WO2009027837A2 - Method for making porous ceramic articles with fugitive pore former - Google Patents

Method for making porous ceramic articles with fugitive pore former Download PDF

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Publication number
WO2009027837A2
WO2009027837A2 PCT/IB2008/003024 IB2008003024W WO2009027837A2 WO 2009027837 A2 WO2009027837 A2 WO 2009027837A2 IB 2008003024 W IB2008003024 W IB 2008003024W WO 2009027837 A2 WO2009027837 A2 WO 2009027837A2
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WO
WIPO (PCT)
Prior art keywords
ceramic
forming agent
green body
pore
cyclododecane
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PCT/IB2008/003024
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French (fr)
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WO2009027837A3 (en
Inventor
Yves Brocheton
David Henry
Michèle Fredholm
Claude Gille
Maxime Moreno
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Corning Incorporated
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Priority claimed from EP07301328A external-priority patent/EP2030957A1/en
Application filed by Corning Incorporated filed Critical Corning Incorporated
Priority to CN200880110037.2A priority Critical patent/CN101808955B/en
Publication of WO2009027837A2 publication Critical patent/WO2009027837A2/en
Publication of WO2009027837A3 publication Critical patent/WO2009027837A3/en

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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/16Shaped 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 silicates other than clay
    • C04B35/18Shaped 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 silicates other than clay rich in aluminium oxide
    • C04B35/195Alkaline earth aluminosilicates, e.g. cordierite or anorthite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/62605Treating the starting powders individually or as mixtures
    • C04B35/62645Thermal treatment of powders or mixtures thereof other than sintering
    • C04B35/62655Drying, e.g. freeze-drying, spray-drying, microwave or supercritical drying
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B38/00Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
    • C04B38/0006Honeycomb structures
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/00474Uses not provided for elsewhere in C04B2111/00
    • C04B2111/00793Uses not provided for elsewhere in C04B2111/00 as filters or diaphragms
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • C04B2235/6562Heating rate
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • C04B2235/6567Treatment time

Definitions

  • the disclosure relates to the manufacture of porous ceramic articles such as wall flow filters and flow through substrates, including filters and substrates comprising honeycomb structures, and more particularly to ceramic forming batch composition comprising a fugitive pore forming agent.
  • Porous ceramic honeycomb structures are useful for pollution control devices such as diesel particulate filters (DPFs).
  • DPFs diesel particulate filters
  • the porosity in the ceramic material is achieved by introducing pore former agents in the batch and subsequent burn off of these pore formers during the firing cycle to create voids or pores.
  • pore formers such as starches, graphite or a mixture of both induces severe complexities during both the drying and the firing of ceramic green bodies regarding generation of cracks.
  • the depth of penetration of microwaves during drying of green bodies can be limited due to the presence of pore formers such as graphite, or strong temperature gradients can occur in the green bodies during drying or firing; also, firing cycles may need to be tailored and lengthened to burn off the pore formers, leading to higher costs, more complexity, and reduced production rates particularly in the case of particulate filters such as DPFs where high porosity (e.g. greater than 50%) is required and consequently high levels of such pore formers are introduced, for example in amounts in super addition of the inorganic raw materials at greater than 40 wt%.
  • pore formers such as graphite, or strong temperature gradients can occur in the green bodies during drying or firing
  • firing cycles may need to be tailored and lengthened to burn off the pore formers, leading to higher costs, more complexity, and reduced production rates particularly in the case of particulate filters such as DPFs where high porosity (e.g. greater than 50%) is required and consequently high levels of such pore formers are introduced, for example in amounts
  • the disclosure relates generally to methods of manufacturing a ceramic forming batch compositions comprising a fugitive, optionally recoverable, pore forming agent such as cyclododecane.
  • a fugitive, optionally recoverable, pore forming agent such as cyclododecane.
  • the cyclododecane pore former features an ability to be removed from a green body using a simple drying process prior to any firing step.
  • the cyclododecane pore former can also be used in relatively high amounts, enabling the manufacture of porous ceramic articles with increased levels of porosity.
  • the disclosed batch composition enable the fabrication of highly porous ceramic substrates such as flow through substrates and particulate filters such as wall flow filters, such as those that are suitable for use as diesel particulate filters (DPFs) having higher catalyst loadings, low pressure drop, and high strengths.
  • highly porous ceramic substrates such as flow through substrates and particulate filters such as wall flow filters, such as those that are suitable for use as diesel particulate filters (DPFs) having higher catalyst loadings, low pressure drop, and high strengths.
  • DPFs diesel particulate filters
  • FIG. 1 illustrates exemplary cyclododecane particles.
  • FIG. 2 illustrates exemplary spherical cyclododecane particles.
  • FIG. 3 illustrates a comparison of the two ceramic honeycomb bodies prepared in Examples 5 and 6.
  • FIG. 4 illustrates a comparison of the two ceramic honeycomb bodies prepared in Examples 5 and 6.
  • FIG. 5 is a graphical comparison of two exemplary firing schedules used to fire certain batch composition in the appended Examples.
  • FIG. 6 is an illustration of the TGA weight loss and DSC thermal phenomenon in the heating of cyclododecane alone, an exemplary cordierite green body without any pore former (HP 300), and cordierite green body comprising a superaddition of 40 wt% cyclododecane, before and after drying.
  • FIG. 7 illustrates examples of porosity v. weight % of fugitive pore formers.
  • FIG. 8 shows TGA analysis weight losses during heat up of various batch compositions.
  • FIG. 9 schematically illustrates an embodiment of a method disclosed herein.
  • FIG. 10 shows examples of various grain size distributions of the fugitive pore former disclosed herein.
  • FIG. 11 is an SEM of a green body having porosity after fugitive pore former has been removed.
  • FIGS. 12-13 schematically illustrate embodiments of a means to recover the fugitive pore former (e.g. cold trap).
  • a "wt. %” or “weight percent” or “percent by weight” of a component is based on the total weight of the composition or article in which the component is included.
  • a "superaddition” refers to a weight percent of a component, such as for example, liquid vehicle, or pore former, based upon and relative to 100 weight percent of the ceramic forming inorganic powder batch component, such as an organic binder superaddition of 10 wt% to 100 wt% of the batch mixture resulting in a total weight percent of 110%.
  • Pore fraction refers to a percent by volume of the total porosity, as measured by mercury porosimetry, divided by 100. Accordingly, the parameters d-m, d 50 , and dg 0 are exemplary pore fractions that can be used to characterize the pore size distribution of ceramic articles manufactured by the batch compositions of the disclosure.
  • the quantity d 50 is the median pore size based upon pore volume, and is measured in micrometers; thus, d 5 o is the pore diameter at which 50% of the open porosity of the ceramic has been intruded by mercury.
  • the quantity d 90 is the pore diameter at which 90% of the pore volume is comprised of pores whose diameters are smaller than the value of d 90 ; thus, d 90 is equal to the pore diameter at which 10% by volume of the open porosity of the ceramic has been intruded by mercury.
  • the quantity d-io is the pore diameter at which 10% of the pore volume is comprised of pores whose diameters are smaller than the value of dio; thus, di 0 is equal to the pore diameter at which 90% by volume of the open porosity of the ceramic has been intruded by mercury.
  • the values of dio and dgo are also in units of micrometers.
  • a pore size distribution or df ac t o r can also be expressed by the quantity (d 50 -dio)/d 5 o and which describes the width of the distribution of pore sizes finer than the median pore size, d 5 o.
  • Fugitive pore formers or fugitive pore forming agents, as used herein generally refers to a compound which is solid at low temperature (and at or near atmospheric pressure) and volatilizes readily at temperature below 200°C, wherein the pore former is a compound preferably comprising at least two carbon atoms.
  • suitable fugitive pore formers include one or more compounds which is solid at low temperature, preferably having a melting point above 0 °C, more preferably above 20 0 C, and even more preferably above 25 °C, and volatilizesjeadily at temperature below 200°C and preferably below 100°C in order to be eliminated from a green body before decomposition of the binder (such as methylcellulose for example).
  • the fugitive pore former has a sufficiently high vapor pressure (P°) allowing elimination by volatilization (that is, sublimation or vaporization) at temperature below 200 0 C and preferably below 100 0 C.
  • the fugitive pore former agent comprises a compound that volatilize readily under atmospheric pressure below 200 0 C having a melting point above 0 0 C and having a vapor pressure (P°) at 25°C above 10 "6 atm.
  • vapor pressure
  • Preferred compounds are those having a melting point above 20°C and vapor pressure 10 "6 atm ⁇ P° ⁇ 10 "2 atm.
  • cryogenic conditions incompatible with the use of liquid water which is a typical solvent or liquid vehicle used in the batch composition to adjust the viscosity of the part to be extruded.
  • the fugitive pore former can be a terpene having a melting point above 0°C and preferably above RT, such as volatile cyclic terpenes like camphene, camphene tricyclene mixture. Camphene exhibits a high vapor pressure (2.0 10 3 Pa at 55°C) and low melting point of 44-48 °C.
  • the fugitive pore former can be a volatile aromatic compound such as naphthalene; naphthalene is a compound which could be removed by sublimation, and its elimination may be performed below the decomposition temperature by sublimation and vapors evacuated during the drying process, and naphthalene can be described as sublimable material, which can be used with other starches (graphite/carbon or starch).
  • the fugitive pore former can be a substituted aromatic compound like phenol, trimethylphenol, salicylic acid esters, p-dichlorobenzene and volatile hydrocarbons such as alicyclic hydrocarbons like cyclododecane or substituted alicyclic compounds such as menthol, camphor this list being indicative and not limitative.
  • a preferred fugitive pore former agent is is cyclododecane. This compound has a low melting point (58-63°C), an appropriate vapor pressure at room temperature (0.1 hPa) and can be easily shaped to form spherical granules.
  • FIG. 7 shows the increase of porosity achieved using particles of fugitive pore formers (cyclododecane, naphthalene and camphene) in comparison to the starting material (without pore formers).
  • the triangle is cyclododecane
  • the diamond is naphthalene
  • the circle is camphene.
  • Powders of fugitive pore formers have been prepared by crushing pieces of wax in a laboratory mixer. Samples (inorganic materials and pore formers) have been hand mixed and mulled, dried overnight in hot air and fired in electrical furnace.
  • the disclosure provides a plasticized ceramic precursor batch composition comprising ceramic forming inorganic batch components; and a pore forming agent comprising cyclododecane.
  • the plasticized ceramic precursor batch composition is capable of forming a porous ceramic article comprising a primary sintered phase composition.
  • the disclosure provides a method for manufacturing a porous ceramic honeycomb article. The method generally comprises first providing a plasticized ceramic forming precursor batch composition as summarized herein. A honeycomb green body can then be formed from the plasticized ceramic forming precursor batch composition. The honeycomb body can be dried under conditions to remove some or substantially all of the cyclododecane pore former prior to firing.
  • the formed honeycomb green body can then be fired under conditions effective to convert the green body into a porous ceramic honeycomb article. Additional embodiments of the disclosure are set forth, in part, in the detailed description, and any claims, and in part from the detailed description, or can be learned by practice of the invention. The foregoing general description and the detailed description are intended to be illustrative and demonstrative, and non- limiting.
  • the disclosure provides improved ceramic precursor batch compositions suitable for forming porous ceramic articles comprised of a primary sintered phase ceramic composition.
  • the disclosed batch compositions can be used to form porous sintered phase ceramic articles having relatively high total porosities without a resulting generation of cracks.
  • the batch compositions of the disclosure can also enable the use of simplified firing cycles to convert the batch compositions into primary sintered phase ceramic compositions.
  • the ceramic precursor batch compositions generally comprise at least one ceramic forming inorganic batch component and a cyclododecane pore forming agent and can further include an optional liquid vehicle, and an optional organic binder system.
  • the ceramic forming inorganic batch components can be selected to form, upon firing; any desired porous sintered phase ceramic composition, including for example a porous cordierite, mullite, spinel, aluminum titanate, or a mixture thereof.
  • Exemplary and non-limiting inorganic powder materials suitable for use in these inorganic ceramic powder batch mixtures can include, for example, cordierite, aluminum titanate, mullite, clay, kaolin, magnesium oxide sources, talc, zircon, zirconia, spinel, alumina forming sources, including aluminas and their precursors, silica forming sources, including silicas and their precursors, silicates, aluminates, lithium aluminosilicates, alumina silica, feldspar, titania, fused silica, nitrides, carbides, borides, e.g., silicon carbide, silicon nitride or mixtures of these.
  • the inorganic batch components can be selected to provide a primary sintered phase cordierite composition having the general formula [A] x [M]y[T] z Oi 8 , where A can be selected from the group consisting of alkali, alkaline earth, rare earth elements, CO 2 , H 2 O, and combinations thereof; M can be selected from the group consisting of Mg, Fe, Mn, Co, and combinations thereof; T is selected from the group consisting of Al, Si, Ga, Ge, and combinations thereof; and where 0 ⁇ x ⁇ 1.0, 1.9 ⁇ y ⁇ 2.1 , and 8.9 ⁇ z ⁇ 9.1.
  • M can be comprised of Mg
  • T can be comprised of Al, Si, or both.
  • the cordierite composition can be approximately represented by the formula. Mg 2 AI 4 Si 5 Oi 8 .
  • an exemplary cordierite phase can be expressed and characterized on an oxide weight percent basis as comprising from about 49 to about 53 percent by weight SiO 2 , from about 33 to about 38 percent by weight AI 2 O 3 , and from about 12 to about 16 percent by weight MgO.
  • An exemplary inorganic cordierite precursor powder batch composition preferably comprises about 33 to about 41 weight percent aluminum oxide source, about 46 to about 53 weight percent of a silica source, and about 11 to about 17 weight percent of a magnesium oxide source.
  • Additional exemplary and non- limiting inorganic batch component mixtures suitable for forming cordierite include those disclosed in U.S. Pat. Nos. 3,885,977; RE 38,888; 6,368,992; 6,319,870; 6,24,437; 6,210,626; 5,183,608; 5,258,150; 6,432,856; 6,773,657; 6,864,198; and U.S. Patent Application Publication Nos.: 2004/0029707; 2004/0261384.
