EP2755741A1 - Honeycomb element with reinforced corners - Google Patents
Honeycomb element with reinforced cornersInfo
- Publication number
- EP2755741A1 EP2755741A1 EP12773022.4A EP12773022A EP2755741A1 EP 2755741 A1 EP2755741 A1 EP 2755741A1 EP 12773022 A EP12773022 A EP 12773022A EP 2755741 A1 EP2755741 A1 EP 2755741A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- thickness
- corner
- monolithic
- section
- elements
- 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- Withdrawn
Links
- 239000011148 porous material Substances 0.000 claims abstract description 11
- 239000004568 cement Substances 0.000 claims description 17
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 15
- 239000007789 gas Substances 0.000 claims description 12
- 239000011499 joint compound Substances 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 9
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 3
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 3
- 239000000470 constituent Substances 0.000 claims description 2
- 239000013589 supplement Substances 0.000 claims description 2
- 241000264877 Hippospongia communis Species 0.000 description 17
- 238000001914 filtration Methods 0.000 description 14
- 229910010271 silicon carbide Inorganic materials 0.000 description 11
- 230000002093 peripheral effect Effects 0.000 description 10
- 239000004071 soot Substances 0.000 description 9
- 239000000919 ceramic Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 239000002245 particle Substances 0.000 description 7
- 238000011144 upstream manufacturing Methods 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 238000005299 abrasion Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 229910000505 Al2TiO5 Inorganic materials 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- AABBHSMFGKYLKE-SNAWJCMRSA-N propan-2-yl (e)-but-2-enoate Chemical compound C\C=C\C(=O)OC(C)C AABBHSMFGKYLKE-SNAWJCMRSA-N 0.000 description 3
- 230000008929 regeneration Effects 0.000 description 3
- 238000011069 regeneration method Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 229910000287 alkaline earth metal oxide Inorganic materials 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 2
- 229910052878 cordierite Inorganic materials 0.000 description 2
- 239000002283 diesel fuel Substances 0.000 description 2
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 229910004298 SiO 2 Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000009849 deactivation Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229920000609 methyl cellulose Polymers 0.000 description 1
- 239000001923 methylcellulose Substances 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000003361 porogen Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
- C04B38/0006—Honeycomb structures
- C04B38/0009—Honeycomb structures characterised by features relating to the cell walls, e.g. wall thickness or distribution of pores in the walls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2482—Thickness, height, width, length or diameter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2455—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure of the whole honeycomb or segments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2466—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure of the adhesive layers, i.e. joints between segments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2474—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure of the walls along the length of the honeycomb
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2478—Structures comprising honeycomb segments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2486—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure characterised by the shapes or configurations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2486—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure characterised by the shapes or configurations
- B01D46/2488—Triangular
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2451—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure
- B01D46/2486—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure characterised by the shapes or configurations
- B01D46/249—Quadrangular e.g. square or diamond
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/50—Catalysts, in general, characterised by their form or physical properties characterised by their shape or configuration
- B01J35/56—Foraminous structures having flow-through passages or channels, e.g. grids or three-dimensional monoliths
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
- C04B38/0006—Honeycomb structures
- C04B38/0016—Honeycomb structures assembled from subunits
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
- B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
- B01D46/2418—Honeycomb filters
- B01D46/2498—The honeycomb filter being defined by mathematical relationships
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
Definitions
- the invention relates to the field of honeycomb structures, more particularly for thermal applications, in particular heat exchangers or particulate filters used in an exhaust line of an engine for the removal of soot produced by the combustion of a diesel fuel or gasoline in an internal combustion engine.
- Filtration structures for soot contained in the exhaust gas of an internal combustion engine are well known in the prior art. These structures most often have a honeycomb structure, one of the faces of the structure for the admission of the exhaust gases to be filtered and the other side the exhaust of the filtered exhaust gases.
- the structure comprises, between the intake and discharge faces, a set of adjacent ducts or channels of axes parallel to each other separated by porous filtration walls, which ducts are closed to one or the other of their ends for delimiting input chambers s' opening according to the inlet face and outlet chambers opening along the discharge face.
- the peripheral part of the structure is most often surrounded by a coating cement.
- the channels or conduits are alternately closed in an order such that the exhaust gases, during the crossing of the honeycomb body, are forced to pass through the side walls of the inlet channels to join the outlet channels. In this way, the particles or soot are deposited and accumulate on the porous walls of the filter body.
- Filter bodies used in automotive exhaust lines are porous ceramic material, for example cordierite, aluminum titanate or silicon carbide or silicon nitride.
- the particulate filter is subjected to a succession of filtration phases (accumulation of soot) and regeneration (removal of soot).
- filtration phases the soot particles emitted by the engine are retained and are deposited inside the filter.
- regeneration phases the soot particles are burned inside the filter, in order to restore its filtration properties.
- the porous structure is then subjected to intense thermomechanical stresses, which can cause microcracks likely over time to cause a severe loss of filtration capacity of the unit, or even its complete deactivation. This phenomenon is particularly observed on monolithic filters of large diameter. It has indeed been observed, operating in an exhaust line, that the thermal gradient between the center and the periphery of such structures is even higher than the dimensions of the monolith are important.
- unitary elongate elements are firstly extruded from a loose slip of particles of the preceding material, most often including porogenic organic materials, and then fired in such a way as to obtain elements in particular. honeycomb, suitable for the filtration of particulate-laden gases by the porous walls that constitute them.
- honeycomb suitable for the filtration of particulate-laden gases by the porous walls that constitute them.
- unitary ceramic elements or monoliths have a section in a polygonal radial section, usually of quadrangular type, in particular square.
- the sections may be triangular or even more rarely hexagonal or a mixture of these different forms (triangular, quadrangular, hexagonal).
- unitary elements of square section are assembled by means of a seal cement first affixed to the outer walls of the unitary elements, then baked at a generally temperature typically less than 1000 ° C, so as to ensure the assembly a sufficient cohesion, without stiffening it in proportions that tend to to render its mechanical properties comparable to that of a monolithic structure of the same size.
- the applicant company has found that the assembly of monolithic ceramic honeycomb elements poses reliability problems of the process for obtaining the assembled filter, especially when one or more peripheral elements in the assembly are subjected to a transverse stress, that is to say in the plane perpendicular to the direction formed by the channels of the Honeycomb.
- a transverse stress that is to say in the plane perpendicular to the direction formed by the channels of the Honeycomb.
- Such a solicitation results in particular from the forces applied during the abrasion and the elimination of the peripheral portions of the assembled filter, with a view to its resizing. If the cement does not allow sufficient grip, it is common that some of the unitary elements, including the most peripheral in the assembly, then detach from the entire structure.
- the surface of the ceramic honeycomb unit elements is also very smooth and the attachment of the cement nevertheless seems to require cements having a very strong adhesion. As previously described, this strong adhesion can quickly be problematic because it helps to stiffen the whole structure. In such a case, when the final assembled filter is subjected to high temperatures related to the burning of soot (typically more than 800 ° C), the expansion phenomena can then create internal mechanical stresses likely to damage and dissociate the together, as explained previously.
- radial mechanical stresses means stresses contributing to dissociating the unit blocks of the assembly with respect to the main central axis of the assembly parallel to the channels of the honeycombs.
- the assembly can also be weakened during handling operations when the cement is not yet completely set and when the hardening is not completed.
- the most peripheral elements, in particular those whose essential of the initial material must be eliminated during the machining, are obviously those which have the greatest probability of detaching.
- the present invention therefore essentially aims to solve the previously discussed manufacturing problems and in particular to provide elements for the formation of a structure formed by the assembly of honeycombs maintaining its integrity even under strong radial mechanical stresses , of the type exercised during of its machining in order to obtain the final external dimensions of the structure.
- the present invention relates in a first aspect to a monolithic honeycomb element comprising a set of adjacent conduits parallel axes between them separated by walls made of a porous material.
- the element has, in a cross section, a polygonal section, in particular quadratic, delimited by external wall elements of average thickness E. It is characterized in that at least one corner of said polygon, preferably all corners of the polygon, present, according to the bisector of the angle at said corner, an excess thickness e c , so that the total thickness E c of the outer wall, also measured along the bisector of the angle at said corner, is greater than the average thickness E (expressed in the same unit) of said outer walls by a factor of at least 1.43.
- said excess thickness e c is obtained at least partly by an additional material disposed on the outer face of said corner.
- the monolithic element has a section, in a cross section, of substantially quadratic or triangular shape and the corners have aperture angles at the vertex a between 60 and 120 °.
- the monolithic element has a section, in a cross section, of substantially square shape.
- Said overthickness has a substantially rounded outer edge s' registering in a radius of curvature R between 0.3 and 3 mm.
- Said excess thickness in cross-section, extends over a length li and has a maximum value e 1 according to the first wall element constituting the corner and over a length 1 2 and said extra thickness has a maximum value e 2 according to the second element wall forming the corner, so that:
- the lengths li and 1 2 described above are substantially equal.
- the ratio of the total thickness E c of the external wall, also measured along the bisector of the angle at the said corner (11), to the average thickness E of the said walls is greater than or equal to 1.45; preferably greater than 1.5 and most preferably greater than 1.6.
- the ratio of the total thickness E c of the external wall, also measured along the bisector of the angle at the said corner, to the average thickness E is less than or equal to 2.8, preferably less than or equal to 2.5 and even more preferably less than 2.
- the average thickness E of the outer walls of the channels is between 100 and 1000 microns, preferably between 300 and 800 microns.
- the thickness of the inner walls of the channels is between 100 and 1000 microns, preferably between 200 and 600 microns.
- said ducts are closed by plugs to one or the other of their ends to define inlet ducts opening along a gas intake face and outlet ducts opening along a gas evacuation face, so that the gas passes through the walls porous.
- the porous material is silicon carbide (SiC), silicon nitride or aluminum titanate, in particular silicon carbide.
- the porous material constituting the unitary element is, for example, recrystallized silicon carbide at a temperature of between 2100 and 2400 ° C.
