WO2009129152A2 - Low coefficient of thermal expansion materials including nonstoichiometric cordierite fibers and methods of manufacture - Google Patents

Low coefficient of thermal expansion materials including nonstoichiometric cordierite fibers and methods of manufacture Download PDF

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Publication number
WO2009129152A2
WO2009129152A2 PCT/US2009/040245 US2009040245W WO2009129152A2 WO 2009129152 A2 WO2009129152 A2 WO 2009129152A2 US 2009040245 W US2009040245 W US 2009040245W WO 2009129152 A2 WO2009129152 A2 WO 2009129152A2
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WIPO (PCT)
Prior art keywords
fibers
fibrous
mixture
precursor materials
honeycomb
Prior art date
Application number
PCT/US2009/040245
Other languages
French (fr)
Other versions
WO2009129152A3 (en
Inventor
James Jenq Liu
William M. Carty
Bilal Zuberi
Sunilkumar C. Pillai
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Geo2 Technologies, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Geo2 Technologies, Inc. filed Critical Geo2 Technologies, Inc.
Priority to JP2011505107A priority Critical patent/JP2011521868A/en
Priority to CN2009801138162A priority patent/CN102036933A/en
Priority to EP09733067A priority patent/EP2265558A4/en
Publication of WO2009129152A2 publication Critical patent/WO2009129152A2/en
Publication of WO2009129152A3 publication Critical patent/WO2009129152A3/en
Priority to ZA2010/06831A priority patent/ZA201006831B/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D39/00Filtering material for liquid or gaseous fluids
    • B01D39/14Other self-supporting filtering material ; Other filtering material
    • B01D39/20Other self-supporting filtering material ; Other filtering material of inorganic material, e.g. asbestos paper, metallic filtering material of non-woven wires
    • B01D39/2068Other inorganic materials, e.g. ceramics
    • B01D39/2082Other inorganic materials, e.g. ceramics the material being filamentary or fibrous
    • B01D39/2086Other inorganic materials, e.g. ceramics the material being filamentary or fibrous sintered or bonded by inorganic agents
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    • 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
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    • C04B35/62227Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres
    • C04B35/62231Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres based on oxide ceramics
    • C04B35/6224Fibres based on silica
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Definitions

  • the invention generally relates to a fibrous ceramic material, and more particularly to a low coefficient of thermal expansion fibrous material including a plurality of nonstoichiometric cordierite fibers and methods of manufacturing the fibrous material.
  • Advanced ceramic materials are commonly utilized in systems located in hostile environments, such as, for example, automotive engines (e.g., catalytic converters), aerospace applications (e.g., space shuttle titles), refractory operations (e.g., firebrick) and electronics (e.g., capacitors, insulators).
  • Porous ceramic bodies are of particular use as filters in these environments.
  • ceramic honeycomb substrates i.e., a porous ceramic body
  • Ceramic honeycomb substrates provide high specific surface area for filtration and support for catalytic reactions and, at the same time, are stable and substantially structurally sound at high operating temperatures associated with an automotive engine environment.
  • ceramic materials such as for example, cordierite
  • ceramic materials are inert materials that perform well in high temperature environments.
  • ceramic materials are not immune to thermal stresses, such as those stresses generated from cycling between ambient temperature and high temperature applications.
  • thermal stresses such as those stresses generated from cycling between ambient temperature and high temperature applications.
  • ceramic filters are known to degrade making them inefficient and ineffective for today's applications.
  • embodiments described herein feature a fibrous ceramic material that can be utilized in a variety of applications, including as a filter in an automotive engine environment.
  • the fibrous ceramic material includes a plurality of nonstoichiometric cordierite fibers (i.e., fibers having a compositional structure of R x Mg2Al4 + 2 ⁇ Si5- x Oi8 or where x is greater than 0 and R is an element other than Mg, Al, Si, or O).
  • Embodiments described herein also feature methods of making the fibrous ceramic material.
  • the fibrous ceramic material is made by forming the R x Mg 2 Al 4+2 ⁇ Si 5 _ ⁇ Oi 8 or R x Mg2- ⁇ Al4Si5 ⁇ i8 fibers via a reaction between two or more precursor materials, wherein at least one of the two or more precursor materials is in the form of a fiber.
  • the plurality of R x Mg2Al 4+ 2 ⁇ Si5_ ⁇ Oi8 or R x Mg2- ⁇ Al 4 Si5 ⁇ i8 fibers made by reaction are extruded or otherwise shaped into a fibrous body.
  • the CTE can be further lowered by changing the compositional structure of the fibers. For example, by altering the compositional structure of cordierite from its stoichiometric form, one can manipulate the crystal lattice of the fibrous material resulting in directional changes to the value of the CTE.
  • embodiments described in the present disclosure are directed to a method of manufacturing a fibrous material wherein at least about 5% of all fibers within the fibrous material have either R x Mg2Al4 + 2 ⁇ Si5- ⁇ 0i8 or RxMg 2 -XAl 4 SiSOiS compositional structure.
  • the method includes mixing at least two R ⁇ Mg2Al 4+ 2 ⁇ Si5- ⁇ Oi8 or R x Mg 2 -XAl 4 SiSOiS precursor materials to form a mixture (one or more of the at least two R x Mg 2 Al 4+2 ⁇ Si5- ⁇ 0i8 or R x Mg 2 _ x Al 4 Si5 ⁇ i8 precursors being in the form of a fiber); extruding the mixture to create a fibrous body; and heat treating the fibrous body to form the fibrous material.
  • Embodiments of this aspect of the invention can include one or more of the following features.
  • at least about 25% of all fibers therein have one of the R x Mg 2 Al 4+2x Si5- ⁇ 0i8 or R x Mg 2 - X Al 4 Si 5 Oi 8 compositional structure. That is about 25% (e.g., 30%, 35%, 45%, 55%, 65% or more) of the precursor fibers reacted to form either R x Mg 2 Al 4+2X Si 5 _ x Oi 8 or R x Mg 2 - x Al4Si5 ⁇ i8 fibers.
  • one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
  • the mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
  • embodiments described herein are directed to a method of manufacturing a fibrous body including R x Mg 2 Al4 +2x Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS fibers.
  • the method includes mixing at least two R x Mg 2 Al4 +2 ⁇ Si5_ x Oi8 or R x Mg 2 - x Al4Si5 ⁇ i8 precursor materials to form a mixture, wherein one or more of the at least two R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 -XAl 4 Si 5 OiS precursor materials is in the form of a fiber; reacting the at least two R x Mg 2 Al4 +2x Si 5 _ x Ois or R x Mg 2 -XAl 4 Si 5 Oi 8 precursor materials to form a plurality of fibers within the mixture that have R ⁇ Mg 2 Al 4+ 2 ⁇ Si 5 - ⁇ 0i8 or
  • R x Mg 2 - X Al 4 Si 5 Oi S compositional structure and shaping the mixture into the fibrous body, wherein at least about 5% of all fibers within the fibrous body have either the R x Mg 2 Al 4+ 2 X Si 5 - x Oi8 compositional structure or the R x Mg 2 - x Al 4 Si 5 0i8 compositional structure.
  • Embodiments of this aspect of the invention can include one or more of the following features.
  • at least about 25% of all fibers within the fibrous body after reacting the at least two R x Mg 2 Al 4+2x Si 5 - x Oi8 or R x Mg 2 - x Al 4 Si 5 0i8 precursor materials have the R x Mg 2 Al 4+2x Si 5 - x Oi8 or R x Mg 2 - x Al 4 Si 5 0i8 compositional structure.
  • the fibers within the fibrous body after the reaction of the precursors have either the R x Mg 2 Al 4+2x Si 5 - x Oi8 compositional structure or R x Mg 2 - x Al 4 Si 5 0i8 compositional structure.
  • the fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction.
  • one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
  • the mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
  • embodiments of the invention are directed to a method of forming a porous honeycomb substrate.
  • the method includes mixing at least two R x Mg2Al 4+ 2 ⁇ Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS precursor materials to form a mixture, wherein one or more of the at least two R x Mg2Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 _ x Al 4 Si5 ⁇ i8 precursor materials is in a form of a fiber; extruding the mixture to form a honeycomb substrate having a porosity of at least about 20%; and heat treating the honeycomb substrate to react the at least two R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 -XAI 4 SiSOiS precursor materials to form a plurality of fibers having R x Mg 2 Al 4+2x Si 5 _ x Oi 8 or R x Mg2-
  • Embodiments of this aspect of the invention can include one or more of the following features.
  • at least about 25% of all fibers therein have one of the R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - X Al 4 Si S Oi S compositional structure.
  • the fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction.
  • one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
  • the mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
  • embodiments are directed to a R x Mg 2 Al 4+2x Si 5 _ x O is or R x Mg 2 - X Al 4 Si S Oi S fibrous honeycomb body.
  • the fibrous honeycomb body including a honeycomb array of walls defining channels between adjacent walls.
  • the walls include a plurality of R ⁇ Mg 2 Al 4+ 2 ⁇ Si5- ⁇ Oi8 or R x Mg 2 -X AUS15O is fibers bonded to form a porous structure having an open network of pores. About 20% of the plurality of fibers within the walls are aligned in a common direction.
  • Embodiments of this aspect can include one or more of the following features.
  • the walls within the fibrous honeycomb body can have a porosity of at least about 20% (e.g., 25%, 30%, 35%, 40%, 45%, 50%).
  • the plurality of R x Mg2Al 4+ 2 ⁇ Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS fibers have an aspect ratio greater than about 1 and less than or equal to 2,000.
  • a catalytic coating is disposed on the plurality of or R x Mg 2 -XAl 4 SiSOiS fibers.
  • inventions are directed to a filter.
  • the filter includes a housing including an inlet and an outlet. Disposed between the inlet and the outlet is a R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i8 fibrous honeycomb body.
  • the body includes a honeycomb array of walls defining channels between adjacent walls.
  • the walls include a plurality of R x Mg 2 Al 4+2x Si 5 _ x Oi 8 or R x Mg 2 - x Al 4 Si 5 ⁇ i 8 fibers bonded to form a porous structure having an open network of pores.
  • the fibers within the walls are aligned in a common direction.
  • at least one catalyst is deposited on the plurality of R x Mg 2 Al 4+2x Si 5 - x Oi8 or fibers.
  • FIG. 1 is a flow chart illustrating a method of forming a fibrous material in accordance with an embodiment of the disclosure.
  • FIG. 2 is a micrograph a portion of a fibrous material formed in accordance with the method of FIG. 1.
  • FIGS. 3 A and 3B are cross-sectional schematics illustrating the presence and the absence of pore formers and binders prior to and after a heat treatment, respectively.
  • FIG. 4 is a flow chart illustrating another method of forming a fibrous material in accordance with an embodiment of the disclosure.
  • FIG. 5 is a schematic illustrated in a perspective view showing a honeycomb body.
  • FIG. 6 is a schematic illustrated in a perspective view showing multiple honeycomb bodies to be adjoined to form a larger body.
  • FIG. 7 is a cross-sectional schematic of a filter that includes a honeycomb body of FIG. 5.
  • FIG. 8 is a schematic illustrating a method of forming a honeycomb body in accordance with an embodiment of the disclosure.
  • the ceramic materials described below have a low CTE value. It is believed that the low CTE value is achieved by one or more of: (1) a substantial alignment of fibers within the material, (2) a manipulation of one or more of the lattice parameters through an adjustment in compositional structure of the ceramic material or (3) a combination of the alignment process of (1) and the manipulation of one or more of the lattice parameters as described in (2) above.
  • the ceramic materials described herein can be utilized in numerous applications, including but not limited to filters for diesel applications.
  • using ceramic materials that have a high coefficient of thermal expansion within a catalytic filter can lead to poor or diminished performance and/or design flexibility.
  • diesel filters are prone to cracking during regeneration (i.e., a high temperature cycle used to burn out particulates trapped in the filter). Therefore, it would be advantageous to minimize the coefficient of thermal expansion of a ceramic material used in a diesel filter.
  • performance of a diesel filter increases with an increased value for the thermal shock parameter (TSP).
  • TSP modulus of rupture (MOR) divided the product of Young's modulus and the coefficient of thermal expansion (CTE).
  • the fibrous ceramic material formed using this method has an ultimate or final structure (i.e., a structure after completion of the method shown in Fig. 1) in which at least about 5% of all fibers therein have either the R x Mg2Al4 + 2 ⁇ Si5- x Oi8 or the R x Mg 2 - x Al 4 Si 5 ⁇ i 8 compositional structure.
  • the fibers within the final structure are interlocking, so as to form a three dimensional porous structure in which fluids (e.g., gases) can pass therethrough.
