JP2002234780A - Method for producing porous ceramic honeycomb structure - Google Patents
Method for producing porous ceramic honeycomb structureInfo
- Publication number
- JP2002234780A JP2002234780A JP2001025974A JP2001025974A JP2002234780A JP 2002234780 A JP2002234780 A JP 2002234780A JP 2001025974 A JP2001025974 A JP 2001025974A JP 2001025974 A JP2001025974 A JP 2001025974A JP 2002234780 A JP2002234780 A JP 2002234780A
- Authority
- JP
- Japan
- Prior art keywords
- drying
- forming agent
- molded body
- honeycomb structure
- furnace
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000000919 ceramic Substances 0.000 title claims abstract description 22
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 18
- 238000001035 drying Methods 0.000 claims abstract description 76
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 39
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 31
- 229910052878 cordierite Inorganic materials 0.000 claims abstract description 13
- 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 13
- 239000002994 raw material Substances 0.000 claims abstract description 13
- 238000002276 dielectric drying Methods 0.000 claims abstract description 12
- 238000001125 extrusion Methods 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims abstract description 11
- 239000000203 mixture Substances 0.000 claims abstract description 8
- 238000007602 hot air drying Methods 0.000 claims abstract description 7
- 238000000465 moulding Methods 0.000 claims abstract description 7
- 238000010304 firing Methods 0.000 claims description 45
- 239000000843 powder Substances 0.000 claims description 19
- 229920002472 Starch Polymers 0.000 claims description 16
- 239000008107 starch Substances 0.000 claims description 16
- 235000019698 starch Nutrition 0.000 claims description 16
- 238000001704 evaporation Methods 0.000 claims description 15
- 238000004898 kneading Methods 0.000 claims description 7
- 238000002156 mixing Methods 0.000 claims description 6
- 239000011148 porous material Substances 0.000 abstract description 24
- 238000005336 cracking Methods 0.000 abstract description 22
- 241000264877 Hippospongia communis Species 0.000 abstract 4
- 230000000052 comparative effect Effects 0.000 description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 12
- 210000004027 cell Anatomy 0.000 description 10
- 210000002421 cell wall Anatomy 0.000 description 10
- 230000008020 evaporation Effects 0.000 description 9
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 6
- 239000004927 clay Substances 0.000 description 6
- 238000001354 calcination Methods 0.000 description 5
- 239000005995 Aluminium silicate Substances 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 4
- 235000012211 aluminium silicate Nutrition 0.000 description 4
- 230000002950 deficient Effects 0.000 description 4
- 238000011156 evaluation Methods 0.000 description 4
- 239000010419 fine particle Substances 0.000 description 4
- 239000010439 graphite Substances 0.000 description 4
- 229910002804 graphite Inorganic materials 0.000 description 4
- 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 4
- 229920000609 methyl cellulose Polymers 0.000 description 4
- 239000001923 methylcellulose Substances 0.000 description 4
- 235000010981 methylcellulose Nutrition 0.000 description 4
- 239000000454 talc Substances 0.000 description 4
- 229910052623 talc Inorganic materials 0.000 description 4
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 3
- 230000003197 catalytic effect Effects 0.000 description 3
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 235000013312 flour Nutrition 0.000 description 3
- 239000001866 hydroxypropyl methyl cellulose Substances 0.000 description 3
- 229920003088 hydroxypropyl methyl cellulose Polymers 0.000 description 3
- 235000010979 hydroxypropyl methyl cellulose Nutrition 0.000 description 3
- UFVKGYZPFZQRLF-UHFFFAOYSA-N hydroxypropyl methyl cellulose Chemical compound OC1C(O)C(OC)OC(CO)C1OC1C(O)C(O)C(OC2C(C(O)C(OC3C(C(O)C(O)C(CO)O3)O)C(CO)O2)O)C(CO)O1 UFVKGYZPFZQRLF-UHFFFAOYSA-N 0.000 description 3
- 239000000377 silicon dioxide Substances 0.000 description 3
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- 241000209140 Triticum Species 0.000 description 2
- 235000021307 Triticum Nutrition 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 229920002134 Carboxymethyl cellulose Polymers 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000001768 carboxy methyl cellulose Substances 0.000 description 1
- 235000010948 carboxy methyl cellulose Nutrition 0.000 description 1
- 239000008112 carboxymethyl-cellulose Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000007429 general method Methods 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
- 239000003566 sealing material Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
- C04B38/06—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof by burning-out added substances by burning natural expanding materials or by sublimating or melting out added substances
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Filtering Materials (AREA)
- Exhaust Gas Treatment By Means Of Catalyst (AREA)
- Press-Shaping Or Shaping Using Conveyers (AREA)
- Catalysts (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、コーディエライト
組成からなる多孔質セラミックハニカム構造体の製造方
法に関する。なかでも50%以上の気孔率を有する多孔
質セラミックハニカム構造体の製造方法に関する。The present invention relates to a method for producing a porous ceramic honeycomb structure comprising a cordierite composition. In particular, the present invention relates to a method for manufacturing a porous ceramic honeycomb structure having a porosity of 50% or more.
【0002】[0002]
【従来技術】地域環境や地球環境の保全面から、自動車
などのエンジンから排出される排気ガスに含まれる有害
物質の削減が求められ、これに応えるため排気ガス浄化
用の触媒コンバータが用いられている。この触媒コンバ
ータのひとつにセラミックハニカム触媒コンバータがあ
る。また、最近はデイーゼルエンジンからの排気ガス中
に含まれる黒鉛微粒子などを捕集するために、コーディ
エライト組成からなる多孔質セラミックハニカム構造体
(以下、「多孔質セラミックハニカム構造体」を略して
「ハニカム構造体」という)を用い、このハニカム構造
体のセル開口部の両端を交互に目封じした排気ガス浄化
フィルタが使用されてきている。2. Description of the Related Art From the standpoint of preserving the local environment and the global environment, it is required to reduce harmful substances contained in exhaust gas emitted from engines of automobiles and the like. To meet this demand, catalytic converters for purifying exhaust gas have been used. I have. One of the catalytic converters is a ceramic honeycomb catalytic converter. Recently, a porous ceramic honeycomb structure made of cordierite (hereinafter referred to as a “porous ceramic honeycomb structure”) has been abbreviated to collect graphite particles and the like contained in exhaust gas from diesel engines. An exhaust gas purifying filter has been used in which both ends of a cell opening of the honeycomb structure are alternately plugged.
【0003】排気ガス浄化フィルタ10での排気浄化作
用は、以下の通り行われる。排気ガスは、ハニカム構造
体11の流入側11dで開口しているセル11cから流
入(10aで示す)し、セル壁11bに形成された細孔
を通過した後、流出側11eから排出(10bで示す)
される。そして、排気ガス中に含まれる黒鉛微粒子など
は、セル壁11b内で連続する細孔から隣接セルに通過
する際に、濾過され、捕集される。[0003] The exhaust gas purifying operation of the exhaust gas purifying filter 10 is performed as follows. Exhaust gas flows in (shown by 10a) from a cell 11c that is open on the inflow side 11d of the honeycomb structure 11, passes through pores formed in the cell wall 11b, and is discharged from an outflow side 11e (in 10b). Show)
Is done. Graphite fine particles and the like contained in the exhaust gas are filtered and collected when passing through adjacent pores in the cell wall 11b to the adjacent cells.
