CATALYST CARRIER OF CORDIERITE HONEYCOMB STRUCTURE AND METHOD OF PRODUCING THE SAME

Abstract: Catalyst carriers of cordierite honeycomb structures of low thermal expansion, porosities of not exceeding 30%, high strengths and thin partition walls with high cell density or low cell density are provided. The method of producing them uses very fine particles of kaoline and talc, specifically talc having an average particle diameter of not more then 7 µm and kaoline having an average particle diameter of not more than 2 µm and not more than of the average particle diamter of the talc.

Description: The present invention relates to a catalyst carrier of cordierite honeycomb structure, particularly to a catalyst carrier of high strength and low thermal expansion honeycomb structure used for catalyst carriers for purifying exhaust gases from automobiles, and a method of producing the carrier. Recently, thermal shock resistant and porous cordierite honeycomb ceramics have been interested, especially as materials for catalyst carriers of honeycomb structure used in devices for purifying hydrocarbons, carbon monoxide and nitrogen oxides in various exhaust gases. Among various devices for purifying exhaust gases, devices for purifying exhaust gases from automobiles are prevailingly used, nowadays. Catalyst carriers used in such purifying devices for exhaust gases from automobile engines are requested to have a few important characteristic properties. One of such property is so-called "thermal shock resistance" which is a property that withstand a crack or breakage caused by a thermal stress exerted by temperature differences. The temperature differences are formed in a honeycomb structure by temperature change due to rapid heat generation by catalytic oxidation reactions of unburnt hydrocarbons, carbon monoxide, etc. in an exhaust gas. The thermal shock resistance is expressed by a temperature difference of the honeycomb structure of withstanding a rapid heating and a rapid cooling, and the temperature difference is known to be inversely proportional to a coefficient of thermal expansion among various properties of the honeycomb structure, and thermal shock resistance becomes larger when the coefficient of thermal expansion (to be referred to as "CTE", hereinafter) becomes smaller. An other property requested to catalyst carriers of ceramic honeycomb structure is an adhering property of catalyst active substances and catalyst substances to the catalyst carriers. Additional important property requested to catalyst carriers of ceramic honeycomb structure is initial activity that is right-off property of the catalyst at the incipient period of using the catalyst of honeycomb structure. Heretofore, low expansion of cordierite ceramics has been publicly known. For instance, U.S. Patent No. 3,885,977 specification discloses an oriented cordierite ceramics of CTE of less than 11×10⁻⁷(1/°C) in at least one direction in a temperature range of 25-1,000°C describes a planar orientation determinated into platelets during processing of stacked clay, which can be platelet clay such as kaoline, etc. as a cause of such orientation. In addition, U.S. Patent No. 4,280,845 discloses use of a magnesia source material such as talc, etc. of a limited coarse particles range of 10-50 µm to obtain an extremely low thermal expansion cordierite ceramics. Meanwhile, according to recent extensive improvement in the technique of applying catalysts on carriers of honeycomb structure, a desire for large porosity strongly requested to the catalyst carriers of honeycomb structure has been decreased. On the other hand, reduction of volume of the catalyst carriers, improvement of the catalyst property, improvement of right-off property and reduction of fuel consumption rate; reduction of pressure loss for increasing engine power; improvement of strength for reducing cost of canning the honeycomb structure in a casing; and improvements of strength and thermal shock resistance from the necessity of arranging the catalyst­ equipped devices for purifying exhaust gases near the automobile engines as near as possible for enhancing the catalyst activity; have been desired earnestly. For solving these recent desires to the catalyst carriers of honeycomb structure, thinning of the partition walls of the cells of the honeycomb structure and increase of cells number per unit crosssectional area of the honeycomb structure for improving the catalyst properties, or thinning of the partition walls and decrease of cells number per unit area for decreasing pressure loss, have been studied. However, the thinning of the partition walls and the increase of cells number lead to a drawback of decreasing the strength of the porous cordierite ceramics of honeycomb structure, and a drawback of largely increasing the CTE of the cordierite honeycomb structure, because of a necessity of using far finer particles as raw materials, particularly magnesia source