WO2004046063A1 - 炭化珪素質多孔体及びその製造方法、並びにハニカム構造体 - Google Patents
炭化珪素質多孔体及びその製造方法、並びにハニカム構造体 Download PDFInfo
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- WO2004046063A1 WO2004046063A1 PCT/JP2003/014726 JP0314726W WO2004046063A1 WO 2004046063 A1 WO2004046063 A1 WO 2004046063A1 JP 0314726 W JP0314726 W JP 0314726W WO 2004046063 A1 WO2004046063 A1 WO 2004046063A1
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- WIPO (PCT)
- Prior art keywords
- silicon carbide
- silicon
- oxide phase
- porous body
- carbide particles
- Prior art date
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- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 title claims abstract description 222
- 229910010271 silicon carbide Inorganic materials 0.000 title claims abstract description 212
- 238000000034 method Methods 0.000 title description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 136
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 135
- 239000010703 silicon Substances 0.000 claims abstract description 135
- 239000002245 particle Substances 0.000 claims abstract description 131
- 239000011148 porous material Substances 0.000 claims abstract description 85
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 43
- 229910052784 alkaline earth metal Inorganic materials 0.000 claims abstract description 13
- 150000001342 alkaline earth metals Chemical class 0.000 claims abstract description 12
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052751 metal Inorganic materials 0.000 claims description 68
- 239000002184 metal Substances 0.000 claims description 68
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 37
- 229910052712 strontium Inorganic materials 0.000 claims description 32
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims description 31
- 150000001875 compounds Chemical class 0.000 claims description 24
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 22
- 238000004519 manufacturing process Methods 0.000 claims description 22
- 239000000126 substance Substances 0.000 claims description 18
- 238000010304 firing Methods 0.000 claims description 16
- 229910021426 porous silicon Inorganic materials 0.000 claims description 10
- 239000002994 raw material Substances 0.000 claims description 10
- 239000011230 binding agent Substances 0.000 claims description 8
- 239000000155 melt Substances 0.000 claims description 8
- 230000008018 melting Effects 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 7
- 238000010191 image analysis Methods 0.000 claims description 6
- 229910052814 silicon oxide Inorganic materials 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 2
- 238000003763 carbonization Methods 0.000 claims 1
- 229920001296 polysiloxane Polymers 0.000 claims 1
- 239000003054 catalyst Substances 0.000 abstract description 20
- 239000000463 material Substances 0.000 abstract description 18
- 238000000746 purification Methods 0.000 abstract description 5
- 230000000717 retained effect Effects 0.000 abstract 1
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 15
- 230000000052 comparative effect Effects 0.000 description 14
- IATRAKWUXMZMIY-UHFFFAOYSA-N strontium oxide Chemical compound [O-2].[Sr+2] IATRAKWUXMZMIY-UHFFFAOYSA-N 0.000 description 11
- 239000007789 gas Substances 0.000 description 10
- 239000000377 silicon dioxide Substances 0.000 description 9
- 235000012239 silicon dioxide Nutrition 0.000 description 9
- 230000007423 decrease Effects 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 230000005496 eutectics Effects 0.000 description 6
- 239000000470 constituent Substances 0.000 description 5
- 239000012535 impurity Substances 0.000 description 5
- 238000005245 sintering Methods 0.000 description 5
- 238000000635 electron micrograph Methods 0.000 description 4
- 238000007654 immersion Methods 0.000 description 4
- 238000011069 regeneration method Methods 0.000 description 4
- 229910052917 strontium silicate Inorganic materials 0.000 description 4
- QSQXISIULMTHLV-UHFFFAOYSA-N strontium;dioxido(oxo)silane Chemical compound [Sr+2].[O-][Si]([O-])=O QSQXISIULMTHLV-UHFFFAOYSA-N 0.000 description 4
- 239000002253 acid Substances 0.000 description 3
- 238000001354 calcination Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 238000011496 digital image analysis Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 230000008929 regeneration Effects 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000004927 clay Substances 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 238000003703 image analysis method Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 238000003672 processing method Methods 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 1
- 238000007088 Archimedes method Methods 0.000 description 1
- 229920002472 Starch Polymers 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- AXCZMVOFGPJBDE-UHFFFAOYSA-L calcium dihydroxide Chemical compound [OH-].[OH-].[Ca+2] AXCZMVOFGPJBDE-UHFFFAOYSA-L 0.000 description 1
- 229910001861 calcium hydroxide Inorganic materials 0.000 description 1
- 239000000920 calcium hydroxide Substances 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000008119 colloidal silica Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- -1 dinitrogen aluminum Chemical compound 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000010828 elution Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000009970 fire resistant effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- BDAGIHXWWSANSR-NJFSPNSNSA-N hydroxyformaldehyde Chemical compound O[14CH]=O BDAGIHXWWSANSR-NJFSPNSNSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 229920000609 methyl cellulose Polymers 0.000 description 1
- 239000001923 methylcellulose Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- UFQXGXDIJMBKTC-UHFFFAOYSA-N oxostrontium Chemical compound [Sr]=O UFQXGXDIJMBKTC-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000013001 point bending Methods 0.000 description 1
- 238000002459 porosimetry Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- LIVNPJMFVYWSIS-UHFFFAOYSA-N silicon monoxide Chemical class [Si-]#[O+] LIVNPJMFVYWSIS-UHFFFAOYSA-N 0.000 description 1
- 239000011856 silicon-based particle Substances 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 229910000018 strontium carbonate Inorganic materials 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
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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
- F01N2330/00—Structure of catalyst support or particle filter
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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
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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
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
-
- 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 porous silicon carbide body, a method for producing the same, and an 82 cam structure.
