WO2001058827A1 - Procede de production d'une structure en ceramique nid d'abeille - Google Patents
Procede de production d'une structure en ceramique nid d'abeille Download PDFInfo
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- WO2001058827A1 WO2001058827A1 PCT/JP2001/000557 JP0100557W WO0158827A1 WO 2001058827 A1 WO2001058827 A1 WO 2001058827A1 JP 0100557 W JP0100557 W JP 0100557W WO 0158827 A1 WO0158827 A1 WO 0158827A1
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- Prior art keywords
- raw material
- cordierite
- forming
- slurry
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- 239000000919 ceramic Substances 0.000 title claims abstract description 33
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 23
- 239000002994 raw material Substances 0.000 claims abstract description 77
- 239000002002 slurry Substances 0.000 claims abstract description 45
- 229910052878 cordierite Inorganic materials 0.000 claims abstract description 33
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 claims abstract description 33
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 29
- 238000000465 moulding Methods 0.000 claims abstract description 20
- 238000000034 method Methods 0.000 claims abstract description 19
- 239000000203 mixture Substances 0.000 claims abstract description 16
- 238000001694 spray drying Methods 0.000 claims abstract description 12
- 239000004927 clay Substances 0.000 claims description 32
- 239000005995 Aluminium silicate Substances 0.000 claims description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 10
- 235000012211 aluminium silicate Nutrition 0.000 claims description 10
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 claims description 10
- 239000000843 powder Substances 0.000 claims description 10
- 238000002156 mixing Methods 0.000 claims description 8
- 229920000609 methyl cellulose Polymers 0.000 claims description 7
- 235000010981 methylcellulose Nutrition 0.000 claims description 7
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 claims description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 5
- 239000000377 silicon dioxide Substances 0.000 claims description 5
- 239000000454 talc Substances 0.000 claims description 5
- 229910052623 talc Inorganic materials 0.000 claims description 5
- 239000000314 lubricant Substances 0.000 claims description 3
- 238000010298 pulverizing process Methods 0.000 claims description 3
- 238000000227 grinding Methods 0.000 claims 1
- 239000002245 particle Substances 0.000 abstract description 12
- 239000011362 coarse particle Substances 0.000 abstract description 11
- 239000002270 dispersing agent Substances 0.000 abstract description 9
- 239000000463 material Substances 0.000 abstract description 9
- 238000001125 extrusion Methods 0.000 abstract description 7
- 230000002776 aggregation Effects 0.000 abstract description 5
- 230000007547 defect Effects 0.000 abstract description 5
- 238000007873 sieving Methods 0.000 abstract description 4
- 238000003825 pressing Methods 0.000 abstract description 2
- 238000005054 agglomeration Methods 0.000 abstract 1
- 230000002265 prevention Effects 0.000 abstract 1
- 239000001923 methylcellulose Substances 0.000 description 5
- 238000004220 aggregation Methods 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 150000003863 ammonium salts Chemical class 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 238000002276 dielectric drying Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 238000007602 hot air drying Methods 0.000 description 3
- 239000004094 surface-active agent Substances 0.000 description 3
- 239000002253 acid Substances 0.000 description 2
- 235000014113 dietary fatty acids Nutrition 0.000 description 2
- 239000000194 fatty acid Substances 0.000 description 2
- 229930195729 fatty acid Natural products 0.000 description 2
- 150000004665 fatty acids Chemical class 0.000 description 2
- LWIHDJKSTIGBAC-UHFFFAOYSA-K tripotassium phosphate Chemical compound [K+].[K+].[K+].[O-]P([O-])([O-])=O LWIHDJKSTIGBAC-UHFFFAOYSA-K 0.000 description 2
- 208000023514 Barrett esophagus Diseases 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 229910000160 potassium phosphate Inorganic materials 0.000 description 1
- 235000011009 potassium phosphates Nutrition 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
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- C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
- C04B38/0006—Honeycomb structures
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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
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/16—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay
- C04B35/18—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay rich in aluminium oxide
- C04B35/195—Alkaline earth aluminosilicates, e.g. cordierite or anorthite
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- C04B35/62605—Treating the starting powders individually or as mixtures
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- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/54—Particle size related information
- C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
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Definitions
- the present invention relates to a method for manufacturing a honeycomb ceramic structure having a cordierite composition by extrusion, and particularly to a manufacturing method most suitable for manufacturing a honeycomb ceramic structure having a thin wall of 50 or less.
