EP1180203A1 - Corps en nids d'abeilles et son procede de fabrication - Google Patents

Corps en nids d'abeilles et son procede de fabrication

Info

Publication number
EP1180203A1
EP1180203A1 EP00938545A EP00938545A EP1180203A1 EP 1180203 A1 EP1180203 A1 EP 1180203A1 EP 00938545 A EP00938545 A EP 00938545A EP 00938545 A EP00938545 A EP 00938545A EP 1180203 A1 EP1180203 A1 EP 1180203A1
Authority
EP
European Patent Office
Prior art keywords
sheet metal
honeycomb body
metal layers
stiffening elements
body according
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.)
Withdrawn
Application number
EP00938545A
Other languages
German (de)
English (en)
Inventor
Helmut Swars
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.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP1180203A1 publication Critical patent/EP1180203A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F01N3/2817—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates only with non-corrugated sheets, plates or foils
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/34—Chemical or biological purification of waste gases
    • B01D53/74—General processes for purification of waste gases; Apparatus or devices specially adapted therefor
    • B01D53/86—Catalytic processes
    • B01D53/88—Handling or mounting catalysts
    • B01D53/885—Devices in general for catalytic purification of waste gases
    • B01J35/56—
    • 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
    • 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
    • F01N3/2814—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates all sheets, plates or foils being corrugated
    • 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
    • F01N3/2821—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates the support being provided with means to enhance the mixing process inside the converter, e.g. sheets, plates or foils with protrusions or projections to create turbulence
    • 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
    • F01N2240/00—Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being
    • F01N2240/20—Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being a flow director or deflector
    • 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
    • F01N2260/00—Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/18—Exhaust treating devices having provisions not otherwise provided for for improving rigidity, e.g. by wings, ribs
    • 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
    • F01N2330/02—Metallic plates or honeycombs, e.g. superposed or rolled-up corrugated or otherwise deformed sheet metal
    • F01N2330/04—Methods of manufacturing
    • 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
    • F01N2330/32—Honeycomb supports characterised by their structural details characterised by the shape, form or number of corrugations of plates, sheets or foils
    • 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
    • F01N2330/32—Honeycomb supports characterised by their structural details characterised by the shape, form or number of corrugations of plates, sheets or foils
    • F01N2330/322—Corrugations of trapezoidal 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
    • F01N2330/00—Structure of catalyst support or particle filter
    • F01N2330/30—Honeycomb supports characterised by their structural details
    • F01N2330/32—Honeycomb supports characterised by their structural details characterised by the shape, form or number of corrugations of plates, sheets or foils
    • F01N2330/323—Corrugations of saw-tooth or triangular 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
    • F01N2330/00—Structure of catalyst support or particle filter
    • F01N2330/30—Honeycomb supports characterised by their structural details
    • F01N2330/38—Honeycomb supports characterised by their structural details flow channels with means to enhance flow mixing,(e.g. protrusions or projections)
    • 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
    • F01N2330/40—Honeycomb supports characterised by their structural details made of a single sheet, foil or plate
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/1234—Honeycomb, or with grain orientation or elongated elements in defined angular relationship in respective components [e.g., parallel, inter- secting, etc.]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/1241—Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]

Definitions

  • the invention relates to a honeycomb body, in particular a catalyst carrier body, according to the preamble of claim 1 and a method for its production.
  • a generic honeycomb body which consists of alternately arranged corrugated and smooth sheet metal layers.
  • the flow channels which have a sinusoidal or triangular cross section, are unfavorable with regard to the catalytic function, since the gussets of the channels are practically ineffective, particularly in the case of laminar flows.
  • the alternating temperature properties of the honeycomb body are unfavorable, since the flat soldering of the smooth and corrugated foils creates a very rigid honeycomb structure.
  • the invention has for its object to provide a honeycomb body which has sufficient stability with high thermal shock resistance, which allows a flow-technically favorable design of the flow channels and which is simple and inexpensive to manufacture.
  • this object is achieved by a honeycomb body with the features of claim 1. Because the expansion of the stiffening elements, which run essentially parallel to the sheet metal layers, transverse to their longitudinal extension is small compared to the extension of the honeycomb structure in this direction, the mass transfer within the flow channels and thus also the effective reaction cross section of the channels is practically not reduced . Unfavorable cross-sectional geometries due to the formation of gussets practically do not arise or only in small volume ranges. Furthermore, due to their orientation parallel to the sheet metal layers, the stiffening elements can simply be introduced into the honeycomb structure during the production thereof. A certain stiffening is already achieved by limiting the minimum distance between adjacent sheet metal layers to one another in structured sheets, so that e.g.
  • the stiffening elements can prevent elongation of the honeycomb structure in a direction perpendicular to the flow channels or sheet metal profiles, which would lead to an undesirable formation of free spaces between sheet metal layers of different elongation and thus to unfavorable vibration stresses on the honeycomb structure.
  • the honeycomb body according to the invention can be constructed practically from sheet metal of any structure or orientation due to the introduced stiffening elements, since it is no longer necessary to fasten the sheet metal layers to one another.
  • the stiffened areas of the honeycomb structure can have a punctiform or locally isolated extension or can form stiffening zones in the case of stiffening elements of a corresponding length.
  • the stiffening elements according to the invention fix the metal sheets more strongly in relation to one another, which results in larger areas of the honeycomb structure which are highly flexible.
  • the length of the stiffening elements irrespective of their direction of extension, is equal to or greater than the transverse extent of a channel in one direction, for example the height or width, and for example bridging a flow channel, i.e. on opposite sides Attack the walls of a duct or the housing.
  • the stiffening elements can also extend transversely to the longitudinal direction of the channel only over several channel diameters, for example 5-10 channel diameters, or over the entire width of the honeycomb body. In the case of non-isometric or non-isogonal channels, the stiffening elements can also only extend over a part of the channel cross-section which is a multiple, for example twice or more, of the channel extension in the cross-sectional direction of small extent.
  • the expansion of the stiffening elements transverse to their longitudinal direction is small compared to the expansion of the flow channels in this direction, e.g. in the range of 1/10 to 1/50 of the dimensioning of the flow channels in this direction or below, without being limited to this.