- the present invention relates to a porous silicon carbide body, a method for producing the same, and a honeycomb structure. More specifically, a silicon carbide-based porous body having a high mechanical strength and suitable for use as a material for forming, for example, a filter catalyst carrier for purifying an exhaust gas of an automobile, and a method for producing the same, and The present invention relates to a honeycomb structure formed of such a silicon carbide porous body.
- DPF for collecting and removing particulate matter contained in dust-containing fluids such as diesel engine exhaust gas, or catalytic component for purifying harmful substances in exhaust gas
- a cell partition (rib) forming a composite of a plurality of adjacent cells, and a honeycomb outer wall surrounding and holding an outermost peripheral cell located at the outermost periphery of the cell composite as a catalyst carrier for supporting the cell composite
- a porous honeycomb structure composed of the following is widely used, and as a constituent material thereof, a silicon carbide porous body using fire-resistant silicon carbide particles as an aggregate is used.
- honeycomb structure for example, silicon carbide having a predetermined specific surface area and containing impurities is used as a starting material, which is formed into a desired shape, dried, and then dried.
- a honeycomb-structured porous silicon carbide-based catalyst carrier obtained by firing in a temperature range of 0 ° C. is disclosed (for example, Japanese Patent Application Laid-Open No. HEI 6-182228)
- necking the sintering mode of the silicon carbide particles themselves in the catalyst carrier disclosed in Japanese Patent Publication No. 228-89 by the recrystallization reaction
- silicon carbide components evaporate from the surface of the silicon carbide particles, and this is the contact portion between the particles (neck).
- a porous honeycomb structure containing refractory particles as an aggregate, particularly silicon carbide and metallic silicon, and a method for manufacturing the same are disclosed (for example, see Japanese Patent Application Laid-Open No. 20-210). 0 2—20 101 08 2).
- a porous honeycomb structure can be manufactured at a relatively low firing temperature at low cost, and the obtained porous honeycomb structure has a relatively high porosity and high heat. It has characteristics such as conductivity and high strength.
- the DPF for catalyst regeneration is required to suppress the pressure loss of the filter as much as possible, and to have a higher porosity, specifically, a porosity of 50% or more, especially around 70%. Is required.
- the present invention has been made in view of the above-mentioned problems of the prior art, and has as its object the purpose of providing a high mechanical strength, for example, a filter for exhaust gas purification of automobiles, a catalyst carrier, and the like.
- Silicon carbide that can be suitably used as a constituent material
- An object of the present invention is to provide an elemental porous body, a method for producing the same, and a honeycomb structure constituted by such a silicon carbide-based porous body.
- the present invention provides the following silicon carbide-based porous body, a method for producing the same, and a honeycomb structure.
- [1] A state in which silicon carbide particles as an aggregate and metal silicon as a binder retain pores between the silicon carbide particles and between Z or the silicon carbide particles and the metal silicon. Wherein the shortest distance between the surfaces of the silicon carbide particles or between the surfaces of the silicon carbide particles and the metal silicon surface is 10 or less.
- An oxide phase containing respective oxides of silicon, aluminum and alkaline earth metal is buried in at least a part of the micropore portion which is a portion of the micropore portion.
- the sum of the volume of the portion where the oxide phase is not embedded among the micropore portions Is less than 20% Silicon carbide-based porous body, characterized in that it.
- a plane image obtained by photographing a cut surface of the silicon carbide based porous material cut along a predetermined plane is subjected to image analysis processing, whereby the oxide phase of the pores including the fine pore portion is A pore portion specified from a portion that is not embedded, a silicon carbide particle portion specified from the silicon carbide particle, a metal silicon portion specified from the metal silicon, A portion where the silicon carbide particle portion, the metal silicon portion, and the oxide phase portion are in contact with each other on the planar image that is distinguished from the oxide phase portion specified from the oxide phase.
- the ratio of the total area of the portions where the silicon carbide particles and the oxide phase are in contact with the total area of the portions where the silicon carbide particles and the metal silicon and the oxide phase are in contact is 10 to 70%, according to any one of the above [1] to [3].
- Silicon carbide based porous material is 10 to 70%, according to any one of the above [1] to [3].
- the ratio of the total area of the portion where the silicon carbide particles and the oxide phase are in contact with the total area of the portion where the silicon carbide particles and the metal silicon and the oxide phase are in contact is The silicon carbide based porous material according to the above [4], wherein the content is 25 to 50%.