  • the cordierite ceramic phases described herein can also comprise either orthorhombic or hexagonal crystal lattice symmetry, or may be comprised of a mixture of both such crystal structures.
  • the inorganic batch components can also be selected to provide a ceramic mullite composition consisting essentially of, as characterized in an oxide weight percent basis, from 27 to 30 percent by weight Si ⁇ 2 , and from about 68 to 72 percent by weight AI 2 O 3 .
  • An exemplary inorganic mullite precursor powder batch composition can comprise approximately 76% mullite refractory aggregate; approximately 9.0% fine clay; and approximately 15% alpha alumina. Additional exemplary non-limiting inorganic batch component mixtures suitable for forming mullite include those disclosed in U.S. Pat. Nos.: 6,254,822 and 6,238,618.
  • the inorganic batch components can also be selected to provide an alumina titanate composition consisting essentially of, as characterized in an oxide weight percent basis, from about 8 to about 15 percent by weight SiO 2 , from about 45 to about 53 percent by weight AI2O3, and from about 27 to about 33 percent by weight TiO 2 .
  • An exemplary inorganic aluminum titanate precursor powder batch composition can comprise about 10% quartz; about 47% alumina; about 30% titania; and about 13% additional inorganic additives.
  • Additional exemplary non-limiting inorganic batch component mixtures suitable for forming aluminum titanate include those disclosed in, for example, U.S. Pat. Nos.
  • An exemplary and non-limiting magnesium oxide source suitable for use in the batch composition can be talc.
  • a suitable talc can have a mean particle size of at least about 5 ⁇ m, at least about 8 ⁇ m, at least about 12 ⁇ m, or even at least about 15 ⁇ m.
  • the talc can be a platy talc.
  • a platy talc refers to talc that exhibits a platelet particle morphology, i.e., particles having two long dimensions and one short dimension, or, for example, a length and width of the platelet that is much larger than its thickness.
  • the talc possesses a morphology index greater than about 0.50, 0.60, 0.70, or 80.
  • the morphology index as disclosed in U.S. Pat. No. 5,141 ,686, is a measure of the degree of platiness of the talc.
  • One typical procedure for measuring the morphology index is to place the sample in a holder so that the orientation of the platy talc is maximized within the plane of the sample holder.
  • the x-ray diffraction (XRD) pattern can then be determined for the oriented talc.
  • the morphology index semi-quantitatively relates the platy character of the talc to its XRD peak intensities using the following equation:
  • magnesium oxide sources suitable for use in the disclosure include, Mistron 002, FCOR Talc, or both, and are available from Luzenac, Inc. of Oakville, Ontario, Canada, and 96-67 Talc available from Barrett's Minerals, Inc. of Dillon, Montana.
  • Exemplary alumina forming sources can include aluminum oxides or a compound containing aluminum which when heated to sufficiently high temperature yields essentially 100% aluminum oxide.
  • Non-limiting examples of alumina forming sources include corundum or alpha-alumina, gamma- alumina, transitional aluminas, aluminum hydroxide such as gibbsite and bayerite, boehmite, diaspore, aluminum isopropoxide and like materials.
  • Commercially available alumina sources can include relatively coarse aluminas, such as the Alcan C-700 series, having a particle size of about 4-6 micrometers, and a surface area of about 0.5-1 m 2 /g, e.g., C-714 and C- 701TM.
  • Relatively fine aluminas having a particle size of about 0.5-2 micrometers, and a surface area of about 8-11 m 2 /g, can also be used, such as A10 and A-16SG alumina, available from Alcoa.
  • the alumina forming source can be a colloidal alumina having particles sizes in the range of from 20nm to 50nm, such as the AL20 available from Nyacol.
  • the alumina source can also comprise a dispersible alumina forming source.
  • a dispersible alumina forming source can be, for example, an alumina forming source that is at least substantially dispersible in a solvent or liquid medium and that can be used to provide a colloidal suspension in a solvent or liquid medium.
  • a dispersible alumina source can be a relatively high surface area alumina source having a specific surface area of, for example, at least 20 m 2 /g.
  • a dispersible alumina source can have a specific surface area of at least 50 m 2 /g.
  • a suitable dispersible alumina source for use in the methods of the disclosure comprises, for example, alpha aluminum oxide hydroxide (AIOOH x ⁇ H 2 O) commonly referred to as boehmite, pseudoboehmite, and as aluminum monohydrate.
  • the dispersible alumina source can comprise the so-called transition or activated aluminas ⁇ i.e., aluminum oxyhydroxide and chi, eta, rho, iota, kappa, gamma, delta, and theta alumina) which can contain various amounts of chemically bound water or hydroxyl functionalities.
  • a silica source can comprise clay, such as for example, raw kaolin, calcined kaolin, or mixtures thereof.
  • Exemplary and non-limiting clays include non-delaminated kaolinite raw clay, having a particle size of about 7-9 micrometers, and a surface area of about 5-7 m 2 /g, such as Hydrite MPTM, those having a particle size of about 2-5 micrometers, and a surface area of about 10-14 m 2 /g, such as Hydrite PXTM and K-10 raw clay, delaminated kaolinite having a particle size of about 1 -3 micrometers, and a surface area of about 13-17 m 2 /g, such as KAOPAQUE-10TM, calcined clay, having a particle size of about 1-3 micrometers, and a surface area of about 6-8 m 2 /g, such as Glomax LL. All of the above named clay materials are available from Dry Branch Kaolin, Dry Branch, Ga.
  • the silica source can further comprise, if desired, a silica raw material including fused SiOa; colloidal silica; crystalline silica, such as quartz or cristobalite, or a low-alumina substantially alkali-free zeolite.
  • a commercially available quartz silica forming source includes, for example, Cerasil 300, Unimim Silverbond 200, and lmsil A25 Silica available from, Madison Clay Co., of Byesville, Ohio.
  • the silica forming source can comprise a compound that forms free silica when heated, for example, silicic acid or a silicon organo-metallic compound.
  • An exemplary titania source can include, for example, rutile, anatase titania, or combinations thereof.
  • optimization of the median particle size of the titania source can be used to avoid entrapment of unreacted oxide by the rapidly growing nuclei in the sintered ceramic structure. Accordingly, in embodiments, it may be preferred for the median particle size of the titania to be up to about 20 micrometers.
  • the inorganic batch components can optionally comprise one or more pre-reacted inorganic refractory fillers.
  • Exemplary pre- reacted inorganic refractory fillers can include powders of silicon carbide, silicon nitride, cordierite, aluminum titanate, calcium aluminate, beta- eucryptite, and beta-spodumene, as well as refractory aluminosilicate fibers formed, for example, by the processing of aluminosilicate clay.
  • the ceramic precursor batch composition can further comprise cyclododecane as a pore forming agent.
  • the cyclododecane pore forming agent or pore former is a fugitive material which evaporates or otherwise undergoes vaporization during drying or heating of the green body to obtain a desired, usually higher porosity, coarser median pore diameter, or both.
  • the use of a pore former enables one to tailor the porosity and pore size distribution in the resulting fired body for a particular application.
  • Cyclododecane exhibits a relatively low melting point, in the range of about 58-63°C, a vapor pressure at room temperature of about 0.1 hPa, and can be readily shaped to form spherical granules. Exemplary shaping techniques can include prilling from molten materials, grinding, spray drying, and like techniques.
  • U.S. Patent No. 5,185,108 describes exemplary methods for preparing wax particles having the appropriate size. Cyclododecane is commercially available from, for example, HANGLEITER Gmbh, Otzberg, Germany.
  • the cyclododecane can be utilized in any desired amount.
  • the cyclododecane can be presented as a superaddition in an amount of from about 20 weight percent to about 80 weight percent, including exemplary superaddition amounts such as 25 weight percent, 30 weight percent, 35 weight percent, 40 weight percent, 45 weight percent, 50 weight percent, 55 weight percent, 60 weight percent, 65 weight percent, 70 weight percent, 80 weight percent, intermediate amounts, and any range of amounts within these values.
  • cyclododecane as a pore forming agent in the batch compositions of the disclosure provides the ability to remove or evacuate the pore former during the drying step and prior to firing and reduced the formation of undesired cracks in the resulting fired ceramic structure. Further, evacuated or removed cyclododecane can, if desired, be recovered from the removal process and subsequently reused, thus reducing the costs associated with the use of conventional unrecoverable pore forming agents. [0040]When used in particulate form, the cyclododecane can be shaped and sized according to any predetermined specifications, further enabling one to obtain any desired pore structure properties, including for example, total porosity and mean pore size.
  • the cyclododecane can be present in particulate form, where the particles are substantially spherical in shape.
  • the cyclododecane particles can be substantially irregular or non-spherical in shape.
  • the cyclododecane particles can have any desired size, commonly characterized by the median particle diameter d 5 o. In some exemplary embodiments, the cyclododecane particles can have a median particle size of from 5 ⁇ m to about 150 ⁇ m.
  • the cyclododecane particles can have a median particle size of from 15 ⁇ m to about 120 ⁇ m, including for example, 25 ⁇ m, 35 ⁇ m, 45 ⁇ m, 55 ⁇ m, 60 ⁇ m, 65 ⁇ m, 75 ⁇ m, 85 ⁇ m, 95 ⁇ m, 105 ⁇ m, 115 ⁇ m, intermediate particle sizes and particle sizes in any range of sizes within these values.
  • the cyclododecane particles can have a median particle size d 50 of from about 80 ⁇ m to about 120 ⁇ m, about 90 ⁇ m to about 110 ⁇ m, or even about 95 ⁇ m to about 105 ⁇ m.
  • the inorganic batch components and the cyclododecane pore former component can be intimately blended with an optional organic binder, optional liquid vehicle, and one or more optional forming aids to impart plastic formability and green strength to the raw materials when they are shaped into a body.
  • exemplary organic binders can include cellulose ether such as methylcellulose, hydroxypropyl methylcellulose, methylcellulose derivatives, or combinations thereof.
  • the relative amounts of binder can vary depending on factors such as the nature and amounts of raw materials used. However, in embodiments, the binder can be present in the batch composition as a superaddition in an amount of from about 2 wt % to about 10 wt %.
  • the optional liquid vehicle component can also vary in amount and kind depending on the type of material used and to impart superior handling properties and compatibility with the other components in the ceramic batch mixture. If used, the liquid vehicle can be present as a superaddition in the range of from about 20 wt % to about 50 wt %.
  • the liquid vehicle component can comprise water.
  • an organic solvent for example, methanol, ethanol, and like solvents, or a mixture thereof, can also be used as the liquid vehicle.
  • Optional forming or processing aids can also include, for example, lubricants, surfactants, plasticizers, sintering aids, and even pore forming agents in addition to the cyclododecane.
  • Additional pore formers can include, for example, carbon, graphite, starch, wood, shell, nut flour, polymers such as polyethylene beads, waxes; or like materials, and combinations thereof. To that end, when used, these additional pore formers can also be presized or shaped to provide a subsequent porosity having desired characteristics.
  • Exemplary lubricants can include, for example, hydrocarbon oil, tall oil, sodium stearate, or like materials, and combinations thereof.
  • An exemplary plasticizer for use in preparing the batch composition can include, for example, glycerine, or like materials.
  • Suitable sintering aids can generally include, for example, an oxide source of one or more metals such as strontium, barium, iron, magnesium, zinc, calcium, aluminum, lanthanum, yttrium, titanium, bismuth, tungsten or like materials, and combinations thereof.
  • a superior optional sintering aid can comprise, for example, a mixture of a strontium oxide source, a calcium oxide source, an iron oxide source, or like materials, and combinations thereof.
  • an optional sintering aid can comprise at least one rare earth metal, and combinations thereof.
  • the sintering aid can be added to the batch composition, for example, in powder form, liquid form, or in combination.
  • the resulting ceramic precursor batch composition can be shaped into a green body by any known conventional forming process, e.g., extrusion, injection molding, slip casting, centrifugal casting, pressure casting, dry pressing, and like methods.
  • extrusion can be done using a hydraulic ram extrusion press, or a two stage de-airing single auger extruder, or a twin screw mixer with a die assembly attached to the discharge end, or like implementations.
  • proper screw elements are selected according to material considerations and other process conditions to build up sufficient pressure to force the batch material through the die.
  • a process is described herein for making a ceramic body (e.g. cordierite) with the use of a sizable and recoverable (and reusable) pore former (such as cyclododecane).
  • a sizable and recoverable (and reusable) pore former such as cyclododecane.
  • An illustrative process flow chart is show in FIG. 9.
  • the fugitive pore former (such as cyclododecane) is delivered in granules or in the form of a block of material.
  • the cyclododecane is preferably sized and shaped in accordance of the porosity to generate in the fired body. Shaping in spherical form can be obtained by a prilling process comprising spraying the molten material in a freezer.
  • Several parameters like the air pressure (in the case of air assisted atomizing system), the liquid pressure and temperature, the spraying nozzle diameter and positioning will define the particle grain size distribution as can be seen in FIG. 10.
  • the batch composition is obtained by blending together (i) a cordierite-providing raw material or raw material mixture; (ii) an adequate proportion of cyclododecane, previously shaped in the desired form, acting as the main (or only) pore-forming agent; (iii) optionally one or more additional known pore-forming agents such as starches and/or graphite; (iv) optionally a mixture of organic binders, surfactants, lubricants, and plasticizers; and (v) optionally a solvent media such as water or alcohol. [0048]
  • the resulting mixture can then be formed into a shape, preferably by extrusion, but other methods such as pressing, slip casting, or injection molding could be used.
  • Dielectric drying, or microwave drying, or a combination dielectric /hot air can be used to dry (remove water) from the shaped article to form a dried green body which is subsequently fired into an article of porous ceramic material.
  • the fugitive pore former can be removed by blowing hot air through the honeycomb structure (preferably in the direction of the axis of extrusion). During drying the green body is kept at sufficiently high temperature to remove substantially all or the entire fugitive pore former agent from the green body (but lower than the organic binder (methylcellulose for instance) decomposition temperature). In some embodiments, the green body is exposed to air at temperatures from 75 to 100°C to remove the pore former. The pore former removal can be controlled by way of weight loss measurement. The pore former removal step can be done simultaneously with the water removal step (hot air blowing in combination with microwave drying).