  • the transverse extension of the stiffening elements can, for. B. if these run across or at an angle to the channels, be 1/100 to 1/1000 or less of the channel length.
  • the width of the stiffening elements can only be 0.5 to 10 times, preferably 1 to 5 times the thickness of the sheets that form the honeycomb structure for the same material, without being limited to this.
  • Is z. B a honeycomb body with a flow channel length of 100 mm and a flow channel diameter of 1 mm in front, can be arranged transversely to the flow channels arranged ribbon-shaped stiffening elements with a width of a few millimeters and / or stiffening wires with a diameter of a few hundredths to a few tenths of a millimeter. If the stiffening elements are arranged in the longitudinal direction of the channels, their width can be in the range from 0.01 to 0.5 mm, preferably 0.003 to 0.2 mm.
  • the stiffening elements can have correspondingly larger diameters or widths.
  • stiffening elements can also be assigned to one sheet or to a pair or a plurality of adjacent sheets.
  • the stiffening elements preferably extend in their longitudinal direction over the entire honeycomb structure.
  • the stiffening elements are designed to be elastically deformable perpendicular to their longitudinal direction, in particular in the direction of the flow channels, under operating conditions.
  • the stiffening elements can run between mutually adjacent sheet metal layers, they can also penetrate profiled sheet metal layers or be braided into flat metal sheets and / or connect adjacent metal sheets to one another.
  • the stiffening elements are advantageously connected to the sheet-metal layers and / or to the housing in the longitudinal direction thereof, e.g. through suitable joining techniques such as welded connections, positive, frictional and / or material connection.
  • a connection of the stiffening elements in particular to the sheet metal layers can, however, also be achieved by coating with a ceramic material which is necessary for producing a catalytic coating.
  • the stiffening elements can be braided into the sheet metal layers, in particular by connecting two adjacent sheet metal layers to one another, or clamped into corresponding sheet metal folds. Sub-areas can be used for this the sheets are released or the stiffening elements are inserted into the folds of connecting webs arranged on the end faces of the sheets.
  • the structured areas such as, for example, the sheet metal corrugations can also be provided with notches or protrusions extending in the longitudinal direction of the channels, which, if necessary arranged in succession with a height offset, form a passage for wires or the like running parallel to the flow channels.
  • the dimensional stability of the honeycomb body is already increased if the stiffening elements loosely support the sheets or loosely by one, e.g. through suitable profiles, or several sheets are carried out.
  • the stiffening elements can also be connected to one another by additional stiffening or connecting struts, in particular if they are arranged at the level of a sheet metal layer or between the sheet metal layers, which struts can each run essentially parallel to and / or perpendicular to the sheet metal layers.
  • additional stiffening or connecting struts in particular if they are arranged at the level of a sheet metal layer or between the sheet metal layers, which struts can each run essentially parallel to and / or perpendicular to the sheet metal layers.
  • extensive associations of stiffening elements can be built up, which can extend in two or three dimensions over larger areas or over the entire extent of the honeycomb body.
  • expanded metal layers or wire mesh can also be inserted between the sheet metal layers to stiffen the honeycomb structure, which layers can be inserted, in particular, into indentations in sheet metal layer profiles and, if necessary, can be fixed here so that they cannot move.
  • the stiffening elements are advantageously connected to the sheet metal layers under axial prestress. As a result, both the rigidity of the honeycomb body can be increased and the geometry of the flow channels or the dimension of the honeycomb body can be calibrated.
  • the stiffening elements can be attached to the housing of the honeycomb body as well as to existing partitions, which act as rigid support walls or as elastically deformable partitions, which, for. B. are composed of folding areas of the sheet metal layers are executed.
  • the folding areas can be U-shaped, V-shaped, W-shaped or Z-shaped without being limited to this, individual or more folding legs being connected to one another to form the wall.
  • the folding structure of the partition walls makes them flexible and, at the same time, compressible to widen them, which results in good resistance to temperature changes.
  • the prestressed areas of the corresponding metal sheets can be combined in sections. This makes it possible, for. B. block-shaped areas of high preload and thus high rigidity, which are separated by areas of low preload and thus increased deformability.
  • Such a formation of prestressed areas within the honeycomb structure can be produced in that the fastening means on the sheet metal layers for fastening the stiffening elements are only provided in certain areas.
  • the connecting webs in the case of zigzag-folded sheet metal strips can be removed in certain areas in the lateral edge areas of the honeycomb body, as a result of which an area of increased extensibility is provided adjacent to the housing and a honeycomb body with particularly favorable mechanical properties results.
  • the cross-sectional geometry of the flow channels can be adjusted by prestressing stiffening elements attached to the sheet metal layers.
  • the stiffening elements can be formed from partial sections of the sheet metal layers.
  • the honeycomb body is formed by a sheet metal strip folded in a zigzag shape
  • the individual sheet metal layers in the folding area are connected to one another by web-like connection points.
  • the connecting webs in the folding area can be produced by punching out, the folding line of the adjacent folding sections of the sheet metal strip running through the punching out.
  • the punching can be carried out in such a way that a web running on the fold line remains, so that the wall regions of a flow channel lying opposite one another along the fold line are connected to one another.
  • the web extending through the cross section of a flow channel can be shortened in the longitudinal direction thereof by a corresponding bending or folding.
  • stiffening elements can also be provided, which are designed as insert pieces that can be inserted into the end faces of the channels.
  • the insert pieces the outer contour of which can be adapted to the cross-sectional geometry of the channels, prevent adjacent sheet metal layers from being pushed into one another without significantly influencing the flow cross section of the channels.
  • the insert pieces can be designed such that, in the inserted state, they have areas protruding from the front of the honeycomb body, which act as flow control devices. The areas which can be formed in one piece can allow a lateral inflow into the inflow area of the honeycomb body and / or can be set at an angle to the longitudinal direction of the honeycomb body.