- oxide phase is strontium, oxides of aluminum and silicon (S R_ ⁇ , A 1 2 0 3, S i 0 2) all the oxide in phase, strontium, content ratio of the respective front Symbol oxides of aluminum and silicon (S R_ ⁇ : a l 2 0 3: S i 0 2) is in each substance amount ratio (molar ratio) (1.0: 0.1: 1.0) to (1.0: 1.0: 3.0).
- the silicon carbide-based porous body according to any of [2] to [5] above.
- a honeycomb structure comprising the silicon carbide-based porous body according to any one of [1] to [10].
- a compound containing strontium, aluminum and silicon is added to the silicon carbide particles and the metal silicon, and the total amount of the silicon carbide particles and the metal silicon is 100 parts by mass. in terms of a 1 2 0 3, S I_ ⁇ 2), from 1.0 to 10.
- the formed body is degreased and fired, and among the pores formed between the silicon carbide particles, between the surfaces of the silicon carbide particles, or between the surfaces of the silicon carbide particles and the metal silicon surface Micropores where the shortest distance is less than 10 m
- An oxide phase containing oxides of silicon, aluminum, and alkaline earth metal in at least a part of the pores of the pores including the fine pores, where the oxide phase is not embedded.
- the ratio of the total volume (portion volume of the micropores) of the portion where the oxide phase is not buried in the micropores to the total volume (total pore volume) is 20% or less.
- FIG. 1 is a cross-sectional view schematically showing one embodiment of the porous silicon carbide body of the present invention.
- FIG. 2 is a graph in which the contact length L (mm / mm 2 ) is plotted against the value of the porosity ⁇ (%) in the silicon carbide based porous material of the example of the present invention.
- FIG. 3 is an electron micrograph of the silicon carbide based porous material of Example 1 of the present invention.
- FIG. 4 is an electron micrograph of the silicon carbide based porous material of Example 2 of the present invention.
- FIG. 1 is a cross-sectional view schematically showing a silicon carbide-based porous body of the present embodiment.
- silicon carbide-based porous body 1 of the present embodiment has silicon carbide particles as an aggregate. 2 and metal silicon 3 as a binder are bonded together while maintaining pores 4 between silicon carbide particles 2 and between Z or silicon carbide particles 2 and metal silicon 3.
- Micropores having a shortest distance of 1 O ⁇ m or less between the surfaces of the silicon carbide particles 2 or between the surfaces of the silicon carbide particles 2 and the metal silicon 3 among the pores 4.
- An oxide phase 5 containing respective oxides of silicon, aluminum and alkaline earth metal is buried in at least a part of the portion 6, and the oxide phase 5 of the pores 4 including the microporous portion 6 is formed.
- the ratio of the total volume (pore volume of the micropore portion) of the portion where the compound phase 5 is not buried is 20% or less.
- the silicon carbide based porous body 1 of the present embodiment is In addition, by burying oxide phase 5, the bond between silicon carbide particles 2 and between Z or silicon carbide particle 2 and metal silicon 3 becomes thicker, and the bond becomes stronger.
- the mechanical strength of the silicon carbide-based porous body 1 can be increased, and for example, it can be suitably used as a material constituting a filter for purifying exhaust gas of automobiles, a catalyst carrier, and the like.
- sintering can be performed at a relatively low sintering temperature during production, which reduces production costs and improves production yield.
- the silicon carbide particles 2 as the aggregate and the metal silicon 3 as the binder are formed between the silicon carbide particles 2 and between Z or the silicon carbide particles 2 and the metal.
- the pores 4 are bonded to the silicon 3 while holding the pores 4, and among the pores 4, between the surfaces of the silicon carbide particles 2 or between the surfaces of the silicon carbide particles 2 and the surface of the metal silicon 3.
- the portion having the shortest distance of 10 m or less is defined as the micropore portion 6.
- oxide phase 5 is buried in at least a part of micropores 6.
- the oxide phase 5 is embedded so as to seal all the micropores 6. You may.
- the volume of the portion of the pores 4 including the micropores 6 described above where the oxide phase 5 is not embedded, and the volume of the portion of the micropores 6 where the oxide phase 5 is not embedded are, for example, mercury. It can be calculated from the pore size distribution measured using porosimetry overnight. Further, a cross section of the silicon carbide based porous body 1 can be photographed with a scanning electron microscope (SEM) or the like, and images photographed in a plurality of cross sections can be analyzed and calculated as an integral value.
- SEM scanning electron microscope
- the total length per unit area (1 mm 2 ) of the portion where silicon carbide particles 2 are in contact with metallic silicon 3 and oxide phase 5 is referred to as “contact length L (mm / mm 2 ) ”, the porosity ⁇ (%) of the silicon carbide based porous material 1 and the contact length L (mm / mm 2 ) described above satisfy the relationship of the following formula (1). Is preferred.
