JPH04130069A - Manufacture of honeycomb-type ceramic structure - Google Patents
Manufacture of honeycomb-type ceramic structureInfo
- Publication number
- JPH04130069A JPH04130069A JP2250641A JP25064190A JPH04130069A JP H04130069 A JPH04130069 A JP H04130069A JP 2250641 A JP2250641 A JP 2250641A JP 25064190 A JP25064190 A JP 25064190A JP H04130069 A JPH04130069 A JP H04130069A
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb
- ceramic
- powder
- ceramic structure
- structures
- 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 63
- 238000004519 manufacturing process Methods 0.000 title claims description 17
- 239000000843 powder Substances 0.000 claims abstract description 29
- 239000000203 mixture Substances 0.000 claims abstract description 14
- 229910000502 Li-aluminosilicate Inorganic materials 0.000 claims abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 4
- 238000010304 firing Methods 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 5
- 239000003054 catalyst Substances 0.000 abstract description 14
- 238000007084 catalytic combustion reaction Methods 0.000 abstract description 13
- 229910010293 ceramic material Inorganic materials 0.000 abstract description 3
- 238000001125 extrusion Methods 0.000 abstract description 2
- 239000010802 sludge Substances 0.000 abstract 2
- 238000001354 calcination Methods 0.000 abstract 1
- 238000012360 testing method Methods 0.000 description 10
- 239000002245 particle Substances 0.000 description 6
- 238000000465 moulding Methods 0.000 description 5
- 230000005856 abnormality Effects 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 239000002002 slurry Substances 0.000 description 4
- 239000004372 Polyvinyl alcohol Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 229910052878 cordierite Inorganic materials 0.000 description 3
- 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 3
- 230000000694 effects Effects 0.000 description 3
- 229910000174 eucryptite Inorganic materials 0.000 description 3
- 239000005350 fused silica glass Substances 0.000 description 3
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 3
- 229920002451 polyvinyl alcohol Polymers 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- CNLWCVNCHLKFHK-UHFFFAOYSA-N aluminum;lithium;dioxido(oxo)silane Chemical compound [Li+].[Al+3].[O-][Si]([O-])=O.[O-][Si]([O-])=O CNLWCVNCHLKFHK-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000000969 carrier Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- NJLLQSBAHIKGKF-UHFFFAOYSA-N dipotassium dioxido(oxo)titanium Chemical compound [K+].[K+].[O-][Ti]([O-])=O NJLLQSBAHIKGKF-UHFFFAOYSA-N 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000011812 mixed powder Substances 0.000 description 2
- 229910052573 porcelain Inorganic materials 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 229910052642 spodumene Inorganic materials 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241001385733 Aesculus indica Species 0.000 description 1
- 241000219112 Cucumis Species 0.000 description 1
- 235000015510 Cucumis melo subsp melo Nutrition 0.000 description 1
- FJJCIZWZNKZHII-UHFFFAOYSA-N [4,6-bis(cyanoamino)-1,3,5-triazin-2-yl]cyanamide Chemical compound N#CNC1=NC(NC#N)=NC(NC#N)=N1 FJJCIZWZNKZHII-UHFFFAOYSA-N 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000001866 hydroxypropyl methyl cellulose Substances 0.000 description 1
- 229920003088 hydroxypropyl methyl cellulose Polymers 0.000 description 1
- 235000010979 hydroxypropyl methyl cellulose Nutrition 0.000 description 1
- 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 1
- 238000002156 mixing Methods 0.000 description 1
- 239000011505 plaster Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 210000002784 stomach Anatomy 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Abstract
Description
【発明の詳細な説明】
産業上の利用分野
本発明(よ 触媒燃焼用触媒体の担体として用いる複合
化した大面積のハニカム状セラミックス構造体の製造方
法に関する。DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a method for manufacturing a composite large-area honeycomb ceramic structure used as a carrier for a catalyst for catalytic combustion.
従来の技術
従来か叙 触媒燃焼用触媒体の担体としては燃料気体が
抵抗なく通過するとともに効率よく触媒と接触して反応
するための構造体としてハニカム状セラミックス構造体
が広く用いられてきている。BACKGROUND OF THE INVENTION Honeycomb-shaped ceramic structures have been widely used as carriers for catalyst bodies for catalytic combustion, as they allow fuel gas to pass therethrough without resistance and efficiently contact and react with the catalyst.
