WO2004087295A1 - ハニカム構造体 - Google Patents
ハニカム構造体 Download PDFInfo
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- WO2004087295A1 WO2004087295A1 PCT/JP2004/002717 JP2004002717W WO2004087295A1 WO 2004087295 A1 WO2004087295 A1 WO 2004087295A1 JP 2004002717 W JP2004002717 W JP 2004002717W WO 2004087295 A1 WO2004087295 A1 WO 2004087295A1
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- honeycomb structure
- pores
- structure according
- relationship
- average particle
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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
- B01D46/2474—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
- 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
- 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
- B01D46/2418—Honeycomb filters
- B01D46/2425—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material
- B01D46/24491—Porosity
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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
- B01D46/24492—Pore diameter
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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
- B01D46/24494—Thermal expansion coefficient, heat capacity or thermal conductivity
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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
- B01D46/247—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
- 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
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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
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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
- B01D46/2498—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
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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
- B01D53/92—Chemical or biological purification of waste gases of engine exhaust gases
- B01D53/94—Chemical or biological purification of waste gases of engine exhaust gases by catalytic processes
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- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
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- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/40—Catalysts, in general, characterised by their form or physical properties characterised by dimensions, e.g. grain size
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- 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
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- 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
- B01J35/57—Honeycombs
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- 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
- B01J35/60—Catalysts, in general, characterised by their form or physical properties characterised by their surface properties or porosity
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- 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
- B01J35/60—Catalysts, in general, characterised by their form or physical properties characterised by their surface properties or porosity
- B01J35/66—Pore distribution
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- 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
- 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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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D2275/00—Filter media structures for filters specially adapted for separating dispersed particles from gases or vapours
- B01D2275/30—Porosity of filtering 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
- B01D46/2425—Honeycomb filters characterized by parameters related to the physical properties of the honeycomb structure material
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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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/48—Processes of making filters
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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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S55/00—Gas separation
- Y10S55/05—Methods of making filter
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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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S55/00—Gas separation
- Y10S55/10—Residue burned
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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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S55/00—Gas separation
- Y10S55/30—Exhaust treatment
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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, and more particularly to a honeycomb structure that can be suitably used as an exhaust gas purifying filter or a catalyst carrier.
- a honeycomb structure has been developed for a filter (DPF) that collects particulate matter (PM) emitted from a diesel engine.
- a honeycomb structure for a DPF generally has porous partition walls arranged so as to form a plurality of through holes penetrating in the axial direction, and the through holes adjacent to each other across the partition wall are opposite to each other. It has a structure plugged at the end face. Then, the exhaust gas is caused to flow into the through-hole opening at one end face and pass through the partition wall in the honeycomb structure, so that the particulate matter in the exhaust gas can be collected and removed.
- Such a honeycomb structure is usually canned by a metal, for example, when mounted on a vehicle body, and used in this state. Therefore, if the isostatic strength of the honeycomb structure is low, the honeycomb structure may be damaged during canning or when used in a canned state. Therefore, when the honeycomb structure is canned, the honeycomb structure usually requires an isostatic strength of about IMPa or more.
- the honeycomb structure is used as a DPF or a catalyst carrier, the pressure loss of exhaust gas becomes a problem. In other words, the exhaust gas passes through the honeycomb structure, causing a pressure loss, which leads to a decrease in output of an internal combustion engine such as a diesel engine or a gasoline engine and a deterioration in fuel efficiency.
- increasing the porosity and opening ratio of the honeycomb structure is effective to reduce the pressure loss.
- Increasing the porosity and aperture ratio of the body generally causes a decrease in the strength of the honeycomb structure, such as the isostatic strength, and the honeycomb structure is easily damaged. Therefore, even if the porosity or the opening ratio is increased to reduce the pressure loss or the like, the honeycomb structure is required to have a high isostatic strength and to be easily broken.