  • the insert pieces can be designed as separate components, advantageously the insert pieces extend over the width, possibly also over the height, of a plurality of channels, or over the entire width and / or height of the honeycomb structure. Stiffened areas of the honeycomb structure can alternate with areas of increased elasticity. By arranging insert pieces differently on both end faces of the honeycomb body, twistable honeycomb bodies can be obtained, for example, which is advantageous for certain fields of application can. If the inserts extend over several channels, they can be arranged both parallel and perpendicular or at an angle to the sheet metal layers.
  • the inserts can also be integrally formed on the sheet metal layers and z. B. generated by suitable folding of sheet metal sections. By deforming the sheet ends or by punching the insert pieces can be designed according to the requirements.
  • the flow cross sections can be varied in a simple manner over the length of the flow channels. It is thus possible to profile the inserts in such a way that the flow channel diameter in the turbulent inflow area of the channels has a smaller diameter than the channel areas in the interior of the honeycomb body with laminar flow.
  • the inflow area is divided into a plurality of flow channels, so that the sum of the flow cross sections of the channels in the inflow area corresponds approximately to the flow cross section of the channel in the central honeycomb area.
  • the stiffening elements can be designed as webs extending along the flow channels.
  • the webs have a considerably smaller width than the profiles that are otherwise available for producing the honeycomb structure, e.g. a quarter or an eighth of the same or less.
  • the two folding legs can lie against one another, advantageously over almost the entire height, or they can be spaced from one another such that the coating composition used in each case does not penetrate into the space between the legs.
  • the webs can extend over the entire height of the channels or advantageously only over part of the same. ben, so that gas exchange between the sub-channels is possible.
  • the webs can also have notches with which adjacent sheet metal layers are supported or which serve to enlarge the catalytically active area.
  • the notches or the webs themselves can serve to fasten or support further stiffening elements, such as, for example, wires running transversely to these.
  • the webs can, in particular, be designed as folding webs of the sheet metal layers, the folding webs having flanged areas at their ends or in the central region, which counteract a spreading of the folding webs, for additional stabilization. Additional wires or the like can also be inserted into the folding webs.
  • the folding webs can, for example, protrude from the sheet metal layers in a direction obliquely or perpendicular to the main sheet metal layer or run essentially parallel to the sheet layers and, for example, be bent laterally so that sheet metal layer duplications or multiple layers with, for example, 3-10 or more folds occur, which also, in particular in the case of smooth sheet metal layers, can be spaced from the honeycomb end faces.
  • individual web-shaped sections of the sheet metal layers can also be released and joined to one another to form stiffening elements with one another or with the sheet metal layers to absorb tensile force.
  • the joints within a single sheet layer can be generated by any joining techniques, e.g. B. by spot welding, in particular positive connections can be generated by punched and folded sheet metal areas which engage in an adjacent flow channel or through corresponding openings provided for this purpose or are non-positive with the wall of a flow channel.
  • stiffening elements of various designs can be provided which extend perpendicular to the sheet metal layers and connect two or more sheet metal layers to one another.
  • a vertical extension is generally understood to be one that has a vertical directional component and an oblique course, e.g. at an angle of 45 ° to the sheet metal layers.
  • the vertical stiffening elements can be designed as rigid supporting walls, preferably they are designed to be elastically deformable, one-dimensional stiffening elements in the form of wires, strips, interconnected sheet metal folds or the like, or two-dimensional elements as deformable outer or intermediate walls, which in particular consist of folded sections the sheet layers exist, can be provided.
  • the stiffening elements which extend parallel to the sheet metal layers can be fastened to the stiffening elements which extend vertically to the sheet metal layers, or can be carried out loosely through them or guided past them.
  • the stiffening elements are arranged upstream or in the inflow region of the flow channels, ie in the region of turbulent flow.
  • the stiffening elements which in particular can extend transversely to the flow channels, thus simultaneously form additional catalytically active surfaces.
  • protruding with catalytically active surfaces can also be arranged by other measures.
  • the stiffening elements in the inflow area which can also be designed as strips or wires, can have a larger diameter than in the area of laminar flow.
  • the inflow region reinforced with stiffening elements can also have sheet-metal layer sections with free-standing ends, which allow a lateral inflow of fluid over one or more sides.
  • stiffening elements are arranged in front of the end faces of the flow channels, it has proven to be advantageous if the distance from the outer edge of the stiffening elements facing away from the flow channels to the end faces of the flow channels is in the range of 0.1 to 3 times the diameter of the channels.
  • the sheets are connected to one another by folding webs which lie on folding lines arranged in front of the end faces of the channels, for the distance of the folding lines from the front edge of the inlet and / or outlet openings of the channels. This applies regardless of whether stiffening elements are arranged in the folding areas or not.
  • the channel ends can be shaped like a blade.
  • window-like sheet metal folds can also be provided at the channel ends.
  • the honeycomb body according to the invention can be constructed not only from a zigzag-shaped profiled sheet metal strip but also from individual profiled sheets, between which, if necessary, unstructured sheets can also be arranged.
  • individual sheet metal layers can also be arranged one above the other in such a way that the flow channels are produced by the profiling of sheet metal layers lying opposite one another.
  • the stiffening elements can also be spaced apart from the end faces of the honeycomb body be provided.
  • FIG. 1 shows schematically and in cross section perpendicular to the longitudinal axis of the honeycomb body a cuboid honeycomb body with a honeycomb structure 11 consisting of only a partial honeycomb in a housing 10.
  • the honeycomb structure consists of thin sheet metal strip with simple, wave-shaped sheet metal sections 13 which are layered one above the other. On the two long sides of the partial honeycomb, the sections 13 are constructed with their free ends 14 by bending at an angle of approximately 90 degrees to outer wall regions 22, which are firmly connected at their ends 16 to the housing 10 by means of the beads 17.
  • Wires 30 for stabilizing the honeycomb structure are inserted between every second sheet metal layer, and their ends 30a are firmly bound into the two lateral outer wall regions of the partial honeycomb. Furthermore, diagonal wires 33 are braided into the honeycomb structure to stabilize the honeycomb structure.