【0004】次に、ハニカム構造体11の一般的な製造
方法について説明する。先ず、コーディエライト組成が
得られるように、カオリン、タルク、アルミナなどのコ
ーディエライト化原料と、成形助剤、気孔を形成させる
造孔剤、水とを混合、混練してセラミック坏土としてい
る。そして、この坏土を真空脱気した後、押出スクリュ
ー又はプランジャーにより特殊な金型を通じて押出成形
して、外周壁11aやセル壁11bが形成されたハニカ
ム構造を有する成形体(以下、「ハニカム構造を有する
成形体」を略して「成形体」という)としている。そし
て、乾燥し、更にトンネル炉または単独炉などの焼成炉
により、成形体中の成形助剤などのバインダ、結晶水な
どを分解、除去し、所定雰囲気、所定温度下で焼成し
て、各成分間の反応を促進させてコーディエライトを形
成し、同時に焼結によって収縮、緻密化させ、所定の形
状と強度を持ち、かつセル壁11bを貫通する微細な気
孔を持つハニカム構造体11としている。Next, a general method for manufacturing the honeycomb structure 11 will be described. First, as a cordierite composition is obtained, a raw material for forming a cordierite such as kaolin, talc, and alumina, a forming aid, a pore former for forming pores, and water are mixed and kneaded to obtain a ceramic clay. I have. Then, after the kneaded clay is degassed in vacuum, it is extruded through a special mold using an extrusion screw or a plunger to form a formed body having a honeycomb structure in which the outer peripheral wall 11a and the cell wall 11b are formed (hereinafter, “honeycomb”). The “formed body having a structure” is abbreviated to “formed body”. Then, it is dried and further decomposed and removed by a sintering furnace such as a tunnel furnace or a single furnace, a binder such as a molding aid in the molded body, water of crystallization, etc. To promote the reaction between them to form cordierite, and at the same time, shrink and densify by sintering to obtain a honeycomb structure 11 having a predetermined shape and strength and having fine pores penetrating the cell wall 11b. .
【0005】ところで、成形体を得る坏土には、前述の
成形助剤として一般に、メチルセルロース、カルボキシ
メチルセルロース、ポリビニールアルコール、澱粉粉、
グリセリンなどの有機バインダーや界面活性剤ワックス
などを含ませている。また、前述の造孔剤としては、グ
ラファイト、小麦粉、澱粉粉などを含ませたりしてい
る。[0005] By the way, in the kneaded clay for obtaining a molded body, methylcellulose, carboxymethylcellulose, polyvinyl alcohol, starch powder, and the like are generally used as the aforementioned molding aid.
An organic binder such as glycerin and a surfactant wax are included. Further, as the above-mentioned pore-forming agent, graphite, wheat flour, starch powder and the like are included.
【0006】例えば、特公昭63−27303号公報に
は、造孔剤として小麦粉、米粉などの澱粉粉を1〜30
質量%添加、坏土自体の温度を70℃以下として混合混
練し、焼成中に燃焼させる記載がある。For example, Japanese Patent Publication No. 27303/1988 discloses that a starch powder such as wheat flour or rice flour is used as a pore-forming agent.
There is a description that the mass% is added, the temperature of the kneaded material itself is set to 70 ° C. or lower, and the mixture is kneaded and burned during firing.
【0007】また、特許第2562186号公報には、
造孔剤として、大気雰囲気中650℃、1時間保持の熱
処理において、質量減少率が50%以上である易燃焼製
のカーボン粉を使用する記載がある。Further, Japanese Patent No. 2562186 discloses that
There is a description of using an easily combustible carbon powder having a mass reduction rate of 50% or more in a heat treatment held at 650 ° C. for one hour in an air atmosphere as a pore former.
【0008】[0008]
【発明が解決しようとする課題】ところで、図3の排気
ガス浄化フィルタ10には、使用中に、排気ガスに含ま
れる黒鉛微粒子などを高効率で捕集することに加え、セ
ル壁11a内に形成する細孔の気孔率を大きくして圧力
損失を低くし、エンジンへの負荷を少なくすることが要
求されている。そして、ハニカム構造体11の気孔率を
大きくするには、気孔を形成する造孔剤の添加量を多く
しなければならない。By the way, the exhaust gas purifying filter 10 shown in FIG. 3 not only collects the graphite fine particles and the like contained in the exhaust gas with high efficiency during use, but also forms the inside of the cell wall 11a. It is required to increase the porosity of the pores to be formed to reduce the pressure loss and reduce the load on the engine. Then, in order to increase the porosity of the honeycomb structure 11, it is necessary to increase the amount of a pore-forming agent that forms pores.
【0009】しかしながら、前記特公昭63−2730
3号公報での造孔剤である澱粉粉の添加量を多くする
と、坏土調整の際に添加される水などの液体により澱粉
粉が膨潤して、押出成形後の乾燥工程において収縮が大
きくなり、変形、割れ等の問題を引き起こすばかりか、
乾燥ムラを生じ易く、結果として、ハニカム構造体ので
きあがりの寸法精度を悪くする。更に気孔率を大きくす
る為、澱粉粉の添加量を多くすると、焼成時、澱粉粉が
約300℃付近で一斉に熱分解するのに伴い、ハニカム
構造体11に割れが発生しやすい。[0009] However, the above-mentioned JP-B-63-2730.
When the amount of starch powder, which is a pore-forming agent in JP-A-3, is increased, the starch powder swells due to a liquid such as water added at the time of kneading, and the shrinkage is large in the drying step after extrusion molding. Not only causes problems such as deformation and cracking,
Drying unevenness easily occurs, and as a result, the dimensional accuracy of the finished honeycomb structure is deteriorated. If the amount of the starch powder is increased to further increase the porosity, the honeycomb structure 11 tends to crack as the starch powder is thermally decomposed at about 300 ° C. at the time of firing.
【0010】一方、前記特許第2562186号公報で
の造孔剤である易燃焼製のカーボン粉の添加量を多くす
ると、乾燥時に割れが発生することがある。即ち、マイ
クロ波により、成形体全体の水分を均一に蒸発して乾燥
させる際に、成形体内部にカーボン粉が多く添加されて
いると、カーボン粉がマイクロ波を吸収して発熱し、発
熱量が大きくなった場合、カーボン粉が燃焼して成形体
内に割れが発生することがある。また、易燃焼製のカー
ボン粉の添加量を多くすると、焼成時、易燃焼製のカー
ボン粉が約800℃付近で一斉に熱分解するのに伴い、
ハニカム構造体に割れが発生することがある。また、焼
成過程においてもカーボンの燃焼がハニカム構造体の内
外で同時に進行せず、その結果ハニカム構造体に割れが
発生することがある。On the other hand, if the amount of the easily combustible carbon powder, which is the pore-forming agent described in Japanese Patent No. 2562186, is increased, cracks may occur during drying. That is, when the whole of the molded body is uniformly evaporated and dried by microwaves, if a large amount of carbon powder is added to the inside of the molded body, the carbon powder absorbs the microwaves and generates heat, thereby generating heat. When the particle size becomes large, the carbon powder may burn and cracks may occur in the molded body. In addition, when the amount of the easily combustible carbon powder is increased, the easily combustible carbon powder is thermally decomposed at about 800 ° C. at the time of firing.
