WO2003101585A1 - Corps a structure en nid d'abeille - Google Patents
Corps a structure en nid d'abeille Download PDFInfo
- Publication number
- WO2003101585A1 WO2003101585A1 PCT/JP2003/005972 JP0305972W WO03101585A1 WO 2003101585 A1 WO2003101585 A1 WO 2003101585A1 JP 0305972 W JP0305972 W JP 0305972W WO 03101585 A1 WO03101585 A1 WO 03101585A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- honeycomb
- honeycomb structure
- partition
- partition wall
- outer peripheral
- Prior art date
Links
- 238000005192 partition Methods 0.000 claims abstract description 147
- 230000002093 peripheral effect Effects 0.000 claims description 47
- 238000005304 joining Methods 0.000 claims description 9
- 241000264877 Hippospongia communis Species 0.000 description 223
- 238000000746 purification Methods 0.000 description 14
- 239000000463 material Substances 0.000 description 13
- 239000000919 ceramic Substances 0.000 description 7
- 230000000052 comparative effect Effects 0.000 description 6
- 238000001125 extrusion Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 6
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 6
- 229910010271 silicon carbide Inorganic materials 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000003054 catalyst Substances 0.000 description 5
- 239000004568 cement Substances 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 230000008646 thermal stress Effects 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 239000007767 bonding agent Substances 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 239000004927 clay Substances 0.000 description 2
- 229910052878 cordierite Inorganic materials 0.000 description 2
- 239000013078 crystal 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
- 230000000694 effects Effects 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 230000001747 exhibiting effect Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 150000002484 inorganic compounds Chemical class 0.000 description 2
- 229910010272 inorganic material Inorganic materials 0.000 description 2
- 239000011812 mixed powder Substances 0.000 description 2
- 229910052863 mullite Inorganic materials 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000008929 regeneration Effects 0.000 description 2
- 238000011069 regeneration method Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 229910052845 zircon Inorganic materials 0.000 description 2
- 229910000505 Al2TiO5 Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000009924 canning Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 229920000609 methyl cellulose Polymers 0.000 description 1
- 239000001923 methylcellulose Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 1
- 229920005591 polysilicon Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D39/00—Filtering material for liquid or gaseous fluids
- B01D39/14—Other self-supporting filtering material ; Other filtering material
- B01D39/20—Other self-supporting filtering material ; Other filtering material of inorganic material, e.g. asbestos paper, metallic filtering material of non-woven wires
- B01D39/2068—Other inorganic materials, e.g. ceramics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
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- B01D39/14—Other self-supporting filtering material ; Other filtering material
- B01D39/20—Other self-supporting filtering material ; Other filtering material of inorganic material, e.g. asbestos paper, metallic filtering material of non-woven wires
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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
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- B01D46/2418—Honeycomb filters
- B01D46/2425—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material
- B01D46/2429—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material of the honeycomb walls or cells
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- 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
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- B01D46/2425—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material
- B01D46/24491—Porosity
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
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- 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
- B01D46/247—Honeycomb filters characterized by the geometrical structure, shape, pattern or configuration or parameters related to the geometry of the structure of the cells
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- 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
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
- B01D53/34—Chemical or biological purification of waste gases
- B01D53/74—General processes for purification of waste gases; Apparatus or devices specially adapted therefor
- B01D53/86—Catalytic processes
- B01D53/88—Handling or mounting catalysts
- B01D53/885—Devices in general for catalytic purification of waste gases
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
- F01N3/022—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous
- F01N3/0222—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous the structure being monolithic, e.g. honeycombs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2807—Metal other than sintered metal
- F01N3/281—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2825—Ceramics
- F01N3/2828—Ceramic multi-channel monoliths, e.g. honeycombs
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- 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
- B01D46/2425—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material
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- 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
- B01D46/2484—Cell density, area or aspect ratio
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B1/00—Producing shaped prefabricated articles from the material
- B28B1/002—Producing shaped prefabricated articles from the material assembled from preformed elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
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- F01N2330/00—Structure of catalyst support or particle filter
- F01N2330/30—Honeycomb supports characterised by their structural details
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2450/00—Methods or apparatus for fitting, inserting or repairing different elements
- F01N2450/28—Methods or apparatus for fitting, inserting or repairing different elements by using adhesive material, e.g. cement
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- 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 present invention relates to a honeycomb structure. More specifically, the present invention relates to a honeycomb structure configured by combining a plurality of honeycomb segments.
- the ceramic honeycomb structure is applied to combustion equipment such as boilers, internal heat engines such as diesel engines, chemical reaction equipment, and reformers for fuel cells, etc., taking advantage of the properties of ceramics that have excellent heat resistance. It is widely used in various applications such as catalysts and catalysts for collecting and removing particulate matter in exhaust gas.
