Honeycomb structure

Abstract

A honeycomb structure includes a honeycomb substrate having a porous partition wall that defines a plurality of cells that extend from an inlet end face as an inlet side for a fluid to an outlet end face as an outlet side for the fluid, and a porous circumferential wall that is monolithically formed with the partition wall, and a coat layer that is disposed on at least a part of the outer surface of the circumferential wall. Here, a part of the coat layer penetrates into the pores of the circumferential wall, and a thickness of the part of the coat layer that penetrates into the pores of the circumferential wall is from 1 to 90% of the thickness of the circumferential wall.

Claims

1. A honeycomb structure, comprising: a honeycomb substrate having a plurality of porous partition walls that define a plurality of cells that extend from an inlet end face as an inlet side for a fluid to an outlet end face as an outlet side for the fluid, and a porous circumferential wall that is formed monolithically with the partition wall, and a coat layer that is disposed on at least a part of the outer surface of the circumferential wall and extends around the entire circumference of the circumferential wall, wherein a part of the coat layer penetrates into the pores of the circumferential wall, and a thickness of the part of the coat layer that penetrates into the pores of the circumferential wall is from 15 to 50% of the thickness of the circumferential wall.

2. A honeycomb structure, comprising: a honeycomb substrate having a plurality of porous partition walls that define a plurality of cells that extend from an inlet end face as an inlet side for a fluid to an outlet end face as an outlet side for the fluid, and a porous circumferential wall having a porosity of 50% or more, that is formed separately from the partition wall, and a coat layer that is disposed on at least a part of the outer surface of the circumferential wall, wherein a part of the coat layer penetrates into the pores of the circumferential wall, and a thickness of the part of the coat layer that penetrates into the pores of the circumferential wall is from 15 to 50% of the thickness of the circumferential wall, and wherein porosity of the circumferential wall and the partition walls are the same.

3. The honeycomb structure according to claim 1, wherein a remaining part of the coat layer, other than the part that penetrates into the pores of the circumferential wall, has a thickness of 70 m or less.

4. The honeycomb structure according to claim 1, wherein the coat layer contains Si.

5. The honeycomb structure according to claim 4, wherein the coat layer further contains Ti.

6. The honeycomb structure according to claim 1, wherein the honeycomb substrate has a porosity of from 50 to 75%.

7. The honeycomb structure according to claim 1, wherein the honeycomb substrate has a porosity of from 59 to 67%.

8. The honeycomb structure according to claim 1, which has plugging portions that are configured to plug the open ends of predetermined cells at the side of the inlet end face and the open ends of residual cells at the side of the outlet end face.

9. The honeycomb structure according to claim 2, wherein a remaining part of the coat layer, other than the part that penetrates into the pores of the circumferential wall, has a thickness of 70 m or less.

10. The honeycomb structure according to claim 9, wherein the coat layer contains Si.

11. The honeycomb structure according to claim 10, wherein the coat layer further contains Ti.

12. The honeycomb structure according to claim 11, wherein the honeycomb substrate has a porosity of from 50 to 75%.

13. The honeycomb structure according to claim 11, wherein the honeycomb substrate has a porosity of from 59 to 67%.

14. The honeycomb structure according to claim 13, which has plugging portions that are configured to plug the open ends of predetermined cells at the side of the inlet end face and the open ends of residual cells at the side of the outlet end face.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a perspective view that schematically shows an exemplary embodiment of a honeycomb structure of the present invention;

(2) FIG. 2 is a schematic view showing a cross-sectional surface that is in parallel with the direction to which cells extend in the exemplary embodiment of the honeycomb structure of the present invention;

(3) FIG. 3 is an enlarged view of the part A in FIG. 2;

(4) FIG. 4 is a perspective view that schematically shows another exemplary embodiment of a honeycomb structure of the present invention; and

(5) FIG. 5 is a schematic view showing a cross-sectional surface that is in parallel with the direction to which cells extend in the other exemplary embodiment of the honeycomb structure of the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

(6) The present invention will be explained below based on specific exemplary embodiments, but the present invention is not interpreted by being limited to those exemplary embodiments, and modification, improvement or the like of a design can be suitably added within a scope that does not deviate from the purport of the present invention based on the general knowledge of a person skilled in the art.

(7) (1) Honeycomb Structure:

(8) FIG. 1 is a perspective view that schematically shows an exemplary embodiment of the honeycomb structure of the present invention. Furthermore, FIG. 2 is a schematic view shows a cross-sectional surface that is in parallel with the direction to which the cells extend in the exemplary embodiment of the honeycomb structure of the present invention, and FIG. 3 is an enlarged view of the part A in FIG. 2. As shown in FIGS. 1 and 2, a honeycomb structure 1 according to the present invention includes a honeycomb substrate 2 and a coat layer 3. The honeycomb substrate 2 has a porous partition wall 4 that defines a plurality of cells 5 that extend from an inlet end face 11 as an inlet side for a fluid to an outlet end face 12 as an outlet side for the fluid, and a porous circumferential wall 6 that is formed monolithically with the partition wall 4. The formed monolithically used herein means that the partition wall 4 and the circumferential wall 6 are simultaneously subjected to extrusion molding in the steps for the production of the honeycomb substrate 2, and thus the partition wall 4 and the circumferential wall 6 have been monolithic from immediately after the extrusion in the obtained formed body. In the honeycomb substrate 2 obtained by firing such formed body, the porosity of the entirety of the honeycomb substrate, i.e., the porosity of the partition wall 4 and the porosity of the circumferential wall 6, is the same.

(9) The coat layer 3 is disposed on at least a part of the outer surface of the circumferential wall 6 of the honeycomb substrate 2. The coat layer 3 contains a material that can penetrate into the pores of the circumferential wall 6. Specifically, it is preferable to contain particles having an average particle diameter that is smaller than the average pore diameter of the circumferential wall 6, and a water repelling material. The material of the particles is not especially limited, and inorganic particles such as silicon carbide, silica, silicon nitride, cordierite, alumina, mullite, zirconia and the like are preferable, and particles containing Si (silicon) such as silicon carbide and silica are especially preferable. Furthermore, the kind of the water repelling material is also not especially limited, and is preferably a water repelling material containing Si such as silicone-based water repelling materials. Specific examples of the silicone-based water repelling materials include silicone oil and the like.