- a honeycomb ceramic structure having a cordierite composition by extrusion molding using a molding die.
- a predetermined ceramic raw material is mixed, and then a molding aid and water are added and kneaded to produce a molding clay, and the produced molding clay is extruded from a molding die.
- a predetermined honeycomb ceramic structure is manufactured.
- the forming die used includes a plurality of clay supplying holes provided on the side where the forming clay is supplied, and a slit communicating with the clay supplying hole on the side where the forming clay is discharged. It is composed of Therefore, the slit defines the wall thickness of the honeycomb structure.
- an elutriation classifier such as an Alpine classifier is applied to a wall thickness of 150 / im or more, and the wall thickness is further reduced. Up to a wall thickness of 50 m, a centrifugal sieving machine was used. However, in elutriation using an alpine classifier, there was a problem of aggregation of the raw material particles. In addition, when a centrifugal sieving machine was used, there was a problem that opening a sieve of 45 m was the limit of processing on an industrial scale.
- An object of the present invention is to solve the above-mentioned problems and to provide a method for manufacturing a honeycomb ceramic structure capable of preventing aggregation of raw material particles and efficiently removing coarse-grained raw materials.
- the first invention of the method for manufacturing a honeycomb ceramic structure of the present invention is to provide a raw material slurry by individually slurrying each raw material of the cordierite-forming raw material, and individually obtaining the raw material slurry having a size of 45 m or less. After passing through an opening sieve, it is individually pulverized by spray drying, and the obtained individual raw material powders are mixed at a predetermined ratio so as to have a cordierite composition, and then a molding aid and water are added. A honeycomb structure having a wall thickness of 50 / zm or less is extruded from the obtained molding clay.
- the second invention of the method for manufacturing a honeycomb ceramic structure according to the present invention is characterized in that a cordierite-forming raw material obtained by mixing raw materials at a predetermined ratio so as to have a cordierite composition is slurried to obtain a cordierite raw material slurry.
- the raw slurry of cordierite is passed through a sieve having a mesh size of 45 xm or less, powdered by spray drying, and a forming aid and water are added to obtain a forming clay. 5 0 from clay
- the present invention is characterized in that a honeycomb structure having a wall thickness of m or less is extruded.
- the third invention of the method for manufacturing a honeycomb ceramic structure according to the present invention is to obtain a cordierite raw material slurry by slurrying a cordierite-forming raw material in which the raw materials are mixed at a predetermined ratio so as to have a cordierite composition.
- the cordierite raw material The slurry is passed through a sieve with a mesh size of 45 m or less, and methyl celluloses and a lubricant are dissolved in the slurry as a forming aid, and then the water is reduced to a predetermined water content by a filter press. It is characterized by extruding a honeycomb structure with a wall thickness of 50 m or less from soil.
- a cordierite-forming raw material is dissolved in water together with a dispersant to form a slurry, and after passing through a sieve of 45 m or less, is dried and powdered by spray drying, and a molding clay is obtained using the dried powder. That is, to obtain a forming clay by a filter press, in other words, to obtain a forming clay by using a raw material powder that has been passed through a sieve in a wet manner, thereby preventing aggregation of raw material particles and efficiently forming a coarse raw material. Can be removed. As a result, a honeycomb ceramic structure having a very thin wall thickness of 50 m or less can be formed without defects by extruding the obtained forming clay.
