| Entries |
| Document | Title | Date |
|---|
| 20080199654 | Method for Producing an Annular Honeycomb Body, and Annular Honeycomb Body - A method for producing a honeycomb body includes providing an annular radial partial region with channels through which a fluid can flow. The honeycomb body is formed from at least one metallic layer fastened at least at one fastening point to an outer casing tube. Each metallic layer has alternating substantially smooth and structured sections folded onto one another. A honeycomb body is also provided. The method and the honeycomb body advantageously permit an annular honeycomb body with low material expenditure and good durability to be produced. | 08-21-2008 |
| 20080206514 | Non-Cylindrical Catalytic-Converter Carrier Element and Tool, and Method for Manufacturing it - A method for the production of a converter-carrier body having a metallic honeycomb body made of a plurality of metal layers, especially smooth layers and corrugated layers, the layers having layer ends, such that an outer shape of the honeycomb body is formed by the layer ends. At least one stack is produced having several alternately disposed metal layers that are structured such that channels are formed for a fluid to flow through. The at least one stack is transformed into a honeycomb body having a cylindrical form. The honeycomb body is deformed from the cylindrical form so that an outer shape that deviates from the cylindrical form is produced. Additionally, the invention relates to a corresponding converter-carrier body and a tool for the production thereof. | 08-28-2008 |
| 20080220203 | Cell Structure And Method Of Manufacturing The Same - There is provided a cell structure, where the outer wall portion has high heat-insulating ability, the cell structural portion has a high temperature rise rate, and a temperature distribution is more uniform, and a method for manufacturing the cell structure. The cell structure | 09-11-2008 |
| 20080220204 | DISPLAY PANEL, METHOD OF MANUFACTURING A DISPLAY PANEL, AND DISPLAY UNIT - A display panel includes a sheet having first and second spaced apart surfaces defining a space therebetween and a plurality of partitions extending from the first surface to the second surface and dividing the space into a plurality of cells, wherein the thickness of each partition is in a range of 0.01 to 10 μm. | 09-11-2008 |
| 20080220205 | HONEYCOMB STRUCTURE AND HONEYCOMB CATALYST - A honeycomb structure | 09-11-2008 |
| 20080233345 | Face finished honeycomb structures and methods of manufacturing same - A method for producing a ceramic honeycomb structure comprises providing a honeycomb body having a side surface, a first cut end surface, a second cut end surface opposite the first end surface, and a maximum width (W), and removing material from at least one of the cut end surfaces of the honeycomb body to reduce the length (L), wherein the step of removing material comprises abrasively removing material from at least one of the ends with a rotating abrasive tool, such as by grinding, and wherein L/W is greater than 0.75. The method may achieve end flatness, parallelism, surface roughness and length accuracy, or combinations thereof which heretofore, were unachievable. Face finished ceramic honeycomb structures having low surface roughness (Ra), high degree of parallelism and accurate lengths are also disclosed. | 09-25-2008 |
| 20080233346 | Repair of a composite sandwich structure having a perforated skin - A method of restoring a section of a composite having a honeycomb bonded to a perforated skin includes the steps of separating a first honeycomb from the perforated skin to expose a portion of the perforated skin, inserting pins through perforations in the perforated skin, extending the pins through a repair material, attaching the repair material to the exposed portion of the perforated skin, and attaching a second honeycomb to the repair material. The method may include removing material from the exposed portion of the perforated skin, prior to inserting pins through the perforations, to create a more even bonding surface for attaching the repair material. | 09-25-2008 |
| 20080233347 | Structural Element, Especially Laminated Panel and Process for the Manufacturing of Such Structural Element - The invention relates to a structural element that has a layer containing cells bordered by stiff lamellas ( | 09-25-2008 |
| 20080241465 | CATALYST CARRIER - A catalyst carrier includes a honeycomb structure where cells extending in a longitudinal direction are divided by cell walls; and a coating layer provided at a peripheral part of the honeycomb structure. The honeycomb structure and the coating layer contain at least one of inorganic fibers and whiskers. At least one of the inorganic fiber and whisker contained in the honeycomb structure is oriented mainly in a first direction. At least one of the inorganic fiber and whisker contained in the coating layer is oriented mainly in a second direction. The first direction and the second direction cross at substantially right angles to each other. | 10-02-2008 |
| 20080241466 | METHOD OF PRODUCING HONEYCOMB STRUCTURE AND HONEYCOMB STRUCTURE - A method of producing a honeycomb structure includes a step of forming a ceramic block by bonding a plurality of honeycomb units that have a plurality of cells partitioned by cell walls using a bonding layer, or steps of forming a ceramic block of a single honeycomb unit and providing a coating layer on an outer peripheral portion of the ceramic block. The bonding layer or coating layer is provided as a paste of a bonding material or a coating material including particles of a foaming material having a diameter in a range of approximately 1 μm to approximately 50 μm. The method further includes a step of blowing up the foaming material, and a step of evaporating the foaming material and forming bubble marks having a diameter in a range of approximately 100 μm to approximately 300 μm. | 10-02-2008 |
| 20080241467 | MIXED PARTICLES AND HONEYCOMB STRUCTURE FOR GAS CONVERSION APPARATUS - Mixed particles including noble metal particles of a noble metal, first particles of one or more metal oxides, and second particles of a metal oxide. The first particles of one or more metal oxides are selected from Al | 10-02-2008 |
| 20080241468 | Method of providing marking on a ceramic structure with a chemically reactive ink - A method is provided for marking a ceramic structure by applying a substance, such as an ink, onto a surface of a ceramic-forming green body structure, wherein the substance has an agent that chemically reacts with an ingredient of the green body structure during firing of the green body to produce a contrasting mark on the resulting ceramic structure. An ink containing an agent that chemically reacts with an ingredient of the green body structure is also provided. A ceramic article having a mark that includes a metal-containing compound is also provided. | 10-02-2008 |
| 20080248236 | Cellular Confinement System - The present invention discloses cellular confinement systems (CCSs) with improved friction with infill at low normal pressure. The invention especially presents novel flaps-containing CCS that includes inter alia a plurality of elongated strips arranged in a side by side pattern, each of the strip is segmentally bonded to an adjacent strip in spaced-apart bonding areas, said bonding areas alternating between the sides of each of said strips, such that when the system is stretched across its width, the strips curl to form a web of cells confined by cell walls disposed between the bonding areas, wherein at least one of the cell walls comprises at least one flap hinged to the wall and friction between the walls and the infill material increases. | 10-09-2008 |
| 20080248237 | Honeycomb Material from Thermofusible Material - The invention relates to a honeycomb material. The material is comprised of sections of a thermofusible textile material and the sections are welded together in such a manner as to define cells. | 10-09-2008 |