  • FIG. 2a shows a section of a honeycomb body in cross-section from flat, sheet-metal layers 13a, b, c, which are layered and have a trapezoidal structure and are connected to one another at their folding ends by webs 34. Hexagonal flow channels are formed by sheet metal layers lying opposite one another. The honeycomb structure is stabilized by wires running parallel to the sheet metal layers 13a, b, c.
  • the wire 30 arranged in the folding line is clamped in the folding webs 34, the wire 31 is loosely guided through the perforations 35a at an intermediate height of the sheet metal layer and the wire 32 on the upper edge of the sheet layer a with the aid of the perforations 35b with a Height offset with each corrugation braided into the sheet and fixed to it by friction.
  • the individual wires 30, 31, 32 can alternatively or simultaneously be provided in the honeycomb structure, the wires 31, 32 can also run obliquely to the corrugations.
  • FIG. 2b shows a corresponding section from a honeycomb structure made of thin sheet metal layers which are layered and have a simple, wave-shaped or sinusoidal structure, the stabilization being effected by the wires 30, 31, 32 as described in FIG. 2a.
  • Figure 3 shows a section of a honeycomb body consisting of a zigzag-shaped sheet metal strip 12a with corrugated sheet layers 13a, 13b and 13c.
  • the stiffening element is a folding web integrally molded onto the sheet metal layers
  • the folding web 37 which protrudes outwards from the end faces of the flow channels 38 and runs parallel to the central plane of the flow channels 38.
  • the folding web 37 which is separated from the corrugated wall 39 of the flow channel by an incision or a punched-out portion, points at the level of each flow channel
  • the folding point 36 can be formed together with the corrugation of the sheet metal layers 13a, 13b and 13c or starting from a curved folding web. Additional stabilizing wires 30 are clamped into the folding web 37, which extends continuously over all or part of the honeycomb body.
  • FIG. 4 shows a section of the honeycomb structure according to FIG. 3 in the only partially folded state, the sheet metal indentation for forming the folding point 36 being recognizable.
  • Figure 5 shows a section of an originally smooth thin sheet metal strip for producing a honeycomb body according to the invention.
  • grooves 41 running in the lengthwise direction of the strip are warmly embossed by means of embossing rollers or laser beams.
  • Folding lines 40 run perpendicular to this in order to enable a zigzag-shaped folding of the sheet metal strip into a stack.
  • the height of the folding lines 40 are narrow webs 42 of a width b formed by punched-out areas 43 with an extension a in the longitudinal direction of the band.
  • the extent a determines the entry openings of the individual channels of the finished honeycomb structure with regard to their height or the maximum width of stiffening elements which are inserted between the webs.
  • Adjacent to the sheet metal sections 12a areas can also remain in the punched-out areas, by means of which stiffening elements running perpendicular or parallel to the sheets can be fastened in a form-fitting manner.
  • Figure 6 shows a vertical longitudinal section through a honeycomb body according to the invention.
  • Flow channels through which an exhaust gas can flow in the flow direction S are built up by two channels of the sheet metal strip 12a placed one above the other.
  • narrow thin bands 34a are held in the fold lines 40 and are held by the webs 42.
  • the webs 42 are arranged in front of the inlet openings E and are widened in cross section by the inserted strips, which provides a catalytically effective arrangement.
  • the folding web 42 connecting the sheet metal layers 13a, 13b can have a certain height h, so that the sheet metal layers 13a, 13b are spaced apart from one another.
  • a correspondingly dimensioned strip or profile piece can be inserted between the sheet metal layers 13a, 13b; notches can also be provided on the sheet metal layers, which are supported on the opposite sheet metal layer.
  • the structure according to FIG. 7, on the left can be produced by rectangular punchings 43b and the formation of folding lines or deformation zones as well as subsequent folding and compression of the sheet metal layers.
  • a honeycomb body with an essentially right angular flow channels 38 are built.
  • folding lines 41 are introduced into the sheet metal strip.
  • the webs 42 connecting the sheet metal layers 13a, 13b and 13c, created by rectangular openings 43 in the sheet metal strip 12a, are cut on both sides at the fold lines, so that sheet sections 44 connected on one side to the webs 42 result, which are folded in to stabilize the inflow region in the flow channel .
  • the sheet metal sections 44 can be used to fasten wires which are parallel or perpendicular to the sheet metal layers 13a, 13b and 13c.
  • the sheet-metal layers 13a, 13b, 13c are placed on top of one another with webs 45 arranged one above the other and aligned parallel to one another.
  • the angled sheet metal sections 49 then encompass the web 45 of the sheet metal layer arranged below it, so that adjacent sheet metal layers are positively connected to one another by stiffening wires 31, the wires 31 arranged above the sheet metal sections 49 being guided through the incisions 47 and the upper region of the adjacent web 49.
  • the webs 45 are cut on the upper side to form tabs 45b, which are inserted into the fold of the web 45 arranged above and are non-positively fixed therein. This creates partitions 45a within the honeycomb structure, which additionally stabilize the honeycomb structure as stiffening zones.
  • the base of the flow channels 38 with provided notches 45c, which serve the gas exchange between adjacent flow channels and / or the support at the base of the underlying flow channel.
  • FIG. 9 shows a further variant of stabilizing the honeycomb structure with wires 50, which simultaneously connect adjacent sheet metal layers 51a, 51b.
  • some of the corrugations 52 of the sheet metal layers are incised at intervals, so that after upsetting these corrugations, regions 55 protruding upwards and regions 56 bent downwards alternately result.
  • the areas 55 of adjacent sheet metal layers, which engage in the areas 56 are arranged in alignment with one another, as shown in FIG.
  • the wire 50 like the sheet metal strip, is folded in a zigzag shape, but it may also only extend over one sheet layer.
  • wires 59 extending perpendicular to them are provided, which are arranged at the level of the incisions delimiting the areas 57, 58 and are laterally delimited by them.
  • the wires 59 are also connected to the folding legs 53 laterally delimiting the sheet metal layers 51a, 51b, which are also connected to one another by joining technology, so that a closed side wall results.
  • the wires 59 are pretensioned to increase the rigidity of the honeycomb body, as a result of which the honeycomb body can be calibrated by adjusting the corresponding pre-tensioning of the wires 59 while the electrical heating of the honeycomb body is carried out in regions.