その製造方法は構造体の目的とする形状、大きさに応じ
てプレス成形用ダイスの形状寸法を選定し原材料を調製
し プレス装置を用いて押出成形の後、乾燥 焼成して
ハニカム状セラミックス構造体としてい九 したがって
、たとえば現在使用している成形ダイスと異なる大きさ
、あるいは異なる形状の構造体が必要になった場合には
新たにブレス成形用ダイスを作り換えなければならなか
つ池 一般にプレス成形用ダイスは非常に高価であって
同一製造ロットの数量が極めて大きい場合以外は製造コ
スト増大の大きな要因となってい旭また大面積の完全な
ハニカム状セラミックス構造体は必要であっても製造は
容易でなく、複数の小面積ハニカム状セラミックス構造
体をガスシール部材等を介しながら連結させて使用して
い九発明が解決しようとする課題
上記従来の製造方法で(よ 大面積のハニカム状セラミ
ックス構造体が必要な場合には そのための寸法の大き
いプレス成形用ダイスを作る必要があり、また場合によ
ってはあまりに成形ダイスが大きくなりすぎ、現状の製
造装置では目的とする構造体を製造することは不可能な
ことがあっ九また 従来の小面積ハニカム状セラミック
ス構造体を連結させて使用する方法で(よ 大面積のハ
ニカム状セラミックス構造体を高い歩留まりで生産する
のは困難であった
本発明は上記課題を解決するもので、大面積の大型ハニ
カム状セラミックス構造体を容易に製造する製造方法を
提供することを目的としている。The manufacturing method involves selecting the shape and dimensions of a press-forming die according to the desired shape and size of the structure, preparing raw materials, extruding them using a press machine, drying and firing them, and producing a honeycomb-shaped ceramic structure. Therefore, for example, if you need a structure with a different size or shape than the molding die you are currently using, you will have to make a new press molding die. Dies are very expensive and are a major factor in increasing production costs unless the quantity of the same production lot is extremely large.Also, even if a large-area complete honeycomb ceramic structure is necessary, it is not easy to produce. Problems to be Solved by the Invention In the conventional manufacturing method described above, a plurality of small-area honeycomb-like ceramic structures are connected via a gas seal member, etc. If necessary, it is necessary to make a press molding die with large dimensions, and in some cases, the molding die becomes so large that it is impossible to manufacture the desired structure with current manufacturing equipment. In addition, it was difficult to produce large-area honeycomb-like ceramic structures with a high yield using the conventional method of connecting and using small-area honeycomb-like ceramic structures.The present invention solves the above problems. The object of the present invention is to provide a manufacturing method for easily manufacturing a large honeycomb-shaped ceramic structure with a large area.
課題を解決するための手段
本発明は上記目的を達成するために 複数のハニカム状
セラミックス構造体の端面部同士を同じ組成からなるセ
ラミックス粉末にリチウムアルミノシリケート粉末を添
加した材料で接合した後、焼成することによって、複数
のハニカム状セラミックス構造体を融着させ、複合41
. 大型化するようにしたものである。Means for Solving the Problems The present invention achieves the above objects by bonding the end faces of a plurality of honeycomb-shaped ceramic structures with a material made by adding lithium aluminosilicate powder to ceramic powder having the same composition, and then firing. By doing so, a plurality of honeycomb-shaped ceramic structures are fused and a composite 41
.. It was designed to be larger.
作用
触媒燃焼装置で触媒担体用ハニカム状セラミックス構造
体として広く用いられている熱膨張係数が小さなコーデ
ィエライト組成あるいは5iO2−A 120 s−T
i O2−K 20系のセラミックス材料と同じ組成
のセラミックス粉末を骨材とし リチウムアルミノシリ
ケートをバインダーとして用いてハニカム状セラミック
ス構造体の端面同志を接着しているので接合部分が他の
部分とほぼ同じ組成で、熱膨張係数の実効的な差が小さ
く接合部における熱応力による破損を防止することがで
きる。Cordierite composition or 5iO2-A 120 s-T with a small coefficient of thermal expansion is widely used as a honeycomb-shaped ceramic structure for a catalyst carrier in catalytic combustion devices.
i O2-K The end faces of the honeycomb-shaped ceramic structure are bonded together using ceramic powder with the same composition as the O2-K 20 series ceramic material as an aggregate and lithium aluminosilicate as a binder, so the joints are almost the same as other parts. Due to the composition, the effective difference in coefficient of thermal expansion is small and damage due to thermal stress at the joint can be prevented.