- FIG. 1 is a flowchart for explaining an example of a method for manufacturing a honeycomb ceramic structure according to the first invention of the present invention
- FIG. 2 is a flowchart for explaining an example of a method for manufacturing a honeycomb ceramic structure according to the second invention of the present invention
- FIG. 3 is a flowchart for explaining an example of the method for manufacturing a honeycomb ceramic structure according to the third invention of the present invention.
- FIG. 1 is a flowchart illustrating an example of a method for manufacturing a honeycomb ceramic structure according to the first invention of the present invention.
- a cordierite-forming raw material such as talc, kaolin, calcined kaolin, alumina and other aluminum hydroxide and silica is prepared.
- a dispersant and water are added to each raw material to obtain raw material slurries individually.
- the obtained raw material slurries are individually passed through a sieve having an aperture of 45 or less.
- the powder is individually pulverized by spray drying to obtain a powder of each raw material.
- the obtained individual raw material powders are mixed so as to have a cordierite composition.
- a forming aid and water are added to the mixed powder to obtain a forming clay.
- the obtained forming clay is extruded to obtain a predetermined honeycomb ceramic structure.
- FIG. 2 is a flowchart for explaining an example of a method for manufacturing an 82 cam ceramic structure according to the second invention of the present invention.
- the second invention of the present invention will be described with reference to the flowchart shown in FIG. 2.
- a cordierite-forming raw material such as talc, kaolin, calcined kaolin, alumina, aluminum hydroxide, or silica is prepared.
- the raw materials are mixed at a predetermined ratio so as to have a cordierite composition.
- a dispersant and water are added to the obtained cordierite-forming raw material to obtain a cordierite raw material slurry.
- the obtained cordierite raw material slurry is passed through a sieve of 45 m or less.
- FIG. 3 is a flowchart illustrating an example of a method for manufacturing a honeycomb ceramic structure according to the third invention of the present invention.
- the third invention of the present invention will be described with reference to the flowchart shown in FIG. 3.
- a raw material for forming a cogelate such as talc, kaolin, calcined kaolin, alumina, aluminum hydroxide, or silica is prepared.
- the raw materials are mixed at a predetermined ratio so as to have a cordierite composition.
- a dispersant and water are added to the cordierite-forming raw material obtained by mixing to obtain a cordierite raw material slurry.
- the obtained cordierite raw material slurry is passed through a sieve of 45 / xm or less.
- slurry with methylcellulose and lubricant as molding aid Dissolve in Next, the obtained slurry is reduced to a predetermined water content by a filter press to obtain a forming clay.
- the obtained forming clay is extruded to obtain a predetermined honeycomb ceramic structure.
- Conventional methods for reducing, dehydrating, drying, and pulverizing the slurry-like raw materials include reducing the water with a Fil Yuichi Press, and drying and crushing and classifying after drying with a hot air dryer.
- the raw materials re-agglomerate during water reduction and drying, and the raw materials such as kaolin and aluminum hydroxide form hard coarse particles, and the effect of removing coarse particles with a sieve of 45 ⁇ m or less is effective. It will be totally impaired.
- a molding aid such as methylcellulose
- the method of using the slurry raw material sieved as in the present invention by pulverizing it by spray drying is particularly effective in the continuous molding step.
- a forming aid to the sieved slurry raw material and then reducing the amount of water to use as a clay (third invention)
- a honeycomb structure having a wall thickness of 50 or less without cell defects is extruded and formed. It became possible.
- the dried raw materials were mixed in the proportions shown in Table 1 below, and water: 30 wt%, methylcellulose binder: 5 wt%, and lwt% of potassium phosphate as a surfactant were added and mixed.
- the mixture was kneaded to obtain a forming clay.
- the obtained molding The kneaded material was extruded into a honeycomb shape having a diameter of 100 mm and a total length of 100 mm using a honeycomb extrusion die with a slit width of 42 m and a width of 170 cells Zcm 2 , and water was removed by dielectric drying and hot air drying. .
