JP4998346B2 - Method for manufacturing ceramic honeycomb structure - Google Patents
Method for manufacturing ceramic honeycomb structure Download PDFInfo
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- JP4998346B2 JP4998346B2 JP2008077291A JP2008077291A JP4998346B2 JP 4998346 B2 JP4998346 B2 JP 4998346B2 JP 2008077291 A JP2008077291 A JP 2008077291A JP 2008077291 A JP2008077291 A JP 2008077291A JP 4998346 B2 JP4998346 B2 JP 4998346B2
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- 239000000919 ceramic Substances 0.000 title claims description 172
- 238000000034 method Methods 0.000 title claims description 35
- 238000004519 manufacturing process Methods 0.000 title claims description 24
- 230000002093 peripheral effect Effects 0.000 claims description 177
- 239000000463 material Substances 0.000 claims description 58
- 238000005245 sintering Methods 0.000 claims description 36
- 238000010304 firing Methods 0.000 claims description 32
- 230000008859 change Effects 0.000 claims description 22
- 239000002994 raw material Substances 0.000 claims description 21
- 238000005192 partition Methods 0.000 claims description 19
- 238000001354 calcination Methods 0.000 claims description 16
- 238000000465 moulding Methods 0.000 claims description 16
- 239000000203 mixture Substances 0.000 claims description 13
- 229910010293 ceramic material Inorganic materials 0.000 claims description 7
- 238000004898 kneading Methods 0.000 claims description 6
- 239000003795 chemical substances by application Substances 0.000 claims description 5
- 239000002612 dispersion medium Substances 0.000 claims description 5
- 239000012752 auxiliary agent Substances 0.000 claims description 4
- 239000011230 binding agent Substances 0.000 claims description 4
- 239000002270 dispersing agent Substances 0.000 claims description 4
- 239000002002 slurry Substances 0.000 claims description 4
- 239000006061 abrasive grain Substances 0.000 claims description 3
- 229910003460 diamond Inorganic materials 0.000 claims description 3
- 239000010432 diamond Substances 0.000 claims description 3
- 238000000638 solvent extraction Methods 0.000 claims 1
- 230000008569 process Effects 0.000 description 18
- 239000004927 clay Substances 0.000 description 14
- 230000015572 biosynthetic process Effects 0.000 description 10
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- 238000001035 drying Methods 0.000 description 10
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- 238000000227 grinding Methods 0.000 description 9
- 238000010586 diagram Methods 0.000 description 8
- 229910052878 cordierite Inorganic materials 0.000 description 6
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 6
- 239000003054 catalyst Substances 0.000 description 5
- 238000009826 distribution Methods 0.000 description 5
- 238000002360 preparation method Methods 0.000 description 5
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 4
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910004298 SiO 2 Inorganic materials 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 3
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- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- 239000004372 Polyvinyl alcohol Substances 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 235000010948 carboxy methyl cellulose Nutrition 0.000 description 2
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- 239000002699 waste material Substances 0.000 description 2
- 229910002706 AlOOH Inorganic materials 0.000 description 1
- 239000005995 Aluminium silicate Substances 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 108010010803 Gelatin Proteins 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 229920002472 Starch Polymers 0.000 description 1
- 229910010413 TiO 2 Inorganic materials 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 125000002947 alkylene group Chemical group 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- 235000012211 aluminium silicate Nutrition 0.000 description 1
- 229910001593 boehmite Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000001768 carboxy methyl cellulose Substances 0.000 description 1
- 239000008112 carboxymethyl-cellulose Substances 0.000 description 1
- 229920006184 cellulose methylcellulose Polymers 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
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- 239000012530 fluid Substances 0.000 description 1
- 229920000159 gelatin Polymers 0.000 description 1
- 239000008273 gelatin Substances 0.000 description 1
- 235000019322 gelatine Nutrition 0.000 description 1
- 235000011852 gelatine desserts Nutrition 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- FAHBNUUHRFUEAI-UHFFFAOYSA-M hydroxidooxidoaluminium Chemical compound O[Al]=O FAHBNUUHRFUEAI-UHFFFAOYSA-M 0.000 description 1
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 229920000609 methyl cellulose Polymers 0.000 description 1
- 239000001923 methylcellulose Substances 0.000 description 1
- 235000010981 methylcellulose Nutrition 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 238000009751 slip forming Methods 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 238000003746 solid phase reaction Methods 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
- RUDFQVOCFDJEEF-UHFFFAOYSA-N yttrium(III) oxide Inorganic materials [O-2].[O-2].[O-2].[Y+3].[Y+3] RUDFQVOCFDJEEF-UHFFFAOYSA-N 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B19/00—Machines or methods for applying the material to surfaces to form a permanent layer thereon
- B28B19/0038—Machines or methods for applying the material to surfaces to form a permanent layer thereon lining the outer wall of hollow objects, e.g. pipes
-
- 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
- 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
-
- 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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
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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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5024—Silicates
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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
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/87—Ceramics
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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
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/00793—Uses not provided for elsewhere in C04B2111/00 as filters or diaphragms
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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
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/0081—Uses not provided for elsewhere in C04B2111/00 as catalysts or catalyst carriers
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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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/9607—Thermal properties, e.g. thermal expansion coefficient
- C04B2235/9615—Linear firing shrinkage
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
- F01N3/022—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous
- F01N3/0222—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous the structure being monolithic, e.g. honeycombs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2825—Ceramics
- F01N3/2828—Ceramic multi-channel monoliths, e.g. honeycombs
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Filtering Materials (AREA)
- Catalysts (AREA)
Description
本発明は、燃焼排気浄化触媒用のセラミック担体や排気微粒子捕集用のディーゼルパーティキュレートフィルタ等に用いられるセラミックハニカム構造体の製造方法に関するものである。 The present invention relates to a method for manufacturing a ceramic honeycomb structure used for a ceramic carrier for a combustion exhaust purification catalyst, a diesel particulate filter for collecting exhaust particulates, and the like.