Cracks may occur in the honeycomb structure. Further, even in the firing process, the combustion of carbon does not proceed simultaneously inside and outside the honeycomb structure, and as a result, cracks may occur in the honeycomb structure.
【0011】ハニカム構造体11の気孔率を大きくする
には、気孔を形成する造孔剤の添加量を多くする必要が
あるが、前述のように乾燥又は焼成後に変形、割れが発
生しやすかった。従って、本発明の課題は、気孔率を大
きくするために、造孔剤を多量に添加しても、成形体の
乾燥又は焼成後に、変形や割れの発生の少ないハニカム
構造体の製造方法を得ることにある。In order to increase the porosity of the honeycomb structure 11, it is necessary to increase the amount of a pore-forming agent for forming pores. However, as described above, deformation and cracking are likely to occur after drying or firing. . Therefore, an object of the present invention is to provide a method for manufacturing a honeycomb structure having less deformation and cracking after drying or firing of a molded article even when a large amount of a pore forming agent is added to increase the porosity. It is in.
【0012】[0012]
【課題を解決するための手段】本発明者らは、造孔剤を
多量に添加した成形体について、乾燥や焼成条件と、発
生する割れとの関係を鋭意研究した。その結果、乾燥工
程において、成形体に添加された水分をマイクロ波又は
誘電乾燥などで適切に蒸発させた後、更に残部を熱風乾
燥により蒸発させること、又は更に、焼成工程におい
て、成形体に添加された造孔剤を熱風循環を行い適切に
焼失させた後、更に残部を単独炉又はトンネル炉等にて
焼失させることで、割れの発生を少なくし、しかも製造
原価を低くできるとの知見を得て本発明に想到した。Means for Solving the Problems The present inventors have made intensive studies on the relationship between drying and firing conditions and cracks generated in a molded article containing a large amount of a pore-forming agent. As a result, in the drying step, after the water added to the molded body is appropriately evaporated by microwave or dielectric drying, the remaining portion is further evaporated by hot air drying, or further added to the molded body in the firing step. It was found that, after the pore forming agent was burned out by circulating hot air and burned out properly, the remainder was burned off in a single furnace or a tunnel furnace to reduce the occurrence of cracks and lower the production cost. The inventors have arrived at the present invention.
【0013】具体的に本発明は、コーディエライト組成
となる原料と、成形助剤、造孔剤、水を混合、混練し、
押出成形法により成形体を作成後、該成形体を乾燥、焼
成する多孔質セラミックハニカム構造体の製造方法であ
って、乾燥工程において、(a)前記成形体の含有水分
の60〜90質量%をマイクロ波乾燥炉又は誘電乾燥炉
にて蒸発させる第1の乾燥工程、(b)前記成形体の含
有水分の残部を熱風炉にて蒸発させる第2の乾燥工程、
を有することを特徴とする。また、焼成工程において、
(c)前記造孔剤を熱風循環炉により50〜70質量%
焼失させる第1の焼成工程、(d)造孔剤の残部を単独
炉又はトンネル炉等にて焼失させる第2の焼成工程、を
有することを特徴とする。また、乾燥工程において、
(a)前記成形体の含有水分の60〜90質量%をマイ
クロ波乾燥炉又は誘電乾燥炉にて蒸発させる第1の乾燥
工程、(b)前記成形体の含有水分の残部を熱風炉にて
蒸発させる第2の乾燥工程、次いで焼成工程において、
(c)前記造孔剤を熱風循環炉により50〜70質量%
焼失させる第1の焼成工程、(d)造孔剤の残部を単独
炉又はトンネル炉等にて焼失させる第2の焼成工程、を
有することを特徴とする。この時、前記造孔剤は澱粉粉
であることが好ましい。Specifically, the present invention is to mix and knead a raw material for forming a cordierite composition, a molding aid, a pore former, and water.
A method for producing a porous ceramic honeycomb structure, in which a molded body is formed by an extrusion molding method, and then dried and fired, wherein in the drying step, (a) 60 to 90% by mass of the water content of the molded body In a microwave drying furnace or a dielectric drying furnace, (b) a second drying step in which the remaining moisture contained in the molded body is evaporated in a hot-air oven,
It is characterized by having. In the firing step,
(C) 50 to 70% by mass of the pore former in a hot air circulating furnace.
It is characterized by having a first firing step for burning out and (d) a second firing step for burning off the remaining part of the pore-forming agent in a single furnace or a tunnel furnace or the like. In the drying step,
(A) a first drying step of evaporating 60 to 90% by mass of the water content of the compact in a microwave drying furnace or a dielectric drying furnace, and (b) the remaining moisture content of the compact in a hot air oven. In the second drying step of evaporating and then in the baking step,
(C) 50 to 70% by mass of the pore former in a hot air circulating furnace.
It is characterized by having a first firing step for burning out and (d) a second firing step for burning off the remaining part of the pore-forming agent in a single furnace or a tunnel furnace or the like. At this time, the pore-forming agent is preferably starch powder.
【0014】次に、本発明での構成の理由を説明する。 (第1の乾燥工程)成形体乾燥後の変形、ワレを少なく
するには、第1の乾燥工程として、マイクロ波乾燥炉又
は誘電乾燥炉にて成形体の含有水分の60質量%以上を
蒸発させる必要がある。一方、この第1の乾燥工程にて
成形体の含有水分の90質量%を超えて蒸発させると、
第1の乾燥工程で、成形体に変形や割れが発生しやす
い。従って、第1の乾燥工程で、成形体の含有水分の6
0〜90質量%を蒸発させる。好ましくは70〜80質
量%である。また、マイクロ波乾燥又は誘電乾燥を行う
際には、成形体の大きさに応じた出力で行うのが好まし
い。Next, the reason for the configuration according to the present invention will be described. (First drying step) In order to reduce deformation and cracking after drying of the compact, as a first drying step, 60% by mass or more of the water content of the compact is evaporated in a microwave drying furnace or a dielectric drying furnace. Need to be done. On the other hand, when evaporating more than 90% by mass of the water content of the molded body in the first drying step,
In the first drying step, the molded body is likely to be deformed or cracked. Therefore, in the first drying step, 6% of the water content
0-90% by weight is evaporated. Preferably it is 70-80 mass%. Further, when performing microwave drying or dielectric drying, it is preferable to perform the drying with an output corresponding to the size of the molded body.
