WO2010001062A2 - Melange de grains pour la synthese d'une structure poreuse du type titanate d'alumine - Google Patents
Melange de grains pour la synthese d'une structure poreuse du type titanate d'alumine Download PDFInfo
- Publication number
- WO2010001062A2 WO2010001062A2 PCT/FR2009/051292 FR2009051292W WO2010001062A2 WO 2010001062 A2 WO2010001062 A2 WO 2010001062A2 FR 2009051292 W FR2009051292 W FR 2009051292W WO 2010001062 A2 WO2010001062 A2 WO 2010001062A2
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- WIPO (PCT)
- Prior art keywords
- mixture
- phase
- grains
- microns
- titanium
- Prior art date
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- 239000000203 mixture Substances 0.000 title claims abstract description 45
- 239000002245 particle Substances 0.000 title claims abstract description 20
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 16
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 12
- 239000004411 aluminium Substances 0.000 title abstract 2
- 230000002194 synthesizing effect Effects 0.000 title 1
- 239000010936 titanium Substances 0.000 claims abstract description 12
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 12
- 239000010419 fine particle Substances 0.000 claims abstract description 3
- 230000003197 catalytic effect Effects 0.000 claims description 17
- 238000001914 filtration Methods 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 14
- 238000004519 manufacturing process Methods 0.000 claims description 12
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims description 10
- 229910010413 TiO 2 Inorganic materials 0.000 claims description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 6
- 229910000505 Al2TiO5 Inorganic materials 0.000 claims description 5
- 239000011230 binding agent Substances 0.000 claims description 5
- 238000002156 mixing Methods 0.000 claims description 5
- AABBHSMFGKYLKE-SNAWJCMRSA-N propan-2-yl (e)-but-2-enoate Chemical compound C\C=C\C(=O)OC(C)C AABBHSMFGKYLKE-SNAWJCMRSA-N 0.000 claims description 5
- 229910017682 MgTi Inorganic materials 0.000 claims description 4
- 238000009472 formulation Methods 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 239000011777 magnesium Substances 0.000 claims description 4
- 229920000609 methyl cellulose Polymers 0.000 claims description 4
- 239000001923 methylcellulose Substances 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 3
- 239000003361 porogen Substances 0.000 claims description 3
- 239000011362 coarse particle Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 description 23
- 239000011148 porous material Substances 0.000 description 10
- 238000001125 extrusion Methods 0.000 description 8
- 238000005245 sintering Methods 0.000 description 8
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 6
- 230000008929 regeneration Effects 0.000 description 6
- 238000011069 regeneration method Methods 0.000 description 6
- 239000007789 gas Substances 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 239000002243 precursor Substances 0.000 description 5
- 239000004071 soot Substances 0.000 description 5
- 229910010293 ceramic material Inorganic materials 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 229910052878 cordierite Inorganic materials 0.000 description 4
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 4
- 229910010271 silicon carbide Inorganic materials 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910004298 SiO 2 Inorganic materials 0.000 description 2
- 239000002585 base Substances 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- CETPSERCERDGAM-UHFFFAOYSA-N ceric oxide Chemical compound O=[Ce]=O CETPSERCERDGAM-UHFFFAOYSA-N 0.000 description 2
- 229910000422 cerium(IV) oxide Inorganic materials 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
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- 230000001590 oxidative effect Effects 0.000 description 2
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- 230000000930 thermomechanical effect Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229920002472 Starch Polymers 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 150000004649 carbonic acid derivatives Chemical class 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
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- 239000000470 constituent Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 150000004679 hydroxides Chemical class 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 125000002524 organometallic group Chemical group 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 238000013001 point bending Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
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- 238000002459 porosimetry Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000010970 precious metal Substances 0.000 description 1
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- 230000000171 quenching effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000011218 segmentation Effects 0.000 description 1
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- C04B35/46—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates
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- C04B35/478—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates based on titanates based on aluminium titanates
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- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
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- B28B3/00—Producing shaped articles from the material by using presses; Presses specially adapted therefor
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Definitions
- the invention relates to a mixture of grains and to a process using said mixture for the production of a porous structure such as a catalytic support or a particulate filter whose material constituting the filtering and / or active part is based on of alumina titanate.
