JPH0685873B2 - Method of manufacturing honeycomb structure carrier comprising boria silica-alumina composition - Google Patents
Method of manufacturing honeycomb structure carrier comprising boria silica-alumina compositionInfo
- Publication number
- JPH0685873B2 JPH0685873B2 JP2417650A JP41765090A JPH0685873B2 JP H0685873 B2 JPH0685873 B2 JP H0685873B2 JP 2417650 A JP2417650 A JP 2417650A JP 41765090 A JP41765090 A JP 41765090A JP H0685873 B2 JPH0685873 B2 JP H0685873B2
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb structure
- silica
- weight
- boria
- alumina
- 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.)
- Expired - Lifetime
Links
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 title claims description 32
- 239000000203 mixture Substances 0.000 title claims description 18
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 239000011230 binding agent Substances 0.000 claims description 13
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims description 12
- 238000010304 firing Methods 0.000 claims description 9
- 239000000314 lubricant Substances 0.000 claims description 9
- 239000004927 clay Substances 0.000 claims description 7
- 238000000465 moulding Methods 0.000 claims description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 4
- 239000000843 powder Substances 0.000 description 14
- 239000003054 catalyst Substances 0.000 description 11
- 229910004298 SiO 2 Inorganic materials 0.000 description 8
- 239000007864 aqueous solution Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 239000002002 slurry Substances 0.000 description 5
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical compound [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 description 4
- 229940063655 aluminum stearate Drugs 0.000 description 4
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 4
- 229960002645 boric acid Drugs 0.000 description 4
- 235000010338 boric acid Nutrition 0.000 description 4
- 239000000969 carrier Substances 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
- 239000004115 Sodium Silicate Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 3
- 229910052911 sodium silicate Inorganic materials 0.000 description 3
- DIZPMCHEQGEION-UHFFFAOYSA-H aluminium sulfate (anhydrous) Chemical compound [Al+3].[Al+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O DIZPMCHEQGEION-UHFFFAOYSA-H 0.000 description 2
- ANBBXQWFNXMHLD-UHFFFAOYSA-N aluminum;sodium;oxygen(2-) Chemical compound [O-2].[O-2].[Na+].[Al+3] ANBBXQWFNXMHLD-UHFFFAOYSA-N 0.000 description 2
- 238000001354 calcination Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- HQKMJHAJHXVSDF-UHFFFAOYSA-L magnesium stearate Chemical compound [Mg+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O HQKMJHAJHXVSDF-UHFFFAOYSA-L 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 229910001388 sodium aluminate Inorganic materials 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 239000005995 Aluminium silicate Substances 0.000 description 1
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920002134 Carboxymethyl cellulose Polymers 0.000 description 1
- 239000004375 Dextrin Substances 0.000 description 1
- 229920001353 Dextrin Polymers 0.000 description 1
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical group OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 235000012211 aluminium silicate Nutrition 0.000 description 1
- 239000000440 bentonite Substances 0.000 description 1
- 229910000278 bentonite Inorganic materials 0.000 description 1
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical compound O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 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
- 239000000919 ceramic Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 229910052878 cordierite Inorganic materials 0.000 description 1
- 235000019425 dextrin Nutrition 0.000 description 1
- 235000014113 dietary fatty acids Nutrition 0.000 description 1
- 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 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000194 fatty acid Substances 0.000 description 1
- 229930195729 fatty acid Natural products 0.000 description 1
- 150000004665 fatty acids Chemical class 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000007062 hydrolysis Effects 0.000 description 1
- 238000006460 hydrolysis reaction Methods 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
- 235000019359 magnesium stearate Nutrition 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 235000019422 polyvinyl alcohol Nutrition 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- UFTFJSFQGQCHQW-UHFFFAOYSA-N triformin Chemical compound O=COCC(OC=O)COC=O UFTFJSFQGQCHQW-UHFFFAOYSA-N 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
Landscapes
- Compositions Of Oxide Ceramics (AREA)
- Press-Shaping Or Shaping Using Conveyers (AREA)
- Catalysts (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、触媒担体として優れた
性質を持つボリア−シリカ−アルミナ組成物よりなるハ
ニカム構造担体の製造方法に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing a honeycomb structure carrier composed of a boria-silica-alumina composition having excellent properties as a catalyst carrier.