- honeycomb structures are installed in the case with their outer peripheral sides gripped, but they are installed with their outer periphery gripped with a large force, such as when they are installed near an engine that continuously receives large vibrations. Often do. Therefore, it is extremely important in practical use that the compressive strength on the outer peripheral side surface is large so that even if it is gripped with a relatively large force and installed in the case, it is not damaged.
- a filter regeneration step of burning and removing carbon fine particles accumulated in the honeycomb structure is performed.
- the honeycomb structure is exposed to a local increase in temperature.
- the honeycomb structure locally increases in thermal stress due to a thermal expansion difference between each part. Therefore, there is a problem that cracks and the like are likely to occur in a relatively short-term use.
- the purification performance is improved by further reducing the heat capacity, reducing the pressure loss, or improving the collection efficiency. Dramatic improvements are required, and in response to this, thinner walls and higher porosity of the honeycomb structure are being developed.
- honeycomb segments are formed so as to have a desired shape.
- a honeycomb structure manufactured by bonding via a wire see Japanese Patent Publication No. Sho 61-512240 and Japanese Patent Laid-Open Publication No. Hei 8-282246).
- the partition wall on the outer peripheral portion is provided so as to provide sufficient compressive strength.
- a structure in which the partition wall is thicker than the inner partition wall or a structure in which the porosity of the partition wall is reduced has been proposed (Japanese Patent Application Laid-Open Nos. 54-15046 and 555-147). 154, etc.).
- the partition wall thickness and cell density are greatly changed during extrusion, the difference in extrusion resistance at each part of the honeycomb structure increases, and the resulting honeycomb structure has poor molding. There is a problem that is easy to occur.
- the material used for the corresponding portion is usually replaced with a material having a smaller porosity.
- the present invention has been made in view of the above-mentioned problems, and an object of the present invention is to highly suppress the occurrence of cracks and the like at the time of using a honeycomb structure; High performance such as purification performance while maintaining compressive strength An object of the present invention is to provide a honeycomb structure that can exhibit its effects.
- the present inventors have conducted intensive studies to solve the above-mentioned problems, and as a result, first, for each honeycomb segment, the structure that contributes to compressive strength such as partition wall thickness, partition wall density, cell density, or cell shape was changed. However, they have found that by forming the outer periphery of a honeycomb structure with a honeycomb segment having a large compressive strength, it is possible to solve the problems such as poor molding of a conventional honeycomb structure integrally manufactured as a whole. Further, the present inventor further studied and found that a honeycomb structure in which a plurality of honeycomb segments were joined when the case was used while being held in a case, was formed by the presence of a joining material such as cement.
- the stress applied to one honeycomb segment by the gripping of the honeycomb structure can be reduced only by the deformation of the partition wall in the honeycomb segment, and the stress can be reduced by the deformation of the partition wall of the entire honeycomb structure. It was found that, unlike the honeycomb structure manufactured in the above, the difference in compressive strength is likely to occur in each honeycomb segment due to its structural characteristics.
- the length direction of the partition wall in the cross section perpendicular to the flow direction of the flow hole was the position where each partition wall was connected to the outer peripheral wall, and the outer peripheral tangent of the honeycomb structure was It was discovered that the honeycomb segments including the partition walls of 20 to 70 ° were selectively generated, and by applying a structure to increase the compressive strength of only the honeycomb segments, the conventional problem described above was obtained. Has been found, and the present invention has been completed.
- a plurality of partition walls intersect each other at right angles, and the cross-sectional shape defined by the partition walls (meaning the cross-sectional shape in a direction perpendicular to the direction of the flow passage of the through-hole) is rectangular.
- a honeycomb structure including a joined body of a plurality of honeycomb segments in which a plurality of flow holes are formed,
- At least a part of a honeycomb segment constituting at least a part of an outer peripheral portion of the honeycomb structure has a structure having a higher compressive strength than a honeycomb segment constituting another part of the honeycomb structure.
- a honeycomb structure is provided.
- compressive strength means a pressure that causes breakage in each honeycomb segment when a honeycomb structure in which each honeycomb segment is joined is pressed by hydrostatic pressure.
- the compressive strength here mainly depends on the flow hole flow direction. For vertical pressure.
- the partition wall length direction in a cross section perpendicular to the flow path direction of the flow hole (hereinafter, may be simply referred to as “partition wall length direction”) ),
- the honeycomb segment including the partition wall at an angle of 20 ° to 70 ° with respect to the outer peripheral tangent of the honeycomb structure at the position where each partition wall is connected to the outer peripheral wall is formed by other portions of the honeycomb structure. It is preferable to provide a structure having a higher compressive strength than the honeycomb segment constituting the above.
- the partition wall length direction is set to 20 to 50 with respect to the outer peripheral tangent of the 82-cam structure at the position where each partition connects to the outer peripheral wall.