- the ceramic material at the base of the ceramic supports or filters according to the present invention consist mainly of oxides of the elements Al and Ti, mainly in the form of a phase of the Al 2 TiO 2 alumina titanate type (pseudobrookite).
- the invention also relates to porous honeycomb structures obtained from such a process, in particular to catalytic supports and / or particulate filters especially used in an exhaust line of an internal combustion engine diesel type, whose properties are improved.
- the exhaust gas depollution structures generally have a honeycomb structure.
- a particulate filter is subjected to a succession of filtration phases (accumulation of soot) and regeneration
- soot particles emitted by the engine are retained and settle inside the filter.
- soot particles are burned inside the filter, in order to restore its filtration properties. It is thus conceivable that the mechanical strength properties at both low and high temperature of the constituent material of the filter are essential for such an application. Similarly, the material must have a sufficiently stable and durable structure to withstand, especially over the entire life of the equipped vehicle, temperatures that can locally rise to values substantially greater than 1000 0 C, especially if certain phases of regeneration are poorly controlled.
- the filters and supports are mainly porous ceramic material, especially silicon carbide or cordierite.
- Silicon carbide filters are for example described in patent applications EP 816 065, EP 1 142 619, EP 1 455 923 or else WO 2004/090294 and WO 2004/065088.
- Such filters make it possible to obtain chemically inert filtering structures with excellent thermal conductivity and having porosity characteristics, in particular the average size and the pore size distribution, which are ideal for a filtering application of soot from a thermal motor.
- a first disadvantage is related to the slightly high coefficient of thermal expansion of SiC, greater than 3.10 ⁇ 6 K -1 , which does not allow the manufacture of monolithic filters of large size and in most cases, it is necessary to segment the filter into a plurality of honeycomb elements bonded by a cement, as described in application EP 1 455 923.
- a second disadvantage is related to the extremely firing temperature. high, typically greater than 2100 0 C enabling sintering ensuring a sufficient thermomechanical resistance of the honeycomb structures, especially during the successive phases of regeneration of the filter. Such temperatures require the installation of special equipment that significantly increases the cost of the filter finally obtained.
- the cordierite filters are known and used for a long time, because of their low cost, it is now known that problems can occur in such structures, especially during poorly controlled regeneration cycles, during which the filter can be subjected locally to temperatures above the melting temperature of cordierite. The consequences of these hot spots can range from a partial loss of efficiency of the filter to its total destruction in the most severe cases.
- the cordierite does not have sufficient chemical inertia, compared to the temperatures reached during successive cycles of regeneration and is therefore likely to react and be corroded by the metals and alkali accumulated in the structure during the phases. filtration, this phenomenon can also be at the origin of the rapid deterioration of the properties of the structure.
- the object of the present invention is thus to provide a material and its manufacturing method, said material having a controlled porosity and which can serve as a base material for the filtering part of a filter or for the active part of a catalytic support.
- Said material mainly comprises or consists of an oxide material of the aluminum titanate type and has properties, as previously described, allowing its advantageous use in the field of porous honeycomb structures currently used in an exhaust line automotive catalytic support type or particulate filter.
- the present invention relates to a mixture of grains mainly comprising or consisting of a pseudo-brookite type oxide phase comprising at least titanium and aluminum, said mixture being obtained from at least two granulometric fractions, including:
- At least part of the grains comprises a main phase consisting of a pseudo-brookite type oxide phase comprising at least titanium and aluminum and at least one secondary phase, said secondary phase being a glassy phase and / or a phase consisting essentially of TiO 2 titanium oxide.
- Said oxide phase of the pseudo-brookite type can comprise titanium, aluminum and optionally magnesium and / or zirconium in proportions such that the aluminum titanate type phase corresponds substantially to the formulation
- the large granulometric fraction has a median diameter d 5 o greater than 15 microns.