【0002】[0002]
【従来の技術】ハニカム構造体の触媒担体は、多数の平
行した流通路を有するため、流体を流す場合に、圧力損
失が小さい上に単位体積当りの見掛表面積が大きい特性
があるので各種の廃ガス処理用触媒担体、燃焼用触媒担
体などとして広く用いられている。これらのハニカム構
造体は、ムライト、コージェライト、α−アルミナなど
よりなるセラミック材料をハニカム型に成型し、乾燥・
焼成して得られた基体表面に、γ−Al2O3をコーテ
ィングして触媒担体を得ていた。しかしながらγ−Al
2O3では、耐熱性が不十分であり耐熱性を改善するた
め、本出願人は、高比表面積を有し、かつ、耐熱性に優
れたボリア−シリカ−アルミナ複合酸化物を見出して提
案した(特願平2−8162号)。2. Description of the Related Art Since a catalyst carrier of a honeycomb structure has a large number of parallel flow passages, it has various characteristics such as a small pressure loss and a large apparent surface area per unit volume when flowing a fluid. It is widely used as a catalyst carrier for waste gas treatment, a catalyst carrier for combustion, and the like. These honeycomb structures are formed by molding a ceramic material, such as mullite, cordierite, or α-alumina, into a honeycomb shape, and
The substrate surface obtained by firing was coated with γ-Al 2 O 3 to obtain a catalyst carrier. However, γ-Al
2 O 3 has insufficient heat resistance and improves heat resistance. Therefore, the applicant has found and proposed a boria-silica-alumina composite oxide having a high specific surface area and excellent heat resistance. (Japanese Patent Application No. 2-8162).
【0003】[0003]
【発明が解決しようとする課題】しかしながら、このボ
リア−シリカ−アルミナ組成物をセラミックハニカム基
体にコーティングすることで優れた耐熱性を有する触媒
担体を得ることができるが、触媒担体の製造工程がセラ
ミックよりなるハニカム基体の製造と、ボリア−シリカ
−アルミナ組成物のコーティングとの2工程を要し、
又、組成物のコーティング量にも制限を生じるといった
問題がある。However, a catalyst carrier having excellent heat resistance can be obtained by coating a ceramic honeycomb substrate with this boria-silica-alumina composition. And a boria-silica-alumina composition coating process.
There is also a problem that the coating amount of the composition is limited.
【0004】本発明は、ボリア−シリカ−アルミナ組成
物で直接ハニカム構造体を作ることにより、1工程によ
って、高温度でも比表面積がきわめて大きく、耐熱性に
優れている触媒担体を製造する方法を提供することを目
的とするものである。The present invention provides a method for producing a catalyst carrier having a very large specific surface area even at a high temperature and excellent heat resistance by one step by directly forming a honeycomb structure from a boria-silica-alumina composition. It is intended to be provided.
【0005】[0005]
【課題を解決するための手段】本発明者は、前記問題を
解決し、前記目的を達成するために鋭意研究を重ねた結
果、特定組成のボリア−シリカ−アルミナ組成物を成型
−乾燥−焼成−粉砕し、各種配合物を添加してハニカム
型構造体として特定温度で焼成することによって目的を
達し得ることを見出して本発明を完成するに至った。す
なわち、本発明は、3〜10重量%のボリア(B
2O3)と4〜19重量%のシリカ(SiO2)と残部
がアルミナ(Al2O3)からなるボリア−シリカ−ア
ルミナ水和物を成型して、乾燥−焼成し、次いで破砕し
た後、有機質滑沢剤と有機質結合剤あるいは粘土と有機
質滑沢剤と有機質結合剤、及び、水とを添加して混練
し、ハニカム型構造体に押出し成型し、乾燥後、600
〜1400℃の温度で焼成するボリア−シリカ−アルミ
ナ組成物よりなるハニカム構造担体の製造方法である。As a result of intensive studies to solve the above problems and achieve the above object, the present inventor has formed a boria-silica-alumina composition having a specific composition by molding, drying and firing. -The present invention has been completed by finding that the object can be achieved by pulverizing, adding various compounds and firing as a honeycomb structure at a specific temperature. That is, the present invention uses 3 to 10% by weight of boria (B
2 O 3 ), 4-19 wt% silica (SiO 2 ) and the balance alumina (Al 2 O 3 ), after molding, drying-calcining and then crushing , An organic lubricant and an organic binder, or a clay, an organic lubricant and an organic binder, and water are added and kneaded, and the mixture is extruded into a honeycomb structure, dried, and then dried.