(10) As shown in FIG. 3, in the present invention, a part of the coat layer 3 penetrates into pores 7 of the circumferential wall 6. FIG. 3 shows an exemplary embodiment in which the coat layer 3 containing particles 8 having an average particle diameter that is smaller than the average pore diameter of the circumferential wall 6 is disposed on the outer surface of the circumferential wall 6 of the honeycomb substrate 2. In this exemplary embodiment, the particles 8 contained in the coat layer 3 are in a state that they penetrate into the pores 7 of the circumferential wall 6.

(11) Accordingly, since a part of the coat layer 3 penetrates into pores 7 of the circumferential wall 6 in the present invention, the pores 7 of the circumferential wall 6 are occluded. Therefore, even when a catalyst slurry is introduced into the cells 5 so that a catalyst is loaded on the partition wall 4 of the honeycomb structure 1 of the present invention, the slurry does not exude on the outer surface of the circumferential wall 6, and thus fine workability can be obtained in the step of loading a catalyst on the partition wall 4 of the honeycomb structure 1. Furthermore, since the circumferential wall 6 is reinforced by the coat layer 3, the strength of the circumferential wall 6 is improved, and thus the breakage of the circumferential wall 6 when a part of the circumferential wall 6 of the honeycomb structure 1 is chucked (gripped) in the step of loading a catalyst on the honeycomb structure 1 can be effectively prevented. Furthermore, as a result of the improvement of the strength of the circumferential wall 6, the isostatic strength of the entirety of the honeycomb structure 1 is improved, and thus the breakage of the honeycomb structure 1 during transportation and actual use can also be effectively prevented. Moreover, in the case when a coat layer containing a water repelling material is disposed, in addition to an effect of preventing the exuding of the catalyst slurry by the occlusion of the pores of the circumferential wall by the coat layer, an effect of preventing the exuding of the catalyst slurry by the repelling of the catalyst slurry by the water repelling material in the coat layer can be obtained.

(12) In the present invention, a thickness T2 of a part 3b that penetrates into the pores 7 of the circumferential wall 6 of the coat layer 3 (hereinafter referred to as penetrated part) is from 1 to 90%, preferably from 10 to 60%, especially preferably from 15 to 50% of a thickness T1 of the circumferential wall 6 of the honeycomb substrate 2 (see FIG. 3). If the thickness T2 of the penetrated part 3b of the coat layer 3 is from 1 to 90% of the thickness T1 of the circumferential wall 6, the pores 7 of the circumferential wall 6 can be effectively occluded even the honeycomb substrate 2 having a high porosity such that the porosity is 50% or more is used. In contrast to this, if the thickness T2 of the penetrated part 3b of the coat layer 3 is lower than 1% of the thickness T1 of the circumferential wall 6, in the case when the honeycomb substrate 2 having a high porosity such that the porosity is 50% or more is used, the occlusion of the pores 7 of the circumferential wall 6 is incomplete, and thus an effect of preventing the exuding of a catalyst slurry may not be obtained. Furthermore, if the thickness T2 of the penetrated part 3b of the coat layer 3 exceeds 90% of the thickness T1 of the circumferential wall 6, the coat layer 3 also penetrates into the pores of the partition wall 4, the loading of the catalyst into the pores of the partition wall 4 is disturbed, and thus the exhaust gas purifying performance may deteriorate. The thickness of the penetrated part 3b of the coat layer 3 was observed by a SEM (scanning electron microscope), and measured.

(13) Furthermore, in the present invention, a remaining part 3a other than the part that penetrates in the pores 7 of the circumferential wall 6 (hereinafter referred to as non-penetrated part) of the coat layer 3 has a thickness T3 of preferably 70 m or less, more preferably 8 m or less (see FIG. 3). If the thickness T3 of the non-penetrated part 3a of the coat layer 3 exceeds 70 m, cracks may be generated on the coat layer 3. The lower limit of the thickness T3 of the non-penetrated part 3a of the coat layer 3 is not especially limited, but the value of the lower limit is preferably about 5 m with consideration for easiness of production, and the like. The thickness of the non-penetrated part 3a of the coat layer 3 was observed by a SEM (scanning electron microscope), and measured.

(14) In the present invention, the coat layer 3 may be disposed on either the entirety or a part of the outer surface of the circumferential wall 6 of the honeycomb substrate 2. For example, in the exemplary embodiment shown in FIGS. 1 and 2, in the outer surface of the circumferential wall 6 of the honeycomb substrate 2, the coat layer 3 is disposed in a band-like manner on the part other than the vicinities of the both end faces (inlet end face 11 and outlet end face 12) of the honeycomb substrate 2. This is an exemplary embodiment in which the catalyst is expected to be loaded on the honeycomb structure 1 in the state that the parts in the vicinities of the both end faces of the honeycomb substrate 2 are chucked (gripped). Specifically, in the case when the catalyst slurry is introduced into the cells 5 under such state, the catalyst slurry does not exude from the chucked parts in the outer surface of the circumferential wall 6 of the honeycomb substrate 2, and thus the workability in the step of loading the catalyst is not deteriorated even if the coat layer 3 is not disposed on that parts.

(15) It is preferable that the coat layer 3 contains Si (silicon). In this case, Si may be contained in the coat layer in the state of particles such as SiC particles and SiO.sub.2 particles, or may be contained as a component of a water repelling material such as a silicone-based water repelling material. Since Si is contained in the coat layer 3, the effect of preventing the exuding of the catalyst slurry is improved. The amount of the Si contained in the coat layer 3 is preferably from 10 to 30% by mass with respect to the entirety of the coat layer 3. If the amount of the Si contained in the coat layer 3 is less than 10% by mass with respect to the entirety of the coat layer 3, an action of improving the effect of preventing the exuding of the catalyst slurry may not be sufficiently exerted. Alternatively, if the amount of the Si contained in the coat layer 3 is more than 30% by mass with respect to the entirety of the coat layer 3, the thermal shock resistance of the coat layer 3 may decrease.

