mehrzahl von ersten Öffnungen 10 vorgesehen, die sich in der axialen Richtung 7 durch den Formteller 5 erstrecken. Die erste Stegstruktur 8 umfasst mehrere Windungen 18 und weist weiter zweite Öffnungen 21 auf, in die sich Mitnehmerstifte 20 der Wickelspirale 12 erstrecken können (siehe Fig. 6). Fig. 5 shows a second mold plate 5 in a perspective view. The comments on Fig. 2 apply accordingly. Here, too, a plurality of first openings 10 are provided, which extend through the shaping plate 5 in the axial direction 7. The first web structure 8 comprises a plurality of windings 18 and also has second openings 21, into which driver pins 20 of the winding spiral 12 can extend (see Fig. 6 ).

Fig. 6 zeigt eine Wickelvorrichtung 25 in Explosionsdarstellung und in perspektivischer Ansicht. Die hier gezeigte Wickelvorrichtung 25 wird in Schritt c. des Verfahrens eingesetzt. Die Wickelvorrichtung 25 umfasst eine Aufnahme 26 die in zumindest in einer Umfangsrichtung 27 antreibbar ist. Weiter umfasst die Wickelvorrichtung 25 einen Formteller 5, eine Wickelspirale 12 sowie einen Wickelteller 22. Fig. 6 shows a winding device 25 in an exploded view and in a perspective view. The winding device 25 shown here is in step c. of the procedure used. The winding device 25 comprises a receptacle 26 which can be driven in at least one circumferential direction 27. The winding device 25 further comprises a shaping plate 5, a winding spiral 12 and a winding plate 22.

Die Wickelspirale 12 weist eine spiralförmige zweite Stegstruktur 13 auf, die der ersten Stegstruktur 8 auf dem Formteller 5 entspricht; wobei die zweite Stegstruktur 13 an einer dem Formteller 5 zugewandten ersten Stirnseite 14 in der axialen Richtung 7 bündig abschließt, wobei die zweite Stegstruktur 13 an der zweiten Stirnseite 15 eine Steigung 16 aufweist. Die zweite Stirnseite 15 nähert sich, ausgehend von einem Zentrum 17 der zweiten Stegstruktur 13 entlang der spiralförmigen Windungen 18 kontinuierlich der ersten Stirnseite 13 an; und wobei die Wickelspirale 12 zumindest zwei Stifte 19 aufweist, die sich ausgehend von dem Zentrum 17 weiter entlang der axialen Richtung 7 erstrecken. Der Stapel 24 von Metallfolien 2 wird zwischen den zwei Stiften 19 aufgenommen und durch Drehung der Wickelspirale 12 kontinuierlich in die zweite Stegstruktur 13 aufgenommen und dann in die erste Stegstruktur 8 überführt.The winding spiral 12 has a spiral-shaped second web structure 13 which corresponds to the first web structure 8 on the shaping plate 5; the second web structure 13 ends flush on the first end face 14 facing the shaping plate 5 in the axial direction 7, the second web structure 13 having an incline 16 on the second end face 15. Starting from a center 17 of the second web structure 13, the second end face 15 continuously approaches the first end face 13 along the spiral windings 18; and wherein the winding spiral 12 has at least two pins 19 which extend further from the center 17 along the axial direction 7. The stack 24 of metal foils 2 is received between the two pins 19 and continuously taken up into the second web structure 13 by rotating the winding spiral 12 and then transferred into the first web structure 8.

Die Wickelspirale 12 ermöglicht so eine automatisierte Anordnung der mindestens einen Metallfolie 2 in der ersten Stegstruktur 8. Ausgehend von einer ersten Stirnseite 14 der Wickelspirale 12, die dem Formteller 5 und der darauf angeordneten ersten Stegstruktur 8 zugewandt ist, erstreckt sich eine zweite Stegstruktur 13 spiralförmig, zum einen entlang einer Umfangsrichtung 27 und in einer radialen Richtung 28 von außen nach innen und zum anderen mit jeder Windung 18 auch in der axialen Richtung 7. Die komplette zweite Stegstruktur 13 schließt dabei bündig an der ersten Stirnseite 14 ab, wobei die zweite Stegstruktur 13 sich an der zweiten Stirnseite 15 mit einer Steigung 16 immer weiter entlang der axialen Richtung 7 erstreckt, so dass ein Zentrum 17 an der zweiten Stirnseite 15 der zweiten Stegstruktur in einem größten Abstand von der ersten Stirnseite 14 angeordnet ist. Die Steigung 16 der spiraligen zweiten Stegstruktur 13 ermöglicht, dass bei Drehung der Wickelspirale 12 die eine Metallfolie 2 (bzw. der Stapel 24 von Metallfolien 2) ausgehend von dem Zentrum 17 sukzessive spiralig aufwickelt wird und immer mehr Windungen 18 (ausgehend von einer innersten Windung 18 im Zentrum 17 hin zu einer äußersten Windung 18) in der zweiten Stegstruktur 13 aufgenommen werden.The winding spiral 12 thus enables an automated arrangement of the at least one metal foil 2 in the first web structure 8. Starting from a first end face 14 of the winding spiral 12, which faces the shaping plate 5 and the first web structure 8 arranged thereon, a second web structure 13 extends in a spiral , on the one hand along a circumferential direction 27 and in a radial direction 28 from the outside inwards and on the other hand with each turn 18 also in the axial direction 7. The complete second web structure 13 is flush with the first end face 14, the second web structure 13 along the second end face 15 with an incline 16 the axial direction 7, so that a center 17 on the second end face 15 of the second web structure is arranged at a greatest distance from the first end face 14. The slope 16 of the spiral second web structure 13 enables the one metal foil 2 (or the stack 24 of metal foils 2) to be wound up successively from the center 17 when the winding spiral 12 rotates and more and more turns 18 (starting from an innermost turn 18 in the center 17 towards an outermost turn 18) in the second web structure 13.

