WO1998005602A1 - Ceramique nid d'abeille et procede de fabrication - Google Patents
Ceramique nid d'abeille et procede de fabrication Download PDFInfo
- Publication number
- WO1998005602A1 WO1998005602A1 PCT/JP1997/002767 JP9702767W WO9805602A1 WO 1998005602 A1 WO1998005602 A1 WO 1998005602A1 JP 9702767 W JP9702767 W JP 9702767W WO 9805602 A1 WO9805602 A1 WO 9805602A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- honeycomb structure
- ceramic honeycomb
- partition
- partition wall
- slit portion
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B3/00—Producing shaped articles from the material by using presses; Presses specially adapted therefor
- B28B3/20—Producing shaped articles from the material by using presses; Presses specially adapted therefor wherein the material is extruded
- B28B3/26—Extrusion dies
- B28B3/269—For multi-channeled structures, e.g. honeycomb structures
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
- C04B38/0006—Honeycomb structures
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/00793—Uses not provided for elsewhere in C04B2111/00 as filters or diaphragms
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/0081—Uses not provided for elsewhere in C04B2111/00 as catalysts or catalyst carriers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
Definitions
- the present invention relates to a ceramic honeycomb structure (hereinafter, simply referred to as a honeycomb structure) and a method for producing the same, and particularly to a ceramic honeycomb structure used for a catalyst carrier for an internal combustion engine, a filter, and the like. And its manufacturing method.
- a honeycomb structure hereinafter, simply referred to as a honeycomb structure
- a method for producing the same and particularly to a ceramic honeycomb structure used for a catalyst carrier for an internal combustion engine, a filter, and the like. And its manufacturing method.
- the present invention has been made in view of the above problems, and has a feature of obtaining a honeycomb structure in which chipping is suppressed even in a honeycomb structure having a small partition wall thickness. Things. Disclosure of the invention
- the honeycomb structure is formed at the outlet of the dryer at the time of removing work from the dryer.
- the honeycomb structure while dragging it from the dryer belt), dragging during transfer, holding condition when cutting the end face, and firing of the honeycomb carrier when firing to form the honeycomb structure External force is applied when moving the furnace in and out.
- the conventional honeycomb structure has a structure that withstands an external impact by dispersing the force by microscopically missing around the peripheral wall.
- the honeycomb structure 80 having a very small wall thickness as shown in FIG. 1 when a force is applied from the inside to the outside with respect to the partition wall and the peripheral wall, the microstructure of the formed peripheral wall is generated. It was found that a large gap 8 2 could be triggered by a lack of quality. This is because, when the partition wall is thick as in the past, the contact width between the peripheral wall and the partition wall is large and the joint strength is sufficient due to the force that peels off the outer peripheral wall. I have.
- the partition wall is extremely thin, particularly when the partition wall is 0.13 mm or less, the contact width between the peripheral wall and the partition wall is small, so that the force applied from the inside of the honeycomb structure to the outside is reduced. They found that it was so weak that chipping would occur.
- Figure 2 shows the relationship between the partition wall thickness and the state of chipping. As is evident from Fig. 2, when the partition wall thickness is 0.13 mm or less, the occurrence of edge chipping sharply increases.
- the average thickness of the peripheral wall is larger than the average thickness T (mm) of the bulkhead, and the relationship between the average thickness T of the bulkhead and the average contact width w (mm) of the bulkhead of the bulkhead is:
- the contact width between the peripheral wall and the partition wall can be made sufficiently large, the force can be extremely increased against the force from the inside to the outside of the honeycomb structure, and the occurrence of edge chipping can be suppressed.
- a rounded corner is formed in the partition at a junction of the partition with the peripheral wall.
- the contact area can be increased without lowering the pressure loss, and in particular, the occurrence of edge chipping can be suppressed.
- the radius portion not only the edge chipping can be simply suppressed, but also the entire weight of the ceramic honeycomb structure that can widen the partition wall and the peripheral wall as a whole.
- the chipping between the peripheral wall and the partition wall can be suppressed without increasing the thickness.
- the average radius of the rounded portion is preferably in the range of 0.06 to 0.30 mm, thereby further suppressing chipping.