  • wires 54 are provided which run perpendicular to the sheet metal layers and penetrate the compressed corrugations and are connected to the wires 59.
  • FIG. 10 shows how the cross section of the flow channels is calibrated or changed by prestressed wires 61, which are drawn into a profiled sheet metal layer 62 can be.
  • the wire 61 is drawn halfway through the corrugated sheet layer 62 and fixed to the sheet sheet layer at the end thereof.
  • the wavy shape of the sheet metal layer 62 represented by the solid line can be converted into the shape 63 shown in dashed lines or shown next to it, the wire 61 being prestressed.
  • stiffening elements can also be provided which run through the sheet metal layers transversely to their corrugation at several different heights, e.g. B. at 1/4, 1/2 and 3/4 of the height of the same, whereby different channel cross sections can be generated.
  • wires 65 can be clamped between the webs 64, the ends of the wires 65 being incorporated in the side walls constructed by folding the end regions 66 of the sheet metal layers.
  • the end regions of the sheet metal layers 66 are provided with notches 68, which are used to fasten the honeycomb body to the housing 67.
  • tapes can also be clamped into the folding webs 64, which tapes can be fixed to the housing 67.
  • the sheet metal layers 70 can have a vertical offset in a central partial area, the offset lines 71 of adjacent sheet metal layers being able to be arranged on a plane 72 which preferably runs parallel to the flow direction. If the height offset, as shown in the figure, is the height a of a sheet metal layer, then the wires 73 run loosely between over the other half of the sheet metal layer over half the width of a sheet metal layer at the level of the webs 74, in which they are clamped in a tension-absorbing manner adjacent sheet metal layers 70a, 70b. The ends of the wires 73 are incorporated in the side walls built up by the sheet ends.
  • the width of the honeycomb body can be calibrated or changed by exerting tension on the wires 73. In this case, by exerting tensile forces on only every second of the wires 73, it can only be targeted the right or only the left half of the sheet layer is calibrated or deformed.
  • the height offset of the sheet metal layers can also be twice the sheet layer height b, as a result of which the length of the expansion legs 76 is increased. As a result, the areas of the honeycomb body separated by the expansion legs can be decoupled in terms of force.
  • 13 (left) shows stiffening elements in the form of insert pieces 80, which are each integrally formed on the two ends of the sheet metal layers 81a and can be inserted into the flow channel formed by the sheet metal layers 81b, 81c and can be fixed in a frictionally locking manner.
  • 13 (right) shows a front view of such a sheet metal layer.
  • the lateral end regions of the sheet metal layer 81a are provided with folds 82 which can be connected to corresponding sheet folds located above or below the sheet metal layers and can be fixed to beads of the corresponding housing.
  • FIG. 14 shows an embodiment in which the honeycomb body is constructed from identical sheet metal sections 90a, b, c, each of which has two corrugated sections 92, 93 which are connected to one another via a kink region 91 and on whose free ends the insert pieces 95 are integrally formed via the connecting webs 94 are.
  • the two insert pieces 95 are arranged on the same side of the sheet metal section 90, so that when the sheet metal sections 90 are rotated relative to one another by 180 °, the insert pieces of the adjacent sheet metal layers can engage on the end face in the flow channel 96 formed by the sheet metal section 90.
  • FIG. 15 shows an embodiment with a separate insert 100, which extends in height over several flow channels of a sheet metal strip 101 which is laid in a zigzag shape and can engage in the end face thereof.
  • a corresponding insert can also be inserted at the opposite end of the deposited sheet metal strip become.
  • the contour of the insert cloths corresponds to that of the flow channels, but this is not necessary.
  • FIG. 16 shows an embodiment in which, in addition to the stiffening wires 111 provided between the individual sheet layers 110, additional stiffening webs 112 are provided in the form of sheet metal doublings which simultaneously serve as flow ribs, the height of the webs being approximately half the height of the flow channels 113 indicated by dashed lines exhibit.
  • the sheet metal layers forming rectangular flow channels are arranged congruently to one another, the wires 111 preventing the troughs of a sheet metal layer from slipping into the depressions in the sheet metal layer located underneath.
  • the sheet metal layers can also be placed in opposite directions to one another, so that the stiffening webs of a first sheet metal layer lie opposite those of the second sheet metal layer and flow ducts of twice the height are created.
  • FIG. 17 shows a zigzag-shaped sheet metal strip 115 with heart-shaped flow channels 116, which are divided by the stiffening webs 117 produced from double layers. As indicated by the dashed circles, three flow channels 114 are combined to form a larger flow channel, thereby enabling gas exchange. Adjacent sheet metal layers 118, 119 are connected to one another by the connecting webs 120. For additional stiffening, the corner regions 121 of the stiffening webs 117 are flanged and in the region of the double layering of the adjacent side walls of adjacent flow channels by making incisions in flanged regions 122.
  • the stiffening webs 117 also have notches 123 extending into the flow channel, by means of which the catalytically active area in the flow channels is increased.
  • the flanges of the stiffening webs 117 and the regions 122 form isolated stiffening elements which elongate the honeycomb structure in a direction transverse to the flow channels and prevent parallel to the sheet layers.
  • the flanges can be provided both on the end faces of the flow channels and in the interior thereof.
  • Figure 18 shows a zigzag-shaped sheet metal strip 130, in which the height h of the almost rectangular corrugations 131 is a multiple of the width b of the same (approx. 4: 1).
  • the corrugations are laterally offset from one another by a partial amount of the width thereof and opened in the direction of the sheet metal layer lying opposite.
  • the individual corrugations inclined towards the sheet-metal layer plane are connected to one another by the connecting webs 132 (see enlarged detail according to FIG. 18, right).
  • Figure 18 (below) shows the sheet metal strip before it is folded.
  • an offset of the upper and lower apexes 134, 135 of the sheet metal corrugations is achieved, so that the lower apex of a sheet metal corrugation above the open side of the flow channel of the underlying sheet metal layer is arranged.
  • the offset y defines the frontal inclination or the axial offset of the upper apex to the lower end edge of the sheet metal corrugations.