material, caused by decrease of width of slits of an extruding die which extrudes the raw materials into a honeycomb structure. Besides, densification of cordierite ceramics is rather difficult. Especially, for producing low thermal expansion cordierite ceramics of CTE of 2.0×10⁻⁶/°C or less in a temperature range of from room temperature to 800°C, batch composition of raw materials have to be used wherein an amount of impurities such as alkali (calcia, potassium, sodium) and the like which function as fluxes in firing the batch is limited to a very minor amount, so that cordierite honeycomb structures obtained by firing the batch composition have very few amount of glass phases and hence are very porous and not dense. Particularly, cordierite honeycomb structures recently used as carriers of catalysts for purifying exhaust gases from automobiles necessitate CTE of not over than 1.5×10⁻⁶/°C in a temperature range of room temperature to 800°C, so that raw materials such as talc, kaoline, alumina, etc. of low impurities are predominantly used, and hence the fired cordierite honeycomb bodies have minimum open porosities of about 25-45% as possible, even if production districts, types and particle sizes of the raw materials are selected cautiously. Especially, for producing honeycomb structures of porosities of not over than 30%, amounts of the impurities and minimization of particle sizes of the raw materials are unavoidable, so that product honeycomb structures of CTE of 1.0×10⁻⁶/°C or less in a temperature range of from room temperature to 800°C have not been obtained. Moreover, when producing cordierite honeycomb structures of relatively small porosity, molded honeycomb structures have so large shrinkage in the drying step and the firing step of the production process that they are liable to suffer from cracks, and honeycomb structures of large sizes have been difficult to produce at high production yields. From the technical reasons as described above, catalyst carriers of very low thermal expansion cordierite honeycomb structures and low porosity and still of sufficiently high strength properties, have been desired earnestly. It is an object of the present invention to provide the above desired cordierite honeycomb structures of splendid properties of very low thermal expansion, thin wall, large number of cells, and high strength properties. Another objects of the present invention will become apparent from the ensuing descriptions of the specification. If fine talc is used as a raw material for batches of raw materials for producing honeycomb structures, the produced honeycomb structures have a drawback of extremely large CTE, as described in the aforementioned U.S. Patent No. 4,280,845. The inventors have dared to use, among the fine talc particles which have the drawback as mentioned above, especially fine talc particles of an average particles diameter of 7 µm or less, preferably 5 µm or less, and have found out that increase of CTE caused by the use of the very fine talc particles can be obviated by co-use of very fine kaoline particles of an average particles diameter of 2 µm or less, preferably 1 µm or less, which finding leading to the present invention. Use of such fine particles together has previously been thought disadvantageous. The fine raw materials including the co-use of very fine talc and kaoline can further include co-use of fine alumina and/or aluminum hydroxide of an average particles diameter of 2 µm or less and/or highly pure amorphous silica. The inventors have found out also that the co-use of the very fine raw materials can decrease the porosity of the produced cordierite honeycomb structures to 30% or less, and exhibit a high strength which can assuredly withstand to practical use of the produced cordierite honeycomb structures, even when the partition walls of the cells of the honeycomb structures are produced thinly. The inventors have further found out that use of kaoline of an average particles diameter of one-third (1/3) or less of an average particles diameter of talc, is preferable. The inventors have also found out that a difference is very small between CTE in the direction perpendicular to the flow passages (to be referred to as "axis B", hereinafter) of the honeycomb structure, which CTE in axis B has great contribution to the thermal shock resistant property of the honeycomb structure, and CTE in the direction of flow passages (to be referred to as "axis A", hereinafter) of the honeycomb structure, which CTE in axis A has the most low thermal property due to orientations of cordierite crystals. Conventional cordierite honeycomb structures using coarse particles of the raw materials have confused orientations of the raw materials such as talc, kaoline, etc. at about the crosssections of the walls of the honeycomb structures when the honeycomb structures are formed by extrusion from the extrusion dies, so that CTE in axis B have showed large