- the porosity of the honeycomb structure is preferably larger than 30%.
- the porosity is less than 30%, it is not possible to secure a sufficient amount of the catalyst carried on the ceramic honeycomb structure.
- a taper portion is formed in a boundary region between the partition and the partition reinforcing portion.
- a round portion may be formed between the peripheral wall and the partition wall reinforcing portion.
- the average radius of the radius portion is 0.06 mm to 0.3 O mm.
- the porosity of the honeycomb structure is preferably larger than 30%.
- the thickness of the peripheral wall of the ceramic structure is preferably 1.1 mm or less.
- the thickness of the peripheral wall is more than 1.1 mm, a honeycomb structure having good thermal shock resistance cannot be obtained.
- a region width of the partition reinforcing portion from the peripheral wall is substantially uniform.
- the peripheral wall includes By passing an abrasive through the initial slit portion while gradually shifting the mask smaller toward the center, a rounded portion is formed at the joint between the peripheral wall and the partition wall.
- an initial slit portion having a width larger than a predetermined width in the mold at least a slit portion corresponding to a boundary region between the partition and the partition reinforcing portion.
- a plating layer is formed on the surface of the initial slit portion by passing a plating liquid through the initial slit portion of the mold with a space provided between the mold and the mask.
- the slit portion having a desired width is formed, and in the slit portion where a space is provided between the slit portion and the mask, the circulation of the plating liquid is restricted, whereby the slit portion is restricted.
- the thickness of the knuckle changes, and accordingly, the slit width of the extrusion die, which gradually changes, passes through the slit portion of the extrusion die, whereby the ceramic having the partition wall reinforcing portion is formed.
- a honeycomb structure can be easily obtained.
- FIG. 1 is an explanatory diagram for explaining a chipped edge of a conventional honeycomb structure.
- FIG. 3A is an overall view of the honeycomb structure of the first embodiment
- FIG. 3B is a partially enlarged view of an end face of the honeycomb structure of the first embodiment.
- Fig. 4 is a relational diagram showing the distribution of occurrence of edge chipping when the partition wall thickness and the average contact width are changed.
- Figure 5 is a relationship diagram showing the relationship between the average radius of the radius and the incidence of edge chipping.
- FIG. 6 is an explanatory diagram showing an effect when a round portion is formed.
- FIG. 7 is a relationship diagram showing the relationship between the porosity and the amount of supported catalyst.
- FIG. 8 is a relationship diagram showing the relationship between the peripheral wall thickness and the thermal shock resistance.
- FIG. 9 is a partially enlarged view of an end face of the honeycomb structure of the second embodiment.
- Figure 10 shows the relationship between the width of the partition wall reinforcement and the rate of edge chipping. Engagement diagram.
- FIG. 11 is an explanatory diagram for explaining the width of the partition wall reinforcing portion.
- Figure 12 shows the relationship between the width of the partition wall and the pressure loss.
- FIGS. 13 to 15 are explanatory diagrams showing another embodiment of the present invention.
- FIG. 16 is an explanatory view for explaining a method for producing a mold according to the present invention.
- FIG. 17 is a schematic view of the mold of the present invention.
- FIG. 18 is an explanatory diagram for explaining a method for producing a mold according to the present invention.
- FIG. 3A and 3B show the configuration of the honeycomb structure of the present invention.
- FIG. 3A is an overall view of the honeycomb structure 1 of the present invention
- FIG. 3B is a partially enlarged view of an end face of the honeycomb structure 1 of the present invention.
- the honeycomb structure 1 of the present invention has a cylindrical shape and is made of a cordierite material obtained by firing kaolin, talc, alumina, or the like.
- the honeycomb structure has a porosity of 35%, in which the partition wall 3 and the peripheral wall 5 are integrally formed by extrusion.
- the honeycomb structure includes a partition wall 3 and a peripheral wall 5 that covers the periphery of the partition wall 3.
- the partition walls 3 form adjacent flow channels 7 having a rectangular cross section, and have an average thickness of 0.104 mm.
- peripheral wall 5 is formed integrally with the partition wall 3 and integrally holds the partition wall 3 from the outer periphery, and has an average thickness of 0.65 mm.