It is a method for manufacturing a honeycomb structure carrier made of a boria-silica-alumina composition, which is fired at a temperature of 1400C.
【0006】[0006]
【作用】本発明のボリア−シリカ−アルミナ組成物は、
たとえば、硫酸アルミニウム水溶液とアルミン酸ナトリ
ウム水溶液との加水分解により生成するアルミナ水和物
スラリーに、シリカ(SiO2)として4〜19重量%
の範囲になるようにケイ酸ナトリウム水溶液を添加して
得られるアルミナ−シリカ水和物スラリーを、ろ過−洗
浄して得たアルミナ−シリカ水和物ケーキに、ボリア
(B2O3)として3〜10重量%の範囲になるように
オルトホウ酸及び/又はオルトホウ酸水溶液を添加して
十分混合する。次に、得られた該混合物を加湿ジャケッ
ト付きニーダー中で加熱捏和し、所望の形状のダイスを
有する成型機により押出し成型した後、10〜40μの
範囲になるように破砕してボリア−シリカ−アルミナの
酸化物粉体として製造する。The boria-silica-alumina composition of the present invention is
For example, in an alumina hydrate slurry produced by hydrolysis of an aqueous solution of aluminum sulfate and an aqueous solution of sodium aluminate, 4 to 19% by weight as silica (SiO 2 ) is added.
The alumina-silica hydrate slurry obtained by adding an aqueous solution of sodium silicate so as to fall within the range of 3 is added to the alumina-silica hydrate cake obtained by filtration and washing to obtain 3 as boria (B 2 O 3 ). Add orthoboric acid and / or an aqueous solution of orthoboric acid so as to be in the range of 10 to 10% by weight and mix well. Next, the obtained mixture is kneaded by heating in a kneader with a humidifying jacket, extruded by a molding machine having a die having a desired shape, and then crushed to a range of 10 to 40 μ, and boria-silica. Manufactured as oxide powder of alumina.
【0007】本発明のボリア−シリカ−アルミナ組成物
において、B2O3を3〜10重量%SiO2を4〜1
9重量%の範囲とするのは、B2O3を3重量%未満及
び10重量%超、SiO2を4重量%未満及び19重量
%超えの組成物では、高温で比表面積がいちじるしく減
少し、耐熱性が低下するからである。In the boria-silica-alumina composition of the present invention, 3 to 10% by weight of B 2 O 3 and 4 to 1 of SiO 2 are added.
The range of 9 wt% is that the composition of B 2 O 3 less than 3 wt% and more than 10 wt% and SiO 2 less than 4 wt% and more than 19 wt% significantly decreases the specific surface area at high temperature. This is because the heat resistance is reduced.
【0008】本発明のボリア−シリカ−アルミナ酸化物
粉体において、ボリア−シリカ−アルミナ水和物を成型
し、80〜120℃で乾燥し、500〜1000℃好ま
しくは500〜800℃で通常2時間焼成する。焼成温
度が500℃未満では酸化物状態にならず、又、100
0℃を越えて焼成すると焼結がおこり、次工程の破砕が
困難になる。In the boria-silica-alumina oxide powder of the present invention, boria-silica-alumina hydrate is molded, dried at 80 to 120 ° C, and usually 500 to 1000 ° C, preferably 500 to 800 ° C. Bake for hours. If the firing temperature is less than 500 ° C, it will not be in an oxide state,
If the temperature exceeds 0 ° C., sintering will occur, making it difficult to crush in the next step.