values of CTEs' difference of exceeding 0.2 × 10⁻⁶/°C in a temperatures range of 40-800°C as compared with CTE in axis A. Now, the inventors have found out that the honeycomb structures are adversely influenced only in a small extent on thermal expansion at the crosssections of the partition walls of the honeycomb structures by virtue of the use of the very fine particles of the raw materials, and the thermal expansion in axis B of the honeycomb structures can be decreased extensively which is very important in improving the thermal shock resistance of the honeycomb structures. The present invention is a catalyst carrier of cordierite honeycomb structure of high strength and low thermal expansion, which has a chemical composition in weight basis of 42-56% of SiO₂, 30-45% of Al₂O₃ and 12-16% of MgO as main components, crystal phases consisting mainly of cordierite, a porosity of 30% or less, preferably 25% or less, CTE of 0.8×10⁻⁶/°C or less in axis A in a temperature range of 40-800°C, and a CTE of 1.0×10⁻⁶/°C or less in axis B in a temperature range of 40-800°C. In an embodiment of the present invention, the honeycomb structure has a partition wall thickness of 203 µm or less. The present invention is also a method of producing a catalyst carrier or cordierite honeycomb structure, comprising, preparing a batch of very fine talc of an average particle diameter of 7 µm or less, very fine kaoline in which the average particle diameter of raw kaoline and calcined kaoline on a weight basis is not more than 2 µm and is 1/3 or less of the average particle diameter of the talc, and other raw materials (not including further talc or further kaoline) for producing a cordierite honeycomb structure of a chemical composition in weight basis of 42-56% of SiO₂, 30-45% of Al₂O₃ and 12-16% of MgO as main components, adding an organic binder and a plasticizer to the batch, kneading the added batch to plasticize the same to an extrudable extent, extruding the admixture to form a honeycomb structure, drying the extruded honeycomb structure, and firing the honeycomb structure at a temperature of 1,350-1,440°C, whereby a catalyst carrier of cordierite honeycomb structure of high strength and low thermal expansion is produced, which has a chemical composition in weight basis of 42-56% of SiO₂, 30-45% of Al₂O₃ and 12-16% of MgO as main components, crystal phases consisting mainly of cordierite, a porosity of 30% or less, CTE of 0.8×10⁻⁶/°C or less in axis A in a temperature range of 40-800°C, CTE of 1.0×10⁻⁶/°C or less in axis B in a temperature range of 40-800°C, and a difference of 0.2×10⁻⁶/°C or less between the two CTE. In producing the cordierite honeycomb structures of the present invention, the raw materials can include further alumina and/or aluminum hydroxide of an average particles diameter of 2 µm or less and/or 8% or less of highly pure amorphous silica. The honeycomb structure of the present invention has a chemical composition in weight basis of 42-65%, preferably 47-53% of SiO₂, 30-45%, preferably 32∼38% of Al₂O₃, and 12-16%, preferably 12.5-15% of MgO, which is in a region extending around a theoretical composition point of cordierite (2MgO·2Al₂O₃·5SiO₂) known heretofore as a composition of low thermal expansion cordierite ceramics, and can achieve the purposes of a porosity of 30% or less, CTE of 0.8×10⁻⁶/°C or less in axis A in a temperature range of 40-800°C, and CTE of 1×10⁻⁶/°C or less in axis B in the same temperature range, by varying various conditions for producing the cordierite honeycomb structure. Chemical components other than the main components are liable to effect adverse influences on the thermal expansion property of the cordierite honeycomb structures, so that the impurities such as TiO₂, CaO, K₂O, Na₂O, Fe₂O₃, P₂O₅, etc. are desirably suppressed to an amount of 2.5% or less. Particularly, the smaller the amount of alkali components such as CaO, K₂ and Na₂O is, the better the thermal expansion property of the honeycomb structures. The amount of P₂O₅ should be substantially zero or less than 0.1%. The crystal phases preferably consist substantially of cordierite crystal phase, the amount of the cordierite crystals is at least 90 wt%, and the amounts of mullite and spinel (inclusive of sapphirine) as other crystals contained are respectively 2.5 wt% at the maximum. The fine talc particles are preferably of small impurities of alkali content, and preferably produced by a pulverizing or crushing means such as Raymond mill, etc., and not by a grinding means such as a a ball mill, etc., which destructs the shape of the talc particles. The talc particles of diameters exceeding 7 µm cause the difference of the two CTE in axes A and B and the porosity large. Also, the fine kaoline particles are preferably of small impurities content, and preferably those of small variations in crystals shape and not intermingled with large crystals. For example, kaolines having large variations