【0015】(第2の乾燥工程)第1の乾燥に続く第2
の乾燥工程で、成形体の含有水分の残部を蒸発させる。
第2の乾燥工程は、熱風乾燥炉で、成形体を100〜1
20℃付近まで加熱するのが好ましい。(Second Drying Step) The second drying step following the first drying step
In the drying step, the remaining water content of the molded body is evaporated.
In the second drying step, the molded body is heated in a hot-air drying oven at 100 to 1 mm.
It is preferred to heat to around 20 ° C.
【0016】(第1の焼成工程)成形体焼成後の割れを
少なくするには、第1の焼成工程として、熱風循環炉に
て造孔剤の50質量%以上焼失させる必要がある。一
方、第1の焼成工程での造孔剤の焼失が70質量%を超
えると、第1の焼成工程中又は後の成形体の強度低下を
招き、熱風によるワレ又は第1の焼成工程から第2の焼
成工程に移る際の成形体の移載作業等が発生した場合に
おける機械的外力により割れの発生することがある。従
って、第1の焼成工程で、造孔剤の50〜70質量%を
焼失させる。好ましくは55〜65質量%である。(First firing step) In order to reduce cracks after firing the compact, it is necessary to burn out at least 50% by mass of the pore former in a hot air circulation furnace as a first firing step. On the other hand, if the loss of the pore-forming agent in the first baking step exceeds 70% by mass, the strength of the formed body during or after the first baking step is reduced, and cracking by hot air or the first baking step is performed. In the case where the transfer operation of the molded body at the time of shifting to the firing step 2 occurs, a crack may be generated due to mechanical external force. Therefore, in the first firing step, 50 to 70% by mass of the pore former is burned off. Preferably it is 55-65 mass%.
【0017】(第2の焼成工程)第1の焼成工程に続く
第2の焼成工程で、添加した造孔剤の残部を焼失させ
る。この第2の焼成工程は、単独炉、トンネル炉または
ローラーハースキルンなどの焼成炉により行うことがで
きる。(Second firing step) In the second firing step following the first firing step, the remaining part of the added pore-forming agent is burned off. This second firing step can be performed in a single furnace, a tunnel furnace, or a firing furnace such as a roller hearth kiln.
【0018】[0018]
【発明の実施の形態】以下、発明の実施の形態を実施例
をもとに詳細に説明する。図1は、実施の形態でのハニ
カム構造体の製造工程を示す図である。図2及び図3に
示すハニカム構造体11を以下のようにして製造した。DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments of the present invention will be described below in detail with reference to examples. FIG. 1 is a diagram illustrating a manufacturing process of the honeycomb structure according to the embodiment. The honeycomb structure 11 shown in FIGS. 2 and 3 was manufactured as follows.
【0019】(実施例1)カオリン、タルク、シリカ、
水酸化アルミ、アルミナなどの粉末を調整してコーディ
エライト質セラミック原料とし、このセラミック原料に
対して、成形助剤として、メチルセルロースを3〜10
質量%と、ヒドロキシプロピルメチルセルロースをメチ
ルセルロースに対して質量比30〜50%添加する。そ
して、造孔剤として、セラミック原料に対して澱粉粉3
0質量%を添加する。次いで、乾式で十分混合した後、
規定量の水を注入して更に十分な混練を行い、坏土を精
製した。次に、押出成形用金型を用い押出成形して、φ
150mm×長さ160mmのハニカム構造を有する成
形体とした。次に、この成形体について、誘電乾燥を行
い成形体の含有水分の蒸発量を変えながら第1の乾燥を
行い、次に、熱風乾燥炉で、第1の乾燥工程後の成形体
を120℃に加熱して第2の乾燥を行った。(Example 1) Kaolin, talc, silica,
A powder of aluminum hydroxide, alumina or the like is prepared to obtain a cordierite ceramic raw material.
% By mass, and 30 to 50% by mass ratio of hydroxypropyl methylcellulose to methylcellulose. And, as a pore-forming agent, starch powder 3
0% by weight is added. Then, after thoroughly mixing in a dry system,
A specified amount of water was injected to perform further sufficient kneading to purify the clay. Next, extrusion molding is performed using an extrusion molding die.
A molded body having a honeycomb structure of 150 mm × length 160 mm was obtained. Next, the formed body is subjected to dielectric drying to perform first drying while changing the amount of moisture contained in the formed body, and then the formed body after the first drying step is heated to 120 ° C. in a hot air drying furnace. To perform a second drying.
【0020】そして、第1の乾燥工程での成形体の含有
水分の蒸発割合と、(A):誘電乾燥での第1の乾燥工
程後の変形又は割れ、(B):乾燥工程終了後の変形又
は割れを評価した。なお、第1の乾燥工程での水分の蒸
発割合は、第1の乾燥工程前後の成形体の質量差及び、
第1及び第2の乾燥工程前後の質量の差から全蒸発量を
求め、その中の第1の乾燥工程時の蒸発量の割合として
求めた。また、変形又は割れの発生は、1ロットあたり
5%以下を優(○)、1ロットあたり5〜10%を良
(△)、1ロットあたり10%を超えるものを不具合
(×)として判定した。その結果を表1に示す。Then, the evaporation rate of the moisture contained in the compact in the first drying step, (A): deformation or cracking after the first drying step in dielectric drying, and (B): after the drying step Deformation or cracking was evaluated. In addition, the evaporation rate of water in the first drying step is based on the difference in mass of the molded body before and after the first drying step, and
The total amount of evaporation was determined from the difference between the masses before and after the first and second drying steps, and was calculated as the ratio of the amount of evaporation during the first drying step. In addition, the occurrence of deformation or cracking was judged as excellent (○) when 5% or less per lot was good (○), good (5〜) when 5 to 10% per lot, and defective ()) when more than 10% per lot. . Table 1 shows the results.
【0021】 (表1) 第1の乾燥工程での 変形又は割れの評価 区 分 水分蒸発割合(質量%) (A)第1の乾燥後 (B)乾燥工程終了後 比較例 1 47 ○ × 比較例 2 51 ○ × 比較例 3 58 ○ × 発明例 1 63 ○ △ 発明例 2 67 ○ △ 発明例 3 72 ○ ○ 発明例 4 75 ○ ○ 発明例 5 77 ○ ○ 発明例 6 80 ○ ○ 発明例 7 87 △ △ 比較例 4 94 × × 比較例 5 100 × ×(Table 1) In the first drying stepEvaluation of deformation or crack Division Water evaporation rate (% by mass) (A) After the first drying (B) After the drying step Comparative Example 1 47 ○ × Comparative Example 2 51 ○ × Comparative Example 3 58 ○ × Invention Example 1 63 ○ △ Invention Example 2 67 ○ △ Invention Example 3 72 ○ ○ Invention Example 4 75 ○ ○ Invention Example 5 77 ○ ○ Invention Example 6 80 ○ ○ Invention 7 87 △ △ Comparative 4 94 × × Comparative 5 100 × ×
【0022】表1の発明例1〜7に示すように、第1の
乾燥工程で含有水分の60〜90質量%を蒸発させれ
ば、第1の乾燥工程後又は乾燥工程終了後に、変形や割
れの発生が少ないことがわかる。更に、第1の乾燥工程
での成形体の含有水分の蒸発量が70〜80質量%で
は、変形や割れの発生が少ない好ましい結果となった。As shown in Inventive Examples 1 to 7 in Table 1, if 60 to 90% by mass of the contained water is evaporated in the first drying step, deformation or deformation occurs after the first drying step or after the drying step. It can be seen that the occurrence of cracks is small. Further, when the amount of moisture contained in the molded body in the first drying step was 70 to 80% by mass, favorable results were obtained in which deformation and cracking were less likely to occur.