- the partition wall is formed.
- the feature is that the contact width w at the joint 9 of FIG. 3 is set to 0.3 mm or more, which is larger than the average thickness of the partition wall 3.
- the honeycomb structure can be strengthened against the force applied from the inside to the outside of the honeycomb structure, so that it is possible to obtain a honeycomb structure in which the occurrence of edge chipping is suppressed.
- the contact width w between the partition wall 3 and the peripheral wall 5 is simply increased, the pressure loss of the honeycomb structure itself is reduced. In addition to this, the heat capacity hardly increases, so that a good early activity can be obtained even when a catalyst is supported.
- the porosity is 35%, and the occurrence of chipping can be suppressed while ensuring the catalyst supporting property of the honeycomb structure 1.
- honeycomb structure 1 Next, a method for manufacturing the above-described honeycomb structure 1 will be described. First, kaolin, talc, alumina, and the like are classified to obtain an appropriate particle size distribution.
- kaolin with an average particle size of 5 m and kaolin with 0.5 ⁇ m in total are 44 to 50%
- talc with an average particle size of 8 ⁇ m is 35 to 41%.
- a mixture of 13 to 19% of aluminum hydroxide having a diameter of 1.2 ⁇ m and a balance of aluminum is made to have a chemical composition of cordierite after firing. Most of these raw materials use natural products. Naturally, the composition of kaolin, talc, and alumina varies depending on the place of production. Therefore, the raw material composition is analyzed each time and converted into a code. The mixing ratio is changed so as to obtain a chemical composition.
- This clay is formed into a rod shape using a screw molding machine or another molding machine, and then extruded through a extrusion molding machine to form a honeycomb carrier, which is a honeycomb structure before firing, through a extrusion molding machine. I do.
- the formed honeycomb carrier is placed in a dryer, uniformly heated to evaporate water, cut into a prescribed size, placed in a continuous furnace, and fired at 135 ° C to 144 ° C for 5 hours. By doing so, the honeycomb structure 1 of the present invention can be obtained.
- This honeycomb structure 1 has a partition wall 3 having a diameter of 103 mm, a length of 150 mm and a porosity of 35% forming a flow path 7 of 400 mesh.
- Figure 4 shows the relationship between the thickness T of each partition 3 and the average contact width w.
- the occurrence rate of edge chipping was defined as ⁇ when the rate of occurrence of edge chipping was 5% or less from among those obtained by firing each of 70 honeycomb carriers before firing. When it was larger than%, it was indicated as X.
- a carrier in which a defect of 10 mm or more in the circumferential direction or in the longitudinal direction occurred was counted as marginal chipping occurrence.
- the contact width w is preferably 0.7 mm or less.
- Fig. 5 shows the relationship between the average radius and the incidence rate of the chipping rate.
- the rate of occurrence of edge chipping was obtained by the same method as the rate of occurrence of edge chipping in Fig. 4.
- the average radius of the round portion is preferably 0.06 mm or more.
- the average radius of the radius is 0.06 to 0.30 mm is preferred.
- the honeycomb structure is chipped due to a force acting from the outside to the inside, a bending force is generated in the partition wall supporting the peripheral wall and the partition wall is similarly formed as described above. Likely to happen.
- the pseudo-dome shape D is formed together with the radius of the contact part, so that it is easy to support external force and the occurrence of chipping is suppressed. be able to.
- FIG. 7 shows the relationship between the porosity of the honeycomb structure and the amount of supported catalyst.
- the honeycomb structure at this time had a partition wall thickness of 0.104 mm and a peripheral wall thickness of 0.65 mm.
- the supported amount of the catalyst can also be increased.
- the desired amount of the supported catalyst can be increased. Of 14 wt% was obtained.
- Fig. 8 shows the relationship between the thickness of the peripheral wall and the thermal shock resistance.
- the impact resistance is as follows: After heating for 1 hour at the set temperature, bring the temperature to room temperature within 1 minute. Then, it was cooled in the air at room temperature as it was, and it was confirmed whether or not cracks occurred.
- the partition wall thickness was 0.104 mm and the porosity was 35%.