従来、車両用エンジン等の内燃機関の燃焼排気流路に設置される排気浄化触媒の担体や、ディーゼルパーティキュレートフィルタ(DPF)のフィルタ基材等として、セラミックハニカム構造体が用いられている。セラミックハニカム構造体は、所望のセラミック材料の組成を構成する主原料粉末と成形性を確保するための結合剤、可塑剤、造孔剤等の成形助剤と水等の分散媒とを混練したセラミック坏土を、所定の格子溝を設けた成形型から押し出して、略筒状の外周壁内を隔壁によって区画した所定形状のセルを多数有するセラミックハニカム成形体としたものを乾燥・焼成したものである。 Conventionally, a ceramic honeycomb structure is used as a carrier for an exhaust purification catalyst installed in a combustion exhaust passage of an internal combustion engine such as a vehicle engine, a filter base material for a diesel particulate filter (DPF), or the like. A ceramic honeycomb structure is obtained by kneading a main raw material powder constituting a composition of a desired ceramic material, a molding aid such as a binder, a plasticizer and a pore former to ensure moldability, and a dispersion medium such as water. A ceramic honeycomb molded body that is formed by extruding a ceramic clay from a forming die provided with predetermined lattice grooves to form a ceramic honeycomb formed body having a large number of cells having a predetermined shape in which a substantially cylindrical outer peripheral wall is partitioned by partitions. It is.
セラミックハニカム構造体においては、成形時に自重によって隔壁の一部が変形するセルよれや外周形状の歪変形や、外周壁の壁厚の不均一性によるクラックの発生といった問題があり、特許文献1には、セラミック坏土を押出成形し、乾燥、焼成してセラミック焼成体を製造する工程と、このセラミックハニカム焼成体の周縁部を研削加工によって除去する工程と、変形セルを除去した後、セラミックハニカム焼成体の外周面にコーティング材を施して外周壁部を形成する工程とを有する製造方法によって、セラミックハニカム構造体の機械的強度、真円度、寸法精度の向上を図る技術が開示されている。
近年、セラミック担体の熱容量を低減して触媒の早期活性化を図る目的や、捕集効率向上のためセル密度の増加を図る目的で、セラミックハニカム構造体の隔壁の薄肉化が進み、さらなる寸法精度、機械的強度、耐熱衝撃強度の向上が要求されている。
ところが、特許文献1にあるように、セラミックハニカム焼成体の組成とその外周面に施すコーティング材料の組成とが異なる場合、熱膨張係数が一致せず、高温環境下で使用するには、熱衝撃に対する強度が不足する虞がある。
さらに、特許文献1にあるように、熱衝撃性を高めるためにセラミックハニカム焼成体にコーティング材料を塗布した後に焼成を行ったとしても、既に焼成されているセラミックハニカム焼成体を再度焼成すると過焼成となって気孔率が低下し、セラミックハニカム構造体の本来目的であるフィルタや触媒担体としての機能を果たさなくなる虞がある。また、セラミックハニカム焼成体の再焼成による寸法変化とコーティング材の焼成による寸法変化との差によって熱ストレスを生じ、外周壁がセラミックハニカム焼成体から剥離したり外周壁にクラックが発生したりする虞もある。
加えて、一般的にセラミック焼成体は硬度が高く、加工が困難であり、焼成後にセラミックハニカム焼成体の外縁部を加工する方法では、極めて多大な加工時間を要し、コストの増大を招く虞もある。
In recent years, with the aim of reducing the heat capacity of the ceramic support and activating the catalyst early, and increasing the cell density to improve the collection efficiency, the thickness of the partition walls of the ceramic honeycomb structure has been reduced, and further dimensional accuracy has increased. Improvements in mechanical strength and thermal shock resistance are required.
However, as disclosed in
Furthermore, as disclosed in
In addition, the ceramic fired body generally has high hardness and is difficult to process, and the method of processing the outer edge portion of the ceramic honeycomb fired body after firing requires an extremely long processing time and may increase the cost. There is also.
そこで、本願発明は、かかる実情に鑑み、寸法精度、機械的強度、耐熱衝撃強度に優れたセラミックハニカム構造体の製造方法を提供することを目的とするものである。 Accordingly, in view of such circumstances, the present invention aims to provide a method for manufacturing a ceramic honeycomb structure excellent in dimensional accuracy, mechanical strength, and thermal shock strength.
請求項1の発明では、略筒状の外周壁内を所定形状の隔壁で区画して気体の流路となる複数のセルを設けたセラミックハニカム構造体の製造法において、所定のセラミック材料と所定の助剤とを混練し、所定形状の格子溝を設けた成形型から押し出してセラミックハニカム成形体を成形する成形工程と、上記セラミックハニカム成形体を焼結温度よりも低い温度で仮焼してセラミックハニカム仮焼体を形成する仮焼工程と、該セラミックハニカム仮焼体の周縁部を加工除去してセラミックハニカム加工体を形成する加工工程と、該セラミックハニカム加工体の外周面に外周壁形成材料を塗布して所定の膜厚の外周壁を形成する外周壁形成工程と、該外周壁と上記セラミックハニカム加工体とを同時に焼結して、一体のセラミックハニカム構造体となす同時焼結工程とを具備する。 According to the first aspect of the present invention, there is provided a method for manufacturing a ceramic honeycomb structure in which a substantially cylindrical outer peripheral wall is partitioned by partition walls having a predetermined shape and a plurality of cells serving as gas flow paths are provided. A forming step of forming a ceramic honeycomb formed body by extruding from a forming die provided with lattice grooves having a predetermined shape, and calcining the ceramic honeycomb formed body at a temperature lower than a sintering temperature. A calcining step for forming a ceramic honeycomb calcined body, a processing step for processing and removing a peripheral portion of the ceramic honeycomb calcined body to form a ceramic honeycomb processed body, and forming an outer peripheral wall on the outer peripheral surface of the ceramic honeycomb processed body An outer peripheral wall forming step in which a material is applied to form an outer peripheral wall having a predetermined film thickness, and the outer peripheral wall and the ceramic honeycomb processed body are simultaneously sintered to form an integrated ceramic honeycomb structure ; And a simultaneous sintering step formed between.
請求項1の発明によれば、仮焼によってセラミックハニカム成形体は加工に耐え得る強度を有するセラミックハニカム仮焼体となり、成形時に発生するクラックやセルよれ、自重による偏芯などの欠陥を加工によって除去できる。また、セラミックハニカム仮焼体は、焼結によって寸法変化する余地があり、セラミックハニカム加工体の表面に形成した外周壁の焼成による寸法変化との差によるストレスが抑制される。したがって、欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。 According to the first aspect of the present invention, the ceramic honeycomb formed body becomes a ceramic honeycomb calcined body having a strength that can withstand processing by calcining, and defects such as eccentricity due to cracks and cells generated during forming and due to its own weight are processed by processing. Can be removed. Moreover, the ceramic honeycomb calcined body has room for dimensional change due to sintering, and stress due to a difference from the dimensional change due to firing of the outer peripheral wall formed on the surface of the ceramic honeycomb processed body is suppressed. Therefore, a ceramic honeycomb structure with few defects, excellent dimensional accuracy, and high thermal shock resistance can be obtained.