Die zweite Stegstruktur 13 bildet dabei ebenfalls die vorbestimmten Luftspalte 4 in der Wabenstruktur 1. Die zweite Stegstruktur 13 entspricht zumindest im Wesentlichen der Form der ersten Stegstruktur 8 (in einer Ebene 9 quer zur axialen Richtung 7). Damit kann die mindestens eine Metallfolie 2 von der Wickelspirale 12 entlang der axialen Richtung 7 in die erste Stegstruktur 8 des Formtellers 5 überführt und die Wickelspirale 12 für den nächsten Wickelvorgang weiterverwendet werden.The second web structure 13 likewise forms the predetermined air gaps 4 in the honeycomb structure 1. The second web structure 13 corresponds at least substantially to the shape of the first web structure 8 (in a plane 9 transverse to the axial direction 7). The at least one metal foil 2 can thus be transferred from the winding spiral 12 along the axial direction 7 into the first web structure 8 of the shaping plate 5 and the winding spiral 12 can be used further for the next winding process.

Hier weist die Wickelspirale 12 sich von der zweiten Stegstruktur 13 an der ersten Stirnseite 14 in der axialen Richtung 7 erstreckende Mitnehmerstifte 20 auf, die sich in zweite Öffnungen 21 in der ersten Stegstruktur 8 und/oder im Formteller 5 und/oder in erste Öffnungen 10 im Formteller 5 hinein erstrecken.Here, the winding spiral 12 has driver pins 20 which extend from the second web structure 13 on the first end face 14 in the axial direction 7 and which extend into second openings 21 in the first web structure 8 and / or in the shaping plate 5 and / or in first openings 10 extend into the molding plate 5.

Diese Mitnehmerstifte 20 stellen eine fluchtende Anordnung von erster Stegstruktur 8 und zweiter Stegstruktur 13 sicher. Weiterhin kann so die Drehbewegung von Aufnahme 26, Formteller 5 und Wickelspirale 12 zum Aufwickeln der mindestens einen Metallfolie 2 gekoppelt werden.These driver pins 20 ensure an aligned arrangement of the first web structure 8 and the second web structure 13. Furthermore, the rotary movement of receptacle 26, shaping plate 5 and winding spiral 12 can be coupled in this way for winding up the at least one metal foil 2.

Hier ist weiter ein Wickelteller 22 gezeigt, der einen sich spiralförmig erstreckenden Schlitz 23 aufweist, der der zweiten Stegstruktur 13 entspricht. Die Wickelspirale 12 taucht während der Drehung der Wickelspirale 12 mit der zweiten Stegstruktur 13 und beginnend mit dem Zentrum 17 in den Schlitz 23 ein und überführt so die zwischen dem Wickelteller 22 und der Wickelspirale 12 angeordnete zumindest eine Metallfolie 2 sukzessive entlang der axialen Richtung 7 in die Wickelspirale 12 und schließlich in die erste Stegstruktur 8.Here, a winding plate 22 is further shown, which has a spirally extending slot 23, which corresponds to the second web structure 13. The winding spiral 12 dips during the rotation of the winding spiral 12 with the second web structure 13 and starting with the center 17 into the slot 23 and thus transfers the at least one metal foil 2 arranged between the winding plate 22 and the winding spiral 12 successively along the axial direction 7 into the winding spiral 12 and finally into the first web structure 8.

Der Wickelteller 22 ist hier eben ausgeführt, so dass die mindestens eine Metallfolie 2 im Wesentlichen in ihrer gesamten Erstreckung entlang der axialen Richtung 7 geführt wird.The winding plate 22 is of flat design here, so that the at least one metal foil 2 is guided essentially in its entire extent along the axial direction 7.