- thermal shock resistance of more than 65 ° C, thermal stress damage due to rapid heating and cooling by exhaust gas and raw gas from the engine is prevented. Can be stopped.
- the contact width w of the joint 9 between the partition wall 3 and the peripheral wall 5 is not made larger than the thickness of the partition wall 3, but the thickness of the partition wall 3 is changed. It is characterized in that the contact area between the partition wall 3 and the peripheral wall 5 is increased by increasing the height in a certain area.
- FIG. 9 shows a partially enlarged view of an end face of the honeycomb structure 10 of the second embodiment.
- the honeycomb structure 10 of the second embodiment has a substantially circular cross section in a direction perpendicular to the flow path direction. ing.
- the thickness is larger than the average thickness of the partition walls 3.
- a 0.2 mm thick partition wall 12 is formed.
- the boundary area A which is the area width between the partition wall reinforcing portion 12 and the partition wall 3, is substantially uniform over the entire circumference.
- the boundary region A between the partition wall 3 and the partition wall reinforcing portion 12 is continuously and integrally formed by a tapered portion 14 formed in one cell.
- a round portion having an average radius of 0.3 mm is formed as in the honeycomb structure of the first embodiment.
- the contact area between the partition wall 3 and the peripheral wall 5 can be largely secured by the partition wall reinforcing portion 12, and the partition wall reinforcing portion 12 can strengthen against the force applied from the inside to the outside of the honeycomb structure.
- a honeycomb structure in which chipping is suppressed can be obtained.
- the partition wall reinforcing portion 12 is newly formed, the occurrence of chipping can be further suppressed as compared with the honeycomb structure of the first embodiment. Thus, it is possible to improve the shape retention of the honeycomb structure and maintain the dimensional accuracy.
- a tapered portion 14 is provided in a boundary region between the partition wall 3 and the partition wall reinforcing portion 12, for example, when the honeycomb structure is used as a catalyst support for an internal combustion engine, the honeycomb structure Receives high heat due to the exhaust gas of the internal combustion engine, and at that time cracks occur due to thermal expansion due to the difference in thickness between the two, and cracks occur due to thermal expansion in the tapered portion 24. Can be suppressed.
- the tapered portion 14 reduces the change in the flow velocity, and the generation of the shear distortion of the partition 3 can also be suppressed.
- the tapered portion 14 is provided in a range of about one flow path, the flow velocity of the clay at the time of molding is alleviated, and the occurrence of distortion of the partition walls can be suppressed.
- the width of the partition wall reinforcing portion may be set to 2 to 3% of the distance from the peripheral wall 5 to the center of the honeycomb structure, and the tapered portion 14 may be provided.
- a taper may be formed over the range of the plurality of flow paths. By forming the taper over the range of the plurality of flow paths, the flow velocity can be further uniformed.
- the size of the contact width w between the partition wall reinforcing portion 12 and the peripheral wall is not preferable if it is longer than the length of one side of the opening, since the effective cross-sectional area of the cell is greatly impaired.
- FIG. 10 shows the relationship between the length of the partition wall reinforcing portion 12 and the incidence of edge chipping.
- the thickness of the partition wall reinforcing section 12 is fixed at 0.15 mm, the partition wall thickness is 0.104 mm, and the radius of the radius section is 0.1 mm. Further, a honeycomb structure having a porosity of 35% was used.
- the width of the partition wall reinforcing portion 12 occupies the width (1) of the partition wall reinforcing portion 12 in the distance (L) from the peripheral wall 5 to the center of the honeycomb structure 10. Shown in percentage.
- the width (1) of the partition wall reinforcing portion 12 is equal to the distance (L) from the peripheral wall 5 to the center of the honeycomb structure 10. It can be seen that by setting it to 2% or more, the incidence of edge chipping can be rapidly suppressed.
- the width (1) of the partition reinforcing portion 12 is, the lower the occurrence of edge chipping can be, but the greater the pressure loss of the honeycomb structure becomes, the larger the partition loss becomes.
- the width (1) of the reinforcing portion 12 cannot be made larger than necessary.
- Fig. 12 shows the relationship between the pressure loss and the width of the partition wall reinforcement section 22.