  • the method includes mixing at least two R x Mg2Al 4+ 2 ⁇ Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS precursor materials, such as a first precursor 105 and a second precursor 107 to form a mixture 120.
  • R x Mg2Al 4+ 2 ⁇ Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS precursor materials such as a first precursor 105 and a second precursor 107 to form a mixture 120.
  • a R x Mg 2 Al4 + 2 ⁇ Si5- x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i8 precursor is a material that when reacted with other materials forms a portion of the R x Mg 2 Al 4+2 ⁇ Si 5 - x Oi 8 or the R x Mg2- x AUSi5 ⁇ i8 compositional structure, respectively.
  • a possible R x Mg 2 Al 4+ 2 X Si5- x Oi8 precursor is Veegum clay (i.e., a clay that includes MgO, SiO, and Al 2 O 3 ); another possible precursor is Al 2 O 3 powder; another possible precursor is a sol of any material including Mg, Al, and/or Si; still yet another precursor is GeO where R in R x Mg2AU + 2 ⁇ Si5- x Oi8 represents Ge.
  • the above R x Mg 2 Al 4+ 2 X Si5_ x Oi8 precursors are also R x Mg 2 - x Al 4 Si5 ⁇ i8 precursors.
  • Precursors 105 and 107 can come in a number of forms.
  • the precursors can be fiber based, colloidal based, particle/powder based, or liquid solution based.
  • one or more of the at least two R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - x AUSi5 ⁇ i8 precursors is in the form of a fiber so that mixture 120 is a fiber based material.
  • precursor 105 and precursor 107 is in the form of a fiber, such as, for example, alumina fibers, silica fibers, mullite fibers, alumina silicate fibers (e.g., Al 2 O 3 SiO 2 fibers, mullite fibers, cordierite fibers), magnesium aluminate fibers, or magnesia silica fibers.
  • alumina fibers such as, for example, alumina fibers, silica fibers, mullite fibers, alumina silicate fibers (e.g., Al 2 O 3 SiO 2 fibers, mullite fibers, cordierite fibers), magnesium aluminate fibers, or magnesia silica fibers.
  • additives 110 such as, for example binders, rheology modifiers (e.g., fluids), and pore formers can be introduced into mixture 120.
  • These additives 110 can be used to modify or manipulate the consistency of mixture 120 so as to aid in later form shaping processes.
  • these additives 110 can be used as pore place holders. That is, these additives are inert with respect to the R x Mg 2 Al 4+2x Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS precursors and can be removed from the mixture 120 after the form shaping processes, thereby allowing for increased porosity in the ultimate form.
  • the mixture 120 is shaped 130 into a form.
  • shaping 130 can occur by extrusion of the mixture 120.
  • extrusion of a fibrous mixture such as mixture 120, results in the substantial alignment of fibers. For example, it is believed that at least about 20% of the fibers within a fibrous mixture are substantially aligned in a common direction after extrusion. Fig.
  • extruded fibrous structure 175 shows an extruded fibrous structure 175 in which an average of 80% of all fibers within the form are aligned along line a-a shown therein. Shear forces that act upon the mixture during extrusion tend to orient the fibers in the direction of extrusion. It will be appreciated that extrusion designs, mixture rheologies, and fiber content and fiber rigidity can influence the orientation behavior of the extruded mixture.
  • shaping processes 130 other than extrusion, can also be utilized to create the form.
  • Other shaping processes include molding, such as injection molding, and casting. In these shaping processes, fiber alignment may occur to a lesser degree than with extrusion.
  • the form can be fired at a temperature of less than about 1,420 0 C for several hours to cause a reaction between the two or more R x Mg2Al4 + 2 ⁇ Si5- x Oi8 precursors or two or more RxMgi-xAUSisOis precursors.
  • the form can be fired at a temperature of less than about 1,420 0 C for several hours to cause a reaction between the two or more R x Mg2Al4 + 2 ⁇ Si5- x Oi8 precursors or two or more RxMgi-xAUSisOis precursors.
  • at least 5% of all fibers within the form are transformed into either R x Mg2Al 4+ 2 ⁇ Si5_ ⁇ Oi8 or R x Mg2- ⁇ Al 4 Si5 ⁇ i8 fibers.
  • the R x Mg2Al4 + 2 ⁇ Si5- ⁇ Oi8 precursors included mullite fibers, MgCO 3 particles, and Ge ⁇ 2 particles
  • 5% or more of the fibers therein are transformed to have the following compositional structure: Ge x Mg 2 Al 4+ ⁇ Si 5 _ ⁇ Oi 8 (where x will be dependent on the relative ratios of the precursors used).
  • the application of energy e.g., heat
  • heat also allows for the creation of bonds between the fibers.
  • heat is applied (e.g., directly in the case of a furnace or inductively as when an RF source is utilized), water and other additives are eliminated or reduced resulting in fiber-to-fiber contact. (See FIGS.
  • bonds may be formed in several ways at these fiber-to-fiber contact sites.
  • a number of types of sintering mechanism can be utilized, including but not limited to liquid assisted sintering, solid state sintering, and reaction-phase sintering wherein a chemical reaction occurs at the fiber-to-fiber contact site.
  • the ceramic material formed utilizing method 100 is a fibrous material having interlocked fibers, wherein at least 5% of all fibers have the either R x Mg2Al 4+ 2 ⁇ Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS compositional structure.
  • the fibrous form can be further processed as shown in step 150 in FIG. 1. Further processing steps include: (a) additional heat treatments to create further bonds between fibers or to remove additives such as pore formers, organic binders, and fluids, such as water (b) application of coatings, such as, for example catalytic coatings on the fibers, (c) introduction of increased porosity or creation of directed flow channels via mechanical processing (e.g., drilling or capping/filling passageways), and (d) incorporating the fibrous material into a filter or other apparatus.
  • additional heat treatments to create further bonds between fibers or to remove additives such as pore formers, organic binders, and fluids, such as water
  • coatings such as, for example catalytic coatings on the fibers
  • introduction of increased porosity or creation of directed flow channels via mechanical processing e.g., drilling or capping/filling passageways
  • incorporating the fibrous material into a filter or other apparatus.
  • a method 200 of forming a fibrous body includes mixing at least two R x Mg2Al4 + 2 X Si5- x Oi8 precursors or R x Mg 2 - x Al 4 Si 5 ⁇ i 8 precursors (205 and 207) together with any optional additives 210 to form a mixture 220.
  • One or more of the at least two R x Mg 2 Al 4+2X Si 5 _ x Oi 8 or R x Mg2- x Al4Si5 ⁇ i8 precursors 205 and 207 is in fiber form.
  • Energy such as heat or light
  • a reaction 230 between the two or more R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 -XAl 4 SiSOiS precursors.
  • the optional additives 210 are inert with respect to the precursors 205 and 207, and as a result do not participate in the reaction.
  • the reacted mixture 230 is then shaped 240 into the fibrous body through extrusion, molding, or other shaping technique.
  • Optional processing steps 250 such as, for example, heat treating the fibrous body to remove or reduce the amount of optional additives 210, sintering the fibrous body to create bonds between fibers, introducing further porosity or directed flow channels into the fibrous body, depositing coatings, and/or incorporating the fibrous material into a filter or other apparatus can be performed after the fibrous body is shaped 240.
  • the R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i8 precursors utilized in methods 100 and 200 can be supplied in various forms. As discussed above, one or more of the at least two R x Mg 2 Al4 + 2 ⁇ Si5- x Oi8 or precursors is in the form of a fiber so that any resulting mixture of the precursors is a fiber based material.
  • R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 _ x Al 4 Si5 ⁇ i8 precursors in fiber form includes, but is not limited to: alumina silicate fibers, such as for example, mullite fibers, aluminosilicate H95C fibers, strontium aluminum silicate fibers, lithium aluminum silicate fibers, and aluminoborosilicate fibers, magnesium silicate fibers, such as, for example Isofrax fibers (a biosoluble fiber available from ISOFRAX, Niagara Falls, NY), magnesium strontium silicate fibers, and magnesium calcium strontium silicate fibers, Al 2 O 3 fiber, SiO fibers, MgO fibers, Li 2 O fibers, where R is Li, and SrCO 3 fibers where R is Sr.
  • alumina silicate fibers such as for example, mullite fibers, aluminosilicate H95C fibers, strontium aluminum silicate fibers, lithium aluminum silicate fiber
  • these fibers have an aspect ratio (i.e., the ratio of the length of the fiber divided by the diameter of the fiber) greater than one.
  • the "diameter" of the fiber assumes for simplicity that the sectional shape of the fiber is a circle; this simplifying assumption is applied to fibers regardless of their true section shape (e.g., square, triangular, etc.)
  • the fibers have an aspect ratio that is less than or equal to 2,000. That is, in certain embodiments, the fibers have a diameter in the micron or submicron range (e.g., 1 micron) while the length of the fibers is a few millimeters (e.g., 2 millimeters).
  • the fibers can have a diameter ranging from about 100 nm to about 100 microns. However, in certain embodiments, the fibers have a diameter within the range of about 100 nm to about 10 microns and in some embodiments, the fibers have a diameter within the range of about 2 microns to about 10 microns.
  • the at least two R x Mg2Al 4+ 2 X Si5_ x Oi8 or R x Mg2_ x Al 4 Si5 ⁇ i8 precursors can be all in fiber form or alternatively, the precursors can be any combination of fibers and some other form.
  • R x Mg2Al4 + 2 X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i8 precursors which are not in fiber form, include but are not limited to: MgCO 3 particles, colloidal silica, silica particles, Al 2 O 3 particles, sols of any material including Mg, Al, or Si, Veegum clays, talcs, or particles, SrCO 3 particles where R is Sr, GeO 2 particles where R is Ge, K 2 O particles where R is K, LiO where R is Li, and MnO particles where R in Mn.
  • MgCO 3 particles colloidal silica, silica particles, Al 2 O 3 particles, sols of any material including Mg, Al, or Si, Veegum clays, talcs, or particles
  • any precursor material that when reacted with other constituents forms a portion of a R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 _ x Al 4 SIsO is fiber can be utilized in methods 100 and 200.
  • the specific R x Mg2Al 4+ 2 X Si5_ x Oi8 precursors or precursors and precursor amounts utilized are selected in accordance with a target fiber chemistry and crystal structure. That is, the amount and type of precursor 105/205 and the amount and type of precursors 107/207 are selected based on the target fiber chemistry and crystal structure.
  • a targeted fiber chemistry is Ca x Mg 2 Al 4+2 ⁇ Si 5 - x Oi 8 having a cordierite type crystal structure (i.e., orthorhombic crystal structure)
  • the following four R x Mg 2 Al 4+2X Si 5 _ x Oi 8 precursors having the following weight percents could be used: 71.2% aluminosilicate fiber: 21.9% Isofrax fiber: 5.3% MgCO 3 particles: 1.5% CaCO 3 particles.
  • the same target fiber chemistry i.e., Ca x Mg 2 Al 4+2X Si 5 _ x Oi 8
  • the following weigh percents of the precursors can be utilized: 62% aluminosilicate fiber: 18% Isofrax fiber: 6.9 % MgCO 3 particles : 12.5% CaCO 3 particles.
  • the relative amounts of the at least two precursors also affects the amount of precursor fibers that participate in reaction 140/230.
  • the relative amounts of the precursors should be substantially equal to their solubility limits for a particular solid solution having a particular crystal structure. If the relative amounts vary from the solubility limit but are still within a range therein to form a particular crystal structure, then the reaction can be limited due to a shortage of one or more elements. As a result, not all of the precursor fibers will participate in the reaction and thus some precursor fibers will remain in the fibrous body after reaction 140/230 has taken place.
  • the fibrous body can include less than 100% R x Mg 2 Al 4+2 ⁇ Sis- x Oi8 or R x Mg 2 - x AUSi5 ⁇ i8 fibers.
  • about 45% of the fibers within a fibrous body are transformed to Ca x Mg 2 Al 4+2 ⁇ Si 5 - x Oi 8 fibers when a ratio of 76.8% mullite fibers: 6.2%
  • Isofrax fibers: 17% bentonite clay is mixed together
  • about 10% of the fibers within a fibrous body are transformed to Ca x Mg 2 Al 4+2X Si5_ x Oi8 fibers when a ratio of 91% mullite fibers: 3.8% Isofrax fibers: 5.1% bentonite clay is used.
  • the fibrous material can be tailored to provide a low CTE value.
  • cordierite, Mg 2 Al 4 Si5 ⁇ i8 is known to have a relatively low average CTE value (1 x 10-6/ 0 C).