- the above formula (1) is an evaluation method for determining the strength of the bond between the silicon carbide particles 2 at a predetermined porosity, and the porosity ⁇ (%) and the contact length L (mm / mm 2 )
- the silicon carbide-based porous body 1 has excellent strength as a constituent material of the DPF. Specifically, first, a silicon carbide-based porous body 1 as a sample is cut to obtain a predetermined cut surface. At this time, the cut surface may be polished as appropriate to make the cut surface uniform.
- a plane image obtained by photographing the cut surface using a scanning electron microscope (SEM) or the like is captured into a computer such as a PC (personal computer) using an image capturing means such as a scanner.
- the captured plane image is subjected to a predetermined image analysis technique to obtain a silicon carbide particle portion specified from silicon carbide particles 2, a metal silicon portion specified from metal silicon 3, and an oxide.
- the ratio of the area of the portion where the silicon carbide particles 2 and the oxide phase 5 are in contact with each other is less than 10%, the mechanical strength of the porous silicon carbide body 1 may not be sufficiently increased. If the ratio of the area of the portion where silicon carbide particles 2 and oxide phase 5 are in contact with each other exceeds 70%, contact between silicon carbide particles 2 and metal silicon 3 becomes insufficient, and the thermal conductivity decreases. There is a risk of doing this.
- the total area of the portions where the silicon carbide particles 2 are in contact with the metal silicon 3 and the oxide phase 5 and the total area of the portions where the silicon carbide particles 2 are in contact with the oxide phase 5 are, for example,
- the polished surface of the silicon carbide-based porous body 1 is photographed using a scanning electron microscope (SEM) or the like, and images photographed in a plurality of cross sections in the thickness direction can be calculated as integral values by computer image analysis. .
- the length of the boundary line (interface length) extracted using the same image analysis method as the evaluation method for determining the strength of the bond between silicon carbide particles 2 at the predetermined porosity described above is approximately calculated. It can also be used.
- the silicon carbide particles 2 and the metal silicon 3 and the oxide phase 5 are in contact with the total area of the contact area. More preferably, the ratio of the total area of the portions where silicon carbide particles 2 and oxide phase 5 come into contact is 25 to 50%.
- the above-mentioned alkaline earth metal is preferably strontium.
- the oxide phase 5 is amorphous, wherein the oxide phase 5 gas strontium, oxides of aluminum and silicon with a (S rO, A 1 2 0 3, S i 0 2) all oxide phase in 5, strontium, content ratio of the oxide of their respective aluminum and silicon (S R_ ⁇ : a 1 2 0 3: S I_ ⁇ 2) in each substance amount ratio (molar ratio) (1 - 0: (0.1: 1.0) to (1.0: 1.0: 3.0).
- each oxide is made a ternary system and the eutectic point is lowered to cover the surfaces of silicon carbide particles 2 and Z or metallic silicon 3 during firing. It is possible to easily remove the oxide film by melting and improve the wettability of the metal silicon 3, and to increase the thickness of the bonding portion connecting the silicon carbide particles 2.
- S I_ ⁇ 2, etc. The oxide film covering the silicon carbide particles 2 and / or the surface of metallic silicon 3 here.
- the oxide phase 5 can be embedded in the fine pores 6 of the pores 4 that could not be embedded with the metallic silicon 3,
- the mechanical strength of the silicon carbide-based porous body 1 can be improved in order to assist the bonding between the silicon carbide particles 2 by the metal silicon 3.
- the substance amount ratio described above when the substance amount ratio of an oxide of aluminum (A l 2 ⁇ 3) (molar ratio) is 0. Less than 1, the wettability of metallic silicon 3 (S i) And the bonding between silicon carbide particles 2 may be weakened.
- strontium oxide (Sr ⁇ ) and silicon dioxide (Sio 2 ) contained in oxide phase 5 may cause strontium silicate (S r S i ⁇ 3 ) may be generated.
- This strontium silicate easily dissolves in acetic acid or the like used for supporting a catalyst when the silicon carbide-based porous material 1 is used as a catalyst carrier or the like, so that the oxide phase 5 is eluted when the catalyst is supported. It is supposed that a problem such as a decrease in strength occurs.
- the ratio of the amounts of substances oxides of aluminum (A 1 2 0 3) (molar ratio) 1.
- the “content ratio of each oxide of strontium, aluminum, and silicon in the oxide phase 5” described above is calculated by converting Al, Ca, and the like contained as impurities in the added compound and the metal silicon as each oxide. And the amount of silicon dioxide (S i 0 2 ) contained in the oxide film on the surface of silicon carbide particles 2 and silicon or metal silicon 3 were converted from the amount of oxygen obtained by chemically analyzing the raw material powder. It can be calculated from the value.
- an oxide (S r O, A 1 2 0 3, S I_ ⁇ 2) described above is preferably the melting temperature of is 1 0 0 0 ⁇ 1 4 0 0 ° C. Melting temperature is 100 ° C If it is less than 1, the viscosity of the oxide phase 5 is too low, so that the oxide phase 5 may be biased in the silicon carbide-based porous body 1, and the melting temperature may be 140 ° C. If it exceeds C, the viscosity of the oxide phase 5 may not be sufficiently reduced, and it may be difficult for the oxide phase 5 to enter the fine pores 6 of the pores 4.