in crystal shape and a tendency of forming secondary particles, such as New Zealand kaoline, etc., are not preferable. In preparing the raw material kaoline from calcined kaoline, the calcined kaoline is preferably ground in a wet type ball mill, in order to obtain dense honeycomb structures. If kaoline of particles diameter of exceeding 2 µm is used simultaneously with talc particles of diameters of 7 µm or less, the cordierite honeycomb structures produced have increased CTE and porosities. If the fine raw materials talc of an average particles diameter of 5 µm or less and/or the fine raw material kaoline of an average particles diameter of 1 µm or less and which is 1/3 or less of the average particles diameter of talc are used, the porosity can be decreased, while maintaining the low expansion. The present invention includes use of calcined talc and calcined kaoline which are effective for preventing the formation of cracks in the honeycomb structures caused by shrinkage, etc. during the drying and firing steps, when using the finely divided or pulverized raw materials kaoline and talc. Use of a higher temperature for calcining talc and kaoline incurs increase of porosity and CTE of the resultant honeycomb structures, so that the calcining temperature should preferably be made as low as possible, if calcined talc or kaoline is used. The splendid effects of the present invention cannot be attained, unless the same fine particles of calcined talc and kaoline as those of the raw materials talc and kaoline are used. In order to achieve porosity of 30% or less, the other raw materials for cordierite, namely, an alumina source material such as alumina, aluminum hydroxide etc., and a silica source material such as amorphous silica, quartz sand, etc., which are the same ones as those used conventionally can be used. However, the amount of impurities such as alkali in the chemical composition of the raw materials has to be properly adjusted and particle sizes of the raw materials have to be properly adjusted by excluding or cutting off the coarse particles, depending on thickness of the partition walls of the honeycomb structures to be produced. When using the fine particles of alumina and/or aluminum hydroxide for achieving a porosity of 25% or less, use of fine particles of a diameter of 2 µm or less contribute to the aimed decrease of porosity, and use of alumina of low sodium content (Na₂O of 0.12% or less) affords further advantageous effects of low CTE and low porosity. Addition of highly pure amorphous silica for achieving low thermal expansion also contributes to decrease of porosity. However, addition in excess of 8% is not preferable, because it deteriorates the catalyst carriers properties. For producing the cordierite honeycomb structures, extrusion process used for the production of conventional cordierite honeycomb structures can be applied. In firing, the firing temperature is desirably elevated at an average temperature raising rate of 20-300°C/hr, preferably 30-200°C/hr, in a temperature range of 1100-1350°C to a maximum temperature of 1350-1440°C where it is held for 0.5-24 hrs. If the average temperature raising rate is less than 20°C/hr, CTE becomes large, and if it exceeds 300°C/hr, deformation of the fired product becomes large. While, if the firing temperature is less than 1350°C, CTE becomes large, and if it exceeds 1440°C, deformation of the fired product becomes large. Regarding cell structure and strength properties, honeycomb structures particularly for use as catalyst carriers for purifying exhaust gases exited from automobile engines are requested usually to have compressive strength in axis A of at least 150-200 kg/cm² for a square cell structure of a cell number of 62 per square centimeters and a partition wall thickness of 152 µm (abbreviated as "152 µm/62 cells/cm²", herein­ after) in order to withstand vibration in operation of automobiles as well as holding pressure of containers holding the catalyst carriers. Now, according to the present invention, porosity can be decreased to 30% or less without increasing CTE of the cordierite honeycomb structures, so that high level of compression strength in axis A of indeed 300 kg/cm² or more at 152 µm/62 cells/cm² can be realized. In addition, honeycomb structures of a cell structure of 152 µm/47 cells/cm² which was so weak in strength that practical use thereof was impossible, and a cell structure of a cell number of 93 per cm² and a wall thickness of 102 µm (abbreviated as "102 µm/93 cells/cm²") which were unable to use in practice from the both view points of strength and CTE, exhibit considerably level of compression strength in axis A of 200 kg/cm² or more, so that it became possible to design various cell structures depending on shape of the catalyst carrier and condition of places at which the catalyst carriers are to be arranged. That is, the improvement of the strength of the honeycomb structures brought