(16) Furthermore, it is preferable that the coat layer 3 further contains Ti (titanium). In order to make the production control of the honeycomb structure easy, information such as size and mass is sometimes displayed on the circumferential surface by a barcode or the like. As a method for displaying information, a method including irradiating a circumferential surface of a honeycomb structure with laser light (laser marking) is widely used. In this case, when the surface of a material containing Ti is irradiated with laser light, the irradiated part comes out black. Therefore, if information is displayed by a method including irradiating the surface of a coat layer containing Ti with laser light, the information can be displayed at a high contrast, and thus a read rate when the information is read by a barcode reader or the like is improved. The amount of the Ti contained in the coat layer 3 is preferably from 10 to 30% by mass with respect to the entirety of the coat layer 3. If the amount of the Ti contained in the coat layer 3 is lower than 10% by mass with respect to the entirety of the coat layer 3, when information is displayed (printed) by laser marking, the printing becomes light (the part irradiated with the laser light does not sufficiently develop a color), and thus an action to improve the rate of reading of information may not be sufficiently exerted. Furthermore, if the amount of the T1 contained in the coat layer 3 is more than 30% by mass of the entirety of the coat layer 3, the thickness of the thickness T2 of the penetrated part 3b may become thick and the coating property may deteriorate.

(17) The problems of exuding of the catalyst slurry on the outer surface of the circumferential wall and an insufficient strength become significant especially in a honeycomb structure having a high porosity such that the porosity is 50% or more. Therefore, the present invention is highly useful in the case when a honeycomb substrate having a porosity of from 50 to 75%, and is especially useful in the case when a honeycomb substrate having a porosity of from 59 to 67% is used. The porosity as mentioned herein is a value measured by means of a mercury porosimeter. Furthermore, typical use of such honeycomb structure having a high porosity includes a GPF of a type used by loading a catalyst. Therefore, the honeycomb structure of the present invention can be especially preferably used in such GPF. However, the honeycomb structure of the present invention is not limited to such GPF, and can be widely used in various filters, catalyst carriers and the like.

(18) As the material for the honeycomb substrate 2, ceramic materials such as silicon carbide, silicon-silicon carbide-based composite materials, cordierite, mullite, alumina, spinel, silicon carbide-cordierite-based composite materials, lithium aluminum silicate and aluminum titanate are preferable. Among these, cordierite is especially preferable. This is because, if the material of the honeycomb substrate 2 is cordierite, a honeycomb structure having a small thermal expansion coefficient and an excellent thermal shock resistance can be obtained.

(19) The honeycomb substrate 2 (partition wall 4 and circumferential wall 6) has an average pore diameter of preferably from 10 to 30 m, especially preferably from 15 to 25 m. If the average pore diameter of the honeycomb substrate 2 is lower than 10 m, the pressure loss of the honeycomb structure 1 becomes too high, and thus decrease in an output of an engine may be caused when the honeycomb structure is used as a GPF. Furthermore, if the average pore diameter of the honeycomb substrate 2 exceeds 30 m, a sufficient strength may not be obtained. The average pore diameter as used herein is a value measured by means of a mercury porosimeter.

(20) The partition wall 4 of the honeycomb substrate 2 has a thickness of preferably from 150 to 350 m, especially preferably from 200 to 310 m. If the thickness of the partition wall 4 is lower than 150 m, a sufficient strength may not be obtained. Alternatively, if the thickness of the partition wall 4 exceeds 350 m, the pressure loss of the honeycomb structure 1 becomes too high, and thus decrease in an output of an engine may be caused when the honeycomb structure is used as a GPF.

(21) The circumferential wall 6 of the honeycomb substrate 2 has a thickness of preferably from 300 to 1,000 m, especially preferably from 500 to 800 m. If the thickness of the circumferential wall 6 is lower than 300 m, a sufficient strength may not be obtained. Alternatively, if the thickness of the circumferential wall 6 exceeds 1,000 m, the pressure loss of the honeycomb structure 1 becomes too high, and thus decrease in an output of an engine may be caused when the honeycomb structure is used as a GPF.

(22) The honeycomb substrate 2 has a cell density of preferably from 232.5 to 620.0 cell/cm.sup.2, especially preferably from 310.0 to 465.0 cell/cm.sup.2. If the cell density is lower than 232.5 cell/cm.sup.2, an effective surface area as a filter is insufficient in the case of use as a GPF, and thus the pressure loss after the deposition of PM may become high, and thus decrease in an output of an engine may be caused. Furthermore, if the cell density exceeds 620.0 cell/cm.sup.2, the pressure loss becomes too high, and thus decrease in an output of an engine may be caused in the case of use as a GPF.

(23) The shape (outer shape) of the honeycomb substrate 2 is not especially limited, and for example, can be a round pillar-shape, an oval pillar-shape, a polygonal pillar-shape or the like. Furthermore, the shape in the cross-sectional surface that is vertical to the longitudinal direction of the honeycomb substrate 2 of the cell 5 (hereinafter referred to as cell shape) is also not especially limited, and is preferably a polygonal shape such as a square shape, a hexagonal shape or an octagonal shape, or a combination thereof such as a combination of a square shape and an octagonal shape, or the like.

(24) In the case when the honeycomb structure 1 of the present invention is used in a PM trapping filter such as a GPF, as shown in FIGS. 4 and 5, it is preferable to form plugging portions 9 that are configured to plug the open ends of the predetermined cells 5a at the side of the inlet end face 11 and the open ends of the residual cells 5b at the side of the outlet end face 12. By plugging one open end of each cell 5 of the honeycomb substrate 2 by the plugging portion 9 in this way, the honeycomb structure 1 becomes a wall flow type filter having a high PM trap efficiency. In this wall flow type filter, an exhaust gas that has flown into the cells 5 from the inlet end face 11 passes through the partition wall 4 and then flows out of the cells 5 from the outlet end face 12. Furthermore, during the passage of the exhaust gas in the partition wall 4, the partition wall 4 functions as a filtration layer, and thus the PM contained in the exhaust gas is trapped. It is preferable that the inlet end face 11 and the outlet end face 12 are respectively formed so as to give an arrangement that gives a checkerboard pattern by the cells 5 of which open ends are plugged by the plugging portions 9 and the cells 5 of which open ends are not plugged by the plugging portions 9.

