WO2006001503A1 - フィルタ、その製造方法及び排気浄化装置 - Google Patents
フィルタ、その製造方法及び排気浄化装置 Download PDFInfo
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- WO2006001503A1 WO2006001503A1 PCT/JP2005/012144 JP2005012144W WO2006001503A1 WO 2006001503 A1 WO2006001503 A1 WO 2006001503A1 JP 2005012144 W JP2005012144 W JP 2005012144W WO 2006001503 A1 WO2006001503 A1 WO 2006001503A1
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- silicon carbide
- oxide
- ceramic
- average particle
- alumina
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
- F01N3/022—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous
- F01N3/0222—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous the structure being monolithic, e.g. honeycombs
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- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
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Definitions
- the present invention relates to a fill evening, a manufacturing method thereof, and an exhaust purification device.
- a honeycomb filter for removing particulate matter contained in exhaust gas has been proposed in which a silica film is formed on the surface of silicon carbide as an aggregate.
- a silica film is formed on the surface of silicon carbide as an aggregate.
- the honeycomb filter described in Japanese Patent Application Laid-Open No. 2 00 0-2 2 1 8 1 6 5 it is formed into a fill shape and sintered in an inert atmosphere, and then calcined in the presence of oxygen.
- a silicon film for improving the strength is formed on the surface of silicon carbide.
- the honeycomb filter is reinforced by the silica film, so that the honeycomb filter is prevented from being broken. Disclosure of the invention
- the silica film is formed on the surface of silicon carbide, the smashing strength is improved.
- the temperature suddenly becomes unexpectedly high for some reason.
- the force film may be reduced by the carbon contained in the particulate matter.
- the silica film is reduced in this way, the function of the silica film as a protective film is lowered, and the heat resistance of the film may be lowered.
- This invention is made
- the present invention adopts the following means in order to achieve at least one of the above objects.
- the filter of the present invention is
- a ceramic particle protective material comprising a non-reducing substance or a precursor thereof which is present on the surface of the ceramic particle and reduced by carbon contained in the granular substance at a higher temperature than an oxide of an element contained in the ceramic particle. Is included.
- the ceramic particle protective material made of a hardly reduced substance or its precursor is present on the surface of the ceramic particle, the protective effect of the ceramic particle is maintained until the temperature becomes considerably high.
- the ceramic particle protective material is not reduced unless the oxide of the element contained in the ceramic particles becomes higher than the temperature at which it is reduced by carbon (contained in the particulate matter). Therefore, according to the present invention, it is possible to protect the ceramic particles until the temperature is higher than when the elemental oxide contained in the ceramic particles is a ceramic particle protective material. The heat resistance of can be improved.
- the ceramic particles are preferably one or more particles selected from, for example, silicon carbide, silicon nitride, silica, alumina, zirconia, titania, ceria, and clay, Silicon carbide is more preferable. Silicon carbide is often used in fills. Silicon carbide also reacts with oxygen and oxidizes at high temperatures in an oxygen atmosphere. Therefore, a stable protective material is required on the surface even at high temperatures. Therefore, the significance of applying the present invention to silicon carbide is high.
- the ceramic particle protective material may be present as a protective film on the surface of the ceramic particles.
- the ceramic particle protective material covers the surface of the ceramic particles, so it is easy to increase the heat resistance of the film.
- the thickness of the protective film is preferably 0.4 to 100 nm, more preferably 0.5 to 5 nm, and preferably 0.6 to 1.5 nm. Most preferred. If the thickness of the protective film is less than 0.4 nm, it is not preferable because the ceramic particles cannot be sufficiently protected. If the thickness exceeds OOO nm, the pressure loss of the exhaust gas flowing through the filter increases, which is preferable. It is not considered.
- “thickness of the protective film” is a value obtained by Auger electron spectroscopy (AES).
- the hardly-reducing substance is preferably one or more substances selected from the group consisting of aluminum oxide, mullite, yttrium oxide, magnesium oxide, lithium oxide, calcium oxide and titanium oxide. These substances are relatively difficult to reduce even at high temperatures. Of these, aluminum oxide (alumina) is more preferred. Alumina is stable to heat and is not easily reduced at high temperatures.
- the above-mentioned “precursor of difficult-to-reduced substance” includes, for example, aluminum oxycarbide when the hardly-reduced substance is aluminum oxide, and oxycarbide when the hardly-reduced substance is yttrium oxide. Trium is mentioned.
- Aligninum oxycarbide refers to compounds containing A 1 ⁇ , C such as A 1 20 C and A 4 C.
- Y “Yttrium oxycarbide” refers to Y 2 0 C and Y 4 ⁇ 4 A compound containing Y, 0, C such as C.
- the manufacturing method of the Phil evening of the present invention is: A method for producing a filter that removes particulate matter contained in exhaust gas, the ceramic particles having a predetermined average particle diameter, and an average particle diameter that is the same material as the ceramic particles and smaller than the predetermined average particle diameter A raw material mixing process that mixes certain fine particles into clay,
- the molded body obtained by molding the clay is fired in the presence of a hard-to-reduced substance reduced by carbon contained in the granular substance or a precursor thereof at a higher temperature than the oxide of the element contained in the ceramic particles.