- the large particle size fraction has a median diameter d 5 o less than 100 microns, preferably less than 80 microns and more preferably in less than 50 microns, or even less than 40 microns or 38 microns or 35 microns.
- the mass ratio between the fat and fine fractions is between 1.5 and 5 and in particular between 1.5 and 4.
- the ratio between the median diameters of the fat and fine fractions is, for example, greater than 15. Notably good results have been obtained when the ratio between the median diameters of the fat and fine fractions is less than 50, or even less than 45, or even less. For example, said ratio may be between 20 and 25 inclusive.
- all the possible combinations according to the invention between the different preferred modes characterizing the grain fractions and their mixture according to the invention, as they have just been described above, are not postponed. It is understood, however, that all possible combinations of the initial and / or preferred domains and values previously described are envisaged and must be considered as described by the applicant in the context of the present description (in particular of two, three or more combinations).
- the invention also relates to a method for manufacturing a catalytic support or a honeycomb particle filter from a mixture of grains as described above, comprising the following main steps: a) mixture said fat and fine fractions, b) mixing the mixture of grains, in the presence of an organic binder of the methylcellulose type and optionally a porogen and an amount of water sufficient to obtain a plasticity allowing step c), c) extrusion of a raw honeycomb structure through a die, d) baking of said structure at a temperature between 1300 0 C and 1800 0 C.
- the invention also relates to a catalytic support capable of being obtained by a process as previously described, comprising mainly or consisting of a pseudo-brookite type oxide phase comprising at least titanium and aluminum.
- the invention relates to a particulate filter, optionally catalytic, obtainable by a process as previously described, the filtering portion mainly comprises or consists of a pseudo-brookite type oxide phase comprising at least titanium and aluminum.
- the porous material is obtained from simple oxides Al2O3, TiO 2 and possibly other oxides of elements capable of entering into the pseudo-brookite structure Al 2 TiO 5, e.g. in the form of a solid solution.
- Such materials are typically oxides of magnesium, silicon, zirconium, iron or other elements.
- the mixture is sintered, i.e., it is heated to a temperature allowing the reaction of simple oxides to form sintered grains comprising at least one main phase of Al 2 TiO 5 type structure.
- any precursor of said oxides for example in the form of carbonates, hydroxides or other organometallic elements of the previous elements.
- precursors is meant a material which decomposes into the simple oxide corresponding to an often early stage of the heat treatment, that is to say at a heating temperature typically below 1000 ° C., or even below 800 ° C. even at 500 ° C.
- the mixture of precursors is sintered, that is to say that it is heated to a temperature allowing a reaction of the precursors to form grains comprising at least a majority of a phase of structure of the type Al 2 TiO 5 .
- the material according to the invention is synthesized from grains obtained by prior melting of the oxides Al 2 ⁇ 3, TiO 2 , and optionally MgO, ZrO 2 , SiO 2 or other oxides. (or their precursors).
- the grains are obtained according to the invention by electrofusion, which allows the manufacture of large quantities with attractive yields and a very good price / performance ratio.
- the successive steps of the manufacture of the grains by melting are for example: a) mixing the raw materials to form the feedstock; b) melting of the feedstock until the molten liquid is obtained; c) cooling said molten liquid so that the molten liquid is fully solidified, this cooling can be performed quickly, for example in less than 3 minutes; d) optionally, grinding said solid mass so as to obtain a mixture of grains.
- any other conventional or known method of manufacturing molten grains may also be implemented, provided that the composition of the feedstock makes it possible to obtain grains having a composition in accordance with the invention. that of the grains according to the invention.
- an electric arc furnace is preferably used, but all known furnaces are conceivable, such as an induction furnace or a plasma furnace, provided that they allow the initial charge to be completely melted.
- the firing is preferably carried out under neutral conditions, for example under argon, or oxidizing, preferably at atmospheric pressure.