  • cordierite' s chemistry R x Mg 2 Al 4+2X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si 5 ⁇ i 8
  • lower CTE values especially in a particular lattice direction can be achieved.
  • further tailoring of the material's CTE value can be achieved.
  • the fibrous materials resulting from methods 100 and 200 can be shaped into porous honeycomb substrates or bodies, which can be utilized as filters and in particular, filters for automotive applications.
  • the honeycomb body 510 has an array of walls 515 that define channels 520 between adjacent walls 515.
  • the walls 515 comprise the fibrous material described above. That is, the walls 515 include a plurality of either R x Mg2Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i8 fibers bonded to form a porous structure.
  • the porous structure has at least 20% porosity and typically has an open-network of pores so that fluids can flow through the structure.
  • At least 20% of the R x Mg 2 Al 4+ 2 X Si5_ x Oi8 or R x Mg 2 - x Al 4 Si5 ⁇ i 8 fibers within the walls 515 are aligned.
  • material properties such as the coefficient of thermal expansion, which have directional values, can be manipulated to provide a lower value in a particular direction. That is, the fibers can be aligned along a particular lattice direction, such as the lattice parameter (a, b, or c) which has the lowest CTE value.
  • the fibers can be extruded or otherwise shaped such that at least 20% (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%, 90%) of the fibers are substantially aligned along the c direction.
  • the walls of the honeycomb body 510 can then be formed such that the c direction of the aligned fibers falls within the plane of the walls 515. As a result, the walls will experience the least amount of expansion when exposed to heat.
  • the fibers in the material can be aligned such that 20% or more (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%) of the fibers are aligned along a direction that has the highest CTE value.
  • the walls 515 of the honeycomb body 510 are formed such that the aligned fibers form the smallest dimension (i.e., depth) of the walls 515 so that the area greatest affected by heat is positioned to have the least structural effect.
  • the honeycomb body 510 can be fabricated in any number of shapes such as, for example, a cylinder (shown in FIG. 5), a pie-shaped wedge or subcylindrical section, a rectangle (as shown in FIG. 6), or a diamond. These honeycomb bodies 510 can be glued together to form a segmented body as shown in FIG. 6. As a result of gluing the bodies together, any size, shape, or dimension honeycomb form can be generated.
  • FIG. 7 depicts a cross-sectional representation of a filter 700 utilizing the porous honeycomb body 510 of FIG. 5.
  • the filter 700 includes a housing 720, which surrounds the porous honeycomb body 510.
  • the housing includes an inlet 705 and an outlet 707 through which gasses, such as exhaust gasses, travel through.
  • a mat 730 Between the housing 720 and the honeycomb body 510 is a mat 730 that supports and forms an airtight seal between the housing 720 and the honeycomb body 510.
  • the honeycomb body 510 is configured in a wall-flow configuration by selectively plugging alternate channels, with outlet blocks 760 and inlet blocks 770 to form a plurality of respective inlet channels 740 and outlet channels 750.
  • the open network of pores within the walls 515 provides sufficient porosity and permeability to permit flow through the walls 515 between the inlet and outlet channels 740, 750.
  • particulate matter can be accumulated on the surface of the inlet channel walls 740, and be removed from the gas stream by means of the filter 700.
  • Coatings such as, catalytic coatings or other reactive coatings, can be deposited along the walls 515 to increase the concentration of particles captured by the walls 515.
  • the walls 515 can be coated with a catalytic coating that facilitates oxidation of accumulated soot and accelerates the conversion of exhaust gas into less-harmful constituents. Techniques for applying catalytic and other types of coatings to substrates and porous bodies are well known in the field of art.
  • FIG. 8 illustrates a method of forming a honeycomb body, such as honeycomb body 510 of FIG. 5.
  • a honeycomb body such as honeycomb body 510 of FIG. 5.
  • step 810 at least two R x Mg 2 Al 4+2X Si 5 _ x Oi 8 or R x Mg2- x Al4Si5 ⁇ i8 precursors wherein one or more of the precursors is in fiber form are mixed together to form a mixture.
  • Fluid, pore formers, and/or rheology agents such as binders can also be added to the mixture to enable efficient extrusion or shaping of the mixture.
  • the mixture is extruded into a honeycomb body having at least 20% porosity (step 820) and then heated to react the at least two
  • steps 830 and 840 occur during one heat treatment process.
  • multiple heat treating processes are utilized to react the R x Mg2Al 4+ 2 ⁇ Si5_ ⁇ Oi8 or R x Mg 2 -XAl 4 SiSOIg precursors, to substantially eliminate optional additives, and to sinter fibers.
  • inlet and outlet blocks e.g., 740, 750 in FIG. 7 are inserted to create a flow path through the filter (optional step 850).
  • a catalytic coating can be applied to the filter to provide the filter with reactive functionality in its intended application, such as, for example, to promote oxidation of captured soot in a diesel particulate filter (optional step 960).
  • the fibrous material can be used in any application where a low coefficient of thermal expansion ceramic material would be desired, such as for example, in the aerospace industry, liquid filtration, cross flow filtration, molten metal filtration, fixed bed chemical reactors, honeycomb high surface area adsorbents, and high temperature reactors.
  • the following precursors are mixed together: 71.2 grams of mullite fibers, 21.9 grams of Isofrax fibers, 5.3 grams Of MgCO 3 particles, and 1.5 grams Of CaCO 3 .
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose (an organic binder and rheology modifier), 65 grams of carbon particles (-45 micron mesh grade and utilized as a pore former), and 130 grams of deionized water as a mixing fluid.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 88% porosity.
  • RF radio-frequency
  • More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca 0 1 Mg 2 Al 4 iSUgOig fibers having an orthorhombic crystal structure.
  • the coefficient of thermal expansion of the porous ceramic body is
  • the following precursors are mixed together: 62 grams of mullite fibers, 18.6 grams of Isofrax fibers, 6.9 grams Of MgCO 3 particles, and 12.5 grams Of CaCO 3 .
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 130 grams of deionized water.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca I Mg 2 Al 3 Si 4 Oi S fibers having a triclinic crystal structure.
  • the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10 -6/°C and the fibers are observed to be approximately 70- 80% aligned in the extrusion direction.
  • the following precursors are mixed together: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, 2.0 grams of MgCO 3 particles, and 0.6 grams of CaCO 3 .
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), and 70 grams of deionized water.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 77% porosity.
  • RF radio-frequency
  • the coefficient of thermal expansion of the porous ceramic body is 3.2 x 10 -6/ 0 C.
  • the following precursors are mixed together: 161.8 grams of mullite fibers, 13 grams of Isofrax fibers, and 35.9 grams of bentonite clay.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 130 grams of deionized water.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio- frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 75% porosity.
  • RF radio- frequency
  • the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/ 0 C.
  • the following precursors are mixed together: 53.2 grams of mullite fibers, 2.2 grams of Isofrax fibers, and 3 grams of bentonite clay.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydro xypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 60 grams of deionized water.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 86% porosity.
  • RF radio-frequency
  • the coefficient of thermal expansion of the porous ceramic body is 3.1 x 10-6/ 0 C.
  • the target fiber chemistry is Ge 0 S Mg 2 Al 4 8 Si 42 Oi S with an orthorhombic crystal structure
  • the following precursors are mixed together: 59.8 grams of alumina silicate fibers, 6 grams of Isofrax fibers, and 11.1 grams of GeO 2 particles.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), 23.2 grams Of MgCO 3 as binder, and 130 grams of deionized water as a mixing fluid.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 85% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ge 0 8 Mg 2 Al 4 sSU 2 Oi 8 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/ 0 C.
  • the target fiber chemistry is MniMgiAl 4 Si5 ⁇ i8 with an orthorhombic crystal structure
  • the following precursors are mixed together: 63.8 grams of alumina silicate fibers, 19.8 grams of Isofrax fibers, and 11.9 grams of MnO particles.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade),4.6 grams of MgCO 3 as binder, and 70 grams of deionized water as a mixing fluid.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 82% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mn 1 Mg 1 Al 4 SIsO 1S fibers having an orthorhombic crystal structure.
  • the coefficient of thermal expansion of the porous ceramic body is 0.6 x 10-6/ 0 C.
  • the target fiber chemistry is K 0 5 Mg 2 Al 45 Si 45 O 18 with an orthorhombic crystal structure
  • the following precursors are mixed together: 71.2 grams of alumina silicate fibers, 2.3 grams of Isofrax fibers, and 1.2 grams of K 2 O particles.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), 25 grams of MgCO 3 as binder, and 70 grams of deionized water as a mixing fluid.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 86% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ko 5Mg 2 AUsSiO 4 SOiS fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.8 x 10-6/ 0 C.
  • the target fiber chemistry is Ko SMg 2 Al 4 SSi 4 SOiS with an orthorhombic crystal structure
  • the following precursors are mixed together: 49.4 grams of mullite fibers, 39.6 grams of Isofrax fibers, and 1.2 grams of K 2 O particles.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (_45 micron mesh grade), 9.7 grams of MgCO 3 as binder, and 70 grams of deionized water as a mixing fluid.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form K 05 Mg 2 Al 4 S SUsOi S fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/ 0 C.
  • the target fiber chemistry is Fe 045 Mg I 55 Al 4 Si 5 ⁇ i 8 with an orthorhombic crystal structure
  • the following precursors are mixed together: 42 grams of mullite fibers, 46.9 grams of Isofrax fibers, and 11.1 grams of Fe 2 O 3 particles.
  • the following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), and 70 grams of deionized water.
  • the materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion.
  • the substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 87% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form FeO 45 MgI 55 Al 4 Si 5 Oi8 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/ 0 C.
  • the targeted fiber chemistry is a modified cordierite structure which includes 10% cordierite fibers with 90% alumina silicate fibers.
  • the 90% alumina silicate with 10% cordierite fibrous material is prepared by mixing the following precursor materials to form an extrudable mixture: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, and 2.0 grams of MgCO 3 particles.
  • the following additives are also added to the extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (_45 micron mesh grade), and 70 grams of deionized water.
  • the materials are mixed and extruded to form 1" diameter honeycomb substrate.
  • the substrate is dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0 C for two hours to form a porous honeycomb structure having about 77% porosity. Only 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mg 2 Al 4 Si 5 ⁇ i 8 fibers.
  • the coefficient of thermal expansion of the porous ceramic body is 2.8 x 10-6/ 0 C.

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Abstract

A fibrous ceramic material comprises a plurality of fibers having a RxMg2A14+xSi5-xO18 or RxMg2-XA14Si5O18 compositional structure. The fibrous ceramic material is form by combining two or more RxMg2A14+xSi5-xO18 or RxMg2-XA14Si5O18 precursors in which at least one of the two or more RxMg2A14+xSi5-xO18 or RxMg2-XA14Si5O18 precursors is in fiber form. The fibrous ceramic material is shaped to form a fibrous body in which at least about 20% of all fibers therein are aligned in a substantially common direction.

Description

LOW COEFFICIENT OF THERMAL EXPANSION MATERIALS INCLUDING NONSTOICHIOMETRIC CORDIERITE FIBERS AND METHODS OF
MANUFACTURE
FIELD OF THE INVENTION
The invention generally relates to a fibrous ceramic material, and more particularly to a low coefficient of thermal expansion fibrous material including a plurality of nonstoichiometric cordierite fibers and methods of manufacturing the fibrous material.
BACKGROUND
Advanced ceramic materials are commonly utilized in systems located in hostile environments, such as, for example, automotive engines (e.g., catalytic converters), aerospace applications (e.g., space shuttle titles), refractory operations (e.g., firebrick) and electronics (e.g., capacitors, insulators). Porous ceramic bodies are of particular use as filters in these environments. For example, today's automotive industry uses ceramic honeycomb substrates (i.e., a porous ceramic body) to host catalytic oxidation and reduction of exhaust gases, and to filter particulate emissions. Ceramic honeycomb substrates provide high specific surface area for filtration and support for catalytic reactions and, at the same time, are stable and substantially structurally sound at high operating temperatures associated with an automotive engine environment.