  • Recoverable pore-former collection allow reuse of the pore-former and can be accomplished by, for example, cold trap equipment (FIGS. 12 & 13) with process conditions given as follow as examples: the hot air flow exits the honeycomb and is conveying the removed pore former (e,g, cyclododecane) to a cold trap which condenses the pore former. Temperature of the trap is set at 10 0 C during the collection step. Once the trap gets saturated with pore former, the temperature of the trap is increased to 65°C allowing the melting and recovery of the pore former. [0053] The melted pore-former can be cooled down or immediately redirected to the shaping process to be processed again (as no degradation or decomposition occurred to the pore former during the previous process steps).
  • the hot air flow exits the honeycomb and is conveying the removed pore former (e,g, cyclododecane) to a cold trap which condenses the pore former. Temperature of the trap is set at 10 0
  • the green body is then fired at a sufficient temperature to provide a sintered, porous, ceramic (e.g. cordierite) article.
  • a sintered, porous, ceramic e.g. cordierite
  • exothermal phenomenon during the firing are considerably reduced. Faster heating rate and/or lower sensitivity to oxygen levels during firing could be expected.
  • the recoverable pore former is not burnt (or reacted or decomposed) and thus green house gases generation can be reduced as compared to known pore former removal steps.
  • the batch compositions of the disclosure can be used to form multicellular honeycomb structures having a high filter volumetric heat capacity, a low pressure drop between the entrance and exit faces of the filter, a low coefficient of thermal expansion (CTE), and high filtration efficiency, and are thus well suited for use as particulate filters like wall flow filters such as diesel particulate filters.
  • the blended ceramic precursor batch composition can be formed or otherwise shaped into a honeycomb configuration.
  • the geometry of the honeycomb configuration need not be restricted to any particular configuration.
  • an exemplary formed honeycomb body can be configured to provide a wall flow filter comprising a plurality of cell channels bounded by porous channel walls that extend longitudinally from an upstream inlet end to a downstream outlet end.
  • a first portion of the plurality of cell channels can comprise end plugs sealed to the respective channel walls at the downstream outlet end to form exhaust gas flow inlet cell channels and a second portion of the plurality of cell channels can comprise end plugs sealed to the respective channel walls at the upstream inlet end to form exhaust gas flow outlet cell channels.
  • the formed honeycomb structure can, for example, be a cylinder having end surfaces with a shape of a circle or an ellipse, a prism having the end surfaces with a shape of a polygon such as a triangle or a square, a shape in which the sides of cylinders or prisms are bent like a "doglegged" shape, or like shapes.
  • the shape of through holes or exhaust gas inlet and outlets is not particularly limited.
  • the cross-sectional shape may be a polygon such as a square, an octagon, a circle, an ellipse, or like shapes, and combinations thereof.
  • Exemplary non-limiting examples of formed honeycombs produced by the process and batch compositions of the disclosure can comprise cell densities of from about 235 cells/cm 2 (about 1 ,500 cells/in 2 ) to about 15 cells/cm 2 (about 100 cells/in 2 ), including those having about 94 cells/cm 2 (about 600 cells/in 2 ), about 62 cells/cm 2 (about 400 cells/in 2 ), or about 47 cells/cm 2 (about 300 cells/in 2 ), those having about 31 cells/cm 2 (about 200 cells/in 2 ), or those having about 15 cells/cm 2 (about 100 cells/in 2 ).
  • the wall or web thicknesses can typically be from about 0.07 to about 0.6 mm (about 3 to about 25 mils).
  • the particular desired size and shape of the ceramic body can depend on the application, e.g., in automotive applications by engine size and space available for mounting, and like considerations.
  • the ceramic articles of the disclosure can be suitable for preparing thin-walled honeycombs, the disclosed mixtures can also be used for thicker walled structures.
  • honeycombs structures having about 15 to about 30 cells/cm 2 (about 100 to about 200 cells/in 2 ) and about 0.30 to about 0.64 mm (about 12 to about 25 mil) wall thicknesses are well suited for particulate filter applications such as diesel particulate filters.
  • the formed green body having a desired size and shape as disclosed herein can then be dried under conditions effective to remove any excess liquids, such as moisture, and to remove the cyclododecane pore former.
  • the drying conditions can depend, at least in part, upon the particular choice of materials used to prepare the batch composition.
  • suitable drying conditions can comprise, for example, heating the formed green body at a temperature of about 50° to about 150 0 C for a sufficient time to eliminate the fugitive cyclododecane pore former.
  • Sufficient time can also vary but, in embodiments, can be, for example, from about 24 to about 72 hours.
  • the drying step can be performed by any known means, including hot air, microwave, steam, or dielectric drying, or like methods, and can optionally be followed by ambient air drying.
  • the dried green body can be fired under conditions effective to convert the dried green body into a ceramic article comprising a primary crystalline phase ceramic composition.
  • the firing conditions effective to convert the green body into a ceramic article can vary depending on a number of conditions, such as the specific composition, size of the green body, the type of equipment used, and like considerations. Therefore, excellent firing conditions to obtain a ceramic article according to the disclosure can be readily ascertained.
  • exemplary firing conditions can be, for example, heating at a maximum soak temperature of about 1 ,400 0 C to about 1 ,600°C, and for a maximum soak time about 1 hour to about 6 hours.
  • exemplary firing conditions can be, for example, heating the green body at a maximum soak temperature of about 1 ,350 0 C to about 1 ,450 0 C and for a maximum soak time of from about 5 to about 50 hours, including exemplary ranges of 10 to 40 hours, or even 15 to 30 hours.
  • an exemplary firing schedule for cordierite forming compositions can include firing at a soak temperature of about 1 ,400 0 C to about 1 ,425°C for a hold or soak time of about 10 to about 35 hours.
  • the resulting fired ceramic bodies of the disclosure can exhibit total porosities %P, as measured by mercury porosimetry, of about 50% to about 80%, including total porosities of, for example, 55%, 60%, 65%, 70%, 75%, and intermediate porosities values.
  • the total porosity can be, for example, of about 55% to about 75%, of about 60% to about 70%, or like porosities.
  • the median pore diameter, d 50 , of the pores present in the resulting ceramic articles can be, for example, from about 8 ⁇ m to about 35 ⁇ m. In other embodiments, the median pore diameter can be from about 10 ⁇ m to about 30 ⁇ m, or from about 15 ⁇ m to about 25 ⁇ m.
  • the following examples provide those of skill in the art with a complete description of how the ceramic precursor batch compositions, ceramic articles, and methods can be accomplished and evaluated. They are exemplary and non-limiting. Efforts have been made to ensure accuracy with respect to numbers (e.g., amounts, temperatures, etc.); however, some variation or deviation may be present. Unless indicated otherwise, parts are parts by weight, temperature is degrees C or is ambient temperature, and pressure is at or near atmospheric. [0064] In the following examples, a series of seven cordierite forming batch compositions were prepared.
  • All seven batch formulation were prepared from a raw material mixture containing 38.5 wt% of a 22 micron talc screened to - 325 mesh, 12,5 wt% of a 10 micron kaolin, 12.4 wt% of a 9 micron corundum screened to -325 mesh, 21.0 wt% of a 4.6 micron aluminum hydroxide, 15.4 wt% of a 25 micron quartz powder.
  • the resulting mixtures were also blended with 4.45 wt% methylcellulose binder and 0.56 wt% sodium stearate lubricant.
  • batch compositions 1 , 2 and 5 each contained a 40.0 wt% superaddition of a 49 micron potato starch.
  • Examples 3, 4, 6, and 7 each contained a 40.0 wt% superaddition of cyclododecane.
  • the coefficient of thermal expansion (CTE) was obtained by dilatometry on a specimen parallel to the lengths of the channels of the honeycomb article ("axial direction") over the temperature range of 25 to 800 0 C and in units of 10 '7 /°C.
  • the %porosity describes the total volume percentage of porosity in the walls of the article as measured by mercury porosimetry.
  • the terms dTM, d 5 o, and d 90 denote the pore diameters, in microns, or micrometers (10 "6 meters), at which 10%, 50%, and 90% of the total pore volume are of a finer pore diameter, respectively, as measured by mercury porosimetry.
  • d 90 is the pore diameter at which 90% (by volume) of the pores have a smaller diameter (equal to the pore diameter at which the cumulative mercury intrusion volume equals 10% of the total mercury intrusion volume).
  • All modulus of rupture (MOR), or flexural strength, values were measured at room temperature by the four-point method on a cellular bar (0.5 inch x 0.25 inch x 3 inches long) parallel to the axial direction of the honeycomb.
  • batch composition 3 which utilized cyclododecane as the pore former, provided desirable properties without the formation of cracks.
  • batch composition 4 which also comprised cyclododecane, provided properties similar to those of batch composition 3, except for the formation of cracks during the firing process.
  • the generation of cracks was believed to be a result of the batch composition being fired in a wet state without having been dried to remove the cyclododecane prior to firing.
  • batch composition 6 also illustrates that when the cyclododecane pore former was used, a firing cycle including a faster ramp of heating rate can be employed to sinter the body without the formation of undesirable cracks.
  • batch composition 5 comprising potato starch as the pore former, resulted in a sintered composition exhibiting cracks which precluded any CTE or strength measurements.
  • FIG. 3 and FIG. 4 As shown in FIG 3, the honeycomb article 10 comprised of 40% potato starch and corresponding to batch composition 5, contains a large crack along the exterior surface or skin of the article.
  • FIG. 5 further illustrates schematically a comparison of the relatively faster firing cycle 3, utilized for the firing of batch compositions 5, 6, and 7, compared to the slower firing cycle 2 used for the firing of batch composition 2, 3 and 4.
  • Firing cycle 3 is schematically represented by line 30.
  • Firing cycle 2 is schematically represented by line 40.
  • cyclododecane can be evacuated at relatively low temperatures, such as below about 250°C.
  • the heating of the dry green cordierite parts without pore formers shows a decrease of weight occurring between about 250°C and about 300°C corresponding to the burn- out of organic binders, as shown by curve 60.
  • the heating of wet cordierite green parts comprising 40% of cyclododecane exhibits losses between room temperature and about 350°C due to removal of water, binders and the cyclododecane, as shown by curve 70.
  • curve 80 the heating of the dry part including 40% of cyclododecane follows a curve similar to that obtained for the dry green part without any pore formers.
  • Table 2 reports measured porosities on hand made samples in order to estimate the increase of porosity due to addition of fugitive pore former. All samples (except example 8) have been prepared using the following conditions: (1) grinding of pore former agent, (2) addition to inorganic components previously mixed, (3) mixing with a mixer, (4) mulling with a rolling pin, (5) cutting in square, (6) overnight drying in hot air at 100 0 C, and then, (6) firing in electrical furnace following the indicated cycle. In comparison, example 8 is an extruded part, fired in the same conditions, is prepared using standard conditions.
  • Example 9 (without pore former) represents the baseline of porosity resulting of packing of raw materials used
  • Examples 10 to 15 illustrate the increase of porosity resulting of addition of fugitive pore formers to the reference batch. Some exemplary results are plotted on FIG. 10.
  • TGA Thermal analysis
  • TSPHT (MOR25°C /E500°C)
  • Table 3 illustrates that fugitive pore formers could be used in conjunction with other known pore formers. All samples included in Table 3 are extruded from paste made using a known extrusion process. [0078] Porosity of all formulations described in the table is achieved using a mixture of pore forming agents. Examples 16 and 18 illustrate the ability of fugitive pore formers to be used conjointly with another pore former (starches and/or graphite). Example 19 reports representative properties achieved with a mixture of starch and graphite commonly put in the batch to gain porosity. Examples 16 and 18 illustrate that a mixture of pore former including at lest one fugitive pore former is possible to obtain similar range of properties.
  • the manufacturing process of the present invention can provide advantages compared to known processes.
  • the present invention provides no pore former burn out and thus reduces CO or CO 2 production or both. With no pore former burning during firing, a benefit on the firing cycle could be expected, especially with high pore former compositions.
  • the pore former can be sized to the desired grain size. Linked to the collection and recapture of the pore former, an economical advantage over lost pore formers could be realized.
  • Some fugitive pore former agents can also benefit the extrusion process for example when a waxy material like cyclododecane is used, the waxy material can act as an aid for extrusion.
  • Ceramic honeycomb bodies such as cordierite or aluminum titanate bodies
  • the present invention describes such bodies and methods for their manufacture.
  • the bodies of the present invention can exhibit a porosity similar or higher than those existing in the prior art. This is achieved using at least one fugitive pore former or a mixture including a fugitive pore former and known pore formers such as starches or graphite, wherein the fugitive pore former is removed at low temperature (preferably during the drying step), preferably without generation of cracks.
  • the invention may enable the fabrication of highly porous converter substrates or particulate filters for higher catalyst loadings while maintaining low pressure drop and high strength.
  • a method for manufacturing a porous ceramic honeycomb article comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent is capable of volatilizing at a temperature below 200°C at atmospheric pressure; forming a green body from the ceramic forming precursor batch composition; and firing the honeycomb green body under conditions effective to convert the ceramic forming precursor batch composition in the green body into a porous ceramic material, wherein the green body is converted into the porous ceramic honeycomb article.
  • the pore forming agent comprises a volatile hydrocarbon, which may be an alicyclic hydrocarbon; a preferred fugitive pore forming agent is cyclododecane.
  • the pore forming agent comprises a substituted alicyclic hydrocarbon, such as menthol or camphor or a combination thereof.
  • substantially all, and even more preferably all, of the fugitive pore forming agent volatilizes and exits the green body prior to the firing.
  • the green body is heated sufficiently to cause substantially all of the fugitive pore forming agent to volatilize and exit the green body prior to the firing.
  • the fugitive pore forming agent volatilizes and exits the green body prior to the conversion of the ceramic forming precursor batch composition into the porous ceramic material.
  • the fugitive pore forming agent is captured or recovered, such as by cold trap, after exiting the green body.
  • the captured fugitive pore forming agent can then be mixed with an additional amount of the ceramic forming inorganic batch components and formed into another green body, thus recycling the fugitive pore former.