from the present invention can exhibit superior effects in thermal shock resistant property and catalyst properties as compared with conventional ones in applying the present invention to the honeycomb structures of thinner partition walls and a higher number of cells, i.e., highly densified cells, and can exhibit excellent effects in improving thermal shock resistance and decreasing pressure loss as compared with conventional ones in applying the present invention to honeycomb structures of thin wall and low number of cells. In contrast to heretofore used honeycomb structures of a partition wall thickness of 300 µm and a cell number of 47 per cm², the present invention can obtain honeycomb structures of a partition wall thickness of 102 µm and a cell number of 93 cm², so that catalyst activity can be extensively improved owing to the cell structure of high density of cell number per unit area as well as thermal shock resistant property. Hence, cordierite honeycomb structures which are suited well as catalyst carriers for purifying exhaust gas from automobile engines can be realized for mounting on manifolds, etc., near automobile engines. Similarly, as compared with a honeycomb structure of conventional 300 µm/47 cells/cm², the honeycomb structure of 152 µm/62 cells/cm² is widely improved in compression strength in axis A, so that canning of the honeycomb structure to a casing thereof can be simplified and honeycomb structures suited well to the mounting at manifolds, etc., near automobile engines of violent vibration can be realized. In addition, honeycomb structures of 152 µm/47 cells/cm² of CTE and compression strength in axis A which are the same level as those of honeycomb structures of 300 µm/47 cells/cm² can be obtained, so that honeycomb structures can be realized which have improved engine powers due to decrease of pressure loss of exhaust gases from automobile engines and which are suited well to decrease the fuel consumption rate. The low CTE in axis B of the honeycomb structures according to the present invention are advantageous, particularly in increasing highly the cell number per unit area to improve the catalyst carriers properties. The honeycomb structures of the present invention provides an advantages that they are composed of cell structure of considerably thinner partition walls thickness as compared with conventional honeycomb structures of partition wall thickness of 203 µm or less. That is, the present invention is suitable for honeycomb structures of thin walls and relatively small number of cells per unit area. Meanwhile, the present invention can also be applied widely to honeycomb structures of large partition wall thickness and a small number of cells per unit area, by virtue of achieved high strength. For a better understanding of the present invention, reference is made to the accompanying drawings, in which: Fig. 1 is a graph showing particle size distributions of a fine talc used in the method of the present invention; Fig. 2 is a graph showing particle size distribution of a fine kaoline used in the method of the present invention; Fig. 3 is a schematic perspective view showing a honeycomb structure of the present invention; and Fig. 4 is a graph showing relations between porosity, partition wall thickness and cell number of the honeycomb structures of the present invention Hereinafter, the present invention will be explained in more detail with reference to Examples. Example 1 Raw materials of chemical compositions and particle sizes as shown in the following Table 1 are reciped based on the recipes as shown in Table 2 to prepare batches of Nos. 1-32 of Table 2. 100 parts by weight of each batch is added with 3.8 parts by weight of methylcellulose and a suitable amount of water to produce mixtures capable of being blended and extruded. The used raw materials are preliminarily passed through a sieve of 63 µm. Then, the mixtures are blended. Thereafter, each mixture of the respective batch is formed by a publicly known extrusion means into a cylindrical honeycomb structure of a diameter of 93 mm and a height of 100 mm having a square cell structure, a partition wall thickness of 102 µm, and a cell number of 93 per cm². Each honeycomb structure is dried, and fired at a firing condition as shown in Table 2 to obtain sintered honeycomb structure bodies. On the sintered bodies are evaluated CTE in axis A in a temperature range of 40-800°C, CTE in axis B in the same temperature range, porosity, amount of cordierite crystals, compression strength in the direction of axis A, and thermal shock resistance. The results of the evaluation are also shown in Table 2. All the sintered bodies have chemical compositions of P₂O₅ content of less than 0.1%. Particle size distributions and average particles diameter of the raw materials are those based on the principle of X-ray sedimentation method, and measured by Sedigraph (Trade name) of Micromeritics Co. Example 2 