In general, ceramic materials, such as for example, cordierite, are inert materials that perform well in high temperature environments. However, ceramic materials are not immune to thermal stresses, such as those stresses generated from cycling between ambient temperature and high temperature applications. Thus, ceramic filters are known to degrade making them inefficient and ineffective for today's applications. SUMMARY OF THE INVENTION
In general, embodiments described herein feature a fibrous ceramic material that can be utilized in a variety of applications, including as a filter in an automotive engine environment. The fibrous ceramic material includes a plurality of nonstoichiometric cordierite fibers (i.e., fibers having a compositional structure of RxMg2Al4+2χSi5-xOi8 or
Figure imgf000004_0001
where x is greater than 0 and R is an element other than Mg, Al, Si, or O). Embodiments described herein also feature methods of making the fibrous ceramic material. Specifically, in one embodiment, the fibrous ceramic material is made by forming the RxMg2Al4+2χSi5_χOi8 or RxMg2-χAl4Si5θi8 fibers via a reaction between two or more precursor materials, wherein at least one of the two or more precursor materials is in the form of a fiber. The plurality of RxMg2Al4+2χSi5_χOi8 or RxMg2-χAl4Si5θi8 fibers made by reaction are extruded or otherwise shaped into a fibrous body. During extrusion or shaping, it is believed that fiber alignment occurs resulting in a decrease of the coefficient of thermal expansion (CTE) in at least one direction of the fibrous body. As a result of the decrease in CTE, a porous, fibrous ceramic body with minimal cracking and minimal expansion at high temperatures can be generated. In addition, in certain embodiments, the CTE can be further lowered by changing the compositional structure of the fibers. For example, by altering the compositional structure of cordierite from its stoichiometric form, one can manipulate the crystal lattice of the fibrous material resulting in directional changes to the value of the CTE.
In one aspect, embodiments described in the present disclosure are directed to a method of manufacturing a fibrous material wherein at least about 5% of all fibers within the fibrous material have either RxMg2Al4+2χSi5-χ0i8 or RxMg2-XAl4SiSOiS compositional structure. The method includes mixing at least two RχMg2Al4+2χSi5-χOi8 or RxMg2-XAl4SiSOiS precursor materials to form a mixture (one or more of the at least two RxMg2Al4+2χSi5-χ0i8 or RxMg2_xAl4Si5θi8 precursors being in the form of a fiber); extruding the mixture to create a fibrous body; and heat treating the fibrous body to form the fibrous material.
Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments after heat treating the fibrous body at least about 25% of all fibers therein have one of the RxMg2Al4+2xSi5-χ0i8 or RxMg2-XAl4Si5Oi8 compositional structure. That is about 25% (e.g., 30%, 35%, 45%, 55%, 65% or more) of the precursor fibers reacted to form either RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 fibers. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
In another aspect, embodiments described herein are directed to a method of manufacturing a fibrous body including RxMg2Al4+2xSi5_xOi8 or RxMg2-XAl4SiSOiS fibers. The method includes mixing at least two RxMg2Al4+2χSi5_xOi8 or RxMg2-xAl4Si5θi8 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+2XSi5_xOi8 or RxMg2-XAl4Si5OiS precursor materials is in the form of a fiber; reacting the at least two RxMg2Al4+2xSi5_xOis or RxMg2-XAl4Si5Oi8 precursor materials to form a plurality of fibers within the mixture that have RχMg2Al4+2χSi5-χ0i8 or
RxMg2-XAl4Si5OiS compositional structure; and shaping the mixture into the fibrous body, wherein at least about 5% of all fibers within the fibrous body have either the RxMg2Al4+2XSi5-xOi8 compositional structure or the RxMg2-xAl4Si50i8 compositional structure.
Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments at least about 25% of all fibers within the fibrous body after reacting the at least two RxMg2Al4+2xSi5-xOi8 or RxMg2-xAl4Si50i8 precursor materials have the RxMg2Al4+2xSi5-xOi8 or RxMg2-xAl4Si50i8 compositional structure. That is, at least 25% (e.g., 35%, 45%, 55%, 65%, 75%, 85%, 95%) of all the fibers within the fibrous body after the reaction of the precursors have either the RxMg2Al4+2xSi5-xOi8 compositional structure or RxMg2-xAl4Si50i8 compositional structure. The fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
In yet another aspect, embodiments of the invention are directed to a method of forming a porous honeycomb substrate. The method includes mixing at least two RxMg2Al4+2χSi5_xOi8 or RxMg2-XAl4SiSOiS precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+2XSi5_xOi8 or RxMg2_xAl4Si5θi8 precursor materials is in a form of a fiber; extruding the mixture to form a honeycomb substrate having a porosity of at least about 20%; and heat treating the honeycomb substrate to react the at least two RxMg2Al4+2XSi5_xOi8 or RxMg2-XAI4SiSOiS precursor materials to form a plurality of fibers having RxMg2Al4+2xSi5_xOi8 or RxMg2-xAUSi5θi8 compositional structure so that at least about 5% of all fibers within the honeycomb substrate have the RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 compositional structure.
Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments after heat treating the honeycomb substrate at least about 25% of all fibers therein have one of the RxMg2Al4+2XSi5_xOi8 or RxMg2-XAl4SiSOiS compositional structure. The fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.
In another aspect, embodiments are directed to a RxMg2 Al4+2xSi5_xO is or RxMg2-XAl4SiSOiS fibrous honeycomb body. The fibrous honeycomb body including a honeycomb array of walls defining channels between adjacent walls. The walls include a plurality of RχMg2Al4+2χSi5-χOi8 or RxMg2-X AUS15O is fibers bonded to form a porous structure having an open network of pores. About 20% of the plurality of fibers within the walls are aligned in a common direction.
Embodiments of this aspect can include one or more of the following features. The walls within the fibrous honeycomb body can have a porosity of at least about 20% (e.g., 25%, 30%, 35%, 40%, 45%, 50%). In some embodiments, the plurality of RxMg2Al4+2χSi5_xOi8 or RxMg2-XAl4SiSOiS fibers have an aspect ratio greater than about 1 and less than or equal to 2,000. In certain embodiments, a catalytic coating is disposed on the plurality of
Figure imgf000007_0001
or RxMg2-XAl4SiSOiS fibers.
In another aspect of the invention, embodiments are directed to a filter. The filter includes a housing including an inlet and an outlet. Disposed between the inlet and the outlet is a RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 fibrous honeycomb body. The body includes a honeycomb array of walls defining channels between adjacent walls. The walls include a plurality of RxMg2Al4+2xSi5_xOi8 or RxMg2-xAl4Si5θi8 fibers bonded to form a porous structure having an open network of pores. In some embodiments the fibers within the walls are aligned in a common direction. In certain embodiments, at least one catalyst is deposited on the plurality of RxMg2Al4+2xSi5-xOi8 or
Figure imgf000007_0002
fibers.
BRIEF DESCRIPTION OF THE DRAWINGS
In the drawings, like reference characters generally refer to the same parts throughout the different views. Also, the drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention.
FIG. 1 is a flow chart illustrating a method of forming a fibrous material in accordance with an embodiment of the disclosure.
FIG. 2 is a micrograph a portion of a fibrous material formed in accordance with the method of FIG. 1.
FIGS. 3 A and 3B are cross-sectional schematics illustrating the presence and the absence of pore formers and binders prior to and after a heat treatment, respectively.
FIG. 4 is a flow chart illustrating another method of forming a fibrous material in accordance with an embodiment of the disclosure.
FIG. 5 is a schematic illustrated in a perspective view showing a honeycomb body.
Fig. 6 is a schematic illustrated in a perspective view showing multiple honeycomb bodies to be adjoined to form a larger body. FIG. 7 is a cross-sectional schematic of a filter that includes a honeycomb body of FIG. 5.
FIG. 8 is a schematic illustrating a method of forming a honeycomb body in accordance with an embodiment of the disclosure.
DETAILED DESCRIPTION
In general, by reducing a ceramic material's CTE value, cracking due to thermal stresses can be minimized. The ceramic materials described below have a low CTE value. It is believed that the low CTE value is achieved by one or more of: (1) a substantial alignment of fibers within the material, (2) a manipulation of one or more of the lattice parameters through an adjustment in compositional structure of the ceramic material or (3) a combination of the alignment process of (1) and the manipulation of one or more of the lattice parameters as described in (2) above.
The ceramic materials described herein can be utilized in numerous applications, including but not limited to filters for diesel applications. In diesel automotive applications, using ceramic materials that have a high coefficient of thermal expansion within a catalytic filter can lead to poor or diminished performance and/or design flexibility. Specifically, diesel filters are prone to cracking during regeneration (i.e., a high temperature cycle used to burn out particulates trapped in the filter). Therefore, it would be advantageous to minimize the coefficient of thermal expansion of a ceramic material used in a diesel filter. In addition, performance of a diesel filter increases with an increased value for the thermal shock parameter (TSP). The thermal shock parameter is defined as follows: TSP = modulus of rupture (MOR) divided the product of Young's modulus and the coefficient of thermal expansion (CTE). As a result, a ceramic material having a low coefficient of thermal expansion will have greater performance.
Referring to Fig. 1, a method 100 for manufacturing a fibrous ceramic material is illustrated. The fibrous ceramic material formed using this method has an ultimate or final structure (i.e., a structure after completion of the method shown in Fig. 1) in which at least about 5% of all fibers therein have either the RxMg2Al4+2χSi5-xOi8 or the RxMg2-xAl4Si5θi8 compositional structure. The fibers within the final structure are interlocking, so as to form a three dimensional porous structure in which fluids (e.g., gases) can pass therethrough. The method includes mixing at least two RxMg2Al4+2χSi5_xOi8 or RxMg2-XAl4SiSOiS precursor materials, such as a first precursor 105 and a second precursor 107 to form a mixture 120. (While Fig. 1, shows two precursors, any number of precursors greater than or equal to two can be utilized.) A RxMg2Al4+2χSi5-xOi8 or RxMg2-xAl4Si5θi8 precursor is a material that when reacted with other materials forms a portion of the RxMg2Al4+2χSi5-xOi8 or the RxMg2-xAUSi5θi8 compositional structure, respectively. For example, a possible RxMg2Al4+2XSi5-xOi8 precursor is Veegum clay (i.e., a clay that includes MgO, SiO, and Al2O3); another possible precursor is Al2O3 powder; another possible precursor is a sol of any material including Mg, Al, and/or Si; still yet another precursor is GeO where R in RxMg2AU+2χSi5-xOi8 represents Ge. (The above RxMg2Al4+2XSi5_xOi8 precursors are also RxMg2-xAl4Si5θi8 precursors.)
Precursors 105 and 107 can come in a number of forms. For example, the precursors can be fiber based, colloidal based, particle/powder based, or liquid solution based. However, one or more of the at least two RxMg2Al4+2XSi5_xOi8 or RxMg2-xAUSi5θi8 precursors (i.e., 105 and 107) is in the form of a fiber so that mixture 120 is a fiber based material. That is, at least one of precursor 105 and precursor 107 is in the form of a fiber, such as, for example, alumina fibers, silica fibers, mullite fibers, alumina silicate fibers (e.g., Al2O3SiO2 fibers, mullite fibers, cordierite fibers), magnesium aluminate fibers, or magnesia silica fibers.
Optionally, additives 110, such as, for example binders, rheology modifiers (e.g., fluids), and pore formers can be introduced into mixture 120. These additives 110 can be used to modify or manipulate the consistency of mixture 120 so as to aid in later form shaping processes. In addition, these additives 110 can be used as pore place holders. That is, these additives are inert with respect to the RxMg2Al4+2xSi5_xOi8 or RxMg2-XAl4SiSOiS precursors and can be removed from the mixture 120 after the form shaping processes, thereby allowing for increased porosity in the ultimate form.
After the RxMg2Al4+xSi5_xOi8 or RxMg2_xAl4Si5θi8 precursors (i.e., 105 and 107) with any optional additives 110 are mixed and homogenized, the mixture 120 is shaped 130 into a form. In one embodiment, shaping 130 can occur by extrusion of the mixture 120. Without wishing to be bound by theory, it is believed that extrusion of a fibrous mixture, such as mixture 120, results in the substantial alignment of fibers. For example, it is believed that at least about 20% of the fibers within a fibrous mixture are substantially aligned in a common direction after extrusion. Fig. 2 shows an extruded fibrous structure 175 in which an average of 80% of all fibers within the form are aligned along line a-a shown therein. Shear forces that act upon the mixture during extrusion tend to orient the fibers in the direction of extrusion. It will be appreciated that extrusion designs, mixture rheologies, and fiber content and fiber rigidity can influence the orientation behavior of the extruded mixture.
Other shaping processes 130, other than extrusion, can also be utilized to create the form. Examples of other shaping processes include molding, such as injection molding, and casting. In these shaping processes, fiber alignment may occur to a lesser degree than with extrusion.