  • the ceramic forming precursor batch composition further comprises a binder.
  • the method can further comprise heating the green body sufficient to decompose the binder, wherein the fugitive pore forming agent is preferably removed from the green body prior to decomposition of the binder.
  • An example of the binder is one which comprises methylcellulose.
  • the fugitive pore forming agent has a melting point above 0 0 C. In other embodiments, the fugitive pore forming agent has a melting point above 20 0 C. In other embodiments, the fugitive pore forming agent has a melting point above 25 0 C.
  • the fugitive pore forming agent has a melting point between 50 0 C and 75 0 C. In some embodiments, the fugitive pore forming agent has a melting point between 55 0 C and 65 0 C.
  • the fugitive pore forming agent has a vapor pressure at 25 0 C above 1 x 10-6 atm. In some embodiments, the fugitive pore forming agent has a vapor pressure at 25 0 C above 5 x 10-5 atm. In some embodiments, the fugitive pore forming agent has a vapor pressure at
  • the fugitive pore forming agent has a melting point above 0 0 C and a vapor pressure at 25 0 C above 10-6 atm.
  • the fugitive pore forming agent has a melting point above 0 0 C and a vapor pressure at 25 0 C between 5 x 10-5 atm and 2 x
  • the fugitive pore forming agent has a melting point between 50 0 C and 75 0 C and a vapor pressure at 25 0 C between 5 x 10-5 atm and 2 x 10-3 atm. [0096] In some embodiments, the fugitive pore forming agent volatilizes below 200 0 C at atmospheric pressure. In some embodiments, the fugitive pore forming agent volatilizes below 100 0 C at atmospheric pressure. [0097] Preferably, the fugitive pore forming agent volatilizes by sublimation or evaporation. [0098] In some embodiments, the fugitive pore forming agent has a melting point above 0 0 C and a vapor pressure at 25 0 C above 10-6 atm.
  • the fugitive pore forming agent has a melting point above 20 0 C and a vapor pressure at 25 0 C between 10-6 atm and 10-2 atm.
  • the ceramic forming precursor batch composition is free of starch, graphite, or combinations thereof.
  • the pore former has a median particle size d50 of from 5 ⁇ m to 150 ⁇ m, in other some embodiments from 5 ⁇ m to 120 ⁇ m, in other embodiments from 5 ⁇ m to 50 ⁇ m, and in some embodiments from 15 ⁇ m to 50 ⁇ m.
  • the ceramic article has a total porosity (%P) of from 30% to 90%, and a median pore size (d50) of from 5 ⁇ m to 40 ⁇ m. In other embodiments, the ceramic article has a total porosity (%P) of from 60% to about 70%, and a median pore size (d50) of from about 5 ⁇ m to about 25 ⁇ m.
  • a ceramic precursor batch composition comprising ceramic forming inorganic batch components and a pore forming agent comprising cyclododecane.
  • a method for manufacturing a porous ceramic article comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent comprises an alicyclic hydrocarbon; and firing the ceramic forming precursor batch composition under conditions effective to convert the ceramic forming precursor batch composition into a porous ceramic material.
  • a preferred embodiment is cyclododecane.
  • a plasticized ceramic precursor batch composition comprising: ceramic forming inorganic batch components; and a pore forming agent comprising cyclododecane.
  • the ceramic forming inorganic batch components are selected to provide a sintered phase cordierite composition; the sintered phase cordierite composition can be characterized in some embodiments on an oxide weight basis as consisting essentially of: about 49 to about 53 percent by weight SiO2, about 33 to about 38 percent by weight AI2O3, and about 12 to about 16 percent by weight MgO.
  • the ceramic forming inorganic batch components are selected to provide a sintered phase mullite composition.
  • the ceramic forming inorganic batch components are selected to provide a sintered phase aluminum titanate composition. In other embodiments, the ceramic forming inorganic batch components are selected to provide a sintered phase silicon carbide composition.
  • the cyclododecane has a median particle size d50 of from about 5 ⁇ m to about 150 ⁇ m. In some embodiments, the cyclododecane is present as substantially spherical particles.
  • the batch composition is formed into a predetermined shape, such as a honeycomb structure.
  • the plasticized ceramic precursor batch composition further comprises a liquid vehicle and an organic binder system.
  • a method for manufacturing a porous ceramic honeycomb article comprising the steps of: providing a plasticized ceramic forming precursor batch composition comprising: ceramic forming inorganic batch components and a pore forming agent comprising cyclododecane; forming a honeycomb green body from the plasticized ceramic forming precursor batch composition; and firing the honeycomb green body under conditions effective to convert the green body into a porous ceramic honeycomb article.
  • the ceramic forming inorganic batch components can be selected to provide at least one of a sintered phase cordierite composition, sintered phased mullite composition, a sintered phase aluminum titanate composition, or combinations thereof.
  • the ceramic forming inorganic batch components can be are selected to provide a sintered phase cordierite composition, as characterized on an oxide weight basis, consisting essentially of: about 49 to about 53 percent by weight SiO2; about 33 to about 38 percent by weight AI2O3; and about 12 to about 16 percent by weight
  • the cyclododecane pore former is present in the plasticized ceramic forming precursor batch composition having a predetermined size and shape. In some embodiments, the cyclododecane pore former is present in the plasticized ceramic forming precursor batch composition as substantially spherical particles; in some embodiments, the substantially spherical cyclododecane particles have a median particle size d50 of from about 5 ⁇ m to about 150 ⁇ m. In some embodiments, the step of forming the honeycomb green body comprises shaping the plasticized ceramic forming precursor batch composition into a honeycomb shape, and drying the shaped plasticized ceramic forming precursor composition under conditions effective to at least remove some of the cyclododecane pore former.
  • effective firing conditions comprise firing the honeycomb green body at a soak temperature at from about 1300 0 C to about 1450 0 C, and subsequently holding the soak temperature for a period of time sufficient to convert the honeycomb green body into a ceramic honeycomb article.
  • the soak temperature is achieved by increasing temperature from 1150 0 C to the soak temperature at a rate of increase greater than 100 0 C per hour.
  • the plasticized ceramic forming precursor batch composition further comprises a liquid vehicle and an organic binder system.
  • the step of forming the honeycomb green body comprises shaping and then drying the shaped plasticized ceramic forming precursor composition under conditions effective to remove substantially all of the cyclododecane pore former.
  • a green honeycomb article comprising ceramic forming precursor materials and a cyclododecane pore former.

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Abstract

Disclosed are ceramic precursor batch compositions for forming porous ceramic articles. The ceramic forming precursor batch compositions include ceramic forming inorganic batch components and a recoverable pore forming agent such as cyclododecane. Also disclosed are methods for manufacturing porous ceramic articles, in particular porous ceramic honeycomb articles.

Description

METHOD FOR MAKING POROUS CERAMIC ARTICLES WITH FUGITIVE PORE FORMER
[0001] The entire disclosure of any publication, patent, or patent document mentioned herein is incorporated by reference.
Field
[0002] The disclosure relates to the manufacture of porous ceramic articles such as wall flow filters and flow through substrates, including filters and substrates comprising honeycomb structures, and more particularly to ceramic forming batch composition comprising a fugitive pore forming agent.
Background
[0003] Porous ceramic honeycomb structures are useful for pollution control devices such as diesel particulate filters (DPFs). The porosity in the ceramic material is achieved by introducing pore former agents in the batch and subsequent burn off of these pore formers during the firing cycle to create voids or pores. The use of pore formers such as starches, graphite or a mixture of both induces severe complexities during both the drying and the firing of ceramic green bodies regarding generation of cracks. For example, the depth of penetration of microwaves during drying of green bodies can be limited due to the presence of pore formers such as graphite, or strong temperature gradients can occur in the green bodies during drying or firing; also, firing cycles may need to be tailored and lengthened to burn off the pore formers, leading to higher costs, more complexity, and reduced production rates particularly in the case of particulate filters such as DPFs where high porosity (e.g. greater than 50%) is required and consequently high levels of such pore formers are introduced, for example in amounts in super addition of the inorganic raw materials at greater than 40 wt%. Summary
[0004] The disclosure relates generally to methods of manufacturing a ceramic forming batch compositions comprising a fugitive, optionally recoverable, pore forming agent such as cyclododecane. The cyclododecane pore former features an ability to be removed from a green body using a simple drying process prior to any firing step. In addition, the cyclododecane pore former can also be used in relatively high amounts, enabling the manufacture of porous ceramic articles with increased levels of porosity. Accordingly, the disclosed batch composition enable the fabrication of highly porous ceramic substrates such as flow through substrates and particulate filters such as wall flow filters, such as those that are suitable for use as diesel particulate filters (DPFs) having higher catalyst loadings, low pressure drop, and high strengths.
Brief Description of the Drawings
[0005] The accompanying drawings illustrate embodiments of the disclosure and with the description further explain, without limitation, the disclosure.
[0006] FIG. 1 illustrates exemplary cyclododecane particles. [0007] FIG. 2 illustrates exemplary spherical cyclododecane particles. [0008] FIG. 3 illustrates a comparison of the two ceramic honeycomb bodies prepared in Examples 5 and 6.
[0009] FIG. 4 illustrates a comparison of the two ceramic honeycomb bodies prepared in Examples 5 and 6. [0010] FIG. 5 is a graphical comparison of two exemplary firing schedules used to fire certain batch composition in the appended Examples. [0011] FIG. 6 is an illustration of the TGA weight loss and DSC thermal phenomenon in the heating of cyclododecane alone, an exemplary cordierite green body without any pore former (HP 300), and cordierite green body comprising a superaddition of 40 wt% cyclododecane, before and after drying. [0012] FIG. 7 illustrates examples of porosity v. weight % of fugitive pore formers.
[0013] FIG. 8 shows TGA analysis weight losses during heat up of various batch compositions. [0014] FIG. 9 schematically illustrates an embodiment of a method disclosed herein.
[0015] FIG. 10 shows examples of various grain size distributions of the fugitive pore former disclosed herein.
[0016] FIG. 11 is an SEM of a green body having porosity after fugitive pore former has been removed.
[0017] FIGS. 12-13 schematically illustrate embodiments of a means to recover the fugitive pore former (e.g. cold trap).
Detailed Description [0018] Various embodiments of the disclosure will be described in detail with reference to drawings, if any. Reference to various embodiments does not limit the scope of the invention, which is limited only by the scope of the claims attached hereto. Additionally, any examples set forth in this specification are not intended to be limiting and merely set forth some of the many possible embodiments for the claimed invention.
[0019] Singular forms "a," "an" and "the" include, plural referents unless the context clearly dictates otherwise. Thus, for example, reference to a "pore forming agent" includes embodiments having two or more such pore forming agents unless the context clearly indicates otherwise. [0020] "Include," "includes," or like terms means including but not limited to. [0021] Ranges can be expressed herein as from "about" one particular value, to "about" another particular value. When such a range is expressed, another embodiment includes from the one particular value to the other particular value. Similarly, when values are expressed as approximations, by use of the antecedent "about," it will be understood that the particular value forms another embodiment. It will be further understood that the endpoints of each of the ranges are significant both in relation to the other endpoint, and independently of the other endpoint.
[0022] A "wt. %" or "weight percent" or "percent by weight" of a component, unless specifically stated to the contrary, is based on the total weight of the composition or article in which the component is included.
[0023] A "superaddition" refers to a weight percent of a component, such as for example, liquid vehicle, or pore former, based upon and relative to 100 weight percent of the ceramic forming inorganic powder batch component, such as an organic binder superaddition of 10 wt% to 100 wt% of the batch mixture resulting in a total weight percent of 110%.
[0024] "Optional" or "optionally" means that the subsequently described event or circumstance may or may not occur, and that the description includes instances where said event or circumstance occurs and instances where it does not. [0025] "Pore fraction" refers to a percent by volume of the total porosity, as measured by mercury porosimetry, divided by 100. Accordingly, the parameters d-m, d50, and dg0 are exemplary pore fractions that can be used to characterize the pore size distribution of ceramic articles manufactured by the batch compositions of the disclosure. The quantity d50 is the median pore size based upon pore volume, and is measured in micrometers; thus, d5o is the pore diameter at which 50% of the open porosity of the ceramic has been intruded by mercury. The quantity d90 is the pore diameter at which 90% of the pore volume is comprised of pores whose diameters are smaller than the value of d90; thus, d90 is equal to the pore diameter at which 10% by volume of the open porosity of the ceramic has been intruded by mercury. The quantity d-io is the pore diameter at which 10% of the pore volume is comprised of pores whose diameters are smaller than the value of dio; thus, di0 is equal to the pore diameter at which 90% by volume of the open porosity of the ceramic has been intruded by mercury. The values of dio and dgo are also in units of micrometers. A pore size distribution or dfactor can also be expressed by the quantity (d50 -dio)/d5o and which describes the width of the distribution of pore sizes finer than the median pore size, d5o.
[0026] Fugitive pore formers, or fugitive pore forming agents, as used herein generally refers to a compound which is solid at low temperature (and at or near atmospheric pressure) and volatilizes readily at temperature below 200°C, wherein the pore former is a compound preferably comprising at least two carbon atoms.
[0027] In some embodiments, suitable fugitive pore formers include one or more compounds which is solid at low temperature, preferably having a melting point above 0 °C, more preferably above 20 0C, and even more preferably above 25 °C, and volatilizesjeadily at temperature below 200°C and preferably below 100°C in order to be eliminated from a green body before decomposition of the binder (such as methylcellulose for example). Preferably, the fugitive pore former has a sufficiently high vapor pressure (P°) allowing elimination by volatilization (that is, sublimation or vaporization) at temperature below 2000C and preferably below 1000C. [0028] In some embodiments, the fugitive pore former agent comprises a compound that volatilize readily under atmospheric pressure below 2000C having a melting point above 00C and having a vapor pressure (P°) at 25°C above 10"6 atm. Preferred compounds are those having a melting point above 20°C and vapor pressure 10"6 atm<P°<10"2 atm.
[0029] We have found that compounds having melting point below 00C are not easily handled and shaped unless using cryogenic conditions. However, cryogenic conditions incompatible with the use of liquid water which is a typical solvent or liquid vehicle used in the batch composition to adjust the viscosity of the part to be extruded.