請求項2の発明では、上記外周壁形成材料は、主成分の焼結後の組成が上記セラミック材料の焼結後の組成と同一となるセラミック原料と、分散剤、結合剤、粘弾性調整剤と分散媒とを混合し、スラリー状又はペースト状としたものを用いる。 In the invention of claim 2, the outer peripheral wall forming material includes a ceramic raw material in which the composition after sintering of the main component is the same as the composition after sintering of the ceramic material, a dispersant, a binder, and a viscoelasticity adjusting agent. And a dispersion medium are mixed to form a slurry or paste.
請求項2の発明によれば、セラミックハニカム加工体と外周壁とを一体的に焼結できるので、さらに、欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。 According to the invention of claim 2, since the ceramic honeycomb processed body and the outer peripheral wall can be integrally sintered, it is possible to obtain a ceramic honeycomb structure with fewer defects, excellent dimensional accuracy, and high thermal shock resistance. it can.
請求項3の発明では、上記外周壁形成材料は、上記セラミックハニカム仮焼体を焼結したときにおける該仮焼体の焼結後の外径寸法DCFDを該仮焼体の焼結前の外径寸法DPREで除した仮焼体焼成変化率SBODと上記外周壁を焼結したときにおける該外周壁の焼結後の膜厚寸法TCFDを該外周壁の焼結前の膜厚寸法TCTDで除した外周壁焼成変化率SSKNとの相対的な焼成変化率ΔSが下記式1の関係を満たす。
−1.5≦ΔS≦0.5・・・式1
但しΔS=SBOD−SSKN(%)
SBOD=100・DCFD/DPRE(%)
SSKN=100・TCFD/TCTD(%)と定義する。
In the invention of claim 3, said outer peripheral wall forming material before sintering of the ceramic honeycomb calcined body outer diameter after sintering of the provisional sintered body in when sintered D CFD the provisional sintered bodies The calcined body firing rate of change S BOD divided by the outer diameter dimension D PRE and the film thickness dimension T CFD of the outer peripheral wall after sintering when the outer peripheral wall is sintered are the film thickness before sintering of the outer peripheral wall. the relative firing shrinkage rate ΔS of the outer peripheral wall firing shrinkage rate S SKN obtained by dividing the dimension T CTD satisfy the relationship of
−1.5 ≦ ΔS ≦ 0.5
However, ΔS = S BOD −S SKN (%)
S BOD = 100 · D CFD / D PRE (%)
It is defined as S SKN = 100 · TCFD / TCTD (%).
請求項3の発明の範囲に上記外周壁形成材料の焼成変化率を調整すれば、上記セラミックハニカム仮焼体との熱膨張率の差による熱ストレスを生じることなく、焼結されるので、さらに、欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。 If the firing rate of change of the outer peripheral wall forming material is adjusted within the scope of the invention of claim 3, it is sintered without causing thermal stress due to the difference in thermal expansion coefficient with the ceramic honeycomb calcined body. A ceramic honeycomb structure having few defects, excellent dimensional accuracy, and high thermal shock resistance can be obtained.
請求項4の発明では、上記外周壁形成工程は、上記セラミックハニカム加工体の両端を保持しつつ回転可能とする保持回転装置と、上記セラミックハニカム加工体の表面から所定の間隙を離隔してスキージ又はブレードを配設し、上記保持回転装置によって上記セラミックハニカム加工体を回転させるとともに、上記間隙から上記外周壁形成材料を流出させ、セラミックハニカム加工体の表面に塗布する外周壁形成材料塗布手段を具備する。 According to a fourth aspect of the present invention, the outer peripheral wall forming step includes: a holding and rotating device that can rotate while holding both ends of the ceramic honeycomb processed body; and a squeegee that separates a predetermined gap from the surface of the ceramic honeycomb processed body. Alternatively, an outer peripheral wall forming material application unit that disposes a blade and rotates the ceramic honeycomb processed body by the holding and rotating device and causes the outer peripheral wall forming material to flow out of the gap and apply to the surface of the ceramic honeycomb processed body. It has.
請求項4の発明によれば、上記スキージ又はブレードによって、上記外周壁形成材料を上記セラミックハニカム加工体の外周表面に極めて均一に塗布することができる。 According to invention of Claim 4, the said outer peripheral wall formation material can be apply | coated to the outer peripheral surface of the said ceramic honeycomb processed body very uniformly with the said squeegee or a braid | blade.
請求項5の発明では、上記外周壁形成工程は、上記外周壁形成材料を複数回に分けて塗布するとともに、塗布後にレベリングを行う。 In the invention of claim 5, in the outer peripheral wall forming step, the outer peripheral wall forming material is applied in a plurality of times and leveling is performed after the application.
請求項5の発明によれば、さらに上記外周壁の膜厚が均一化され、さらに欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。 According to the fifth aspect of the present invention, a ceramic honeycomb structure having a more uniform outer peripheral wall thickness, fewer defects, excellent dimensional accuracy, and high thermal shock resistance can be obtained.
請求項6の発明では、上記加工工程は、上記セラミックハニカム仮焼体の外周面にダイヤモンド砥粒を施した砥石を所定の回転数で回転するとともに、上記セラミックハニカム仮焼体の外周を所定の周速で周回しつつ、所定の加工速度で上記セラミックハニカム仮焼体の外周縁を研削除去する。
In the invention of
請求項6の発明によれば、上記セラミックハニカム仮焼体の加工途中でチッピング等の加工不良を起こす虞がなく、さらに欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。
According to the invention of
請求項7の発明では、上記成形工程は、上記外周壁を形成する溝部を有さず上記隔壁を形成する上記溝部のみからなる成形型を用いる。 In a seventh aspect of the present invention, the molding step uses a molding die that does not have a groove portion that forms the outer peripheral wall but includes only the groove portion that forms the partition wall.
請求項7の発明によれば、外周壁を有さず隔壁のみからなるセラミックハニカム成形体を形成することができる。該セラミックハニカム成形体には、外周壁が存在しないので、クラックの起点となる外周壁厚の不均一化が起こらず、クラックが発生しがたくなる。外周壁が存在せず、クラックもないので、仮焼後の上記外周部加工工程において、加工除去するのはセルよれ部分のみとなり、加工に要する時間が大幅に短縮できる上に、加工除去する材料の無駄も大幅に抑制できる。 According to the invention of claim 7, it is possible to form a ceramic honeycomb formed body having only the partition walls without having the outer peripheral wall. Since the ceramic honeycomb molded body does not have an outer peripheral wall, the thickness of the outer peripheral wall, which is the starting point of the crack, does not become uneven and cracks are less likely to occur. Since there is no outer peripheral wall and there are no cracks, in the above outer peripheral portion processing step after calcination, only the portion of the cell is removed by processing, and the time required for processing can be greatly shortened, and the material to be processed and removed Waste can be greatly reduced.