| 20080248238 | BONDING MATERIAL, PROCESS FOR PRODUCING THE SAME, AND HONEYCOMB STRUCTURE MADE WITH THE SAME - There is provided bonding material having a Young's Modulus after hardening of not less than 20% of articles to be bonded, and an average linear coefficient of thermal expansion after hardening of not more than 70% of the articles to be bonded. This bonding material can suppress deformation of a honeycomb segment due to thermal stress to be generated by a bonding material layer and can suitably be used at the time of manufacturing exhaust gas trapping filters capable of reducing the generation of defects such as a crack, and above all, a diesel particulate filter (DPF) for trapping particulate matter (particulates) in exhaust gas from the diesel engine. | 10-09-2008 |
| 20080254254 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A pillar-shaped honeycomb structure has a plurality of cells longitudinally placed in parallel with one another with a wall portion therebetween, wherein the honeycomb structure mainly includes inorganic fibers which form the honeycomb structure without lamination interfaces. | 10-16-2008 |
| 20080260991 | CATALYST SUPPORTING HONEYCOMB AND METHOD OF MANUFACTURING THE SAME - A catalyst supporting honeycomb including a pillar-shaped honeycomb structure having a plurality of cells formed in parallel with one another in a longitudinal direction with a cell wall interposed therebetween, and catalyst particles supported on the honeycomb structure. The catalyst particles include an oxide catalyst, an average particle diameter of which is at least about 0.05 μm and at most about 1.00 μm. | 10-23-2008 |
| 20080268200 | Methods and apparatus for making honeycomb structures with chamfered after-applied skin and honeycomb structures produced thereby - The present invention provides methods for manufacturing a honeycomb filter having an after-applied skin with chamfered edges formed on the face-ends of the honeycomb filter structure. Apparatus for the manufacture of these honeycomb structures having after-applied skin with chamfered edges are also provided. In addition, honeycomb filter structures with chamfered after-applied skins are provided | 10-30-2008 |
| 20080286522 | Honeycomb having a low coefficient of thermal expansion and articles made from same - This invention relates to a honeycomb and articles made therefrom, the articles having cell walls provided with a structural or matrix resin, the planes of the cell walls being parallel to the Z-dimension of the honeycomb, the honeycomb cell walls comprising 5 to 35 parts by weight thermoplastic material having a melting point of from 120° C. to 350° C. and a coefficient of thermal expansion of 180 ppm/° C. or less; and 65 to 95 parts by weight of a high modulus fiber having a modulus of 525 grams per denier (480 grams per dtex) or greater and having an axial coefficient of thermal expansion of 2 ppm/° C. or less, based on the total amount of thermoplastic and high modulus fiber in the honeycomb cell walls; wherein the honeycomb has a coefficient of thermal expansion in the Z-dimension of 10 ppm/° C. or less as measured by ASTM E831. | 11-20-2008 |
| 20080286523 | HONEYCOMB STRUCTURE AND METHOD OF MANUFACTURING THE HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block formed by bonding a plurality of pillar-shaped honeycomb fired bodies by interposing an adhesive layer therebetween, and a sealing material layer provided on the periphery of the ceramic block. Each of the honeycomb fired bodies has a large number of cells disposed in parallel with one another in a longitudinal direction with a cell wall therebetween. The adhesive layer and the sealing material layer are integrally formed with substantially no interface to divide the two layers. | 11-20-2008 |
| 20080286524 | Method of manufacturing porous product, porous product and honeycomb structure - A sintering aid for promoting sintering of ceramic particles and fine particles that are the same materials as ceramic particles and have smaller average particle diameter are mixed to obtain a puddle. The average particle diameter of ceramic particles is preferably about in a range of 5 to 100 μm; the average particle diameter of the fine particles is preferably about in a range of 0.1 to 1.0 μm, and the average particle diameter of the sintering aid is preferably about in a range of 0.1 to 10 μm. As the sintering aid, for example, alumina is used. This puddle is extrusion molded into a honeycomb shape and the molded object is fired at a firing temperature lower than a temperature for sintering without mixing a sintering aid. The thermal conductivity of the obtained honeycomb structure | 11-20-2008 |
| 20080292841 | Regenerative aramid honeycomb sandwich energy absorbing matrix and square tube supported honeycomb sandwich bridge - The function of the Regenerative Aramid Honeycomb Sandwich Energy Absorbing Matrix and Square
| 11-27-2008 |
| 20080292842 | Carbon Fiber Substrate and Method for Forming the Same - A porous carbon fiber substrate and method of forming the same including providing a fiber material including carbon, providing at least one extrusion aid and providing at least one bonding phase material. The fiber material, the at least one extrusion aid and the at least one bonding phase material are mixed with a fluid. The mixed fiber material, at least one extrusion aid, at least one bonding phase material and fluid are extruded into a green honeycomb substrate. The green honeycomb substrate is fired, enabling bond formation and forming a porous carbon fiber honeycomb substrate. | 11-27-2008 |
| 20080292843 | HONEYCOMB STRUCTURE, METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE AND EXHAUST GAS PURIFYING DEVICE - A honeycomb structure is a pillar-shaped honeycomb structure in which a plurality of cells, separated from each other by a cell wall, are formed in a longitudinal direction. When the honeycomb structure is divided into two portions by a plane in parallel with either one of end faces in the longitudinal direction of the honeycomb structure so that apparent volumes of the respective two portions become equal to each other, the respective two portions have apparent densities different from each other. | 11-27-2008 |
| 20080311340 | HONEYCOMB STRUCTURE AND PRODUCTION METHOD THEREOF - A honeycomb structure excellent in thermal dispersibility upon heating and being protected from damage due to thermal stress, and an efficient method for manufacturing the honeycomb structure. The structure is provided with porous partition walls, functioning as a filtration layer, through which exhaust gas flowing into the cells can flow out, and plugging portions. Additional plugging portions are further disposed in the open end portions to which the plugging portions are not disposed (unplugged open end portions) not so as to plug unplugged open end portions. Each cross-sectional shape of additional plugging portions in a direction perpendicular to the axial direction forms a predetermined pattern shape as a whole, and a barycenter of the pattern shape is located in almost the center of a cross section of a flow of the exhaust gas in a direction perpendicular to the axial direction. | 12-18-2008 |
| 20080317999 | Gas Catalysts Comprising Porous Wall Honeycombs - Embodiments of the invention pertain to a catalyst, which may be used in a catalytic converter for treating a gas stream containing pollutants. In an embodiment, the catalyst comprises a substrate having a plurality of axially enclosed channels defined by the porous wall elements extending between an inlet end and an outlet end. Washcoat particles are disposed substantially within the pores of the walls, and the surfaces of the wall elements have a porous, rough texture after coating with the washcoat and substantially no fillets formed on the channels. | 12-25-2008 |
| 20080318000 | SANDWICH PANEL - There is provided a lightweight sandwich panel of exceptional utility, which satisfies the flexural strength and in-plane shear strength requirements for an inner wall material used in aircraft. The sandwich panel comprises a laminating material in which a plurality of fiber bodies_is laminated, and a surface material, the laminating material and the surface material being laminated in the stated order from the inside to the outside on the upper and lower surfaces of a hollow columnar core. The laminating material comprises at least four unidirectional fiber bodies each of which has fibers aligned in a uniform direction and is laminated so that each of the fiber directions thereof is at approximately 0 , +45°, −45°, and 90°, respectively, in relation to one edge of the sandwich panel. The unidirectional fiber bodies are stitched together using a stitching yarn. | 12-25-2008 |