[0030] We have also found that compounds having vapor pressure less than 10'6 atm at room temperature (RT) are difficult to eliminate easily because of their low tendency to volatilize whereas compounds having vapor pressure > 10'2 atm are very difficult to handle because they volatilize too quickly and thus are difficult to handle and to shape. Volatility is a tendency for a material to convert from condensed (i.e. solid or liquid) phase to the gas phase; a general expression of this tendency is vapor pressure (P0). Vapor pressure (P°) is the pressure of a vapor in equilibrium with its condensed phase (solid or liquid).
Sublimation is the transition from the solid to gas phase with no intermediate liquid stage. [0031] In one set of embodiments, the fugitive pore former can be a terpene having a melting point above 0°C and preferably above RT, such as volatile cyclic terpenes like camphene, camphene tricyclene mixture. Camphene exhibits a high vapor pressure (2.0 103 Pa at 55°C) and low melting point of 44-48 °C. In another set of embodiments, the fugitive pore former can be a volatile aromatic compound such as naphthalene; naphthalene is a compound which could be removed by sublimation, and its elimination may be performed below the decomposition temperature by sublimation and vapors evacuated during the drying process, and naphthalene can be described as sublimable material, which can be used with other starches (graphite/carbon or starch). [0032] In another set of embodiments, the fugitive pore former can be a substituted aromatic compound like phenol, trimethylphenol, salicylic acid esters, p-dichlorobenzene and volatile hydrocarbons such as alicyclic hydrocarbons like cyclododecane or substituted alicyclic compounds such as menthol, camphor this list being indicative and not limitative. [0033] A preferred fugitive pore former agent is is cyclododecane. This compound has a low melting point (58-63°C), an appropriate vapor pressure at room temperature (0.1 hPa) and can be easily shaped to form spherical granules. Techniques suitable to prepare the spherical granules include prilling from molten materials, grinding, and spray drying. US Patent No. 5185108 describes a method to prepare wax micro-spheres having an appropriate size. [0034] Table A lists illustrative compounds that can be used as fugitive pore forming agents.
Table A Compound Vapor Pressure @ RT Meltinq point
(mm. Hg) (atm) (0C)
Benzoic acid 7.5 10-4 1.0 x 10-6 122
Tetradecane 0.0116 1.5 x 10-5 5.8 Naphtalene 0.030 3.95 x 10-5 80
Ethyl salicylate 0.05 6.5 x 10-5 2-3
Trimethyl phenol 0.05 6.5 x 10-5 73
Cyclododecane 0.075 9.87 x 10-5 58-61
Phenol 0.35 4.6 x 10-4 40 Camphor 0.65 8.55 x 10-4 180
Menthol 0.8 1.05 x 10-3 36-38 p-Dichlorobenzene 1.28 1.68 x 10-3 53
Dicyclopentadiene 1.35 1.78 x 10-3 32-34
Camphene 2.47 3.25 x 10-3 45-46
[0035] FIG. 7 shows the increase of porosity achieved using particles of fugitive pore formers (cyclododecane, naphthalene and camphene) in comparison to the starting material (without pore formers). The triangle is cyclododecane, the diamond is naphthalene,. and the circle is camphene. Experiments have been conducted on hand-made square pieces. Powders of fugitive pore formers have been prepared by crushing pieces of wax in a laboratory mixer. Samples (inorganic materials and pore formers) have been hand mixed and mulled, dried overnight in hot air and fired in electrical furnace. [0036] FIG. 8 shows reports weight losses (from TGA analysis) occurring during the heat up of pastes including cyclododecane as pore former (1 ,3, and 4) and a paste without pore former (2). TGA curves confirm that fugitive pore formers are removed at low temperature.
[0037] In embodiments, the disclosure provides a plasticized ceramic precursor batch composition comprising ceramic forming inorganic batch components; and a pore forming agent comprising cyclododecane. The plasticized ceramic precursor batch composition is capable of forming a porous ceramic article comprising a primary sintered phase composition. [0038] In embodiments, the disclosure provides a method for manufacturing a porous ceramic honeycomb article. The method generally comprises first providing a plasticized ceramic forming precursor batch composition as summarized herein. A honeycomb green body can then be formed from the plasticized ceramic forming precursor batch composition. The honeycomb body can be dried under conditions to remove some or substantially all of the cyclododecane pore former prior to firing. The formed honeycomb green body can then be fired under conditions effective to convert the green body into a porous ceramic honeycomb article. Additional embodiments of the disclosure are set forth, in part, in the detailed description, and any claims, and in part from the detailed description, or can be learned by practice of the invention. The foregoing general description and the detailed description are intended to be illustrative and demonstrative, and non- limiting.
[0039] In embodiments, the disclosure provides improved ceramic precursor batch compositions suitable for forming porous ceramic articles comprised of a primary sintered phase ceramic composition. For example, the disclosed batch compositions can be used to form porous sintered phase ceramic articles having relatively high total porosities without a resulting generation of cracks. Still further, the batch compositions of the disclosure can also enable the use of simplified firing cycles to convert the batch compositions into primary sintered phase ceramic compositions. The ceramic precursor batch compositions generally comprise at least one ceramic forming inorganic batch component and a cyclododecane pore forming agent and can further include an optional liquid vehicle, and an optional organic binder system.
[0040] The ceramic forming inorganic batch components can be selected to form, upon firing; any desired porous sintered phase ceramic composition, including for example a porous cordierite, mullite, spinel, aluminum titanate, or a mixture thereof. Exemplary and non-limiting inorganic powder materials suitable for use in these inorganic ceramic powder batch mixtures can include, for example, cordierite, aluminum titanate, mullite, clay, kaolin, magnesium oxide sources, talc, zircon, zirconia, spinel, alumina forming sources, including aluminas and their precursors, silica forming sources, including silicas and their precursors, silicates, aluminates, lithium aluminosilicates, alumina silica, feldspar, titania, fused silica, nitrides, carbides, borides, e.g., silicon carbide, silicon nitride or mixtures of these. [0041] In embodiments, the inorganic batch components can be selected to provide a primary sintered phase cordierite composition having the general formula [A]x[M]y[T]zOi8, where A can be selected from the group consisting of alkali, alkaline earth, rare earth elements, CO2, H2O, and combinations thereof; M can be selected from the group consisting of Mg, Fe, Mn, Co, and combinations thereof; T is selected from the group consisting of Al, Si, Ga, Ge, and combinations thereof; and where 0 < x < 1.0, 1.9 < y < 2.1 , and 8.9 < z < 9.1. In embodiments, 0 < x < 0.05, 1.98 < y < 2.02, 8.98 < z < 9.02, M can be comprised of Mg, and T can be comprised of Al, Si, or both. In embodiments, the cordierite composition can be approximately represented by the formula. Mg2AI4Si5Oi8. [0042] Alternatively, an exemplary cordierite phase can be expressed and characterized on an oxide weight percent basis as comprising from about 49 to about 53 percent by weight SiO2, from about 33 to about 38 percent by weight AI2O3, and from about 12 to about 16 percent by weight MgO. An exemplary inorganic cordierite precursor powder batch composition preferably comprises about 33 to about 41 weight percent aluminum oxide source, about 46 to about 53 weight percent of a silica source, and about 11 to about 17 weight percent of a magnesium oxide source. Additional exemplary and non- limiting inorganic batch component mixtures suitable for forming cordierite include those disclosed in U.S. Pat. Nos. 3,885,977; RE 38,888; 6,368,992; 6,319,870; 6,24,437; 6,210,626; 5,183,608; 5,258,150; 6,432,856; 6,773,657; 6,864,198; and U.S. Patent Application Publication Nos.: 2004/0029707; 2004/0261384. The cordierite ceramic phases described herein can also comprise either orthorhombic or hexagonal crystal lattice symmetry, or may be comprised of a mixture of both such crystal structures. [0028] The inorganic batch components can also be selected to provide a ceramic mullite composition consisting essentially of, as characterized in an oxide weight percent basis, from 27 to 30 percent by weight Siθ2, and from about 68 to 72 percent by weight AI2O3. An exemplary inorganic mullite precursor powder batch composition can comprise approximately 76% mullite refractory aggregate; approximately 9.0% fine clay; and approximately 15% alpha alumina. Additional exemplary non-limiting inorganic batch component mixtures suitable for forming mullite include those disclosed in U.S. Pat. Nos.: 6,254,822 and 6,238,618.
[0029] Still further, the inorganic batch components can also be selected to provide an alumina titanate composition consisting essentially of, as characterized in an oxide weight percent basis, from about 8 to about 15 percent by weight SiO2, from about 45 to about 53 percent by weight AI2O3, and from about 27 to about 33 percent by weight TiO2. An exemplary inorganic aluminum titanate precursor powder batch composition can comprise about 10% quartz; about 47% alumina; about 30% titania; and about 13% additional inorganic additives. Additional exemplary non-limiting inorganic batch component mixtures suitable for forming aluminum titanate include those disclosed in, for example, U.S. Pat. Nos. 4,483,944; 4,855,265; 5,290,739; 6,620,751 ; 6,942,713; 6,849,181 ; U.S. Patent Application Publication Nos.:2004/0020846; 2004/0092381 ; and in PCT Application Publication Nos.: WO 2006/015240; WO 2005/046840; and WO 2004/011386. [0030] An exemplary and non-limiting magnesium oxide source suitable for use in the batch composition can be talc. In embodiments, a suitable talc can have a mean particle size of at least about 5 μm, at least about 8 μm, at least about 12 μm, or even at least about 15 μm. Alternatively, the talc can be a platy talc. As used herein, a platy talc refers to talc that exhibits a platelet particle morphology, i.e., particles having two long dimensions and one short dimension, or, for example, a length and width of the platelet that is much larger than its thickness. In one aspect, the talc possesses a morphology index greater than about 0.50, 0.60, 0.70, or 80. The morphology index, as disclosed in U.S. Pat. No. 5,141 ,686, is a measure of the degree of platiness of the talc. One typical procedure for measuring the morphology index is to place the sample in a holder so that the orientation of the platy talc is maximized within the plane of the sample holder. The x-ray diffraction (XRD) pattern can then be determined for the oriented talc. The morphology index semi-quantitatively relates the platy character of the talc to its XRD peak intensities using the following equation:
M=-
where Ix is the intensity of the peak and \v is that of the reflection. Examples of commercially available magnesium oxide sources suitable for use in the disclosure include, Mistron 002, FCOR Talc, or both, and are available from Luzenac, Inc. of Oakville, Ontario, Canada, and 96-67 Talc available from Barrett's Minerals, Inc. of Dillon, Montana.
[0031] Exemplary alumina forming sources can include aluminum oxides or a compound containing aluminum which when heated to sufficiently high temperature yields essentially 100% aluminum oxide. Non-limiting examples of alumina forming sources include corundum or alpha-alumina, gamma- alumina, transitional aluminas, aluminum hydroxide such as gibbsite and bayerite, boehmite, diaspore, aluminum isopropoxide and like materials. Commercially available alumina sources can include relatively coarse aluminas, such as the Alcan C-700 series, having a particle size of about 4-6 micrometers, and a surface area of about 0.5-1 m2 /g, e.g., C-714 and C- 701™. Relatively fine aluminas, having a particle size of about 0.5-2 micrometers, and a surface area of about 8-11 m2 /g, can also be used, such as A10 and A-16SG alumina, available from Alcoa. In still another aspect, the alumina forming source can be a colloidal alumina having particles sizes in the range of from 20nm to 50nm, such as the AL20 available from Nyacol. [0032] If desired, the alumina source can also comprise a dispersible alumina forming source. A dispersible alumina forming source can be, for example, an alumina forming source that is at least substantially dispersible in a solvent or liquid medium and that can be used to provide a colloidal suspension in a solvent or liquid medium. In one aspect, a dispersible alumina source can be a relatively high surface area alumina source having a specific surface area of, for example, at least 20 m2/g. Alternatively, a dispersible alumina source can have a specific surface area of at least 50 m2 /g. In an exemplary aspect, a suitable dispersible alumina source for use in the methods of the disclosure comprises, for example, alpha aluminum oxide hydroxide (AIOOH x H2O) commonly referred to as boehmite, pseudoboehmite, and as aluminum monohydrate. In another exemplary aspect, the dispersible alumina source can comprise the so-called transition or activated aluminas {i.e., aluminum oxyhydroxide and chi, eta, rho, iota, kappa, gamma, delta, and theta alumina) which can contain various amounts of chemically bound water or hydroxyl functionalities. Specific examples of commercially available dispersible alumina sources that can be used in the disclosure include, for example, Dispal Boehmite, commercially available from CONDEA Vista Company of Houston, Texas, and Alpha Alumina A1000, commercially available from Almatis, Inc. [0033]A silica source can comprise clay, such as for example, raw kaolin, calcined kaolin, or mixtures thereof. Exemplary and non-limiting clays include non-delaminated kaolinite raw clay, having a particle size of about 7-9 micrometers, and a surface area of about 5-7 m2 /g, such as Hydrite MP™, those having a particle size of about 2-5 micrometers, and a surface area of about 10-14 m2 /g, such as Hydrite PX™ and K-10 raw clay, delaminated kaolinite having a particle size of about 1 -3 micrometers, and a surface area of about 13-17 m2 /g, such as KAOPAQUE-10™, calcined clay, having a particle size of about 1-3 micrometers, and a surface area of about 6-8 m2 /g, such as Glomax LL. All of the above named clay materials are available from Dry Branch Kaolin, Dry Branch, Ga.
[0034]The silica source can further comprise, if desired, a silica raw material including fused SiOa; colloidal silica; crystalline silica, such as quartz or cristobalite, or a low-alumina substantially alkali-free zeolite. A commercially available quartz silica forming source includes, for example, Cerasil 300, Unimim Silverbond 200, and lmsil A25 Silica available from, Laguna Clay Co., of Byesville, Ohio. In embodiments, the silica forming source can comprise a compound that forms free silica when heated, for example, silicic acid or a silicon organo-metallic compound.