- the melt viscosity of oxide phase 5 is preferably lower than the melt viscosity of metal silicon 3. With such a configuration, oxide phase 5 can more easily enter fine pores 6 of pores 4 of silicon carbide porous body 1.
- the ratio of the mass of oxide phase 5 to the total mass of silicon carbide particles 2 and metallic silicon 3 is preferably 1.0 to 10.0 mass%. .
- the mass ratio of the oxide phase 5 is less than 1.0% by mass, the effect of sufficiently improving the strength of the silicon carbide-based porous body 1 may not be obtained, and the mass of the oxide phase 5 If the ratio exceeds 10.0% by mass, the amount of the oxide phase 5 is too large, so that the firing shrinkage increases and the porosity of the silicon carbide-based porous body 1 decreases. Pressure loss may be too large.
- the ratio of the mass of the oxide phase 5 to the total mass of the silicon carbide particles 2 and the metal silicon 3 is More preferably, it is 4.0 to 8.0% by mass.
- the honeycomb structure of the present embodiment is characterized by being constituted by the silicon carbide-based porous body 1 described above (see FIG. 1).
- the honeycomb structure of the present embodiment reflects the characteristics of the silicon carbide porous body 1 (see FIG. 1) as a constituent material thereof, and has excellent oxidation resistance, acid resistance, particulate resistance reactivity, and thermal shock resistance. Have the property.
- the honeycomb structure of the present embodiment can be used as a DPF, a DPF for catalyst regeneration, a catalyst carrier, or the like under a high SV (space velocity) condition.
- the method for producing a silicon carbide-based porous body of the present embodiment first, strontium, silicon carbide particles and metal silicon, and a total amount of 100 parts by mass of silicon carbide particles and metal silicon, Compounds containing aluminum and silicon are converted to their respective oxides (SrO, A In terms of 1 2 ⁇ 3, S I_ ⁇ 2) to obtain a 1.0 to 1 0.0 parts by addition material.
- the compound containing strontium, aluminum and silicon contains only one of alkaline earth metals (Mg, Ca, Sr, Ba) containing strontium, aluminum and silicon. Or a plurality of types may be contained.
- the finally formed oxide phase is one of alkali earth metals. It suffices to include at least one type and aluminum and silicon.
- the amounts to be added may be different from each other or may be equally divided.
- a molding aid such as an organic binder may be added as necessary.
- silicon carbide particles and metallic silicon may contain trace impurities such as iron, aluminum, calcium hydroxide, etc., but may be used as they are and purified by chemical treatment such as chemical cleaning. A thing may be used.
- aluminum is preferably contained in the state of trioxide of aluminum (A 1 2 0 3) and metallic aluminum.
- the metallic aluminum may be contained as an impurity of metallic silicon.
- silicon have preferably be contained in the state of silicon dioxide (S i 0 2) Ya colloidal silica. The silicon dioxide at this time may be contained as an oxide film (Sio 2 ) covering the surfaces of silicon carbide particles and z or metallic silicon.
- the raw materials thus obtained are mixed and kneaded to form a kneaded clay, which is formed into a predetermined shape such as a honeycomb shape and calcined.
- the obtained molded body is fired, and at least a part of the pores formed between the silicon carbide particles contains oxides of silicon, aluminum, and alkaline earth metal.
- the phase is defined as the volume of the portion of the micropore portion where the oxide phase is not embedded, relative to the total volume (the total pore volume) of the portion of the pores including the micropore portion where the oxide phase is not embedded. It is characterized by obtaining a porous body with a porous structure by embedding so that the ratio of the total (pore volume of the micropore portion) becomes 20% or less.
- l 2 0 3 : S i 0 2 is (1.0: 0.1: 1. 0) to (: 1.0: 1.0: 3.0) in each substance ratio (molar ratio)
- the compound containing strontium, aluminum and silicon added as a raw material is decomposed or oxidized during firing and melts.
- the strontium, aluminum and silicon oxides to be melted have a ternary system, which lowers the eutectic point and further reduces the viscosity.
- the oxide film on the surface of the silicon carbide particles and / or the metal silicon is melted and removed, so that the wettability of the metal silicon bonding the silicon carbide particles is improved, and the bonding portion bonding the silicon carbide particles is made thicker.
- the excess oxide phase since the excess oxide phase has a reduced viscosity, it becomes easy to enter the pores of the porous body, particularly, the fine pores having a small pore diameter. The mechanical strength is increased to assist the bond.
- strontium, aluminum, and silicon in addition to silicon carbide particles and metallic silicon, are used from the viewpoint of producing a silicon carbide-based porous body having high porosity and high mechanical strength.
- the calcination is preferably performed at a temperature lower than the temperature at which metallic silicon melts. Specifically, at a predetermined temperature of about 150 to 700 ° C, The temperature may be maintained, or the calcination may be performed at a predetermined temperature range at a heating rate of 50 / hr or less. Regarding the method of once holding at a predetermined temperature, depending on the type and amount of the organic binder used, it is possible to hold at only one temperature level or at multiple temperature levels, and to hold at multiple temperature levels. The retention times may be the same or different. Similarly, with respect to the method of slowing down the heating rate, the heating rate may be slowed down only for a certain temperature zone or for a plurality of sections. You may let it.