- this method for producing a filter it is possible to obtain a fill that has higher heat resistance than a fill that is made of an oxide of an element contained in ceramic particles as a ceramic particle protective material.
- the manufacturing method of the Phil evening of the present invention is:
- a method of manufacturing a filter that removes particulate matter contained in exhaust gas, the ceramic particles having a predetermined average particle diameter, and an average particle diameter that is the same material as the ceramic particles and smaller than the predetermined average particle diameter Mixing raw materials to form clay by mixing fine particles and a hard-to-reduced substance reduced by carbon contained in the granular material or a precursor thereof at a higher temperature than the oxide of the element contained in the ceramic particle Process,
- the elements contained in the ceramic particles It is possible to obtain a filter having higher heat resistance than that of the filter film in which the oxide is a ceramic particle protective material.
- the molding and firing step when the molded body is fired, the molded body and the hardly-reduced substance or precursor thereof are allowed to coexist, and the molded body is also used by the coexisting hardly-reduced substance or precursor thereof.
- the ceramic particle protective material may be present on the surface of the substrate.
- the ceramic particles are, for example, one or more particles selected from silicon carbide, silicon nitride, silica, alumina, zirconium, titania, ceria, and mullite.
- silicon carbide is more preferable.
- Silicon carbide is often used for filling to remove particulate matter contained in the exhaust, and it reacts with oxygen and oxidizes at high temperatures in an oxygen atmosphere. Therefore, the significance of applying the present invention to silicon carbide is high.
- metal silicon in the raw material mixing step, metal silicon may be further mixed to form clay.
- the metal silicon binds the ceramic particles at a lower temperature than that without adding it, so the firing temperature can be lowered.
- the temperature at which the molded body is fired may be 1100 to 180 ° C.
- a temperature at which the molded body is fired is 1600 to 2200 ° C. If the firing temperature of the molded body is less than 1600, the strength of the fill cannot be increased, and if it exceeds 2200, the environmental load increases from the viewpoint of heat energy consumption.
- the predetermined average particle diameter of the ceramic particles is preferably 5 to 100 / im, and is preferably 10 to 50 m. It is more preferable. If the average particle size of the ceramic particles is less than 5 nm, the pore size decreases and the exhaust pressure loss increases. If it exceeds 100 / im, the joint between the particles may decrease and the strength may decrease.
- the average particle size of the fine particles is preferably 0.1 to 10 m, and more preferably 0.1 to 5 m. If the average particle size of the fine particles is less than 0.1 ⁇ m, the fine particles may agglomerate and disperse, resulting in uneven sintering. This is considered undesirable because it may be present at the joint (neck) of the metal and the strength may decrease.
- the “average particle diameter” is a value obtained by a laser single diffraction scattering method using a master sizer manufactured by MA L VERN.
- the hardly reducing substance is one or more selected from the group consisting of aluminum oxide, mullite, yttrium oxide, magnesium oxide, lithium oxide, calcium oxide and titanium oxide. It is preferable that the substance is These substances are less likely to be reduced than the oxides of elements contained in ceramic particles. Of these, aluminum oxide (alumina) is more preferred. Alumina is relatively heat stable and can protect ceramic particles at high temperatures.
- An exhaust purification device that removes particulate matter contained in exhaust from an internal combustion engine
- a connecting pipe that is connected to the internal combustion engine and through which exhaust from the internal combustion engine circulates
- a filter container connected to the connecting pipe and storing the filter.
- FIG. 1 is an explanatory diagram of the honeycomb fill 10 of the present embodiment.
- FIG. 2 is an explanatory diagram of the ⁇ two-cam filter 20 of the present embodiment.
- FIG. 3 is an explanatory diagram of the honeycomb filter 30 of the present embodiment.
- Fig. 4 is an explanatory diagram showing the relationship between the standard free energy ⁇ G of Si, A1 and C and the temperature.
- FIG. 5 is an explanatory diagram of the exhaust purification device 40 of the present embodiment.
- FIG. 6 is a TEM photograph of a cross section of the honeycomb filter of the present embodiment.
- Fig. 7 is a photograph of the appearance after the Excess PM regeneration test at Yuji Cam Phil. BEST MODE FOR CARRYING OUT THE INVENTION
- FIG. 1 (a) is an explanatory view of the honeycomb filter 10, and FIG. 1 (b) shows a cross-sectional view taken along the line AA in FIG. 1 (a).
- the honeycomb filter 10 is a diesel particulate filter (hereinafter referred to as DPF) having a function of filtering and purifying particulate matter (hereinafter referred to as PM) in exhaust gas from diesel engines.
- DPF diesel particulate filter
- PM purifying particulate matter
- This honeycomb filter 10 has an outer dimension of 34.3 mm ⁇ 34.3 mm ⁇ 150 mm, and the thickness of the wall portion 15 between the through holes 1 2 is 0.1 ⁇ : L 0.
- the number of through-holes 1 2 per unit cross-sectional area is 0.1 6 to 6 2 screws m 2 (1.0 to 0 to 2 mm, more preferably 0.2 to 6.0 mm) 4 0 cpsi).