図1を参照して、本発明の第1の実施形態におけるセラミックハニカム構造体の製造方法の概要を示す。図1は本発明の第1の実施形態におけるセラミックハニカム構造体の製造方法の概要を示すフローチャートである。 With reference to FIG. 1, an outline of a method for manufacturing a ceramic honeycomb structure according to the first embodiment of the present invention will be described. FIG. 1 is a flowchart showing an outline of a method for manufacturing a ceramic honeycomb structure according to the first embodiment of the present invention.
図1に示すように、原料調合工程P1にて、所定のセラミック組成となるように原料を調合し、混練工程P2にて、所定の粒度分布に調整した調合原料と水等の分散媒と所定の助剤等とを混練し、セラミック坏土とし、坏土調整工程P3にて、セラミック坏土の流動性を調整し、成形工程P4にて、セラミック坏土を所定の成形型から押し出して隔壁によって区画されたセルを多数設けたセラミックハニカム成形体を形成し、乾燥工程P5にて十分に乾燥した後、仮焼工程P6にて、焼結温度より低い所定の温度で仮焼し、セラミックハニカム仮焼体を形成する。外周部加工工程P7にて、セラミックハニカム仮焼体の外周縁を加工装置によって所定の形状に加工し、セラミックハニカム加工体を得る。 外周壁材料調整工程P80にて、調合原料と焼結後の組成は同じで、セラミックハニカム加工体と比較して所定の焼成変化率を具備する外周壁材料を調整する。外周壁形成工程P8にて、外周壁材料をセラミックハニカム加工体の外周面に均一に塗布し、外周壁を形成する。乾燥工程P9にてこれを十分に乾燥した後、同時焼結工程P10にて、外周壁とセラミックハニカム加工体とが一体となるように同時焼結を行う。本発明によれば、仮焼によってセラミックハニカム成形体は加工に耐え得る強度を有するセラミックハニカム仮焼体となり、成形時に発生するクラックやセルよれ、自重による偏芯などの欠陥を加工によって除去できる。また、セラミックハニカム仮焼体は、焼結によって寸法変化する余地があり、セラミックハニカム加工体の表面に形成した外周壁の焼成による寸法変化との差によるストレスが抑制され、さらに、セラミックハニカム加工体と外周壁とを一体的に焼結できるので、欠陥が少なく、寸法精度に優れ、耐熱衝撃性の高いセラミックハニカム構造体を得ることができる。なお、外周壁形成工程P8において、外周壁形成材料の粘度特性を調整しながら複数回に分けて外周壁を形成してもよい。 As shown in FIG. 1, in the raw material preparation step P1, raw materials are prepared so as to have a predetermined ceramic composition, and in the kneading step P2, the prepared raw material adjusted to a predetermined particle size distribution, a dispersion medium such as water, and the predetermined And kneading with an auxiliary agent, etc., to form a ceramic clay, in the clay adjustment step P3, the fluidity of the ceramic clay is adjusted, and in the molding step P4, the ceramic clay is extruded from a predetermined molding die. After forming a ceramic honeycomb formed body provided with a large number of cells partitioned by the above, sufficiently dried in the drying step P5, and then calcined at a predetermined temperature lower than the sintering temperature in the calcining step P6. A calcined body is formed. In the outer peripheral portion processing step P7, the outer peripheral edge of the ceramic honeycomb calcined body is processed into a predetermined shape by a processing apparatus to obtain a ceramic honeycomb processed body. In the outer peripheral wall material adjusting step P80, the prepared raw material and the composition after sintering are the same, and an outer peripheral wall material having a predetermined firing change rate is adjusted as compared with the ceramic honeycomb processed body. In the outer peripheral wall forming step P8, the outer peripheral wall material is uniformly applied to the outer peripheral surface of the ceramic honeycomb processed body to form the outer peripheral wall. After sufficiently drying in the drying step P9, simultaneous sintering is performed in the simultaneous sintering step P10 so that the outer peripheral wall and the processed ceramic honeycomb body are integrated. According to the present invention, the ceramic honeycomb formed body becomes a ceramic honeycomb calcined body having a strength that can withstand processing by calcining, and defects such as cracks and cells generated during molding and eccentricity due to its own weight can be removed by processing. In addition, the ceramic honeycomb calcined body has room for dimensional change due to sintering, and the stress due to the difference from the dimensional change due to firing of the outer peripheral wall formed on the surface of the ceramic honeycomb processed body is suppressed. And the outer peripheral wall can be integrally sintered, so that a ceramic honeycomb structure with few defects, excellent dimensional accuracy, and high thermal shock resistance can be obtained. In the outer peripheral wall forming step P8, the outer peripheral wall may be formed in a plurality of times while adjusting the viscosity characteristics of the outer peripheral wall forming material.
本発明の第1の実施形態におけるセラミックハニカム構造体1CFDの製造方法について、ディーゼルエンジンの燃焼排気流路に設けられ粒子状物質PMを捕集するディーゼルパーティキュレートフィルタ(DPF)に用いられるコーディエライト質のセラミックハニカム構造体1CFD(例えば、隔壁厚:15mil、セル密度:250cpsi、外径:φ200mm、外周壁厚:40mil、長さ:200mm、気孔率:50%)の製造に本発明を適用した場合を具体例として、従来の製造方法の問題点及び本発明の効果と共に詳述する。
原料調合工程P1では、調合原料として、焼成によりコーディエライト(2MgO・3Al2O3・5SiO2)組成となる原料、即ち、タルク3MgO・4SiO2・H2O、マグネシアMgO、シリカSiO2、カオリンAl2O3・2SiO2・2H2O、アルミナAl2O3、ベーマイトAlOOH、水酸化アルミニウムAl(OH)3等から適宜選択されたセラミック原料粉末を所定の配合比で調合して所定の粒度分布を有する調合原料に調整する。また、用途に応じてイットリアY2O3、チタニアTiO2や、遷移金属等を添加しても良い。
About the manufacturing method of the
In the raw material preparation step P1, as a preparation raw material, a raw material that becomes a cordierite (2MgO · 3Al 2 O 3 · 5SiO 2 ) composition by firing, that is, talc 3MgO · 4SiO 2 · H 2 O, magnesia MgO, silica SiO 2 , A ceramic raw material powder appropriately selected from kaolin Al 2 O 3 · 2SiO 2 · 2H 2 O, alumina Al 2 O 3 , boehmite AlOOH, aluminum hydroxide Al (OH) 3 and the like is prepared at a predetermined blending ratio to obtain a predetermined Adjust to raw material with particle size distribution. Further, yttria Y 2 O 3 , titania TiO 2 , transition metal, or the like may be added depending on the application.