- the coefficient of thermal expansion is 3 XI 0 to 16
- pores are conventionally used.
- a honeycomb structure having a ratio of 55 to 80% and an average pore diameter of 25 to 40 has been disclosed (JP-A-9-77573).
- the porosity is 55 to 80%
- the average pore diameter is 30 to 50 ⁇ m.
- the present invention has been made in view of such circumstances, and an object of the present invention is to provide a honeycomb structure that is not easily damaged even if the porosity or the opening ratio is large, and a method for manufacturing the same.
- a first aspect of the present invention is a honeycomb structure including a porous partition wall arranged to form a plurality of through holes penetrating from one end to another end in the axial direction,
- the porosity value is P (%)
- the compressive strength value in the A-axis direction is C (MPa)
- the aperture ratio value is A (), the following equation ( 1),
- the average pore diameter is 15 m or more and less than 30 m, and that the pore diameter is 10 to 40 m.
- the volume ratio to the total pores is preferably 50% or more, more preferably 70% or more. Further, the volume ratio of the pores having a pore diameter of 70 / m or more to all the pores is preferably 10% or less. Further, the volume ratio of pores having a pore diameter of 10 / m or less to all the pores is preferably 30% or less, more preferably 10% or less. Further, the porosity is preferably at least 55%, more preferably from 60 to 70%.
- the present invention also relates to a method for manufacturing a honeycomb structure, comprising kneading and forming a raw material containing a cordierite forming raw material, a pore former, and water, and forming the raw material from one end in the axial direction to the other end.
- the method includes a forming step of obtaining a honeycomb formed body having a plurality of partition walls arranged so as to form a plurality of through holes penetrating to an end, and a firing step of firing the formed body, wherein the porosity value is P (% ),
- the value of the compressive strength in the A-axis direction is C (MPa) and the value of the aperture ratio is A (%)
- a second aspect of the present invention is a method for manufacturing a honeycomb structure, comprising kneading a raw material containing a cordierite-forming raw material, a pore former, and water, forming the raw material, and forming the raw material at one end in the A-axis direction.
- the raw materials include aluminum source material, kaolin, talc and sili force, the average particle size of the aluminum source material is 1 to 6 m, the average particle size of the force olin is 1 to 10/2 m, and the average of the lux and sili force Particle size is 10-60
- An object of the present invention is to provide a method for manufacturing an 82 cam structure and a honeycomb structure manufactured by the manufacturing method.
- the average particle diameter of the aluminum source raw material is l ⁇ 4 ⁇ m
- the average particle diameter of kaolin is 1 ⁇ 6 ⁇ m
- the average particle diameters of talc and silicide are respectively 10 ⁇ 30xm
- the average particle diameter of the aluminum source material is 1 to 2 and the average particle diameter of the violin is 1 to 3 m
- the average particle diameters of talc and silica are 10 to 30 m, respectively. More preferred.
- the method further includes a plugging step of plugging a predetermined one of the through holes at any end.
- the pore-forming material contains a resin that foams when heated, and that the pore-forming material also contains a resin that has already foamed, and that the pore-forming material contains graphite. Is also preferred.
- the honeycomb structure according to the first aspect of the present invention is a honeycomb structure that is not easily damaged even if the porosity or the opening ratio is large, and is suitably used as a filter for purifying exhaust gas such as DPF, a catalyst carrier, and the like. Can be. Further, the method for manufacturing a honeycomb structure according to the second aspect of the present invention can suitably manufacture the honeycomb structure according to the first aspect. BRIEF DESCRIPTION OF THE FIGURES
- FIG. 1A is a schematic perspective view showing an embodiment of the 82 cam structure according to the present invention
- FIG. 1B is a partially enlarged plan view of a portion 1b in FIG. 1A.
- FIG. 2 is a diagram showing a relationship between compressive strength in the A-axis direction and porosity.