| 20080318001 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block and a sealing material layer. The ceramic block includes a plurality of honeycomb fired bodies each having a large number of cells longitudinally disposed substantially in parallel with one another with a cell wall between the cells, an adhesive layer for bonding side faces of the honeycomb fired bodies, and a cavity-holding member placed between the side faces of the honeycomb fired bodies. The sealing material layer is formed on a peripheral face of the ceramic block. The cavity-holding member includes a nonflammable material having Young's modulus of at least about 0.001 GPa and at most about 0.07 GPa. | 12-25-2008 |
| 20090004431 | HONEYCOMB STRUCTURAL BODY AND EXHAUST GAS PURIFYING DEVICE - The present invention provides a pillar-shaped honeycomb structural body made of porous ceramics in which a large number of through holes are placed in parallel with one another in the length direction with a wall portion interposed therebetween. Herein, the honeycomb structural body is provided with a sealing material layer which includes inorganic fibers containing at least about 60% and at most about 85% by weight of silica and at least about 15% and at most about 40% by weight of at least one kind of compound selected from the group consisting of an alkali metal compound, an alkali-earth metal compound and a boron compound. | 01-01-2009 |
| 20090011176 | Honeycomb structure and method of manufacturing the same - A tubular honeycomb structure | 01-08-2009 |
| 20090011177 | EXHAUST GAS CLEANING CATALYST AND PROCESS FOR PRODUCING THE SAME - The present invention relates to an exhaust gas cleaning catalyst, and aiming at providing a catalyst which has a higher catalytic activity than that of conventional catalysts and, in particular, a strong ability to oxidize nitrogen monoxide. The present invention relates to an exhaust gas cleaning catalyst whose catalytic component is supported on a carrier, characterized in that the catalytic component is platinum colloid which has an average particle size of 80 nm to 120 nm, a particle size D | 01-08-2009 |
| 20090011178 | HONEYCOMB STRUCTURE AND BONDING MATERIAL TO BE USED FOR SAME - There is disclosed a honeycomb structure | 01-08-2009 |
| 20090011179 | POROUS SILICON CARBIDE AND PROCESS FOR PRODUCING THE SAME - A silicon carbide porous object includes silicon carbide as an aggregate and metal silicon as a binder, the particles of silicon carbide being bonded to one another so as to have pores thereamong. A method for producing a silicon carbide porous object includes: firing raw materials formed by mixing silicon carbide and metal silicon with metal aluminum or an alloy including metal silicon and metal aluminum in an inert gas atmosphere or a reduced-pressure atmosphere to produce a metal aluminum-metal silicon-silicon carbide porous object; and oxidizing and firing the metal aluminum-metal silicon-silicon carbide porous object in an oxygen atmosphere. | 01-08-2009 |
| 20090022941 | SELF-ADHESIVE ELEMENT - The invention relates to self-adhesive elements which can be fastened to the most varied adhesive bodies and can be used for the most varied applications. It is the object of the invention to propose elements which can be fastened in a self-adhesive manner to the different adhesive bodies, with the fastening having to be possible in a detachable manner and a multiple use of the elements being possible. At least one sensor/pickup, an electronic element, an optoelectronic element and/or an actuator are present in a self-adhesive element in accordance with the invention. Elastically deformable pimple-shaped elevated portions are formed at a surface of the element to which an adhesive body can be connected in a self-adhesive and detachable manner. The surface of the pimple-shaped elevated portions is spherically curved at least in the region which is in touching contact with the adhesive body. | 01-22-2009 |
| 20090022942 | HONEYCOMB SEGMENT, HONEYCOMB STRUCTURE AND PROCESS FOR PRODUCING THE SAME - A honeycomb structure which effectively prevents generation of defects such as cracks by thermal stress during use and regeneration and has excellent durability is provided. In a honeycomb structure | 01-22-2009 |
| 20090022943 | BONDED BODY, BONDING MATERIAL COMPOSITION, HONEYCOMB SEGMENT BONDED BODY, AND HONEYCOMB STRUCTURE USING THE SAME - There is provided a bonding material composition capable of suppressing crack generation on an end face of a resultant honeycomb structure to a large extent by reducing anisotropy of Young's modulus after curing of the bonding material by the use of an isotropic filler without using inorganic fibers. The bonded body has two or more members unitarily bonded by means of a bonding material layer, and the relational expression of 0.5| 01-22-2009 | |
| 20090022944 | HONEYCOMB STRUCTURE BODY - In a honeycomb structure | 01-22-2009 |
| 20090029103 | POROUS OBJECT BASED ON SILICON CARBIDE AND PROCESS FOR PRODUCING THE SAME - A silicon carbide-based porous article comprising silicon carbide particles as an aggregate, metallic silicon and an aggregate derived from siliceous inorganic particles to form pores through volume shrinkage by heat treatment, wherein the porosity is 45 to 70%, and the average pore diameter is 10 to 20 μm is provided. Also provided is a method for producing a silicon carbide-based porous article, comprising; adding inorganic particles to form pores through volume shrinkage by heat treatment to a raw-material mixture containing silicon carbide particles and metallic silicon, then forming into an intended shape, calcinating and firing the resultant green body, forming pores through volume shrinkage of the inorganic particles by heat treatment, and the shrunk inorganic particles being present as an aggregate in the porous article. | 01-29-2009 |
| 20090029104 | HONEYCOMB STRUCTURE - A honeycomb structure | 01-29-2009 |
| 20090029105 | HONEYCOMB STRUCTURE AND METHOD FOR PRODUCING SAME - Disclosed is a honeycomb structure which is bonded with a bonding material containing 0.1 to 10 mass % of a layered clay mineral. Also disclosed are a honeycomb structure which is bonded with a bonding material containing 0.1 to 10 mass % of an organic binder, and a honeycomb structure which is bonded with a bonding material having a Casson yield value of 6 Pa or more. Further disclosed is a method for producing such a honeycomb structure. | 01-29-2009 |
| 20090035510 | COMPOSITE STRUCTURE HAVING REINFORCED CORE AND METHOD OF MAKING SAME - A polymer-based composite sandwich includes a core bonded between fiber reinforced resin facesheets. The core includes a truss formed by groups of composite pins held in a low density foam. The pins in each group intersect to form nodes adjacent to one of the facesheets. The ends of the pins extend parallel and are bonded to the facesheets. | 02-05-2009 |
| 20090035511 | Fiber-Based Ceramic Substrate and Method of Fabricating the Same - Low cost aluminosilicate fibers are used to form a ceramic substrate material using inorganic binders that promote the formation of stable compounds that inhibit the formation of crystal silica, or cristobalite, when the substrate is used or exposed to high operating temperatures. The aluminosilicate fibers are mixed with additives including organic and inorganic binders and a fluid to form a plastic mixture. The plastic mixture is formed into a green substrate, and subsequently cured into the ceramic substrate. The fiber-based constituents permit the formation of rigid porous structures for filtration, insulation, and high temperature processes and chemical reactions. | 02-05-2009 |
| 20090035512 | HONEYCOMB STRUCTURE, PROCESS FOR PRODUCING THE SAME, AND BONDING MATERIAL - The present invention provides:
| 02-05-2009 |
| 20090041975 | BONDED ELEMENT, HONEYCOMB SEGMENT BONDED ELEMENT, AND HONEYCOMB STRUCTURE USING THE SAME - There is disclosed a bonded element manufactured from a bonding material composition being capable of contributing to the lowering of thermal expansion of a bonding material layer sufficiently to relax any thermal stress generated in a honeycomb structure and largely inhibiting the cracking of the resultant honeycomb structure as well. In a bonded element in which two or more objects to be bonded are integrated via a bonding material layer, the bonding material layer having a Young's modulus of 20% or less of that of the objects to be bonded and having an average linear thermal expansion coefficient of 70% or less of that of the objects to be bonded, the bonding material layer being prepared from a bonding material composition composed mainly of fillers and a matrix in which fillers having an average linear thermal expansion coefficient of 2.0×10 | 02-12-2009 |