(25) The material of the plugging portions 9 is preferably a material that is deemed as a preferable material for the honeycomb substrate 2. The material of the plugging portion 9 and the material of the honeycomb substrate 2 may be the same material or different materials.

(26) The honeycomb structure 1 of the present invention is supposed to be used by loading a catalyst on the partition wall 4 of the honeycomb substrate 2. The kind of the catalyst to be loaded on the partition wall 4 of the honeycomb substrate 2 is not especially limited, and for example, in the case when the honeycomb structure is used for purifying an exhaust gas from an automobile, it is preferable to use a precious metal. As the precious metal, platinum, rhodium or palladium, or a combination thereof is preferable. The loading amount of these precious metals is preferably from 0.3 to 3.5 g/L per a unit volume of the honeycomb structure 1.

(27) In order to load the catalyst such as a precious metal on the partition wall 4 in a highly dispersed state, it is preferable to load the catalyst once on a heat-resistant inorganic oxide having a large specific surface area such as alumina in advance, and then load the catalyst on the partition wall 4 of the honeycomb substrate 2. As the heat-resistant inorganic oxide on which the catalyst is to be loaded, zeolite or the like can also be used depending on use besides alumina. Furthermore, the catalyst such as a precious metal may be loaded on the partition wall 4 of the honeycomb substrate 2 after being fixed on a co-catalyst composed of ceria, zirconia, or a composite oxide thereof or the like.

(28) The honeycomb structure of the present invention may be such that the circumferential wall of the honeycomb substrate has been separately formed from the partition wall, rather than formed monolithically with the partition wall. The has been separately formed from the partition wall herein means that the formation of the part that becomes the circumferential wall of the honeycomb substrate is conducted after the formation of the part that becomes the partition wall in the step of production of the honeycomb substrate. As mentioned above, also in the case when the catalyst is loaded on the partition wall of the honeycomb structure in which the partition wall and the circumferential wall have been separately formed, if the circumferential wall has a porosity of 35% or more, the catalyst slurry that has been introduced in the cells may exude on the outer surface of the circumferential wall. However, if a predetermined coat layer has been disposed as in the present invention, the exuding of the catalyst slurry can be effectively prevented also in the case when the circumferential wall of the honeycomb substrate that constitutes the honeycomb structure has been formed separately from the partition wall and the circumferential wall has a porosity of 35% or more.

(29) In the case when the circumferential wall of the honeycomb substrate has been formed separately from the partition wall, the porosity of the circumferential wall and the porosity of the partition wall may the same or different. Furthermore, in this case, the average pore diameter of the circumferential wall and the average pore diameter of the partition wall may the same or different. Furthermore, in this case, the material of the circumferential wall and the material of the partition wall may the same or different. The porosity and average pore diameter as mentioned herein are values measured by a mercury porosimeter.

(30) (2) Method for Producing Honeycomb Structure:

(31) An example of the method for producing the honeycomb structure according to the present invention will be explained. Firstly, in order to prepare a honeycomb substrate, a forming raw material containing a ceramic raw material is prepared. The ceramic raw material is preferably at least one kind selected from the group consisting of silicon carbide, silicon-silicon carbide-based composite materials, cordierite forming raw materials, mullite, alumina, spinel, silicon carbide-cordierite-based composite materials, lithium aluminum silicate and aluminum titanate. Among these, cordierite forming raw materials, which have a small thermal expansion coefficient and an excellent thermal shock resistance, are preferable. The cordierite forming raw materials are ceramic raw materials in which silica, alumina and magnesia are incorporated so as to give a chemical composition wherein the silica is within a scope of from 42 to 56% by mass, the alumina is within a scope of from 30 to 45% by mass, and the magnesia is within a scope of from 12 to 16% by mass. The cordierite forming raw materials give cordierite by being fired.

(32) It is preferable to prepare the forming raw material by mixing the ceramic raw material as mentioned above with a dispersing medium, an organic binder, an inorganic binder, a pore former, a surfactant and the like. The composition ratio of the respective raw materials is not especially limited, and a composition rate in accordance with the structure, material and the like of a honeycomb substrate to be prepared is preferable.

(33) Secondly, a kneaded material is formed by kneading the forming raw material. The method for forming a kneaded material by kneading the forming raw material is not especially limited. Examples of preferable methods can include methods using a kneader, a vacuum pugmill and the like.

(34) Secondly, a honeycomb formed body in which a partition wall and a circumferential wall are formed monolithically is formed by extrusion from the kneaded material by using a die in which grid-like slits are formed, and the honeycomb formed body is dried. The drying method is not especially limited. Examples of preferable drying methods can include hot air drying, microwave drying, dielectric drying, drying under a reduced pressure, vacuum drying, freeze drying and the like. Among these, dielectric drying, microwave drying, hot air drying are preferably used singly or in combination.

(35) Secondly, the dried honeycomb formed body (honeycomb dried form) is fired to prepare a honeycomb substrate. In order to remove the binder and the like contained in the honeycomb formed body, it is preferable to conduct calcination (degreasing) before this firing (main firing). The conditions for the calcination are not especially limited, and the conditions may be such conditions that the organic substances (organic binder, surfactant, pore former and the like) contained in the honeycomb formed body can be removed. Generally, the combustion temperature of the organic binder is from about 100 to 300 C., and the combustion temperature of the pore former is from about 200 to 800 C. Therefore, as the conditions for the calcination, it is preferable to heat under an oxidation atmosphere at from about 200 to 1,000 C. for from about 3 to 100 hours. Since the conditions for the firing (main firing) of the honeycomb formed body (temperature, time, atmosphere and the like) differ depending on the kind of the forming raw material, suitable conditions may be selected depending on the kind. For example, in the case when a cordierite forming raw material is used, the firing temperature is preferably from 1,410 to 1,440 C. Furthermore, the firing time is preferably set to about from 4 to 8 hours as a keep time at the highest temperature. The apparatus for conducting the calcination and main firing is not especially limited. Examples of preferable apparatuses can include an electric furnace, a gas furnace and the like.