The batches of Nos. 6 and 21 of Table 2 are extruded respectively from dies of different cell structures in the same manner as in Example 1, and the green honeycomb structures are fired to produce cylindrical honeycomb structures of Nos. 41-47 of a diameter of 93 mm and a height of 100 mm and cell structures as shown in Table 3. Thus produced honeycomb structures are evaluated on CTE in axis A in a temperature range of 40-800°C, CTE in axis B in the same temperature range, and compression strength in axis A. The results of the evaluation are also shown in Table 3. As clearly apparent from the above Tables 2 and 3, the cordierite honeycomb structures of the present invention exhibit exceedingly superior low expansion and strength as catalyst carriers. Example 3 Raw materials of characteristic properties as shown in the following Table 4 are used to prepare batches of Nos. 51-87 of Table 5 based on batch composition shown in Table 5. 100 parts by weight of the batch composition of the raw materials are added and kneaded with 3.8 parts by weight of methylcellulose and a suitable amount of water to form an extrudable blend. The raw materials were all preliminarily treated to pass a sieve of 63 µm. Then, each blend of the respective batch is formed into a cylindrical honeycomb structure of a diameter of 93 mm and a height of 100 mm having a square cell structure, a cell number of 93 per cm² and a partition wall thickness of 102 µm by a publicly known extrusion means. The honeycomb structures of respective batches are dried, and fired at firing conditions shown in Table 5 to sinter the same. The sintered bodies are evaluated on CTE in axis A in 40-800°C, CTE is axis B in 40-800°C, porosity, amount of cordierite crystals, compression strength in the direction of axis A, and thermal shock resistance. The results of the evaluation are also shown in Table 5. All the sintered bodies have chemical compositions of P₂O₅ content of less than 0.1%. Particle size distributions and average particles diameter of the raw materials are measured in the same way as in Example 1. As seen from Table 5, test Nos. 51-62 64, 65 and 67 wherein fine talc and kaoline are admixtured with alumina and/or aluminum hydroxide of an average particles diameter of 2 µm or less, and test Nos. 71, 73-87 wherein highly pure amorphous silica is added in an amount of not over than 8%, achieve smaller porosities and lower CTE than Example 1 wherein relatively coarse alumina particles of an average particles diameter of 4 µm are used. Examples of test Nos. 63, 66 and 71 used aluminum hydroxide of a particle size of 3.6 µm larger than 2.0 µm, and test No. 72 used crystalline silica as a silica source material, so that their porosities are higher than other test Nos. in Table 5. However, these porosities are substantially equal to the porosities of the present honeycomb structures, so that they fall within the scope of the present invention. Example 4 Batches of test Nos. 60 (porosity 18.0%), 56 (porosity 20.3%), 53 (porosity 23.0%), 51 (porosity 25.0%), 78 (porosity 27.0%) and 73 (porosity 30.0%) are respectively formed into honeycomb structures by extrusion from dies of different cell structures in the same manner as in Example 3, and the extrudates are dried and fired to produce cylindrical honeycomb structures of diameter of 93 mm and a height of 100 mm having cell structures as shown in the following Table 6. Respective honeycomb structures are measured on compression strength in axis A. From the measurements, points corresponding to compression strength in axis A of 200±10 kg/cm² are plotted, and interrelations between porosity, partition wall thickness and cell number per unit area, are shown in the attached Fig. 4. From Table 6 and Fig. 4, it becomes clear that, when calculated a partition wall thickness at the time of the compression strength in axis A of the honeycomb structure of 200 kg/cm² from the porosities which are included in the scope of the present invention, the partition wall thickness can be defined as 437 µm or less in a range of cell density of 2-140 cells/cm². As described in detail in the foregoings, the present invention can provide honeycomb structures of low expansion, porosities of 30% of less, high strengths and thin partition walls with high or low cell densities. These honeycomb structures can be used advantageously in a broader range as catalyst carriers of honeycomb structures, particularly catalyst carriers for purifying exhaust gases from automobile engines. Thus, the present invention is eminently useful industrially. Although the present invention has been described with reference to specific examples and numerical values, it should be understood that the present invention is not restricted to such examples and numerical values, and numerous changes and modifications are possible without departing from the broad spirit and the aspect of the present invention as defined in the appended claims.