[0035]An exemplary titania source can include, for example, rutile, anatase titania, or combinations thereof. In embodiments, optimization of the median particle size of the titania source can be used to avoid entrapment of unreacted oxide by the rapidly growing nuclei in the sintered ceramic structure. Accordingly, in embodiments, it may be preferred for the median particle size of the titania to be up to about 20 micrometers. [0036] In embodiments, the inorganic batch components can optionally comprise one or more pre-reacted inorganic refractory fillers. Exemplary pre- reacted inorganic refractory fillers can include powders of silicon carbide, silicon nitride, cordierite, aluminum titanate, calcium aluminate, beta- eucryptite, and beta-spodumene, as well as refractory aluminosilicate fibers formed, for example, by the processing of aluminosilicate clay. [0037] The ceramic precursor batch composition can further comprise cyclododecane as a pore forming agent. The cyclododecane pore forming agent or pore former is a fugitive material which evaporates or otherwise undergoes vaporization during drying or heating of the green body to obtain a desired, usually higher porosity, coarser median pore diameter, or both. The use of a pore former enables one to tailor the porosity and pore size distribution in the resulting fired body for a particular application. Cyclododecane exhibits a relatively low melting point, in the range of about 58-63°C, a vapor pressure at room temperature of about 0.1 hPa, and can be readily shaped to form spherical granules. Exemplary shaping techniques can include prilling from molten materials, grinding, spray drying, and like techniques. U.S. Patent No. 5,185,108, describes exemplary methods for preparing wax particles having the appropriate size. Cyclododecane is commercially available from, for example, HANGLEITER Gmbh, Otzberg, Germany.
[0038] The cyclododecane can be utilized in any desired amount. However, in embodiments, the cyclododecane can be presented as a superaddition in an amount of from about 20 weight percent to about 80 weight percent, including exemplary superaddition amounts such as 25 weight percent, 30 weight percent, 35 weight percent, 40 weight percent, 45 weight percent, 50 weight percent, 55 weight percent, 60 weight percent, 65 weight percent, 70 weight percent, 80 weight percent, intermediate amounts, and any range of amounts within these values.
[0039] The use of cyclododecane as a pore forming agent in the batch compositions of the disclosure provides the ability to remove or evacuate the pore former during the drying step and prior to firing and reduced the formation of undesired cracks in the resulting fired ceramic structure. Further, evacuated or removed cyclododecane can, if desired, be recovered from the removal process and subsequently reused, thus reducing the costs associated with the use of conventional unrecoverable pore forming agents. [0040]When used in particulate form, the cyclododecane can be shaped and sized according to any predetermined specifications, further enabling one to obtain any desired pore structure properties, including for example, total porosity and mean pore size. In one exemplary and non-limiting embodiment, the cyclododecane can be present in particulate form, where the particles are substantially spherical in shape. Alternatively, in another non-limiting and exemplary embodiment, the cyclododecane particles can be substantially irregular or non-spherical in shape. Likewise, the cyclododecane particles can have any desired size, commonly characterized by the median particle diameter d5o. In some exemplary embodiments, the cyclododecane particles can have a median particle size of from 5μm to about 150μm. In other exemplary embodiments, the cyclododecane particles can have a median particle size of from 15μm to about 120μm, including for example, 25μm, 35μm, 45μm, 55μm, 60μm, 65μm, 75μm, 85μm, 95μm, 105μm, 115μm, intermediate particle sizes and particle sizes in any range of sizes within these values. For example, in embodiments, the cyclododecane particles can have a median particle size d50 of from about 80μm to about 120μm, about 90μm to about 110μm, or even about 95μm to about 105μm. [0041] The inorganic batch components and the cyclododecane pore former component can be intimately blended with an optional organic binder, optional liquid vehicle, and one or more optional forming aids to impart plastic formability and green strength to the raw materials when they are shaped into a body. Exemplary organic binders can include cellulose ether such as methylcellulose, hydroxypropyl methylcellulose, methylcellulose derivatives, or combinations thereof. The relative amounts of binder can vary depending on factors such as the nature and amounts of raw materials used. However, in embodiments, the binder can be present in the batch composition as a superaddition in an amount of from about 2 wt % to about 10 wt %. [0042] The optional liquid vehicle component can also vary in amount and kind depending on the type of material used and to impart superior handling properties and compatibility with the other components in the ceramic batch mixture. If used, the liquid vehicle can be present as a superaddition in the range of from about 20 wt % to about 50 wt %. In embodiments, the liquid vehicle component can comprise water. However, in embodiments, an organic solvent, for example, methanol, ethanol, and like solvents, or a mixture thereof, can also be used as the liquid vehicle. [0043] Optional forming or processing aids can also include, for example, lubricants, surfactants, plasticizers, sintering aids, and even pore forming agents in addition to the cyclododecane. Additional pore formers can include, for example, carbon, graphite, starch, wood, shell, nut flour, polymers such as polyethylene beads, waxes; or like materials, and combinations thereof. To that end, when used, these additional pore formers can also be presized or shaped to provide a subsequent porosity having desired characteristics. Exemplary lubricants can include, for example, hydrocarbon oil, tall oil, sodium stearate, or like materials, and combinations thereof. An exemplary plasticizer for use in preparing the batch composition can include, for example, glycerine, or like materials. Other suitable sintering aids can generally include, for example, an oxide source of one or more metals such as strontium, barium, iron, magnesium, zinc, calcium, aluminum, lanthanum, yttrium, titanium, bismuth, tungsten or like materials, and combinations thereof. In embodiments, a superior optional sintering aid can comprise, for example, a mixture of a strontium oxide source, a calcium oxide source, an iron oxide source, or like materials, and combinations thereof. In embodiments, an optional sintering aid can comprise at least one rare earth metal, and combinations thereof. The sintering aid can be added to the batch composition, for example, in powder form, liquid form, or in combination. [0044] Once the components of the batch composition have been blended, the resulting ceramic precursor batch composition can be shaped into a green body by any known conventional forming process, e.g., extrusion, injection molding, slip casting, centrifugal casting, pressure casting, dry pressing, and like methods. In an exemplary aspect, extrusion can be done using a hydraulic ram extrusion press, or a two stage de-airing single auger extruder, or a twin screw mixer with a die assembly attached to the discharge end, or like implementations. In the twin screw mixer example, proper screw elements are selected according to material considerations and other process conditions to build up sufficient pressure to force the batch material through the die.
[0045] In embodiments, a process is described herein for making a ceramic body (e.g. cordierite) with the use of a sizable and recoverable (and reusable) pore former (such as cyclododecane). An illustrative process flow chart is show in FIG. 9.
[0046] In some embodiments, the fugitive pore former (such as cyclododecane) is delivered in granules or in the form of a block of material. To be used as pore former in ceramic processing, the cyclododecane is preferably sized and shaped in accordance of the porosity to generate in the fired body. Shaping in spherical form can be obtained by a prilling process comprising spraying the molten material in a freezer. Several parameters like the air pressure (in the case of air assisted atomizing system), the liquid pressure and temperature, the spraying nozzle diameter and positioning will define the particle grain size distribution as can be seen in FIG. 10.
[0047] In one set of embodiments, the batch composition is obtained by blending together (i) a cordierite-providing raw material or raw material mixture; (ii) an adequate proportion of cyclododecane, previously shaped in the desired form, acting as the main (or only) pore-forming agent; (iii) optionally one or more additional known pore-forming agents such as starches and/or graphite; (iv) optionally a mixture of organic binders, surfactants, lubricants, and plasticizers; and (v) optionally a solvent media such as water or alcohol. [0048] The resulting mixture can then be formed into a shape, preferably by extrusion, but other methods such as pressing, slip casting, or injection molding could be used.
[0049] Dielectric drying, or microwave drying, or a combination dielectric /hot air can be used to dry (remove water) from the shaped article to form a dried green body which is subsequently fired into an article of porous ceramic material. [0050] The fugitive pore former can be removed by blowing hot air through the honeycomb structure (preferably in the direction of the axis of extrusion). During drying the green body is kept at sufficiently high temperature to remove substantially all or the entire fugitive pore former agent from the green body (but lower than the organic binder (methylcellulose for instance) decomposition temperature). In some embodiments, the green body is exposed to air at temperatures from 75 to 100°C to remove the pore former. The pore former removal can be controlled by way of weight loss measurement. The pore former removal step can be done simultaneously with the water removal step (hot air blowing in combination with microwave drying).
[0051] Once the pore former has been removed, consequent porosity has been generated in the green body (prior to firing). Evidence of porosity can be seen on SEM pictures (e.g. FIG. 11) and has been controlled by mercury porosimetry measurement.
[0052] Recoverable pore-former collection allow reuse of the pore-former and can be accomplished by, for example, cold trap equipment (FIGS. 12 & 13) with process conditions given as follow as examples: the hot air flow exits the honeycomb and is conveying the removed pore former (e,g, cyclododecane) to a cold trap which condenses the pore former. Temperature of the trap is set at 100C during the collection step. Once the trap gets saturated with pore former, the temperature of the trap is increased to 65°C allowing the melting and recovery of the pore former. [0053] The melted pore-former can be cooled down or immediately redirected to the shaping process to be processed again (as no degradation or decomposition occurred to the pore former during the previous process steps).
[0054]The green body is then fired at a sufficient temperature to provide a sintered, porous, ceramic (e.g. cordierite) article. In some embodiments, due to the absence of pore-forming agent, exothermal phenomenon during the firing are considerably reduced. Faster heating rate and/or lower sensitivity to oxygen levels during firing could be expected.
[0055] In this process, the recoverable pore former is not burnt (or reacted or decomposed) and thus green house gases generation can be reduced as compared to known pore former removal steps.
[0056] In embodiments, the batch compositions of the disclosure can be used to form multicellular honeycomb structures having a high filter volumetric heat capacity, a low pressure drop between the entrance and exit faces of the filter, a low coefficient of thermal expansion (CTE), and high filtration efficiency, and are thus well suited for use as particulate filters like wall flow filters such as diesel particulate filters. In one aspect the blended ceramic precursor batch composition can be formed or otherwise shaped into a honeycomb configuration. The geometry of the honeycomb configuration need not be restricted to any particular configuration. However, in embodiments, an exemplary formed honeycomb body can be configured to provide a wall flow filter comprising a plurality of cell channels bounded by porous channel walls that extend longitudinally from an upstream inlet end to a downstream outlet end. A first portion of the plurality of cell channels can comprise end plugs sealed to the respective channel walls at the downstream outlet end to form exhaust gas flow inlet cell channels and a second portion of the plurality of cell channels can comprise end plugs sealed to the respective channel walls at the upstream inlet end to form exhaust gas flow outlet cell channels. [0057]The formed honeycomb structure can, for example, be a cylinder having end surfaces with a shape of a circle or an ellipse, a prism having the end surfaces with a shape of a polygon such as a triangle or a square, a shape in which the sides of cylinders or prisms are bent like a "doglegged" shape, or like shapes. In addition, the shape of through holes or exhaust gas inlet and outlets is not particularly limited. For example, the cross-sectional shape may be a polygon such as a square, an octagon, a circle, an ellipse, or like shapes, and combinations thereof. [0058] Exemplary non-limiting examples of formed honeycombs produced by the process and batch compositions of the disclosure can comprise cell densities of from about 235 cells/cm2 (about 1 ,500 cells/in2) to about 15 cells/cm2 (about 100 cells/in2), including those having about 94 cells/cm2 (about 600 cells/in2), about 62 cells/cm2 (about 400 cells/in2), or about 47 cells/cm2 (about 300 cells/in2), those having about 31 cells/cm2 (about 200 cells/in2), or those having about 15 cells/cm2 (about 100 cells/in2). Further, the wall or web thicknesses can typically be from about 0.07 to about 0.6 mm (about 3 to about 25 mils). However, the particular desired size and shape of the ceramic body can depend on the application, e.g., in automotive applications by engine size and space available for mounting, and like considerations. Although the ceramic articles of the disclosure can be suitable for preparing thin-walled honeycombs, the disclosed mixtures can also be used for thicker walled structures. For example, honeycombs structures having about 15 to about 30 cells/cm2 (about 100 to about 200 cells/in2) and about 0.30 to about 0.64 mm (about 12 to about 25 mil) wall thicknesses are well suited for particulate filter applications such as diesel particulate filters. [0059] The formed green body having a desired size and shape as disclosed herein can then be dried under conditions effective to remove any excess liquids, such as moisture, and to remove the cyclododecane pore former. The drying conditions can depend, at least in part, upon the particular choice of materials used to prepare the batch composition. However, in embodiments, suitable drying conditions can comprise, for example, heating the formed green body at a temperature of about 50° to about 1500C for a sufficient time to eliminate the fugitive cyclododecane pore former. Sufficient time can also vary but, in embodiments, can be, for example, from about 24 to about 72 hours. The drying step can be performed by any known means, including hot air, microwave, steam, or dielectric drying, or like methods, and can optionally be followed by ambient air drying. [0060] Once dried, the dried green body can be fired under conditions effective to convert the dried green body into a ceramic article comprising a primary crystalline phase ceramic composition. The firing conditions effective to convert the green body into a ceramic article can vary depending on a number of conditions, such as the specific composition, size of the green body, the type of equipment used, and like considerations. Therefore, excellent firing conditions to obtain a ceramic article according to the disclosure can be readily ascertained. However, for batch compositions used to form mullite, exemplary firing conditions can be, for example, heating at a maximum soak temperature of about 1 ,4000C to about 1 ,600°C, and for a maximum soak time about 1 hour to about 6 hours. Alternatively, for batch compositions that are primarily for forming cordierite, exemplary firing conditions can be, for example, heating the green body at a maximum soak temperature of about 1 ,3500C to about 1 ,4500C and for a maximum soak time of from about 5 to about 50 hours, including exemplary ranges of 10 to 40 hours, or even 15 to 30 hours. In embodiments, an exemplary firing schedule for cordierite forming compositions can include firing at a soak temperature of about 1 ,4000C to about 1 ,425°C for a hold or soak time of about 10 to about 35 hours. [0061 ]The resulting fired ceramic bodies of the disclosure can exhibit total porosities %P, as measured by mercury porosimetry, of about 50% to about 80%, including total porosities of, for example, 55%, 60%, 65%, 70%, 75%, and intermediate porosities values. For example, in embodiments, the total porosity can be, for example, of about 55% to about 75%, of about 60% to about 70%, or like porosities. [0062]The median pore diameter, d50, of the pores present in the resulting ceramic articles can be, for example, from about 8μm to about 35μm. In other embodiments, the median pore diameter can be from about 10μm to about 30μm, or from about 15μm to about 25μm. EXAMPLES
[0063]To further illustrate the disclosure, the following examples provide those of skill in the art with a complete description of how the ceramic precursor batch compositions, ceramic articles, and methods can be accomplished and evaluated. They are exemplary and non-limiting. Efforts have been made to ensure accuracy with respect to numbers (e.g., amounts, temperatures, etc.); however, some variation or deviation may be present. Unless indicated otherwise, parts are parts by weight, temperature is degrees C or is ambient temperature, and pressure is at or near atmospheric. [0064] In the following examples, a series of seven cordierite forming batch compositions were prepared. All seven batch formulation were prepared from a raw material mixture containing 38.5 wt% of a 22 micron talc screened to - 325 mesh, 12,5 wt% of a 10 micron kaolin, 12.4 wt% of a 9 micron corundum screened to -325 mesh, 21.0 wt% of a 4.6 micron aluminum hydroxide, 15.4 wt% of a 25 micron quartz powder. The resulting mixtures were also blended with 4.45 wt% methylcellulose binder and 0.56 wt% sodium stearate lubricant. To obtain comparative results, batch compositions 1 , 2 and 5 each contained a 40.0 wt% superaddition of a 49 micron potato starch. Examples 3, 4, 6, and 7 each contained a 40.0 wt% superaddition of cyclododecane. [0065] Prior to use, large pieces of initial cyclododecane wax were crushed in small pieces (flecks) of several millimeters with a hammer. The flecks were then introduced in a laboratory chopper and grinded for approximately 30 seconds to provide powdered cyclododecane having particle diameters of about 100μm. The final powdered cyclododecane is illustrated in FIG.1. The preparation of the powder could be further refined to obtain more spherical forms using other methods, for example prilling. Exemplary spherical powdered cyclododecane is illustrated in FIG. 2.