  • gaps extending between opposing corrugations extend over the entire width of the honeycomb body, so that a media exchange over the entire width of the honeycomb body is also provided by the gaps arranged next to one another. Since the punched-out sections can generally be designed differently along a folding line, the width of the honeycomb body, via which a media exchange in the transverse direction is possible, can be set. Stiffening wires, not shown, are drawn in between the sheet layers.
  • Figure 19 shows a meandering sheet metal strip 140 with almost rectangular corrugations, in which the lower vertices 141 of a sheet layer are arranged above the open sides 142 of the sheet layer below.
  • Stands have the sheet metal layers with the formation of legs on a height offset 143, which extends over an integer multiple of the height h of the corrugations, the legs are connectable to partition walls.
  • the stiffening wires 144 arranged perpendicular to the corrugations rest on flattened areas 145, which are produced by slots or indented grooves cut into the sheet metal layers, so that the lower apex 141 of a sheet metal layer is arranged below the upper apex 146 of the underlying sheet metal layer.
  • the connecting wires 144 are guided through sheet metal duplications 147, which are provided by notched sheet metal sections on the end faces or within the flow channels. Furthermore, web-like notches 148 running in the longitudinal direction of the flow channels are provided, which are supported on the opposite side wall of the flow channel and at the same time enable gas exchange through the openings 149.
  • FIG. 20 shows a further embodiment of a honeycomb body in the cutout, which has an asymmetrical cross section of the flow channels 151 with respect to the plane of the sheet metal layers 150.
  • the sheet metal strip 152 is provided in the area of the folding lines 154 with rectangular punched-out areas 155, along the diagonal of which the folding line runs.
  • folding webs 156 running in the longitudinal direction of the flow channels are provided, which are supported with their notches 157 on the stiffening wires 158, instead of which layers of expanded metal or wire mesh can also be provided.
  • stiffening wires 159 are clamped in the connecting webs of the sheet metal layers. With a suitable height of the folding webs, these can also be supported directly on the wires.
  • FIG. 21 shows a section of a honeycomb body with a meandering sheet metal strip 251 and expanded metal layers 258 extending transversely thereto, the ends of which protrude beyond the individual sheet layers 257 are folded over the respective sheet layer ends and in the adjacent intervene in the flow channel.
  • the end regions 262 of the expanded metal layers 258 are then perpendicular to the opposite sheet metal layers 257 and are supported or support them.
  • each of the sheet metal layers of the sheet metal strip has two stiffening ribs 253, 254 running transversely to the direction of flow indicated by the arrows, the length of the folding webs 255 being long compared to the sheet metal layer spacing.
  • the sheet metal sections 256 lying in the folding area are notched out laterally and at the same time serve to fasten the honeycomb body to a housing (not shown).
  • the expanded metal layers 258 have sections 259 which extend in the longitudinal direction of the flow channel and are placed on the face of the sheet metal layers and which are perpendicular to the sheet metal layers and support the sheet metal layer lying above them.
  • the sections 259 are provided with lateral bulges 260 to increase the rigidity when the compressive forces are exerted vertically on the sheet metal layers, and are guided through the ribs 253 without play in vertical gaps.
  • the sheet metal sections 259 can also have areas with a lower height, which can be arranged between the bulges 260 and enable fluid exchange.
  • the sheet metal sections 259 are connected to one another by intersecting connecting webs 261 which are integrally formed on one another at the crossing points and which can be produced by making incisions in the sheet metal layers and which also enable fluid exchange in the transverse direction.
  • connecting webs 261 which are integrally formed on one another at the crossing points and which can be produced by making incisions in the sheet metal layers and which also enable fluid exchange in the transverse direction.
  • these can, like the sheet metal layers 257, be connected to form an endless meandering expanded metal strip.
  • the expanded metal layers also serve to enlarge the active catalyst area.
  • expanded metal layers 287 can be inserted between the individual sheet metal layers 277 with a corrugated profile, whereby the spacing of the sheet metal layers can also be set as desired.
  • the one-piece expanded metal layers In this case, elongate sections 289 in the form of narrow strips, which are arranged perpendicular to the main planes of the sheet metal layers, and connecting webs 291 which are connected to one another via intersection points. The intersection points are inserted in recesses 290 in the sheet metal layers and can be additionally secured here, for example by Solder connections or by stiffening wires extending vertically to the sheet metal layers.
  • the expanded metal layers can be fixed on the lateral folding webs of the sheet metal layers. Corresponding to the sheet metal strip, the expanded metal layers can also be designed as a meandering strip.
  • the flow-around profiles 289 simultaneously improve the pollutant conversion in the channels.
  • FIG. 23 shows a honeycomb body 160 which is provided in a housing 161 with gas inlet 162 and gas outlet 163.
  • the flow channels 164 of the honeycomb body are flowed at obliquely.
  • the individual sheet metal layers of the honeycomb body are connected to one another at the inflow and outflow area by a separate insert piece 165, which at the same time are shaped at their free ends by the arrangement of beveled areas 166 such that the inlet opening into the flow channels is larger in the flow direction is the cross section of the flow channels in a plane perpendicular to their longitudinal direction.
  • the catalytic effectiveness of the honeycomb body can be increased in the inlet region of the gas to be cleaned into the flow channels or pressure losses due to turbulence can be reduced in the outlet region.
  • the inflow and outflow areas of the honeycomb body are e.g. stabilized by increasing the wall thickness, whereas in the central area of the honeycomb the channels remain unchanged with a larger cross-section, e.g. with gaps extending over the entire width, which are less stable but allow fluid exchange across the honeycomb body unhindered.
  • Figures 24 and 25 illustrate that by appropriate shaping of the punched 170 and incisions 171, the in In the exemplary embodiment shown are diamond-shaped or V-shaped, the end regions 169 of the individual flow channels can be structured such that they have a different cross-section or contour on the end side than the regions of the flow channels spaced from the ends of the honeycomb body or the envelope of the end region of the entire honeycomb body, which is the case, for example, if the end faces of the flow channels are not perpendicular to the longitudinal direction of the flow channel.