【0023】(実施例2)カオリン、タルク、シリカ、
水酸化アルミ、アルミナなどの粉末を調整してコーディ
エライト質セラミック原料とし、このセラミック原料に
対して、成形助剤として、メチルセルロースを3〜10
質量%と、ヒドロキシプロピルメチルセルロースをメチ
ルセルロースに対して質量比30〜50%添加する。そ
して、セラミック原料に対して造孔剤として澱粉粉30
質量%を添加する。次いで、乾式で十分混合した後、規
定量の水を注入して更に十分な混練を行い、坏土を精製
した。次に、押出成形用金型を用い押出成形して、φ1
50mm×長さ160mmのハニカム構造を有する成形
体とした。次に、この成形体を乾燥後、熱風循環を行い
添加した造孔剤である澱粉粉の焼失量を変えながら熱風
循環炉にて第1の焼成を行った。更に、第1の焼成をし
た成形体を熱風循環を行わず、バッチ式焼成炉にて14
00℃までの第2の焼成を行い、φ145mm×長さ1
55mm、セル壁厚0.30mm、セルピッチ1.80
mm、気孔率50〜80%のハニカム構造体とした。Example 2 Kaolin, talc, silica,
A powder of aluminum hydroxide, alumina or the like is prepared to obtain a cordierite ceramic raw material.
% By mass, and 30 to 50% by mass ratio of hydroxypropyl methylcellulose to methylcellulose. Then, starch powder 30 is used as a pore-forming agent for the ceramic raw material.
% By weight is added. Next, after sufficient mixing in a dry system, a specified amount of water was poured and further sufficient kneading was performed to purify the clay. Next, extrusion molding is performed using an extrusion molding die.
A molded body having a honeycomb structure of 50 mm × length 160 mm was obtained. Next, after drying this molded body, the first baking was performed in a hot-air circulating furnace while circulating hot air and changing the burnout amount of starch powder, which was the added pore-forming agent. Further, the molded body subjected to the first calcination is subjected to a batch-type calcination furnace without circulating hot air.
A second firing up to 00 ° C. is performed, φ145 mm × length 1
55 mm, cell wall thickness 0.30 mm, cell pitch 1.80
mm and a porosity of 50 to 80%.
【0024】そして、第1の焼成工程での造孔剤の焼失
割合と、(C):第1の焼成工程後の変形又は割れ、
(D):焼成工程終了後の変形又は割れを評価した。な
お、造孔剤の第1の焼成工程での焼失割合は、第1の焼
成工程前後の製品の質量差から添加した成形助剤及び、
セラミック原料に含まれる結晶水の理論焼失質量を減じ
て造孔剤の焼失質量とし、造孔剤添加量との比率を焼失
割合とした。また、変形又は割れの発生は、1ロットあ
たり1%以下を優(○)、1ロットあたり1〜2%を良
(△)、1ロットあたり2%を超えるものを不具合
(×)として判定した。その結果を表2に示す。Then, the burnout ratio of the pore-forming agent in the first firing step, and (C): deformation or cracking after the first firing step;
(D): The deformation or crack after the completion of the firing step was evaluated. The burn-out rate of the pore-forming agent in the first baking step was determined based on the difference in mass of the product before and after the first baking step.
The theoretical mass of crystallization water contained in the ceramic raw material was subtracted to obtain the mass of the pore-forming agent, and the ratio to the amount of the pore-forming agent added was defined as the proportion of the burning-off. In addition, the occurrence of deformation or cracking was determined as excellent (○) when 1% or less per lot was good (○), 1-2% per lot was good (△), and that exceeding 2% per lot was defective (×). . Table 2 shows the results.
【0025】 (表2) 第1の焼成工程での 変形又は割れの評価 区 分 造孔剤焼失割合(質量%) (C)第1の焼成後 (D)焼成工程終了後 比較例 6 41 ○ × 比較例 7 47 ○ × 比較例 8 49 ○ × 発明例 8 52 ○ △ 発明例 9 55 ○ ○ 発明例10 57 ○ ○ 発明例11 60 ○ ○ 発明例12 63 ○ ○ 発明例13 68 △ △ 発明例14 70 △ △ 比較例 9 80 × × 比較例10 100 × ×[0025] (Table 2) first modification or cracking evaluation Classification pore former burn off ratio of at firing step (wt%) (C) after the first calcination (D) firing step after completion of Comparative Example 6 41 ○ × Comparative Example 7 47 ○ × Comparative Example 8 49 ○ × Invention Example 8 52 ○ △ Invention Example 9 55 ○ ○ Invention Example 10 57 ○ ○ Invention Example 11 60 ○ ○ Invention Example 12 63 ○ ○ Invention Example 13 68 △ △ Invention Example 14 70 △ △ Comparative Example 9 80 × × Comparative Example 10 100 × ×
【0026】表2の発明例8〜14に示すように、第1の
焼成工程で添加した澱粉粉の50〜70質量%を焼失さ
せれば、第1の焼成工程後又は焼成工程終了後に、変形
や割れの発生が少ないことがわかる。好ましくは55〜
65質量%である。As shown in Invention Examples 8 to 14 in Table 2, if 50 to 70% by mass of the starch powder added in the first baking step is burned off, after the first baking step or after the completion of the baking step, It can be seen that the occurrence of deformation and cracking is small. Preferably 55 to
65% by mass.
【0027】変形や割れの発生が無かったハニカム構造
体は、必要に応じて、セル壁11b及び細孔内に触媒を
担持する。そして、ハニカム構造体11は、排気ガス流
入側11dのセルを一個おきに目封じし、排気ガス流出
側11eでは流入側11dで目封じしてないセルについ
てのみ目封じし、収納容器12内に収納することで、圧
力損失が少ないと共に、排気ガス中の微粒子を高効率に
捕集し、又は更に、エンジン始動直後から浄化機能を高
めることのできる、排気ガス浄化フィルタ10となる。The honeycomb structure, which has not been deformed or cracked, supports a catalyst in the cell walls 11b and in the pores as necessary. The honeycomb structure 11 plugs every other cell on the exhaust gas inflow side 11d, and plugs only cells not sealed on the inflow side 11d on the exhaust gas outflow side 11e. By storing the filter, the exhaust gas purifying filter 10 can reduce the pressure loss and efficiently collect the fine particles in the exhaust gas, or can further enhance the purifying function immediately after the engine is started.