[0066] Distilled water was also added to each batch composition in a stainless steel muller until the batch was of a suitable plasticity to be extruded. The wet batch compositions were then extruded to form a 2-inch diameter honeycomb with approximately 275 cells per square inch and 0.016-inch thick walls. The extruded honeycomb bodies were then dried and fired according to the drying and firing schedules in Table 1. The resulting ceramic honeycomb articles were then evaluated for several physical performance properties, including coefficient of thermal expansion, pore microstructure, and modulus of rupture, the results are contained in Table 1. The coefficient of thermal expansion (CTE) was obtained by dilatometry on a specimen parallel to the lengths of the channels of the honeycomb article ("axial direction") over the temperature range of 25 to 8000C and in units of 10'7/°C. The %porosity describes the total volume percentage of porosity in the walls of the article as measured by mercury porosimetry. The terms d™, d5o, and d90 denote the pore diameters, in microns, or micrometers (10"6 meters), at which 10%, 50%, and 90% of the total pore volume are of a finer pore diameter, respectively, as measured by mercury porosimetry. Thus, for example, d90 is the pore diameter at which 90% (by volume) of the pores have a smaller diameter (equal to the pore diameter at which the cumulative mercury intrusion volume equals 10% of the total mercury intrusion volume). All modulus of rupture (MOR), or flexural strength, values were measured at room temperature by the four-point method on a cellular bar (0.5 inch x 0.25 inch x 3 inches long) parallel to the axial direction of the honeycomb. [0067] A review of the results obtained in Table 1 indicate properties that can be obtained by the use of the cyclododecane pore former in the manufacture of porous ceramic articles. For example, batch compositions 2 and 5 report properties achieved in a ceramic article that was fired in an electrical furnace utilizing two different ramps of heating. As indicated, even for a slower ramping rate, a significant level of cracks, precluding any CTE or strength measurements, were present when potato starch was used as the pore former to achieve desired porosity. In contrast, batch composition 3, which utilized cyclododecane as the pore former, provided desirable properties without the formation of cracks. Further, batch composition 4, which also comprised cyclododecane, provided properties similar to those of batch composition 3, except for the formation of cracks during the firing process. However, the generation of cracks was believed to be a result of the batch composition being fired in a wet state without having been dried to remove the cyclododecane prior to firing. [0068] A review of batch composition 6 also illustrates that when the cyclododecane pore former was used, a firing cycle including a faster ramp of heating rate can be employed to sinter the body without the formation of undesirable cracks. In contrast, as described above, batch composition 5, comprising potato starch as the pore former, resulted in a sintered composition exhibiting cracks which precluded any CTE or strength measurements. This comparison can be seen in FIG. 3 and FIG. 4. As shown in FIG 3, the honeycomb article 10 comprised of 40% potato starch and corresponding to batch composition 5, contains a large crack along the exterior surface or skin of the article. In contrast, the honeycomb article 20 including 40% cyclododecane and the corresponding article produced from batch composition 6, did not exhibit any cracks. Likewise, as shown in FIG. 4, the honeycomb article 10 comprised of 40% potato starch and again corresponding to batch composition 5, contained a large series of cracks along a portion of the honeycomb channel walls, indicated by the circled region 15. In contrast, the honeycomb article 20 including 40% cyclododecane and corresponding to the article produced from batch composition 6, did not exhibit any cracks. FIG. 5 further illustrates schematically a comparison of the relatively faster firing cycle 3, utilized for the firing of batch compositions 5, 6, and 7, compared to the slower firing cycle 2 used for the firing of batch composition 2, 3 and 4. Firing cycle 3 is schematically represented by line 30. Firing cycle 2 is schematically represented by line 40.
[0069] Accordingly, the data reported in Table 1 demonstrate that cyclododecane can be used as a pore former to successfully achieve high porosities while all other properties remain acceptable and comparable to those obtained if potato starch is selected. In addition, faster ramp of heating can be achieved without concern for the generation of cracks. [007O]In a subsequent study, the TGA weight losses and DSC thermal phenomenon that occurred during the heating of cyclododecane alone, an exemplary cordierite green body without any pore formers and cordierite green body including a superaddition of 40 wt% cyclododecane, before and after drying, were evaluated. The results are reported on graph of FIG. 6. [0071] As shown by curve 50 in Fig. 6, cyclododecane can be evacuated at relatively low temperatures, such as below about 250°C. The heating of the dry green cordierite parts without pore formers shows a decrease of weight occurring between about 250°C and about 300°C corresponding to the burn- out of organic binders, as shown by curve 60. The heating of wet cordierite green parts comprising 40% of cyclododecane exhibits losses between room temperature and about 350°C due to removal of water, binders and the cyclododecane, as shown by curve 70. As shown by curve 80, the heating of the dry part including 40% of cyclododecane follows a curve similar to that obtained for the dry green part without any pore formers. These results indicate that cyclododecane can be evacuated during the drying process conducted in hot air at about 800C for about 48 hours.
TABLE 1
Example
1 2 3 4 5 6 7 Number
Wt % Potato 40 0
40 0 40 0 0 starch
Wt % 0 40
0 40 0 40 40 Cyclododecane
Drying Dry Dry Wet Dry Dry Wet
Dry Condition Firing Cycle #1 #2 #2 #2 #3 #3 #3
0-150 °C Rate
120 120 120 120 120 120 120 (0CYh)
150-800 °C
27 27 27 27 120 120 120 Rate (0CYh)
800-9000C
37 27 27 27 120 120 120
Rate (0CYh)
1150-1350°C
25 109 109 109 120 120 120 Rate (0CYh)
1350-Tmax
5 109 109 109 120 120 120 Rate (0CYh)
Hold
Temperature 1409 1409 1409 1409 1409 1409 1409
(0C)
Hold Time (h) 11 20 20 20 20 20 20
% Porosity 66.1 62.7 67.8 67.7 64.3 67.4 68.3 dio (μm) 8.0 20.4 16.6 15.5 16.8 14.2 15.5 dso (μm) 16.5 30.7 32.6 30.5 25.0 29.0 30.6 dgo (μm) 33.0 56.6 87.9 79.7 51.5 77.6 82.6
(d5o-dio)/d5O 0.51 0.34 0.49 0.49 0.33 0.51 0.49
(d9o-d5o)/d5o 1.00 0.84 1.69 1.61 1.06 1.67 1.70
(d9o-d1 o)/d5o 1.51 1.18 2.18 2.11 1.39 2.18 2.20
PCF (pore connectivity 43 .8 53.1 31.1 32.1 46.3 30.9 31.0 factor)
Figure imgf000027_0001
TABLE 2
Example Number 8 9 10 11 12
Weight % Potato
0 0 0 0 0 starch
Weight %
0 0 30 60 75 Cyclododecane
MW + hot Hot air Hot air Hot air Hot air
Drying air
Firing Cycle #2 #2 #2 #2 #2
0- 150 0C Rate
120 120 120 120 120 (°C/h)
150- 800 °C Rate
27 27 27 27 27 (°C/h)
800-9000C Rate
27 27 27 27 27 (°C/h)
1150-13500C Rate
109 109 109 109 109 (°C/h)
1350-Tmax Rate
109 109 109 109 109 (°C/h)
Hold Temperature
1409 1409 1409 1409 1409 (0C)
Hold Time (h) 20 20 20 20 20
% Porosity 50.4 51.7 67.6 73.0 75.1 dio (μm) 4.2 3.1 5.6 7.8 9.4 dso (μm) 10.5 12.5 21.7 34.3 41.4 dgo (μm) 24.4 19.0 74.3 93.9 115.5
(d5o-dio)/d5o 0.60 0.48 0.74 0.77 0.77 Example Number 13 14 15
Weight % Potato
0 0 0 starch
Weight %
0 0 40 Camphene
Weight %
20 40 0 Naphthalene
Drying Dry Dry Dry
Firing Cycle #2 #2 #2
0- 150 0C Rate
120 120 120 (°C/h)
150- 800 °C Rate
27 27 27 (°C/h)
800-900°C Rate
27 27 27 (°C/h)
1150-13500C Rate
109 109 109 (°C/h)
1350-Tmax Rate
109 109 109 (°C/h)
Hold Temperature
1409 1409 1409 (0C)
Hold Time (h) 20 20 20
% Porosity 62.5 66.4 66.0 dio (μm) 13.2 14.0 14.7 d50 (μm) 25.6 29.4 27.3 dgo (μm) 13.2 14.0 14.7
(d5o-dio)/d5o 0.48 0.52 0.46
[0072]Table 2 reports measured porosities on hand made samples in order to estimate the increase of porosity due to addition of fugitive pore former. All samples (except example 8) have been prepared using the following conditions: (1) grinding of pore former agent, (2) addition to inorganic components previously mixed, (3) mixing with a mixer, (4) mulling with a rolling pin, (5) cutting in square, (6) overnight drying in hot air at 1000C, and then, (6) firing in electrical furnace following the indicated cycle. In comparison, example 8 is an extruded part, fired in the same conditions, is prepared using standard conditions.
[0073] Comparison of examples 8 and 9 confirms the relative good agreement observed concerning properties (porosity) between hands made pieces and extruded part and consequently suggests that hand made pieces provide reliable results regarding increase of porosity with addition of fugitive pore formers.
[0074] Example 9 (without pore former) represents the baseline of porosity resulting of packing of raw materials used [0075] Examples 10 to 15 illustrate the increase of porosity resulting of addition of fugitive pore formers to the reference batch. Some exemplary results are plotted on FIG. 10.
[0076] Thermal analysis (TGA) related to paste including fugitive pore formers is reported on graph 2. Curves clearly indicates important weight losses at low temperature (below 150°C) corresponding to sublimation of fugitive pore formers.
TABLE 3
Example Number 16 17 18 19
Weight % Y2O3 0.6 0.6 0.6 0.6
Weight % Potato starch 22 22 11 22
Weight % graphite - 22 11 22
Weight % Cyclododecane 22 - 22 -
MW + hot MW + hot MW + hot MW + hot
Drying air air air air Firing Cycle #3 #3 #3 #3
0- 130 °C Rate (0Cm) 50 50 50 50
130- 315 °C Rate (°C/h) 5 5 5 5
315- 550 0C Rate (0Cm) 11 11 11 11
550- 730 0C Rate (°C/h) 3 3 3 3
730-1020°C Rate (°C/h) 24 24 24 24
1020- 1150°C Rate (°C/h) 6 6 6 6
1150-1360°C Rate (°C/h) 25 25 25 25
1350-Tmax Rate (0Cm) 5 5 5 5
Hold Temperature (0C) 1409 1409 1409 1409
Hold Time (h) 11 11 11 11
% Porosity 65.0 64.8 65.9 66.8 d10 (μm) 7.4 6.8 7.0 9.7 d50 (μm) 17.3 16.6 15.8 18.5 d90 (μm) 40.2 39.6 31.5 34.7
(d50-d10)/d50 0.57 0.59 0.56 0.48
(d90-d50)/d50 1.32 1.39 0.99 0.87
(d90-d10)/d50 1.90 1.98 1.55 1.35
E at 25°C (105 psi) 4.15 3.48 3.65 2.53
E at 500°C (105 psi) 4.13 3.43 3.61 2.46
E at 900°C (105 psi) 4.26 3.40 3.71 2.34
Microcrack parameter, Nb3 0.137 0.091 0.131 0.046 CTE, 25-800°C (10-7/oC) 7.9 7.6 8.2 10.3
CTE, 500-9000C (10-7/0C) 15.2 15.4 15.4 17.4
MOR (psi) 406 382 431 384
TSPRT=(MOR/E)25°C(CTE25
1238 1444 1440 1474
-800°C)-1
TSPHT=(MOR25°C /E500°C)
647 723 760 897
(CTE500-800°C)-1
[0077] Table 3 illustrates that fugitive pore formers could be used in conjunction with other known pore formers. All samples included in Table 3 are extruded from paste made using a known extrusion process. [0078] Porosity of all formulations described in the table is achieved using a mixture of pore forming agents. Examples 16 and 18 illustrate the ability of fugitive pore formers to be used conjointly with another pore former (starches and/or graphite). Example 19 reports representative properties achieved with a mixture of starch and graphite commonly put in the batch to gain porosity. Examples 16 and 18 illustrate that a mixture of pore former including at lest one fugitive pore former is possible to obtain similar range of properties. [0079]The manufacturing process of the present invention can provide advantages compared to known processes. [0080] In some embodiments, the present invention provides no pore former burn out and thus reduces CO or CO2 production or both. With no pore former burning during firing, a benefit on the firing cycle could be expected, especially with high pore former compositions. The pore former can be sized to the desired grain size. Linked to the collection and recapture of the pore former, an economical advantage over lost pore formers could be realized. Some fugitive pore former agents can also benefit the extrusion process for example when a waxy material like cyclododecane is used, the waxy material can act as an aid for extrusion.