- the dried body was in a good condition without any lack of cells in the honeycomb structure due to the mixing of coarse-grained raw materials.
- the dried body is then fired at a maximum temperature of 140 O: to obtain a cordierite honeycomb structure obtained by firing a cordierite honeycomb formed body having a rib thickness of 38 m, a cell count of 140 cells and a Zcm of 2. Was.
- the characteristics of the obtained cordierite honeycomb structure are shown in Table 2 below.
- the raw materials shown in Table 3 below were mixed in the proportions shown in Table 3, and 1.5 wt% of a polycarbonate ammonium salt was added as a dispersant to form a slurry having a solid content of 27%.
- the slurry was passed through a micro sieve having a sieve opening of 0 m to remove coarse particles of 30 m or more from the slurry.
- the slurry from which coarse particles had been removed was dried by spray drying so that the particles had a particle size of 30 or less.
- Water: 28 wt%, methylcellulose binder 1: 5 wt%, and lwt% of a fatty acid potassium stone as a surfactant were added to the spray-dried raw material, mixed and kneaded to obtain a forming clay.
- the obtained forming clay was extruded into a honeycomb shape having a diameter of 100 mm and a total length of 100 mm using a honeycomb-shaped extrusion die having a slit width of 40 m and 160 cello cm 2 , and water was removed by dielectric drying and hot-air drying. .
- the dried body was in a good condition without any lack of cells in the honeycomb structure due to the mixing of coarse-grained raw materials.
- the dried body was fired at a maximum temperature of 1400 ° C. to obtain a cordierite honeycomb structure obtained by firing a cordierite honeycomb formed body having a rib thickness of 38 zm and a cell number of 140 cells Zcm 2 .
- the characteristics of the obtained cordierite honeycomb structure are shown in Table 4 below.
- the raw materials were mixed in the same manner as in Table 3 of Example 2, and 1.5 wt% of a polycarboxylic acid ammonium salt was added as a dispersant to form a slurry having a solid content of 15%. After passing through a sieve, coarse particles of 30 m or more were removed from the slurry.
- methylcellulose binder 5 wt% of methylcellulose binder and 1 wt% of fatty acid lithite as a surfactant were added to the raw solid content, and the slurry was cooled down to a temperature of 20 ° C or less.
- the mixture was mixed to form a uniform slurry, and then the water content was reduced to 22% by a filter press to obtain a forming clay.
- the obtained forming clay is extruded into a honeycomb shape having a diameter of 100 mm and a total length of 100 mm using a honeycomb-shaped extrusion die having a slit width of 40/160 cells / cm 2 , and water is dried by dielectric drying and hot air drying. Removed.
- the dried body was in a good condition without any lack of cells in the honeycomb structure due to the mixing of coarse-grained raw materials. Thereafter, the dried body was fired at a maximum temperature of 1400 ° C. to obtain a cordierite honeycomb structure obtained by firing a cordierite honeycomb formed body having a rib thickness of 38 mm and a cell number of 140 cells Zcm 2 .
- the cordierite-forming raw material is dissolved in water together with a dispersing agent to form a slurry, passed through a sieve of 45 mm or less, then dried and powdered by spray drying, and the dried powder was dried.
- a sieve of 45 mm or less since the forming clay is obtained by using Since the raw material powder is obtained by passing through a sieve, the aggregation of the raw material particles can be prevented and the coarse raw material can be efficiently removed.