【0028】(実施例3)カオリン、タルク、シリカ、
水酸化アルミ、アルミナなどの粉末を調整してコーディ
エライト質セラミック原料とし、このセラミック原料に
対して、成形助剤として、メチルセルロースを3〜10
質量%と、ヒドロキシプロピルメチルセルロースをメチ
ルセルロースに対して質量比30〜50%添加する。そ
して、セラミック原料に対して造孔剤として澱粉粉30
質量%を添加する。次いで、乾式で十分混合した後、規
定量の水を注入して更に十分な混練を行い、坏土を精製
した。次に、押出成形用金型を用い押出成形して、φ1
50mm×長さ160mmのハニカム構造を有する成形
体とした。次に、この成形体について、誘電乾燥を行い
成形体の含有水分の蒸発量を変えながら第1の乾燥を行
い、次に、熱風乾燥炉で、第1の乾燥工程後の成形体を
120℃に加熱して第2の乾燥を行った。次に、熱風循
環炉にて添加した造孔剤である澱粉粉の焼失量を変えな
がら第1の焼成を行った。更に、第1の焼成をした成形
体を熱風循環を行わず、バッチ式焼成炉にて1400℃
までの第2の焼成を行い、φ145mm×長さ155m
m、セル壁厚0.30mm、セルピッチ1.80mm、
気孔率50〜80%のハニカム構造体とした。Example 3 Kaolin, talc, silica,
A powder of aluminum hydroxide, alumina or the like is prepared to obtain a cordierite ceramic raw material.
% By mass, and 30 to 50% by mass ratio of hydroxypropyl methylcellulose to methylcellulose. Then, starch powder 30 is used as a pore-forming agent for the ceramic raw material.
% By weight is added. Next, after sufficient mixing in a dry system, a specified amount of water was poured and further sufficient kneading was performed to purify the clay. Next, extrusion molding is performed using an extrusion molding die.
A molded body having a honeycomb structure of 50 mm × length 160 mm was obtained. Next, the formed body is subjected to dielectric drying to perform first drying while changing the amount of moisture contained in the formed body, and then the formed body after the first drying step is heated to 120 ° C. in a hot air drying furnace. To perform a second drying. Next, the first baking was performed in a hot-air circulating furnace while changing the burnout amount of the starch powder as a pore-forming agent added. Further, the molded body subjected to the first calcination is not subjected to hot air circulation, and is heated to 1400 ° C. in a batch-type calcination furnace.
The second firing is performed until φ145 mm x length 155 m
m, cell wall thickness 0.30 mm, cell pitch 1.80 mm,
The honeycomb structure had a porosity of 50 to 80%.
【0029】そして、乾燥工程において、第1の乾燥工
程での成形体の含有水分の蒸発割合と、(A):誘電乾
燥での第1の乾燥工程後の変形又は割れ、(B):乾燥
工程終了後の変形又は割れを評価した。なお、第1の乾
燥工程での水分の蒸発割合は、第1の乾燥工程前後の成
形体の質量差及び、第1及び第2の乾燥工程前後の質量
の差から全蒸発量を求め、その中の第1の乾燥工程時の
蒸発量の割合として求めた。また、変形又は割れの発生
は、1ロットあたり5%以下を優(○)、1ロットあた
り5〜10%を良(△)、1ロットあたり10%を超え
るものを不具合(×)として判定した。その結果を表3
に示す。更に、第1の焼成工程での造孔剤の焼失割合
と、(C):第1の焼成工程後の変形又は割れ、
(D):焼成工程終了後の変形又は割れを評価した。な
お、造孔剤の第1の焼成工程での焼失割合は、第1の焼
成工程前後の製品の質量差から添加した成形助剤及び、
セラミック原料に含まれる結晶水の理論焼失質量を減じ
て造孔剤の焼失質量とし、造孔材添加量との比率を焼失
割合とした。また、変形又は割れの発生は、1ロットあ
たり1%以下を優(○)、1ロットあたり1〜2%を良
(△)、1ロットあたり2%を超えるものを不具合
(×)として判定した。その結果を表4に示す。Then, in the drying step, the evaporation rate of the moisture contained in the compact in the first drying step, (A): deformation or cracking after the first drying step in dielectric drying, and (B): drying Deformation or cracking after the end of the process was evaluated. In addition, the evaporation rate of water in the first drying step is obtained by calculating the total evaporation amount from the difference in mass between the molded bodies before and after the first drying step and the difference in mass between before and after the first and second drying steps. In the first drying step. In addition, the occurrence of deformation or cracking was judged as excellent (○) when 5% or less per lot was good (○), good (5〜) when 5 to 10% per lot, and defective ()) when more than 10% per lot. . Table 3 shows the results.
Shown in Further, the burnout ratio of the pore-forming agent in the first firing step, and (C): deformation or cracking after the first firing step,
(D): The deformation or crack after the completion of the firing step was evaluated. The burn-out rate of the pore-forming agent in the first baking step was determined based on the difference in mass of the product before and after the first baking step.
The theoretical mass of crystallization water contained in the ceramic raw material was subtracted to obtain the mass of the pore-forming agent, and the ratio with the amount of the pore-forming material added was taken as the mass-burning ratio. In addition, the occurrence of deformation or cracking was determined as excellent (○) when 1% or less per lot was good (○), 1-2% per lot was good (△), and that exceeding 2% per lot was defective (×). . Table 4 shows the results.
【0030】 (表3) 第1の乾燥工程での 変形又は割れの評価 区 分 水分蒸発割合(質量%) (A)第1の乾燥後 (B)乾燥工程終了後 比較例11 60 ○ △ 発明例15 69 ○ △ 発明例16 74 ○ ○ 発明例17 79 ○ ○ 比較例12 89 ○ △(Table 3) In the first drying stepEvaluation of deformation or crack Division Water evaporation rate (% by mass) (A) After the first drying (B) After the drying step Comparative Example 11 60 ○ △ Invention Example 15 69 ○ △ Invention Example 16 74 ○ ○ Invention Example 17 79 ○ ○ Comparative Example 12 89 ○ △
【0031】 (表4) 第1の焼成工程での 変形又は割れの評価 区 分 造孔剤焼失割合(質量%) (C)第1の焼成後 (D)焼成工程終了後 比較例11 46 ○ × 発明例15 54 ○ △ 発明例16 58 ○ ○ 発明例17 64 ○ ○ 比較例12 75 × ×[0031] (Table 4) the first variant or cracking evaluation Classification pore former burn off ratio of at firing step (wt%) (C) first after firing (D) firing step after completion of Comparative Example 11 46 ○ × Invention Example 15 54 ○ △ Invention Example 16 58 ○ ○ Invention Example 17 64 ○ ○ Comparative Example 12 75 × ×
【0032】表3、4の発明例15〜17に示すよう
に、第1の乾燥工程で成形体の含有水分の60〜90質
量%を蒸発させれば、第1の乾燥工程後又は乾燥工程終
了後に、変形や割れの発生が少なく、更に、第1の焼成
工程で添加した澱粉粉の50〜70質量%を焼失させれ
ば、第1の焼成工程後又は焼成工程終了後に、変形や割
れの発生が少ないことがわかる。好ましくは55〜65
質量%焼失させればよい。As shown in Inventive Examples 15 to 17 in Tables 3 and 4, if 60 to 90% by mass of the water content of the molded body is evaporated in the first drying step, after or after the first drying step. After the completion, deformation or cracking is less likely to occur, and if 50 to 70% by mass of the starch powder added in the first baking step is burned off, deformation or cracking will occur after the first baking step or after the baking step. It can be seen that the occurrence of is small. Preferably 55 to 65
What is necessary is just to burn out by mass%.