- the firing temperature in the main firing is preferably set to 140 ° C. or higher.
- the optimal firing temperature is determined from the microstructure and characteristic values. However, if the temperature exceeds 160 ° C., evaporation of metallic silicon proceeds, and it becomes difficult to bond through metallic silicon. Therefore, a firing temperature of 141 to 160 ° C. is appropriate. It is preferable that the temperature is in the range of 142 to 150 ° C.
- Silicon carbide particles having an average particle diameter of 33 m and metal silicon powder having an average particle diameter of 5 m are blended so as to have a composition of 80:20 by mass ratio, and strontium oxide (SrO), It was added trioxide aluminum (a l 2 ⁇ 3) and silicon dioxide (S i 0 2) containing the compound to obtain a raw material.
- strontium oxide strontium oxide
- a l 2 ⁇ 3 trioxide aluminum
- silicon dioxide S i 0 2
- the obtained kneaded material was extruded with an extruder to an outer diameter of 45 mm, a length of 120 mm, a partition wall thickness of 0.43 mm, a cell density of 100 cells Z square inch (16 cells Z cm 2 ), And then calcined at 500 ° C for 5 hours for degreasing, and then fired in a non-oxidizing atmosphere at 1450 ° C for 2 hours to obtain a honeycomb structure.
- a honeycomb structure was prepared.
- the obtained silicon carbide-based porous body has silicon carbide particles and The metal silicon bonds with the silicon carbide particles and / or between the silicon carbide particles and the metal silicon while holding the pores, and among these pores, between the surfaces of the silicon carbide particles, or An oxide phase containing respective oxides of silicon, aluminum and strontium is buried in at least a part of the micropore portion where the shortest distance between the silicon particle surface and the metal silicon surface is 10 m or less. It was something.
- strontium oxide of an alkaline earth metal (S r O)
- a compound containing, foamed resin (acrylonitrile-based plastic Examples 1 and 2 were added except that 10 parts by mass of a balloon (average particle size of 50 m)) and 15 parts by mass of an organic pore-forming agent (starch (average particle size of 50 zm)) were added.
- a silicon carbide porous body having a honeycomb structure (Example 3 and Comparative Example 7) was produced in the same manner as in Comparative Examples 1 to 6.
- the oxide phase is not buried in the micropores where the shortest distance between the surfaces of the silicon carbide particles or between the surface of the silicon carbide particles and the surface of the metal silicon is 10 m or less with respect to the volume.
- the ratio (%) hereinafter, sometimes referred to as the microporosity (%)
- the ratio (%) (hereinafter, sometimes referred to as the microporosity (%)) of the total volume (porosity volume of the micropores) of the part having a pore diameter of 10 m or less is calculated as follows: It was calculated using the pore size distribution measured in the above. Table 1 shows the results.
- each substance amount ratio of the respective oxides of aluminum and silicon (molar ratio) (S r ⁇ : A 1 2 ⁇ 3: S i ⁇ 2 ) and the ratio of the mass of the oxide phase to the total mass of the silicon carbide particles as the aggregate and the silicon metal as the binder (% by mass) (hereinafter simply referred to as the ratio of the mass of the oxide phase ( Mass%) was calculated from the added compound and the compound contained as an impurity in the silicon carbide particles and the metal silicon raw material. Table 1 shows the results.
- these values show the characteristic X-ray characteristic of each element (Sr, A 1, S i, ⁇ ) in the oxide phase present on the polished surface of the produced silicon carbide porous body by EDS point analysis and the like. It can be calculated by measuring and quantifying it, or by quantifying it by a predetermined chemical analysis or the like, but the measuring method is not limited to the above.
- image analysis of each silicon carbide-based porous body was performed. Specifically, first, a silicon carbide porous body to be a sample is cut to obtain a predetermined cut surface. At this time, the cut surface may be appropriately polished in order to make the cut surface uniform. A plane image obtained by capturing the cut surface using a scanning electron microscope (SEM) or the like is captured by a computer such as a PC (personal computer) using an image capturing means such as a scanner. The captured planar image is converted into silicon oxide particles 2, metallic silicon 3, oxide phase 5, and oxide phase 5 out of pores 4 including fine pores 6 as shown in FIG. Is extracted separately from the part not buried (porous part).
- SEM scanning electron microscope
- FIG. 2 is a graph plotting the contact length L (mm / mm 2 ) against the value of the porosity ⁇ (%). Note that the straight line in FIG. 2 is a straight line drawn based on the lower limit of the following equation (1).
- the total area of the portion where the silicon carbide particles come into contact with the metallic silicon and oxide phases The ratio of the total area (%) (hereinafter, sometimes referred to as the oxide bonding ratio (%)) of the area where the silicon carbide particles and the oxide phase come into contact with each other is expressed by Photographs were taken using a scanning electron microscope (SEM) and calculated by computer image analysis.