- the honeycomb segment including the partition walls at an angle of 70 ° is formed of partition walls having an average partition wall thickness larger than that of the honeycomb segments forming the other portions of the honeycomb structure, or other portions of the honeycomb structure. It is preferable that the honeycomb structure is constituted by partition walls having a smaller porosity than the 82 cam segments or the cell density is larger than the honeycomb segments constituting other portions of the honeycomb structure.
- the partition wall length direction is set to 20 to 100 with respect to the outer peripheral tangent of the honeycomb structure at the position where each partition connects to the outer peripheral wall.
- the honeycomb segment including the partition walls having an angle of 70 ° further includes partition walls connecting diagonal sides of the respective flow holes having a rectangular cross-sectional shape, and a flow hole having a triangular radial cross-sectional shape is provided between the partition walls.
- a plurality of partition walls intersect perpendicularly with each other, and a plurality of honeycomb segments each having a plurality of rectangular through-holes formed in a radial cross section are joined between the partition walls.
- a honeycomb structure wherein the outer periphery of the honeycomb structure is arranged such that the partition wall length direction is 0 ° or more and less than 20 ° with respect to the outer peripheral tangent of the honeycomb structure at a position where each partition is connected to the outer peripheral wall, or 7
- a honeycomb structure characterized by being formed of a honeycomb segment consisting of only partition walls which are larger than 0 ° and equal to or smaller than 90 °.
- the honeycomb segments that constitute the honeycomb structure are changed on a per-unit basis. Therefore, the material and the like can be easily changed in each part of the honeycomb structure, and the density of the partition walls can be largely changed. Similarly, it is possible to obtain a honeycomb structure in which the partition walls are not deformed at all even when the partition wall thickness or the cell density is largely changed.
- the partition thickness Since the partition wall density and the cell density are increased, high purification performance and the like can be exhibited while maintaining the desired compressive strength.
- FIG. 1A is a top view schematically showing one embodiment of the honeycomb structure according to the present invention
- FIGS. 1B and 1C are partially enlarged views.
- FIG. 2 schematically shows a positional relationship between a partition wall length direction of a honeycomb structure radial cross section in each honeycomb segment partition wall and an outer circumferential tangent of an 82-cam structure in the honeycomb structure according to the present invention. It is a partially enlarged view.
- FIG. 3 is a graph showing the results of the compressive strength of the honeycomb structure of Example 1 and the honeycomb structure of Comparative Example 1.
- FIG. 1 (a) is a top view schematically showing an embodiment of a honeycomb structure according to the present invention
- FIGS. 1 (b) and 1 (c) each show a specific position of the honeycomb structure.
- FIG. 2 is a partially enlarged view of a honeycomb segment.
- FIG. 2 schematically shows a positional relationship between a partition wall length direction in each honeycomb segment and an outer peripheral tangent of the honeycomb structure in the honeycomb structure according to the present invention.
- a honeycomb structure 10 of the present invention is formed by joining a plurality of honeycomb segments 1 and 2 each having a plurality of flow holes 4 having a rectangular cross section between a plurality of partition walls 3. At least a portion 1a of the honeycomb segment 1 constituting the outer periphery 5 of the body 10 has a structure having a higher compressive strength than the honeycomb segment 2 constituting the other part of the honeycomb structure 10 .
- the 82 cam structure 10 in the present invention is composed of a plurality of honeycomb segments having at least different physical properties, for example, a segment 1 mainly arranged in a peripheral portion and a segment 2 mainly arranged in a central portion. Even if the honeycomb structure is made of a material with a high coefficient of thermal expansion such as SiC, it is possible to reduce the occurrence of local thermal stress during use and prevent the occurrence of cracks etc. Further, in each of the honeycomb segments constituting the joined body according to the present invention, the cross-sectional shape of the plurality of flow holes 4 defined between the partition walls 3 which intersect each other at right angles is quadrangular, that is, square or rectangular. Therefore, not only is it extremely easy to manufacture a die for extrusion molding of each segment, but also the thermal shock resistance of the obtained honeycomb structure can be improved.
- 1 a which is a kind of a series of honeycomb segments 1 arranged to constitute the outer periphery 5, constitutes the outer periphery 5 of the honeycomb structure 10. It has a structure with higher compressive strength than the honeycomb segment 2 which is a segment other than the segment used for the construction (hereinafter sometimes referred to as “high-strength structure”). With this configuration, as in the case of manufacturing an integrated honeycomb structure having partition walls having different thicknesses depending on positions, A honeycomb structure having a desired compressive strength can be manufactured without causing any deformation of the partition walls due to the extrusion resistance difference.
- the high-strength structure is such that the partition wall length direction in a cross section perpendicular to the flow direction of the flow hole 4 is aligned with the outer peripheral tangent T of the honeycomb structure 10.