【0033】変形や割れの発生が無かったハニカム構造
体は、必要に応じて、セル壁11b及び細孔内に触媒を
担持する。そして、ハニカム構造体11は、排気ガス流
入側11dのセルを一個おきに目封じし、排気ガス流出
側11eでは流入側11dで目封じしてないセルについ
てのみ目封じし、収納容器12内に収納することで、圧
力損失が少ないと共に、排気ガス中の微粒子を高効率に
捕集し、又は更に、エンジン始動直後から浄化機能を高
めることのできる、排気ガス浄化フィルタ10となる。The honeycomb structure, which has not been deformed or cracked, supports a catalyst in the cell walls 11b and in the pores as needed. The honeycomb structure 11 plugs every other cell on the exhaust gas inflow side 11d, and plugs only cells not sealed on the inflow side 11d on the exhaust gas outflow side 11e. By storing the filter, the exhaust gas purifying filter 10 can reduce the pressure loss and efficiently collect the fine particles in the exhaust gas, or can further enhance the purifying function immediately after the engine is started.
【0034】[0034]
【発明の効果】以上詳細に説明のとおり、本発明のハニ
カム構造体の製造方法によれば、気孔率を大きくするた
めに、造孔剤を多量に添加しても、乾燥後や焼成後に変
形や割れの発生の少ないハニカム構造体を得ることがで
きる。As described in detail above, according to the method for manufacturing a honeycomb structure of the present invention, even if a large amount of a pore-forming agent is added to increase the porosity, the honeycomb structure is deformed after drying or firing. A honeycomb structure with less occurrence of cracks and cracks can be obtained.
【図1】実施の形態でのハニカム構造体の製造工程を示
す図である。FIG. 1 is a diagram illustrating a manufacturing process of a honeycomb structure according to an embodiment.
【図2】ハニカム構造体の斜視図である。FIG. 2 is a perspective view of a honeycomb structure.
【図3】図2のハニカム構造体を用いた排気ガス浄化フ
ィルタ10の一例の断面模式図である。FIG. 3 is a schematic cross-sectional view of an example of an exhaust gas purification filter 10 using the honeycomb structure of FIG.
10a:ガス流入 10b:ガス排出 11:ハニカム構造体 11a:外周壁 11b:セル壁 11c:セル 11d:流入側 11e:流出側 12:収納容器 23a、23b:把持部材 31a、31b:封じ材 31d:貫通孔 10a: gas inflow 10b: gas discharge 11: honeycomb structure 11a: outer peripheral wall 11b: cell wall 11c: cell 11d: inflow side 11e: outflow side 12: storage container 23a, 23b: gripping member 31a, 31b: sealing material 31d: Through hole
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI テーマコート゛(参考) B01J 32/00 ZAB B01J 35/04 301N 35/04 301 B28B 3/20 K B28B 3/20 B01D 53/36 C Fターム(参考) 4D019 AA01 BA05 BB06 CB06 4D048 AA14 BB02 BB17 CC41 4G054 AA06 AB09 BD01 BD19 DA03 4G069 AA01 AA08 BA13A BA13B BA29C DA05 EA19 FB30 FB57 FB58 FB67 FC03 ──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. 7 Identification symbol FI Theme coat ゛ (Reference) B01J 32/00 ZAB B01J 35/04 301N 35/04 301 B28B 3/20 K B28B 3/20 B01D 53/36 CF term (reference) 4D019 AA01 BA05 BB06 CB06 4D048 AA14 BB02 BB17 CC41 4G054 AA06 AB09 BD01 BD19 DA03 4G069 AA01 AA08 BA13A BA13B BA29C DA05 EA19 FB30 FB57 FB58 FB67 FC03
Claims (4)
形助剤、造孔剤、水を混合、混練し、押出成形法により
成形体を作成後、該成形体を乾燥、焼成する多孔質セラ
ミックハニカム構造体の製造方法であって、乾燥工程に
おいて、(a)前記成形体の含有水分の60〜90質量
%をマイクロ波乾燥炉又は誘電乾燥炉にて蒸発させる第
1の乾燥工程、(b)前記成形体の含有水分の残部を熱
風乾燥炉にて蒸発させる第2の乾燥工程、を有すること
を特徴とする多孔質セラミックハニカム構造体の製造方
法。1. A porous ceramic obtained by mixing and kneading a raw material for forming a cordierite composition, a molding aid, a pore-forming agent, and water, forming a molded body by an extrusion molding method, and drying and firing the molded body. A method for manufacturing a honeycomb structure, wherein in a drying step, (a) a first drying step of evaporating 60 to 90% by mass of the water content of the molded body in a microwave drying furnace or a dielectric drying furnace, (b) A) a second drying step of evaporating a remaining portion of the water content of the molded body in a hot-air drying oven.
形助剤、造孔剤、水を混合、混練し、押出成形後、乾
燥、焼成する多孔質セラミックハニカム構造体の製造方
法であって、焼成工程において、(c)前記造孔剤を熱
風循環炉にて50〜70質量%焼失させる第1の焼成工
程、(d)前記造孔剤の残部を単独炉又はトンネル炉等
にて焼失させる第2の焼成工程、を有することを特徴と
する多孔質セラミックハニカム構造体の製造方法。2. A method for producing a porous ceramic honeycomb structure, comprising mixing and kneading a raw material for forming a cordierite composition, a molding aid, a pore-forming agent, and water, extruding, drying, and firing. In the firing step, (c) a first firing step in which the pore-forming agent is burned out by 50 to 70% by mass in a hot-air circulation furnace, and (d) the remaining part of the hole-forming agent is burned out in a single furnace or a tunnel furnace. A method for producing a porous ceramic honeycomb structure, comprising a second firing step.