- a honeycomb ceramic structure having a very thin wall thickness of 50 zm or less can be formed without defects by extruding the obtained forming clay.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- Materials Engineering (AREA)
- Inorganic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Press-Shaping Or Shaping Using Conveyers (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Filtering Materials (AREA)
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU27107/01A AU2710701A (en) | 2000-02-14 | 2001-01-26 | Method for producing honeycomb ceramic structure |
DE60143148T DE60143148D1 (de) | 2000-02-14 | 2001-01-26 | En mit honigwaben |
US09/958,711 US6589465B2 (en) | 2000-02-14 | 2001-01-26 | Method for producing ceramic honeycomb structural body |
JP2001558382A JP4047009B2 (ja) | 2000-02-14 | 2001-01-26 | ハニカムセラミックス構造体の製造方法 |
EP01901556A EP1203758B1 (en) | 2000-02-14 | 2001-01-26 | Method for producing honeycomb ceramic structure |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000035323 | 2000-02-14 | ||
JP2000-35323 | 2000-02-14 | ||
JP2000346649 | 2000-11-14 | ||
JP2000-346649 | 2000-11-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2001058827A1 true WO2001058827A1 (fr) | 2001-08-16 |
Family
ID=26585306
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2001/000557 WO2001058827A1 (fr) | 2000-02-14 | 2001-01-26 | Procede de production d'une structure en ceramique nid d'abeille |
Country Status (6)
Country | Link |
---|---|
US (1) | US6589465B2 (ja) |
EP (1) | EP1203758B1 (ja) |
JP (1) | JP4047009B2 (ja) |
AU (1) | AU2710701A (ja) |
DE (1) | DE60143148D1 (ja) |
WO (1) | WO2001058827A1 (ja) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005097703A1 (ja) * | 2004-03-31 | 2005-10-20 | Ngk Insulators, Ltd. | ハニカム構造体の製造方法及びハニカム構造体 |
WO2006033392A1 (ja) * | 2004-09-24 | 2006-03-30 | Ngk Insulators, Ltd. | コーディエライト質ハニカム構造体の製造方法 |
JP2006298705A (ja) * | 2005-04-21 | 2006-11-02 | Denso Corp | セラミックスラリー |
JP2009061751A (ja) * | 2007-09-10 | 2009-03-26 | Ngk Insulators Ltd | ハニカム構造体の製造方法 |
DE112007002036T5 (de) | 2006-08-31 | 2009-07-23 | Ngk Insulators, Ltd., Nagoya | Verfahren zur Herstellung einer Waben-Struktur |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE112005000601T5 (de) * | 2004-03-19 | 2007-03-01 | Ngk Insulators, Ltd. | Verfahren zur Herstellung einer porösen keramischen Struktur |
US7300898B2 (en) * | 2005-05-31 | 2007-11-27 | Corning Incorporated | Low CTE cordierite body |
US9908260B2 (en) | 2013-05-20 | 2018-03-06 | Corning Incorporated | Porous ceramic article and method of manufacturing the same |
US9376347B2 (en) | 2013-05-20 | 2016-06-28 | Corning Incorporated | Porous ceramic article and method of manufacturing the same |
US9623360B2 (en) | 2013-05-20 | 2017-04-18 | Corning Incorporated | Porous ceramic article and method of manufacturing the same |
MX2018014812A (es) | 2016-05-31 | 2019-03-14 | Corning Inc | Articulo poroso y metodo para la fabricacion del mismo. |
US11447422B2 (en) | 2017-10-31 | 2022-09-20 | Corning Incorporated | Batch compositions comprising spheroidal pre-reacted inorganic particles and spheroidal pore-formers and methods of manufacture of honeycomb bodies therefrom |
Citations (3)
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FR2306956A1 (fr) * | 1975-04-11 | 1976-11-05 | Gen Refractories Co | Matiere refractaire a base de cordierite et son procede de preparation |