- the present invention also relates to a structure, in particular a particle filter, obtained by assembling a plurality of monolithic elements as previously described, said elements being bonded by a joint cement.
- the ratio of the excess thickness ei on the average thickness of the joint cement between two constituent elements (measured according to the same unit, of course), according to said transverse plane, is less than or equal to 0, 4 and / or the ratio of the excess thickness e 2 on the average thickness of joint cement, always according to said transverse plane, is less than or equal to 0.4.
- these two ratios are less than or equal to 0.4.
- the joint cement comprises grains and / or a matrix of a ceramic nature.
- said elements and the joint cement essentially comprise the same ceramic material, and preferably are based on silicon carbide (SiC).
- SiC silicon carbide
- FIG. 1 schematizes a cross-section and in perspective of a monolithic element according to the invention.
- FIG. 2 diagrammatically and in more detail voluntarily exaggerates, according to this same cross-section, the corner portion of the monolithic element according to the invention.
- all the monolithic elements are advantageously obtained by extrusion of a loose paste, for example silicon carbide, to form after baking a porous honeycomb structure.
- a loose paste for example silicon carbide
- the shape of the extruder head is configured according to conventional methods, for example as described in US Pat. No. 5,761,787, for obtaining and forming honeycomb elements having the wedge thicknesses according to the invention. , as schematized in Figures 1 and 2 which follow.
- FIG. 1 the extruded structure is presented according to FIG. 1 in the form of a block or monolithic unitary element 1 whose external shape is that of a rectangular parallelepiped extending along a longitudinal axis between its faces. upstream and downstream. Its cross section is substantially square. On the ends of the elements 1 open a plurality of adjacent channels 2, 3, whose main axis is parallel to the longitudinal axis L of the block.
- the extruded porous structures may be alternately plugged on their upstream face or on their downstream face by upstream and downstream plugs, respectively, to form outlet channels 3 and inlet channels 2, respectively, for the formation of filtering structures.
- Each channel 2 or 3 then defines an interior volume delimited by internal walls 4, a closure plug (not shown in the figures) disposed either on the upstream face for an outlet channel, or on the downstream face for a control channel. an inlet and an opening opening alternately towards the downstream face or the upstream face, such that the inlet and outlet channels 3 and 3 are in fluid communication by the internal walls 4.
- monolithic unit elements 1 are assembled together by bonding by means of a cement cement of a ceramic nature, for example also based on silicon carbide, into a filtration structure or filter assembled.
- the assembly thus formed must then be machined to take, for example, a round or ovoid section, then for example to be covered with a coating cement to seal and have a smooth outer surface.
- the section transversal input channels 2 is different from that of the output channels 3.
- the cross sections of the input channels 2 are greater than those of the output channels 3, to increase the overall volume of the input channels at the expense of that of the exit channels.
- the walls 4 follow one another in cross-section and in a horizontal (along the x-axis) or vertical (along the y-axis) row of channels to define a sinusoidal or wave shape. (wavy in English).
- the wall elements wave substantially a half-period of sinusoid over the width of a channel.
- the storage capacity of the particles per unit element 1 is thus advantageously increased.
- the cross sections of the input and output channels were identical and the walls 4 planar.
- FIG. 2 diagrammatically and in greater detail shows, in the same cross section, the corner portion of the monolithic element described in FIG. 1. More precisely, FIG. 2 illustrates in greater detail (and in an exaggerated manner to facilitate comprehension and reading), the profile of the wedges 11 having extra thicknesses 10.
- the filtering elements are therefore characterized, at the wedge 11, by the presence of an excess thickness 10, in the form a supplementary material disposed at the outer portion 12 of the corner 11.
- This extra thickness is characterized by an additional layer of material relative to the conventional configuration described in the documents of the art, illustrated for example in the application EP0816065.
- the two wall elements 6 and 7 meet to form the outer corners of the unitary element, according to straight edges having an angle of 90 °, to form outer edges along the entire length of the element.
- an additional quantity of material of a thickness e c measured along the bisector 13 of the angle formed by the wall elements 6 and 7, is disposed at said corner 11.
- this additional quantity of material is present on the outer side (the edge) 12 of the corner of the element such that, along said bisector 13, the value e c contributes to the total thickness E c of the outer wall, and in such a way that said total thickness E c of the wall, again according to this same bisector, is greater than the average thickness E of said walls 6 and 7 by a factor of at least 1, 43, preferably at least 1, 45 or even at least 1.5, or very preferably at least 1.6.
- said extra thickness preferably has a rounded outer edge, in particular inscribed in a radius of curvature R between 0.3 and 3 mm, the center of the circle inscribed along the rounded outer edge being placed on said bisector 13.
- said excess thickness extends over a length li on the first wall element 6 constituting the wedge 11 (that is to say in the X direction) and over a length 1 2 on the second wall element 7 constituting the corner 11 (that is to say in the Y direction).
- the ratio of the lengths li and 1 2 is between 0.5 and 2 and very preferably is close to 1 or equal to 1.
- said excess thickness 10 has a maximum value ei vis-vis the first wall element 7 constituting the corner and a maximum value ⁇ 2 vis-a-vis the second wall element 6 constituting the corner.
- the ratio of the lengths e 1 and e 2 is between 0.5 and 2 and very preferably is close to 1 or equal to 1.
- the element channel density is from 1 to about 280 c / cm 2 , preferably from about 14 to about 62 c / cm 2 .
- the extra thickness at the corners preferably extends over the entire length L of the element, from the upstream face to the downstream face.
- a population of monolithic elements in the form of a honeycomb and, for example, those described in patents EP 816065, EP 1142619, EP 1455 923 or WO 2004/090294, has been synthesized according to the techniques of the art, for example silicon carbide.
- a SiC powder whose grains have a median diameter d 5 o of 10 microns are mixed initially with a second one.
- the median pore diameter d 5 o is the diameter of the particles such as respectively 50% of the total population of grains has a size smaller than this diameter.
- a porogen of the polyethylene type in a proportion equal to 5% by weight of the total weight of the SiC grains and a methylcellulose type shaping additive in a proportion equal to 10% by weight of the total weight of the SiC grains.
- the quantity of water required is then added and kneaded to obtain a homogeneous paste whose plasticity allows extrusion through a die configured to obtain monolithic blocks of square section and whose internal channels have a cross section. illustrated schematically in Figure 1.
- the half-period p ripples is 1.83mm.
- the green monoliths obtained are dried by microwave for a time sufficient to bring the water content not chemically bound to less than 1% by weight.
- the channels of each face of the monolith are alternately blocked according to well-known techniques, for example described in application WO 2004/065088.
- the monoliths (elements) are debonded then baked under argon according to a rise in temperature of 20 ° C / hour until reaching a maximum temperature of 2200 ° C which is maintained for 6 hours.
- the porous material obtained has an open porosity of 47% and a median pore diameter of the order of 15 microns.
- the assembly is then machined by abrasion, the most peripheral parts being eliminated in order to constitute assembled filters of cylindrical shape.
- a cement of the same composition as the joint cement is deposited at the periphery of the machined filter at an average thickness of 1 mm in order to smooth the outer surface of the cylindrical filters.
- a plurality of assembled filters have thus been made from the unit elements.
- Thickness Thickness max Thickness max li e c according to the total E c ei e 2 (mm) bisector according to ( ⁇ ) ( ⁇ )
- the advantages of the present invention have been mainly exposed in relation to the honeycomb structures used as particulate filters in an exhaust line of an internal combustion engine, allowing the elimination of soot produced by the combustion of a diesel fuel or gasoline.
- the invention is obviously not limited to such an application and also finds application in all areas where the previously discussed problems arise, particularly in the field of heat exchangers.
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Abstract
Monolithic honeycomb element (1) comprising a plurality of adjacent channels (2,3) with axes parallel to each other, separated by walls (4) made of a porous material, said element (1) having, in cross section, a polygonal, particularly square, cross section, delimited by outer wall elements (6-9), said element being characterised in that at least one corner (11) of said polygon, and preferably all the corners of the polygon, have an extra thickness ec according to the bisector (13) of the angle at said corner (11), such that the total thickness Ec of the outer wall, also measured according to said bisector (13) of the angle at said corner (11), is greater than average thickness E of said outer walls by a factor of at least 1.43, said extra thickness ec being obtained at least in partlby an addition (10) of porous material to the outer face of said corner.
Description
ELEMENT EN NID D ' ABEILLE A COINS RENFORCES BEAN NEST ELEMENT WITH REINFORCED CORNERS
L'invention se rapporte au domaine des structures en nid d'abeille, plus particulièrement pour les applications thermiques, notamment les échangeurs thermiques ou les filtres à particules utilisés dans une ligne d ' échappement d'un moteur pour l'élimination des suies produites par la combustion d'un carburant diesel ou essence dans un moteur à combustion interne. Les structures de filtration pour les suies contenues dans les gaz d'échappement de moteur à combustion interne sont bien connues de l'art antérieur. Ces structures présentent le plus souvent une structure en nid d'abeille, une des faces de la structure permettant l'admission des gaz d'échappement à filtrer et l'autre face l'évacuation des gaz d'échappement filtrés. La structure comporte, entre les faces d'admission et d'évacuation, un ensemble de conduits ou canaux adjacents d'axes parallèles entre eux séparés par des parois poreuses de filtration, lesquels conduits sont obturés à l'une ou l'autre de leurs extrémités pour délimiter des chambres d'entrée s ' ouvrant suivant la face d'admission et des chambres de sortie s'ouvrant suivant la face d'évacuation. Pour une bonne étanchéité, la partie périphérique de la structure est le plus souvent entourée d'un ciment de revêtement. Les canaux ou conduits sont alternativement obturés dans un ordre tel que les gaz d'échappement, au cours de la traversée du corps en nid d'abeille, sont contraints de traverser les parois latérales des canaux d'entrée pour rejoindre les canaux de sortie. De cette manière, les particules ou suies se déposent et s'accumulent sur les parois poreuses du corps filtrant. Le plus souvent, les
corps filtrants utilisés dans les lignes d'échappement automobile sont en matière céramique poreuse, par exemple en cordiérite, en titanate d'aluminium ou en carbure de silicium ou encore en nitrure de silicium. The invention relates to the field of honeycomb structures, more particularly for thermal applications, in particular heat exchangers or particulate filters used in an exhaust line of an engine for the removal of soot produced by the combustion of a diesel fuel or gasoline in an internal combustion engine. Filtration structures for soot contained in the exhaust gas of an internal combustion engine are well known in the prior art. These structures most often have a honeycomb structure, one of the faces of the structure for the admission of the exhaust gases to be filtered and the other side the exhaust of the filtered exhaust gases. The structure comprises, between the intake and discharge faces, a set of adjacent ducts or channels of axes parallel to each other separated by porous filtration walls, which ducts are closed to one or the other of their ends for delimiting input chambers s' opening according to the inlet face and outlet chambers opening along the discharge face. For a good seal, the peripheral part of the structure is most often surrounded by a coating cement. The channels or conduits are alternately closed in an order such that the exhaust gases, during the crossing of the honeycomb body, are forced to pass through the side walls of the inlet channels to join the outlet channels. In this way, the particles or soot are deposited and accumulate on the porous walls of the filter body. Most often, Filter bodies used in automotive exhaust lines are porous ceramic material, for example cordierite, aluminum titanate or silicon carbide or silicon nitride.