- the shape of the through hole 1 2 may be, for example, a substantially triangular or hexagonal cross section. It is said.
- the honeycomb filter 10 contains silicon carbide as ceramic particles as an aggregate and alumina (aluminum oxide) as a ceramic particle protective material.
- This alumina is a hardly-reducing substance that is reduced by carbon at a higher temperature than the Si oxide (silica) contained in silicon carbide.
- the amount of silicon carbide contained in the honeycomb filter 10 is 80 to 98% by weight, and the amount of alumina is 2 to 20% by weight (more preferably 3 to 10% by weight).
- the honeycomb fill evening 1 0 of the surface of the silicon carbide particles, the protective layer comprising alumina and its precursor (such as A 1 2 OC and A 1 4 ⁇ 4 C) is formed.
- This protective film is present on the surface of the silicon carbide particles with a thickness of 0.4 to 100 nm (more preferably 0.5 to 5 nm, most preferably 0.6 to 1.5 nm). Yes.
- silicon carbide hereinafter referred to as coarse-grained silicon carbide
- silicon carbide hereinafter referred to as fine particles
- a method for manufacturing a honeycomb fill 10 using alumina as a ceramic particle protective material will be described.
- the average grain size of coarse silicon carbide contained in the raw material for the honeycomb fill is in the range of 5 to 100 mm (preferably 30 to 40 xm).
- Fine silicon carbide having an average particle diameter of 0.1 to 10 m (preferably 0.5 m) is used.
- the average particle diameter of alumina is preferably 0.1 to 10 mm, and here 0.5 m is used.
- Alumina is excellent in stability at high temperatures, has a high function as a ceramic particle protective material, and can promote the sintering of silicon carbide.
- the amount of coarse silicon carbide is 50 to 70% by weight and the amount of fine silicon carbide is 20 to 35% by weight (more preferably 25 to 5%) based on the whole of coarse silicon carbide, fine silicon carbide and alumina. 30 wt%), and the amount of alumina is preferably 1 to 30 wt% (more preferably 3 to 7 wt%). If the amount of coarse silicon carbide is less than 50% by weight, the amount of fine silicon carbide or alumina is relatively large, and the pore size of the honeycomb fill is small, which is not preferable. If it exceeds 70% by weight, fine carbonization This is not preferable because the amount of silicon or alumina is relatively small and the strength is weakened.
- the amount of fine silicon carbide is less than 20% by weight, the material forming the bonding part (neck part) between the coarse silicon carbide particles is reduced, and the thermal conductivity and thermal shock resistance are reduced, which is not preferable.
- Exceeding 35% by weight is not preferable because the pore diameter of the honeycomb fill is reduced.
- the alumina content is less than 1% by weight, it is not preferable because the aluminum component is less likely to be present on the surface. This is not preferable because of a decrease.
- examples of the dispersion medium include organic solvents (such as benzene) and alcohols (such as methanol).
- an organic binder or molding aid may be appropriately added to the clay in accordance with the moldability.
- examples of the organic binder include one or more organic binders selected from methyl cellulose, carboxymethyl cellulose, hydroxyethyl cellulose, polyethylene glycol, phenol resin, and epoxy resin.
- the blending amount of the organic binder is preferably 1 to 10 parts by weight with respect to 100 parts by weight of the total of coarse silicon carbide, fine silicon carbide and alumina.
- molding aids include ethylene glycol, Mention may be made of dextrin, fatty acid sarcophagus and polyalcohol. This clay may be mixed using, for example, a mixer and a kneader, or may be sufficiently kneaded with a kneader.
- the clay containing coarse silicon carbide, fine silicon carbide and alumina obtained in the raw material mixing step is formed into a honeycomb shape.
- the method of molding the clay can be performed by extrusion molding, staking molding, press molding, or the like, but here it is performed by extrusion molding.
- the fine silicon carbide is added to the clay, the fine silicon carbide is molded between the coarse silicon carbide particles at the time of molding.
- the shape of the honeycomb filter to be formed is appropriately selected depending on the intended use and the like, but may be any shape and size, and may be, for example, a cylindrical shape, a prismatic shape, or an elliptical column shape.
- each of the plurality of through holes is sealed, and only one end face is sealed with a paste having the same composition as the clay.
- a plurality of through-holes are formed so that one end face is sealed and the other end face is opened, and one end face is opened and the other end face is sealed.
- the obtained green molded body is dried and fired. Drying is performed at a temperature of about 100 to 200 ° C. using a microwave dryer or a hot air dryer.
- an organic component such as an organic binder
- the calcination conditions are appropriately selected depending on the amount and type of added organic components.
- the compact is fired under an inert gas atmosphere such as nitrogen or argon at 1600 to 2200 ° C (more preferably 1900 to 2100 ° C). . In this way, the honeycomb fill 10 of the present embodiment can be obtained.
- a honeycomb filter 20 in which a plurality of the honeycomb filters 10 are joined and processed into a cylindrical shape may be used.