したがって急へ 急冷時にも破壊されることなくいわゆ
るスポーリング性にも優れ 機械的強度も実用状十分な
ハニカム状セラミッス構造体が得られる。また新たに大
型のプレス成形ダイスを製作することなく接合するのみ
で作成できるから製造も容易で製造コストを低減するこ
とができる。Therefore, it is possible to obtain a honeycomb-shaped ceramic structure that does not break even during rapid cooling, has excellent so-called spalling properties, and has sufficient mechanical strength for practical use. Further, since it can be created by simply joining without creating a new large press molding die, manufacturing is easy and manufacturing costs can be reduced.
実施例
以下、本発明の一実施例について第1図〜第2(a)、
(b)を参照しながら説明する。EXAMPLE Below, an example of the present invention is shown in FIGS. 1 to 2(a),
This will be explained with reference to (b).
実施例1
再水和性アルミナ10重置皿 溶融シリカ85重量服
チタン酸カリウム5重量部を使用して、ハニカム状に押
出成形後、 1200℃で1h焼成L 150x15
0mm、 厚み10mm、 セル密度300セル/
in’(セルピッチ1 、5 m @ リブIFf0
.20mm)のハニカム状セラミックス構造体4枚を作
成し總 その後、前記焼成後のセラミックスと同じ組成
粉末(粒度100メツシユ以下)を調製し 前記粉末9
8重量部とリチウムアルミノシリケート粉末(ユークリ
プタイト粉末)(粒度100メツシユ以下)2重量部を
混合し その後少量のポリビニールアルコール(PVA
)を添加、した水溶液で、前記混合粉末を泥漿とし 接
合すべき各ハニカム状セラミックス構造体の側端面部の
2カ所に前記泥漿を塗布 接合 乾燥させた後、 11
00℃で1h焼成し ハニカム状セラミックス構造体の
側端面部同士を融着させた この時の焼成温度はセラミ
ックス材料粉末の焼結温度よりも低く、 リチウムアル
ミノシリケートの軟化点よりも高く設定することが好ま
しl、% そうすることにより、セラミックス粉末を
膏剤とし リチウムアルミノシリケートはバインダーと
して作用させながらハニカム状セラミックス構造体の端
面部同士を接着させることができる。Example 1 Rehydratable alumina 10-layer plate Fused silica 85 weight suit
Using 5 parts by weight of potassium titanate, extrusion molded into a honeycomb shape and fired at 1200°C for 1 hour L 150x15
0mm, thickness 10mm, cell density 300 cells/
in' (cell pitch 1, 5 m @ rib IFf0
.. After that, a powder with the same composition as the ceramic after firing (particle size of 100 mesh or less) was prepared.
Mix 8 parts by weight of lithium aluminosilicate powder (eucryptite powder) (particle size 100 mesh or less) with 2 parts by weight, and then add a small amount of polyvinyl alcohol (PVA).
) was added to make the mixed powder a slurry, and the slurry was applied to two places on the side end face of each honeycomb-shaped ceramic structure to be bonded. Bonding After drying, 11
The side end surfaces of the honeycomb ceramic structure were fused together by firing at 00°C for 1 hour.The firing temperature at this time should be set lower than the sintering temperature of the ceramic material powder and higher than the softening point of the lithium aluminosilicate. It is preferable that the ceramic powder be used as a plaster and the lithium aluminosilicate be used as a binder to bond the end surfaces of the honeycomb ceramic structure to each other.