  • the flow conditions in front of the inflow areas into the flow channels, which are defined by the protruding sheet metal sections 172, 173, and their position can thereby be determined, so that the inflow areas of the honeycomb body can be adapted to the respective requirements.
  • means 175 are provided before or after the inflow and / or outflow region of a structural body (cf. also FIGS. 3, 26), which extend axially from the honeycomb or Projecting structure end faces 176 (as shown in Figure 25 below) and cause a flow deflection of the medium with respect to the main flow direction within the structure body or its longitudinal direction.
  • the flow deflection can take place, for example, in the manner of a macroscopic change in flow direction (see, for example, FIGS. 22, 26) or else, for example, in the manner of a swirling, such as at the front or deflection edges 175 of the incisions in FIG. 25, below.
  • the means can be assigned separately to each flow channel or flow path.
  • the extent of the means in the flow direction can be small compared to the length of the structural body, for example in the range of a few (for example 10) or less than a channel or flow path diameter. There is thus a continuous or gradual change in the flow conditions through structural elements in the inflow region of the structural body over a depth starting from the front envelope 177 of the above flow deflecting means over a certain depth, for example 0.5 to 10 (without being limited to this) Flow channel widths or the distances between the core flows, ie the flow paths of the highest flow speeds, can correspond.
  • the Means can be formed in one piece on the sheet metal layers, for example produced by the incisions described above or by axially extending structured or flat sheet metal layers, or can be designed as separate components, for example in the form of axially extending wires.
  • the means can be arranged centrally to flow channels or flow paths with the highest flow speed or in each case between them.
  • the axial protrusion of the flow deflecting means relates to the front face or front face envelope 178 of the honeycomb body, which defines the beginning of the individual flow channels or flow paths, which result from a division of the total flow hitting the structure body into partial flows, in the inflow region of the structure body.
  • the above means can accordingly also be provided in the case of honeycomb bodies with a conically shaped end face, which can be produced, for example, by telescoping a wound band.
  • the means can also be implemented, if appropriate, in the case of structural bodies without stiffening elements according to the invention, if appropriate also in the case of structural bodies with partially or completely unhindered fluid exchange in one or two transverse directions.
  • the free ends of the protruding regions can form an angle between 150-20 °, preferably 90-30 °, with the end region lying centrally between them.
  • the inlet areas 180 in the honeycomb body in which a turbulent gas flow prevails, can be formed in a blade-like manner, increasing the inner deflection radius of the flow threads, and in order to enlarge the inflow opening of the flow channels and to align them approximately perpendicularly to the flow direction indicated by the arrows 181, and staggered axially.
  • flattened areas 183 are provided at the end of the flow channel ends facing away from the flow direction, which increase the deflection radius, wherein slots 184 are made in the opposite areas and the free ends 185, 186 are bent outwards until they approximate with the flattened areas of the opposite Flow channel come to the plant.
  • the folding webs 187 which are reinforced and thickened by inserted tapes, are angled in the direction of the inflow direction and thereby act as front guide vanes. A correspondingly opposite shape can be provided in the outflow area of the honeycomb body.
  • FIG. 27 shows an arrangement of sheet metal layers 263 with folding webs 267 which extend along the flow direction to stiffen the honeycomb structure and to increase the conversion.
  • the sheet-metal layer sections 264a, 265a of the end regions 264, 265 of the honeycomb body are angled relative to the central region 266, for which purpose incisions are made in the folding webs 267. This reduces pressure losses in the inflow region of the honeycomb body when the flow to the sheet metal layers 263 is oblique.
  • the sheet-metal layers are supported at the level of the incisions and in the inflow regions by stiffening wires 269 inserted in the webs 267 and extending transversely to the direction of flow. Furthermore, stiffening wire wires 268 running perpendicular to the sheet metal layers 263 are provided, which are partially connected to the wires 269.
  • FIG. 28 shows a cuboid honeycomb body made of individual sheets 277 with triangular grooves 279 and flow channels which extend over the entire width of the sheet layers and which can also be designed isometrically.
  • each of the channels 279 is provided at its ends with a chamfer 280 pointing towards the free end of the honeycomb body, which is angled toward the flow direction.
  • the front end regions 281 of the sheet metal layers 277 are provided with stiffening flanges 282, into which additional stiffening wires 283 are clamped.
  • bands 284 are provided which run transversely to the sheet metal layers 277 and are deposited on the upper edges of the grooves 279 and support the sheet metal layer arranged above them.
  • the trough-shaped Profiling of the sheet metal layers 277 is interrupted by a flattened region 86 which extends over the entire width of the sheet metal layer and runs at the level of the upper edge of the groove 279 and into which stiffening wires 287 are braided.
  • the flow channels 279 are continued with a lateral and a vertical offset (see arrow 287), so that the fluid carried in one channel area is forcibly mixed with fluid carried in adjacent channel areas.
  • FIG. 29 shows a honeycomb body consisting of three partial honeycombs 190a, b, c, which is fastened in the housing 192 via the beads 191.
  • the partial honeycombs are each generated by a zigzag-shaped sheet metal strip, stiffening wires 193 or sheets being inserted between the individual sheet layers.
  • Figure 29 (center) shows an enlarged end view of the honeycomb structure. According to this, in the area hatched in FIG. 29 (top), the webs 194 connecting the individual sheet metal layers are clamped, as a result of which a comparatively rigid structure is created.
  • the connecting webs have been removed, so that the sheet metal layers can be formed in an arc shape by means of the reinforcing wires or sheets set back from the end plane in this area, in that the corrugation apices can shift relative to one another in layers without sliding into one another.
  • Figure 30 a, b, c shows stiffening elements 25, 26, 27 and 28 in the form of multiple folds of simple sheet metal layers 21a, 21b, which can be flat or profiled, for example corrugated.
  • the broachable folding areas separated by folding lines are advantageously compressed, so that the adjacent folding tion sections lie flat against each other.
  • the multiple folds provide additional stiffening elements in the form of wires 29a or spirals 29b that run perpendicular to the sheet metal layers.