- a method for manufacturing the honeycomb fill 20 will be described. First, a plurality of honeycomb filters 10 described above are manufactured, and a seal material paste is applied to the outer surface 13 of the honeycomb filter 10 to join the plurality of honeycomb filters 10. Dry and solidify to form a sealant layer 26. Next, the joined material is cut into a cylindrical shape using a diamond cutter or the like, and the outer peripheral surface where the through holes 12 are not opened is coated with the same paste as the sealing material paste. Dry and solidify with 20 to form a coating material layer 2 7.
- the sealing material paste includes at least one of inorganic fibers and inorganic particles, and an inorganic binder or an organic binder added thereto as appropriate can be used.
- the inorganic fibers include one or more ceramic fibers selected from silica monoalumina, mullite, alumina, silica, and the like.
- the inorganic particles include one or more particles selected from silicon carbide, silicon nitride, boron nitride, and the like.
- the inorganic binder include one or more binders selected from silica sol, alumina sol, and the like.
- organic binder examples include one or more selected from polyvinyl alcohol, methyl cellulose, ethyl cellulose, carboxymethyl cellulose and the like.
- a cylindrical honeycomb filter 30 having through holes 32 is integrally formed.
- An integrated DPF may be provided by alternately providing plugged portions 3 4 at the end faces of the through holes 3 2 of the two cam fills 30.
- alumina exists on the surface of the silicon carbide particles, and the silicon carbide as an aggregate is oxidized even if the collected particulate matter is heated to a considerably high temperature. It is hard to be done. The reason for such high heat resistance is not clear at present, but may be due to the following points. That is, in the green compact before firing, fine silicon carbide and alumina are intercalated between the coarse silicon carbide particles. When firing at a high temperature, alumina diffuses together with the fine silicon carbide on the surface of the coarse silicon carbide. At this time, alumina reacts with carbon to produce alumina precursors such as aluminum oxycarbide (such as A 1 2 0 C and A 1 4 0 4 C).
- a protective film of alumina and its precursor is formed on the surface of the coarse silicon carbide. Thereafter, when the honeycomb fill 10 is heated to a high temperature, this precursor is oxidized to further form alumina, and it is assumed that a protective film of alumina is formed on the surface of the silicon carbide particles.
- the surface of the silicon carbide silica (S i ⁇ 2) film is formed is an oxide of S i contained in the silicon carbide.
- This silica film serves as a protective material that prevents silicon carbide from oxidizing at high temperatures. Therefore, the case where an SiO 2 film is formed on the surface of silicon carbide and the case where an alumina (A 1 2 0 3 ) film, which is a ceramic particle protective material, is formed will be described in comparison.
- the protective properties of silicon carbide can be explained from the difference in reducing properties of the S i 0 2 film and the A 1 2 0 3 film due to the force of Bonn (C) contained in the granular material.
- Figure 4 shows the relationship between the standard free energy AG of Si, A 1 and C and the temperature.
- a lower ⁇ G is more stable as an oxide.
- the following formulas (1) to (3) show the formulas in which Si, A1 and C react with ⁇ 2.
- S i ⁇ 2 when the protective film of silicon force is formed on the surface of silicon carbide This will be explained by the relationship between CO and CO. As shown in Fig. 4, below the temperature T1, S i 0 2 with a lower ⁇ G than CO is more stable. Therefore, S I_ ⁇ 2 be present and S i 0 2 and C is not reduced.
- the direction of S i 0 2 and stability of the CO is reversed against the S i ⁇ 2 ⁇ G is lower CO at point A shown in FIG. 4 becomes stable.
- a 1 2 ⁇ 3 The presence of the A 1 ⁇ 3 and C are reduced A 1 and Do Ri, C is the CO is oxidized. From these, the 3 1_Rei 2, but the oxidation of the silicon carbide without being reduced to a temperature T1s can be prevented, the A 1 2 0 3, stable oxide of silicon carbide without being reduced to a temperature T 2 exceeding it Can be prevented. Therefore, in the honeycomb filter 1 0, when protecting the more silicon carbide S i 0 2 film decreases is reduced by carbon S i ⁇ 2 film is included in the PM exceeds the temperature T 1, protection The function as a membrane is reduced.
- Si contained in silicon carbide is vaporized and reduced as S i 0 (g: gas).
- This S i 0 is oxidized by oxygen inside the through-holes 12 of the honeycomb fill 10 and becomes white fiber-like or whisker-like S i 0 2 and is deposited inside the through-holes 12.
- the silicon carbide when silicon carbide is protected by the A 1 2 0 3 film, the silicon carbide can be protected up to a temperature T 2 higher than the temperature T 1.
- FIG. 5 is an explanatory diagram of the exhaust emission control device 40 of the present embodiment.
- the exhaust purification device 40 includes a diesel engine 4 2, a manifold 4 3 connected to the engine 4 2 (corresponding to the connecting pipe of the present invention), and a catalyst component connected to the manifold 4 3. It is composed of a supported honeycomb cam filter 20 and a casing 46 holding the 820 cam filter 20 via an alumina mat 45 (corresponding to the filter container of the present invention) and is mounted on an automobile. ing.
- the exhaust from the engine 42 contains nitrogen oxides (NO x), hydrocarbons (HC), carbon monoxide (CO), and PM generated from carbon contained in the fuel.