| 20090041976 | High porosity honeycomb and method - A ceramic honeycomb substrate for use in an automotive catalytic converter system which exhibits improved light-off performance by virtue of a high porosity of 45 to 75% while still maintaining a wall thickness of greater than 2.0 mil (0.0020 inch, 0.0508 mm), preferably 2.5 mil (0.0025 in., 0.0635 mm) to 7 mil (0.0070 in., 0.1778 mm), and more preferably 2.5 mil (0.0025 in., 0.0635 mm) to 3 mil (0.0030 in., 0.0762 mm). The median pore size is in the range of 2-10 micrometers, and a coefficient of thermal expansion (CTE) (25-800° C.) of less than 15×10 | 02-12-2009 |
| 20090068395 | EPOXY RESIN COMPOSITION FOR FIBER-REINFORCED COMPOSITE MATERIAL - Provided is an epoxy resin composition for fiber-reinforced composite materials, which serves as a matrix resin composition for use in a self-adhesive prepreg for a face sheet of a honeycomb panel. The epoxy resin composition enables to increase self-adhesiveness of the prepreg, while improving workability and appearance quality of the prepreg. The epoxy resin composition is characterized by containing an epoxy resin (A) which is in a liquid state at room temperature; a thermoplastic resin (B) which dissolves in the epoxy resin (A) at a temperature not less than 90° C.; thermosetting resin particles (C) which do not completely dissolve in the epoxy resin (A) at a temperature less than 90° C. and has a softening point of not less than 120° C.; and a curing agent (D). | 03-12-2009 |
| 20090092786 | Fibrous aluminum titanate substrates and methods of forming the same - A porous fibrous honeycomb substrate having an aluminum titanate composition and methods of producing the same are provided herein. Precursors of aluminum titanate are provided in an extrudable mixture that includes fiber materials to form a green honeycomb substrate. When cured, the precursors of aluminum titanate form an aluminum titanate composition, with the fiber materials defining the porous microstructure. Various composite structures including aluminum titanate are provided to form a porous honeycomb substrate that can be configured to be filtration media and/or a catalytic host. | 04-09-2009 |
| 20090098333 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE HONEYCOMB STRUCTURE - A honeycomb structure includes honeycomb fired bodies having cell walls extending along the longitudinal direction to define a plurality of cells, and an outer wall at the outermost peripheral face. The fired bodies are connected at the outer wall by an adhesive layer. The cell wall has a thickness of at least about 0.15 mm and at most about 0.30 mm. A thickness of a border wall is at least about 5 times greater and at most about 20 times greater than the thickness of the cell wall. The border wall includes the adhesive layer, and first and second outer walls which are connected to each other. The catalyst permeation preventive region is provided in the outer wall or between the outer wall and the adhesive layer. The catalyst permeation preventive region includes at least one of a water repellent material, a cation exchanger and water absorbing material. | 04-16-2009 |
| 20090098334 | CORRUGATED HONEYCOMB CARDBOARD MACHINE - The invention relates to a machine for producing corrugated honeycomb cardboard, the machine comprising a block supplying device for supplying blocks of corrugated cardboard along a direction of conveyance, a cutting device for cutting strips from a block of corrugated cardboard, a gluing device for applying glue to at least one side of the strips, a corrugated-cardboard-strip turning device for changing the spatial orientation of the strips, and a joining device for adhesively joining the strips together to form corrugated honeycomb cardboard. | 04-16-2009 |
| 20090098335 | EPOXY RESIN COMPOSITION FOR FIBER-REINFORCED COMPOSITE MATERIAL - Provided is an epoxy resin composition for fiber-reinforced composite materials, which is improved in toughness necessary for improving the strength of self-adhesion of a matrix resin for use in a prepreg for a face sheet of a honeycomb panel. The epoxy resin composition, which comprises: an epoxy resin (A); a thermoplastic resin (B); fine solid resin particles (C); and a curing agent (D), is characterized in that the epoxy resin composition after being cured has a morphology in which the epoxy resin (A) and the thermoplastic resin (B) form co-continuous phases, and the fine solid resin particles (C) are dispersed in at least the continuous phase of the epoxy resin (A) in the co-continuous phases. | 04-16-2009 |
| 20090110873 | Polymer Hybrid Membrane Structures - Hybrid membrane structures that include: an inorganic porous support that includes first and second ends, and a plurality of inner channels having surfaces defined by porous walls and extending through the support from the first to the second ends; optionally, one or more porous inorganic intermediate layers coating the inner channel surfaces; and a polymeric amine-containing membrane. | 04-30-2009 |
| 20090110874 | Sports Flooring - A flooring, preferentially designed to be used for laying running tracks, includes a treading layer constituted by an elastomer mass and a supporting layer also constituted by an elastomer mass. The supporting layer has, on the side opposite to the treading layer, an array of cavities delimited by ribbings constituting a mesh of uniform ribbings. The cavities are cavities having an elongated shape in the direction of running on the flooring. The cavities occupy a volume equal to at least 28%, and preferentially at least 30%, of the volume of the supporting layer. | 04-30-2009 |
| 20090110875 | Low Thermal Expansion High Strength Honeycomb Cement And Method Therefor - A cement mixture suitable for use with ceramic honeycomb bodies, such as for forming an outer layer on the outer periphery of the honeycomb body, or for forming plugs in the honeycomb body. The cement mixture, when fired, preferably exhibits low coefficient of thermal expansion and high strength. The cement mixture can be applied to a green honeycomb body and simultaneously fired with the green body or can be applied to an already fired ceramic honeycomb body and then fired. Includes cement mixture comprising a plurality of inorganic components comprising talc, kaolin, alumina, silica, and aluminum hydroxide, wherein the mixture contains less than or equal to 18.0% silica and greater than or equal to 17.0% aluminum hydroxide, in percent by weight of the inorganic components. | 04-30-2009 |
| 20090130378 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - A honeycomb structure includes a ceramic block including a plurality of honeycomb fired bodies, a first adhesive layer, and a second adhesive layer. The plurality of honeycomb fired bodies includes center-portion honeycomb fired bodies located at a center portion in a cross-section perpendicular to the longitudinal direction and peripheral honeycomb fired bodies surrounding the center-portion honeycomb fired bodies. The first adhesive layer is interposed between the center-portion honeycomb fired bodies to connect the center-portion honeycomb fired bodies. The second adhesive layer is interposed between each of the center-portion honeycomb fired bodies and each of the peripheral honeycomb fired bodies and between the peripheral honeycomb fired bodies. An adhesive strength α between the center-portion honeycomb fired bodies bonded via the first adhesive layer is higher than an adhesive strength β between honeycomb fired bodies bonded via the second adhesive layer. | 05-21-2009 |