De façon connue, durant sa mise en œuvre, le filtre à particules est soumis à une succession de phases de filtration (accumulation des suies) et de régénération (élimination des suies) . Lors des phases de filtration, les particules de suies émises par le moteur sont retenues et se déposent à l'intérieur du filtre. Lors des phases de régénération, les particules de suie sont brûlées à l'intérieur du filtre, afin de lui restituer ses propriétés de filtration. La structure poreuse est alors soumise à des contraintes thermo-mécaniques intenses, qui peuvent entraîner des micro-fissurations susceptibles sur la durée d'entraîner une perte sévère des capacités de filtration de l'unité, voire sa désactivâtion complète. Ce phénomène est particulièrement observé sur des filtres monolithiques de grand diamètre. Il a en effet été observé, en fonctionnement dans une ligne d'échappement, que le gradient thermique entre le centre et la périphérie de telles structures est d'autant plus élevé que les dimensions du monolithe sont importantes . In known manner, during its implementation, the particulate filter is subjected to a succession of filtration phases (accumulation of soot) and regeneration (removal of soot). During the filtration phases, the soot particles emitted by the engine are retained and are deposited inside the filter. During the regeneration phases, the soot particles are burned inside the filter, in order to restore its filtration properties. The porous structure is then subjected to intense thermomechanical stresses, which can cause microcracks likely over time to cause a severe loss of filtration capacity of the unit, or even its complete deactivation. This phenomenon is particularly observed on monolithic filters of large diameter. It has indeed been observed, operating in an exhaust line, that the thermal gradient between the center and the periphery of such structures is even higher than the dimensions of the monolith are important.
Pour résoudre ces problèmes et augmenter la durée de vie des filtres, il a été proposé plus récemment des structures de filtration associant plusieurs blocs ou éléments monolithiques en nid d'abeille. Les éléments sont le plus souvent assemblés entre eux par collage au moyen d'une colle ou d'un ciment de nature céramique, appelés dans la suite de la description ciment de joint. Des exemples de telles structures filtrantes sont par exemple décrits dans les demandes de brevets EP 816 065, EP 1 142 619, EP 1 455 923, WO 2004/090294 ou encore WO 2005/063462. Afin d'assurer une meilleure relaxation des contraintes dans une structure assemblée, il est
connu que les coefficients de dilatation thermique des différentes parties de la structure (éléments de filtration, ciment de revêtement, ciment de joint) doivent être sensiblement du même ordre. De ce fait, lesdites parties sont avantageusement synthétisées sur la base d'un même matériau, le plus souvent le carbure de silicium (SiC), la cordiérite ou le titanate d'aluminium. Ce choix permet en outre d'homogénéiser la répartition de la chaleur lors de la régénération du filtre. To solve these problems and increase the life of the filters, it has been proposed more recently filtration structures associating several blocks or monolithic elements in honeycomb. The elements are most often assembled together by gluing by means of a glue or cement of a ceramic nature, hereinafter called seal cement. Examples of such filter structures are for example described in patent applications EP 816,065, EP 1 142 619, EP 1 455 923, WO 2004/090294 or WO 2005/063462. In order to ensure a better relaxation of the stresses in an assembled structure, it is known that the thermal expansion coefficients of different parts of the structure (filter elements, coating cement, joint cement) must be substantially of the same order. As a result, said parts are advantageously synthesized on the basis of the same material, most often silicon carbide (SiC), cordierite or aluminum titanate. This choice also makes it possible to homogenize the distribution of heat during the regeneration of the filter.
Lors du procédé de fabrication de telles structures filtrantes, des éléments allongés unitaires sont dans un premier temps extrudés à partir d'une barbotine meuble de particules du matériau précédent incluant le plus souvent des matériaux organiques porogènes, puis cuits de manière à obtenir des éléments en nid d'abeille, apte à la filtration des gaz chargés en particules par les parois poreuses qui les constituent. Ces éléments céramiques unitaires ou monolithes présentent une section selon une coupe radiale polygonale, le plus souvent de type quadrangulaire, en particulier carrée. During the manufacturing process of such filtering structures, unitary elongate elements are firstly extruded from a loose slip of particles of the preceding material, most often including porogenic organic materials, and then fired in such a way as to obtain elements in particular. honeycomb, suitable for the filtration of particulate-laden gases by the porous walls that constitute them. These unitary ceramic elements or monoliths have a section in a polygonal radial section, usually of quadrangular type, in particular square.
Selon d'autres modes possibles, les sections peuvent être triangulaires ou encore plus rarement hexagonales ou un mélange de ces différentes formes (triangulaire, quadrangulaire, hexagonale) . According to other possible modes, the sections may be triangular or even more rarely hexagonal or a mixture of these different forms (triangular, quadrangular, hexagonal).
Classiquement dans le procédé d'obtention d'une structure en nid d'abeille de grande taille (que les parois soient obturées ou non par des bouchons à l'une ou l'autre des extrémités), des éléments unitaires de section carré (qu'on prendra pour référence dans la suite de la description sans pourtant s'y limiter) sont assemblés au moyen d'un ciment de joint d'abord apposé sur les parois externes des éléments unitaires, puis cuit à généralement une température typiquement inférieure à 1000 °C, de façon à assurer à l'assemblage une cohésion suffisante, sans pour autant le rigidifier dans des proportions qui tendent à
rendre ses propriétés mécaniques comparables à celle d'une structure monolithique de même taille. Conventionally in the process of obtaining a large honeycomb structure (whether the walls are closed off or not by plugs at one or the other end), unitary elements of square section (which are taken for reference in the following description without however being limited) are assembled by means of a seal cement first affixed to the outer walls of the unitary elements, then baked at a generally temperature typically less than 1000 ° C, so as to ensure the assembly a sufficient cohesion, without stiffening it in proportions that tend to to render its mechanical properties comparable to that of a monolithic structure of the same size.
La production des structures assemblées est donc nécessairement le résultat d'un compromis entre l'adhérence souhaitée entre les éléments unitaires et une valeur limitée de la rigidité globale de la structure assemblée finalement obtenue . The production of the assembled structures is therefore necessarily the result of a compromise between the desired adhesion between the unit elements and a limited value of the overall rigidity of the assembled structure finally obtained.
Un tel problème est d' autant plus crucial que la structure assemblée doit le plus souvent faire l'objet d'un réajustement de ses dimensions extérieures pour l'adapter à son logement dans la ligne d'échappement. Le plus souvent, la structure de grande dimension doit par exemple se présenter sous la forme d'un cylindre allongé, de section plus ou moins elliptique selon le cahier des charges imposé par chaque constructeur automobile (on entend ici par constructeur automobile, le constructeur de véhicules particuliers mais aussi celui qui réalise des véhicules utilitaires, notamment des camions) . Pour obtenir de telles formes adaptées, il est nécessaire d'éliminer la partie périphérique des structures assemblées à partir des éléments de section carrée par abrasion et de recouvrir finalement le filtre découpé aux bonnes dimensions par un ciment de revêtement externe pour en lisser la surface externe, selon les principes décrits par exemple dans les demandes EP 1142619 Al, EP 1516659 Al ou encore US 2006/289501 Al. Such a problem is all the more crucial as the assembled structure must most often be readjusted to its external dimensions in order to adapt it to its housing in the exhaust line. Most often, the large structure must for example be in the form of an elongated cylinder, of more or less elliptical section according to the specifications imposed by each car manufacturer (here is meant by car manufacturer, the manufacturer of private vehicles but also the one that makes commercial vehicles, including trucks). To obtain such adapted shapes, it is necessary to eliminate the peripheral portion of the structures assembled from the square section elements by abrasion and finally cover the filter cut to the right dimensions by an external coating cement to smooth the outer surface according to the principles described, for example, in applications EP 1142619 A1, EP 1516659 A1 or US 2006/289501 A1.