その結果 第1図に示すように4枚の小型ハニカム状セ
ラミックス構造体1は一体化L 300x300mm
のハニカム状セラミックス構造体2を得ることができた
上記ハニカム状セラミックス構造体2にAlaOa・C
eO2(A l 2Qs: C602=10:3重量比
)からなるウォッシュコートを120gコーティングし
白金族触媒を約2g担持味 触媒燃焼用触媒体3とし
な
この触媒燃焼用触媒体3を実使用条件下でテストするた
め第2図(a)および(b)に示すような6000kc
al/h用触媒燃焼装置を作製し九 これらの図におい
て、 4は小型ハニカム状セラミックス構造体の接合部
5は枠体 6は燃料タン久 7は送風ファン、 8は
燃料用ポンプ、 9は予混合室 10は補助炎μ 11
は点火電機12は前面ガラ入 13は排気経路である。As a result, as shown in FIG.
The honeycomb-shaped ceramic structure 2 was obtained by adding AlaOa.C to the honeycomb-shaped ceramic structure 2.
The catalyst body 3 for catalytic combustion and the catalyst body 3 for catalytic combustion of shinako were coated with 120 g of wash coat consisting of eO2 (A l 2 Qs: C602 = 10:3 weight ratio) and supported about 2 g of platinum group catalyst under actual usage conditions. 6000kc as shown in Figure 2(a) and (b) for testing.
In these figures, 4 is the joint of the small honeycomb ceramic structure, 5 is the frame, 6 is the fuel tank, 7 is the blower fan, 8 is the fuel pump, and 9 is the pre-heater. Mixing chamber 10 is auxiliary flame μ 11
13 is an exhaust path.
得られたハニカム状セラミックス構造体2の評価は下記
のような燃焼条件テストと転倒テストで行っ九 まず、
燃焼条件テストは触媒燃焼装置の触媒体の燃料上流面側
を約800℃に設定L1時間燃焼後、消火L−30分間
冷却する工程を1サイクルとLA 5000サイクルま
で行っ九上記テストの結果 ハニカム状セラミックス構
造体の接合部分に異常はなかっ九
まな 転倒テストは上記触媒燃焼装置の底部を滑らない
ようにし 上部中央から力を加え 前後に各5回転倒さ
せん
その結果においてもハニカム状セラミックス構造体平板
の接合部分に異常はなかつれ
本実施例ではりチウムアルミノシリケートとしてユーク
リプタイトを使用しため(スポジュメンを使用しても同
様の効果が得られも
実施例2
実施例1と同様な小型ハニカム状セラミックス構造体2
を4枚作成した後、同じ組成粉末(粒度100メツシユ
以下)を調製し 前記粉末98重量部とりチウムアルミ
ノシリケート粉末(ユークリプタイト粉末)(粒度10
0メツシユ以下)2重量部とヒドロキシプロピルメチル
セルロース2重量部と所定の水とを混合り、 150
x 10mm、 厚み1mmのシート状に成形し九
その後前記シート成形物の表面を少量の水で湿らせた
後、各ハニカム状セラミックス構造体の側端面2カ所を
前記シート成形物を介在させなが叙 接合、乾燥させた
後、 1100℃で1時間焼成し ハニカム状セラミッ
クス構造体側端面部同志を融着させ九 その結果 4枚
の小型ハニカム状セラミックス構造体1は一体化L
300X300mmのハニカム状セラミックス構造体2
を得ることができへ
上記ハニカム状セラミックス構造体2にA120a・C
e0e (A1201: Ce02=10: 3重量
比)からなるウォッシュコートを120gコーティング
し 白金族触媒を約2g担持し 触媒燃焼用触媒体3と
し九
本実施例の触媒燃焼用触媒体3についても実施例1と同
様な燃焼条件テストと転倒テストを行った
その結果 ハニカム状セラミックス構造体平板の接合
部分に異常はなかっな
実施例1、2で使用した再水和性アルミナと溶融シリカ
とチタン酸カリウムからなるセラミックスは5iOp
80〜92wt% Al2O35〜18wt%、Ti
1t 2〜6wt% K2O0゜4〜1.5wt%
の組成が好ましu% このセラミックスは1000℃
以上から徐々に焼結を開始し次第にアルミナとチタン酸
カリウムとが溶融シリカ粒界で固溶相となり、 120
0℃では優れた機械的強度を有するようになる。また
用いた溶融シリカの低熱膨張特性も兼ね備えたセラミッ
クスとなる。The obtained honeycomb-shaped ceramic structure 2 was evaluated by the following combustion condition test and fall test.9 First,
The combustion condition test was carried out by setting the fuel upstream side of the catalyst body of the catalytic combustion device at approximately 800°C. After burning for L1 hour, extinguishing L and cooling for 30 minutes for 1 cycle and LA 5000 cycles. 9. The results of the above test were honeycomb-shaped. There were no abnormalities in the joints of the ceramic structure.In the fall test, the bottom of the catalytic combustion device was made to avoid slipping, force was applied from the center of the top, and the device was caused to fall back and forth five times each. There was no abnormality in the joint part, and since eucryptite was used as the lithium aluminosilicate in this example (the same effect could be obtained even if spodumene was used). Structure 2
After preparing four sheets of powder, prepare a powder with the same composition (particle size of 100 mesh or less), take 98 parts by weight of the powder, and add lithium aluminosilicate powder (eucryptite powder) (particle size of 10 mesh or less).