| 20090130379 | EPOXY RESIN COMPOSITION FOR FIBER-REINFORCED COMPOSITE MATERIAL - Provided is an epoxy resin composition for fiber-reinforced composite materials, which serves as a matrix resin for a prepreg. This epoxy resin composition is improved in tackiness stability during storage, while maintaining mechanical characteristics. The epoxy resin composition for fiber-reinforced composite materials is characterized by containing 25 to 50 parts by weight of an amine curing agent (B) selected from aliphatic polyamines, alicyclic polyamines and aromatic polyamines, and 1 to 20 parts by weight of an organic acid dihydrazide compound (C) having a melting point of not less than 150° C., per 100 parts by weight of an epoxy resin (A). | 05-21-2009 |
| 20090130380 | METHOD FOR MANUFACTURING POUROUS STRUCTURE AND METHOD FOR FORMING PATTERN - A pattern forming material contains a block copolymer or graft copolymer and forms a structure having micro polymer phases, in which, with respect to at least two polymer chains among polymer chains constituting the block copolymer or graft copolymer, the ratio between N/(Nc−No) values of monomer units constituting respective polymer chains is 1.4 or more, where N represents total number of atoms in the monomer unit, Nc represents the number of carbon atoms in the monomer unit, No represents the number of oxygen atoms in the monomer unit. | 05-21-2009 |
| 20090136709 | Extruded Porous Substrate having Inorganic Bonds - A method is provided for producing a highly porous substrate. More particularly, the present invention enables fibers, such as organic, inorganic, glass, ceramic, polymer, or metal fibers, to be combined with binders and additives, and extruded, to form a porous substrate. Depending on the selection of the constituents used to form an extrudable mixture, the present invention enables substrate porosities of about 60% to about 90%, and enables process advantages at other porosities, as well. The extrudable mixture may use a wide variety of fibers and additives, and is adaptable to a wide variety of operating environments and applications. Additives can be selected that form inorganic bonds between overlapping fibers in the extruded substrate that provide enhanced strength and performance of the porous substrate in a variety of applications, such as, for example, filtration and as a host for catalytic processes, such as catalytic converters. | 05-28-2009 |
| 20090142539 | Plastic Honeycomb Composite Board with Curved Surface - A plastic honeycomb composite board with curved surface comprises a plastic curved surface plate and a plastic bottom plate. The surface plate joints the bottom plate with edges. At least a honeycomb paper core is positioned between the surface plate and the bottom plate. The board further contains a plastic foam filler in the profile space formed between the plastic curved surface and the honeycomb paper core. The composite board of the invention meets the need of application and overcomes the biased view that a plastic honeycomb composite board cannot have a profile curved surface. | 06-04-2009 |
| 20090142540 | Process for passivating porous ceramic articles and an article made therefrom - A method for passivating a porous ceramic article containing microcracks including filling the microcracks with a liquid, such as water, and then applying a washcoat as described herein. | 06-04-2009 |
| 20090142541 | Methods for applying a washcoat and heat treating a ceramic honeycomb, and treated articles - A method for treating a microcracked, ceramic substrate is provided that obviates the need for filling the microcracks of the substrate via a passivation step prior to sintering a layer of washcoat to the surfaces of the substrate that may either contain a catalyst, or provide a support layer for a catalyst subsequently applied. In the first step of the method, a slurry of particles of a washcoating composition is applied over the surface of the substrate such that particles of the composition are lodged into microcracks of the substrate. Next, the substrate is heat treated to between about 700° C. and 1300° C. The applicants have discovered that such heat treating not only sets the washcoating particles into the substrate, but also causes the microcracks in the substrate to permanently enlarge as a result of the resistance of the lodged particles of washcoating composition against the walls of the microcracks as they attempt to close as a result of thermal expansion of the substrate. The consequent enlargement of the microcracks advantageously reduces both the coefficient of thermal expansion (CTE) and the modulus of elasticity (E | 06-04-2009 |
| 20090142542 | SANDWICH SYSTEM - A composite system comprises a base layer, a capping layer, and at least one core geocell layer. The base layer and capping layer are stacked below and above the core geocell layer, which is infilled with a low quality material. In specific embodiments, the base layer and capping layer are each geocells infilled with a high quality material. This composite system meets engineering specifications economically. | 06-04-2009 |
| 20090142543 | CERAMIC HONEYCOMB STRUCTURE AND METHOD FOR PRODUCING CERAMIC HONEYCOMB STRUCTURE - A ceramic honeycomb structure having porous cell walls defining large numbers of flow paths, the cell walls having porosity of 55-70%, an average pore diameter of 10-40 μm, a concave area ratio CR (projected area ratio of portions lower than an average surface determined from cell wall surface roughness by a least square method) of 0.32-0.6, and an average concave depth H | 06-04-2009 |
| 20090155524 | COMPOSITE PANEL AND METHOD OF MANUFACTURING THE SAME - A method of manufacturing a composite panel is described. The method includes pre-stabilizing a honeycomb core with at least one layer of a pre-stabilizing material, surrounding the honeycomb core with at least one composite laminate skin layer, and curing the at least one composite laminate skin layer. | 06-18-2009 |
| 20090155525 | Passivation-Free Coating Process For A CSF - An emission treatment system and method for simultaneously remediating the nitrogen oxides (NOx), particulate matter, and gaseous hydrocarbons present in diesel engine exhaust streams. The emission treatment system includes a catalyzed soot filter comprising a wall flow monolith and a catalyst comprising support particles. The wall flow monolith may be washcoated with a slurry comprising catalytic support particles without applying a passivation layer to the wall flow monolith. | 06-18-2009 |
| 20090155526 | HONEYCOMB HAVING A HIGH COMPRESSION STRENGTH AND ARTICLES MADE FROM SAME - High compression strength honeycomb is made from polymer paper containing 5 to 35 parts by volume solid material and 65 to 95 parts by volume voids having a normalized peak load at bend equal or greater than 0.33 mgf/(g/m2)̂3 and a Gurley air resistance equal or greater than 50 seconds/100 ml | 06-18-2009 |
| 20090155527 | SILICON CARBIDE-BASED POROUS BODY - A silicon carbide-based porous body comprising a plurality of silicon carbide (SiC) particles as an aggregate and a binder which binds the silicon carbide particles to each other, wherein
| 06-18-2009 |
| 20090155528 | SILICON CARBIDE-BASED POROUS BODY - There is provided a silicon carbide-based porous body which can avoid excessive temperature elevation when it is used as a filter and the captured particulate matter (PM) is burnt for removal and which is low in strength reduction caused by heat cycle. The silicon carbide-based porous body comprises a plurality of silicon carbide (SiC) particles as an aggregate and a plurality of binding phases which bind the silicon carbide particles to each other, wherein
| 06-18-2009 |
| 20090162605 | Papers containing floc derived from diamino diphenyl sulfone - This invention relates to papers made with floc containing a polymer or copolymer derived from a monomer selected from the group consisting of 4,4′diaminodiphenyl sulfone, 3,3′diaminodiphenyl sulfone, and mixtures thereof. Such papers have higher elongation-at-break and work-to-break (toughness) properties and exhibit less shrinkage at high temperatures than papers made with solely with poly (metaphenylene isophthalamide) floc. | 06-25-2009 |
| 20090169805 | POROUS FIRED BODY AND MANUFACTURING METHOD THEREOF - A porous fired body including a structure that aggregates are bonded by a bonding material, wherein the aggregates include oxide particles having a larger thermal capacity per unit volume than an SiC particle and SiC, the bonding material includes metallic Si, volume ratio of the metallic Si in the whole porous fired body is between 8 and 43% by volume, volume ratio of the particles of the oxide in the whole aggregates is between 14 and 55% by volume, the SiC particles and the oxide particles respectively include one or more particle groups, and an average particle size of each particle group is within a range of between 5 and 100 μm. | 07-02-2009 |