- the honeycomb fill 20 is a DPF that removes PM contained in the exhaust of the engine 42.
- This honeycomb fill 20 is produced by the above-described manufacturing method. As shown in FIG. 2, the honeycomb fill 10 having a plurality of through holes 12 arranged in parallel along the longitudinal direction is obtained. A plurality of them are joined and processed into a cylindrical shape.
- the honeycomb filter 20 is held by an alumina mat 45 and fixed in a metal casing 46.
- honeycomb film 10 and the like it was inferred that an alumina protective film was formed on the surface of the silicon carbide particles, but even if such a film was not formed, According to the manufacturing method of fill evening, the heat resistance of fill evening can be improved. Moreover, it can be said that the honeycomb filter obtained by this manufacturing method has high heat resistance. According to the present embodiment described in detail above, alumina, which is a hardly reducing substance, exists as a protective film on the surface of the silicon carbide particles, and thus is included in silicon carbide.
- an oxide of S i is in the protective film can protect the silicon carbide to a more high temperature. Therefore, the heat resistance of the honey-fil fill can be improved.
- the present invention is not limited to the above-described embodiments, and can be implemented in various modes as long as they belong to the technical scope of the present invention.
- alumina is present as a protective film on the surface of the silicon carbide particles, but it may not be a complete protective film made of alumina. This also improves the heat resistance of at least the portion where alumina is present.
- the alumina when the green molded body is fired in the absence of oxygen, the alumina may be present in the presence of alumina and the alumina may be present on the surface of the ceramic particles of the honeycomb fill. .
- the condition for coexisting alumina is preferably in the range of 80 to 400 parts by weight of alumina with respect to 150 parts by weight of the honeycomb filter.
- Method of coexisting alumina For example, there are a method in which alumina powder is placed on a glass or the like, and a method in which alumina powder is packed inside the through hole.
- alumina was mixed and molded.
- a raw material mixing step of mixing coarse silicon carbide and fine silicon carbide without mixing alumina was performed, and in the molding and firing step, Alumina may be present on the surface of the ceramic particles of the honeycomb filter 10 by firing in the presence of alumina.
- the amount of coarse silicon carbide is preferably 50 to 70% by weight with respect to the whole of coarse silicon carbide, fine silicon carbide, metal silicon and alumina.
- the amount of fine silicon carbide is preferably 5 to 35% by weight (more preferably 10 to 30% by weight), and the amount of metal silicon is 5 to 35% by weight (more preferably Is preferably 10 to 30% by weight), and the amount of alumina is preferably 1 to 30% by weight (more preferably 3 to 7% by weight).
- the molding and firing step the molded body can be sintered at a firing temperature of 1100 to 180 ° C.
- honeycomb structure 10 is specifically manufactured.
- ⁇ -type silicon carbide powder (average particle size 40 zm) 6 7500 parts by weight as ceramic particles and ⁇ -type silicon carbide powder (average particle size 0.5 u rn) 2 9 5 0 parts by weight as fine particles And alumina as a sintering aid (average particle size 0.5 lim) 30.0 parts by weight and water 1800 parts by weight, Add 400 parts by weight of methylcellulose as a powder, 150 parts by weight of glycerin as a plasticizer, and lubricant (trade name: uniloop; manufactured by Nippon Oil & Fats Co., Ltd.). It was.
- This kneaded material was extruded with an extruder so as to form a prism having a plurality of through-holes having a square cross section arranged in parallel along the longitudinal direction, to obtain a green molded body.
- the obtained green compact is dried by a microwave dryer, and end faces of a plurality of through holes arranged in parallel along the longitudinal direction are alternately plugged with a paste having the same composition as the clay. Further, it was dried and degreased at 400 ° C. for 3 hours.
- This molded body was fired at 200 ° C. for 3 hours in an argon atmosphere at normal pressure to obtain 34.3 mm X 34.3 mm X 15 500 shown in Fig. 1 (a).
- An 82-cam structure 10 made of a sintered silicon carbide with a through hole of 31 mm / cm 2 (20 cpsi) and a partition wall thickness of 0.3 mm was prepared (Experiment 1). .
- the average particle diameter of coarse silicon carbide, the average particle diameter of fine silicon carbide, the average particle diameter of alumina, the mixing ratio of coarse particles, the mixing ratio of fine particles, the mixing ratio of alumina, the honeycomb filter 10 of Experimental Example 1 Table 1 summarizes the numerical values such as ratio and firing temperature. In addition, each compounding ratio was made into the weight% with respect to the whole coarse grain silicon carbide, fine grain silicon carbide, and alumina. Table 1 also summarizes the contents related to Experimental Examples 2 to 9 described later. The results of the three-point bending strength, average pore diameter, alumina film thickness, and excess PM regeneration test described later are also shown.
- a honeycomb filter was produced in the same manner as in Experimental Example 1, except that the composition ratio and firing temperature shown in Table 1 were used.
- Experimental example 7 is the same mixing ratio as experimental example 2, and the firing temperature was 160 ° C., and experimental example 8 was not added with alumina as a ceramic particle protective material.
- Experimental Example 9 does not include silicon carbide fine particles.