次いで、混練工程P2では、結合剤、可塑剤、分散剤、潤滑剤、邂逅剤、界面活性剤、造孔剤等の助剤として、メチルセルロースMC、カルボキシメチルセルロースCMC、ポリビニルアルコールPVA、デンプン糊、ポリアルキレン誘導体、グリセリン、ゼラチン、ワックスエマルジョン、カーボン、おがくず等から適宜必要な材料を選択して、上記調合原料と混練し、セラミック坏土100とし、さらに、坏土調整工程P3にて、セラミック坏土100を所定の流動特性となるよう含水率や粘度の調整を行う。
Next, in the kneading step P2, as auxiliary agents such as a binder, a plasticizer, a dispersant, a lubricant, a glaze, a surfactant, and a pore-forming agent, methyl cellulose MC, carboxymethyl cellulose CMC, polyvinyl alcohol PVA, starch glue, poly A necessary material is appropriately selected from an alkylene derivative, glycerin, gelatin, wax emulsion, carbon, sawdust, etc., kneaded with the above-mentioned preparation raw material to form
成形工程P4では、図2に示すように、調整されたセラミック杯土100をプランジャ式又はスクリュー式の押出成形機3を用いて、所定の格子溝を設けた成形型2から押し出す。外周壁10FMD内を隔壁11FMDによって区画された多数のセル12FMDが連続的に形成されながらローラコンベア等の搬送装置4によって引取られ、さらに乾燥前又は乾燥後に切断装置5等を用いて所定の長さに切断されて、セラミックハニカム成形体1FMDが形成される。
In the forming step P4, as shown in FIG. 2, the adjusted
一般にセラミック坏土100は、非ニュートン流体であり、図2に示すように、押出成形機3内において層流とはならず比較的狭い速度分布を示すが、押出成形機3の中心部に比べ、押出成形機3の内周壁近傍では、押出成形機3の内周壁とセラミック杯土100との摩擦により流速が遅くなる。このため、成形型2から押し出される際にも、この速度分布の影響により、外周壁10に局所的に壁厚の薄い部分が発生しやすい。
このような外周壁10の隔壁の薄い部分は、図3(a)及び図3(b)の枠A内に拡大して示すような、外周壁表面に微細なクラック13FMDとして現れ、これが起点となり、焼成したときに大きな亀裂に成長する虞がある。
また、セラミックハニカム成形体1FMDは、成形直後には柔らかいので、隔壁11FMDは極めて薄いので、隔壁11FMDの一部、特に、搬送時に使用されセラミックハニカム成形体1FMDを載置する図略のセッターと接するセラミックハニカム成形体1FMDの下端部において、図3(b)の枠B内に拡大して示すような、自重によって変形したセルよれ14FMDが発生する虞もある。
In general, the
Such a thin part of the partition wall of the outer peripheral wall 10 appears as fine cracks 13 FMD on the outer peripheral wall surface as shown in an enlarged manner in the frame A in FIGS. 3A and 3B, and this is the starting point. And there is a risk of growing into large cracks when fired.
Further, since the ceramic honeycomb formed
得られたセラミックハニカム成形体1FMDは、乾燥工程P5にてマイクロ波乾燥装置等により十分に乾燥され、さらに、仮焼工程P6にて、焼結温度よりも低い温度で仮焼する。
本実施形態においては、MgO−SiO2−Al2O3三成分系においてコーディエライト相の生成が開始され、かつ、完全には焼結せず、焼結により寸法変化する余地を残した温度として、仮焼温度を1360℃から1400℃とする。仮焼過程において、セラミックハニカム成形体1FMDに含まれる助剤として添加した有機物は焼失し、原材料中のMgO−SiO2−Al2O3成分の固相反応によりコーディエライト相の生成が開始され、セラミックハニカム仮焼体1PREが得られる。
The obtained ceramic honeycomb formed
In this embodiment, the temperature at which the generation of cordierite phase is started in the MgO—SiO 2 —Al 2 O 3 ternary system, and there is no room for dimensional change due to sintering without complete sintering. The calcining temperature is 1360 ° C. to 1400 ° C. In the calcination process, the organic substance added as an auxiliary agent contained in the ceramic honeycomb formed
外周部加工工程P7において、得られたセラミックハニカム仮焼体1PREの外周縁を研削してセラミックハニカム加工体1SPDが得られる。セラミックハニカム仮焼体1PREは、セラミックハニカム成形体1FMDに比べると、遙かに高い機械的強度を有するが、焼結後に比べれば、粒子間の結合が弱く、加工が容易である。セラミックハニカム仮焼体1PREの研削には、図4(a)に示すように、外周面にダイヤモンド砥粒を施した砥石を所定の回転数(例えば100〜7000rpm)で回転させながら、セラミックハニカム仮焼体1PREの外周を所定の周速(例えば630〜4400m/min)で回転しつつ、所定の加工速度(例えば500mm/min)でセラミックハニカム仮焼体1PREの外周縁を研削加工するNC外周研削装置6等が用いられる。
所定の加工外周面LSPに至るまでの所定の研削代ARSP(例えば7mm、5セル分)は、仮焼体の焼成による寸法変化を考慮して設定されている。
従来の焼結後の加工では、焼結体が硬いため研削代をできるだけ少なくする必要があったが、本発明では、仮焼後の加工であるため研削が容易で、十分な研削代を確保できるので、セルよれやクラックなどの欠陥部分を確実に除去できる。
図4(b)に示すように、セラミックハニカム仮焼体1PREからクラック13PRE及びセルよれ14PREが切除され、変形のない隔壁11PREによってのみ区画された複数のセル12PREからなるセラミックハニカム加工体1SPDが得られる。なお、セラミックハニカム加工体1SPDの表面部位には、表面に開口する開口セル12OPNが形成されている。
In the outer peripheral portion processing step P7, the outer peripheral edge of the obtained ceramic honeycomb calcined
Predetermined machining the outer peripheral surface L of the predetermined ranging SP grinding allowance AR SP (e.g. 7 mm, 5 cell fraction) is set in consideration of the dimensional change due to sintering of the calcined body.
In the conventional post-sintering process, the sintered body was hard, so it was necessary to reduce the grinding allowance as much as possible. However, in the present invention, the process after calcining is easy, so grinding is easy and sufficient grinding allowance is ensured. As a result, it is possible to reliably remove defective portions such as cell twists and cracks.