| 20090176053 | HONEYCOMB STRUCTURE, HONEYCOMB CATALYTIC BODY AND MANUFACTURING METHOD OF THE SAME - There are disclosed a honeycomb structure capable of providing a honeycomb catalytic body which is excellent in purification efficiency with a small pressure loss and which can be mounted even in a limited space, a honeycomb catalytic body which is excellent in purification efficiency with a small pressure loss and which can be mounted even in a limited space, and a manufacturing method of the same. A honeycomb catalytic body | 07-09-2009 |
| 20090186187 | PHOTOSENSITIVE PASTE COMPOSITION, BARRIER RIBS PREPARED USING THE COMPOSITION AND PLASMA DISPLAY PANEL COMPRISING THE BARRIER RIBS - A photosensitive paste composition includes: a fluoride sol dispersed in an organic material; and an inorganic material, wherein an average refractive index of the fluoride sol N | 07-23-2009 |
| 20090186188 | HONEYCOMB SEGMENT WITH SPACER AND HONEYCOMB STRUCTURE - A honeycomb segment | 07-23-2009 |
| 20090191378 | HONEYCOMB STRUCTURE - A honeycomb structure includes a plurality of honeycomb fired bodies and an adhesive layer. The plurality of honeycomb fired body has a longitudinal direction and a plurality of cell walls extending along the longitudinal direction to define a plurality of cells. The adhesive layer is provided between the plurality of honeycomb fired bodies to connect the honeycomb fired bodies. Pore diameters of pores in the adhesive layer are about 300 μm or less. A ratio of a total area of pores having a pore diameter of at least about 50 μm and at most about 300 μm and an aspect ratio of at least about 1 and at most about 1.5 in a cross-section perpendicular to the longitudinal direction to a total area of pores having a pore diameter of at least about 50 μm and at most about 300 μm is about 90% or more. | 07-30-2009 |
| 20090202779 | Honeycomb structure and seal material - A honeycomb structure is formed by adhering a plurality of honeycomb units provided with cells to each other through a layer of a seal material layer, in which the layer of the seal material comprises an inorganic binder and oxide particles having a particle size of about 0.01 to about 100 μm. | 08-13-2009 |
| 20090208700 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A honeycomb structure includes periphery honeycomb fired bodies which include at least a single piece of a periphery small honeycomb fired body having in the cross-section a cross-sectional area which is less than about 60% of a cross-sectional area of a single piece of the center-portion honeycomb fired body. A cross-sectional area of a periphery honeycomb bonded body in the cross-section is about 60% or more of the cross-sectional area of a single piece of the center-portion honeycomb fired body. The second adhesive layer is provided between the periphery small honeycomb fired body and the at least one piece of the honeycomb fired body. The second adhesive layer has thermal conductivity higher than thermal conductivity of a first adhesive layer. The second adhesive layer has Young's modulus higher than Young's modulus of the first adhesive layer. The center-portion honeycomb fired bodies are bonded together with the first adhesive layer. | 08-20-2009 |
| 20090214817 | Panel for Furniture or the Like - The present invention refers to a panel for furniture or the like, comprising a support bearing sheet, an intermediate layer of superimposed filling material, with in between a first adhesive layer, on one surface of the bearing sheet, and a superimposed covering board, with in between a second adhesive layer, on the surface of the intermediate layer opposite the bearing sheet, the bearing sheet having a thickness greater than that of the covering board and being able to fasten anchoring means to the structure of a piece of furniture. | 08-27-2009 |
| 20090214818 | CORE HAVING A HIGH SHEAR STRENGTH AND ARTICLES MADE FROM SAME - This invention relates to a honeycomb core having improved shear properties made from a p-aramid paper substrate. The paper comprises 50-85 parts by weight of p-aramid floc, 10-40 parts by weight of p-aramid pulp and 5-30 parts by weight of aramid fibrids. Prior to impregnation with resin, the paper has a Gurley air resistance of from 3 to 40 seconds per 100 milliliters. | 08-27-2009 |
| 20090214819 | CERAMIC KNEADED CLAY AND USAGE THEREOF - An oxide-ceramic forming clay comprising an oxide-ceramic forming material, a layered double hydroxide, a pore-forming agent, and water, wherein the amount of the pore-forming agent is between 3 and 50 parts by mass by superaddition to 100 parts by mass of a sum of the oxide-ceramic forming material and the layered double hydroxide and a sum of the pore-forming agent and an organic binder is between 5 and 55 parts by mass also by superaddition which has environment-friendly characteristics in a forming firing step, and usage thereof. | 08-27-2009 |
| 20090220733 | Dispersion-toughened cordierite for filter and substrate applications - A porous ceramic substrate includes a first phase of microcracked cordierite ceramic material and a second phase of non-cordierite metal oxide particles dispersed in the cordierite ceramic, wherein at least a portion of the interface between the first and second phases is wetted by glass and the particles of the second phase have a size in the range of from about 0.1 to about 10 μm. A method for toughening a porous microcracked cordierite ceramic includes the steps of providing a cordierite batch composition; adding to the cordierite batch composition at least one non-cordierite forming metal oxide or metal oxide precursor; mixing the batch composition with a pore former, binder, and water into a paste; shaping the paste into a green body; firing the green body; and annealing the fired green body at a temperature below the firing temperature to form a toughened cordierite ceramic honeycomb having a second phase of crystallized non-cordierite particles dispersed within the cordierite ceramic, wherein at least a portion of the interface between the first and second phases is wetted by glass. | 09-03-2009 |
| 20090220734 | Anisotropic Porous Ceramic Article And Manufacture Thereof - An aluminum titanate-based ceramic is provided having an anisotropic microstructure which includes the reaction products of a plurality of ceramic-forming precursors. The batch contains at least one precursor in fibrous form. The inorganic ceramic has low thermal expansion. Porous ceramic bodies and the method of manufacture are also provided. | 09-03-2009 |
| 20090220735 | SEALING MATERIAL FOR HONEYCOMB STRUCTURE, HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A sealing material for a honeycomb structure includes inorganic fibers, oxide sol, and inorganic particles. The inorganic fibers include at least one of an alkali metal compound, an alkaline earth metal compound and a boron compound. The sealing material has a pH of at least about 4 and at most about 6. | 09-03-2009 |
| 20090220736 | Stabilized Low-Microcracked Ceramic Honeycombs And Methods Thereof - Disclosed are high-porosity cordierite honeycomb substrates having a narrow pore size distribution, little or no microcracking, and high thermal shock resistance. The porous ceramic honeycomb substrates generally comprise a primary cordierite ceramic phase as defined herein. Also disclosed are methods for making and using the cordierite substrates. | 09-03-2009 |
| 20090239028 | HONEYCOMB STRUCTURE - A honeycomb structure includes a plurality of honeycomb fired bodies each having cells. The honeycomb fired bodies include a center-portion honeycomb fired body and a peripheral-portion honeycomb fired body. An area of the center-portion honeycomb fired body is at least about 900 mm | 09-24-2009 |
| 20090239029 | HONEYCOMB STRUCTURE - Provided is a honeycomb structure that is divided by a porous partition wall | 09-24-2009 |