- a honeycomb segment including the partition wall 3a having the above-described angle hereinafter simply referred to as “ It is preferable to dispose 1a, and to form the partition wall 3a in which the partition wall length direction X is at an angle of 30 to 60 ° with respect to the outer peripheral tangent line T. It is more preferable to arrange the honeycomb segments 1a including the partition walls 3a in which the partition wall length direction X is at an angle of 40 to 50 ° with respect to the outer peripheral tangent line T. Is particularly preferred.
- the honeycomb segment la including the partition wall 3a in which the partition wall length direction X in the cross section perpendicular to the flow direction of the flow hole is within the above range has extremely high compressive strength. Because of its small size, the location is intensively reinforced with honeycomb segment 1a to effectively increase the compressive strength while minimizing the increase in heat capacity and pressure loss, or reduction in collection efficiency As a result, high purification performance can be achieved in response to the demands of increasingly strict times.
- segment 1a is located at the site where the first compression break occurs when a compressive load is applied to the whole, because the compression during canning is applied from an oblique direction (so-called C axis). Therefore, the effect of increasing the strength while minimizing other effects by exerting intensive reinforcement here is exhibited.
- the average thickness of the partition walls is smaller than that of lb or 2 which is a honeycomb segment constituting another portion of the honeycomb structure. Thick ones, those having a small average porosity of the partition walls, or those having a large cell density can be provided as the low-strength honeycomb segments 1a.
- the high-strength structure may be composed of the low-strength honeycomb segment 1a using only one of the segments having the above-described properties. It is preferable to provide a combination of two or more of these high-strength structures in that the compression strength can be secured without impairing the performance such as purification performance by strengthening.
- the thickness of the partition walls of each of the honeycomb segments 1 and 2 is not particularly limited, but local breakage of the partition walls while exhibiting a desired purification performance by suppressing a pressure loss, an increase in heat capacity, and the like is suppressed.
- the ratio of the thickness of the partition wall 3a of the low-strength honeycomb segment 1a to the partition wall thickness of the other honeycomb segments 1b and 2 is preferably from 1.1 to 5.0, more preferably from 1.2 to 3.0, and particularly preferably from 1.2 to 2.0.
- each honeycomb segment including 1a has a maximum partition wall thickness as long as the above relationship is satisfied, in order to suppress a pressure loss and an increase in heat capacity and to exhibit a desired purification performance.
- the average porosity of the partition walls 3 constituting each honeycomb segment there is no particular limitation on the average porosity of the partition walls 3 constituting each honeycomb segment.
- the average porosity of the bulkhead 3a that constitutes the low-strength honeycomb segment 1a and the average porosity of the bulkhead 3b that constitutes the basic honeycomb segments 1b and 2 Is preferably 5 to 90% smaller, more preferably 10 to 70% smaller, and particularly preferably 10 to 45% smaller.
- the average porosity of the partition walls is 5 to 80 in order to secure pressure loss and desired mechanical strength.
- the cell density of each honeycomb segment there is no particular limitation on the cell density of each honeycomb segment.
- the cell density of the low-strength honeycomb segment 1a is reduced. Is preferably increased by 10 to 40% with respect to the cell density of the basic honeycomb segments 1 b and 2, and 15 to 200%. % Is more preferable, and 20 to 100% is particularly preferable.
- the cell density is from 100 to 150 Cells / in 2 (15.5 to 22.5 cells / cm 2 ), preferably 150 to: L 2 0 cells in 2 (23.3 to 186.0 cells Z cm 2) ) Is more preferable, and 200 to 900 cells in 2 (31.0 to 139.5 cells Z cm 2 ) is particularly preferable.
- the high-strength structure is provided in units of honeycomb segments, a honeycomb structure having a high-strength structure can be obtained without deformation of a partition wall during molding or the like.
- the average partition wall thickness of the low-strength honeycomb segment 1a And the ratio of the average partition wall thickness of the basic honeycomb segments 1 b and 2 to 1.4 to 2.0, or the porosity of the partition walls constituting the low-strength honeycomb segment 1 a constitutes the basic honeycomb segments 1 b and 2.
- the low-strength honeycomb segment 1a further includes a partition wall connecting the diagonal of each flow hole having a rectangular cross-section, and a flow hole having a triangular cross-section between the partition walls. Can be mentioned.
- the ratio of providing the flow holes having a triangular cross section is determined by other structures related to compressive strength such as partition wall thickness and porosity, and usage conditions. An appropriate range may be set in consideration of the above.
- the cross-sectional shape of the low-strength honeycomb segment 1a is triangular at a ratio of 10 to 70% in all the flow holes. It is preferable to provide a flow hole, and it is more preferable to provide a flow hole having a triangular cross section at a ratio of 30 to 50%.