Claims (10)

  1. Method for producing a honeycomb structure (1) comprising at least one at least partially structured metal foil (2), wherein, in subregions (3) of the honeycomb structure (1), the metal foil (2) is arranged spaced apart from an adjacently arranged metal foil (2) so as to be electrically insulated by an air gap (4), at least comprising the following steps:
    a. providing the at least one metal foil (2);
    b. providing a forming plate (5) with a bearing surface (6) and with at least one first web structure (8) extending from the bearing surface (6) in an axial direction (7), wherein the first web structure (8) also extends in a plane (9) parallel to the bearing surface (6) and images the air gap (4) to be produced in the honeycomb structure (1);
    c. arranging the at least one metal foil (2) on the bearing surface (6) in the first web structure (8).
  2. Method according to Claim 1, wherein, in a further step d., the forming plate (5) is sent, together with the at least one metal foil (2), to a connection step in which interconnection of the at least one metal foil (2) is realized for the permanent formation of the honeycomb structure (1), wherein, in a following step e., the forming plate (5) with the first web structure (8) is removed from the honeycomb structure (1).
  3. Method according to Claim 2, wherein the connection step comprises a soldering process.
  4. Method according to one of the preceding claims, wherein the forming plate (5) has a plurality of first openings (10) which extend through the forming plate (5) in the axial direction (7), wherein a support pin (11) is able to be passed through at least one of the first openings (10) for the purpose of arrangement in the honeycomb structure (1) according to step c.
  5. Method according to one of the preceding claims, wherein, in step c. of the method, use is additionally made of a winding spiral (12) which has a spiral-shaped second web structure (13) which corresponds to the first web structure (8), wherein the second web structure (13) terminates in a flush manner in the axial direction (7) at a first end side (14) facing the forming plate (5), wherein the second web structure (13) has a pitch (16) at the second end side (15), wherein, proceeding from a center (17) of the second web structure (13), the second end side (15) continuously approaches the first end side (14) along the spiral-shaped windings (18), and wherein the winding spiral (12) has at least two pins (19), which extend further along the axial direction (7) proceeding from the center (17), wherein the at least one metal foil (2) is received between the at least two pins (19) and, by rotation of the winding spiral (12), continuously received into the second web structure (13) and then transferred into the first web structure (8).
  6. Method according to Claim 5, wherein the winding spiral (12) has driving pins (20) which extend from the second web structure (13) at the first end side (14) and which extend into second openings (21) in the first web structure (8) and/or in the forming plate (5) and/or into first openings (10) in the forming plate (5).
  7. Method according to Claim 5 or 6, wherein, in step c., use is also made of a winding plate (22) which has a slot (23) extending in a spiral-shaped manner and corresponding to the second web structure (13), wherein, during the rotation of the winding spiral (12), the winding spiral (12) sinks into the slot (23) with the second web structure (13) and starting with the center (17), and thus the at least one metal foil (2), arranged between the winding plate (22) and the winding spiral (12), is, along the axial direction (7), gradually introduced into the winding spiral (12) and, finally, transferred into the first web structure (8).
  8. Method according to one of the preceding claims, wherein, prior to being arranged in the first web structure (8), the at least one at least partially structured metal foil (2) forms a multi-layered stack (24).
  9. Winding device (25) for implementing a method according to one of Claims 1 to 8, at least comprising a forming plate (5) with a first web structure (8).
  10. Winding device (25) according to Claim 9, wherein the winding device (25) furthermore comprises at least one winding spiral (12) with a second web structure (13), and a winding plate (22).
EP17726272.2A 2016-06-09 2017-05-24 Method for producing a honeycomb structure Active EP3469196B1 (en)

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DE102016210235.4A DE102016210235A1 (en) 2016-06-09 2016-06-09 Process for producing a honeycomb structure
PCT/EP2017/062599 WO2017211592A1 (en) 2016-06-09 2017-05-24 Method for producing a honeycomb structure

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EP (1) EP3469196B1 (en)
JP (1) JP6622429B2 (en)
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DE102022213319B3 (en) 2022-12-08 2024-03-21 Vitesco Technologies GmbH Device for exhaust gas aftertreatment and method for producing it

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KR20190003760A (en) 2019-01-09
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US20200340385A1 (en) 2020-10-29
JP2019521273A (en) 2019-07-25
CN109154226B (en) 2021-01-05
US11078820B2 (en) 2021-08-03
WO2017211592A1 (en) 2017-12-14
CN109154226A (en) 2019-01-04
JP6622429B2 (en) 2019-12-18
KR102130238B1 (en) 2020-07-03

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