| 20090239030 | CEMENT TO MAKE THERMAL SHOCK RESISTANT CERAMIC HONEYCOMB STRUCTURES AND METHOD TO MAKE THEM - A ceramic honeycomb structure comprised of at least two separate smaller ceramic honeycombs that have been adhered together by a cement comprised of inorganic fibers and a binding phase wherein the smaller honeycombs and fibers are bonded together by the binding phase which is comprised of an amorphous silicate, aluminate or alumino-silicate glass and the cement has at most about 5% by volume of other inorganic particles. The cement may be made in the absence of other inorganic and organic additives while achieving a shear thinning cement, for example, by mixing oppositely charged inorganic binders in water together so as to make a useful cement for applying to the smaller honeycombs to be cemented. | 09-24-2009 |
| 20090239031 | PLUGGED HONEYCOMB STRUCTURE - There is provided a honeycomb structure including: porous partition walls separating and forming a plurality of cells extending between two end faces, and an outer peripheral wall formed unitarily with the partition walls. The cells include outermost peripheral portion partial cells each locating in an outermost peripheral portion of the honeycomb structure and having an incomplete cell cross section, a part of which is brought into contact with the outer peripheral wall, and complete cells each having a complete cell cross section other than the outermost peripheral portion partial cells. The complete cells and the outermost peripheral portion partial cells having plugging portions formed on one end portion so that an entire end face of the honeycomb structure shows a checkerwise plugging pattern, and the depth of the plugging portions in the outermost peripheral partial cells is smaller than that of the plugging portions in the complete cells. | 09-24-2009 |
| 20090246450 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit having a first end face and a second end face. The at least one honeycomb unit includes an inorganic binder, inorganic particles, and cell walls extending from the first end face to the second end face to define a plurality of cells. The inorganic particles include ceria particles doped with zirconia. A percentage by weight of zirconia doped in ceria in the ceria particles is in a range of about 20% to about 50%. | 10-01-2009 |
| 20090246451 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit and coating layers. The at least one honeycomb unit includes a first SOx-occluding agent, first inorganic particles, an inorganic binder, and partition walls extending along the longitudinal direction of the at least one honeycomb unit to define parallel through holes. The coating layers are formed on the partition walls. A basicity of the at least one honeycomb unit is higher than a basicity of the coating layers. The coating layers include a second SOx-occluding agent and second inorganic particles. | 10-01-2009 |
| 20090246452 | MANUFACTURING METHOD OF HONEYCOMB STRUCTURE - A manufacturing method of a honeycomb structure that can improve a manufacturing efficiency and a raw material yield is provided. There is provided a manufacturing method of a honeycomb structure comprising: subjecting a raw material to extrusion forming to form a honeycomb formed body | 10-01-2009 |
| 20090246453 | HONEYCOMB STRUCTURE - A honeycomb structure includes: a porous substrate having porous partition walls separating and forming a plurality of cells functioning as fluid passages, a porous coat layer disposed on a surface of the partition walls to inhibit microparticles from entering, a surface of the coat layer having an uneven shape to increase a surface area, and plugging portions for plugging cells so that a fluid flowing into the structure from an opening portions on one end side of predetermined cells may pass through the partition walls and flows out from opening portions on the other side of the other cells to allow the gas to flow through the partition walls and the coat layers. The honeycomb structure can inhibit the pressure loss from increasing upon trapping particulate matter in exhaust gas and can effectively combust and remove the trapped particulate matter. | 10-01-2009 |
| 20090246454 | HONEYCOMB STRUCTURE - A precise exhaust gas control can be achieved without being influenced by fluctuations of the excess air ratio (λ) between cylinders of engines or the size of the diameter (the sectional area) of the honeycomb structure. The honeycomb structure is formed by a plurality of cells separated from one another by porous partition walls and functioning as fluid flow paths, the honeycomb structure includes: a sensor plug-in hole | 10-01-2009 |
| 20090246455 | HONEYCOMB STRUCTURE - The honeycomb structure comprising a plurality of columnar honeycomb segments in which two kinds of plural through-holes different in end face area are formed side by side by being surrounded by partition walls, each honeycomb segment having, at one end face, an inlet side of high opening ratio, wherein through-holes of smaller end face area are plugged and, at other end face, an outlet side of low opening ratio and wherein through-holes of larger end face area are plugged, the plurality of honeycomb segments being bonded to each other via a bonding material in the longitudinal direction of each honeycomb segment. The bonded width of the bonding material is larger at the inlet side end face of the honeycomb structure than at the outlet side end face is presented. | 10-01-2009 |
| 20090252918 | SANDWICH MATERIAL - The invention relates to a sandwich material comprising two top layers and a core material, wherein the core material is built up from a sandwich material consisting of layers of thermoplastic honeycomb material which are connected to each other by means of fiber reinforced plastic layers and wherein said plastic layers are at right angles relative to said top layers, and to a method for manufacturing such sandwich material. | 10-08-2009 |
| 20090252919 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - A honeycomb structure | 10-08-2009 |
| 20090252920 | COMPOSITE PANELS HAVING IMPROVED FLUID IMPERMEABILITY - A prepreg composite material that includes a fiber layer and a resin comprising a thermoset resin component, a curing agent and a fibrous micropulp. The micropulp component is an aramid fiber having a volume average length of from 0.01 to 100 micrometers. The prepreg is useful in composite panel construction for minimizing fluid permeation into the cured structure. This prepreg is particularly suitable for making honeycomb sandwich panels. Film adhesives, liquid and paste resins containing aramid fiber micropulp are also disclosed. | 10-08-2009 |
| 20090252921 | METHOD FOR THE PRODUCTION OF A SANDWICH COMPONENT HAVING A HONEYCOMB CORE AND THE SANDWICH COMPONENT OBTAINED IN THIS WAY - The invention relates to a method for the production of a fiber reinforced sandwich component ( | 10-08-2009 |
| 20090252922 | ANTIMICROBIAL FLUOROPOLYMER FILM, LAMINATES AND ARTICLES AND PROCESS FOR MAKING THEREOF - Films, laminates and articles comprising a fluoropolymer that contains amino-reactive functional groups only after activation are made antimicrobial by activating the fluoropolymer surface and then contacting the activated surface with a solution comprising chitosan. Films, laminates and articles comprising activated fluoropolymers and contacted with a solution comprising chitosan. | 10-08-2009 |
| 20090258185 | Metallic doubler for repair of a gas turbine engine part - A method and system of repairing an engine part having a cracked metal skin bonded to a honeycomb core includes removing a portion of the honeycomb that corresponds to a cracked portion of the metal skin. A crack in the metal skin originates from an edge of the engine part. A portion of the honeycomb is removed to form a slot in the honeycomb beginning at the edge of the part. A doubler is inserted into the slot in the honeycomb and is attached to an underside of the metal skin to form a lap joint between the doubler and the metal skin. In one embodiment, the portion of the metal skin that includes the crack remains. In an alternative embodiment, the cracked portion of the metal skin is removed and a metal patch is attached to the doubler such that the patch replaces the removed metal skin. | 10-15-2009 |