- the length of the boundary line (interface length) between the silicon carbide particles and the metal silicon and the oxide phase and the oxide phase were determined using the same image analysis method as described above. Of the interface length between the silicon carbide particles and the oxide phase with respect to the total interface length between the silicon carbide particles and the metallic silicon and oxide phases.
- the total ratio was calculated and defined as the oxide phase bonding ratio.
- Table 1 shows the results. 3 shows an electron micrograph of the silicon carbide porous body of Example 1
- FIG. 4 shows an electron micrograph of the silicon carbide porous body of Example 2.
- Image-Pro Plus (trade name) (manufactured by MEDIA CYBERNET ICS) is used as application software for performing the above-described computer image analysis. It is not limited to using software.
- the porosity (%) of each silicon carbide porous body was measured by the Archimedes method. Table 1 shows the results.
- each of the obtained porous silicon carbide bodies was immersed in an aqueous solution of 10% by mass of acetic acid for 30 minutes, and the mass of the porous silicon carbide body before and after immersion was measured. The mass loss rate (% by mass) due to elution of was calculated. Table 2 shows the results.
- Example 1 since the mass ratio of the oxide phase was as large as 1.7%, the microporosity was 17%, the number of micropores in which the oxide phase was buried was large, and Because of its good wettability, the strength was excellent at 25 MPa. In Example 2, the ratio of the oxide phase was even higher at 4.1%, and the microporosity was 8%. Therefore, between the silicon carbide particles due to the oxide phase and between Z or silicon carbide particles and the metal, The effect of strengthening the bond with silicon was sufficient (oxide bond ratio: 35%), and the strength was extremely excellent at 40 MPa.
- Comparative Example 3 ratio is 0.06 trioxide aluminum (A 1 2 0 3) is the oxide phase by a containing Murrell strontium oxide (S and rO) and silicon dioxide (S i 0 2), more that strontium silicate which is readily soluble in acetic acid (S r S i 0 3) is generated, the mass with acetic acid The decrease rate (% by mass) is increasing.
- the oxide phase by trioxide aluminum (A l 2 ⁇ 3) is amorphous, and prevent the formation of strontium silicate described above.
- the oxide phase could not sufficiently enter between the silicon carbide particles and / or between the silicon carbide particles and the metallic silicon, and the strength of the silicon carbide-based porous body was limited to 16 MPa.
- Comparative Example 6 in which the ratio of silicon dioxide (Si 2 ) in each material ratio (molar ratio) of the oxide is 5.0, it is necessary to sufficiently lower the eutectic point of the oxide phase.
- the strength of the silicon carbide-based porous material could not be reduced because the viscosity of the molten compound and the oxide film covering the surface of the silicon carbide particles and Z or metallic silicon could not be sufficiently reduced. Stopped at MP a.
- Example 7 in which a pore-forming agent was used to reduce pressure loss, although the porosity was improved, the strength was significantly reduced (9 MPa). It has been difficult to suitably use it as a material for a filter for exhaust gas purification, a catalyst carrier, and the like.
- Example 3 in which the porosity was similarly increased, the ratio of the oxide phase was extremely large at 5.8% and the microporosity was 9%, as compared with Comparative Example 7. Since the effect of strengthening the bond between the silicon carbide particles by the oxide phase and between the Z or silicon carbide particles and the metal silicon is sufficient (oxide bond ratio: 38%), the porosity is 5%. Despite having a very high porosity of 9%, the strength is extremely excellent at 18MPa.For example, it is used as a material for automobile exhaust gas purification, catalyst carriers, etc. It could be suitably used.
- Examples 1 to 3 have excellent strength as a constituent material of DPF in order to sufficiently satisfy the expression (1).
- the silicon carbide-based porous body of the present invention and the honeycomb structure constituted by such a silicon carbide-based porous body have high mechanical strength, and include, for example, a filter for purifying exhaust gas of an automobile, It can be suitably used as a material constituting a catalyst carrier or the like.