- the partition length direction in a cross section perpendicular to the flow direction of the flow hole as shown in FIG. X is the honeycomb segment 1a including the partition 3a having the above range with respect to the outer peripheral tangent T of the honeycomb structure 10 at the position where each partition 3 is connected to the outer peripheral wall 5, and the partition having the partition outside the range is included.
- the outer periphery 5 of the honeycomb structure 10 is divided by a honeycomb segment including the honeycomb segment, and the partition wall length direction X in a cross section perpendicular to the flow direction of the circulation hole is such that each partition is connected to the outer peripheral wall.
- honeycomb structure consisting of only the partition walls having an angle of 0 ° or more and less than 20 ° or greater than 70 ° and 90 ° or less with respect to the outer peripheral tangent line T of the honeycomb structure 10 at the position C. To list It can be.
- a desired compressive strength can be obtained without any change in the partition wall thickness and the porosity of the partition walls described above, so that it is possible to further suppress pressure loss and increase in heat capacity. It is possible to exhibit higher purification performance and the like.
- the partition wall length direction X can be adjusted for each of the honeycomb segments 1 and 2, it is not necessary to manufacture a die having a complicated shape, unlike a honeycomb structure integrally manufactured. Also, no deformation of the partition walls due to the extrusion resistance difference occurs during molding.
- the honeycomb segments 1 constituting the outer periphery of the honeycomb structure 10 are arranged such that the partition wall length direction X is equal to the outer circumference at a position C where each partition is connected to the outer peripheral wall.
- the partition wall is formed of only a partition wall having an angle of 0 ° or more and less than 20 ° with respect to the tangent line or an angle greater than 70 ° and 90 ° or less, and the length direction of the partition wall is 0 ° with respect to the outer peripheral tangent line. More preferably, it is less than 15 °, or more than 75 ° and 90 ° or less.
- the honeycomb structure of the present invention may be provided with another high-strength structure as long as the structure can increase the compressive strength.
- the object of the present invention can be achieved even if the material strength is improved by coating or impregnating the honeycomb structure with a catalyst supported on alumina or the like.
- the material of the honeycomb segments 1 and 2 is, for example, non-oriented Cordierite, Oriented Cordierite, Mullite-Zircon, Mullite, Zircon, Cordierite-Mullite, Mullite-Aluminum Titanate, Cr-Polysilicon Carbide, Silicon Carbide, Metallic Silicon and Zirconia Earth Spinel Ceramics with at least one selected from the group consisting of a main crystal phase can be cited.
- heat resistance and heat conductivity are excellent, and high thermal conductivity of the entire filter is secured to reduce thermal stress in each part of the filter.
- silicon carbide or silicon carbide or metal silicon and silicon carbide are main crystals, it is preferable.
- the number of the honeycomb segments 1 and 2 constituting the honeycomb structure 10 is not particularly limited. However, in order to reduce the generation of local thermal stress, nine or more honeycomb segments 1 and 2 are used. , 2 preferably form the honeycomb structure 10. In addition, in order to improve the strength of only the portion that is likely to be damaged during gripping and not to reduce the basic performance such as purification performance, the outer periphery 5 of the honeycomb structure 10 is made of eight or more honeycombs. It is preferable that the honeycomb segment 1 be composed of the segments 1, and more preferably that it be composed of 12 or more honeycomb segments 1.
- the shape of the flow hole 4 may be any shape as long as the cross-sectional shape is rectangular, and examples thereof include those having a cross-sectional shape of square or rectangular.
- the cross-sectional shape in the radial direction is rectangular.
- the compressive strength of the honeycomb structure 10 can be improved, so that at least one of the honeycomb segments 1 constituting the outer periphery 5 of the honeycomb structure 10 can be improved.
- the section has a flow hole whose cross section in the radial direction is square.
- honeycomb structure of the present invention When the honeycomb structure of the present invention is used as an exhaust gas purifying filter, a plurality of flow holes 4 in each of the 82-cam segments 1 and 2 are sealed at both end surfaces where the flow holes 4 are opened with a plugging material. May be alternately plugged.
- a metal having a catalytic ability such as Pt; Pd, Rh may be supported on the partition walls 3.
- the honeycomb structure 10 of the present invention is obtained by joining and integrating the above-described honeycomb segments 1 and 2, but there are no particular restrictions on the joining structure, joining material type, and the like. Instead, for example, adjacent honeycomb segments 1a and lb may be joined to each other with a bonding agent 21 on a part of the opposing side surfaces, and the entirety of the opposing side surfaces may be bonded by a bonding agent 21.
- Fig. 1 (a) shows an example where the entire side surface is joined).