【0009】次に、得られた焼成物は、平均粒径が10
〜40μの範囲になるように破砕することが望ましい。
平均粒径は、10μ未満でもよいが破砕工程に長時間を
必要とし、平均粒径が40μを超えると好ましいハニカ
ム成型体が得られない。Next, the obtained fired product has an average particle size of 10
It is desirable to crush it to a range of -40 μ.
The average particle size may be less than 10 μ, but the crushing process requires a long time, and if the average particle size exceeds 40 μ, a preferable honeycomb molded body cannot be obtained.
【0010】このようにして、ボリア−シリカ−アルミ
ナ酸化物粉体を得るのは、ボリア−シリカ−アルミナ水
和物を乾燥・焼成して得た該酸化物を用いて得るハニカ
ム構造体にはクラックの発生がおこり好ましいハニカム
構造体が得られないからである。In this manner, the boria-silica-alumina oxide powder is obtained in the honeycomb structure obtained by using the oxide obtained by drying and firing boria-silica-alumina hydrate. This is because cracks occur and a preferable honeycomb structure cannot be obtained.
【0011】このようにして得られたボリア−シリカ−
アルミナ酸化物粉体は、次に、25重量%以下の粘土と
有機質滑沢剤と有機質結合剤あるいは有機質滑沢剤と有
機質結合剤、及び、水とを添加して、十分混練し可塑化
した後、真空押出し成型機を用いて所望の形状のハニカ
ム金型を通して押出し、貫通孔を有するハニカム構造体
に成型する。次いで該成型体を温度70〜90℃、湿度
80〜95%の範囲で乾燥させ、600〜1400℃の
範囲で焼成して、ハニカム構造担体とする。Boria-silica-obtained in this way
Next, the alumina oxide powder was sufficiently kneaded and plasticized by adding 25% by weight or less of clay, an organic lubricant and an organic binder, or an organic lubricant and an organic binder, and water. After that, it is extruded through a honeycomb mold having a desired shape using a vacuum extrusion molding machine, and molded into a honeycomb structure having through holes. Next, the molded body is dried at a temperature of 70 to 90 ° C. and a humidity of 80 to 95% and fired at a temperature of 600 to 1400 ° C. to obtain a honeycomb structure carrier.
【0012】本発明のハニカム構造体を成型する際にバ
インダーとして添加する粘土としては、たとえば、カオ
リン、ベントナイト、セリサイトなどが挙げられ、添加
量を25重量%以下とすることが望ましく、25重量%
を超えて添加すると触媒担体としての比表面積が減少す
るので好ましくないものである。Examples of clay to be added as a binder when molding the honeycomb structure of the present invention include kaolin, bentonite, sericite, etc. The addition amount is preferably 25% by weight or less, and 25% by weight or less. %
If it is added over the range, the specific surface area as a catalyst carrier decreases, which is not preferable.
【0013】又、有機質滑沢剤としては、たとえば、ス
テアリン酸アルミニウム、ステアリン酸マグネシウム、
脂肪酸トリグリセリドなどが挙げられ、添加量は、5〜
15重量%の範囲とすることが望ましく、添加量が5重
量%未満では好ましいハニカム成型体が得られず、15
重量%を超えて添加してもよいがハニカム構造体を乾燥
・焼成する際に、有機質滑沢剤が燃焼し部分的に異常な
高温となり、ハニカム構造体の一部が崩壊することもあ
るので好ましくない。Examples of organic lubricants include aluminum stearate, magnesium stearate,
Fatty acid triglyceride etc. are mentioned, and the addition amount is 5
It is desirable to set it in the range of 15% by weight, and if the addition amount is less than 5% by weight, a preferable honeycomb molded body cannot be obtained.
Although it may be added in an amount exceeding the amount by weight, when the honeycomb structure is dried and fired, the organic lubricant may be burned to cause an abnormally high temperature and a part of the honeycomb structure may collapse. Not preferable.