- honeycomb fill so that it has the same blending ratio and shape as Example 2 ', and put alumina into a tray made of a single-bonn so that 100 g of alumina can coexist with 10 honeycomb fills.
- the green compact was fired at 20 ° C. in an argon atmosphere to prepare a honeycomb fill 10.
- the average particle size of coarse silicon carbide, the average particle size of fine silicon carbide, the average particle size of alumina, the mixing ratio of coarse particles, the mixing ratio of fine particles, and the mixing ratio of alumina Table 2 summarizes the numerical values such as the ratio, firing temperature, and the coexistence of alumina.
- each compounding ratio was made into the weight% with respect to the whole coarse grain silicon carbide, fine grain silicon carbide, and alumina.
- Table 2 also summarizes the contents of Experimental Examples 11 to 16 described later. The three-point bending strength, average pore diameter, alumina film thickness, and excess PM regeneration test results described later are also summarized.
- a honeycomb fill was manufactured in the same manner as in Experimental Example 10, except that the composition ratio and firing temperature shown in Table 2 were used.
- Experimental Example 14 alumina as a ceramic particle protective material was not added, and in Experimental Example 15, fine silicon carbide particles were not added.
- ⁇ -type silicon carbide powder (average particle size 40 m) as ceramic particles 6 6 50 parts by weight, and diamond-type silicon carbide powder (average particle size 0.5 m) 20 0 parts by weight as fine particles, metal Silicon (average particle size 4 m) 8 50 parts by weight, ceramic particle protective material alumina (average particle size 0.5 / xm) 5 0 0 parts by weight, water 240 0 parts by weight, and organic binder 1 part by weight of methylcellulose as a base material, 100 parts by weight of dalyserin as a plasticizer, and 50 parts by weight of a lubricant (trade name: Yuelbubu, manufactured by NOF Corporation) are kneaded and kneaded.
- a lubricant trade name: Yuelbububu, manufactured by NOF Corporation
- This clay is molded in the same manner as in Experimental Example 1, and alumina is placed in a carbon tray so that 100 g of alumina coexists with 10 of the two cam filters.
- the honeycomb filter 10 (experimental example 16) shown in Fig. 1 (a) was fabricated by firing at 450 ° C in an argon atmosphere.
- the three-point bending strength measurement of Experimental Examples 1 to 16 was performed. This measurement was performed based on JIS-R 1600 using an instrument manufactured by Instoton 5 5 8 2 as a measuring instrument. Specifically, the crosshead speed was 0.5 mmZm in, the span distance was 125 mm, and the prismatic honeycomb filter shown in Fig. 1 (a) The fracture load was measured by applying a load, and the strength was calculated by calculating the second moment of the cross section from the wall thickness and honeycomb structure. [Average pore size measurement]
- the average pore diameter of Experimental Examples 1 to 16 was measured. This measurement was performed by a mercury intrusion method based on JIS-R 1 65 5 5 using an automatic porosime Ichiba autopore 9405 manufactured by Shimadzu Corporation as a measuring instrument. Specifically, the honeycomb film 10 is cut into cubes of about 0.8 cm, ultrasonically cleaned with ion-exchanged water, dried, and then used to measure 0.2 to 500 / m. Measured in the measuring range. Measurements were made at pressures of 0.1 psia in the range of 100-500 / xm, and measurements were made at pressures of 0.25 psia in the range of 0.2-100 m.
- the alumina film thickness of Experimental Examples 1 to 16 was measured. This measurement was performed by an etching method using a PHI-700 type Auger analyzer manufactured by ULVAC-FAI as a measuring instrument.
- Experimental Examples 1 to 16 Excess PM regeneration tests at high temperatures were performed. This test observes changes in the honeycomb filter 10 after burning an excessive amount of PM. As test conditions, Experimental Examples 1 to 16 were collected so that the amount of the particulate matter per unit volume of the honeycomb filter 10 was 20 gZL, and the particulate matter was forcibly burned and regenerated. Evaluation was made by visually observing the surface of the sample after burning the particulate matter. In the evaluation results, X indicates that the sample changed after the test, and ⁇ indicates that the sample did not change.
- Figure 6 (a) shows a TEM photograph taken by slicing Experimental Example 2.
- Figure 6 (b) also shows the results of elemental analysis of points A, B, and C in the photograph of Fig. 6 (a). From this result, only S i and C were detected at point C, which is the bulk portion, whereas A 1 and O were detected at point B in addition to S i and C being detected. Note that the distance between points B and C is approximately 1 nm. From this result, it was found that A 1 due to the added alumina was present on the surface of the silicon carbide particles as the aggregate. In addition, because the sample that had been subjected to SEM observation after forming a force vapor deposition film was used for TEM observation, carbon (C) due to the carbon deposition film was detected at point A.
- Table 1 shows the measurement results of the three-point bending strength, average pore diameter, alumina film thickness, and excess PM regeneration test of Experimental Examples 1 to 9, and Table 2 shows those of Experimental Examples 10 to 16.
- Tables 1 and 2 show that the alumina film thickness increased as the alumina compounding ratio increased.