JPH02164765A (ja) * | 1988-12-17 | 1990-06-25 | Tokishi | 高強度磁器製品の製造法 |
EP0899248A1 (en) | 1997-08-29 | 1999-03-03 | Ngk Insulators, Ltd. | Production method of thin wall cordierite honeycomb structure |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
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JPS5841758A (ja) * | 1981-09-01 | 1983-03-11 | 信越化学工業株式会社 | セラミツク成型体の製造方法 |
US4968460A (en) * | 1986-03-07 | 1990-11-06 | Basf Aktiengesellschaft | Ceramics |
JP3961683B2 (ja) * | 1998-07-07 | 2007-08-22 | 株式会社日本自動車部品総合研究所 | コーディエライトハニカム構造体の製造方法およびハニカム構造体成形用成形助剤 |
-
2001
- 2001-01-26 EP EP01901556A patent/EP1203758B1/en not_active Expired - Lifetime
- 2001-01-26 JP JP2001558382A patent/JP4047009B2/ja not_active Expired - Lifetime
- 2001-01-26 WO PCT/JP2001/000557 patent/WO2001058827A1/ja active Application Filing
- 2001-01-26 US US09/958,711 patent/US6589465B2/en not_active Expired - Fee Related
- 2001-01-26 DE DE60143148T patent/DE60143148D1/de not_active Expired - Lifetime
- 2001-01-26 AU AU27107/01A patent/AU2710701A/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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FR2306956A1 (fr) * | 1975-04-11 | 1976-11-05 | Gen Refractories Co | Matiere refractaire a base de cordierite et son procede de preparation |
JPH02164765A (ja) * | 1988-12-17 | 1990-06-25 | Tokishi | 高強度磁器製品の製造法 |
EP0899248A1 (en) | 1997-08-29 | 1999-03-03 | Ngk Insulators, Ltd. | Production method of thin wall cordierite honeycomb structure |
Non-Patent Citations (1)
Title |
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See also references of EP1203758A4 |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005097703A1 (ja) * | 2004-03-31 | 2005-10-20 | Ngk Insulators, Ltd. | ハニカム構造体の製造方法及びハニカム構造体 |
JPWO2005097703A1 (ja) * | 2004-03-31 | 2008-02-28 | 日本碍子株式会社 | ハニカム構造体の製造方法及びハニカム構造体 |
CN100537471C (zh) * | 2004-03-31 | 2009-09-09 | 日本碍子株式会社 | 蜂窝结构体的制造方法及蜂窝结构体 |
JP4745963B2 (ja) * | 2004-03-31 | 2011-08-10 | 日本碍子株式会社 | ハニカム構造体の製造方法及びハニカム成形体 |
US9193125B2 (en) | 2004-03-31 | 2015-11-24 | Ngk Insulators, Ltd. | Method of manufacturing honeycomb structure and honeycomb structure |
WO2006033392A1 (ja) * | 2004-09-24 | 2006-03-30 | Ngk Insulators, Ltd. | コーディエライト質ハニカム構造体の製造方法 |
US8591800B2 (en) | 2004-09-24 | 2013-11-26 | Ngk Insulators, Ltd. | Method for producing cordierite-based honeycomb structure |
JP2006298705A (ja) * | 2005-04-21 | 2006-11-02 | Denso Corp | セラミックスラリー |
DE112007002036T5 (de) | 2006-08-31 | 2009-07-23 | Ngk Insulators, Ltd., Nagoya | Verfahren zur Herstellung einer Waben-Struktur |
US8974723B2 (en) | 2006-08-31 | 2015-03-10 | Ngk Insulators, Ltd. | Process for producing honeycomb structure |
DE112007002036B4 (de) | 2006-08-31 | 2018-03-29 | Ngk Insulators, Ltd. | Verfahren zur Herstellung einer Waben-Struktur |
JP2009061751A (ja) * | 2007-09-10 | 2009-03-26 | Ngk Insulators Ltd | ハニカム構造体の製造方法 |
Also Published As
Publication number | Publication date |
---|---|
US6589465B2 (en) | 2003-07-08 |
JP4047009B2 (ja) | 2008-02-13 |
US20020180119A1 (en) | 2002-12-05 |
EP1203758A1 (en) | 2002-05-08 |
AU2710701A (en) | 2001-08-20 |
EP1203758B1 (en) | 2010-09-29 |
DE60143148D1 (de) | 2010-11-11 |
EP1203758A4 (en) | 2006-06-07 |
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