Cependant, lors de la mise en œuvre des différentes solutions décrites dans ces publications antérieures, la société déposante a pu constater que l'assemblage des éléments monolithiques céramique en nid d'abeille pose des problèmes de fiabilité du procédé d'obtention du filtre assemblé, notamment lorsqu'un ou plusieurs éléments périphériques dans l'assemblage sont soumis à une sollicitation transversale, c'est-à-dire dans le plan perpendiculaire à la direction formée par les canaux du
nid d'abeille. Une telle sollicitation résulte en particulier des forces appliquées lors de l'abrasion et de l'élimination des portions périphériques du filtre assemblé, en vue de son redimensionnement . Si le ciment ne permet pas une accroche suffisante, il est fréquent que certains des éléments unitaires, notamment les plus périphériques dans l'assemblage, se détachent alors de l'ensemble de la structure. However, during the implementation of the various solutions described in these prior publications, the applicant company has found that the assembly of monolithic ceramic honeycomb elements poses reliability problems of the process for obtaining the assembled filter, especially when one or more peripheral elements in the assembly are subjected to a transverse stress, that is to say in the plane perpendicular to the direction formed by the channels of the Honeycomb. Such a solicitation results in particular from the forces applied during the abrasion and the elimination of the peripheral portions of the assembled filter, with a view to its resizing. If the cement does not allow sufficient grip, it is common that some of the unitary elements, including the most peripheral in the assembly, then detach from the entire structure.
La surface des éléments unitaires en nids d' abeille en céramique est en outre très lisse et l'accrochage du ciment semble pourtant nécessiter des ciments présentant une très forte adhésion. Comme décrit précédemment, cette forte adhésion peut rapidement être problématique car elle contribue à rigidifier l'ensemble de la structure. Dans un tel cas, lorsque le filtre assemblé final est soumis à des températures élevées liés au brûlage des suies (typiquement plus de 800°C) , les phénomènes de dilatation peuvent alors créer des contraintes mécaniques internes susceptibles d'endommager et de désolidariser l'ensemble, comme expliqué précédemment. The surface of the ceramic honeycomb unit elements is also very smooth and the attachment of the cement nevertheless seems to require cements having a very strong adhesion. As previously described, this strong adhesion can quickly be problematic because it helps to stiffen the whole structure. In such a case, when the final assembled filter is subjected to high temperatures related to the burning of soot (typically more than 800 ° C), the expansion phenomena can then create internal mechanical stresses likely to damage and dissociate the together, as explained previously.
II a été proposé des solutions consistant à réduire la rigidité du ciment en utilisant des compositions conduisant à un matériau de joint présentant un module d'élasticité plus faible comme dans EP1249262. Des ensembles avec joints à base de fibres céramiques sont ainsi dévoilés par EP0816065, permettant une meilleure accroche. Solutions have been proposed to reduce the rigidity of the cement by using compositions leading to a joint material having a lower modulus of elasticity as in EP1249262. Sets with joints based on ceramic fibers are thus unveiled by EP0816065, allowing better grip.
D'autres solutions existent, qui consistent à réaliser des zones de non adhésion pour relaxer les contraintes ou réduire la rigidité de l'ensemble (FR2833857A1 ou FR2853256A1) . Ces solutions, qui apportent une amélioration sensible en ce qui concerne la tendance observée précédemment à la désolidarisation des éléments unitaires, restent cependant perfectibles, en particulier en ce qui concerne la résistance aux contraintes mécaniques radiales exercées sur la structure
lors de l'étape de redimensionnement de la structure assemblé.Other solutions exist, which consist in making nonadhering zones to relax the stresses or reduce the rigidity of the assembly (FR2833857A1 or FR2853256A1). These solutions, which provide a significant improvement with regard to the previously observed tendency to separate the unit elements, remain however perfectible, in particular as regards the resistance to radial mechanical stresses exerted on the structure during the step of resizing the assembled structure.
Au sens de la présente invention et comme indiqué précédemment, on entend par contraintes mécaniques radiales des contraintes contribuant à dissocier les blocs unitaires de l'assemblage par rapport à l'axe central principal de l'assemblage parallèles aux canaux des nids d'abeille. L'ensemble peut également être fragilisé lors de manipulations réalisées lorsque le ciment n'est pas encore complètement pris et lorsque le durcissement n'est pas achevé. Les éléments les plus périphériques, en particulier ceux dont l'essentiel de la matière initiale doit être éliminée lors de l'usinage, sont bien évidemment ceux qui présentent la plus grande probabilité de se détacher. For the purposes of the present invention and as indicated above, the term "radial mechanical stresses" means stresses contributing to dissociating the unit blocks of the assembly with respect to the main central axis of the assembly parallel to the channels of the honeycombs. The assembly can also be weakened during handling operations when the cement is not yet completely set and when the hardening is not completed. The most peripheral elements, in particular those whose essential of the initial material must be eliminated during the machining, are obviously those which have the greatest probability of detaching.
Des solutions existent visant à éliminer l'opération d'usinage comme par exemple EP1977808A1 en assemblant des blocs unitaires périphériques de forme finale. Le problème de la manipulation persiste. Par ailleurs cette solution est peu flexible industriellement car elle suppose la gestion d'au moins trois familles de blocs unitaires différents par forme de filtre et une adaptation des filières pour chacun des éléments. En outre les filières doivent être changées dès que la forme finale du filtre évolue. Ainsi, sur la base d'un eu de filière approprié et spécifique, cette solution ne permet de réaliser que des structures en nid d'abeille assemblées répondant à un diamètre extérieur fixé et unique, sans adaptation possible. Solutions exist to eliminate the machining operation such as for example EP1977808A1 by assembling peripheral unit blocks of final shape. The problem of manipulation persists. Furthermore this solution is industrially inflexible because it assumes the management of at least three families of different unit blocks by filter form and an adaptation of the dies for each of the elements. In addition, the dies must be changed as soon as the final shape of the filter changes. Thus, on the basis of an appropriate and specific die, this solution makes it possible to achieve only honeycomb structures assembled to a fixed outer diameter and single, without possible adaptation.
La présente invention a donc essentiellement pour but de résoudre les problèmes de fabrication précédemment exposés et en particulier de fournir des éléments pour la formation d'une structure formée par l'assemblage de nids d'abeille conservant son intégrité même sous de fortes contraintes mécaniques radiales, du type de celle exercées lors
de son usinage afin d'obtenir les dimensions externes finales de la structure. The present invention therefore essentially aims to solve the previously discussed manufacturing problems and in particular to provide elements for the formation of a structure formed by the assembly of honeycombs maintaining its integrity even under strong radial mechanical stresses , of the type exercised during of its machining in order to obtain the final external dimensions of the structure.
Plus précisément, la présente invention se rapporte selon un premier aspect à un élément monolithique en nid d'abeille comprenant un ensemble de conduits adjacents d'axes parallèles entre eux séparés par des parois faites dans une matière poreuse. L'élément présente, selon une coupe transversale, une section polygonale, notamment quadratique, délimitée par des éléments de parois extérieures d'épaisseur moyenne E. Il se caractérise en ce qu'au moins un coin dudit polygone, de préférence tous les coins du polygone, présente, selon la bissectrice de l'angle au niveau dudit coin, une surépaisseur ec, de telle sorte que l'épaisseur totale Ec de la paroi externe, mesurée également selon la bissectrice de l'angle au niveau dudit coin, soit supérieure à l'épaisseur moyenne E (exprimée dans la même unité) desdites parois extérieures d'un facteur d'au moins 1,43. Selon une autre caractéristique essentielle de la présente invention, ladite surépaisseur ec est obtenue au moins pour partie par un supplément de matière disposée sur la face externe dudit coin. More specifically, the present invention relates in a first aspect to a monolithic honeycomb element comprising a set of adjacent conduits parallel axes between them separated by walls made of a porous material. The element has, in a cross section, a polygonal section, in particular quadratic, delimited by external wall elements of average thickness E. It is characterized in that at least one corner of said polygon, preferably all corners of the polygon, present, according to the bisector of the angle at said corner, an excess thickness e c , so that the total thickness E c of the outer wall, also measured along the bisector of the angle at said corner, is greater than the average thickness E (expressed in the same unit) of said outer walls by a factor of at least 1.43. According to another essential characteristic of the present invention, said excess thickness e c is obtained at least partly by an additional material disposed on the outer face of said corner.
Selon des réalisations avantageuses de la présente invention, qui peuvent bien évidemment le cas échéant être combinées entre elles : According to advantageous embodiments of the present invention, which can of course possibly be combined with one another:
- L'élément monolithique présente une section, selon une coupe transversale, de forme sensiblement quadratique ou triangulaire et les coins présentent des angles d'ouverture au sommet a compris entre 60 et 120°. - The monolithic element has a section, in a cross section, of substantially quadratic or triangular shape and the corners have aperture angles at the vertex a between 60 and 120 °.
- L'élément monolithique présente une section, selon une coupe transversale, de forme sensiblement carrée. - The monolithic element has a section, in a cross section, of substantially square shape.
- Ladite surépaisseur présente un bord externe sensiblement arrondie s' inscrivant dans un rayon de courbure
R compris entre 0,3 et 3 mm. Said overthickness has a substantially rounded outer edge s' registering in a radius of curvature R between 0.3 and 3 mm.
- Ladite surépaisseur, selon une coupe transversale, s'étend sur une longueur li et présente une valeur maximale ei selon le premier élément de paroi constituant le coin et sur une longueur 12 et ladite surépaisseur présente une valeur maximale e2 selon le second élément de paroi constituant le coin, de telle sorte que :
Said excess thickness, in cross-section, extends over a length li and has a maximum value e 1 according to the first wall element constituting the corner and over a length 1 2 and said extra thickness has a maximum value e 2 according to the second element wall forming the corner, so that:
Les longueurs li et 12 décrites précédemment sont sensiblement égales. The lengths li and 1 2 described above are substantially equal.
- Les surépaisseurs ei et e2 décrites précédemment sont sensiblement égales. - The oversize ei and e 2 described above are substantially equal.
- Le rapport de l'épaisseur totale Ec de la paroi externe, mesurée également selon la bissectrice de l'angle au niveau dudit coin (11), sur l'épaisseur moyenne E desdites parois est supérieur ou égal à 1,45, de préférence supérieur à 1,5 et de façon très préférée supérieur à 1,6. The ratio of the total thickness E c of the external wall, also measured along the bisector of the angle at the said corner (11), to the average thickness E of the said walls is greater than or equal to 1.45; preferably greater than 1.5 and most preferably greater than 1.6.