【0014】さらに、有機質結合剤としては、たとえ
ば、ポリビニルアルコール、メチルセルロース、カルボ
キシメチルセルロース、デキストリンなどが挙げられ、
添加量は、4〜10重量%の範囲とすることが望まし
い。添加量が4重量%未満では可塑性が不十分であって
好ましいハニカム構造体を得ることができず、10重量
%を超えて添加してもよいが、ハニカム構造体を乾燥後
焼成する際に有機質結合剤が燃焼し部分的に異常な高温
となり、ハニカム構造体を崩壊することもあるので好ま
しくない。Further, examples of the organic binder include polyvinyl alcohol, methyl cellulose, carboxymethyl cellulose, dextrin and the like,
The addition amount is preferably in the range of 4 to 10% by weight. If the addition amount is less than 4% by weight, the plasticity is insufficient and a preferable honeycomb structure cannot be obtained, and it may be added in excess of 10% by weight, but when the honeycomb structure is dried and fired, the organic substance is not added. It is not preferable because the binder may be burned to cause an abnormally high temperature in part, and the honeycomb structure may be destroyed.
【0015】成型したハニカム構造体を、温度70〜9
0℃、湿度80〜95%の条件で乾燥するが、80%未
満の低湿度条件ではハニカム構造体の一部にクラックが
生じ、好ましいハニカム構造体が得られないものであ
り、ハニカム構造体の焼成温度を600〜1400℃の
範囲にするのは、600℃未満の温度では有機質滑沢
剤、有機質結合剤が分解せずに炭素分として残存してし
まい、1400℃を超える温度では、比表面積が小さく
なり触媒担体としての特性が失なわれるからである。The formed honeycomb structure was heated at a temperature of 70-9.
Although the honeycomb structure is dried at 0 ° C. and a humidity of 80 to 95%, under a low humidity condition of less than 80%, a crack occurs in a part of the honeycomb structure, and a preferable honeycomb structure cannot be obtained. The firing temperature is set in the range of 600 to 1400 ° C. because the organic lubricant and the organic binder remain as carbon without being decomposed at a temperature lower than 600 ° C. and a specific surface area at a temperature higher than 1400 ° C. Is reduced and the properties as a catalyst carrier are lost.
【0016】[0016]
【実施例】次に、本発明の実施例を述べる。 実施例 1 容量100lのかきまぜ機付きステンレス製反応槽に、
水49.5lをいれ、これにAl2O3として774g
を含む硫酸アルミニウム水溶液9540gを加え、70
℃まで加温し、保持し、かきまぜながらAl2O3とし
て1275gを含むアルミン酸ナトリウム水溶液を滴下
して、pH9.0のアルミナ水和物スラリーを得た。次
いで、該スラリーに、濃度30%の硝酸55gを加えて
pHを5.4とし、次いで、かきまぜながらSiO2と
して252gを含むケイ酸ナトリウム水溶液1800g
を滴下してpH8.5のアルミナ−シリカ水和物を得、
ろ過し、洗浄してアルミナ−シリカ水和物ケーキを得
た。このアルミナ−シリカ水和物ケーキ6760g(ア
ルミナ−シリカとして1014g)に、試薬特級のオル
トホウ酸94.4g(B2O3として53.4g)を加
え、ニーダー中で加熱捏和し、直径5.0mmのダイス
を有する押出し成型機にて成型し、110℃で15時間
乾燥し、電気炉で600℃で2時間焼成した後、破砕
し、平均粒径20μのB2O35.0重量%、SiO2
10.5重量%、Al2O384.6重量%のボリア−
シリカ−アルミナ酸化物粉体を得た。次いで、前記粉体
840gにステアリン酸アルミニウム150g(14重
量%)と、メチルセルロース50g( 5重量%)、及
び、水1050mlを加え十分可塑化する間まで混練し
た後、壁厚0.4mm、壁間距離2.0mm、セル形状
正方形のハニカム金型を通しハニカム構造体に成型し、
温度85℃、湿度90%の条件で48時間乾燥した後、
1200℃で3時間焼成し、ハニカム構造担体Aを得
た。EXAMPLES Next, examples of the present invention will be described. Example 1 In a stainless steel reaction tank with a stirrer having a capacity of 100 l,
49.5 l of water was added, and 774 g of Al 2 O 3 was added.