- the bonding material 21 is preferably a material containing a heat-resistant inorganic compound as a main component in terms of excellent heat resistance and thermal shock resistance. Examples of the heat-resistant inorganic compound include, for example, at least one of the same ceramics as the honeycomb segments 1 and 2 described above, a fiber material containing metal, or a cement such as hydrated cement or thermosetting cement. Are preferred.
- Each segment constituting the honeycomb structure 10 of the present invention is manufactured by a method usually used for a ceramic honeycomb structure, and is joined by a method used for joining a ceramic structure.
- a clay obtained by mixing a desired amount of water with a raw material obtained by adding a binder and a dispersant to a desired ceramic material is obtained, and a honeycomb segment having a desired shape is formed by extrusion molding or the like, and then dried. After, or after further firing, it can be obtained by joining the honeycomb segments.
- a mixed powder of 75% by weight of SiC powder and 25% by weight of metallic Si powder is used, and 100% by weight of this mixed powder is mixed with 6% by weight of a binder composed of methylcellulose and hydroxypropoxylmethylcellulose.
- Parts, 0.8 part by weight of a surfactant, and 22 parts by weight of water were charged and kneaded by a kneader to obtain a plastic clay.
- this kneaded material is extruded, and as shown in FIGS. 1 (a) and 2, a honeycomb structure corresponding to a shape obtained by dividing a honeycomb structure 10 having a cylindrical appearance into 16 in the axial direction. la, lb and 2 were molded.
- the partition wall length direction X in the cross section perpendicular to the flow direction of the flow hole corresponds to the position where each partition wall 3 is connected to the outer peripheral wall (which forms the outer peripheral wall of the honeycomb structure after joining).
- all the partition walls have a thickness of 0.432 mm, and the external dimensions are 35 mm X 3 5 mm X 1 5 4 mm.
- the thickness of all the partitions was 0.304 mm.
- the cross-sectional shape of the flow hole 4 was square and the cell density was 300 cells / in 2 (46.5 cells Zcm 2 ).
- each honeycomb segment After drying each honeycomb segment with microwaves and hot air, a cement bonding agent is applied to the side surface of each honeycomb segment to bond and integrate each honeycomb segment, and further, in an Ar atmosphere.
- a cement bonding agent By firing at about 1550 ° C, a honeycomb structure of 143m ⁇ X 154mmL was manufactured.
- the porosity of the partition walls constituting each honeycomb segment was almost the same at 52%.
- Example 1 the partition length direction X in the cross section perpendicular to the direction of the flow passage shown in FIGS. 1 and 2 is such that each partition 3 is an outer peripheral wall (the outer peripheral wall of the honeycomb structure after bonding is formed). 4) For the four honeycomb segments 1a including the partition walls that are 20 to 70 ° with respect to the outer peripheral tangent line T at the position connected to 5, except that the partition wall thickness was set to 0.304 mm. A honeycomb structure was manufactured in the same manner as in Example 1.
- Example 1 Five honeycomb structures each manufactured by the manufacturing method described in Example 1 and Comparative Example 1 were manufactured, and the following compressive strengths were evaluated.
- both ends of the honeycomb structure are covered with a metal plate having the same diameter as each honeycomb structure, and a metal plate is fixed with a rubber tube having the same diameter as the honeycomb structure. Rubber tape was attached to the tube and its surroundings, and sealed to prevent water from entering.
- the honeycomb structure of the first embodiment has substantially the same configuration.
- compressive strength is obtained, and that the pressure loss and heat capacity are extremely smaller than the honeycomb structure of the comparative example.
- the occurrence of cracks and the like during use of the honeycomb structure can be highly suppressed, and at the same time, high purification performance and the like can be maintained while maintaining practically sufficient compressive strength. It is possible to provide a honeycomb structure capable of exhibiting the performance described above.