- Experimental Example 8 where no alumina was added and in Experimental Examples 9 and 15 where fine particles of silicon carbide were not added, the alumina film was not observed or was very thin, and the honeycomb filter was whitened in the excess PM regeneration test.
- Figure 7 shows a photograph of the experimental example 8 after the excess PM regeneration test.
- the part that became quite hot due to the combustion heat of PM was vitrified to a white state. This was presumed to be fibrous or whisker-like silica.
- the alumina was baked in the coexistence, the thickness of the alumina increased, and it was assumed that the alumina was deposited. Similar results were obtained with the sample mixed with metallic silicon. Therefore, it has been found that the heat resistance of the honeycomb fill 10 can be enhanced by the method of manufacturing the fill evening.
- the honeycomb filter 10 manufactured by this manufacturing method burns excess PM. As a result, the appearance did not change even at a high temperature (1500 ° C. or higher), and it was found that it had high heat resistance.
- the sealing material paste is composed of alumina fiber (fiber length 0.2 mm) 30% by weight, silicon carbide particles (average particle size 0 to ⁇ m) 2 1% by weight, silica sol (silica content in sol 30 wt%) 1 5 wt%, carboxymethylcellulose 5.6 wt%, water 28.4 wt%.
- the coating material paste consists of silica-alumina fiber (fiber length 0.1 ⁇ : LO Omm) 23.3 wt%, silicon carbide particles (average particle size 0.3 ⁇ m) 3 0.2 wt% Silica sol (the silica content in the sol was 30% by weight) 7% by weight, carboxymethylcellulose 0.5% by weight, and water 39% by weight was used.
- the present invention is based on Japanese patent application No. 2 0 4-1 8 8 8 5 7 filed on June 25, 2004, and the contents of all of the contents are incorporated. .
- Industrial applicability is based on Japanese patent application No. 2 0 4-1 8 8 8 5 7 filed on June 25, 2004, and the contents of all of the contents are incorporated. .
- the filter, porous body and honeycomb structure of the present invention are used in various industries, for example. In particular, it can be used in places where filtration is necessary. Specifically, it can be used as an exhaust gas purification device in the automobile industry or as a water purification device in the water supply industry.
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Abstract
Description
Claims
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JP2006528833A JP4796496B2 (ja) | 2004-06-25 | 2005-06-24 | フィルタ、その製造方法及び排気浄化装置 |
EP05755162A EP1759754B1 (en) | 2004-06-25 | 2005-06-24 | Method for producing a filter for exhaust purification system |
US11/335,695 US7311750B2 (en) | 2004-06-25 | 2006-01-20 | Filter, method of manufacturing the same, and exhaust gas purification device |
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US11/335,695 Continuation US7311750B2 (en) | 2004-06-25 | 2006-01-20 | Filter, method of manufacturing the same, and exhaust gas purification device |
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WO2006001503A1 true WO2006001503A1 (ja) | 2006-01-05 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPWO2006001509A1 (ja) * | 2004-06-25 | 2008-04-17 | イビデン株式会社 | 多孔体の製造方法、多孔体及びハニカム構造体 |
JP2010516608A (ja) * | 2007-01-29 | 2010-05-20 | サン−ゴバン サントル ドゥ ルシェルシェ エ デトゥードゥ ユーロペン | SiC系セラミック多孔質体の製造方法 |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006001503A1 (ja) | 2004-06-25 | 2006-01-05 | Ibiden Co., Ltd. | フィルタ、その製造方法及び排気浄化装置 |
JP5161458B2 (ja) | 2004-09-02 | 2013-03-13 | イビデン株式会社 | ハニカム構造体の製造方法 |
JP5095215B2 (ja) | 2004-09-30 | 2012-12-12 | イビデン株式会社 | 多孔体の製造方法、多孔体及びハニカム構造体 |
WO2006041174A1 (ja) * | 2004-10-12 | 2006-04-20 | Ibiden Co., Ltd. | セラミックハニカム構造体 |
WO2006057344A1 (ja) * | 2004-11-26 | 2006-06-01 | Ibiden Co., Ltd. | ハニカム構造体 |
WO2006092986A1 (ja) * | 2005-03-02 | 2006-09-08 | Ibiden Co., Ltd. | 無機繊維集合体、無機繊維集合体の製造方法、ハニカム構造体及びハニカム構造体の製造方法 |