- the cooling is preferably but not necessarily fast, that is to say so that the molten liquid is fully solidified in less than 3 minutes.
- it results from casting in CS molds as described in US Patent 3,993,119 or quenching.
- step d the solid mass is milled, according to conventional techniques, to obtain the size of the grains according to the present invention.
- a method of manufacturing such a structure from an initial mixture of grains according to the invention is in general the following:
- the grains obtained are mixed by sintering or melting as previously described.
- the melted grains have been ground in such a way that they have a suitable particle size, within the meaning of the present invention.
- the manufacturing method typically comprises a step of mixing the initial mixture of the grains with an organic binder of the methylcellulose type and a porogen, for example of the starch, graphite, polyethylene, PMMA, etc. type. and gradually adding water until the necessary plasticity is obtained to allow the extrusion step of the honeycomb structure.
- the mixture of grains is kneaded and 1 to 30% by weight of at least one porogenic agent chosen according to the desired pore size, then at least one organic plasticizer and / or or an organic binder and water.
- the kneading results in a homogeneous product in the form of a paste.
- the extrusion step of this product through a suitably shaped die makes it possible, according to well-known techniques, to obtain monoliths in the form of a honeycomb.
- the process may for example comprise a drying step of the monoliths obtained. During the drying step, the green ceramic monoliths obtained are typically dried by microwave or at a temperature and for a time sufficient to bring the water content not chemically bound to less than 1% by mass.
- the method may further comprise a plugging step of every other channel at each end of the monolith.
- the firing step of the monoliths whose filtering portion is based on aluminum titanate is in principle carried out at a temperature greater than 1300 ° C. but not exceeding 1800 ° C., preferably not exceeding 1750 ° C.
- the temperature is especially adjusted depending on the other phases and / or oxides present in the porous material.
- the monolith structure is brought to a temperature between 1300 and 1600 0 C 0 C under an atmosphere containing oxygen or an inert gas.
- the method may optionally comprise a step of assembling the monoliths in an assembled filtration structure according to well-known techniques, for example described in application EP 816 065.
- the filtering structure or porous ceramic material according to the invention is preferably of the honeycomb type. It has a suitable porosity and in general between 20 and 65%, preferably between 30 and 50%, the average pore size being ideally between 10 and 20 microns.
- Such filtering structures typically have a central portion comprising a set of adjacent ducts or channels of axes parallel to each other separated by walls constituted by the porous material.
- the ducts are closed by plugs at one or the other of their ends to delimit inlet chambers opening on a gas inlet face and outlet chambers opening. following a gas evacuation face, so that the gas passes through the porous walls.
- the present invention also relates to a filter or a catalytic support obtained from a structure as previously described and by deposition, preferably by impregnation, of at least one supported or preferably unsupported active catalytic phase, typically comprising at least one precious metal such as Pt and / or Rh and / or Pd and optionally an oxide such as CeO2, ZrO2, CeO2 ⁇ ZrO2.
- the catalytic supports also have a honeycomb structure, but the conduits are not plugged and the catalyst is deposited in the pores of the channels.
- TiO 2 in rutile form comprising more than 95% of TiO 2 and approximately 1% of zirconia and having a median diameter dso of about 120 microns, marketed by the company Europe Minerais,
- SiO 2 approximately 5% by weight of SiO 2 with a degree of purity greater than 99.5% and a median diameter of 5 o: 208 ⁇ m, marketed by the company SIFRACO,
- MgO approximately 4% by weight of MgO with a degree of purity greater than 98% with more than 80% of particles having a diameter of between 0.25 and 1 mm, sold by the company Nedmag.
- the mixture of the initial reactive oxides was melted in an electric arc furnace, under air, with an electric oxidizing step.
- the molten mixture was then cast into a CS mold so as to obtain rapid cooling.