0 mesh or less), 2 parts by weight of hydroxypropyl methyl cellulose, and the specified amount of water, and mix 150
After that, the surface of the sheet molded product was moistened with a small amount of water, and then the two side end faces of each honeycomb-shaped ceramic structure were shaped into a sheet with the sheet molded product having a size of 10 mm x 10 mm and a thickness of 1 mm. After joining and drying, it was fired at 1100°C for 1 hour to fuse the side end surfaces of the honeycomb-shaped ceramic structures to each other.As a result, the four small honeycomb-shaped ceramic structures 1 were integrated into one L.
300x300mm honeycomb ceramic structure 2
A120a/C can be obtained in the honeycomb-shaped ceramic structure 2.
A catalytic combustion catalyst body 3 was prepared by coating 120 g of a wash coat consisting of e0e (A1201: Ce02 = 10: 3 weight ratio) and supporting approximately 2 g of a platinum group catalyst. The same combustion condition test and fall test as in Example 1 were carried out.The results showed that there was no abnormality in the joints of the flat plates of the honeycomb-shaped ceramic structure. Naru Ceramics is 5iOp
80-92wt% Al2O35-18wt%, Ti
1t 2~6wt% K2O0゜4~1.5wt%
The composition of this ceramic is preferably 1000℃
From the above, sintering begins gradually, and alumina and potassium titanate gradually become a solid solution phase at the fused silica grain boundaries, resulting in 120
At 0°C, it has excellent mechanical strength. Also
The result is a ceramic that also has the low thermal expansion properties of the fused silica used.
実施例3
150X150m瓜 厚さIDmm、 セル密度30
0セル/1n2(セルピッチ1.5m凪 リブ厚0.2
0mm)の小型コーディエライト磁器ハニカム状セラミ
ックス構造体1を4枚作成し その後、コーディエライ
ト磁器組成からなる粉末(粒度100メツシユ以下)を
調製し 前記コーディエライト粉末98重量部とりチウ
ムアルミノシリケート粉末(スポジュメン粉末)(粒度
100メツシユ以下)2重量部を混合し その後少量の
PVAを添加させた水溶液で、前記混合粉末を泥漿とし
小型ハニカム状セラミックス構造体1の側端面部の2
カ所に前記泥漿を塗布 接合、乾燥させた後、 110
0℃で1時間焼成し 小型ハニカム状セラミックス構造
体1の側端面部同志を融着させん その結果 4枚の小
型ハニカム状セラミックス構造体1は一体化L 30
0x300mmのハニカム状セラミックス構造体2を得
ることができた
上記ハニカム状セラミックス構造体2にAl2O3・C
eo2(A I2O3: Ce02=10: 3重量
比)からなるウォッシュコートを120gコーティング
し 白金族触媒を約2g担持し 触媒燃焼用触媒体3と
した
本実施例の触媒燃焼用触媒体3についても実施例1と同
様な燃焼条件テストと転倒テストを行った
その結果 ハニカム状セラミックス構造体2の接合部分
に異常はなかっへ
ここで、セラミックス粉末に対するリチウムアルミノシ
リケート粉末の添加量は0.5〜3wt%であることが
好まししも 添加量が0 、5 wt%未満では充分な
接着強度が得られず、また3wt%を超えると接合部分
の耐熱性が悪くなる。Example 3 150x150m melon, thickness IDmm, cell density 30
0 cell/1n2 (cell pitch 1.5m, rib thickness 0.2
0 mm) small-sized cordierite porcelain honeycomb-shaped ceramic structures 1 were prepared, and then a powder (particle size of 100 mesh or less) having a cordierite porcelain composition was prepared. Mix 2 parts by weight of powder (spodumene powder) (particle size: 100 mesh or less), and then use an aqueous solution to which a small amount of PVA is added to turn the mixed powder into a slurry.