WO2007097056A1 (ja) * | 2006-02-23 | 2007-08-30 | Ibiden Co., Ltd. | ハニカム構造体および排ガス浄化装置 |
WO2007096986A1 (ja) * | 2006-02-24 | 2007-08-30 | Ibiden Co., Ltd. | 端面加熱装置、ハニカム集合体の端面乾燥方法、及び、ハニカム構造体の製造方法 |
DE102006026769A1 (de) * | 2006-06-09 | 2007-12-13 | Robert Bosch Gmbh | Filter zur Entfernung von Partikeln aus einem Gasstrom sowie Verfahren zu seiner Herstellung |
DE102006034119A1 (de) * | 2006-07-24 | 2008-01-31 | Robert Bosch Gmbh | Filter zur Entfernung von Partikeln aus einem Gasstrom sowie Verfahren zu seiner Herstellung |
WO2008126319A1 (ja) * | 2007-03-30 | 2008-10-23 | Ibiden Co., Ltd. | 多孔質炭化ケイ素焼結体の製造方法 |
US7819298B2 (en) | 2008-02-14 | 2010-10-26 | Ethicon Endo-Surgery, Inc. | Surgical stapling apparatus with control features operable with one hand |
WO2012140755A1 (ja) * | 2011-04-13 | 2012-10-18 | イビデン株式会社 | ハニカム構造体およびハニカム構造体の製造方法 |
JP6581934B2 (ja) | 2016-03-24 | 2019-09-25 | 日本碍子株式会社 | ハニカムフィルタ |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000001463A1 (en) | 1998-07-07 | 2000-01-13 | Silentor Notox A/S | Diesel exhaust gas filter |
JP2003265964A (ja) * | 2002-03-14 | 2003-09-24 | Ibiden Co Ltd | 排気ガス浄化用の触媒担持フィルタ |
WO2003086579A1 (fr) * | 2002-03-29 | 2003-10-23 | Ibiden Co., Ltd. | Filtre en ceramique et unite de decontamination de gaz d'echappement |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5238478A (en) * | 1992-03-23 | 1993-08-24 | Zievers James F | Ceramic filter element and method of manufacture |
US5456740A (en) * | 1994-06-22 | 1995-10-10 | Millipore Corporation | High-efficiency metal membrane getter element and process for making |
JP2002530175A (ja) * | 1998-11-20 | 2002-09-17 | コーニンクレッカ フィリップス エレクトロニクス エヌ ヴィ | コードレス走査ヘッドの充電器を備える超音波診断イメージングシステム |
JP4071381B2 (ja) | 1999-01-29 | 2008-04-02 | イビデン株式会社 | ハニカムフィルタ及びその製造方法 |
JP2002054422A (ja) * | 2000-08-08 | 2002-02-20 | Ngk Insulators Ltd | セラミック製フィルター及びその製造方法 |
JP4590076B2 (ja) * | 2000-08-10 | 2010-12-01 | 興和株式会社 | 眼底撮影装置 |
JP4464568B2 (ja) * | 2001-02-02 | 2010-05-19 | 日本碍子株式会社 | ハニカム構造体及びその製造方法 |
US6840976B2 (en) * | 2001-04-23 | 2005-01-11 | Dow Global Technologies Inc. | Method of making wall-flow monolith filter |
JP4567285B2 (ja) * | 2002-11-22 | 2010-10-20 | 日本碍子株式会社 | 排ガス浄化用触媒体 |
JP4376579B2 (ja) * | 2003-09-09 | 2009-12-02 | 日本碍子株式会社 | 窒化珪素結合SiC耐火物及びその製造方法 |
JPWO2006001509A1 (ja) * | 2004-06-25 | 2008-04-17 | イビデン株式会社 | 多孔体の製造方法、多孔体及びハニカム構造体 |
WO2006001503A1 (ja) | 2004-06-25 | 2006-01-05 | Ibiden Co., Ltd. | フィルタ、その製造方法及び排気浄化装置 |
-
2005
- 2005-06-24 WO PCT/JP2005/012144 patent/WO2006001503A1/ja not_active Application Discontinuation
- 2005-06-24 JP JP2006528833A patent/JP4796496B2/ja active Active
- 2005-06-24 EP EP05755162A patent/EP1759754B1/en not_active Not-in-force
-
2006
- 2006-01-20 US US11/335,695 patent/US7311750B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000001463A1 (en) | 1998-07-07 | 2000-01-13 | Silentor Notox A/S | Diesel exhaust gas filter |
JP2002519186A (ja) * | 1998-07-07 | 2002-07-02 | シレントーア ノトックス アクティーゼルスカブ | ディーゼル排出ガスフィルター |
JP2003265964A (ja) * | 2002-03-14 | 2003-09-24 | Ibiden Co Ltd | 排気ガス浄化用の触媒担持フィルタ |
WO2003086579A1 (fr) * | 2002-03-29 | 2003-10-23 | Ibiden Co., Ltd. | Filtre en ceramique et unite de decontamination de gaz d'echappement |
Non-Patent Citations (1)
Title |
---|
See also references of EP1759754A4 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPWO2006001509A1 (ja) * | 2004-06-25 | 2008-04-17 | イビデン株式会社 | 多孔体の製造方法、多孔体及びハニカム構造体 |
JP2010516608A (ja) * | 2007-01-29 | 2010-05-20 | サン−ゴバン サントル ドゥ ルシェルシェ エ デトゥードゥ ユーロペン | SiC系セラミック多孔質体の製造方法 |
Also Published As
Publication number | Publication date |
---|---|
EP1759754B1 (en) | 2012-12-19 |
US20060179803A1 (en) | 2006-08-17 |
JP4796496B2 (ja) | 2011-10-19 |
US7311750B2 (en) | 2007-12-25 |
EP1759754A4 (en) | 2009-07-01 |
JPWO2006001503A1 (ja) | 2008-04-17 |
EP1759754A1 (en) | 2007-03-07 |
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