Once shaped, energy is applied to the form to initiate a reaction 140 between the precursors 105 and 107. For example, the form can be fired at a temperature of less than about 1,4200C for several hours to cause a reaction between the two or more RxMg2Al4+2χSi5-xOi8 precursors or two or more RxMgi-xAUSisOis precursors. As a result of this reaction, at least 5% of all fibers within the form are transformed into either RxMg2Al4+2χSi5_χOi8 or RxMg2-χAl4Si5θi8 fibers. For example, if the RxMg2Al4+2χSi5-χOi8 precursors included mullite fibers, MgCO3 particles, and Geθ2 particles, under the influence of heat, 5% or more of the fibers therein are transformed to have the following compositional structure: GexMg2Al4+χSi5_χOi8 (where x will be dependent on the relative ratios of the precursors used). The application of energy (e.g., heat) also allows for the creation of bonds between the fibers. As heat is applied (e.g., directly in the case of a furnace or inductively as when an RF source is utilized), water and other additives are eliminated or reduced resulting in fiber-to-fiber contact. (See FIGS. 3 A and 3B showing fiber 300 interactions as a result of the presence and the removal of pore formers 305 and binders 310, respectively). It will be appreciated that the bonds may be formed in several ways at these fiber-to-fiber contact sites. For example, a number of types of sintering mechanism can be utilized, including but not limited to liquid assisted sintering, solid state sintering, and reaction-phase sintering wherein a chemical reaction occurs at the fiber-to-fiber contact site. As a result of fiber bond formation, the ceramic material formed utilizing method 100 is a fibrous material having interlocked fibers, wherein at least 5% of all fibers have the either RxMg2Al4+2χSi5_xOi8 or RxMg2-XAl4SiSOiS compositional structure.
As an optional step, the fibrous form can be further processed as shown in step 150 in FIG. 1. Further processing steps include: (a) additional heat treatments to create further bonds between fibers or to remove additives such as pore formers, organic binders, and fluids, such as water (b) application of coatings, such as, for example catalytic coatings on the fibers, (c) introduction of increased porosity or creation of directed flow channels via mechanical processing (e.g., drilling or capping/filling passageways), and (d) incorporating the fibrous material into a filter or other apparatus.
In another embodiment, shown in FIG. 4, a method 200 of forming a fibrous body includes mixing at least two RxMg2Al4+2XSi5-xOi8 precursors or RxMg2- xAl4Si5θi8 precursors (205 and 207) together with any optional additives 210 to form a mixture 220. One or more of the at least two RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 precursors 205 and 207 is in fiber form. Energy, such as heat or light, is applied to the mixture to initiate a reaction 230 between the two or more RxMg2Al4+2XSi5_xOi8 or RxMg2-XAl4SiSOiS precursors. The optional additives 210 are inert with respect to the precursors 205 and 207, and as a result do not participate in the reaction. The reacted mixture 230 is then shaped 240 into the fibrous body through extrusion, molding, or other shaping technique. Optional processing steps 250, such as, for example, heat treating the fibrous body to remove or reduce the amount of optional additives 210, sintering the fibrous body to create bonds between fibers, introducing further porosity or directed flow channels into the fibrous body, depositing coatings, and/or incorporating the fibrous material into a filter or other apparatus can be performed after the fibrous body is shaped 240.
The RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 precursors utilized in methods 100 and 200 can be supplied in various forms. As discussed above, one or more of the at least two RxMg2Al4+2χSi5-xOi8 or
Figure imgf000011_0001
precursors is in the form of a fiber so that any resulting mixture of the precursors is a fiber based material. An illustrative list of RxMg2Al4+2XSi5_xOi8 or RxMg2_xAl4Si5θi8 precursors in fiber form includes, but is not limited to: alumina silicate fibers, such as for example, mullite fibers, aluminosilicate H95C fibers, strontium aluminum silicate fibers, lithium aluminum silicate fibers, and aluminoborosilicate fibers, magnesium silicate fibers, such as, for example Isofrax fibers (a biosoluble fiber available from ISOFRAX, Niagara Falls, NY), magnesium strontium silicate fibers, and magnesium calcium strontium silicate fibers, Al2O3 fiber, SiO fibers, MgO fibers, Li2O fibers, where R is Li, and SrCO3 fibers where R is Sr. In general, these fibers have an aspect ratio (i.e., the ratio of the length of the fiber divided by the diameter of the fiber) greater than one. As used herein, the "diameter" of the fiber assumes for simplicity that the sectional shape of the fiber is a circle; this simplifying assumption is applied to fibers regardless of their true section shape (e.g., square, triangular, etc.) In certain embodiments, the fibers have an aspect ratio that is less than or equal to 2,000. That is, in certain embodiments, the fibers have a diameter in the micron or submicron range (e.g., 1 micron) while the length of the fibers is a few millimeters (e.g., 2 millimeters). In general, the fibers can have a diameter ranging from about 100 nm to about 100 microns. However, in certain embodiments, the fibers have a diameter within the range of about 100 nm to about 10 microns and in some embodiments, the fibers have a diameter within the range of about 2 microns to about 10 microns.
The at least two RxMg2Al4+2XSi5_xOi8 or RxMg2_xAl4Si5θi8 precursors can be all in fiber form or alternatively, the precursors can be any combination of fibers and some other form. Other RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 precursors, which are not in fiber form, include but are not limited to: MgCO3 particles, colloidal silica, silica particles, Al2O3 particles, sols of any material including Mg, Al, or Si, Veegum clays, talcs, or particles, SrCO3 particles where R is Sr, GeO2 particles where R is Ge, K2O particles where R is K, LiO where R is Li, and MnO particles where R in Mn. The above list of precursors is for illustrative purposes only and is by no means exhaustive. That is, any precursor material that when reacted with other constituents forms a portion of a RxMg2Al4+2XSi5_xOi8 or RxMg2_x Al4SIsO is fiber can be utilized in methods 100 and 200.
The specific RxMg2Al4+2XSi5_xOi8 precursors or
Figure imgf000012_0001
precursors and precursor amounts utilized are selected in accordance with a target fiber chemistry and crystal structure. That is, the amount and type of precursor 105/205 and the amount and type of precursors 107/207 are selected based on the target fiber chemistry and crystal structure. For example, if a targeted fiber chemistry is CaxMg2Al4+2χSi5-xOi8 having a cordierite type crystal structure (i.e., orthorhombic crystal structure), then the following four RxMg2Al4+2XSi5_xOi8 precursors having the following weight percents could be used: 71.2% aluminosilicate fiber: 21.9% Isofrax fiber: 5.3% MgCO3 particles: 1.5% CaCO3 particles. Similarly if the same target fiber chemistry (i.e., CaxMg2Al4+2XSi5_xOi8) is desired but instead of an orthorhombic crystal structure a triclinic or anorthite crystal structure is desired, then the following weigh percents of the precursors can be utilized: 62% aluminosilicate fiber: 18% Isofrax fiber: 6.9 % MgCO3 particles : 12.5% CaCO3 particles. By lowering the amount of Al but increasing the amount of Ca available during the reaction, a different crystal structure forms and thus different lattice parameters and associated properties are achieved. As a result, the fiber chemistry and crystal structure can be tailored to achieve optimum properties for a specific application.
In addition to determining the crystal structure of the resulting fiber, the relative amounts of the at least two precursors also affects the amount of precursor fibers that participate in reaction 140/230. In order for all or substantially all of the precursor material to participate in the reaction 140/230 the relative amounts of the precursors should be substantially equal to their solubility limits for a particular solid solution having a particular crystal structure. If the relative amounts vary from the solubility limit but are still within a range therein to form a particular crystal structure, then the reaction can be limited due to a shortage of one or more elements. As a result, not all of the precursor fibers will participate in the reaction and thus some precursor fibers will remain in the fibrous body after reaction 140/230 has taken place. Accordingly, the fibrous body can include less than 100% RxMg2Al4+2χSis-xOi8 or RxMg2-xAUSi5θi8 fibers. For example, about 45% of the fibers within a fibrous body are transformed to CaxMg2Al4+2χSi5-xOi8 fibers when a ratio of 76.8% mullite fibers: 6.2% Isofrax fibers: 17% bentonite clay is mixed together; whereas about 10% of the fibers within a fibrous body are transformed to CaxMg2Al4+2XSi5_xOi8 fibers when a ratio of 91% mullite fibers: 3.8% Isofrax fibers: 5.1% bentonite clay is used.
With the ability to control fiber chemistry and crystal structure, the fibrous material can be tailored to provide a low CTE value. For example, cordierite, Mg2Al4Si5θi8, is known to have a relatively low average CTE value (1 x 10-6/0C). However, by modifying cordierite' s chemistry (RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8) and crystal structure, lower CTE values, especially in a particular lattice direction can be achieved. Moreover, by providing fiber alignment within the fibrous material, further tailoring of the material's CTE value can be achieved.
The fibrous materials resulting from methods 100 and 200 can be shaped into porous honeycomb substrates or bodies, which can be utilized as filters and in particular, filters for automotive applications.
Referring to FIG. 5, a porous honeycomb body 510 is shown. The honeycomb body 510 has an array of walls 515 that define channels 520 between adjacent walls 515. The walls 515 comprise the fibrous material described above. That is, the walls 515 include a plurality of either RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 fibers bonded to form a porous structure. The porous structure has at least 20% porosity and typically has an open-network of pores so that fluids can flow through the structure. At least 20% of the RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 fibers within the walls 515 are aligned. As a result, material properties, such as the coefficient of thermal expansion, which have directional values, can be manipulated to provide a lower value in a particular direction. That is, the fibers can be aligned along a particular lattice direction, such as the lattice parameter (a, b, or c) which has the lowest CTE value. For example, if a particular material has the lowest CTE along the c direction, then the fibers can be extruded or otherwise shaped such that at least 20% (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%, 90%) of the fibers are substantially aligned along the c direction. The walls of the honeycomb body 510 can then be formed such that the c direction of the aligned fibers falls within the plane of the walls 515. As a result, the walls will experience the least amount of expansion when exposed to heat. Similarly, the fibers in the material can be aligned such that 20% or more (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%) of the fibers are aligned along a direction that has the highest CTE value. In this embodiment, the walls 515 of the honeycomb body 510 are formed such that the aligned fibers form the smallest dimension (i.e., depth) of the walls 515 so that the area greatest affected by heat is positioned to have the least structural effect.
The honeycomb body 510 can be fabricated in any number of shapes such as, for example, a cylinder (shown in FIG. 5), a pie-shaped wedge or subcylindrical section, a rectangle (as shown in FIG. 6), or a diamond. These honeycomb bodies 510 can be glued together to form a segmented body as shown in FIG. 6. As a result of gluing the bodies together, any size, shape, or dimension honeycomb form can be generated. With a low coefficient of thermal expansion porous fibrous material, it is possible to extrude or otherwise form shapes (e.g., cylinders) with large widths (e.g., diameters between 5.66 inches and 14 inches) without utilizing a low Young's modulus glue/adhesive to adjoin smaller segments to form a larger form. The ability to extrude or form larger widths provides flexibility in production techniques and potential cost reduction in volume production.
FIG. 7 depicts a cross-sectional representation of a filter 700 utilizing the porous honeycomb body 510 of FIG. 5. The filter 700 includes a housing 720, which surrounds the porous honeycomb body 510. The housing includes an inlet 705 and an outlet 707 through which gasses, such as exhaust gasses, travel through. Between the housing 720 and the honeycomb body 510 is a mat 730 that supports and forms an airtight seal between the housing 720 and the honeycomb body 510. The honeycomb body 510 is configured in a wall-flow configuration by selectively plugging alternate channels, with outlet blocks 760 and inlet blocks 770 to form a plurality of respective inlet channels 740 and outlet channels 750. In this embodiment, the open network of pores within the walls 515 provides sufficient porosity and permeability to permit flow through the walls 515 between the inlet and outlet channels 740, 750. As a result, particulate matter can be accumulated on the surface of the inlet channel walls 740, and be removed from the gas stream by means of the filter 700. Coatings, such as, catalytic coatings or other reactive coatings, can be deposited along the walls 515 to increase the concentration of particles captured by the walls 515. For example, for a filter used in a diesel automotive environment, the walls 515 can be coated with a catalytic coating that facilitates oxidation of accumulated soot and accelerates the conversion of exhaust gas into less-harmful constituents. Techniques for applying catalytic and other types of coatings to substrates and porous bodies are well known in the field of art.