As shown in FIG. 4 (b), a ceramic honeycomb composed of a plurality of
外周壁形成工程P8では、図5に示すように、セラミックハニカム加工体1SPDの両端を保持しつつ回転可能とする保持回転装置7によって、セラミックハニカム加工体1SPDを回転させながら、外周壁形成材料150をセラミックハニカム加工体150SPDの外周表面に塗布し、加工外周面LSPとの間に所定の間隙GPを離隔して設けられるスキージ又はブレード等の膜厚均一化手段8によって過剰な外周壁形成材料150を掻き取りつつ、開口セル12OPN内を外周壁形成材料150で埋めることによって、所定の膜厚(例えば0.3mm〜2mm)の外周壁151を形成する。
外周壁形成材料150には、外周壁材料調整工程P80において、焼結後の組成がセラミックハニカム仮焼体1PREの焼結後の組成と同じになるコーディエライト化原料と、分散剤、結合剤、粘弾性調整剤等と水などの分散媒とを混合し、スラリー状又はペースト状に調整したものを用いる。
In the outer circumferential wall formation step P8, as shown in FIG. 5, the holding and rotating device 7 for rotatable while holding both ends of the ceramic honeycomb worked
In the outer peripheral
なお、外周壁形成工程P8を複数回に分けて行っても良い。
図6(a)に示すように、セラミックハニカム加工体1SPDの表面に1回の外周壁形成材料150の塗布により外周壁151を形成して1次外周壁形成体1CTDとしたときには、開口セル12OPN内に外周壁形成材料150が十分に充填されず、僅かに空隙VCが点在する虞がある。
そこで、1次外周壁形成体1CTDを静置して、外周壁151のレベリングを行うと図6(b)に示すように、空隙VC内に外周壁151の一部が流入し空隙VC内は外周壁形成材料によって充填される。
しかし、図6(c)に示すような外周膜形成静置体1STLDの表面には、押出方向の縦スジ状に膜厚が薄くなった凹部152が形成される虞がある。
そこで、図7(a)に示すように、外周壁形成静置体1STLDの表面に再度外周壁形成材料150を塗布し、凹部152を埋めつつ、2次外周壁123を形成すると、図7(b)に示すように滑らかな表面状態の2次外周壁形成体1WCTDとなる。
The outer peripheral wall forming step P8 may be performed in a plurality of times.
As shown in FIG. 6A, when the outer
Therefore, when the primary outer peripheral
However, the circumferential membrane forming electrostatic mounting
Therefore, as shown in FIG. 7 (a), the outer peripheral wall forming the electrostatic mounting body 1 STLD outer peripheral
セラミックハニカム加工体1SPDの加工外周面LSP表面に現れる開口セル12OPNの開口形状は必ずしも一定ではないので、1次外周壁形成体1CTDの形成に用いる外周壁材料150の粘度が高いと、開口の狭い開口セル12OPNには、外周壁材料150が十分に充填されない虞があり、外周壁材料調整工程P80において、1次外周壁形成体1CTDの形成に用いる外周壁材料150は、低粘度に調整するのが望ましい。また、凹部152は比較的浅いので、外周壁材料150の粘度が高くても、容易に充填され、膜厚の均一化が容易となるので、2次外周壁形成体1WCTDの形成に用いる外周壁材料150は、高粘度に調整するのが望ましい。
Ceramic honeycomb worked body 1 SPD opening shape of the processed outer peripheral surface L SP appears on the surface open cells 12 OPN of not necessarily constant, the viscosity of the outer
外周壁151を形成した後、乾燥工程P9にて、マイクロ波乾燥機等により外周壁151を十分に乾燥した後、同時焼結工程P10にて、所定の焼成温度で1次外周壁形成体1CTD又は2次外周壁形成体1WCTDを同時焼結すると、外周壁151と隔壁11PREとが同時に焼結され、図10に示すような、完全一体となった外周壁124CFD内に隔壁11CFDによって区画されたセル12CFDを多数有するセラミックハニカム構造体1CFDができる。
なお、本実施形態において、同時焼結温度は、1430℃から1450℃の範囲に調整される。
After the outer
In the present embodiment, the simultaneous sintering temperature is adjusted to a range of 1430 ° C. to 1450 ° C.
本発明の効果について、表1、表2及び図9を参照して説明する。
従来のセラミックハニカム成形体をそのまま焼成した場合のクラック発生率を比較例1とし、本発明の第1の実施形態において、焼成変化率SSKNの異なる外周壁形成材料150を用いて、外周壁の膜厚を変化させた場合のクラックの発生率を実施例1、2、3として表1に示す。
The effects of the present invention will be described with reference to Tables 1 and 2 and FIG.
When the conventional ceramic honeycomb formed body is fired as it is, the crack generation rate is set as Comparative Example 1, and in the first embodiment of the present invention, the outer peripheral
外周壁形成材料150は、セラミックハニカム仮焼体1PREを焼結したときの仮焼体焼成変化を表す指標として、該仮焼体1PREの焼結後の寸法DCFDを該仮焼体1PREの焼結前の寸法DPREで除した仮焼体焼成変化率SBODを算出し、外周壁151を焼成したときの焼成変化を示す指数として、外周壁151の焼結後の膜厚寸法TCFDを外周壁151の焼結前の膜厚寸法TCTDで除した外周壁焼成変化率SSKNとの相対的な焼成変化率ΔSが下記式1の関係を満たすときに、クラックの発生率が低くなることが判明した。
−1.5≦ΔS≦0.5・・・式1
但しΔS=SBOD−SSKN(%)
SBOD=100・DCFD/DPRE(%)
SSKN=100・TCFD/TCTD(%)と定義する。
The outer peripheral
−1.5 ≦ ΔS ≦ 0.5
However, ΔS = S BOD −S SKN (%)
S BOD = 100 · D CFD / D PRE (%)
It is defined as S SKN = 100 · TCFD / TCTD (%).