(36) In the case when a honeycomb structure having plugging portions is prepared, plugging portions are formed on a honeycomb substrate. The plugging portions are formed so as to plug the open ends of the predetermined cells at the side of one end face (an inlet end face) and the open ends of the residual cells at the side of another end face (an outlet end face). For the formation of these plugging portions, a conventionally-known method can be used. An example of a specific method is as follows. Firstly, a sheet is attached to an end face of a honeycomb substrate prepared by the method as mentioned above. Secondly, holes are opened on the positions on this sheet which correspond to the cells on which plugging portions are to be formed. Secondly, the end face of the honeycomb substrate is immersed in a plugging slurry, which is a material for forming plugging portions in the form of a slurry, in the state that this sheet is attached, whereby the open ends of the cells to be plugged are filled with the plugging slurry through the holes opened on the sheet. The plugging slurry filled in this way is dried, and cured by firing, whereby the plugging portions are formed. As the material for forming the plugging portions, the same material as the material that forms the honeycomb substrate is preferably used. The plugging portions may be formed at any stage, after the drying of the honeycomb formed body, after the calcination or after the firing (main firing).

(37) Secondly, a slurry for forming a coat layer, which contains particles having a smaller average particle diameter than the average pore diameter of the circumferential wall of the honeycomb substrate prepared in this way, is prepared. As the particles to be incorporated in the slurry for forming a coat layer, inorganic particles of silicon carbide, silica, silicon nitride, cordierite, alumina, mullite, zirconia and the like are preferable, and particles containing Si such as silicon carbide and silica are especially preferable. Preferably the slurry for forming a coat layer contains, in addition to such particles, a bonding material capable of binding the particles to the inner surfaces of the pores of the circumferential wall, and is obtained by diluting those with water. Moreover, a dispersing agent and a defoaming agent may further be suitably incorporated in the slurry or forming a coat layer. As the bonding material, colloidal sols such as silica sol and alumina sol, and laminar compounds that show bonding property by swelling, and the like can be preferably used.

(38) A coat layer is disposed by applying such slurry for forming a coat layer onto the outer surface of the circumferential wall of the honeycomb substrate, and drying. When the slurry for forming a coat layer is applied, in order that a part of the slurry penetrates into the pores of the circumferential wall, and a thickness of the penetrated part is from 1 to 90% of the thickness of the circumferential wall, the control of the thickness of the penetrated part is carried out. For example, in the case when the slurry for forming a coat layer is applied by using a roller, the above-mentioned control can be conducted by the pressure in pressing the roller against the circumferential wall, the rotation number of the roller, and the like. In addition, the coat layer may also be disposed by applying a water repelling material, instead of the slurry for forming a coat layer, to the outer surface of the circumferential wall of the honeycomb substrate, and subjecting the water repelling material to a curing treatment by heating, irradiation with light, or the like. In this case, as the water repelling material, those containing Si such as silicone-based water repelling materials are preferable. Furthermore, in the case when the coat layer is disposed on a part of the outer surface of the circumferential wall, it is preferable to mask the part on which the coat layer is not to be formed on the outer surface of the circumferential wall with a tape or the like, and then apply the slurry for forming a coat layer or the water repelling material.

(39) By forming the coat layer on the outer surface of the circumferential wall of the honeycomb substrate in this way, the honeycomb structure of the present invention can be obtained. In the case when a catalyst is loaded on the honeycomb structure of the present invention, it is preferable to attach a catalyst slurry containing a catalyst such as a precious metal to the surface and pores of the partition wall by using a conventionally-known catalyst loading method such as an aspiration method, and subjecting the catalyst slurry to a high temperature treatment to bake the catalyst contained in the catalyst slurry on the partition wall.

EXAMPLES

(40) The present invention will further be explained below in more detail based on Examples, but the present invention is not construed to be limited to these Examples.

Examples 1 to 20 and Comparative Examples 1 and 2

(41) A pore former, a binder, a surfactant and water were added to a cordierite forming raw material containing talc, kaolin and alumina as major raw materials to prepare a forming raw material, and the forming raw material was kneaded in a vacuum pugmill to give a kneaded material. Starch was used as the pore former. Furthermore, methyl cellulose and hydroxypropoxymethyl cellulose were used as the binder. Sodium laurate was used as the surfactant. The addition amounts of the respective raw materials were 5 parts by mass of the pore former, 3 parts by mass of the methyl cellulose, 3 parts by mass of the hydroxypropoxymethyl cellulose, 1 part by mass of the surfactant, and 32 parts by mass of water with respect to 100 parts by mass of the cordierite forming raw material.

(42) The obtained kneaded material was subjected to extrusion molding by using a honeycomb body forming die, whereby pillar-shaped honeycomb formed bodies, each of which had a partition wall that had defined a plurality of cells extending from an inlet end face as an inlet side for a fluid to an outlet end face as an outlet side for the fluid, and a circumferential wall that had been formed monolithically with the partition wall, was obtained. Thereafter these honeycomb formed bodies were dried by microwave and hot air to give honeycomb dried forms.

(43) Subsequently, plugging portions were formed on one open ends of the respective cells of these honeycomb dried forms. The plugging portions were formed so that the respective end faces of each of the dried forms gave a checkerboard pattern by the cells having plugging portions formed on the open ends and the cells having no plugging portions formed on the open ends. The method for forming the plugging portions was as follows. Firstly, a sheet was attached to the end face of each of the dried forms, and holes were formed on the positions on this sheet which correspond to the cells on which plugging portions were to be formed. Secondly, the end face of each of the dried forms was immersed in a plugging slurry, which was a material for forming plugging portions in the form of a slurry, in the state that this sheet was attached, whereby the open ends of the cells to be plugged were filled with the plugging slurry through the holes formed on the sheet. As the material for forming the plugging portions, the same material as the above-mentioned forming raw material was used.