- the honeycomb structure used had a partition wall reinforcement section thickness of 0.3 mm and a partition wall thickness of 0.1. 0.4 mm, the radius of the radius is 0.1 mm, the porosity is 35%, and a 400-mesh, diameter of 103 mm was used.
- the rotation speed of the internal combustion engine was set at 400 rpm.
- the width of the partition wall reinforcing portion is a ratio of the width (1) of the partition wall reinforcing portion 12 to the distance (L) from the peripheral wall 5 to the center of the honeycomb structure 10. Indicated.
- the width (1) of the partition wall reinforcing portion 12 is 15% or more of the distance (L) from the peripheral wall 5 to the center of the honeycomb structure, the pressure loss is reduced. 7.8 kPa or more.
- the width of the partition wall reinforcing portion is preferably from 1.2% to 15% with respect to the distance from the peripheral wall 5 to the center of the honeycomb structure. You can see that.
- the shapes of the honeycomb structures shown in the first and second embodiments are determined by passing the slurry through the slit portion formed in the extrusion die.
- the flow paths of the honeycomb structures 20 and 30 as shown in FIGS. 13 and 14 may be used.
- the partition wall thickness (T) is 0.15 mm and the average contact width (w) is 0.25 mm.
- the partition wall reinforcing part 31 (thickness t) is included. It can also take a different structure.
- the flow channel according to the present invention has a honeycomb structure having a communicating portion 42 and a defective portion 46 in which a part of the peripheral wall 44 is missing, as shown in FIG. It may be 40.
- a method for manufacturing a mold for obtaining a honeycomb structure having a rounded portion formed in a contact portion or a partitioning portion as described in the present invention is provided. Therefore, the following two methods are preferred.
- a desired width of the slit is obtained by performing a method of forming the desired width of the slit, and performing surface treatment such as plating. There are two ways to do it.
- the first method only a thickness smaller than a desired thickness is formed in advance in a slit region of a mold corresponding to a portion where a partition wall, a partition wall reinforcing portion, and the like of the mold 50 are formed.
- the initial slit portion 52 is formed by, for example, a grinding wheel, electric discharge machining or the like.
- polishing clay (not shown) is passed through the slit portion 56.
- this polishing clay is obtained by mixing abrasive powder into a resin having high viscosity.
- the polishing clay is initialized.
- the slit width of the initial slit portion 52 and the slit portion 56 is gradually increased through the slit portion 52 and the flow path 56 that has not been masked.
- the slit portion which is not masked from the beginning is formed into a slit having a larger width, and the slit portion which is formed by removing the mask force in a later process becomes smaller.
- a slit portion having a width is formed.
- the change in the slit width is continuously changed as shown in Fig. 17 by slightly shifting the mask by 1/2 to 1 Z4 of one slit part using the mask.
- a mold 60 having a slit portion 58 having a slit width that varies can be obtained.
- the polishing clay is passed through the slit portions 52 and 56 over the entire surface to form a slit portion having a desired width and shape.
- a slit portion corresponding to a boundary portion between the peripheral wall of the mold and the partition wall reinforcing portion is first processed, and a slit portion corresponding to a boundary region A between the partition wall 3 and the partition wall reinforcing portion 12 is formed.
- a slit portion corresponding to a boundary region A between the partition wall 3 and the partition wall reinforcing portion 12 is formed.
- molds corresponding to the honeycomb structures 1 and 10 having the round portion and the taper portion 14 as in the first and second embodiments can be easily obtained. be able to.
- the slit portion is polished with almost the same polishing clay, the internal surface roughness of the tapered slit portion is reduced.
- the surface roughness can be made substantially uniform, and the difference in the flow velocity of clay between the slit portion corresponding to the partition wall 3 and the slit portion corresponding to the partition wall reinforcing portion 12 is also reduced. Can be.
- the slit portion 72 a corresponding to the peripheral wall and the slit portion 72 b corresponding to the partition wall reinforcing portion are masked by a Teflon tape 74 serving as a mask. Apply a surface treatment.
- a space 7 is provided between the slit portion and the teflon tape 74. 8 will be provided.
- a plating solution (not shown) is passed through the slit portions 76a and 76b.