- FIG. 3 is a schematic cross-sectional view showing one embodiment of the honeycomb structure according to the present invention.
- a honeycomb structure and a method for manufacturing the honeycomb structure according to the first aspect, a method for manufacturing a honeycomb structure according to the second aspect, and a honeycomb structure obtained by the method according to the present invention will be described in specific embodiments.
- the present invention will be described in detail, but the present invention is not limited to the following embodiments.
- a section is a section perpendicular to the longitudinal direction of the through hole (for example, the A-axis direction in FIG. 1A) unless otherwise specified.
- the honeycomb structure 1 has cordierite as a main component, and has one end (end surface 42) in the A-axis direction as shown in FIGS. 1 (a) and 1 (b). And a porous partition wall 2 arranged so as to form a plurality of through holes 3a and 3b penetrating from the other end (end surface 44).
- the porosity value is P (%)
- the compressive strength value in the A-axis direction is C (MPa)
- the aperture value is A (%).
- P (%) and C (MPa) And A (%) for example, in a honeycomb structure with A (%) value of 62.8 (%), when P () value is about 69.5 (%), when the value of C (MPa) is about 1.4 (MPa) and the value of P (%) is about 60.3 (), the value of C (MPa) is about 3.5 (MPa). ) Only to the extent. According to such data for the conventional honeycomb structure, P (%) and C (MPa) at an aperture ratio of about 62.8% are approximated by an approximate curve, as shown in Fig. 2. The following equation (3)
- the porosity means the ratio of the volume of the pores contained therein to the volume of the partition walls
- the A-axis direction means the longitudinal direction of the through-hole as shown in Fig. 1 (a).
- the compressive strength in the A-axis direction means a compressive strength measured by a method based on JASO standard M505-87.
- the aperture ratio means the ratio of the area of the through hole 3 to the total area of the through hole 3 and the partition 2 in the cross section of the honeycomb structure 1 shown in FIG.
- the opening ends of predetermined through holes 3a and 3b It is in a form plugged at either end, that is, at one of the end faces 42 and 44.
- the gap is set so that the end faces 42 and 44 have a checkered pattern.
- the through holes 3 adjacent to each other across the wall are plugged at one end opposite to each other.
- all the flow holes need not be plugged when the pressure loss is more important, but when the collection efficiency is more important, all the holes are not necessarily plugged. It is preferable that the flow hole is plugged at any end. In some cases, such as when the honeycomb structure is used as a catalyst carrier, plugging is not required, and plugging is not essential in the present invention.
- the average pore diameter is preferably 15 or more and less than 30.
- the present inventor conducted a PM collection experiment on the average pore diameter and the collection efficiency. As a result, it was found that the pressure loss was small and good collection efficiency could be obtained in the above average pore diameter range. This is because if the average pore diameter is too small, the pressure loss becomes too large, and if the average pore diameter is too large, the PM that permeates the partition walls becomes too large.
- the collection efficiency means the amount of PM collected in the honeycomb structure with respect to the amount of PM introduced into the honeycomb structure.
- the volume ratio of the pores having a pore diameter of 10 to 40 m to all the pores is preferably 50% or more, more preferably 70% or more. If there are too many small pores, for example, when a catalyst is supported on a honeycomb structure, too many pores will be blocked, resulting in an increase in pressure loss, which is not preferable. If the number of pores is too large, the amount of PM passing through the partition walls becomes too large, and the trapping efficiency decreases. For the same reason, the volume ratio of the pores having a pore diameter of 70 m or more to all the pores is preferably 10% or less. Furthermore, for the same reason, The volume ratio of the pores having a pore diameter of 10 m or less to all the pores is preferably 30% or less, and more preferably 10% or less.
- the porosity is 55% or more for reasons such as reducing pressure loss.However, from the viewpoint of further reducing pressure loss, the porosity is preferably 60% or more. Particularly preferred. In particular, in the first aspect of the present invention, the porosity is preferably 60% or more in that sufficient strength can be obtained even if the porosity is increased. On the other hand, in applications where the strength is more important, it is not preferable to increase the porosity too much, and it is preferable that the porosity is 70% or less.