(44) The plugging slurry that was filled in the open ends of the cells in this way was dried, and these honeycomb dried forms were calcined (degreased) in an atmospheric atmosphere at about 400 C. The honeycomb dried forms were then fired at about 1,450 C., whereby honeycomb substrates each having a circumferential wall and a partition wall that were formed monolithically were obtained. The obtained honeycomb substrates each had a round pillar-shape having a diameter of 118.4 mm and a length of 127.0 mm, had cells each having a square shape, and the other structures were as shown in Table 1.

(45) Subsequently, 25 parts by mass of TiO.sub.2 and 25 parts by mass of SiC were added to 50 parts by mass of colloidal silica particles having an average particle diameter of 0.002 m, and thoroughly stirred to prepare a slurry for forming a coat layer. This slurry for forming a coat layer was applied in a band-like manner on the part other than the vicinities of the both end faces, of the outer surface of the circumferential wall of each of the honeycomb substrates. Each of the honeycomb substrates was then dried, and a coat layer such that the penetrated part and non-penetrated part had thicknesses of the values shown in Table 1 was disposed thereon. In this way, the honeycomb structures of Examples 1 to 20 and Comparative Examples 1 and 2 were obtained. The slurry for forming a coat layer was applied by using a roller, and the thicknesses of the penetrated part and non-penetrated part were controlled by the pressure for pressurizing the roller against the circumferential wall of each of the honeycomb substrates, the rotation number of the roller, and the like.

Examples 21 to 40 and Comparative Examples 3 and 4

(46) Kneaded materials obtained in a similar manner to that in the above-mentioned Examples 1 to 20 and Comparative Examples 1 and 2 were each subjected to extrusion molding by using a honeycomb body forming die to give honeycomb formed bodies each having a partition wall defining a plurality of cells that extend from an inlet end face as an inlet side for a fluid to an outlet end face as an outlet side for the fluid. Thereafter these honeycomb formed bodies were dried by microwave and hot air to give honeycomb dried forms.

(47) Secondly, one open end of each of the cells in these honeycomb dried forms was filled with a plugging slurry in a similar manner to that in the above-mentioned Examples 1 to 20 and Comparative Examples 1 and 2 to form plugging portions. The plugging slurry filled in the open ends of the cells was dried, and these honeycomb dried forms were calcined (degreased) under an atmospheric atmosphere at about 400 C. The honeycomb dried forms were then fired at about 1,450 C. to give honeycomb fired forms. Secondly, the circumferences of the honeycomb fired forms were subjected to grinding so that the outer shape of each honeycomb fired form became a round pillar-shape. After the grinding, a circumferential wall-forming material composed of the same material as the above-mentioned forming raw material was applied to the grinded surface and cured by drying at 700 C. for 2 hours to form a circumferential wall, whereby honeycomb substrates each having the circumferential wall and a partition wall that had been separately formed were obtained. The obtained honeycomb substrates each had a round pillar-shape having a diameter of 118.4 mm and a length of 127.0 mm and had square-shaped cells, and the other structures were as shown in Table 2.

(48) Subsequently, a slurry for forming a coat layer that was obtained in a similar manner to that in the above-mentioned Examples 1 to 20 and Comparative Examples 1 and 2 was applied in a band-like manner on the part other than the vicinities of the both end faces in the outer surface of the circumferential wall of each of the honeycomb substrates. Thereafter the honeycomb substrates were dried, and coat layers such that the thicknesses of the penetrate parts and non-penetrate parts became the values shown in Table 2 were disposed thereon to give the honeycomb structures of Examples 21 to 40 and Comparative Examples 3 and 4. The slurry for forming a coat layer was applied by using a roller, and the thicknesses of the penetrated part and non-penetrated part were controlled by the pressure for pressurizing the roller against the circumferential wall of each of the honeycomb substrates, the rotation number of the roller, and the like.

(49) TABLE-US-00001 TABLE 1 Coat layer Honeycomb substrate Thick- Rate of thick- Thick- Thickness Thickness ness of ness of pene- ness of Average of par- of circum- pene- trated part with non-pene- Form of Poros- pore tition Cell ferential Cell trated respect to thick- trated circumferential ity *1 diameter wall pitch wall density part ness of circum- part wall (%) (m) (m) (mm) (m) (cell/cm.sup.2) (m) ferential wall (%) (m) Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 4 ple 1 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 600 60.0 4 ple 2 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 100 10.0 4 ple 3 with partition wall Exam- Formed monolithically 50 20 305 1.47 1000 46.5 800 80.0 4 ple 4 with partition wall Exam- Formed monolithically 70 20 305 1.47 1000 46.5 800 80.0 4 ple 5 with partition wall Exam- Formed monolithically 50 10 305 1.47 1000 46.5 900 90.0 4 ple 6 with partition wall Exam- Formed monolithically 65 10 305 1.47 1000 46.5 800 80.0 4 ple 7 with partition wall Exam- Formed monolithically 65 20 305 1.47 700 46.5 560 80.0 4 ple 8 with partition wall Exam- Formed monolithically 65 20 254 1.47 600 46.5 480 80.0 4 ple 9 with partition wall Exam- Formed monolithically 65 20 241 1.64 400 37.2 320 80.0 4 ple 10 with partition wall Exam- Formed monolithically 65 20 203 1.34 400 55.8 320 80.0 4 ple 11 with partition wall Exam- Formed monolithically 65 20 203 1.47 400 46.5 320 80.0 4 ple 12 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 8 ple 13 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 15 ple 14 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 50 5.0 4 ple 15 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 70 ple 16 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 15 1.5 4 ple 17 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 30 ple 18 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 60 ple 19 with partition wall Exam- Formed monolithically 65 20 305 1.47 1000 46.5 800 80.0 75 ple 20 with partition wall Compar- Formed monolithically 65 20 305 1.47 1000 46.5 930 93.0 4 ative with partition wall Example 1 Compar- Formed monolithically 65 20 305 1.47 1000 46.5 5 0.5 4 ative with partition wall Example 2 *1: The porosity of the entirety of the honeycomb substrate (the partition wall and the circumferential wall)