- Le rapport de l'épaisseur totale Ec de la paroi externe, mesurée également selon la bissectrice de l'angle au niveau dudit coin, sur l'épaisseur moyenne E est inférieur ou égal à 2,8, de préférence inférieur ou égal à 2,5 et de manière encore plus préférée inférieur à 2. The ratio of the total thickness E c of the external wall, also measured along the bisector of the angle at the said corner, to the average thickness E is less than or equal to 2.8, preferably less than or equal to 2.5 and even more preferably less than 2.
- L'épaisseur moyenne E des parois externes des canaux est comprise entre 100 et 1000 microns, de préférence entre 300 et 800 microns. - The average thickness E of the outer walls of the channels is between 100 and 1000 microns, preferably between 300 and 800 microns.
- L'épaisseur des parois internes des canaux est comprise entre 100 et 1000 microns, de préférence entre 200 et 600 microns. - The thickness of the inner walls of the channels is between 100 and 1000 microns, preferably between 200 and 600 microns.
- Lesdits conduits sont obturés par des bouchons à l'une ou
l'autre de leurs extrémités pour délimiter des conduits d'entrée s'ouvrant suivant une face d'admission des gaz et des conduits de sortie s'ouvrant suivant une face d'évacuation des gaz, de telle façon que le gaz traverse les parois poreuses. - said ducts are closed by plugs to one or the other of their ends to define inlet ducts opening along a gas intake face and outlet ducts opening along a gas evacuation face, so that the gas passes through the walls porous.
- Ladite surépaisseur s'étend sur toute la longueur de - Said overthickness extends over the entire length of
1' élément . 1 element.
- La matière poreuse est du carbure de silicium (SiC) , du nitrure de silicium ou du titanate d'aluminium, en particulier du carbure de silicium. Le matériau poreux constituant l'élément unitaire est par exemple du carbure de silicium recristallisé à une température comprise entre 2100 et 2400°C. - The porous material is silicon carbide (SiC), silicon nitride or aluminum titanate, in particular silicon carbide. The porous material constituting the unitary element is, for example, recrystallized silicon carbide at a temperature of between 2100 and 2400 ° C.
Selon un autre aspect, la présente invention se rapporte également à une structure, notamment un filtre à particules, obtenu par 1 ' assemblage d ' une pluralité d ' éléments monolithiques tels que précédemment décrits, lesdits éléments étant liés par un ciment de joint. According to another aspect, the present invention also relates to a structure, in particular a particle filter, obtained by assembling a plurality of monolithic elements as previously described, said elements being bonded by a joint cement.
De préférence, dans une telle structure, le rapport de la surépaisseur ei sur l'épaisseur moyenne du ciment de joint entre deux éléments constitutifs (mesurées selon la même unité, bien évidemment) , selon ledit plan transversal, est inférieur ou égal à 0,4 et/ou le rapport de la surépaisseur e2 sur l'épaisseur moyenne de ciment de joint, toujours selon ledit plan transversal, est inférieur ou égal à 0,4. De préférence ces deux rapports sont inférieurs ou égaux à 0,4. Preferably, in such a structure, the ratio of the excess thickness ei on the average thickness of the joint cement between two constituent elements (measured according to the same unit, of course), according to said transverse plane, is less than or equal to 0, 4 and / or the ratio of the excess thickness e 2 on the average thickness of joint cement, always according to said transverse plane, is less than or equal to 0.4. Preferably these two ratios are less than or equal to 0.4.
De préférence, le ciment de joint comporte des grains et/ou une matrice de nature céramique . Preferably, the joint cement comprises grains and / or a matrix of a ceramic nature.
Avantageusement, au sein du filtre, lesdits éléments et le ciment de joint comprennent essentiellement le même matériau céramique, et préférentiellement sont à base de carbure de silicium (SiC) .
L'invention sera mieux comprise à la lecture de la description de différents modes de réalisations de l'invention qui suivent, respectivement illustrés par les figures 1 et 2. Advantageously, within the filter, said elements and the joint cement essentially comprise the same ceramic material, and preferably are based on silicon carbide (SiC). The invention will be better understood on reading the description of various embodiments of the invention which follow, respectively illustrated by FIGS. 1 and 2.
La figure 1 schématise une coupe transversale et en perspective d'un élément monolithique selon l'invention. FIG. 1 schematizes a cross-section and in perspective of a monolithic element according to the invention.
La figure 2 représente schématiquement et plus en détail, de façon volontairement exagérée, selon cette même coupe transversale, la partie de coin de l'élément monolithique selon l'invention. FIG. 2 diagrammatically and in more detail voluntarily exaggerates, according to this same cross-section, the corner portion of the monolithic element according to the invention.
Selon des techniques bien connues, tous les éléments monolithiques sont avantageusement obtenus par extrusion d'une pâte meuble, par exemple en carbure de silicium, pour former après cuisson une structure poreuse en nid d'abeille. La forme de la tête d'extrudeuse est configurée selon les méthodes classiques, par exemple telles que décrites dans le brevet US 5,761,787, pour l'obtention et la formation d'éléments en nid d'abeille présentant les surépaisseurs en coin selon l'invention, telles que schématisées sur les figures 1 et 2 qui suivent. According to well-known techniques, all the monolithic elements are advantageously obtained by extrusion of a loose paste, for example silicon carbide, to form after baking a porous honeycomb structure. The shape of the extruder head is configured according to conventional methods, for example as described in US Pat. No. 5,761,787, for obtaining and forming honeycomb elements having the wedge thicknesses according to the invention. , as schematized in Figures 1 and 2 which follow.
Sans que cela puisse être considéré comme restrictif, la structure extrudée se présente selon la figure 1 sous forme d'un bloc ou élément unitaire monolithique 1 dont la forme extérieure est celle d'un parallélépipède rectangle s 'étendant selon un axe longitudinal entre ses faces amont et aval. Sa section transversale est sensiblement carrée. Sur les extrémités des éléments 1 débouchent une pluralité de canaux 2, 3 adjacents, dont l'axe principal est parallèle à l'axe longitudinal L du bloc. Without this being considered restrictive, the extruded structure is presented according to FIG. 1 in the form of a block or monolithic unitary element 1 whose external shape is that of a rectangular parallelepiped extending along a longitudinal axis between its faces. upstream and downstream. Its cross section is substantially square. On the ends of the elements 1 open a plurality of adjacent channels 2, 3, whose main axis is parallel to the longitudinal axis L of the block.
De façon connue mais non représentée sur les figures, les
structures poreuses extrudées peuvent être alternativement bouchées sur leur face amont ou sur leur face aval par des bouchons amont et aval, respectivement, pour former des canaux de sortie 3 et des canaux d'entrée 2, respectivement, pour la formation de structures filtrantes. Chaque canal 2 ou 3 définit alors un volume intérieur délimité par des parois internes 4, un bouchon d'obturation (non représenté sur les figures) disposé soit sur la face amont pour un canal de sortie, soit sur la face aval pour un canal d'entrée et une ouverture débouchant alternativement vers la face aval ou la face amont, de telle façon que les canaux d'entrée 2 et de sortie 3 sont en communication de fluide par les parois internes 4. In known manner but not shown in the figures, the extruded porous structures may be alternately plugged on their upstream face or on their downstream face by upstream and downstream plugs, respectively, to form outlet channels 3 and inlet channels 2, respectively, for the formation of filtering structures. Each channel 2 or 3 then defines an interior volume delimited by internal walls 4, a closure plug (not shown in the figures) disposed either on the upstream face for an outlet channel, or on the downstream face for a control channel. an inlet and an opening opening alternately towards the downstream face or the upstream face, such that the inlet and outlet channels 3 and 3 are in fluid communication by the internal walls 4.
De manière connue et non représentée sur les figures, plusieurs éléments unitaires monolithes 1 sont assemblés entre eux par collage au moyen d'un ciment de joint de nature céramique, par exemple également à base de carbure de silicium, en une structure de filtration ou filtre assemblé. L'assemblage ainsi constitué doit être ensuite usiné pour prendre, par exemple, une section ronde ou ovoïde, puis par exemple être recouvert d'un ciment de revêtement pour en assurer l'étanchéité et présenter une surface externe lisse. In a known manner and not shown in the figures, several monolithic unit elements 1 are assembled together by bonding by means of a cement cement of a ceramic nature, for example also based on silicon carbide, into a filtration structure or filter assembled. The assembly thus formed must then be machined to take, for example, a round or ovoid section, then for example to be covered with a coating cement to seal and have a smooth outer surface.
Lorsque les éléments monolithiques sont bouchés tels que précédemment décrit, il en résulte un filtre assemblé apte à être inséré dans une ligne d'échappement, selon des techniques bien connues. En fonctionnement, le flux des gaz d'échappement entre dans le filtre par les canaux d'entrée 2, puis traverse les parois internes filtrantes 4 de ces canaux pour rejoindre les canaux de sortie 3. Pour plus de précision en ce qui concerne la structure des éléments monolithiques et leur assemblage pour la formation d'un filtre, on pourra par exemple se reporter aux demandes EP 1142619, WO 05/063462 ou encore WO 05/016491. When the monolithic elements are plugged as described above, this results in an assembled filter capable of being inserted into an exhaust line, according to well-known techniques. In operation, the flow of the exhaust gases enters the filter through the inlet channels 2, then passes through the filtering internal walls 4 of these channels to join the outlet channels 3. For more precision with regard to the structure monolithic elements and their assembly for the formation of a filter, one can for example refer to the applications EP 1142619, WO 05/063462 or WO 05/016491.