  • honeycomb bodies provided with stiffening elements according to the invention can also have stacks of strongly curved sheet metal layers, e.g. then arise when entire stacks of sheet metal layers are folded or entwined around a central crease line.
  • the stiffening elements can follow the bending of the sheet metal layers and, if necessary, be connected to them in a manner that increases the absorption.
  • the stiffening elements according to the invention can be essentially rigid, but in particular also elastic, the elasticity being smaller or, with a corresponding arrangement, greater than that of the sheet metal layers.
  • the elastic properties can relate to the honeycomb body under operating conditions; they are advantageously present in the entire range between operating and room temperature.

Abstract

L'invention concerne un corps en nids d'abeilles, en particulier un corps de support de catalyseur, présentant une structure en nids d'abeilles constituée d'une pluralité de canaux s'étendant dans le sens longitudinal du corps en nids d'abeilles et pouvant être traversés par un fluide. Ce corps en nids d'abeilles présente des tôles (13a) structurées, disposées les unes sur les autres, en couche plane ou incurvée, et au moins un élément de rigidification (30) qui s'étend sensiblement au moins partiellement de façon parallèle aux tôles. Pour que l'on obtienne un corps en nids d'abeilles qui présente une stabilité suffisante et également une grande résistance aux changements de température, qui permette une configuration des canaux d'écoulement la plus favorable possible en ce qui concerne la mécanique des fluides, et qui, en outre, soit d'une fabrication simple et bon marché, il est proposé d'insérer des éléments de rigidification dans ledit corps en nids d'abeilles, éléments dont l'étendue, transversalement par rapport à leur longueur, est plus petite que l'allongement de la structure en nids d'abeilles dans ce sens.
EP00938545A 1999-05-14 2000-05-12 Corps en nids d'abeilles et son procede de fabrication Withdrawn EP1180203A1 (fr)

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DE19922357A DE19922357C1 (de) 1999-05-14 1999-05-14 Wabenkörper und Verfahren zu dessen Herstellung
DE19922357 1999-05-14
PCT/DE2000/001488 WO2000070205A1 (fr) 1999-05-14 2000-05-12 Corps en nids d'abeilles et son procede de fabrication

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EP (1) EP1180203A1 (fr)
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Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19922356C2 (de) * 1999-05-14 2001-06-13 Helmut Swars Wabenkörper
JP3685106B2 (ja) * 2001-08-08 2005-08-17 トヨタ自動車株式会社 排気浄化装置
DE102004001419A1 (de) * 2003-05-30 2004-12-16 Emitec Gesellschaft Für Emissionstechnologie Mbh Herstellung eines strukturierten Bleches für Abgasbehandlungseinrichtungen
DE102005034137A1 (de) * 2005-07-19 2007-01-25 Behr Gmbh & Co. Kg Wärmeübertrager
EP1913324B1 (fr) * 2005-07-19 2011-09-14 Behr GmbH & Co. KG Echangeur thermique
CN102798123B (zh) * 2011-05-26 2016-05-04 中山炫能燃气科技股份有限公司 一种红外线金属发热体及其制作方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2733640C3 (de) * 1977-07-26 1981-04-30 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co KG, 7000 Stuttgart Matrix für einen katalytischen Reaktor zur Abgasreinigung bei Brennkraftmaschinen
US4348360A (en) * 1979-11-05 1982-09-07 Minnesota Mining And Manufacturing Company Catalytic converter for ozone removal in aircraft
DE3517035C1 (de) 1985-05-11 1986-10-30 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co KG, 7000 Stuttgart Matrix fuer einen katalytischen Reaktor zur Abgasreinigung
EP0245738B1 (fr) * 1986-05-12 1989-08-09 INTERATOM Gesellschaft mit beschränkter Haftung Corps métallique en forme de nid d'abeilles, en particulier support pour catalyseur, avec paroi de support, et son procédé de fabrication
SE461018B (sv) 1987-07-06 1989-12-18 Svenska Emmisionsteknik Ab Katalysatorbaerare
DE3726072A1 (de) 1987-08-06 1989-02-16 Thyssen Edelstahlwerke Ag Loet-verfahren
US4793136A (en) * 1987-08-26 1988-12-27 W. R. Grace & Co. Reinforced metallic honeycomb structure
JP2813679B2 (ja) * 1989-05-08 1998-10-22 臼井国際産業株式会社 排気ガス浄化装置
WO1992002714A1 (fr) * 1990-07-30 1992-02-20 Emitec Gesellschaft Für Emissionstechnologie Mbh Corps en nid d'abeilles a chauffage electrique, notamment corps de support de catalyseur, a structures internes de support
US5525309A (en) * 1991-01-31 1996-06-11 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb body with a plurality of disks braced against one another
FR2683854A1 (fr) 1991-11-19 1993-05-21 Ecia Equip Composants Ind Auto Structure de support d'au moins un materiau de catalyse des gaz d'echappement d'un moteur notamment de vehicule automobile.
BR9306740A (pt) * 1992-07-14 1998-12-08 Emitec Emissionstechnologie Corpo de colmeia metálico de camadas de chapas entrelaçadas e processo para sua fabricação
US5948504A (en) * 1993-01-21 1999-09-07 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Electrically insulating supporting structure capable of metallic bonding, process for producing the same, electrically heatable catalytic converter and electrically conductive honeycomb body using the same
DE9317050U1 (de) * 1993-11-08 1995-03-09 Emitec Emissionstechnologie Mechanisch stabilisierte Heizkatalysatoranordnung
CZ289693B6 (cs) 1994-04-11 2002-03-13 Scambia Industrial Developments Katalyzátor na katalytické oąetření výfukových plynů
JP3802592B2 (ja) * 1995-10-13 2006-07-26 株式会社ユタカ技研 金属製触媒担体
US6036926A (en) * 1995-10-20 2000-03-14 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Honeycomb body of sheet metal layers with reinforcing structures and catalytic reactor having the honeycomb body
DE19539168A1 (de) 1995-10-20 1997-04-24 Emitec Emissionstechnologie Wabenkörper aus Blechlagen mit Verstärkungsstrukturen

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO0070205A1 *

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US6537681B1 (en) 2003-03-25
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