形助剤、造孔剤、水を混合、混練し、押出成形法により
成形体を作成後、該成形体を乾燥、焼成する多孔質セラ
ミックハニカム構造体の製造方法であって、乾燥工程に
おいて(a)前記成形体の含有水分の60〜90質量%
をマイクロ波乾燥炉又は誘電乾燥炉にて蒸発させる第1
の乾燥工程、(b)前記成形体の含有水分の残部を熱風
乾燥炉にて蒸発させる第2の乾燥工程、次いで焼成工程
において(c)前記造孔剤を熱風循環炉にて50〜70
質量%焼失させる第1の焼成工程、(d)前記造孔剤の
残部を単独炉又はトンネル炉等にて焼失させる第2の焼
成工程、を有することを特徴とする多孔質セラミックハ
ニカム構造体の製造方法。3. A porous ceramic obtained by mixing and kneading a raw material having a cordierite composition, a molding aid, a pore-forming agent, and water, forming a molded body by an extrusion molding method, and drying and firing the molded body. A method for manufacturing a honeycomb structure, comprising: (a) 60 to 90% by mass of water content of the molded body in a drying step;
First in a microwave drying oven or a dielectric drying oven
(B) a second drying step of evaporating the remaining moisture content of the compact in a hot-air drying furnace, and then a baking step (c) the pore-forming agent is heated to 50 to 70 in a hot-air circulating furnace.
A porous ceramic honeycomb structure, comprising: a first firing step of burning out the mass% by mass; and (d) a second firing step of burning out the remainder of the pore-forming agent in a single furnace or a tunnel furnace. Production method.
する請求項1乃至請求項3の何れか1項に記載の多孔質
セラミックハニカム構造体の製造方法。4. The method for producing a porous ceramic honeycomb structure according to claim 1, wherein the pore-forming agent is starch powder.
Priority Applications (1)
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|---|---|---|---|
| JP2001025974A JP2002234780A (en) | 2001-02-01 | 2001-02-01 | Method for producing porous ceramic honeycomb structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001025974A JP2002234780A (en) | 2001-02-01 | 2001-02-01 | Method for producing porous ceramic honeycomb structure |
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|---|---|
| JP2002234780A true JP2002234780A (en) | 2002-08-23 |
Family
ID=18890877
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001025974A Pending JP2002234780A (en) | 2001-02-01 | 2001-02-01 | Method for producing porous ceramic honeycomb structure |
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| Country | Link |
|---|---|
| JP (1) | JP2002234780A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005000873A (en) * | 2003-06-13 | 2005-01-06 | Catalysts & Chem Ind Co Ltd | Process for producing hydrocarbon hydrotreating catalyst composition |
| JP2005013930A (en) * | 2003-06-27 | 2005-01-20 | Catalysts & Chem Ind Co Ltd | Method for producing alumina-containing porous inorganic oxide support and hydrotreating catalyst composition using the support |
| WO2005023503A1 (en) * | 2003-09-02 | 2005-03-17 | Ngk Insulators, Ltd. | Method and apparatus for drying honeycomb formed article |
| WO2008044508A1 (en) * | 2006-09-29 | 2008-04-17 | Hitachi Metals, Ltd. | Process for producing cordierite ceramic honeycomb filter |
| JP2008119666A (en) * | 2006-11-15 | 2008-05-29 | Denso Corp | Manufacturing method of exhaust gas purifying filter |
| JP2008119664A (en) * | 2006-11-15 | 2008-05-29 | Denso Corp | Manufacturing method of exhaust gas purifying filter |
| JP2008290077A (en) * | 2008-08-14 | 2008-12-04 | Hitachi Metals Ltd | Ceramic honeycomb filter and method for manufacturing ceramic honeycomb filter |
| CN100577383C (en) * | 2003-09-02 | 2010-01-06 | 日本碍子株式会社 | Drying method and drying device for honeycomb formed body |
| US20100080930A1 (en) * | 2007-03-28 | 2010-04-01 | Hitachi Metals, Ltd. | Method for producing ceramic honeycomb structure |
| CN107718262A (en) * | 2017-08-29 | 2018-02-23 | 神华集团有限责任公司 | The manufacturing system of haydite |
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| JPH0977552A (en) * | 1995-09-18 | 1997-03-25 | Sharp Corp | Method for drying ceramic molded products |
| JPH0977573A (en) * | 1995-07-12 | 1997-03-25 | Denso Corp | Honeycomb structure and its production |
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| JPH0977573A (en) * | 1995-07-12 | 1997-03-25 | Denso Corp | Honeycomb structure and its production |
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Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005000873A (en) * | 2003-06-13 | 2005-01-06 | Catalysts & Chem Ind Co Ltd | Process for producing hydrocarbon hydrotreating catalyst composition |
| JP2005013930A (en) * | 2003-06-27 | 2005-01-20 | Catalysts & Chem Ind Co Ltd | Method for producing alumina-containing porous inorganic oxide support and hydrotreating catalyst composition using the support |
| CN100577383C (en) * | 2003-09-02 | 2010-01-06 | 日本碍子株式会社 | Drying method and drying device for honeycomb formed body |
| WO2005023503A1 (en) * | 2003-09-02 | 2005-03-17 | Ngk Insulators, Ltd. | Method and apparatus for drying honeycomb formed article |
| JPWO2005023503A1 (en) * | 2003-09-02 | 2007-11-01 | 日本碍子株式会社 | Method and apparatus for drying honeycomb molded body |
| JP4713342B2 (en) * | 2003-09-02 | 2011-06-29 | 日本碍子株式会社 | Method and apparatus for drying honeycomb molded body |
| US7721461B2 (en) | 2003-09-02 | 2010-05-25 | Ngk Insulators, Ltd. | Method and apparatus for drying honeycomb formed body |
| WO2008044508A1 (en) * | 2006-09-29 | 2008-04-17 | Hitachi Metals, Ltd. | Process for producing cordierite ceramic honeycomb filter |
| US8398797B2 (en) | 2006-09-29 | 2013-03-19 | Hitachi Metals, Ltd. | Production method of cordierite-based ceramic honeycomb filter |
| JP5338317B2 (en) * | 2006-09-29 | 2013-11-13 | 日立金属株式会社 | Cordierite ceramic honeycomb filter manufacturing method |
| KR101419291B1 (en) | 2006-09-29 | 2014-07-14 | 히타치 긴조쿠 가부시키가이샤 | Process for producing cordierite ceramic honeycomb filter |
| JP2008119664A (en) * | 2006-11-15 | 2008-05-29 | Denso Corp | Manufacturing method of exhaust gas purifying filter |
| JP2008119666A (en) * | 2006-11-15 | 2008-05-29 | Denso Corp | Manufacturing method of exhaust gas purifying filter |
| US20100080930A1 (en) * | 2007-03-28 | 2010-04-01 | Hitachi Metals, Ltd. | Method for producing ceramic honeycomb structure |
| US8551579B2 (en) * | 2007-03-28 | 2013-10-08 | Hitachi Metals, Ltd. | Method for producing ceramic honeycomb structure |
| JP2008290077A (en) * | 2008-08-14 | 2008-12-04 | Hitachi Metals Ltd | Ceramic honeycomb filter and method for manufacturing ceramic honeycomb filter |
| CN107718262A (en) * | 2017-08-29 | 2018-02-23 | 神华集团有限责任公司 | The manufacturing system of haydite |
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