Dans le mode représenté sur la figure 1, la section
transversale des canaux d'entrée 2 est différente de celle des canaux de sortie 3. Ainsi, les sections transversales des canaux d'entrée 2 sont supérieures à celles des canaux de sortie 3, afin d'accroître le volume global des canaux d'entrée aux dépens de celui des canaux de sortie. Dans le mode illustré par les figures, les parois 4 se succèdent, en coupe transversale et en suivant un rang horizontal (selon l'axe x) ou vertical (selon l'axe y) de canaux, pour définir une forme sinusoïdale ou en vague (wavy en anglais) . Les éléments de paroi ondulent par exemple sensiblement d'une demi-période de sinusoïde sur la largeur d'un canal. In the mode shown in Figure 1, the section transversal input channels 2 is different from that of the output channels 3. Thus, the cross sections of the input channels 2 are greater than those of the output channels 3, to increase the overall volume of the input channels at the expense of that of the exit channels. In the mode illustrated by the figures, the walls 4 follow one another in cross-section and in a horizontal (along the x-axis) or vertical (along the y-axis) row of channels to define a sinusoidal or wave shape. (wavy in English). For example, the wall elements wave substantially a half-period of sinusoid over the width of a channel.
Dans une application de la structure comme filtre, la capacité de stockage des particules par élément unitaire 1 est ainsi avantageusement augmentée. On ne sortirait cependant pas de l'invention si les sections transversales des canaux d'entrée et de sortie étaient identiques et les parois 4 planes. In an application of the structure as a filter, the storage capacity of the particles per unit element 1 is thus advantageously increased. However, it would not come out of the invention if the cross sections of the input and output channels were identical and the walls 4 planar.
Des éléments de paroi externes 6, 7, 8, 9 d'épaisseur E complètent et entourent les parois internes 4. Ces éléments de paroi se rejoignent et se recoupent deux à deux suivant une bissectrice, au niveau de coins présentant des angles d'ouverture au sommet a= 90° pour la structure de section carrée représentée sur la figure 1. External wall elements 6, 7, 8, 9 of thickness E complement and surround the inner walls 4. These wall elements meet and intersect two by two along a bisector, at the corners having opening angles. at the top a = 90 ° for the square section structure shown in FIG.
Sur la figure 2, on a représenté schématiquement et plus en détail, selon la même coupe transversale, la partie de coin de l'élément monolithique décrit sur la figure 1. Plus précisément, la figure 2 illustre plus en détail (et de façon exagérée pour en faciliter la compréhension et la lecture) , le profil des coins 11 présentant des surépaisseurs 10. Selon l'invention, les éléments filtrants se caractérisent donc, au niveau du coin 11, par la présence d'une surépaisseur 10, sous la forme d'un supplément de matière disposé au niveau de la partie externe 12 du coin 11. Cette surépaisseur est caractérisée par une couche supplémentaire de matière par rapport à la
configuration classique décrite dans les documents de l'art, illustrée par exemple dans la demande EP0816065. FIG. 2 diagrammatically and in greater detail shows, in the same cross section, the corner portion of the monolithic element described in FIG. 1. More precisely, FIG. 2 illustrates in greater detail (and in an exaggerated manner to facilitate comprehension and reading), the profile of the wedges 11 having extra thicknesses 10. According to the invention, the filtering elements are therefore characterized, at the wedge 11, by the presence of an excess thickness 10, in the form a supplementary material disposed at the outer portion 12 of the corner 11. This extra thickness is characterized by an additional layer of material relative to the conventional configuration described in the documents of the art, illustrated for example in the application EP0816065.
Plus précisément, selon la configuration classique et tel que représentée par les lignes en pointillés sur la figure 2, les deux éléments de parois 6 et 7 se rejoignent pour former les coins extérieurs de l'élément unitaire, selon des bords droits présentant un angle de 90°, pour former des arêtes extérieures sur toute la longueur de l'élément. More precisely, according to the conventional configuration and as represented by the dashed lines in FIG. 2, the two wall elements 6 and 7 meet to form the outer corners of the unitary element, according to straight edges having an angle of 90 °, to form outer edges along the entire length of the element.
Selon l'invention et tel que représentée sur la figure 1, une quantité supplémentaire de matière, d'une épaisseur ec mesurée selon la bissectrice 13 de l'angle formé par les éléments de parois 6 et 7, est disposée au niveau dudit coin 11. Selon l'invention, cette quantité supplémentaire de matière est présente sur le côté (l'arête) extérieur 12 du coin de l'élément de telle façon que, selon ladite bissectrice 13, la valeur ec contribue à l'épaisseur totale Ec de la paroi externe, et de telle façon que ladite épaisseur totale Ec de la paroi, toujours selon cette même bissectrice, soit supérieure à l'épaisseur moyenne E desdites parois 6 et 7 d'un facteur d'au moins 1,43, de préférence d' au moins 1 , 45 ou même d' au moins 1 , 5 , ou encore de façon très préférée d'au moins 1,6. According to the invention and as shown in FIG. 1, an additional quantity of material, of a thickness e c measured along the bisector 13 of the angle formed by the wall elements 6 and 7, is disposed at said corner 11. According to the invention, this additional quantity of material is present on the outer side (the edge) 12 of the corner of the element such that, along said bisector 13, the value e c contributes to the total thickness E c of the outer wall, and in such a way that said total thickness E c of the wall, again according to this same bisector, is greater than the average thickness E of said walls 6 and 7 by a factor of at least 1, 43, preferably at least 1, 45 or even at least 1.5, or very preferably at least 1.6.
Tel que représenté sur la figure 2, ladite surépaisseur présente préférentiellement un bord externe arrondi, en particulier s' inscrivant dans un rayon de courbure R compris entre 0,3 et 3 mm, le centre du cercle inscrit selon le bord extérieur arrondi se plaçant sur ladite bissectrice 13. As represented in FIG. 2, said extra thickness preferably has a rounded outer edge, in particular inscribed in a radius of curvature R between 0.3 and 3 mm, the center of the circle inscribed along the rounded outer edge being placed on said bisector 13.
Selon l'invention, ladite surépaisseur s'étend sur une longueur li sur le premier élément de paroi 6 constituant le coin 11 (c'est-à-dire dans la direction X) et sur une longueur 12 sur le second élément de paroi 7 constituant le coin 11 (c'est-à-dire dans la direction Y) . De préférence, le rapport des longueurs li et 12 est compris entre 0,5 et 2 et de manière très préférée est proche de 1 ou égal à 1.
Selon l'invention, ladite surépaisseur 10 présente une valeur maximale ei vis-vis du premier élément de paroi 7 constituant le coin et une valeur maximale Θ2 vis-vis du second élément de paroi 6 constituant le coin. De préférence, le rapport des longueurs ei et e2 est compris entre 0,5 et 2 et de manière très préférée est proche de 1 ou égal à 1. According to the invention, said excess thickness extends over a length li on the first wall element 6 constituting the wedge 11 (that is to say in the X direction) and over a length 1 2 on the second wall element 7 constituting the corner 11 (that is to say in the Y direction). Preferably, the ratio of the lengths li and 1 2 is between 0.5 and 2 and very preferably is close to 1 or equal to 1. According to the invention, said excess thickness 10 has a maximum value ei vis-vis the first wall element 7 constituting the corner and a maximum value Θ2 vis-a-vis the second wall element 6 constituting the corner. Preferably, the ratio of the lengths e 1 and e 2 is between 0.5 and 2 and very preferably is close to 1 or equal to 1.
Typiquement, la densité de canaux éléments est comprise entre 1 et environ 280 c/cm2, de préférence entre environ 14 et environ 62 c/cm2. Selon l'invention, la surépaisseur au niveau des coins s'étend de préférence sur toute la longueur L de l'élément, depuis la face amont jusqu'à la face aval. Typically, the element channel density is from 1 to about 280 c / cm 2 , preferably from about 14 to about 62 c / cm 2 . According to the invention, the extra thickness at the corners preferably extends over the entire length L of the element, from the upstream face to the downstream face.
L'invention et ses avantages seront mieux compris à la lecture de l'exemple qui suit, donné à titre purement illustratif. The invention and its advantages will be better understood on reading the example which follows, given purely by way of illustration.
Exemple : Example:
Les éléments selon l'invention ont été synthétisés de manière classique: The elements according to the invention have been synthesized in a conventional manner:
Plus précisément, on a synthétisé selon les techniques de l'art, par exemple décrites dans les brevets EP 816065, EP 1142619, EP 1455 923 ou encore WO 2004/090294, une population d'éléments monolithiques en forme de nid d'abeille et en carbure de silicium. More specifically, a population of monolithic elements in the form of a honeycomb and, for example, those described in patents EP 816065, EP 1142619, EP 1455 923 or WO 2004/090294, has been synthesized according to the techniques of the art, for example silicon carbide.
Pour ce faire, de manière comparable au procédé décrit dans la demande EP 1 142 619, on mélange dans un premier temps 70% poids d'une poudre de SiC dont les grains présentent un diamètre médian d5o de 10 microns, avec une deuxième poudre de SiC dont les grains présentent un diamètre médian d5o de 0,5 micron. Au sens de la présente description, on désigne par diamètre médian de pore d5o le diamètre des particules tel que
respectivement 50% de la population totale des grains présente une taille inférieure à ce diamètre. A ce mélange est ajouté un porogène du type polyéthylène dans une proportion égale à 5% poids du poids total des grains de Sic et un additif de mise en forme du type méthylcellulose dans une proportion égale à 10% poids du poids total des grains de SiC. For this purpose, in a manner comparable to the process described in application EP 1 142 619, 70% by weight of a SiC powder whose grains have a median diameter d 5 o of 10 microns are mixed initially with a second one. SiC powder whose grains have a median diameter of 5 o 0.5 micron. For the purposes of the present description, the median pore diameter d 5 o is the diameter of the particles such as respectively 50% of the total population of grains has a size smaller than this diameter. To this mixture is added a porogen of the polyethylene type in a proportion equal to 5% by weight of the total weight of the SiC grains and a methylcellulose type shaping additive in a proportion equal to 10% by weight of the total weight of the SiC grains. .