9540 g of an aluminum sulfate aqueous solution containing
A sodium aluminate aqueous solution containing 1275 g of Al 2 O 3 was added dropwise while being heated to and held at ℃ while stirring to obtain an alumina hydrate slurry having a pH of 9.0. Next, 55 g of nitric acid having a concentration of 30% was added to the slurry to adjust the pH to 5.4, and then 1800 g of an aqueous sodium silicate solution containing 252 g of SiO 2 while stirring.
Is added dropwise to obtain an alumina-silica hydrate having a pH of 8.5,
It was filtered and washed to obtain an alumina-silica hydrate cake. To this 6760 g of alumina-silica hydrate cake (1014 g as alumina-silica), 94.4 g of reagent grade orthoboric acid (53.4 g as B 2 O 3 ) was added and kneaded by heating in a kneader to give a diameter of 5. Molded by an extrusion molding machine having a 0 mm die, dried at 110 ° C. for 15 hours, baked at 600 ° C. for 2 hours in an electric furnace, and then crushed, 5.0 wt% of B 2 O 3 having an average particle size of 20 μm. , SiO 2
Boria containing 10.5 wt% and Al 2 O 3 84.6 wt%
A silica-alumina oxide powder was obtained. Then, 840 g of the powder was added with 150 g (14% by weight) of aluminum stearate, 50 g (5% by weight) of methylcellulose, and 1050 ml of water, and kneaded until sufficiently plasticized, and then the wall thickness was 0.4 mm and the wall thickness was 0.4 mm Molded into a honeycomb structure through a cell-shaped square honeycomb mold with a distance of 2.0 mm,
After drying at a temperature of 85 ° C and a humidity of 90% for 48 hours,
The honeycomb structure carrier A was obtained by firing at 1200 ° C. for 3 hours.
【0017】又、前記ハニカム構造体を前記同様乾燥し
た後、600℃、1000℃、1400℃の温度でそれ
ぞれ3時間焼成し、ハニカム構造担体B、C、Dを得
た。The honeycomb structure was dried in the same manner as described above and then fired at temperatures of 600 ° C., 1000 ° C. and 1400 ° C. for 3 hours to obtain honeycomb structure carriers B, C and D.
【0018】ハニカム構造担体A、B、C、Dの性状、
及び、窒素ガス吸着によるBEF法によって求めた比表
面積(m2/g)を表1に示す。1400℃で3時間焼
成しても比表面積は13m2/gであって、耐熱性に優
れた触媒担体として十分適用できることが明らかであ
る。 比較例 1 市販のγ−Al2O3を用いたこと以外は、実施例1と
ほぼ同様な方法でハニカム構造担体R−1を得た。得ら
れたハニカム構造担体の性状を表1に示す。実施例1で
得た本発明のハニカム構造担体に較べていちじるしく比
表面積が劣っていることが明らかである。又、1200
℃の温度で焼成することでα−Al2O3に転移し、耐
熱性触媒担体としての比表面積が失なわれていることも
明らかである。 実施例 2 Al2O3/SiO2として80/20重量%、95/
5重量%となるようにアルミナ水和物スラリーに添加す
るケイ酸ナトリウム水溶液の添加量を変化させた以外
は、実施例1のボリア−シリカ−アルミナ酸化物粉体を
得る製造方法と同様にして平均粒径20μのB2O
35.0重量%、SiO219.0重量%、Al2O3
76.0重量%と、B2O35.0重量%、SiO
24.8重量%、Al2O390.2重量%のボリア−
シリカ−アルミナ酸化物粉体を得た。次いで前記粉体を
用いて実施例1のハニカム構造体を得る方法と同様にし
て、ハニカム構造担体E、Fを得た。得られたハニカム
構造担体の性状を表1に示す。B2O3/SiO2/A
l2O3として、それぞれ、5.0/19.0/76.