After applying the slurry to the parts, bonding and drying, 110
The side end surfaces of the small honeycomb ceramic structures 1 are fused together by firing at 0°C for 1 hour.As a result, the four small honeycomb ceramic structures 1 are integrated L30
A honeycomb-shaped ceramic structure 2 of 0x300 mm was obtained.Al2O3.C was added to the honeycomb-shaped ceramic structure 2.
The catalyst body 3 for catalytic combustion of this example was also coated with 120 g of wash coat consisting of eo2 (A I2O3: Ce02 = 10: 3 weight ratio) and supported about 2 g of platinum group catalyst. The same combustion condition test and fall test as in Example 1 were conducted, and the results showed that there were no abnormalities in the joints of the honeycomb-shaped ceramic structure 2.Here, the amount of lithium aluminosilicate powder added to the ceramic powder was 0.5 to 3 wt%. However, if the amount added is less than 0.5 wt%, sufficient adhesive strength will not be obtained, and if it exceeds 3 wt%, the heat resistance of the bonded portion will deteriorate.
なお本発明の製造方法は 触媒燃焼用触媒体の担体とし
て使用される構造体のみならずその他のプレス成形が困
難な大型のハニカム状セラミックス構造体の製造方法と
しても同様な効果があることは言うまでもない。It goes without saying that the manufacturing method of the present invention has similar effects not only on structures used as carriers for catalytic combustion catalysts, but also as a method for manufacturing other large honeycomb-shaped ceramic structures that are difficult to press-form. stomach.
発明の効果
以上の実施例から明かなように本発明によれ(よ比較的
小型のハニカム状セラミックス構造体を連結して容易に
複合化 大型化することができ、接合部における接着強
度、耐衝撃性、耐熱性も良好で優れた大型のハニカム状
セラミックス構造体を容易に製造することができる。Effects of the Invention As is clear from the above embodiments, the present invention (relatively small honeycomb-shaped ceramic structures can be easily connected to form a composite structure and can be made larger), and the adhesive strength and impact resistance at the joints can be increased. It is possible to easily produce a large honeycomb-shaped ceramic structure with good properties and heat resistance.
第1図は本発明の一実施例におけるハニカム状セラミッ
クス構造体の斜視@ 第2図(a)はハニカム状セラミ
ックス構造体を評価するための触媒燃焼装置の正面医
第2図(b)は同触媒燃焼装置の一部断面図である。Figure 1 is a perspective view of a honeycomb ceramic structure according to an embodiment of the present invention; Figure 2 (a) is a front view of a catalytic combustion device for evaluating a honeycomb ceramic structure.
FIG. 2(b) is a partial sectional view of the catalytic combustion device.
Claims (3)
士を前記構造体と同じ組成からなるセラミックス粉末に
リチウムアルミノシリケート粉末を添加した材料で接合
した後、焼成し、融着させることを特徴とするハニカム
状セラミックス構造体の製造方法。(1) The end surfaces of a plurality of honeycomb-shaped ceramic structures are bonded together using a material obtained by adding lithium aluminosilicate powder to ceramic powder having the same composition as the structure, and then fired and fused. A method for manufacturing a honeycomb ceramic structure.