FIG. 8 illustrates a method of forming a honeycomb body, such as honeycomb body 510 of FIG. 5. First, as shown in step 810, at least two RxMg2Al4+2XSi5_xOi8 or RxMg2-xAl4Si5θi8 precursors wherein one or more of the precursors is in fiber form are mixed together to form a mixture. Fluid, pore formers, and/or rheology agents such as binders can also be added to the mixture to enable efficient extrusion or shaping of the mixture. After obtaining a desired consistency, the mixture is extruded into a honeycomb body having at least 20% porosity (step 820) and then heated to react the at least two
RxMg2Al4+2χSi5_xOi8 or RxMg2-XAl4SiSOiS precursors and to substantially eliminate or remove the optional additives (i.e., fluids, pore formers, and binders (step 830)). At least 5% of all of the fibers within the honeycomb body are transformed to have either the RxMg2Al4+2χSi5_xOi8 or RxMg2-χAl4Si5θi8 compositional structure. Bonds between fibers (i.e., between the fibers formed from the precursors in step 830 and any unreacted fibers) are formed via sintering 840 the honeycomb body. In some embodiments, steps 830 and 840 occur during one heat treatment process. In other embodiments, multiple heat treating processes are utilized to react the RxMg2Al4+2χSi5_χOi8 or RxMg2-XAl4SiSOIg precursors, to substantially eliminate optional additives, and to sinter fibers. In embodiments where the honeycomb body is a filter, inlet and outlet blocks (e.g., 740, 750 in FIG. 7) are inserted to create a flow path through the filter (optional step 850). In addition, a catalytic coating can be applied to the filter to provide the filter with reactive functionality in its intended application, such as, for example, to promote oxidation of captured soot in a diesel particulate filter (optional step 960).
Variations, modifications, and other implementations of what is described herein will occur to those of ordinary skill in the art without departing from the spirit and scope of the invention. For example, while an number of embodiments have been described in which the fibrous material has been utilized as a filter, especially a filter for diesel applications, the fibrous material can be used in any application where a low coefficient of thermal expansion ceramic material would be desired, such as for example, in the aerospace industry, liquid filtration, cross flow filtration, molten metal filtration, fixed bed chemical reactors, honeycomb high surface area adsorbents, and high temperature reactors. EXAMPLES
The following examples are provided to further illustrate and to facilitate the understanding of the disclosure. These specific examples are intended to be illustrative of the disclosure and are not intended to be limiting.
In a first illustrative example in which the target fiber chemistry is CaxMg2Al4+xSi5_xOi8 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 71.2 grams of mullite fibers, 21.9 grams of Isofrax fibers, 5.3 grams Of MgCO3 particles, and 1.5 grams Of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose (an organic binder and rheology modifier), 65 grams of carbon particles (-45 micron mesh grade and utilized as a pore former), and 130 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 88% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0 1Mg2Al4 iSUgOig fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is
0.8 x 10-6/0C and the fibers are observed to be approximately 70-80% aligned in the extrusion direction.
In a second illustrative in which the target fiber chemistry is CaxMg2Al4+xSi5-xOi8 (where x =1.0) with a triclinic crystal structure, the following precursors are mixed together: 62 grams of mullite fibers, 18.6 grams of Isofrax fibers, 6.9 grams Of MgCO3 particles, and 12.5 grams Of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 130 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form CaIMg2Al3Si4OiS fibers having a triclinic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10 -6/°C and the fibers are observed to be approximately 70- 80% aligned in the extrusion direction.
In a third illustrative example in which the target fiber chemistry is CaxMg2Al4+xSi5_xOi8 (where x =0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, 2.0 grams of MgCO3 particles, and 0.6 grams of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), and 70 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0C for two hours to form a porous honeycomb structure having about 77% porosity. Approximately 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Cao 1Mg2Al4 1SU9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 3.2 x 10 -6/0C.
In a third illustrative example in which the target fiber chemistry is CaxMg2Al4+xxSi5_xOi8 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 161.8 grams of mullite fibers, 13 grams of Isofrax fibers, and 35.9 grams of bentonite clay. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 130 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio- frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 75% porosity. Approximately, 45% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Cao 1Mg2Al41SU9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/0C.
In a fourth illustrative example in which the target fiber chemistry is CaxMg2Al4+xxSi5-xOi8 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 53.2 grams of mullite fibers, 2.2 grams of Isofrax fibers, and 3 grams of bentonite clay. The following additives are also added to form an extrudable mixture: 16 grams of hydro xypropyl methylcellulose, 65 grams of carbon particles (-45 micron mesh grade), and 60 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 86% porosity. Approximately, 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0 1Mg2Al4 iSUgOis fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 3.1 x 10-6/0C.
In a fifth illustrative example in which the target fiber chemistry is Ge0 SMg2Al4 8Si42OiS with an orthorhombic crystal structure, the following precursors are mixed together: 59.8 grams of alumina silicate fibers, 6 grams of Isofrax fibers, and 11.1 grams of GeO2 particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), 23.2 grams Of MgCO3 as binder, and 130 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0C for two hours to form a porous honeycomb structure having about 85% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ge0 8Mg2Al4 sSU 2Oi8 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/0C.
In a sixth illustrative example in which the target fiber chemistry is MniMgiAl4Si5θi8 with an orthorhombic crystal structure, the following precursors are mixed together: 63.8 grams of alumina silicate fibers, 19.8 grams of Isofrax fibers, and 11.9 grams of MnO particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade),4.6 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0C for two hours to form a porous honeycomb structure having about 82% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mn1Mg1Al4SIsO1S fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.6 x 10-6/0C.
In a seventh illustrative example in which the target fiber chemistry is K0 5Mg2Al45Si45O18 with an orthorhombic crystal structure, the following precursors are mixed together: 71.2 grams of alumina silicate fibers, 2.3 grams of Isofrax fibers, and 1.2 grams of K2O particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), 25 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300 0C for two hours to form a porous honeycomb structure having about 86% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ko 5Mg2AUsSiO4SOiS fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.8 x 10-6/0C.
In an eight illustrative example in which the target fiber chemistry is Ko SMg2Al4SSi4SOiS with an orthorhombic crystal structure, the following precursors are mixed together: 49.4 grams of mullite fibers, 39.6 grams of Isofrax fibers, and 1.2 grams of K2O particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (_45 micron mesh grade), 9.7 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form K05Mg2Al4 SSUsOiS fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/0C.
In a ninth illustrative example in which the target fiber chemistry is Fe045MgI 55Al4Si5θi8 with an orthorhombic crystal structure, the following precursors are mixed together: 42 grams of mullite fibers, 46.9 grams of Isofrax fibers, and 11.1 grams of Fe2O3 particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (-45 micron mesh grade), and 70 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1" diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 87% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form FeO45MgI 55Al4Si5Oi8 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7 x 10-6/0C.
In a tenth illustrative example, the targeted fiber chemistry is a modified cordierite structure which includes 10% cordierite fibers with 90% alumina silicate fibers. Thus, in this example there is no R to modify the cordierite structure, however modification from the cordierite structure is achieve by having less than 95% conversion of the precursor materials so that the ultimate fiber chemistry is a blend of cordierite and alumina silicate. The 90% alumina silicate with 10% cordierite fibrous material is prepared by mixing the following precursor materials to form an extrudable mixture: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, and 2.0 grams of MgCO3 particles. The following additives are also added to the extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (_45 micron mesh grade), and 70 grams of deionized water. The materials are mixed and extruded to form 1" diameter honeycomb substrate. The substrate is dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,3000C for two hours to form a porous honeycomb structure having about 77% porosity. Only 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mg2Al4Si5θi8 fibers. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 2.8 x 10-6/0C.

Claims

CLAIMSWe Claim:
1. A method of manufacturing a fibrous material wherein at least about 5% of all fibers within the fibrous material have a RxMg2Al4+xSi5_xOi8 compositional structure or a RxMg2-xAl4Si5θi8 compositional structure, the method comprising: mixing at least two RxMg2Al4+xSi5_xOi8 precursor materials or RxMg2-xAl4Si5θi8 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4SisOi8 precursor materials is in a form of a fiber; extruding the mixture to create a fibrous body; and heat treating the fibrous body to form the fibrous material.
2. The method of claim 1 wherein after heat treating at least about 25% of all fibers within the fibrous body have either the RxMg2Al4+xSi5_xOi8 compositional structure or the RxMg2-xAl4Si5θi8 compositional structure.
3. The method of claim 1 wherein one or more of the at least two RxMg2Al4+xSi5_xOi8 or RxMg2-x Al4SIsO is precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
4. The method of claim 1 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.
5. The method of claim 4 wherein the one or more additives are substantially removed by heating the fibrous body.
6. A method of manufacturing a fibrous body including RxMg2Al4+xSi5-xOi8 or RxMg2-xAl4Si5θi8 fibers, the method comprising: mixing at least two RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4Si5θi8 precursor materials to form a mixture, wherein one or more of the at least two
Figure imgf000024_0001
or
RχMg2-χAl4Si5θi8 precursor materials is in a form of a fiber; reacting the at least two RxMg2 Al4+xSi5_xOi8 or
Figure imgf000024_0002
precursor materials to form a plurality of fibers within the mixture that have RxMg2Al4+χSi5_xOi8 or RxMg2-XAl4Si5OiS compositional structure; and shaping the mixture into the fibrous body, wherein at least about 5% of all fibers within the fibrous body have either the RxMg2Al4+xSi5_xOi8 compositional structure or the RxMg2-xAl4Si5Oi8 compositional structure.
7. The method of claim 6 wherein at least about 25% of all fibers within the fibrous body after reacting the at least two RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4Si5Oi8 precursor materials have the RxMg2 Al4+xSi5_xOi8 or
Figure imgf000024_0003
compositional structure, respectively.
8 The method of claim 6 wherein at least about 20% of all fibers within the fibrous body are aligned in a common direction.
9. The method of claim 6 wherein one or more of the at least two RxMg2Al4+xSi5_xOi8 or RxMg2-UAl4Si5O is precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
10. The method of claim 6 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.
11. The method of claim 10 wherein the one or more additives are substantially removed by heating the fibrous body.
12. A method of forming a porous honeycomb substrate, the method comprising: mixing at least two RxMg2Al4+xSi5_xOis or RxMg2-xAl4Si50is precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+xSi5-xOi8 or RxMg2-xAl4Si50i8 precursor materials is in a form of a fiber; extruding the mixture to form a honeycomb substrate having a porosity of at least about 20%; and heat treating the honeycomb substrate to react the at least two RxMg2Al4+xSi5-xOi8 or RxMg2-xAl4Sis0i8 precursor materials to form a plurality of fibers having RxMg2Al4+xSi5_xOi8 or RxMg2_xAl4Si5θi8 compositional structure so that at least about 5% of all fibers within the honeycomb substrate have the RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4Sis0i8 compositional structure.
13. The method of claim 12 wherein after heat treating the honeycomb substrate at least about 25% of all fibers have the RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4Si5θi8 compositional structure.
14. The method of claim 12 wherein one or more of the at least two RxMg2Al4+xSi5_xOi8 or RxMg2-x Al4SIsO is precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.
15. The method of claim 12 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.
16. The method of claim 15 wherein the one or more additives are substantially removed by heating the honeycomb substrate.
17. A RxMg2Al4+xSi5-xOi8 or
Figure imgf000025_0001
fibrous honeycomb body comprising: a honeycomb array of walls defining channels between adjacent walls; the walls comprising a plurality of RxMg2 Al4+xSis_xO is or RxMg2-xAl4SisOis fibers bonded to form a porous structure having an open network of pores, wherein at least about 20% of the plurality of RxMg2 Al4+xSis_xO is or RxMg2-xAl4SisOis fibers within the walls being aligned in a common direction.
18. The RxMg2Al4+xSi5_xOi8 or RxMg2-xAl4Si5θi8 fibrous honeycomb body of claim 17, wherein the walls have a porosity of at least about 20%.
19. The RxMg2Al4+xSi5-xOi8 or RxMg2_xAUSi5θi8 fibrous honeycomb body of claim 17 wherein the plurality of RxMg2Al4+xSi5_xOi8 or RxMg2_x Al4SIsO is fibers have an aspect ratio greater than 1 and less than or equal to 2,000.
20. The RxMg2Al4+xSi5-xOi8 or RxMg2_xAl4Si5θi8 fibrous honeycomb body of claim 17 further comprising a catalytic coating on the plurality of RxMg2Al4+xSi5_xOi8 or RxMg2_xAl4Si5θi8 fibers.
21. A filter comprising: a housing including an inlet and an outlet; and the RxMg2Al4+xSi5_xOi8 or RxMg2_xAl4Si5θi8 fibrous honeycomb body of claim 17 disposed between the inlet and the outlet.
22. The filter of claim 21 further comprising at least one catalyst deposited on the plurality of RxMg2Al4+xSi5-xOi8 or RxMg2_xAl4Si5θi8 fibers of the walls.