0重量%、及び、5.0/4.8/90.2重量%のボ
リア−シリカ−アルミナ酸化物粉体を用いても高比表面
積を有し、耐熱性に優れたハニカム構造担体が得られる
ことが明らかである。 比較例 2 実施例1とほぼ同様にして得たアルミナ−シリカ水和物
ケーキに加えるオルトホウ酸の添加量をB2O3として
2.0重量%、15重量%と変化させた以外は、実施例
1と同様な方法でハニカム構造担体R−2を得た。その
性状を表1に示す。B2O3が30重量%未満あるいは
15重量%を超えると比表面積が小さくなり、耐熱性が
劣ることが明らかである。 実施例 3 実施例1と同様にして得たボリア−シリカ−アルミナ酸
化物粉体をハニカム構造体を生成する際に添加するバイ
ンダーの添加量をセリサイトを5重量%、ステアリン酸
アルミニウム10重量%、メチルセルロースを5重量%
加えたこと以外は実施例1と同様にしてハニカム構造担
体Gを得た。又、バインダーとしてのセリサイトを20
重量%加えた以外は前記同様にしてハニカム構造担体H
を得た。Properties of the honeycomb structure carriers A, B, C and D,
Table 1 shows the specific surface area (m 2 / g) obtained by the BEF method by nitrogen gas adsorption. Even if calcined at 1400 ° C. for 3 hours, the specific surface area is 13 m 2 / g, and it is clear that it can be sufficiently applied as a catalyst carrier having excellent heat resistance. Comparative Example 1 A honeycomb structure carrier R-1 was obtained in substantially the same manner as in Example 1 except that commercially available γ-Al 2 O 3 was used. Table 1 shows the properties of the obtained honeycomb structure carrier. It is clear that the specific surface area is significantly inferior to the honeycomb structure carrier of the present invention obtained in Example 1. Also 1200
It is also apparent that the calcination at a temperature of ° C transforms into α-Al 2 O 3 and loses the specific surface area as the heat-resistant catalyst carrier. Example 2 80/20 wt% as Al 2 O 3 / SiO 2 , 95 /
Except that the addition amount of the sodium silicate aqueous solution added to the alumina hydrate slurry was changed to be 5% by weight, the production method for obtaining the boria-silica-alumina oxide powder of Example 1 was repeated. B 2 O with an average particle size of 20μ
3 5.0% by weight, SiO 2 19.0% by weight, Al 2 O 3
76.0% by weight, B 2 O 3 5.0% by weight, SiO
2 4.8 wt%, Al 2 O 3 90.2% by weight of boria -
A silica-alumina oxide powder was obtained. Next, honeycomb structure carriers E and F were obtained in the same manner as in the method for obtaining the honeycomb structure of Example 1 using the powder. Table 1 shows the properties of the obtained honeycomb structure carrier. B 2 O 3 / SiO 2 / A
I 2 O 3 as 5.0 / 19.0 / 76.
Even if the boria-silica-alumina oxide powder of 0% by weight and 5.0 / 4.8 / 90.2% by weight is used, a honeycomb structure carrier having a high specific surface area and excellent heat resistance can be obtained. It is clear that Comparative Example 2 Except that the amount of orthoboric acid added to the alumina-silica hydrate cake obtained in substantially the same manner as in Example 1 was changed to 2.0% by weight and 15% by weight as B 2 O 3. A honeycomb structure carrier R-2 was obtained in the same manner as in Example 1. The properties are shown in Table 1. When the content of B 2 O 3 is less than 30% by weight or exceeds 15% by weight, it is clear that the specific surface area is small and the heat resistance is poor. Example 3 The amount of the binder added when the boria-silica-alumina oxide powder obtained in the same manner as in Example 1 was added to the honeycomb structure was 5% by weight of sericite and 10% by weight of aluminum stearate. , Methylcellulose 5% by weight
A honeycomb structure carrier G was obtained in the same manner as in Example 1 except for the addition. In addition, 20 Sericite as a binder
Honeycomb structure carrier H in the same manner as above except that the weight% was added.