(50) TABLE-US-00002 TABLE 2 Coat layer Honeycomb substrate Thick- Rate of thick- Thick- Porosity Porosity Thickness Thickness ness of ness of pene- ness of of circum- of par- Average of par- of circum- pene- trated part with non-pene- Form of ferential tition pore tition Cell ferential Cell trated respect to thick- trated circumferential wall wall diameter wall pitch wall density part ness of circum- part wall (%) (%) (m) (m) (mm) (m) (cell/cm.sup.2) (m) ferential wall (%) (m) Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1600 80.0 4 ple 21 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1000 50.0 4 ple 22 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 400 20.0 4 ple 23 from partition wall Exam- Formed separately 40 40 20 305 1.47 2000 46.5 1600 80.0 4 ple 24 from partition wall Exam- Formed separately 40 70 20 305 1.47 2000 46.5 1600 80.0 4 ple 25 from partition wall Exam- Formed separately 40 50 15 305 1.47 2000 46.5 1600 80.0 4 ple 26 from partition wall Exam- Formed separately 40 40 10 305 1.47 2000 46.5 1600 80.0 4 ple 27 from partition wall Exam- Formed separately 40 65 20 305 1.47 1400 46.5 1120 80.0 4 ple 28 from partition wall Exam- Formed separately 40 65 20 254 1.47 1800 46.5 1440 80.0 4 ple 29 from partition wall Exam- Formed separately 40 65 20 241 1.64 1000 37.2 800 80.0 4 ple 30 from partition wall Exam- Formed separately 40 65 20 203 1.34 1000 55.8 800 80.0 4 ple 31 from partition wall Exam- Formed separately 40 65 20 203 1.47 1000 46.5 800 80.0 4 ple 32 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1600 80.0 10 ple 33 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1600 80.0 50 ple 34 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1600 80.0 70 ple 35 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1600 80.0 75 ple 36 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 1000 50.0 4 ple 37 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 400 20.0 4 ple 38 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 200 10.0 4 ple 39 from partition wall Exam- Formed separately 40 65 20 305 1.47 2000 46.5 100 5.0 4 ple 40 from partition wall Compar- Formed separately 40 65 20 305 1.47 2000 46.5 1860 93.0 4 ative from partition wall Example 3 Compar- Formed separately 40 65 20 305 1.47 2000 46.5 10 0.5 4 ative from partition wall Example 4

(51) (Evaluation)

(52) For the honeycomb structures of Examples 1 to 40 and Comparative Examples 1 to 4, an effect for preventing the exuding of the catalyst slurry, an exhaust gas purifying performance, the presence or absence of cracks on the coat layer and the strength of the circumferential wall were evaluated by the following methods, and the results thereof were shown in Tables 3 and 4.

(53) [Effect for Preventing Exuding of Catalyst Slurry]

(54) 1,200 parts by mass of Al.sub.2O.sub.3, 300 parts by mass of CeO.sub.2, 1 part by mass of Pt and 15,000 parts by mass of water were mixed, and the mixture was subjected to wet pulverization to prepare a catalyst slurry having a viscosity of about 2 mPa.Math.s. The inlet end face of the honeycomb structure was immersed in the catalyst slurry in the state that the parts in the vicinities of the both end faces of the honeycomb structure (the parts on which the coat layer was not disposed) were chucked. The catalyst slurry was introduced into the cells with aspiration from the outlet end face, whereby the catalyst slurry was attached to the partition wall. Furthermore, the upper and lower surfaces of the honeycomb structure were reversed, and the outlet end face of the honeycomb structure was immersed in the catalyst slurry, and the catalyst slurry was introduced into the cells with aspiration from the inlet end face, whereby the catalyst slurry was attached to the partition wall. Furthermore, whether or not the catalyst slurry had exuded on the outer surface of the circumferential wall of the honeycomb structure when the catalyst slurry was introduced into the cell with aspiration in this way was examined. As to results of the examination, the case when the catalyst slurry, including the water contained in the catalyst slurry, did not exude was deemed as excellent, the case when only the water contained in the catalyst slurry exuded was deemed as acceptable, and the case when Al.sub.2O.sub.3 and CeO.sub.2, which are the components of the catalyst slurry, exuded was deemed as not acceptable.

(55) (Exhaust Gas Purification Performance)

(56) The catalyst slurry that had been attached to the partition wall of the honeycomb structure as mentioned above was dried at 120 C. for 2 hours and heated at 550 C. for 1 hour to bake the catalyst contained in the catalyst slurry on the partition wall. Furthermore, honeycomb structures on which a coat layer had not been disposed were prepared in similar manners to those in Examples 1 to 40 and Comparative Examples 1 to 4, except that a coat layer was not disposed, and a catalyst was baked on the partition wall in a similar manner. In this way, a catalyst was loaded on each of the honeycomb structures of Examples 1 to 40 and Comparative Examples 1 to 4 on which a coat layer had been disposed, and on each of the honeycomb structures that were similar to those of Examples 1 to 40 and Comparative Examples 1 to 4 except that a coat layer was not disposed. A purification rate when each of these honeycomb structures purifies NO contained in an exhaust gas in running at a NEDC mode by a direct injection type gasoline engine of stoichiometric combustion at a displacement of 1.4 L was measured. Furthermore, the case when the purification rate of NO of the honeycomb structure on which a coat layer had been disposed was 90% or more of the purification rate of NO of the honeycomb structure on which a coat layer had not been disposed was deemed as excellent. Furthermore, the case when the purification rate of NO of the honeycomb structure on which a coat layer had been disposed was lower than 90% of the purification rate of NO of the honeycomb structure on which a coat layer had not been disposed was deemed as not acceptable.

(57) (Presence or Absence of Cracks on Coat Layer)

(58) The coat layer of the honeycomb structure was observed by visual observation, and the presence or absence of cracks was examined. Furthermore, the case when cracks were absent on the coat layer was deemed as excellent, and the case when the presence of cracks on the coat layer was confirmed, but the cracks did not extend to the honeycomb substrate was deemed as acceptable.