PCT/US2009/040245 2008-04-17 2009-04-10 Low coefficient of thermal expansion materials including nonstoichiometric cordierite fibers and methods of manufacture WO2009129152A2 (en)

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CN2009801138162A CN102036933A (en) 2008-04-17 2009-04-10 Low coefficient of thermal expansion materials including nonstoichiometric cordierite fibers and methods of manufacture
EP09733067A EP2265558A4 (en) 2008-04-17 2009-04-10 Low coefficient of thermal expansion materials including nonstoichiometric cordierite fibers and methods of manufacture
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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070152364A1 (en) * 2005-11-16 2007-07-05 Bilal Zuberi Process for extruding a porous substrate
US7858554B2 (en) * 2007-05-24 2010-12-28 Geo2 Technologies, Inc. Cordierite fiber substrate and method for forming the same
US8038759B2 (en) * 2005-11-16 2011-10-18 Geoz Technologies, Inc. Fibrous cordierite materials
WO2020101968A1 (en) * 2018-11-16 2020-05-22 Corning Incorporated Cordierite-containing ceramic bodies, batch composition mixtures, and methods of manufacturing cordierite-containing ceramic bodies

Family Cites Families (170)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1335466A (en) 1919-09-02 1920-03-30 Hydraulic Press Mfg Co Extrusion-press
US1533813A (en) 1921-03-30 1925-04-14 Firm Heinrich Lanz Apparatus for separating and binding dust or other impurities in combustion air of combustion engines
US1993821A (en) 1931-10-03 1935-03-12 Carborundum Co Bond for abrasive articles
US2752001A (en) 1952-11-27 1956-06-26 Muller Jacques Filter for gaseous fluids
US3819334A (en) 1970-10-27 1974-06-25 Mitsui Mining & Smelting Co Catalytic reaction apparatus for purifying waste gases containing carbon monoxide
JPS5036248B1 (en) 1971-01-13 1975-11-22
US3790654A (en) * 1971-11-09 1974-02-05 Corning Glass Works Extrusion method for forming thinwalled honeycomb structures
JPS517475B2 (en) 1972-05-04 1976-03-08
US3961907A (en) 1972-12-08 1976-06-08 Minnesota Mining And Manufacturing Company Catalytic converter
US4071594A (en) 1974-09-03 1978-01-31 Aluminum Company Of America Production of continuous ceramic fibers
US4053011A (en) 1975-09-22 1977-10-11 E. I. Du Pont De Nemours And Company Process for reinforcing aluminum alloy
US4047965A (en) 1976-05-04 1977-09-13 Minnesota Mining And Manufacturing Company Non-frangible alumina-silica fibers
JPS53139872A (en) 1977-05-10 1978-12-06 Toray Industries Porous body comprising metal coated carbon fiber
DK183380A (en) 1979-05-11 1980-11-12 Shinetsu Chemical Co PROCEDURE FOR THE PREPARATION OF FOAMED CELL BODY OF VINYL CHLORIDE BASE RESIN
JPS5915028B2 (en) 1980-03-26 1984-04-07 ニチアス株式会社 Manufacturing method of catalyst carrier
US4329162A (en) 1980-07-03 1982-05-11 Corning Glass Works Diesel particulate trap
US4409284A (en) 1980-07-15 1983-10-11 Kabushiki Kaisha Kobe Seiko Sho Porous moldings made of accumulated mass of stringy or thready extrudates
US4448833A (en) 1981-06-16 1984-05-15 Nippondenso Co., Ltd. Porous ceramic body and a method of manufacturing the same
AU540009B2 (en) 1982-02-16 1984-10-25 Matsushita Electric Industrial Co., Ltd. Exhaust gas filter
US4417908A (en) 1982-02-22 1983-11-29 Corning Glass Works Honeycomb filter and method of making it
US4419108A (en) * 1982-02-22 1983-12-06 Corning Glass Works Filter apparatus and method of filtering
US4420316A (en) 1982-02-22 1983-12-13 Corning Glass Works Filter apparatus and method of making it
US4416676A (en) * 1982-02-22 1983-11-22 Corning Glass Works Honeycomb filter and method of making it
DE3444407A1 (en) 1984-12-05 1986-06-05 Didier-Werke Ag, 6200 Wiesbaden CERAMIC MOLDED PART WITH GRADIENT-SHAPED POROSITY AND THE USE THEREOF FOR THE PRODUCTION OF COMPOSITE MOLDED PARTS
GB2176179A (en) 1985-06-06 1986-12-17 Morgan Materials Technology Li Porous ceramic body formed by extrusion process
EP0213725A3 (en) 1985-08-05 1987-07-29 BREHK Ventures Method and apparatus for trapping and incinerating particulate matter found in diesel engine exhaust
DE3623786A1 (en) 1985-11-13 1987-05-14 Man Technologie Gmbh METHOD FOR PRODUCING SOOT FILTERS
US4828785A (en) 1986-01-27 1989-05-09 Lanxide Technology Company, Lp Inverse shape replication method of making ceramic composite articles
DE3632322A1 (en) 1986-09-19 1988-03-24 Otto Feuerfest Gmbh CATALYST MOLDED BODY AND METHOD AND DEVICE FOR PRODUCING IT
JPS63102911A (en) 1986-10-18 1988-05-07 日本碍子株式会社 Injection molding method of ceramic body
US5207807A (en) 1986-12-05 1993-05-04 Iveco Fiat S.P.A. Regenerable filter for exhaust gases of an internal-combustion engine
US4824711A (en) 1987-01-29 1989-04-25 The United States Of America As Represented By The United States National Aeronautics And Space Administration Ceramic honeycomb structures and method thereof
JP2548754B2 (en) 1987-12-02 1996-10-30 三菱重工業株式会社 Nitrogen oxide removal catalyst
US5194407A (en) 1987-12-16 1993-03-16 Stemcor Corporation Molten metal-resistant ceramic fiber-containing composition
US4868142A (en) 1987-12-16 1989-09-19 Stemcor Corporation Method of manufacturing a molten metal-resistant ceramic fiber composition
US5053092A (en) 1988-03-21 1991-10-01 Corning Incorporated Method for producing a sinterable extruded laminated article
US5075160A (en) 1988-06-13 1991-12-24 Martin Marietta Energy Systems, Inc. Ceramic fiber reinforced filter
US5108964A (en) 1989-02-15 1992-04-28 Technical Ceramics Laboratories, Inc. Shaped bodies containing short inorganic fibers or whiskers and methods of forming such bodies
US5153057A (en) 1989-02-15 1992-10-06 Technical Ceramics Laboratories, Inc. Shaped bodies containing short inorganic fibers or whiskers within a metal matrix
JPH0645130B2 (en) 1989-03-23 1994-06-15 日本碍子株式会社 Manufacturing method of ceramic honeycomb extrusion die
US5488017A (en) 1989-04-14 1996-01-30 General Electric Company Fibert reinforced ceramic matrix composite member
US4968467A (en) 1989-07-10 1990-11-06 Industrial Filter & Pump Mfg. Co. Hot gas filter
US5135896A (en) 1989-10-31 1992-08-04 North American Refractories Company Spinel bondable ceramic composition
US5126431A (en) 1989-12-29 1992-06-30 Phillips Petroleum Company Production and recovery of poly(arylene sulfide ketone) and poly(arylene sulfide diketone) resins
US5078818A (en) 1990-04-18 1992-01-07 Hexcel Corporation Method for producing a fiber-reinforced ceramic honeycomb panel
US5251564A (en) 1990-04-26 1993-10-12 Rim Julius J Combustion box exhaust filtration system and method
DE4040104A1 (en) 1990-12-16 1992-06-17 Behr Gmbh & Co FILTERS FOR AN AIR CONDITIONING OR HEATING SYSTEM FOR A MOTOR VEHICLE
US5098455A (en) 1990-12-21 1992-03-24 The Dow Chemical Company Regenerable exhaust gas filter element for diesel engines
DE4200995C2 (en) 1991-01-21 2002-02-14 Seibu Giken Fukuoka Kk Process for producing a honeycomb gas adsorption element or a honeycomb catalyst carrier
US5249948A (en) 1991-04-08 1993-10-05 Koslow Technologies Corporation Apparatus for the continuous extrusion of solid articles
US6194066B1 (en) 1991-04-24 2001-02-27 The United States Of America As Represented By The Secretary Of The Air Force Microscopic tube devices and method of manufacture
DE59208738D1 (en) 1991-05-04 1997-09-04 Hoechst Ag Porous honeycomb material, process for its production and its use
US5196120A (en) 1991-05-13 1993-03-23 Minnesota Mining And Manufacturing Company Ceramic-ceramic composite filter
JP2577147B2 (en) 1991-09-30 1997-01-29 日本碍子株式会社 Method for manufacturing ceramic honeycomb structure
JP3308979B2 (en) 1992-01-21 2002-07-29 バブコック日立株式会社 Method for producing denitration catalyst containing inorganic fibers
US5629067A (en) 1992-01-30 1997-05-13 Ngk Insulators, Ltd. Ceramic honeycomb structure with grooves and outer coating, process of producing the same, and coating material used in the honeycomb structure
JPH05270943A (en) 1992-03-27 1993-10-19 Nippon Soken Inc Fiber-reinforced porous body
JPH05306614A (en) 1992-04-28 1993-11-19 Matsushita Electric Ind Co Ltd Exhaust gas filter and manufacture thereof
ES2122001T3 (en) 1992-05-08 1998-12-16 Gates Formed Fibre Products MOLDABLE COMPOUND WITHOUT WEAVING AND IMPROVED MANUFACTURING METHOD.
US5376341A (en) 1992-07-24 1994-12-27 Corning Incorporated Catalytic converter for motorcycles
US5260035A (en) 1992-08-05 1993-11-09 Corning Incorporated Apparatus and method for modifying gaseous mixtures
US5545297A (en) 1992-08-11 1996-08-13 E. Khashoggi Industries Methods for continuously placing filaments within hydraulically settable compositions being extruded into articles of manufacture
US5662731A (en) 1992-08-11 1997-09-02 E. Khashoggi Industries Compositions for manufacturing fiber-reinforced, starch-bound articles having a foamed cellular matrix
US5549859A (en) 1992-08-11 1996-08-27 E. Khashoggi Industries Methods for the extrusion of novel, highly plastic and moldable hydraulically settable compositions
US5298046A (en) 1993-01-06 1994-03-29 Minnesota Mining And Manufacturing Company Diesel particulate filter element and filter
JPH08507599A (en) 1993-03-01 1996-08-13 エンゲルハード・コーポレーシヨン Improved catalytic combustion system including separate bodies
NL9300642A (en) 1993-04-15 1994-11-01 Tno Process for the production of ceramic hollow fibers, in particular hollow fiber membranes for microfiltration, ultrafiltration and gas separation.
JPH0768172A (en) 1993-07-20 1995-03-14 Sakai Chem Ind Co Ltd Catalyst for catalyst production of nox and method thereof
JP2938740B2 (en) 1993-12-14 1999-08-25 日本碍子株式会社 Cordierite-based ceramic filter and method of manufacturing the same
US5518678A (en) 1994-01-26 1996-05-21 Kawata Manufacturing Co., Ltd. Adsorptive honeycomb-shaped ceramic structure and method for its production
US6040266A (en) 1994-02-22 2000-03-21 Ultramet Foam catalyst support for exhaust purification
US5518833A (en) 1994-05-24 1996-05-21 Eagle-Picher Industries, Inc. Nonwoven electrode construction
US5611831A (en) 1994-11-16 1997-03-18 Isuzu Ceramics Research Institute Co., Ltd. Diesel particulate filter apparatus
US5623013A (en) 1994-12-16 1997-04-22 Ube Industries, Ltd. Xonotlite-reinforced organic polymer composition
TW377313B (en) 1995-02-27 1999-12-21 Corning Inc The method of making extruded structures
US5681373A (en) 1995-03-13 1997-10-28 Air Products And Chemicals, Inc. Planar solid-state membrane module
DE69629979T2 (en) 1995-06-02 2004-07-29 Corning Inc. Device for removing contaminants from fluid streams
US5759219A (en) 1995-09-22 1998-06-02 Morton International, Inc. Unitary drop-in airbag filters
US5851326A (en) 1995-10-25 1998-12-22 Hexcel Corpation Method for making ceramic honeycomb
EP1382443B1 (en) 1996-01-12 2013-04-24 Ibiden Co., Ltd. A filter for purifying exhaust gas
US5738817A (en) 1996-02-08 1998-04-14 Rutgers, The State University Solid freeform fabrication methods
JPH09217618A (en) 1996-02-09 1997-08-19 Isuzu Ceramics Kenkyusho:Kk Exhaust emission control device
US5948257A (en) 1996-05-03 1999-09-07 Hexcel Corporation Candle filter and method for making
DE69610830T2 (en) 1996-07-22 2001-05-17 Hexcel Corp Honeycomb core materials with particulate reinforcement
US5853439A (en) 1997-06-27 1998-12-29 Donaldson Company, Inc. Aerosol separator and method
US6057030A (en) 1997-07-21 2000-05-02 Kanebo Ltd. Porous ceramic body and kiln furniture made from a porous ceramic body
DE19736560C2 (en) 1997-08-22 2002-01-24 Daimler Chrysler Ag Process for producing a porous body, body made of SiC, and use of the porous body
WO1999017874A1 (en) 1997-10-08 1999-04-15 Corning Incorporated Method of making activated carbon-supported catalysts
NL1007456C2 (en) 1997-11-05 1999-05-07 Tno A method of manufacturing hollow fiber membranes for microfiltration, ultrafiltration or gas separation.