- the product obtained is crushed and sieved to obtain powders of different size fractions. More specifically, the grinding and sieving are carried out under conditions allowing the final production of four size fractions:
- a particle size fraction is characterized by a median diameter d 5 o substantially equal to 30 microns, referred to as a large fraction according to the present invention
- a particle size fraction is characterized by a median diameter d 5 o substantially equal to 16 microns, referred to as a large fraction according to the present invention
- a particle size fraction is characterized by a median diameter d 5 o substantially equal to 1.5 microns, referred to as the fine fraction according to the present invention
- a particle size fraction characterized by a median diameter dso substantially equal to 0.7 microns referred to as the fine fraction according to the present invention.
- the median diameter d 5 o denotes the diameter of the particles, measured by sedigraphy, below which 50% by volume of the population is found.
- Microprobe analysis shows that all the grains of the melt phase thus obtained have the following composition, as a percentage by weight of the oxides:
- composition and nature of the phases present within the grains was also analyzed, the results of the analysis being given in Table 2. On the basis of these results, the weight percentage of each phase could be estimated by calculation.
- Bars of a porous ceramic material are conventionally obtained in the following manner: one or more granulometric fractions are mixed with 4% of an organic binder of the methylcellulose type and 15% by weight of a pore-forming agent. Water is added by kneading to obtain a homogeneous paste and whose plasticity allows the extrusion of a sample in the form of a section bar 8 mm x 6 mm and length 70 mm which is then sintered at 1450 0 C for 4 hours. On these samples, in order to estimate the value of the porous material in a "particle filter" application, the porous webs obtained in this way measure the MoR rupture modulus, the porosity characteristics and the sintering shrinkage.
- the conventional porosity characteristics are measured by the well-known high-pressure mercury porosimetry techniques using a Micromeritics 9500 porosimeter.
- the sintering shrinkage expresses the dimensional variation of the sample after sintering at 1450 ° C. More precisely, according to the invention, sintering shrinkage is understood to mean the average decrease in each of the two dimensions of the section of the material, which is persistent at low temperature, that is to say at a temperature below 400 0 C and in particular at room temperature.
- the reported value of the withdrawal corresponds to the average of the shrinkage for the two dimensions, expressed as a percentage of the initial dimension of the bar before sintering, for each of said dimensions. This feature is extremely important for estimating the feasibility of the porous structure manufacturing process. Indeed a strong sintering shrinkage implies that the honeycomb made of the material presents major difficulties of industrialization, in particular to obtain with an acceptable reproducibility structures whose dimensional characteristics can be guaranteed with sufficient precision to allow without difficulty the use especially in an automobile exhaust line.
- the modulus of rupture is determined at room temperature in 3-point bending on the porous webs of dimensions 60 mm ⁇ 6 mm ⁇ 8 mm obtained previously.
- the green monoliths obtained were cut and observed in order to check the homogeneity of the distribution of the material within the extruded honeycomb structure.
- Example 7 shows that problems of formatting and in particular Extrudability occurs when two large and fine fractions are used but the ratio of the median diameters of the fat and fine fractions is less than 12.
- Example 8 illustrates an embodiment in which three size fractions are used: a large fraction and a fine fraction according to the invention to which is added a fraction of intermediate size.