- a plating layer (not shown) is formed only in the slit portion 76b through which the plating liquid has passed, and by the formation of the plating layer, the plating layer 76b is formed.
- the width becomes narrow.
- the space portion 78 serves as an obstruction plate against the inflow of the plating solution, and Does not turn enough.
- the width of the slit portion 76a corresponding to the space portion 78 of the Teflon tape 74 is the slit portion 76 not covered by the Teflon tape 74. It is possible to obtain a mold that can be gradually increased with respect to the width of b.
- the space portion 78 is provided between the slit portion and the Teflon tape 74 in the same manner. It is possible to obtain a mold with a gradually reduced slot width.
- the surface treatment including the boundary between the outer peripheral reinforcing cell and the inner cell is performed first, and the surface treatment including the boundary between the outer peripheral wall and the outer peripheral cell is performed later.
- Teflon tape is used as the mask.
- the mask is not limited to Teflon tape.
- a vinyl chloride type may be used.
- the former requires a long time for mold finishing, but has a long mold life and is suitable for mass production.
- the latter has a short mold life instead of a short mold production time. Suitable for small prototypes.
- the present invention can provide a honeycomb structure that can sufficiently suppress the occurrence of edge chipping even with a very thin partition wall.
- a honeycomb structure having a rectangular cross section is employed.
- the cross section of the flow path is not limited to a rectangular cross section.
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- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Press-Shaping Or Shaping Using Conveyers (AREA)
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Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10507820A JP3060539B2 (ja) | 1996-08-07 | 1997-08-07 | セラミックハニカム構造体およびその製造方法 |
US09/051,232 US5952079A (en) | 1996-08-07 | 1997-08-07 | Ceramic honeycomb structure and method of production thereof |
EP97934733A EP0854123B1 (en) | 1996-08-07 | 1997-08-07 | Ceramic honeycomb structure and method of production thereof |
DE69735618T DE69735618T2 (de) | 1996-08-07 | 1997-08-07 | Keramische wabenstruktur und verfahren zu deren herstellung |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20808296 | 1996-08-07 | ||
JP8/208082 | 1996-08-07 |
Publications (1)
Publication Number | Publication Date |
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WO1998005602A1 true WO1998005602A1 (fr) | 1998-02-12 |
Family
ID=16550352
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP1997/002767 WO1998005602A1 (fr) | 1996-08-07 | 1997-08-07 | Ceramique nid d'abeille et procede de fabrication |
Country Status (5)
Country | Link |
---|---|
US (1) | US5952079A (ja) |
EP (1) | EP0854123B1 (ja) |
JP (1) | JP3060539B2 (ja) |
DE (1) | DE69735618T2 (ja) |
WO (1) | WO1998005602A1 (ja) |
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JP2000225340A (ja) * | 1998-11-30 | 2000-08-15 | Denso Corp | ハニカム構造体 |
JP2003025316A (ja) * | 2001-07-13 | 2003-01-29 | Ngk Insulators Ltd | ハニカム構造体、及びその製造方法 |
JP2003523282A (ja) * | 2000-02-21 | 2003-08-05 | エグゼキア | 多チャンネル要素およびその製造法 |
JPWO2004024295A1 (ja) * | 2002-09-13 | 2006-01-05 | イビデン株式会社 | ハニカム構造体 |
JP2007524030A (ja) * | 2003-12-24 | 2007-08-23 | サン−ゴバン・サントル デゥ ルシェルシュ エ デチューデ・ウロペアン | 内燃機関の排気ガス中に存在する微粒子をろ過するためのブロック |