(59) (Strength of Circumferential Wall)

(60) The strength of the circumferential wall of each of the honeycomb structures of Examples 1 to 40 and Comparative Examples 1 to 4 before the coat layer was disposed, and the strength of the circumferential wall of each of the honeycomb structures of Examples 1 to 40 and Comparative Examples 1 to 4 after the coat layer had been disposed were measured. The strength of the circumferential wall was measured, by such a method that a spherical weight made of alumina was vertically dropped on the circumferential wall of the honeycomb structure. Specifically, the dropping was repeated with changing the weight of the weight and the dropping distance, until breakage occurred on the circumferential wall of the honeycomb structure by the impact of the dropping of the weight, and an impact energy was calculated from the weight of the weight and the dropping distance when breakage occurred on the circumferential wall, and deemed as the strength of the circumferential wall.

(61) TABLE-US-00003 TABLE 3 Strength of circumferential wall Effect of Presence or (N .Math. m) preventing Exhaust gas absence of Before exuding of catalyst purifying cracks on coat disposition of After disposition slurry performance layer coat layer of coat layer Example 1 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 2 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 3 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 4 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 5 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 6 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 7 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 8 Excellent Excellent Excellent 8.29 10.sup.4 9.11 10.sup.4 Example 9 Excellent Excellent Excellent 5.79 10.sup.4 6.37 10.sup.4 Example 10 Excellent Excellent Excellent 2.25 10.sup.4 2.48 10.sup.4 Example 11 Excellent Excellent Excellent 2.25 10.sup.4 2.48 10.sup.4 Example 12 Excellent Excellent Excellent 2.25 10.sup.4 2.48 10.sup.4 Example 13 Excellent Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 14 Excellent Excellent Acceptable 1.90 10.sup.3 2.09 10.sup.3 Example 15 Acceptable Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 16 Excellent Excellent Acceptable 1.90 10.sup.3 2.09 10.sup.3 Example 17 Acceptable Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 18 Excellent Excellent Acceptable 1.90 10.sup.3 2.09 10.sup.3 Example 19 Excellent Excellent Acceptable 1.90 10.sup.3 2.09 10.sup.3 Example 20 Excellent Excellent Acceptable 1.90 10.sup.3 2.09 10.sup.3 Comparative Excellent Not acceptable Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 1 Comparative Not acceptable Excellent Excellent 1.90 10.sup.3 2.09 10.sup.3 Example 2

(62) TABLE-US-00004 TABLE 4 Strength of circumferential wall Effect of Presence or (N .Math. m) preventing Exhaust gas absence of Before exuding of catalyst purifying cracks on coat disposition of After disposition slurry performance layer coat layer of coat layer Example 21 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 22 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 23 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 24 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 25 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 26 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 27 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 28 Excellent Excellent Excellent 1.18 10.sup.2 1.30 10.sup.2 Example 29 Excellent Excellent Excellent 1.51 10.sup.2 1.66 10.sup.2 Example 30 Excellent Excellent Excellent 9.53 10.sup.3 1.05 10.sup.2 Example 31 Excellent Excellent Excellent 9.53 10.sup.3 1.05 10.sup.2 Example 32 Excellent Excellent Excellent 9.53 10.sup.3 1.05 10.sup.2 Example 33 Excellent Excellent Acceptable 1.72 10.sup.2 1.89 10.sup.2 Example 34 Excellent Excellent Acceptable 1.72 10.sup.2 1.89 10.sup.2 Example 35 Excellent Excellent Acceptable 1.72 10.sup.2 1.89 10.sup.2 Example 36 Excellent Excellent Acceptable 1.72 10.sup.2 1.89 10.sup.2 Example 37 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 38 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 39 Excellent Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Example 40 Acceptable Excellent Excellent 1.72 10.sup.2 1.89 10.sup.2 Comparative Excellent Not acceptable Excellent 2.72 10.sup.2 2.99 10.sup.2 Example 3 Comparative Not acceptable Excellent Excellent 2.72 10.sup.2 2.99 10.sup.2 Example 4

(63) (Discussion)

(64) The strength of the circumferential wall was higher after the coat layer had been disposed than the strength before the disposition of the coat layer, in either of the honeycomb structures of Examples 1 to 40 and Comparative Examples 1 to 4. Furthermore, in the honeycomb structures of Examples 1 to 40, the effect of preventing the exuding of the catalyst slurry was excellent or acceptable, and the exhaust gas purification performance was excellent. In addition, in the honeycomb structures of Examples 14, 16, 18 to 20 and 33 to 36, cracks generated on the coat layer, but either of the effect of preventing the exuding of the catalyst slurry and the exhaust gas purification performance was excellent. The reason therefor is considered that the cracks generated on the coat layer were so slight that they did not extend to the honeycomb substrate. On the other hand, in the honeycomb structures of Comparative Examples 2 and 4 in which the thickness of the penetrated part of the coat layer was lower than 1% of the thickness of the circumferential wall, the effect of preventing the exuding of the catalyst slurry was not acceptable. The reason therefor is considered that, since the thickness of the penetrated part of the coat layer was too thin, the pores of the circumferential wall were occluded incompletely, and thus the exuding of the catalyst slurry was not able to be sufficiently prevented. Furthermore, in the honeycomb structures of Comparative Examples 1 and 3 in which the thickness of the penetrated part of the coat layer was more than 90% of the thickness of the circumferential wall, the exhaust gas purifying performance was not acceptable. The reason therefor is considered that, since the thickness of the penetrated part of the coat layer was too thick, the coat layer penetrated into the pores of the partition wall, and thus the loading of the catalyst in the pores of the partition wall in the penetrated part was disturbed.

(65) The present invention can be preferably used in filters for trapping particulate matters contained in exhaust gases from diesel engines and gasoline engines, and the like, especially in filters for which loading of a catalyst is required, and the like.

DESCRIPTION OF REFERENCE NUMERALS

(66) 1: honeycomb structure, 2: honeycomb substrate, 3: coat layer, 4: partition wall, 5: cell, 6: circumferential wall, 7: pore, 8: particle, 9: plugging portion, 11: inlet end face, 12: outlet end face.