外周壁形成材料150の焼成変化率SSKNは、セラミックハニカム成形体1FMDを形成したセラミック原料と焼結後の組成が同一となる原料を主成分としつつ、外周壁形成材料150に使用するセラミック原料の粒度分布の調整や、出発原料の種類、スラリーの濃度等を換えることによって調整できる。
なお、本実施形態においては、出発原料のうち、アルミニウムAl源となる原料の配合比率の調整により、外周壁形成材料150の焼成変化率SSKNの調整を行った。
The firing change rate S SKN of the outer peripheral
In the present embodiment, the firing rate of change S SKN of the outer peripheral
図10を参照して、本発明の第2の実施形態における外周壁形成工程について説明する。本実施形態は、上記実施形態に示した製造方法を基本とし、より均一な外周壁の形成方法を示すものである。セラミックハニカム構造体の外形形状は、円柱状に限らず、断面が楕円形やオーバル型、矩形、多角形など、用途に応じて適宜変更されるものである。このような形状の変化に対して、成形工程P4においては、成形型2の形状を変更することにより容易に対応可能であり、また、外周部加工工程P7においても、NC研削装置6等によれば、任意のプロファイルを有した形状に研削できる。そこで、本実施形態においては、図10に示すような保持回転装置7a及び、外周壁均一化装置8aを用いて、均一な膜厚の外周壁を形成する手段用いた点が相違する。本図(a)は一部省略正面図、(b)は断面図である。
保持回転装置7aは、セラミックハニカム加工体1SPDを保持回転部70aによって回転させつつ、昇降機構71aによって上下方向にも移動可能としているため、任意の形状を有したセラミックハニカム加工体1SPDの表面に外周壁151を形成することができる。
また、外周壁均一化装置8aは、外周壁形成材料150を貯留する貯留タンク81を設け、貯留タンク81の開口部にセラミックハニカム加工体1SPDとその先端との間に所定の間隙GPを設けてブレード80を配設し、ラミックセラミックハニカム加工体1SPDが形状に沿った回転運動をすると、貯留タンク81内の外周壁形成材料150が一定の膜厚でセラミックハニカム加工体150SPDの外周表面に塗布することができる。外周壁151形成後には、シャッタ82が下降して、外周壁形成材料150の供給を遮断することができる。
With reference to FIG. 10, the outer peripheral wall formation process in the 2nd Embodiment of this invention is demonstrated. This embodiment is based on the manufacturing method shown in the above embodiment, and shows a more uniform method for forming an outer peripheral wall. The external shape of the ceramic honeycomb structure is not limited to a columnar shape, and the cross section may be appropriately changed according to the application, such as an oval shape, an oval shape, a rectangle, or a polygon. Such a change in shape can be easily coped with by changing the shape of the mold 2 in the molding step P4, and also in the outer peripheral portion machining step P7 by the
The holding and rotating device 7a allows the ceramic honeycomb processed
Further, the outer peripheral
図11、図12を参照して、本発明の第3の実施形態におけるセラミックハニカム構造体の製造方法について説明する。本実施形態においては、上記実施形態におけるセラミックハニカム構造体の製造方法を基本とし、成形工程P7において成形型2aを用いる点が相違し、これにより、材料コスト及び外周部加工工程P4の大幅なコスト削減が可能となる。
上記実施形態においては、図11(a)に示すような外周壁形成用溝部と隔壁形成用溝部とを備えた成形型2を用いて外周壁と隔壁とを同時に形成してセラミックハニカム成形体1とした場合について説明したが、本図(b)に示すような外周壁形成用溝部を有しない成形型2aを用いることによって、外周壁を有さず隔壁のみからなるセラミックハニカム成形体1aを形成することができる。図12に示すように、セラミックハニカム成形体1aは、下端部のセルよれ14aは、上記実施形態と同様に形成される虞があるが、外周壁が存在しないので、クラックの起点となる外周壁厚の不均一化が起こらず、クラックが発生しがたくなる。外周壁が存在せず、クラックもないので、仮焼後の外周部加工工程P7において、加工除去するのはセルよれ14a部分のみとなり、加工に要する時間が大幅に短縮でき、加工除去する材料の無駄も大幅に抑制できる。
With reference to FIG. 11 and FIG. 12, the manufacturing method of the ceramic honeycomb structure in the 3rd Embodiment of this invention is demonstrated. The present embodiment is based on the manufacturing method of the ceramic honeycomb structure in the above-described embodiment, and is different in that the forming
In the above embodiment, the outer peripheral wall and the partition wall are simultaneously formed using the molding die 2 having the outer peripheral wall forming groove portion and the partition wall forming groove portion as shown in FIG. However, by using the molding die 2a that does not have the outer peripheral wall forming groove as shown in this figure (b), the ceramic honeycomb formed
図13に、本発明の第1の実施形態におけるセラミックハニカム構造体の製造方法に用いたコーディエライト質材料の焼成温度に対する変位(%)を示す。
SBODは、セラミックハニカム加工体1SPDの変位を示し、SSKNは、外周壁形成体1CTDの変位を示す。
FIG. 13 shows the displacement (%) with respect to the firing temperature of the cordierite material used in the method for manufacturing the ceramic honeycomb structure according to the first embodiment of the present invention.
S BOD indicates the displacement of the ceramic honeycomb processed
なお、本発明は上記実施形態に限定されるものではなく、仮焼温度及び焼成温度を適用するセラミック材料の特性に応じて、適宜選択するとともに、その材料によって形成したセラミックハニカム仮焼体の焼成変化率と外周壁形成材料の焼成変化率とを調整すれば、上記実施形態において例示したコーディエライトの他、アルミナ、シリカ、チタニア、窒化珪素、炭化珪素といった酸化物、窒化物、炭化物等の種々のセラミック材料を用いたセラミックハニカム構造体の製造に適用することができる。 The present invention is not limited to the above-described embodiment, and is appropriately selected according to the characteristics of the ceramic material to which the calcination temperature and the calcination temperature are applied, and the calcination of the ceramic honeycomb calcined body formed by the material. If the change rate and the firing change rate of the outer peripheral wall forming material are adjusted, in addition to the cordierite exemplified in the above embodiment, oxides such as alumina, silica, titania, silicon nitride, silicon carbide, nitride, carbide, etc. The present invention can be applied to the production of a ceramic honeycomb structure using various ceramic materials.
また、このようにして得られたセラミックハニカム構造体は、例えば自動車用の排ガス浄化触媒の担体、あるいは微粒子捕集用フィルタのフィルタ基材として好適であり、外周壁を形成した後でもその前でも良いが、外周壁形成材料と同材質のセラミック材料を用いてセラミックハニカム構造体の両端においてセルを交互に目封じた後、同時焼成しても良い。 The ceramic honeycomb structure thus obtained is suitable as a carrier for an exhaust gas purification catalyst for automobiles or as a filter base material for a filter for collecting particulates, for example, either before or after forming the outer peripheral wall. Although it is good, after the cells are alternately plugged at both ends of the ceramic honeycomb structure using the same ceramic material as the outer peripheral wall forming material, simultaneous firing may be performed.