US7318954B2 (en) | 2004-02-19 | 2008-01-15 | Ngk Insulators, Ltd. | Honeycomb structure |
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US7803447B2 (en) | 2001-08-30 | 2010-09-28 | Ngk Insulators Ltd. | High strength honeycomb structure, method of molding the same, and honeycomb structure converter |
US7989047B2 (en) * | 2005-12-27 | 2011-08-02 | Denso Corporation | Hexagonal-cell honeycomb structure |
WO2013008788A1 (ja) * | 2011-07-12 | 2013-01-17 | 住友化学株式会社 | ハニカム構造体 |
WO2019232148A1 (en) * | 2018-05-31 | 2019-12-05 | Corning Incorporated | Honeycomb bodies with honeycomb structure strengthening features and extrusion dies therefor |
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DE60041464D1 (de) * | 1999-09-29 | 2009-03-12 | Ibiden Co Ltd | Wabenförmiger Filter und Anordnung von keramischen Filtern |
DE10024038A1 (de) * | 2000-05-13 | 2001-11-22 | Dmc2 Degussa Metals Catalysts | Wabenkörper aus einem keramischen Material mit verbesserter radialer Druckfestigkeit |
JP4548968B2 (ja) * | 2000-06-05 | 2010-09-22 | 株式会社日本自動車部品総合研究所 | セラミック担体およびセラミック触媒体 |
US6656564B2 (en) * | 2000-08-03 | 2003-12-02 | Ngk Insulators, Ltd. | Ceramic honeycomb structure |
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Cited By (18)
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JP2000225340A (ja) * | 1998-11-30 | 2000-08-15 | Denso Corp | ハニカム構造体 |
JP2003523282A (ja) * | 2000-02-21 | 2003-08-05 | エグゼキア | 多チャンネル要素およびその製造法 |
JP2003025316A (ja) * | 2001-07-13 | 2003-01-29 | Ngk Insulators Ltd | ハニカム構造体、及びその製造方法 |
JP4640903B2 (ja) * | 2001-07-13 | 2011-03-02 | 日本碍子株式会社 | ハニカム構造体、及びその製造方法 |
US7803447B2 (en) | 2001-08-30 | 2010-09-28 | Ngk Insulators Ltd. | High strength honeycomb structure, method of molding the same, and honeycomb structure converter |
JPWO2004024295A1 (ja) * | 2002-09-13 | 2006-01-05 | イビデン株式会社 | ハニカム構造体 |
US8012234B2 (en) | 2002-09-13 | 2011-09-06 | Ibiden Co., Ltd. | Honeycomb structural body |
US7766991B2 (en) | 2002-09-13 | 2010-08-03 | Ibiden Co., Ltd. | Honeycomb structural body |
JP2007524030A (ja) * | 2003-12-24 | 2007-08-23 | サン−ゴバン・サントル デゥ ルシェルシュ エ デチューデ・ウロペアン | 内燃機関の排気ガス中に存在する微粒子をろ過するためのブロック |
US7318954B2 (en) | 2004-02-19 | 2008-01-15 | Ngk Insulators, Ltd. | Honeycomb structure |
US7989047B2 (en) * | 2005-12-27 | 2011-08-02 | Denso Corporation | Hexagonal-cell honeycomb structure |
US7666240B2 (en) | 2007-02-28 | 2010-02-23 | Ibiden Co., Ltd. | Honeycomb filter |
EP1978006A1 (en) | 2007-02-28 | 2008-10-08 | Ibiden Co., Ltd. | Honeycomb filter |
JP2009233582A (ja) * | 2008-03-27 | 2009-10-15 | Ngk Insulators Ltd | ハニカム触媒体 |
WO2013008788A1 (ja) * | 2011-07-12 | 2013-01-17 | 住友化学株式会社 | ハニカム構造体 |
WO2019232148A1 (en) * | 2018-05-31 | 2019-12-05 | Corning Incorporated | Honeycomb bodies with honeycomb structure strengthening features and extrusion dies therefor |
JP2021525663A (ja) * | 2018-05-31 | 2021-09-27 | コーニング インコーポレイテッド | ハニカム構造強化機能を有するハニカム体及びそのための押出ダイ |
US11839995B2 (en) | 2018-05-31 | 2023-12-12 | Corning Incorporated | Honeycomb bodies with honeycomb structure strengthening features and extrusion dies therefor |
Also Published As
Publication number | Publication date |
---|---|
US5952079A (en) | 1999-09-14 |
DE69735618D1 (de) | 2006-05-18 |
JP3060539B2 (ja) | 2000-07-10 |
EP0854123B1 (en) | 2006-04-05 |
EP0854123A1 (en) | 1998-07-22 |
DE69735618T2 (de) | 2007-05-03 |
EP0854123A4 (en) | 2000-11-08 |
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