- the method for producing a silicon carbide-based porous body of the present invention includes the steps of: An elemental porous body can be easily and inexpensively manufactured.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Filtering Materials (AREA)
- Catalysts (AREA)
- Ceramic Products (AREA)
- Porous Artificial Stone Or Porous Ceramic Products (AREA)
- Exhaust Gas After Treatment (AREA)
Abstract
Description
Claims
Priority Applications (5)
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KR1020057009242A KR100649476B1 (ko) | 2002-11-20 | 2003-11-19 | 탄화규소질 다공체, 그 제조 방법 및 허니컴 구조체 |
JP2004553202A JP4426459B2 (ja) | 2002-11-20 | 2003-11-19 | 炭化珪素質多孔体及びその製造方法、並びにハニカム構造体 |
US10/535,213 US7244685B2 (en) | 2002-11-20 | 2003-11-19 | Silicon carbide porous body, process for producing the same and honeycomb structure |
AU2003284416A AU2003284416A1 (en) | 2002-11-20 | 2003-11-19 | Silicon carbide porous body, process for producing the same and honeycomb structure |
EP03775840A EP1568669B1 (en) | 2002-11-20 | 2003-11-19 | Silicon carbide porous body, process for producing the same and honeycomb structure |
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JP2002336142 | 2002-11-20 | ||
JP2002-336142 | 2002-11-20 |
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WO2004046063A1 true WO2004046063A1 (ja) | 2004-06-03 |
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PCT/JP2003/014726 WO2004046063A1 (ja) | 2002-11-20 | 2003-11-19 | 炭化珪素質多孔体及びその製造方法、並びにハニカム構造体 |
Country Status (7)
Country | Link |
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US (1) | US7244685B2 (ja) |
EP (1) | EP1568669B1 (ja) |
JP (1) | JP4426459B2 (ja) |
KR (1) | KR100649476B1 (ja) |
AU (1) | AU2003284416A1 (ja) |
PL (1) | PL214868B1 (ja) |
WO (1) | WO2004046063A1 (ja) |
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EP1600432A4 (en) * | 2002-12-11 | 2008-04-23 | Ngk Insulators Ltd | POROUS MATERIAL BASED ON SILICON CARBIDE AND PROCESS FOR PREPARING SAME AND HONEYCOMB STRUCTURE |
JP2009517208A (ja) * | 2005-11-30 | 2009-04-30 | サン−ゴバン サントル ドゥ ルシェルシェ エ デトゥードゥ ユーロペン | 気体用ろ過構造体を選択する方法 |
JP2022155296A (ja) * | 2021-03-30 | 2022-10-13 | 日本碍子株式会社 | 多孔質ハニカム構造体及びその製造方法 |
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WO2008114895A1 (en) * | 2007-03-22 | 2008-09-25 | Posco | Silicon carbide-based porous body and method of fabricating the same |
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JP6239307B2 (ja) | 2013-07-31 | 2017-11-29 | イビデン株式会社 | ハニカムフィルタ |
JP6285225B2 (ja) | 2014-03-12 | 2018-02-28 | 日本碍子株式会社 | ハニカム構造体 |
US9487448B2 (en) | 2014-03-18 | 2016-11-08 | Ngk Insulators, Ltd. | Honeycomb structure |
JP6654085B2 (ja) * | 2016-03-31 | 2020-02-26 | 日本碍子株式会社 | 多孔質材料、及び多孔質材料の製造方法並びにハニカム構造体 |
JP6788515B2 (ja) * | 2017-02-02 | 2020-11-25 | 日本碍子株式会社 | 目封止ハニカム構造体 |
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2003
- 2003-11-19 AU AU2003284416A patent/AU2003284416A1/en not_active Abandoned
- 2003-11-19 US US10/535,213 patent/US7244685B2/en not_active Expired - Lifetime
- 2003-11-19 PL PL377069A patent/PL214868B1/pl unknown
- 2003-11-19 WO PCT/JP2003/014726 patent/WO2004046063A1/ja active Application Filing
- 2003-11-19 KR KR1020057009242A patent/KR100649476B1/ko not_active IP Right Cessation
- 2003-11-19 EP EP03775840A patent/EP1568669B1/en not_active Expired - Lifetime
- 2003-11-19 JP JP2004553202A patent/JP4426459B2/ja not_active Expired - Fee Related
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1600432A4 (en) * | 2002-12-11 | 2008-04-23 | Ngk Insulators Ltd | POROUS MATERIAL BASED ON SILICON CARBIDE AND PROCESS FOR PREPARING SAME AND HONEYCOMB STRUCTURE |
JP2009517208A (ja) * | 2005-11-30 | 2009-04-30 | サン−ゴバン サントル ドゥ ルシェルシェ エ デトゥードゥ ユーロペン | 気体用ろ過構造体を選択する方法 |
US8066798B2 (en) | 2005-11-30 | 2011-11-29 | Saint-Gobain Centre De Recherches Et D'etudes European | Method for selecting a gas filtering structure |
JP2022155296A (ja) * | 2021-03-30 | 2022-10-13 | 日本碍子株式会社 | 多孔質ハニカム構造体及びその製造方法 |
JP7325473B2 (ja) | 2021-03-30 | 2023-08-14 | 日本碍子株式会社 | 多孔質ハニカム構造体及びその製造方法 |
Also Published As
Publication number | Publication date |
---|---|
PL214868B1 (pl) | 2013-09-30 |
EP1568669A4 (en) | 2009-03-04 |
US7244685B2 (en) | 2007-07-17 |
KR100649476B1 (ko) | 2006-11-28 |
JP4426459B2 (ja) | 2010-03-03 |
EP1568669B1 (en) | 2012-09-05 |
JPWO2004046063A1 (ja) | 2006-03-16 |
PL377069A1 (pl) | 2006-01-23 |
AU2003284416A1 (en) | 2004-06-15 |
EP1568669A1 (en) | 2005-08-31 |
US20060029768A1 (en) | 2006-02-09 |
KR20050083959A (ko) | 2005-08-26 |
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