On ajoute ensuite la quantité d'eau nécessaire et on malaxe jusqu'à obtenir une pâte homogène dont la plasticité permet l'extrusion à travers une filière configurée pour l'obtention de blocs monolithes de section carrée et dont les canaux internes présentent une section transversale illustrée schématiquement en figure 1. La demi-période p des ondulations est de 1,83mm. The quantity of water required is then added and kneaded to obtain a homogeneous paste whose plasticity allows extrusion through a die configured to obtain monolithic blocks of square section and whose internal channels have a cross section. illustrated schematically in Figure 1. The half-period p ripples is 1.83mm.
Les monolithes crus obtenus sont séchés par micro-onde pendant un temps suffisant pour amener la teneur en eau non liée chimiquement à moins de 1% en masse. The green monoliths obtained are dried by microwave for a time sufficient to bring the water content not chemically bound to less than 1% by weight.
Les canaux de chaque face du monolithe sont alternativement bouchés selon des techniques bien connues, par exemple décrites dans la demande WO 2004/065088. Les monolithes (éléments) sont déliantés puis cuits sous argon selon une montée en température de 20°C/heure jusqu'à atteindre une température maximale de 2200 °C qui est maintenue pendant 6 heures. The channels of each face of the monolith are alternately blocked according to well-known techniques, for example described in application WO 2004/065088. The monoliths (elements) are debonded then baked under argon according to a rise in temperature of 20 ° C / hour until reaching a maximum temperature of 2200 ° C which is maintained for 6 hours.
Le matériau poreux obtenu, présente une porosité ouverte de 47% et un diamètre médian de pores de l'ordre de 15 micromètres . The porous material obtained has an open porosity of 47% and a median pore diameter of the order of 15 microns.
Les caractéristiques structurales des éléments ainsi obtenus sont données dans le tableau 1 ci-après, en connexion avec les données déjà décrites dans la description précédente des figures 1 et 2.
Pour la formation du filtre, 16 éléments (4x4) sont ensuite assemblés entre eux par collage au moyen d'un ciment de composition chimique suivante : 72% poids de Sic, 15% poids d'Al203, 11% poids de S1O2, le reste étant constitué par des impuretés ma oritairement de Fe2Û3 et d'oxydes de métaux alcalins et alcalino-terreux . L'épaisseur moyenne du joint entre deux blocs voisins est de l'ordre de 2 mm. La conductivité thermique du ciment de joint après traitement thermique est d'environ 2,1 W/m.K à la température ambiante et sa porosité ouverte mesurée est d'environ 38%. The structural characteristics of the elements thus obtained are given in Table 1 below, in connection with the data already described in the previous description of FIGS. 1 and 2. For the formation of the filter, 16 elements (4x4) are then assembled together by bonding with a cement of the following chemical composition: 72% by weight of SiC, 15% by weight of Al 2 O 3, 11% by weight of SiO 2 the remainder being impurities, usually Fe 2 O 3, and alkali and alkaline-earth metal oxides. The average thickness of the joint between two adjacent blocks is of the order of 2 mm. The thermal conductivity of the joint cement after heat treatment is about 2.1 W / mK at room temperature and its measured open porosity is about 38%.
L'ensemble est ensuite usiné par abrasion, les parties les plus périphériques étant éliminées afin de constituer des filtres assemblés de forme cylindrique. Un ciment de même composition que le ciment de joint est déposé à la périphérie du filtre usiné selon une épaisseur moyenne de 1mm afin de lisser la surface externe des filtres de forme cylindrique. The assembly is then machined by abrasion, the most peripheral parts being eliminated in order to constitute assembled filters of cylindrical shape. A cement of the same composition as the joint cement is deposited at the periphery of the machined filter at an average thickness of 1 mm in order to smooth the outer surface of the cylindrical filters.
Une pluralité de filtres assemblés ont ainsi été confectionnés à partir des éléments unitaires .
A plurality of assembled filters have thus been made from the unit elements.
Section Taille des Longueur des Géométrie des Densité de éléments éléments éléments canaux canaux Section Size Length Geometry Density of Elements Elements Elements Channel Channels
(section) (cm) internes (c/cm2)(section) (cm) internal (c / cm 2 )
(mm x mm) (mm x mm)
carrée 35,8 35,8 25,4 « Wavy » Environ 30 square 35.8 35.8 25.4 "Wavy" About 30
Nombre Epaisseur du Diamètre Epaisseur des Epaisseur d' éléments j oint final du parois moyenne E des assemblés (mm) filtre internes parois assemblé (mm) (μπι) externes Number Thickness of Thickness Thickness of Thickness of elements final joint of the average wall E of assemblies (mm) external filter internal walls (mm) (μπι) external
(μπι) (Μπι)
16 1,2 144 370 65016 1.2 144 370 650
Surépaisseur Epaisseur Epaisseur max Epaisseur max li ec selon la totale Ec ei e2 (mm) bissectrice selon la (μπι) (μπι) Thickness Thickness max Thickness max li e c according to the total E c ei e 2 (mm) bisector according to (μπι) (μπι)
(μπι) bissectrice (μπι) bisector
(μπι) (Μπι)
420 1136 300 300 10 420 1136 300 300 10
12 Rayon de 1 2 Ray of
(mm) courbure R (mm) curvature R
(mm) (Mm)
10 2 10 2
Tableau 1 Lors de l'étape de redimensionnement des filtres, contrairement aux filtres connus de l'art, il n'a été constaté aucun arrachement des éléments unitaires périphériques des structures pré-assemblées, sous les forces permettant l'abrasion des parties périphériques du filtre. Un tel résultat indique sans conteste que les éléments filtrants polygonaux selon la présente l'invention, présentant un supplément de matière poreuse sur les faces externes des coins, permettent d'améliorer de manière significative de la cohésion des éléments filtrants au sein de la structure, notamment lorsque celle-ci doit être soumise à des contraintes mécaniques radiales importantes. Table 1 In the step of resizing the filters, unlike the filters known in the art, there was no evidence of tearing of the peripheral unit elements of the pre-assembled structures, under the forces allowing the abrasion of the peripheral parts of the filtered. Such a result clearly indicates that the polygonal filter elements according to the present invention, having a supplement of porous material on the outer faces of the corners, make it possible to significantly improve the cohesion of the filtering elements within the structure, especially when it must be subjected to significant radial mechanical stresses.
Dans la description qui précède, les avantages de la présente invention ont été principalement exposés en relation avec les structures en nid d'abeille utilisées comme filtres à particules dans une ligne d'échappement d'un moteur à combustion interne, permettant l'élimination des suies produites par la combustion d'un carburant diesel ou essence.
L'invention n'est bien évidemment pas limitée à une telle application et trouve également son application dans tous les domaines où les problèmes précédemment exposés se posent, en particulier dans le domaine des échangeurs thermiques.
In the foregoing description, the advantages of the present invention have been mainly exposed in relation to the honeycomb structures used as particulate filters in an exhaust line of an internal combustion engine, allowing the elimination of soot produced by the combustion of a diesel fuel or gasoline. The invention is obviously not limited to such an application and also finds application in all areas where the previously discussed problems arise, particularly in the field of heat exchangers.
Claims
1. Élément monolithique en nid d'abeille (1) comprenant un ensemble de conduits adjacents (2,3) d'axes parallèles entre eux séparés par des parois internes (4) faites dans une matière poreuse, ledit élément (1) présentant, selon une coupe transversale, une section polygonale, notamment quadratique, délimitée par des éléments de parois extérieures (6-9), ledit élément se caractérisant en ce qu'au moins un coin (11) dudit polygone, de préférence tous les coins du polygone, présente, selon la bissectrice (13) de 1 ' angle au niveau dudit coin (11), une surépaisseur ec, de telle sorte que l'épaisseur totale Ec de la paroi externe, également mesurée selon ladite bissectrice (13) de l'angle au niveau dudit coin (11), soit supérieure à l'épaisseur moyenne E desdites parois extérieures d'un facteur d'au moins 1,43, ladite surépaisseur ec étant obtenue au moins pour partie par un supplément (10) de matière sur la face externe dudit coin. A monolithic honeycomb element (1) comprising a set of adjacent conduits (2, 3) with mutually parallel axes separated by internal walls (4) made of a porous material, said element (1) having, in a cross section, a polygonal section, in particular quadratic, delimited by outer wall elements (6-9), said element being characterized in that at least one corner (11) of said polygon, preferably all corners of the polygon , according to the bisector (13) of the angle at said wedge (11), has an excess thickness e c , so that the total thickness E c of the external wall, also measured along said bisector (13) of the angle at said corner (11) is greater than the average thickness E of said outer walls by a factor of at least 1.43, said excess thickness e c being obtained at least partly by a supplement (10) of material on the outer face of said corner.
2. Élément monolithique selon la revendication 1 présentant une section, selon une coupe transversale, de forme sensiblement quadratique ou triangulaire et dont les coins présentent des angles d'ouverture au sommet a compris entre 60 et 120°. 2. A monolithic element according to claim 1 having a section, in a cross section, of substantially quadratic or triangular shape and whose corners have aperture angles at the apex of between 60 and 120 °.
3. Élément monolithique selon l'une des revendications 1 ou 2, présentant une section, selon une coupe transversale, de forme sensiblement carrée. 3. monolithic element according to one of claims 1 or 2, having a section in a cross section, substantially square shape.
4. Élément monolithique selon l'une des revendications 1 à 3 dans lequel ladite surépaisseur présente un bord externe sensiblement arrondie s' inscrivant dans un rayon de courbure R compris entre 0,3 et 3 mm. 4. monolithic element according to one of claims 1 to 3 wherein said extra thickness has a substantially rounded outer edge s' enrolling in a radius of curvature R between 0.3 and 3 mm.