1 セラミックハニカム構造体
1FMD セラミックハニカム成形体
1PRE セラミックハニカム仮焼体
1SPT セラミックハニカム加工体
1CTD (1次)外周壁形成体
150 (1次)外周壁形成材料
151 (1次)外周壁
1WCTD 2次外周壁形成体
160 2次外周壁形成材料
161 2次外周壁
1CFD セラミックハニカム同時焼結体
100 セラミック坏土
2 成形型
P1 調合工程
P2 混練工程
P3 杯土調整工程
P4 成形工程
P5 乾燥工程
P6 仮焼工程
P7 外周部加工工程
P8 外周壁形成工程
P9 乾燥工程
P10 同時焼成工程
DPRE セラミックハニカム仮焼体外径
DCFD セラミックハニカム焼成体外径
TCTD 外周壁形成材料乾燥膜厚
TCFD 外周壁形成材料焼成膜厚
SBOD 仮焼体焼成変化率
SSKN 外周壁材料焼成変化率
ΔS 相対焼成変化率
DESCRIPTION OF SYMBOLS 1
150 (primary) outer peripheral wall forming material 151 (primary) outer
P3 Fill soil adjustment process P4 Molding process P5 Drying process P6 Pre-firing process P7 Outer peripheral part processing process P8 Outer peripheral wall forming process P9 Drying process P10 Simultaneous firing process D PRE ceramic honeycomb calcined body outer diameter D CFD ceramic honeycomb fired body outer diameter T CTD outer periphery Wall forming material dry film thickness T CFD outer peripheral wall forming material fired film thickness S BOD calcined body firing change rate S SKN outer peripheral wall material firing change rate ΔS Relative firing change rate
Claims (7)
所定のセラミック材料と所定の助剤とを混練し、所定形状の格子溝を設けた成形型から押し出してセラミックハニカム成形体を成形する成形工程と、
上記セラミックハニカム成形体を焼結温度よりも低い温度で仮焼してセラミックハニカム仮焼体を形成する仮焼工程と、
該セラミックハニカム仮焼体の周縁部を加工除去してセラミックハニカム加工体を形成する加工工程と、
該セラミックハニカム加工体の外周面に外周壁形成材料を塗布して所定の膜厚の外周壁を形成する外周壁形成工程と、
該外周壁と上記セラミックハニカム加工体とを同時に焼結して、一体のセラミックハニカム構造体となす同時焼結工程とを具備することを特徴とするセラミックハニカム構造体の製造方法。 In the method for manufacturing a ceramic honeycomb structure in which a plurality of cells serving as gas flow paths are provided by partitioning a substantially cylindrical outer peripheral wall with partition walls having a predetermined shape,
A molding step of kneading a predetermined ceramic material and a predetermined auxiliary agent and extruding from a molding die provided with a lattice groove of a predetermined shape to form a ceramic honeycomb molded body,
A calcining step of calcining the ceramic honeycomb formed body at a temperature lower than a sintering temperature to form a ceramic honeycomb calcined body;
A processing step of processing and removing the peripheral portion of the ceramic honeycomb calcined body to form a ceramic honeycomb processed body,
An outer peripheral wall forming step of forming an outer peripheral wall having a predetermined film thickness by applying an outer peripheral wall forming material to the outer peripheral surface of the ceramic honeycomb processed body;
A method for manufacturing a ceramic honeycomb structure, comprising: simultaneously sintering the outer peripheral wall and the ceramic honeycomb processed body to form an integrated ceramic honeycomb structure.
−1.5≦ΔS≦0.5・・・式1
但し、ΔS=SBOD−SSKN(%)
SBOD=100・DCFD/DPRE(%)
SSKN=100・TCFD/TCTD(%)と定義する。 The outer peripheral wall-forming material is obtained by dividing the sintered outer diameter D CFD of the calcined body when the ceramic honeycomb calcined body is sintered by the outer diameter D PRE of the calcined body before sintering. periphery obtained by dividing the thickness dimension T CFD after sintering of the outer peripheral wall of the calcined body firing shrinkage rate S BOD and the outer peripheral wall which is in when sintered at the sintering thickness before dimension T CTD of the outer peripheral wall 3. The method for manufacturing a ceramic honeycomb structure according to claim 1, wherein a relative firing change rate ΔS with a wall firing rate S SKN satisfies the relationship of the following formula 1.
−1.5 ≦ ΔS ≦ 0.5 Formula 1
However, ΔS = S BOD −S SKN (%)
S BOD = 100 · D CFD / D PRE (%)
It is defined as S SKN = 100 · TCFD / TCTD (%).
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EP2668147A1 (en) | 2011-01-28 | 2013-12-04 | Mann + Hummel Gmbh | Ceramic body composed of an aluminium titanate mixture |
JP2012170935A (en) * | 2011-02-24 | 2012-09-10 | Denso Corp | Honeycomb structure |
EP2905112A4 (en) * | 2012-10-05 | 2016-10-26 | Ibiden Co Ltd | Drying method for honeycomb molded body and production method for honeycomb structure |
JPWO2014054169A1 (en) * | 2012-10-05 | 2016-08-25 | イビデン株式会社 | Cutting method of dried honeycomb body and manufacturing method of honeycomb structure |
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Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2604876B2 (en) * | 1990-03-27 | 1997-04-30 | 日本碍子株式会社 | Method for manufacturing ceramic honeycomb structure |
JP4246475B2 (en) * | 2002-04-26 | 2009-04-02 | 日本碍子株式会社 | Manufacturing method of honeycomb structure |
JP4474633B2 (en) * | 2002-06-17 | 2010-06-09 | 日立金属株式会社 | Method for manufacturing ceramic honeycomb structure |
JP4421858B2 (en) * | 2003-09-12 | 2010-02-24 | 日本碍子株式会社 | Honeycomb structure and manufacturing method thereof |
WO2007148764A1 (en) * | 2006-06-23 | 2007-12-27 | Ngk Insulators, Ltd. | Honeycomb structure and method for manufacturing same |
CN101346184B (en) * | 2006-07-03 | 2012-07-11 | 日本碍子株式会社 | Honeycomb structure and method for manufacturing the same |
-
2008
- 2008-03-25 JP JP2008077291A patent/JP4998346B2/en not_active Expired - Fee Related
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US9862650B2 (en) | 2014-03-18 | 2018-01-09 | Corning Incorporated | Skinning of ceramic honeycomb bodies |
US10807914B2 (en) | 2014-03-18 | 2020-10-20 | Corning Incorporated | Skinning of ceramic honeycomb bodies |
US11220466B2 (en) | 2014-03-18 | 2022-01-11 | Corning Incorporated | Skinning of ceramic honeycomb bodies |
Also Published As
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JP2009226350A (en) | 2009-10-08 |
DE102009001820A1 (en) | 2009-10-01 |
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