- thermal expansion coefficient in the longitudinal direction of the partition wall in the cross section shown in FIG. 3 (B axis) is 1. a 0 X 10- 6 / ° C, to suppress the generation of thermal stress, thermal It is preferable from the viewpoint of suppressing breakage due to stress.
- the coefficient of thermal expansion means the coefficient of thermal expansion at 40 to 800 ° C.
- the thickness of the partition wall is not particularly limited. However, if the partition wall 2 is too thick, the processing capacity of the fluid to be treated is reduced and the pressure loss is increased, and if the partition wall 2 is too thin, the strength as a honeycomb structure is obtained. Are insufficient and each is not preferable.
- the thickness of the partition walls 2 is preferably in the range of 100 to 1000 m, more preferably 150 to 750 m, most preferably 200 to 500 m.
- the number of through holes per square inch (6.44516 cm 2 ) on the cross section of the honeycomb structure is not particularly limited, but if the cell density is too low, the strength and the strength of the honeycomb structure may be reduced. If the effective filtration area when used as a filter is insufficient and the cell density is too large, the pressure loss when the fluid to be treated flows will be too large.
- the cell density is preferably 50 to 1000 / square inch (7.75 to 15 5 Z cm 2), more preferably 75 to 500 cells / square Inchi (1 1.6 to 77.5 or ZCM 2) Most preferably, it is in the range of 100 to 400 pieces / square inch (15.5 to 62.0 pieces Zcm 2 ).
- the cross-sectional shape (cell shape) of the through-hole is not particularly limited, but is preferably any one of a triangle, a quadrangle, a hexagon, and a corrugated shape from the viewpoint of manufacturing.
- One specific preferred embodiment of the honeycomb structure according to the first aspect of the present invention has a partition wall thickness of 290 to 310 and a cell density of 270 to 330 cells. In inches, the relationship between the compressive strength C (MPa) in the A-axis direction and the porosity P (%) is expressed by the following equation (2):
- ⁇ 2 0.5.
- the main component of the honeycomb structure of the present invention is cordierite. That is, the cordierite needs to be 50% by mass or more of the honeycomb structure, preferably 70% by mass or more, and more preferably 90% by mass.
- cross-sectional shape of the 82-cam structure of the present invention is not particularly limited, and may be any shape such as a polygon, such as an ellipse, an oval, an opal shape, a substantially triangular shape, or a substantially square shape, in addition to a circular shape. .
- a catalyst for example, a metal having catalytic ability
- a metal having catalytic ability when used for DPF, it is preferable to carry a catalyst for lowering the combustion start temperature.
- Typical examples of the metal having catalytic ability include Pt ;, Pd, and Rh, and it is preferable that at least one of them is supported on the honeycomb structure.
- a raw material containing a cordierite-forming raw material, a pore former, and water is kneaded to obtain a kneaded material, which is extruded and formed into a honeycomb-shaped formed body as described above.
- a slurry containing, for example, a cordierite forming raw material, a binder, a dispersant, and water is plugged with a slurry containing, for example, a cordierite forming raw material, a binder, a dispersant, and water.
- the honeycomb structure can be obtained by a firing step in which the plugged or unplugged molded body is dried and then fired at a predetermined temperature.
- the cordierite forming raw material is cordierite or co-fired by firing.
- the raw materials from which cordierite is formed by firing include, for example, aluminum source components such as aluminum oxide and / or aluminum hydroxide, and mixtures of kaolin, talc, quartz, fused silica, mullite, magnesite, etc., and are preferred. Is a blend of these raw materials so as to have the theoretical composition of cordierite crystals.
- the manufacturing process in the second aspect includes the above-described forming process and firing process.