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Description
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Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
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US10/511,899 US7468202B2 (en) | 2002-05-30 | 2003-05-14 | Honeycomb structural body |
EP03723359A EP1508354B1 (en) | 2002-05-30 | 2003-05-14 | Honeycomb structural body |
AU2003235280A AU2003235280A1 (en) | 2002-05-30 | 2003-05-14 | Honeycomb structural body |
KR1020047019322A KR100619128B1 (ko) | 2002-05-30 | 2003-05-14 | 허니컴 구조체 |
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JP2002-157966 | 2002-05-30 | ||
JP2002157966A JP2003340224A (ja) | 2002-05-30 | 2002-05-30 | ハニカム構造体、及びその製造方法 |
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PCT/JP2003/005972 WO2003101585A1 (fr) | 2002-05-30 | 2003-05-14 | Corps a structure en nid d'abeille |
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US (1) | US7468202B2 (ja) |
EP (1) | EP1508354B1 (ja) |
JP (1) | JP2003340224A (ja) |
KR (1) | KR100619128B1 (ja) |
AU (1) | AU2003235280A1 (ja) |
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Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006110413A (ja) * | 2004-10-12 | 2006-04-27 | Ngk Insulators Ltd | ハニカムフィルター |
US20090010817A1 (en) * | 2004-10-12 | 2009-01-08 | Ngk Insulators, Ltd. | Honeycomb filter |
JP2006223983A (ja) * | 2005-02-17 | 2006-08-31 | Ibiden Co Ltd | ハニカム構造体 |
WO2006126507A1 (ja) * | 2005-05-23 | 2006-11-30 | Ngk Insulators, Ltd. | ハニカム構造体 |
EP1955751A4 (en) * | 2005-10-25 | 2009-12-23 | Ngk Insulators Ltd | HONEYCOMB FILTER |
US7674513B2 (en) * | 2006-03-31 | 2010-03-09 | Corning Incorporated | Crack-resistant ceramic honeycomb structures |
WO2007122715A1 (ja) * | 2006-04-20 | 2007-11-01 | Ibiden Co., Ltd. | ハニカム焼成体の検査方法、及び、ハニカム構造体の製造方法 |
JP5346284B2 (ja) * | 2006-05-31 | 2013-11-20 | コーニング インコーポレイテッド | 耐亀裂性セラミック・ハニカム物品及びその製造方法 |
DE602007002470D1 (de) * | 2007-02-28 | 2009-10-29 | Ibiden Co Ltd | Wabenstrukturkörper |
WO2008105081A1 (ja) | 2007-02-28 | 2008-09-04 | Ibiden Co., Ltd. | ハニカムフィルタ |
EP2113643B1 (en) * | 2008-03-24 | 2012-01-25 | Ibiden Co., Ltd. | Honeycomb structured body |
JP5771541B2 (ja) | 2012-01-27 | 2015-09-02 | 株式会社デンソー | ハニカム構造体 |
JP5892911B2 (ja) * | 2012-01-27 | 2016-03-23 | 株式会社デンソー | ハニカム構造体 |
DE102012004924A1 (de) * | 2012-03-10 | 2013-09-12 | Volkswagen Aktiengesellschaft | Abgasnachbehandlungskomponente mit HC-Adsorberfunktion sowie Abgasanlage mit einer solchen |
JP2014180600A (ja) * | 2013-03-18 | 2014-09-29 | Ngk Insulators Ltd | ハニカムフィルタ |
US10112271B2 (en) * | 2015-03-26 | 2018-10-30 | Hamilton Sundstrand Corporation | Compact heat exchanger |
KR102045100B1 (ko) * | 2015-04-14 | 2019-11-14 | 주식회사 엘지화학 | 멤브레인 분리 장치용 텔레스코핑 방지 장치 |
JP6847724B2 (ja) | 2017-03-21 | 2021-03-24 | 日本碍子株式会社 | 目封止ハニカム構造体 |
US10814266B2 (en) * | 2017-11-24 | 2020-10-27 | Ngk Insulators, Ltd. | Honeycomb filter |
JP7002377B2 (ja) | 2018-03-19 | 2022-01-20 | 日本碍子株式会社 | ハニカム構造体 |
JP7057691B2 (ja) | 2018-03-19 | 2022-04-20 | 日本碍子株式会社 | ハニカム構造体 |
JP7061491B2 (ja) | 2018-03-27 | 2022-04-28 | 日本碍子株式会社 | ハニカム構造体 |
US11988471B2 (en) * | 2021-03-27 | 2024-05-21 | Massachusetts Institute Of Technology | Devices and methods for fabrication of components of a multiscale porous high-temperature heat exchanger |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0647617U (ja) * | 1992-08-07 | 1994-06-28 | イビデン株式会社 | 排気ガス浄化装置 |
US5514446A (en) * | 1994-03-11 | 1996-05-07 | Ngk Insulators, Ltd. | Ceramic honeycomb structural body |
JP2002301325A (ja) * | 2001-04-03 | 2002-10-15 | Ngk Insulators Ltd | ハニカム構造体及びそのアッセンブリ |