5. Élément monolithique selon l'une des revendications précédente, dans lequel selon une coupe transversale, ladite surépaisseur (10) s'étend sur une longueur li et présente une valeur maximale ei selon le premier élément de paroi (7) constituant le coin et sur une longueur 12 et présente une valeur maximale e2 selon le second élément de paroi (6) constituant le coin, et dans lequel : 5. Monolithic element according to one of the preceding claims, wherein in a cross section, said extra thickness (10) extends over a length li and has a maximum value ei according to the first wall element (7) constituting the corner and over a length 1 2 and has a maximum value e 2 according to the second wall element (6) constituting the corner, and wherein:
6. Élément monolithique selon la revendication précédente, dans lequel les longueurs li et 12 sont sensiblement égales et/ou dans lequel les surépaisseurs ei et e2 sont sensiblement égales. 6. monolithic element according to the preceding claim, wherein the lengths li and 1 2 are substantially equal and / or wherein the thicknesses ei and e 2 are substantially equal.
7. Élément monolithique selon l'une des revendications précédentes dans lequel le rapport de l'épaisseur totale Ec de la paroi externe, mesurée selon la bissectrice de l'angle au niveau dudit coin (11), sur l'épaisseur moyenne E desdites parois est supérieur ou égal à 1,45, de préférence supérieur à 1,5, et de manière très préférée supérieur à 1,6. 7. Monolithic element according to one of the preceding claims wherein the ratio of the total thickness E c of the outer wall, measured along the bisector of the angle at said corner (11), on the average thickness E of said walls is greater than or equal to 1.45, preferably greater than 1.5, and very preferably greater than 1.6.
8. Elément monolithique selon l'une des revendications précédentes, dans lequel l'épaisseur moyenne E des parois externes des canaux est comprise entre 100 et 1000 microns. 8. Monolithic element according to one of the preceding claims, wherein the average thickness E of the outer walls of the channels is between 100 and 1000 microns.
9. Elément monolithique selon l'une des revendications précédentes, dans lequel lesdits conduits sont obturés par des bouchons à l'une ou l'autre de leurs extrémités pour délimiter des conduits d'entrée (2) s ' ouvrant suivant une face d'admission des gaz et des conduits de sortie (3) s ' ouvrant suivant une face d'évacuation des gaz, de telle façon que le gaz traverse les parois poreuses (4) . 9. monolithic element according to one of the preceding claims, wherein said ducts are closed by plugs at one or the other of their ends to define inlet ducts (2) s 'opening on a side d' intake of gases and outlet pipes (3) opening on a gas evacuation face, in such a way that the gas passes through the porous walls (4).
10. Elément monolithique selon l'une des revendications précédentes, dans lequel ladite surépaisseur (10) est présente sur toute la longueur de l'élément. 10. Monolithic element according to one of the preceding claims, wherein said thickness (10) is present over the entire length of the element.
11. Elément monolithique selon l'une des revendications précédentes, dans lequel la matière poreuse est du carbure de silicium (SiC) ou du nitrure de silicium. Monolithic element according to one of the preceding claims, wherein the porous material is silicon carbide (SiC) or silicon nitride.
12. Structure assemblée, notamment filtre à particules, obtenu par 1 ' assemblage d ' une pluralité d ' éléments monolithiques selon l'une des revendications précédentes, lesdits éléments étant liés par un ciment de joint. 12. Assembled structure, in particular particulate filter, obtained by one assembly of a plurality of monolithic elements according to one of the preceding claims, said elements being bonded by a joint cement.
13. Structure assemblée selon la revendication précédente, dans laquelle le rapport de la surépaisseur ei sur l'épaisseur moyenne du ciment de joint entre deux éléments constitutifs, selon ledit plan transversal, est inférieur ou égal à 0,4 et/ou dans lequel le rapport de la surépaisseur e2 sur l' épaisseur moyenne de ciment de joint, selon ledit plan transversal, est inférieur ou égal à 0,4. 13. Assembled structure according to the preceding claim, wherein the ratio of the excess thickness ei on the average thickness of the joint cement between two constituent elements, according to said transverse plane, is less than or equal to 0.4 and / or in which the ratio of the excess thickness e 2 on the average thickness of cement joint, according to said transverse plane, is less than or equal to 0.4.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1158187A FR2979837B1 (en) | 2011-09-14 | 2011-09-14 | HONEYCOMB ELEMENT HAS REINFORCED CORNERS |
PCT/FR2012/052034 WO2013038103A1 (en) | 2011-09-14 | 2012-09-12 | Honeycomb element with reinforced corners |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2755741A1 true EP2755741A1 (en) | 2014-07-23 |
Family
ID=47022956
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12773022.4A Withdrawn EP2755741A1 (en) | 2011-09-14 | 2012-09-12 | Honeycomb element with reinforced corners |
Country Status (4)
Country | Link |
---|---|
US (1) | US9546115B2 (en) |
EP (1) | EP2755741A1 (en) |
FR (1) | FR2979837B1 (en) |
WO (1) | WO2013038103A1 (en) |
Citations (5)
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US4294806A (en) * | 1979-02-14 | 1981-10-13 | Sakai Chemical Industry Co., Ltd. | Method for preventing the wear of a monolithic catalyst by dusts |
WO1994009901A1 (en) * | 1992-11-04 | 1994-05-11 | Technische Universiteit Delft | Catalyst element, reactor comprising such catalyst element, die for producing such catalyst element, and method for the hydrogenating conversion of an oil |
WO2002079346A2 (en) * | 2001-03-30 | 2002-10-10 | Corning Incorporated | Hydrotreating process and catalyst |
US20040170804A1 (en) * | 2002-02-28 | 2004-09-02 | Niknafs Hassan S. | Ceramic packing element with enlarged fluid flow passages |
EP1586375A1 (en) * | 2004-03-15 | 2005-10-19 | Vereinigte Füllkörper-Fabriken GmbH & Co. KG | Packing element |
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US5761787A (en) | 1995-11-30 | 1998-06-09 | Corning Incorporated | Method of making bonded pin extrusion die |
EP1270202B1 (en) | 1996-01-12 | 2006-04-26 | Ibiden Co., Ltd. | Filter for purifying exhaust gas |
WO2001023069A1 (en) | 1999-09-29 | 2001-04-05 | Ibiden Co., Ltd. | Honeycomb filter and ceramic filter assembly |
JP3889194B2 (en) | 2000-01-13 | 2007-03-07 | 日本碍子株式会社 | Honeycomb structure |
FR2833857B1 (en) | 2001-12-20 | 2004-10-15 | Saint Gobain Ct Recherches | FILTER BODY COMPRISING A PLURALITY OF FILTER BLOCKS, IN PARTICULAR FOR A PARTICLE FILTER |
JP4723173B2 (en) | 2003-01-20 | 2011-07-13 | 日本碍子株式会社 | Manufacturing method of honeycomb structure |
JP4267947B2 (en) * | 2003-03-19 | 2009-05-27 | 日本碍子株式会社 | Honeycomb structure |
FR2853256B1 (en) | 2003-04-01 | 2005-10-21 | Saint Gobain Ct Recherches | FILTRATION STRUCTURE, PARTICULARLY PARTICLE FILTER FOR THE EXHAUST GASES OF AN INTERNAL COMBUSTION ENGINE. |
FR2857696B1 (en) | 2003-07-18 | 2005-10-21 | Saint Gobain Ct Recherches | FILTER BLOCK FOR FILTRATION OF PARTICLES CONTAINED IN THE EXHAUST GASES OF AN INTERNAL COMBUSTION ENGINE. |
FR2864576B1 (en) | 2003-12-24 | 2006-03-03 | Saint Gobain Ct Recherches | BLOCK FOR FILTRATION OF PARTICLES CONTAINED IN THE EXHAUST GASES OF AN INTERNAL COMBUSTION ENGINE |
JP4731993B2 (en) | 2005-05-18 | 2011-07-27 | 日本碍子株式会社 | Manufacturing method of honeycomb structure |
JP4863995B2 (en) * | 2005-06-24 | 2012-01-25 | イビデン株式会社 | Honeycomb structure |
FR2906159B1 (en) * | 2006-09-27 | 2008-10-31 | Saint Gobain Ct Recherches | MONOLITHIC ELEMENT WITH REINFORCED CORNERS FOR FILTRATION OF PARTICLES |
WO2008126334A1 (en) | 2007-03-30 | 2008-10-23 | Ibiden Co., Ltd. | Process for producing honeycomb structure |
DE102009038049A1 (en) * | 2009-08-19 | 2011-03-10 | Saint-Gobain Industriekeramik Rödental GmbH | Filter element, particulate filter, method for marking a filter element, method for producing a particulate filter and use of a filter element |
-
2011
- 2011-09-14 FR FR1158187A patent/FR2979837B1/en not_active Expired - Fee Related
-
2012
- 2012-09-12 EP EP12773022.4A patent/EP2755741A1/en not_active Withdrawn
- 2012-09-12 US US14/344,273 patent/US9546115B2/en not_active Expired - Fee Related
- 2012-09-12 WO PCT/FR2012/052034 patent/WO2013038103A1/en active Application Filing
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US4294806A (en) * | 1979-02-14 | 1981-10-13 | Sakai Chemical Industry Co., Ltd. | Method for preventing the wear of a monolithic catalyst by dusts |
WO1994009901A1 (en) * | 1992-11-04 | 1994-05-11 | Technische Universiteit Delft | Catalyst element, reactor comprising such catalyst element, die for producing such catalyst element, and method for the hydrogenating conversion of an oil |
WO2002079346A2 (en) * | 2001-03-30 | 2002-10-10 | Corning Incorporated | Hydrotreating process and catalyst |
US20040170804A1 (en) * | 2002-02-28 | 2004-09-02 | Niknafs Hassan S. | Ceramic packing element with enlarged fluid flow passages |
EP1586375A1 (en) * | 2004-03-15 | 2005-10-19 | Vereinigte Füllkörper-Fabriken GmbH & Co. KG | Packing element |
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Also Published As
Publication number | Publication date |
---|---|
WO2013038103A1 (en) | 2013-03-21 |
US20140356570A1 (en) | 2014-12-04 |
FR2979837A1 (en) | 2013-03-15 |
FR2979837B1 (en) | 2013-08-23 |
US9546115B2 (en) | 2017-01-17 |
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