- An important feature of the second aspect of the present invention is that the cordierite forming raw material contains at least an aluminum source material, kaolin, talc and silica, the aluminum source material has an average particle diameter of 1 to 6 ⁇ m, A raw material having an average particle diameter of ore of 1 to 10 m and a mean particle diameter of talc and silica of 10 to 60 is to be used.
- the aluminum source material means aluminum oxide and / or aluminum hydroxide.
- the particle diameter of each of the aluminum source materials falls within the above range. If both are used together, the particle size of both should be within the above range.
- the average diameter may be set in the above range and used.
- the average diameter may be set in the above range by mixing kaolin having two different average particle diameters, and this may be used.
- talc and silica the average diameter may be set to the above range by mixing talc silica having two different average particle diameters, and may be used.
- the pore-forming material used examples include graphite, foamed resin, flour, starch, phenolic resin, methyl methyl acrylate, polyethylene, and polyethylene terephthalate.
- the foamed resin includes a resin foamed by heating and a resin already foamed. It is preferable to include a resin that expands when heated as a pore-forming material from the viewpoint of improving the performance as a fill filler because many open pores can be formed.By heating, foaming occurs at 100 ° C or higher. It is more preferable to use a resin that can form a large number of open pores and suppress deformation of the structure. It is preferable to include resin that has already been foamed from the viewpoint of suppressing breakage of the partition walls during firing (so-called cell breakage).
- binder examples include hydroxypropylmethylcellulose, methylcellulose, hydroxyethylcellulose, propyloxylmethylcellulose, and polyvinyl alcohol.
- dispersant examples include ethylene glycol, dextrin, and fatty acid. Examples include stone, polyalcohol, and the like.
- the mixing ratio of the kneaded clay is, for example, 100 to 100 parts by mass of the main component, 5 to 40 parts by mass of a pore former, 10 to 40 parts by mass of a dispersion medium, and if necessary, binder 3 After adding 5 to 5 parts by mass of the dispersant and 0.5 to 2 parts by mass, the mixture can be kneaded. Kneading Examples of the apparatus and the manufacturing apparatus include combining an extruder and a continuous kneading extruder.
- the method for drying the molded body examples include hot-air drying, microwave drying, dielectric drying, reduced-pressure drying, vacuum drying, and freeze-drying.
- the sintering temperature is preferably from 140 to 140 ° (:
- the sintering atmosphere is usually preferably baked in an air atmosphere.
- the plugging for plugging a predetermined through hole is performed.
- a predetermined raw material for example, a cordierite forming raw material is added with water, a binder or the like to form a slurry, which is sealed at the opening end of a predetermined through hole.
- the plugging can be performed by drying and / or baking.Punching is performed by sandwiching the partition wall so that the end face of the 82-cam structure has a checkered pattern. It is preferable to perform the plugging at the ends where the holes are opposite to each other, and the plugging step may be performed at any stage after the molding step. If firing is required, it can be done before the firing step, with only one firing For preferred.
- cordierite forming raw materials aluminum oxide (alumina), aluminum hydroxide, kaolin, talc and fused silica having the average particle diameters shown in Table 1 were used.
- An unfoamed resin) and a resin that is foamed by heating (unfoamed resin) are added at the compounding ratio shown in Table 2, and a water-soluble cellulose derivative, a surfactant and water are further added as a binder, followed by kneading, kneading, and extrusion molding.
- a honeycomb formed body was formed.
- the total pore volume was determined by the mercury intrusion method, and the porosity was calculated. Of coredierite The true density was 2.52 g / cm 3 . The average pore diameter was the value of the median pore diameter on a volume basis.
- a cylindrical test specimen with a length of 25.4 mm in the A-axis direction and a diameter of 25.4 mm in a direction perpendicular thereto was cut out from the honeycomb structure, and the compressive strength in the A-axis direction was measured by an autograph.