DE19753249B4 (en) 1997-12-01 2005-02-24 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Ceramic network, process for its manufacture and use
DE19805868C2 (en) 1998-02-13 2002-09-12 Daimler Chrysler Ag Process for the production of a fiber composite material
FR2776286B1 (en) 1998-03-20 2000-05-12 Ceramiques Tech Soc D MULTI-CHANNEL POROUS CERAMIC FIBER
US6651773B1 (en) 2002-09-24 2003-11-25 Gregory M. Marocco Exhaust sound attenuation and control system
US6935461B2 (en) 1998-08-18 2005-08-30 Gregory M. Marocco Exhaust sound and emission control systems
US6238618B1 (en) 1998-10-01 2001-05-29 Corning Incorporated Production of porous mullite bodies
DE19860256A1 (en) 1998-12-24 2000-06-29 Krupp Werner & Pfleiderer Gmbh Two-shaft extruder
US6155432A (en) 1999-02-05 2000-12-05 Hitco Carbon Composites, Inc. High performance filters based on inorganic fibers and inorganic fiber whiskers
NO315549B1 (en) 1999-02-19 2003-09-22 Norsk Hydro As A method of producing a dense and crack-free ceramic membrane that selectively transports oxygen when subjected to a gradient oxygen partial pressure
DE19910012C1 (en) 1999-03-08 2001-01-18 Ostthueringische Materialpruef Process for the production of molded articles
US6365092B1 (en) 1999-06-23 2002-04-02 Abb Lummus Global, Inc. Method for producing a sintered porous body
KR100699974B1 (en) 1999-07-02 2007-03-27 엥겔하드 코포레이션 Oxidation catalyst for treating diesel engine exhaust gases
US6306335B1 (en) 1999-08-27 2001-10-23 The Dow Chemical Company Mullite bodies and methods of forming mullite bodies
WO2001016049A1 (en) 1999-09-01 2001-03-08 Corning Incorporated Fabrication of ultra-thinwall cordierite structures
ES2321331T3 (en) 1999-09-29 2009-06-04 Ibiden Co., Ltd. BEE NEST FILTER AND CERAMIC FILTER SET.
US6300263B1 (en) * 1999-12-16 2001-10-09 Corning Incorporated Low-expansion cordierite glass ceramics
US7052532B1 (en) 2000-03-09 2006-05-30 3M Innovative Properties Company High temperature nanofilter, system and method
US6444006B1 (en) 2000-05-18 2002-09-03 Fleetguard, Inc. High temperature composite ceramic filter
US6582490B2 (en) 2000-05-18 2003-06-24 Fleetguard, Inc. Pre-form for exhaust aftertreatment control filter
JP2001327818A (en) * 2000-03-13 2001-11-27 Ngk Insulators Ltd Ceramic filter and filtration device
JP2001252529A (en) 2000-03-13 2001-09-18 Mitsui & Co Ltd Exhaust gas cleaning apparatus and method of manufacturing the same
US6375450B1 (en) 2000-03-17 2002-04-23 Corning Incorporated Extrusion apparatus for ceramic honeycomb articles
US6379446B1 (en) 2000-04-03 2002-04-30 E. Khashoggi Industries, Llc. Methods for dispersing fibers within aqueous compositions
US20010037972A1 (en) 2000-04-04 2001-11-08 Quick Nathaniel R. Fluid separating device
US6743273B2 (en) 2000-09-05 2004-06-01 Donaldson Company, Inc. Polymer, polymer microfiber, polymer nanofiber and applications including filter structures
JP2004510676A (en) 2000-10-02 2004-04-08 コーニング インコーポレイテッド Lithium aluminosilicate ceramic
AU2001295311A1 (en) 2000-10-02 2002-04-15 Indexable Cutting Tools Of Canada Limited "siaion material and cutting tools made thereof"
US20030022247A1 (en) * 2000-10-03 2003-01-30 Masabumi Shibuya Substance which inhibits binding of information transfer molecule for 1175-tyrosine phosphorylated KDR/FLK-1 and usages of the same
CN1186110C (en) 2000-10-24 2005-01-26 邱文亮 Composite for producing macroporous ceramic filter element
US6899777B2 (en) 2001-01-02 2005-05-31 Advanced Ceramics Research, Inc. Continuous fiber reinforced composites and methods, apparatuses, and compositions for making the same
FR2821281B1 (en) 2001-02-28 2003-04-18 Inst Francais Du Petrole SEPARATOR IN POROUS MATERIAL COMPRISING A FELT STRUCTURE AND APPARATUS COMPRISING SUCH A SEPARATOR
EP1383990B1 (en) 2001-02-05 2006-05-17 N.V. Bekaert S.A. Filter element comprising pleated metal fiber fleece
US6991672B2 (en) 2001-02-05 2006-01-31 N.V. Behaert S.A. Filter element comprising pleated metal fiber fleece
US6471394B2 (en) 2001-03-07 2002-10-29 Littleford Day, Incorporated Mixer apparatus and method with improved shaft stub end seal structure
JP4511070B2 (en) 2001-03-29 2010-07-28 日本碍子株式会社 Honeycomb structure and assembly thereof
JP2002292225A (en) 2001-03-30 2002-10-08 Ngk Insulators Ltd Honeycomb structure and its assembly
JP4094823B2 (en) 2001-04-03 2008-06-04 日本碍子株式会社 Honeycomb structure and assembly thereof
DE60211339D1 (en) 2001-06-22 2006-06-14 Argonide Corp SUBMICRON FILTER
CN1553885A (en) * 2001-07-06 2004-12-08 3M Inorganic fiber substrates for exhaust systems and methods of making same
JP3983117B2 (en) 2001-07-31 2007-09-26 日本碍子株式会社 Honeycomb structure and manufacturing method thereof
BR0211833A (en) 2001-08-10 2004-09-21 Ceratech Inc Composite materials and methods for the manufacture and use of such composite materials
JP4367683B2 (en) 2001-10-09 2009-11-18 日本碍子株式会社 Honeycomb filter
US6860917B2 (en) 2001-12-04 2005-03-01 Fleetguard, Inc. Melt-spun ceramic fiber filter and method
EP1479881B1 (en) 2002-02-05 2017-05-10 Ibiden Co., Ltd. Honeycomb filter for exhaust gas decontamination, adhesive, coating material and process for producing honeycomb filter for exhaust gas decontamination
JP3971215B2 (en) 2002-03-13 2007-09-05 日本碍子株式会社 Exhaust gas purification filter
JP4293753B2 (en) 2002-03-19 2009-07-08 日本碍子株式会社 Honeycomb filter
DE10213016B4 (en) 2002-03-22 2006-08-17 Helsa-Automotive Gmbh & Co. Kg Mechanically stable, porous activated carbon moldings, process for its preparation and its use
ATE411095T1 (en) 2002-03-29 2008-10-15 Ibiden Co Ltd CERAMIC FILTER AND EXHAUST GAS DECONTAMINATION UNIT
AU2003279633A1 (en) 2002-06-26 2004-01-19 Corning Incorporated Magnesium aluminum silicate structures for dpf applications
US7278259B2 (en) 2002-08-23 2007-10-09 Donaldson Company, Inc. Apparatus for emissions control, system, and methods
DE50212920D1 (en) 2002-08-30 2008-11-27 Itn Nanovation Ag POWDER PARTICLES
US20040250683A1 (en) 2002-10-18 2004-12-16 Innovative Construction And Building Materials, Llc Advanced filtration devices and methods
US6946013B2 (en) 2002-10-28 2005-09-20 Geo2 Technologies, Inc. Ceramic exhaust filter
US7572311B2 (en) * 2002-10-28 2009-08-11 Geo2 Technologies, Inc. Highly porous mullite particulate filter substrate
JP2004188819A (en) 2002-12-12 2004-07-08 Ngk Insulators Ltd Method for manufacturing honeycomb molded body and honeycomb structure
JP4284588B2 (en) 2003-01-10 2009-06-24 トヨタ自動車株式会社 Exhaust gas purification filter catalyst
JP2004270569A (en) 2003-03-10 2004-09-30 Ngk Insulators Ltd Honeycomb structure
US20040194505A1 (en) 2003-04-01 2004-10-07 Ji Wang Method of making a photonic crystal preform
US7521025B2 (en) 2003-06-10 2009-04-21 Ibiden Co., Ltd. Honeycomb structural body
US7112050B2 (en) 2003-06-26 2006-09-26 Corning Incorporated Extrusion die for making a double-skin honeycomb substrate
DE602004029544D1 (en) * 2003-07-15 2010-11-25 Ibiden Co Ltd Honeycomb structure body
WO2005009614A1 (en) 2003-07-28 2005-02-03 Ngk Insulators, Ltd. Honeycomb structure and method of producing the same
DE10338199B4 (en) 2003-08-20 2006-06-08 Audi Ag Clutch linings made of fiber-reinforced ceramic materials
US7041780B2 (en) 2003-08-26 2006-05-09 General Electric Methods of preparing a polymeric material composite
US7442425B2 (en) 2003-09-30 2008-10-28 Corning Incorporated High porosity honeycomb and method
EP1538134A1 (en) 2003-12-04 2005-06-08 Ceramtec AG Porous Fibre-Ceramic-Composite Material
JP4358662B2 (en) * 2004-03-23 2009-11-04 日本碍子株式会社 Method for producing cordierite honeycomb structure
US7341970B2 (en) 2004-03-31 2008-03-11 Corning Incorporated Low thermal expansion articles
US20070152364A1 (en) 2005-11-16 2007-07-05 Bilal Zuberi Process for extruding a porous substrate
US7510755B2 (en) 2004-04-30 2009-03-31 Ngk Insulators, Ltd. Honeycomb structure and method for producing same
US7422813B2 (en) 2004-06-08 2008-09-09 Microcell Corporation Fuel cell systems comprising microfibrous fuel cell elements and methods of making and using same
KR20080042902A (en) 2004-12-27 2008-05-15 이비덴 가부시키가이샤 Ceramic honeycomb structural body
US20060272306A1 (en) 2005-06-01 2006-12-07 Kirk Brian S Ceramic wall flow filter manufacture
EP1741685B1 (en) 2005-07-05 2014-04-30 MANN+HUMMEL Innenraumfilter GmbH & Co. KG Porous beta-SiC containing shaped ceramic body and method of making it.
KR20080077081A (en) * 2005-08-30 2008-08-21 인더스트리얼 세라믹 솔루션스, 엘엘씨 Multiple integrated-layer ceramic fiber filter paper and method
ATE476396T1 (en) 2005-11-10 2010-08-15 Morgan Crucible Co HIGH TEMPERATURE RESISTANT FIBERS
US8039050B2 (en) 2005-12-21 2011-10-18 Geo2 Technologies, Inc. Method and apparatus for strengthening a porous substrate
JP5485546B2 (en) 2006-03-30 2014-05-07 日本碍子株式会社 Bonded body, honeycomb segment bonded body, and honeycomb structure using the same
US7722705B2 (en) 2006-05-11 2010-05-25 Corning Incorporated Activated carbon honeycomb catalyst beds and methods for the use thereof
US7927682B2 (en) * 2006-06-30 2011-04-19 Corning Incorporated Low-microcracked, porous ceramic honeycombs and methods of manufacturing same
US7964262B2 (en) * 2006-08-29 2011-06-21 Corning Incorporated Layered silicate modified cordierite and method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of EP2265558A4 *

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US7938876B2 (en) 2011-05-10
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WO2009129152A3 (en) 2010-01-21
US20080242530A1 (en) 2008-10-02

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