Claims: 1. A catalyst carrier of cordierite honeycomb structure which as a chemical composition in weight basis of 42-56% of SiO₂, 30-45% of Al₂O₃ and 12-16% of MgO as main components, crystalline phases consisting mainly of cordierite, a porosity not exceeding 30%, CTE not exceeding 0.8x10⁻⁶/°C in the direction perpendicular to the flow passages of the honeycomb structure in a temperature rang of 40-800°C, CTE not exceeding 1.0×10⁻²/°C in the direction of flow passages of the honeycomb structure in the same temperature range. 2. A catalyst carrier of cordierite honeycomb structure as defined in claim 1, which has a porosity of not exceeding 25%. 3. A catalyst carrier of cordierite honeycomb structure as defined in claim 1, which has a difference of CTE of not exceeding 0.2×10⁻⁶°C between CTE in axis B and CTE in axis A. 4. A catalyst carrier of cordierite honeycomb structure as defined in claim 1, which has a compressive strength in axis A of not less than 200 kg/cm². 5. A catalyst carrier of cordierite honeycomb structure as defined in claim 1, which has a partition wall thickness of not exceeding 437 µm. 6. A method of producing a catalyst carrier of cordierite honeycomb structure, comprising, preparing a batch of very fine talc of an average particles diameter of not exceeding 7 µm, very fine kaoline of an average particles diameter of not exceeding 2 µm and not exceeding of the average particles diameter of talc, and other raw materials for producing the cordierite, adding an organic binder and a plasticizer to the batch, kneading the added batch to plasticize the same to an extrudable extent, extruding the admixture to form a honeycomb structure, drying the extruded honeycomb structure, and firing the honeycomb structure at a temperature of 1350-1440°C. 7. A method as defined in claim 6, wherein the talc has an average particles diameter of not exceeding 5 µm. 8. A method as defined in claim 6 or claim 7, wherein the kaoline has an average particles diameter of not exceeding 1 µm. 9. A method as defined in any one of claims 6 to 8, wherein at least one of alumina and aluminum hydroxide of an average particles diameter of not exceeding 2 µm is added to the batch. 10. A method as defined in claim 9, wherein the raw material alumina has a Na₂O content of not exceeding 0.12%. 11. A method as defined in any one of claims 6 to 10 wherein the kaoline is prepared by grinding calcined kaoline in a wet type ball mill. 12. A method as defined in any one of claims 6 to 11 wherein highly pure amorphous silica is added to the batch. 13. A method as defined in claim 12, wherein the highly pure amorphous silica is added to the batch in an amount of not exceeding 8%.

Inventors: ASAMI, SEIICHI, HAMANAKA, TOSHIYUKI, HARADA, TAKASHI, WATANABE, KEIICHIRO
Applicants: NGK INSULATORS, LTD.
Application year: 1986
Main classification: B01J35
IPC codes: C04B38, B01J35, B01J21, C04B35