- the load cell was 25 kN, and the load speed was 0.5 mm / min.
- the longitudinal direction of the flow holes in the honeycomb structure (for example, the A-axis direction in Fig. 1 (a)) is the A-axis direction, and the longitudinal direction of the partition walls in the cross section of the honeycomb structure (for example, the B-axis direction in Fig. 1 (b)).
- the linear thermal expansion coefficient between 40 and 800 ° C in each direction was measured with the B axis direction.
- Table 3 shows the results.
- the honeycomb structures manufactured by Comparative Examples 1 to 3 using alumina and force oline having a particle diameter outside the range of the second aspect of the present invention exhibited low A-axis compression strength.
- Examples 1 to 11 were manufactured according to the second aspect of the present invention, and the obtained honeycomb structure exhibited a very high A-axis compressive strength even if the porosity and / or the opening ratio was high, It can be seen that when used as a filter such as a DPF, the honeycomb structure has a small pressure loss and is hard to crack.
- honeycomb structures obtained in Examples 1 to 11 have an average pore diameter of 15 zm or more and less than 3 O ⁇ m, a porosity of 55% or more, and a pore diameter of 10 to 40 / zm.
- the volume ratio of the fine pores to the total fine pores is 50% or more, and when used as a filter such as DPF, the trapping efficiency is excellent.
- the honeycomb structure according to the first aspect of the present invention is a honeycomb structure having a porosity, which is unlikely to be damaged even if the opening ratio is large, and a filter for purifying exhaust gas such as DPF. It can be suitably used as a catalyst carrier or the like.
- the method for manufacturing a honeycomb structure according to the second aspect of the present invention can suitably manufacture the honeycomb structure according to the first aspect.
- the present invention has been described centering on a plugged honeycomb structure used for a DPF or the like, the present invention provides a honeycomb structure having a higher strength at a predetermined porosity and opening ratio. It is useful regardless of the presence or absence of plugging and the intended use.
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- Chemical & Material Sciences (AREA)
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- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
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- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Environmental & Geological Engineering (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- General Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Ceramic Engineering (AREA)
- Biomedical Technology (AREA)
- Combustion & Propulsion (AREA)
- Health & Medical Sciences (AREA)
- Structural Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- Filtering Materials (AREA)
- Catalysts (AREA)
- Porous Artificial Stone Or Porous Ceramic Products (AREA)
- Exhaust Gas Treatment By Means Of Catalyst (AREA)
- Exhaust Gas After Treatment (AREA)
- Processes For Solid Components From Exhaust (AREA)
- Filtering Of Dispersed Particles In Gases (AREA)
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/547,509 US7470302B2 (en) | 2003-03-28 | 2004-03-04 | Honeycomb structure |
DE112004000457T DE112004000457T5 (de) | 2003-03-28 | 2004-03-04 | Wabenstruktur |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2003090178 | 2003-03-28 | ||
JP2003-090178 | 2003-03-28 | ||
JP2004-025767 | 2004-02-02 | ||