Got
【0019】得られたハニカム構造担体G及びHの性状
を表1に示す。粘土の添加量が5〜20重量%の範囲で
あれば高比表面積を有し、耐熱性に優れたハニカム構造
担体が得られることが明らかである。 比較例 3 実施例1とほぼ同様な方法で得たボリア−シリカ−アル
ミナ酸化物粉体に添加するセリサイトを30重量%、ス
テアリン酸アルミニウム10重量%、メチルセルロース
を5重量%加えたこと以外は、実施例1と同様にしてハ
ニカム構造担体R−4を得た。その性状を表1に示す。
粘土の添加量が30重量%になると得られるハニカム構
造担体の比表面積が減少し、耐熱性が劣ることが明らか
である。Table 1 shows the properties of the obtained honeycomb structure carriers G and H. It is clear that when the amount of clay added is in the range of 5 to 20% by weight, a honeycomb structure carrier having a high specific surface area and excellent heat resistance can be obtained. Comparative Example 3 Except that 30% by weight of sericite, 10% by weight of aluminum stearate, and 5% by weight of methylcellulose were added to the boria-silica-alumina oxide powder obtained in the same manner as in Example 1. A honeycomb structure carrier R-4 was obtained in the same manner as in Example 1. The properties are shown in Table 1.
It is clear that when the amount of clay added is 30% by weight, the specific surface area of the resulting honeycomb structure carrier is reduced and the heat resistance is poor.
【0020】[0020]
【表1】[Table 1]
【0021】[0021]
【発明の効果】本発明は、特定組成範囲のボリア−シリ
カ−アルミナ酸化物粉体を得、これにバインダーを添加
して得たハニカム構造体を特定温度範囲で焼成するもの
であるから、1工程で優れた耐熱性を有する高比表面積
のハニカム構造担体を得ることができ、顕著な効果が認
められる。The present invention is intended to obtain a boria-silica-alumina oxide powder having a specific composition range, and to add a binder to the powder, and to fire the honeycomb structure in a specific temperature range. A honeycomb structure carrier having a high specific surface area having excellent heat resistance can be obtained in the process, and a remarkable effect is recognized.
【表1】 [Table 1]
【表1】 [Table 1]
Claims (2)
4〜19重量%のシリカ(SiO2)と残部がアルミナ
(Al2O3)からなるボリア−シリカ−アルミナ水和
物を成型して、乾燥・焼成し、次いで破砕した後、有機
質滑沢剤と有機質結合剤あるいは粘土と有機質滑沢剤と
有機質結合剤、及び、水とを添加して混練し、ハニカム
型構造体に押出し成型し、乾燥後、600〜1400℃
の温度で焼成することを特徴とするボリア−シリカ−ア
ルミナ組成物よりなるハニカム構造担体の製造方法。1. A boria-silica-alumina hydrate comprising 3 to 10% by weight of boria (B 2 O 3 ), 4 to 19% by weight of silica (SiO 2 ) and the balance alumina (Al 2 O 3 ). After molding, drying and firing, and then crushing, an organic lubricant and an organic binder or clay, an organic lubricant and an organic binder, and water are added and kneaded to form a honeycomb structure. Extruded and dried, then 600-1400 ℃
A method for producing a honeycomb structure carrier comprising a boria-silica-alumina composition, which comprises firing at a temperature of.
とを特徴とする請求項1のボリア−シリカ−アルミナ組
成物よりなるハニカム構造担体の製造方法。2. The method for producing a honeycomb structure carrier comprising the boria-silica-alumina composition according to claim 1, wherein the amount of clay added is 25% by weight or less.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2417650A JPH0685873B2 (en) | 1990-12-28 | 1990-12-28 | Method of manufacturing honeycomb structure carrier comprising boria silica-alumina composition |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2417650A JPH0685873B2 (en) | 1990-12-28 | 1990-12-28 | Method of manufacturing honeycomb structure carrier comprising boria silica-alumina composition |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH04250849A JPH04250849A (en) | 1992-09-07 |
JPH0685873B2 true JPH0685873B2 (en) | 1994-11-02 |
Family
ID=18525725
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Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2417650A Expired - Lifetime JPH0685873B2 (en) | 1990-12-28 | 1990-12-28 | Method of manufacturing honeycomb structure carrier comprising boria silica-alumina composition |
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JP (1) | JPH0685873B2 (en) |
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JP4161652B2 (en) * | 2001-10-10 | 2008-10-08 | 株式会社デンソー | Method for manufacturing ceramic structure and method for manufacturing ceramic honeycomb structure |
-
1990
- 1990-12-28 JP JP2417650A patent/JPH0685873B2/en not_active Expired - Lifetime
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