[0081] Ceramic honeycomb bodies (such as cordierite or aluminum titanate bodies) exhibiting high porosity (and an associated high content of pore former in their batch compositions), while maintaining an easy ability to be processed would represent an advance in the state of the art. The present invention describes such bodies and methods for their manufacture. The bodies of the present invention can exhibit a porosity similar or higher than those existing in the prior art. This is achieved using at least one fugitive pore former or a mixture including a fugitive pore former and known pore formers such as starches or graphite, wherein the fugitive pore former is removed at low temperature (preferably during the drying step), preferably without generation of cracks. Thus, crack-free green bodies could be obtained and simplified firing cycle implemented. The invention may enable the fabrication of highly porous converter substrates or particulate filters for higher catalyst loadings while maintaining low pressure drop and high strength.
[0082]Thus, in one aspect, a method is disclosed herein for manufacturing a porous ceramic honeycomb article, comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent is capable of volatilizing at a temperature below 200°C at atmospheric pressure; forming a green body from the ceramic forming precursor batch composition; and firing the honeycomb green body under conditions effective to convert the ceramic forming precursor batch composition in the green body into a porous ceramic material, wherein the green body is converted into the porous ceramic honeycomb article.
[0083] In some embodiments, the pore forming agent comprises a volatile hydrocarbon, which may be an alicyclic hydrocarbon; a preferred fugitive pore forming agent is cyclododecane. [0084] In some embodiments, the pore forming agent comprises a substituted alicyclic hydrocarbon, such as menthol or camphor or a combination thereof. [0085] Preferably, substantially all, and even more preferably all, of the fugitive pore forming agent volatilizes and exits the green body prior to the firing. [0086] In some embodiments, the green body is heated sufficiently to cause substantially all of the fugitive pore forming agent to volatilize and exit the green body prior to the firing. [0087] Preferably, the fugitive pore forming agent volatilizes and exits the green body prior to the conversion of the ceramic forming precursor batch composition into the porous ceramic material.
[0088] In some embodiments, the fugitive pore forming agent is captured or recovered, such as by cold trap, after exiting the green body. The captured fugitive pore forming agent can then be mixed with an additional amount of the ceramic forming inorganic batch components and formed into another green body, thus recycling the fugitive pore former.
[0089] In some embodiments, the ceramic forming precursor batch composition further comprises a binder. The method can further comprise heating the green body sufficient to decompose the binder, wherein the fugitive pore forming agent is preferably removed from the green body prior to decomposition of the binder. An example of the binder is one which comprises methylcellulose. [0090] In some embodiments, the fugitive pore forming agent has a melting point above 0 0C. In other embodiments, the fugitive pore forming agent has a melting point above 200C. In other embodiments, the fugitive pore forming agent has a melting point above 25 0C.
[0091] In some embodiments, the fugitive pore forming agent has a melting point between 50 0C and 75 0C. In some embodiments, the fugitive pore forming agent has a melting point between 55 0C and 65 0C.
[0092] In some embodiments, the fugitive pore forming agent has a vapor pressure at 25 0C above 1 x 10-6 atm. In some embodiments, the fugitive pore forming agent has a vapor pressure at 25 0C above 5 x 10-5 atm. In some embodiments, the fugitive pore forming agent has a vapor pressure at
25 0C between 5 x 10-5 atm and 2 x 10-3 atm.
[0093] In some embodiments, the fugitive pore forming agent has a melting point above 0 0C and a vapor pressure at 25 0C above 10-6 atm.
[0094] In some embodiments, the fugitive pore forming agent has a melting point above 0 0C and a vapor pressure at 25 0C between 5 x 10-5 atm and 2 x
10-3 atm. [0095] In some embodiments, the fugitive pore forming agent has a melting point between 50 0C and 75 0C and a vapor pressure at 25 0C between 5 x 10-5 atm and 2 x 10-3 atm. [0096] In some embodiments, the fugitive pore forming agent volatilizes below 200 0C at atmospheric pressure. In some embodiments, the fugitive pore forming agent volatilizes below 100 0C at atmospheric pressure. [0097] Preferably, the fugitive pore forming agent volatilizes by sublimation or evaporation. [0098] In some embodiments, the fugitive pore forming agent has a melting point above 0 0C and a vapor pressure at 25 0C above 10-6 atm.
[0099] In some embodiments, the fugitive pore forming agent has a melting point above 20 0C and a vapor pressure at 25 0C between 10-6 atm and 10-2 atm.
[00100] In some embodiments, the ceramic forming precursor batch composition is free of starch, graphite, or combinations thereof.
[00101] In some embodiments, the pore former has a median particle size d50 of from 5 μm to 150 μm, in other some embodiments from 5 μm to 120 μm, in other embodiments from 5 μm to 50 μm, and in some embodiments from 15 μm to 50 μm. [00102] In some embodiments, the ceramic article has a total porosity (%P) of from 30% to 90%, and a median pore size (d50) of from 5μm to 40μm. In other embodiments, the ceramic article has a total porosity (%P) of from 60% to about 70%, and a median pore size (d50) of from about 5μm to about 25μm. [00103] In another aspect, a ceramic precursor batch composition is disclosed herein comprising ceramic forming inorganic batch components and a pore forming agent comprising cyclododecane. [00104] In another aspect, a method for manufacturing a porous ceramic article, comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent comprises an alicyclic hydrocarbon; and firing the ceramic forming precursor batch composition under conditions effective to convert the ceramic forming precursor batch composition into a porous ceramic material. A preferred embodiment is cyclododecane.
[00105] In another aspect, a plasticized ceramic precursor batch composition is disclosed herein comprising: ceramic forming inorganic batch components; and a pore forming agent comprising cyclododecane. In some embodiments, the ceramic forming inorganic batch components are selected to provide a sintered phase cordierite composition; the sintered phase cordierite composition can be characterized in some embodiments on an oxide weight basis as consisting essentially of: about 49 to about 53 percent by weight SiO2, about 33 to about 38 percent by weight AI2O3, and about 12 to about 16 percent by weight MgO. In some embodiments, the ceramic forming inorganic batch components are selected to provide a sintered phase mullite composition. In other embodiments, the ceramic forming inorganic batch components are selected to provide a sintered phase aluminum titanate composition. In other embodiments, the ceramic forming inorganic batch components are selected to provide a sintered phase silicon carbide composition. In some embodiments, the cyclododecane has a median particle size d50 of from about 5μm to about 150μm. In some embodiments, the cyclododecane is present as substantially spherical particles. In some embodiments, the batch composition is formed into a predetermined shape, such as a honeycomb structure. In some embodiments, the plasticized ceramic precursor batch composition further comprises a liquid vehicle and an organic binder system. [00106] In another aspect, a method is disclosed herein for manufacturing a porous ceramic honeycomb article, comprising the steps of: providing a plasticized ceramic forming precursor batch composition comprising: ceramic forming inorganic batch components and a pore forming agent comprising cyclododecane; forming a honeycomb green body from the plasticized ceramic forming precursor batch composition; and firing the honeycomb green body under conditions effective to convert the green body into a porous ceramic honeycomb article. The ceramic forming inorganic batch components can be selected to provide at least one of a sintered phase cordierite composition, sintered phased mullite composition, a sintered phase aluminum titanate composition, or combinations thereof. The ceramic forming inorganic batch components can be are selected to provide a sintered phase cordierite composition, as characterized on an oxide weight basis, consisting essentially of: about 49 to about 53 percent by weight SiO2; about 33 to about 38 percent by weight AI2O3; and about 12 to about 16 percent by weight
MgO. In some embodiments, the cyclododecane pore former is present in the plasticized ceramic forming precursor batch composition having a predetermined size and shape. In some embodiments, the cyclododecane pore former is present in the plasticized ceramic forming precursor batch composition as substantially spherical particles; in some embodiments, the substantially spherical cyclododecane particles have a median particle size d50 of from about 5μm to about 150μm. In some embodiments, the step of forming the honeycomb green body comprises shaping the plasticized ceramic forming precursor batch composition into a honeycomb shape, and drying the shaped plasticized ceramic forming precursor composition under conditions effective to at least remove some of the cyclododecane pore former. In some embodiments, effective firing conditions comprise firing the honeycomb green body at a soak temperature at from about 13000C to about 14500C, and subsequently holding the soak temperature for a period of time sufficient to convert the honeycomb green body into a ceramic honeycomb article. In some embodiments, the soak temperature is achieved by increasing temperature from 11500C to the soak temperature at a rate of increase greater than 1000C per hour. In some embodiments, the plasticized ceramic forming precursor batch composition further comprises a liquid vehicle and an organic binder system. In some embodiments, the step of forming the honeycomb green body comprises shaping and then drying the shaped plasticized ceramic forming precursor composition under conditions effective to remove substantially all of the cyclododecane pore former. [00107] In another aspect, a green honeycomb article is disclosed herein comprising ceramic forming precursor materials and a cyclododecane pore former. [00108] The disclosure has been described with reference to various specific embodiments and techniques. However, many variations and modifications are possible while remaining within the spirit and scope of the disclosure.

Claims

1. A method for manufacturing a porous ceramic honeycomb article, comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent is capable of volatilizing at a temperature below 200°C at atmospheric pressure; forming a green body from the ceramic forming precursor batch composition; and firing the honeycomb green body under conditions effective to convert the ceramic forming precursor batch composition in the green body into a porous ceramic material, wherein the green body is converted into the porous ceramic honeycomb article.
2. The method of claim 1 wherein the pore forming agent comprises a volatile hydrocarbon.
3. The method of claim 1 or 2 wherein the pore forming agent comprises an alicyclic hydrocarbon.
4. The method of any one of claims 1 to 3 wherein the pore forming agent comprises cyclododecane.
5. The method of claim 1 wherein the pore forming agent comprises a substituted alicyclic hydrocarbon.
6. The method of claim 1 and 5 wherein the pore forming agent comprises menthol or camphor or a combination thereof.
7. The method of any one of claims 1 to 6 wherein substantially all of the fugitive pore forming agent volatilizes and exits the green body prior to the firing.
8. The method of any one of claims 1 to 7 wherein the green body is heated sufficiently to cause substantially all of the fugitive pore forming agent to volatilize and exit the green body prior to the firing.
9. The method of any one of claims 1 to 8 wherein the fugitive pore forming agent volatilizes and exits the green body prior to the conversion of the ceramic forming precursor batch composition into the porous ceramic material.
10. The method of any one of claims 1 to 9 wherein the fugitive pore forming agent is recovered after exiting the green body.
11. The method of claim 10 wherein the recovered fugitive pore forming agent is mixed with an additional amount of the ceramic forming inorganic batch components and formed into another green body.
12. The method of any one of claims 1 to 1 1 wherein the ceramic forming precursor batch composition further comprises a binder.
13. The method of claim 12 further comprising heating the green body sufficient to decompose the binder, wherein the fugitive pore forming agent is removed from the green body prior to decomposition of the binder.
14. The method of claim 12 or 13 wherein the binder comprises methylcellulose.
15. A ceramic precursor batch composition comprising ceramic forming inorganic batch components and a pore forming agent comprising cyclododecane.
16. A method for manufacturing a porous ceramic article, comprising the steps of: mixing ceramic forming inorganic batch components and at least one fugitive pore forming agent to provide a ceramic forming precursor batch composition, wherein the fugitive pore forming agent comprises an alicyclic hydrocarbon; and firing the ceramic forming precursor batch composition under conditions effective to convert the ceramic forming precursor batch composition into a porous ceramic material.
17. The method of claim 16 wherein the alicyclic hydrocarbon is cyclododecane.
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EP2607336A1 (en) * 2010-08-19 2013-06-26 Hitachi Metals, Ltd. Manufacturing method for ceramic honeycomb structure
EP3124138A1 (en) * 2015-07-28 2017-02-01 Commissariat à l'énergie atomique et aux énergies alternatives Additive manufacturing method and machine reducing the risk of scattering powder during handling
CN115038550A (en) * 2020-01-31 2022-09-09 3M创新有限公司 Bonded abrasive article and method of manufacture

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EP2390307A1 (en) * 2010-05-27 2011-11-30 Corning Incorporated Porous ceramic processing using prilled wax and non-ionic surfactant
EP2607336A1 (en) * 2010-08-19 2013-06-26 Hitachi Metals, Ltd. Manufacturing method for ceramic honeycomb structure
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US9085091B2 (en) 2010-08-19 2015-07-21 Hitachi Metals, Ltd. Production method of ceramic honeycomb structure
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US8679385B2 (en) 2010-11-29 2014-03-25 Corning Incorporated Method of forming porous ceramic articles using inert gas
EP3124138A1 (en) * 2015-07-28 2017-02-01 Commissariat à l'énergie atomique et aux énergies alternatives Additive manufacturing method and machine reducing the risk of scattering powder during handling
FR3039439A1 (en) * 2015-07-28 2017-02-03 Commissariat Energie Atomique METHOD AND ADDITIVE MANUFACTURING MACHINE REDUCING THE RISK OF DISSEMINATION OF POWDER DURING HANDLING
US10576540B2 (en) 2015-07-28 2020-03-03 Commissariat A L'energie Atomique Et Aux Energies Alternatives Method and machine for additive manufacturing reducing risks of powder dissemination during manipulations
CN115038550A (en) * 2020-01-31 2022-09-09 3M创新有限公司 Bonded abrasive article and method of manufacture

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