JP2004025767A JP2004315346A (ja) | 2003-03-28 | 2004-02-02 | ハニカム構造体 |
Publications (1)
Publication Number | Publication Date |
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WO2004087295A1 true WO2004087295A1 (ja) | 2004-10-14 |
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ID=33134291
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PCT/JP2004/002717 WO2004087295A1 (ja) | 2003-03-28 | 2004-03-04 | ハニカム構造体 |
Country Status (4)
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US (1) | US7470302B2 (ja) |
JP (1) | JP2004315346A (ja) |
DE (1) | DE112004000457T5 (ja) |
WO (1) | WO2004087295A1 (ja) |
Cited By (1)
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CN107129318A (zh) * | 2016-02-29 | 2017-09-05 | 日本碍子株式会社 | 蜂窝结构体的制造方法 |
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JP2006231113A (ja) * | 2005-02-22 | 2006-09-07 | Meidensha Corp | 光触媒及び光触媒の製造方法 |
US8318627B2 (en) * | 2005-08-10 | 2012-11-27 | Sd Lizenzverwertungsgesellschaft Mbh & Co. Kg | Process for preparation of a catalyst carrier |
JP2007045686A (ja) | 2005-08-12 | 2007-02-22 | Ngk Insulators Ltd | 多孔質セラミックス構造体の製造方法 |
WO2007058006A1 (ja) * | 2005-11-18 | 2007-05-24 | Ibiden Co., Ltd. | ハニカム構造体 |
CN101395099A (zh) * | 2006-03-07 | 2009-03-25 | 日本碍子株式会社 | 陶瓷结构体及其制造方法 |
US7923093B2 (en) * | 2006-06-30 | 2011-04-12 | Corning Incorporated | High porosity filters for 4-way exhaust gas treatment |
EP2058042B2 (en) * | 2006-08-30 | 2017-05-03 | Hitachi Metals, Ltd. | Ceramic honeycomb filter |
EP1941940A1 (en) * | 2007-01-03 | 2008-07-09 | Ford Global Technologies, LLC | Porous substrate for use as a particulate filter for catalytic or non-catalytic soot regeneration methods |
US7789929B2 (en) * | 2007-04-04 | 2010-09-07 | Ford Global Technologies Llc | Diesel particulate filter and method for forming such filter |
JP4571990B2 (ja) | 2008-03-31 | 2010-10-27 | 日本碍子株式会社 | ハニカム構造体の製造方法 |
US8894917B2 (en) * | 2008-05-30 | 2014-11-25 | Corning Incorporated | High porosity cordierite honeycomb articles |
JP4920752B2 (ja) * | 2010-01-05 | 2012-04-18 | 日本碍子株式会社 | ハニカム構造体 |
JP2011194342A (ja) * | 2010-03-19 | 2011-10-06 | Ngk Insulators Ltd | ハニカム構造体およびハニカム触媒体 |
US9856177B2 (en) | 2010-05-28 | 2018-01-02 | Corning Incorporated | Cordierite porous ceramic honeycomb articles |
US9334191B2 (en) | 2010-05-28 | 2016-05-10 | Corning Incorporated | Methods for forming ceramic honeycomb articles |
US8609032B2 (en) | 2010-11-29 | 2013-12-17 | Corning Incorporated | Porous ceramic honeycomb articles and methods for making the same |
DE102014010858A1 (de) * | 2014-07-25 | 2016-01-28 | Man Diesel & Turbo Se | Katalysatoreinheit und Abgaskatalysator |
JP6633952B2 (ja) * | 2016-03-28 | 2020-01-22 | 日本碍子株式会社 | ハニカム構造体 |
JP7123597B2 (ja) * | 2018-03-29 | 2022-08-23 | 日本碍子株式会社 | ハニカムフィルタ |
JP7049156B2 (ja) * | 2018-03-30 | 2022-04-06 | 日本碍子株式会社 | ハニカムフィルタ |
JP6965289B2 (ja) * | 2019-01-17 | 2021-11-10 | イビデン株式会社 | ハニカム構造体及びハニカム構造体の製造方法 |
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- 2004-03-04 US US10/547,509 patent/US7470302B2/en active Active
- 2004-03-04 DE DE112004000457T patent/DE112004000457T5/de not_active Withdrawn
- 2004-03-04 WO PCT/JP2004/002717 patent/WO2004087295A1/ja active Application Filing
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CN107129318B (zh) * | 2016-02-29 | 2021-03-09 | 日本碍子株式会社 | 蜂窝结构体的制造方法 |
Also Published As
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US20060193756A1 (en) | 2006-08-31 |
DE112004000457T5 (de) | 2006-04-13 |
US7470302B2 (en) | 2008-12-30 |
JP2004315346A (ja) | 2004-11-11 |
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