- Table 4 it can be seen in Table 4 that only the mixtures of grains in accordance with the invention as defined in the claims below allow the possible obtaining of materials:
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- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
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- Compositions Of Oxide Ceramics (AREA)
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Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
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EP09772744A EP2303797A2 (fr) | 2008-07-04 | 2009-07-02 | Melange de grains pour la synthese d'une structure poreuse du type titanate d'alumine |
JP2011515575A JP5491500B2 (ja) | 2008-07-04 | 2009-07-02 | チタン酸アルミニウム型の多孔質構造体を製造するための粒子混合物 |
US13/002,513 US8399376B2 (en) | 2008-07-04 | 2009-07-02 | Particle blend for synthesizing a porous structure of the aluminum titanate type |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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FR0854581A FR2933399B1 (fr) | 2008-07-04 | 2008-07-04 | Melange de grains pour la synthese d'une structure poreuse du type titanate d'alumine |
FR0854581 | 2008-07-04 |
Publications (2)
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WO2010001062A2 true WO2010001062A2 (fr) | 2010-01-07 |
WO2010001062A3 WO2010001062A3 (fr) | 2010-03-18 |
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PCT/FR2009/051292 WO2010001062A2 (fr) | 2008-07-04 | 2009-07-02 | Melange de grains pour la synthese d'une structure poreuse du type titanate d'alumine |
Country Status (6)
Country | Link |
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US (1) | US8399376B2 (fr) |
EP (1) | EP2303797A2 (fr) |
JP (1) | JP5491500B2 (fr) |
KR (1) | KR20110028332A (fr) |
FR (1) | FR2933399B1 (fr) |
WO (1) | WO2010001062A2 (fr) |
Cited By (3)
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US20120217669A1 (en) * | 2011-02-28 | 2012-08-30 | Balster Jean E | Method for Manufacturing Ceramic Honeycombs with Reduced Shrinkage |
CN107794393A (zh) * | 2016-09-05 | 2018-03-13 | 中南大学 | 一种微米级的低孔隙率多孔铝合金的制备方法 |
US10301222B2 (en) | 2014-11-19 | 2019-05-28 | Corning Incorporated | Ceramic powders with controlled size distribution |
Families Citing this family (3)
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FR2933401B1 (fr) * | 2008-07-04 | 2010-07-30 | Saint Gobain Ct Recherches | Structure poreuse du type titanate d'alumine |
EP3071538B1 (fr) * | 2013-11-20 | 2021-02-17 | Lummus Technology LLC | Catalyseur d'isomérisation de double liaison d'oléfine à haute résistance à l'empoisonnement |
JP2019147701A (ja) * | 2018-02-26 | 2019-09-05 | イビデン株式会社 | ハニカム構造体の製造方法 |
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WO2002081054A1 (fr) | 2001-04-09 | 2002-10-17 | Corning Incorporated | Corps de filtre poreux et procede |
WO2004011124A1 (fr) | 2002-07-31 | 2004-02-05 | Corning Incorporated | Filtre en titanate de mullite-aluminium pour echappements diesel |
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- 2009-07-02 EP EP09772744A patent/EP2303797A2/fr not_active Withdrawn
- 2009-07-02 US US13/002,513 patent/US8399376B2/en not_active Expired - Fee Related
- 2009-07-02 KR KR1020117000006A patent/KR20110028332A/ko not_active Application Discontinuation
- 2009-07-02 JP JP2011515575A patent/JP5491500B2/ja not_active Expired - Fee Related
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US20120217669A1 (en) * | 2011-02-28 | 2012-08-30 | Balster Jean E | Method for Manufacturing Ceramic Honeycombs with Reduced Shrinkage |
US9464004B2 (en) * | 2011-02-28 | 2016-10-11 | Corning Incorporated | Method for manufacturing ceramic honeycombs with reduced shrinkage |
CN108997005A (zh) * | 2011-02-28 | 2018-12-14 | 康宁股份有限公司 | 用于制造收缩减小的多孔陶瓷制品的方法 |
US10301222B2 (en) | 2014-11-19 | 2019-05-28 | Corning Incorporated | Ceramic powders with controlled size distribution |
CN107794393A (zh) * | 2016-09-05 | 2018-03-13 | 中南大学 | 一种微米级的低孔隙率多孔铝合金的制备方法 |
Also Published As
Publication number | Publication date |
---|---|
US20110190120A1 (en) | 2011-08-04 |
EP2303797A2 (fr) | 2011-04-06 |
JP5491500B2 (ja) | 2014-05-14 |
US8399376B2 (en) | 2013-03-19 |
FR2933399A1 (fr) | 2010-01-08 |
KR20110028332A (ko) | 2011-03-17 |
WO2010001062A3 (fr) | 2010-03-18 |
FR2933399B1 (fr) | 2011-02-18 |
JP2011526573A (ja) | 2011-10-13 |
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