JP2002326035A (ja) * | 2001-05-02 | 2002-11-12 | Ngk Insulators Ltd | ハニカム構造体、及びそれを用いたハニカムフィルター、コンバーターシステム |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS54110189A (en) | 1978-02-17 | 1979-08-29 | Ngk Insulators Ltd | Ceramic honeycomb structure |
JPS54150406A (en) * | 1978-05-18 | 1979-11-26 | Nippon Soken | Ceramic honeycomb structure |
JPS6052450B2 (ja) * | 1978-08-25 | 1985-11-19 | カシオ計算機株式会社 | Romチエツク方式 |
JPS5546338A (en) * | 1978-09-28 | 1980-04-01 | Ngk Insulators Ltd | Heat and shock resistant, revolving and heat-regenerating type ceramic heat exchanger body and its manufacturing |
JPS55147154A (en) | 1979-05-07 | 1980-11-15 | Ngk Spark Plug Co Ltd | High-strength honeycomb structure |
JPS55155742A (en) * | 1979-05-22 | 1980-12-04 | Ngk Spark Plug Co Ltd | High strength honeycomb structure |
JPS56129043A (en) | 1980-03-14 | 1981-10-08 | Ngk Insulators Ltd | Honeycomb structure of ceramic |
US4436538A (en) * | 1981-04-22 | 1984-03-13 | Nippon Soken, Inc. | Filter for cleaning exhaust gases from diesel engine |
JPS6151240A (ja) | 1984-08-20 | 1986-03-13 | Mitsubishi Electric Corp | デ−タ処理装置 |
JPS62163697A (ja) | 1985-10-28 | 1987-07-20 | マブコ・リミテツド | のう胞性線維症の検出とモノクロ−ナル抗体の使用 |
JPH0356354Y2 (ja) * | 1986-04-08 | 1991-12-18 | ||
JP2659504B2 (ja) | 1991-12-26 | 1997-09-30 | 大阪瓦斯株式会社 | 触媒燃焼装置 |
JP2525312B2 (ja) | 1992-06-19 | 1996-08-21 | 日本スピンドル製造株式会社 | シヤリング機における駆動制御方法 |
JPH07286797A (ja) | 1994-04-18 | 1995-10-31 | Osaka Gas Co Ltd | ハニカム構造体 |
JP3121497B2 (ja) * | 1994-07-14 | 2000-12-25 | イビデン株式会社 | セラミック構造体 |
EP1382442B1 (en) | 1996-01-12 | 2013-04-24 | Ibiden Co., Ltd. | A filter for purifying exhaust gas |
JP3466862B2 (ja) * | 1997-03-28 | 2003-11-17 | 日本碍子株式会社 | セラミックハニカム構造体 |
JP4159155B2 (ja) | 1998-01-22 | 2008-10-01 | 株式会社日本自動車部品総合研究所 | セラミックハニカム構造体および押出金型 |
DE60032391T2 (de) * | 1999-09-29 | 2007-10-11 | Ibiden Co., Ltd., Ogaki | Wabenfömiger Filter und Anordnung von keramischen Filtern |
JP4259703B2 (ja) * | 1999-12-07 | 2009-04-30 | 株式会社デンソー | セラミックスハニカム構造体及びその製造方法 |
DE10024038A1 (de) | 2000-05-13 | 2001-11-22 | Dmc2 Degussa Metals Catalysts | Wabenkörper aus einem keramischen Material mit verbesserter radialer Druckfestigkeit |
JP4473505B2 (ja) | 2000-08-03 | 2010-06-02 | 日本碍子株式会社 | セラミック製ハニカム構造体 |
-
2002
- 2002-05-30 JP JP2002157966A patent/JP2003340224A/ja active Pending
-
2003
- 2003-05-14 AU AU2003235280A patent/AU2003235280A1/en not_active Abandoned
- 2003-05-14 PL PL03371807A patent/PL371807A1/xx unknown
- 2003-05-14 WO PCT/JP2003/005972 patent/WO2003101585A1/ja active Application Filing
- 2003-05-14 EP EP03723359A patent/EP1508354B1/en not_active Expired - Lifetime
- 2003-05-14 KR KR1020047019322A patent/KR100619128B1/ko active IP Right Grant
- 2003-05-14 US US10/511,899 patent/US7468202B2/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0647617U (ja) * | 1992-08-07 | 1994-06-28 | イビデン株式会社 | 排気ガス浄化装置 |
US5514446A (en) * | 1994-03-11 | 1996-05-07 | Ngk Insulators, Ltd. | Ceramic honeycomb structural body |
JP2002301325A (ja) * | 2001-04-03 | 2002-10-15 | Ngk Insulators Ltd | ハニカム構造体及びそのアッセンブリ |
JP2002326035A (ja) * | 2001-05-02 | 2002-11-12 | Ngk Insulators Ltd | ハニカム構造体、及びそれを用いたハニカムフィルター、コンバーターシステム |
Non-Patent Citations (1)
Title |
---|
See also references of EP1508354A4 * |
Also Published As
Publication number | Publication date |
---|---|
AU2003235280A1 (en) | 2003-12-19 |
EP1508354A4 (en) | 2006-06-28 |
US7468202B2 (en) | 2008-12-23 |
EP1508354B1 (en) | 2012-12-26 |
KR100619128B1 (ko) | 2006-09-08 |
US20050214503A1 (en) | 2005-09-29 |
KR20050016470A (ko) | 2005-02-21 |
PL371807A1 (en) | 2005-06-27 |
JP2003340224A (ja) | 2003-12-02 |
EP1508354A1 (en) | 2005-02-23 |
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