るセラミックス粉末にリチウムアルミノシリケート粉末
を添加した材料でシート状部材を成形し、前記構造体の
複数個を前記シート状部材を介在させて接合した後、焼
成し、前記構造体の端面部同士を融着させることを特徴
とするハニカム状セラミックス構造体の製造方法。(2) After forming a sheet-like member using a material in which lithium aluminosilicate powder is added to ceramic powder having the same composition as that of the honeycomb-shaped ceramic structure, and joining a plurality of the structures with the sheet-like member interposed therebetween; . A method for manufacturing a honeycomb-shaped ceramic structure, which comprises firing and fusing the end surfaces of the structure.
ミックス粉末に対して0.5〜3wt%であることを特
徴とする請求項1または請求項2記載のハニカム状セラ
ミックス構造体の製造方法。(3) The method for manufacturing a honeycomb-shaped ceramic structure according to claim 1 or 2, wherein the amount of lithium aluminosilicate powder added is 0.5 to 3 wt% based on the ceramic powder.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2250641A JPH04130069A (en) | 1990-09-19 | 1990-09-19 | Manufacture of honeycomb-type ceramic structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2250641A JPH04130069A (en) | 1990-09-19 | 1990-09-19 | Manufacture of honeycomb-type ceramic structure |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04130069A true JPH04130069A (en) | 1992-05-01 |
Family
ID=17210884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2250641A Pending JPH04130069A (en) | 1990-09-19 | 1990-09-19 | Manufacture of honeycomb-type ceramic structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04130069A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001053232A1 (en) * | 2000-01-24 | 2001-07-26 | Ngk Insulators, Ltd. | Ceramic structure |
WO2001093984A1 (en) * | 2000-06-05 | 2001-12-13 | Ngk Insulators,Ltd. | Honeycomb structure and honeycomb filter, and method of producing them |
EP1171224A1 (en) * | 1999-02-22 | 2002-01-16 | Ceramem Corporation | Cross-flow filtration device with filtrate conduit network and method of making same |
WO2003031371A1 (en) * | 2001-10-02 | 2003-04-17 | Ngk Insulators, Ltd. | Honeycomb structural body and method of manufacturing the structural body |
US7024916B2 (en) | 2001-06-04 | 2006-04-11 | Dowa Mining Co., Ltd. | Vacuum heat treatment furnace and method of and apparatus for measuring carbon concentration in atmosphere having reduced pressure. |
JP2015174798A (en) * | 2014-03-14 | 2015-10-05 | 日本碍子株式会社 | plugged honeycomb structure |
JP2015182926A (en) * | 2014-03-25 | 2015-10-22 | 日本碍子株式会社 | Method of producing honeycomb structure |
-
1990
- 1990-09-19 JP JP2250641A patent/JPH04130069A/en active Pending
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1171224A1 (en) * | 1999-02-22 | 2002-01-16 | Ceramem Corporation | Cross-flow filtration device with filtrate conduit network and method of making same |
EP1171224A4 (en) * | 1999-02-22 | 2004-04-07 | Ceramem Corp | Cross-flow filtration device with filtrate conduit network and method of making same |
WO2001053232A1 (en) * | 2000-01-24 | 2001-07-26 | Ngk Insulators, Ltd. | Ceramic structure |
US6395370B1 (en) | 2000-01-24 | 2002-05-28 | Ngk Insulators, Ltd. | Ceramic structure |
WO2001093984A1 (en) * | 2000-06-05 | 2001-12-13 | Ngk Insulators,Ltd. | Honeycomb structure and honeycomb filter, and method of producing them |
US7294316B2 (en) | 2000-06-05 | 2007-11-13 | Ngk Insulators, Ltd | Honeycomb structure, honeycomb filter and processes for the production thereof |
US7024916B2 (en) | 2001-06-04 | 2006-04-11 | Dowa Mining Co., Ltd. | Vacuum heat treatment furnace and method of and apparatus for measuring carbon concentration in atmosphere having reduced pressure. |
WO2003031371A1 (en) * | 2001-10-02 | 2003-04-17 | Ngk Insulators, Ltd. | Honeycomb structural body and method of manufacturing the structural body |
JP2015174798A (en) * | 2014-03-14 | 2015-10-05 | 日本碍子株式会社 | plugged honeycomb structure |
JP2015182926A (en) * | 2014-03-25 | 2015-10-22 | 日本碍子株式会社 | Method of producing honeycomb structure |
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