| 20090263620 | COMPOSITE BOARD WITH OPEN HONEYCOMB STRUCTURE - A reinforcing core structure for a composite panel includes a body having a plurality of generally parallel, alternating ridges and grooves, in which walls extending between the ridges and grooves have a corrugated surface. The resulting core structure has an open honeycomb geometry that may be employed in various applications to provide a composite panel exhibiting an exceptional strength to weight ratio. In accordance with certain preferred embodiments, the panels may comprise reinforcing core structures fabricated from fibrous bodies containing a binder material to provide inexpensive structural members exhibiting excellent mechanical properties. | 10-22-2009 |
| 20090263621 | POROUS ORGANIC-INORGANIC HYBRID MATERIALS AND ADSORBENT COMPRISING THE SAME - The present invention relates to an adsorbent using the porous organic-inorganic hybrid material(s) containing iron having a large surface area and a high pore volume, in particular, a water adsorbent. Also, it relates to an adsorbent that can be used in humidifiers, dehumidifiers, coolers/heaters, a refrigerating machine or an air conditioner, etc., which can easily absorb or desorb at 100° C. and below, and has a great adsorption amount per weight of the adsorbent. | 10-22-2009 |
| 20090263622 | REPAIR OF COMPOSITE SANDWICH STRUCTURES WITH UNEVEN BOND SURFACES - A method of restoring a section of a component having a honeycomb bonded to a skin includes the steps of separating a first honeycomb from the skin, wherein the honeycomb includes an uneven surface. At least a portion of the uneven surface is removed to form a bonding surface on the skin. A conformable layer is bonded to the uneven surface. Then a replacement honeycomb is then bonded to the conformable layer. | 10-22-2009 |
| 20090269547 | REPAIR OF HONEYCOMB STRUCTURES - A process for the repair of a honeycomb structure which comprises a honeycomb bonded to at least one surface layer wherein a replacement for a damaged piece of the structure is bonded to the honeycomb structure by means of a foamable adhesive material. | 10-29-2009 |
| 20090274866 | CERAMIC ARTICLE AND METHOD FOR MAKING IT - Extruded ceramic bodies such as extruded honeycomb bodies formed of plasticized ceramic powder pastes made from paste batches comprising one or a combination of ceramic powders together with a water vehicle and a cellulose ether binder, wherein a high-molecular-weight polymeric dispersant is incorporated in the batches to reduce batch mixing torque and extrusion pressure while maintaining the stiffness and mechanical durability of the extrusions. | 11-05-2009 |
| 20090286040 | Impact Resistant Core - Impact resistant cores and methods of manufacturing such impact resistant cores are provided. Additionally, components made using the impact resistant cores are provided. A particular impact resistant core includes a composite structure of at least one non-woven sheet including poly p-phenylene-2,6-benzobisoxazole fiber and a binding resin. | 11-19-2009 |
| 20090286041 | Cement Compositions For Applying To Honeycomb Bodies - Disclosed are cement compositions for applying to honeycomb bodies as a plugging cement composition, segment cement, or even as an after-applied artificial skin or coating. The cement compositions generally comprise an inorganic powder batch mixture; an organic binder; a liquid vehicle; and a gelled inorganic binder. Also disclosed are honeycomb bodies having the disclosed cement compositions applied thereto, and methods for making same. | 11-19-2009 |
| 20090286042 | HONEYCOMB SEGMENT - A honeycomb segment containing outer walls and porous partition walls disposed inside the outer walls has a structure where first cells each open in one end portion on one side and plugged in the other end portion on the other side and second cells each plugged in one end portion on one side and open in the other end portion on the other side are alternately disposed, a cross-sectional area of the first cells in a cross section cut along a plane perpendicular to a longitudinal direction of the cells is larger than that of the second cells, and the first cells and the second cells are alternately disposed in a first direction and in a second direction perpendicular to the first direction in the cross section, and the outer walls are linearly formed so as to have a uniform thickness except for corner portions. | 11-19-2009 |
| 20090291252 | HONEYCOMB STRUCTURE AND MANUFACTURING METHOD OF THE HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit having opening ratio (P) of at least approximately 50% and at most approximately 65% and a cell density ρ of at least approximately 31/cm | 11-26-2009 |
| 20090291253 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit. The at least one honeycomb unit has a longitudinal direction and includes zeolite and an inorganic binder. A content of the zeolite per apparent unit volume of the at least one honeycomb unit is about 230 g/L or greater. The at least one honeycomb includes plural cell walls extending from one end face to another end face along the longitudinal direction to define plural cell walls. A porosity of substantially all pores in the cell walls is about 40% or less. A porosity of pores having diameters in a range of about 0.005 μm through about 0.02 μm in the cell walls is about 5% or greater. A porosity of pores having diameters in a range of about 0.05 μm through about 0.2 μm in the cell walls is about 17.5% or greater. | 11-26-2009 |
| 20090291254 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit. The at least one honeycomb unit has a longitudinal direction and includes plural cell walls extending from one end face to another end face along the longitudinal direction to define plural cells. The at least one honeycomb unit includes inorganic particles, an inorganic binder, and inorganic fibers. A degree of orientation of the inorganic fibers in an a-axis direction parallel to the longitudinal direction is about 0.5 or less. | 11-26-2009 |
| 20090291255 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit. The at least one honeycomb unit has cell walls extending from one end face to another end face of the at least one honeycomb unit along a longitudinal direction of the at least one honeycomb unit to define cells. The at least one honeycomb unit includes zeolite, inorganic particles, and inorganic binder. The zeolite includes a hydroxyl group. The inorganic particles includes a hydroxyl group. A hydroxyl group content in the inorganic particles is greater than a hydroxyl group content in the zeolite. | 11-26-2009 |
| 20090297762 | Flow-Through Sorbent Comprising A Metal Sulfide - A flow-through sorbent comprising at least 30 wt % of a metal sulfide, and a binder. The sorbent may be used, for example, for the removal of a contaminant, such as mercury, from a fluid stream. | 12-03-2009 |
| 20090297763 | COMPOSITE PANEL - A door panel | 12-03-2009 |
| 20090297764 | Stablized Low-Microcracked Ceramic Honeycombs And Methods Thereof - Disclosed are stabilized, high-porosity cordierite honeycomb substrates having little or no microcracking, and a high thermal shock resistance. The porous ceramic honeycomb substrates generally comprise a primary cordierite ceramic phase as defined herein. Also disclosed are methods for making and using the cordierite substrates. | 12-03-2009 |
| 20090297765 | Method Of Applying A Cement Mixture To A Honeycomb Body - A method of applying a cement mixture to an exposed matrix of intersecting walls of a honeycomb body is disclosed. The method may include the steps of providing an applicator, feeding the cement mixture into applicator, forcing the cement mixture to exit the applicator with a substantially uniform velocity, while depositing the cement mixture on the exposed matrix of the honeycomb body. | 12-03-2009 |
| 20090297766 | HONEYCOMB FILTER - A honeycomb segment has two kinds of cells having different cross-sectional areas in a cross-section cut along a plane perpendicular to the longitudinal direction of the segnent. When the cells are cut along a plane perpendicular to the longitudinal direction of the cells, each cross-sectional area of first cells (large cells) is larger than that of second cells (small cells). The first cells are formed into an octagon where corners are cut off or into a square having circular arc corners. The second cells are formed into a square. The thickness of a 1-1 wall between the adjacent first cells is larger than that of a 1-2 wall between each first cell and each second cell adjacent to the first cell. | 12-03-2009 |
| 20090304987 | METHOD AND APPARATUS FOR MANUFACTURING THERMOFORMED COMPONENTS COMPRISING A CORE BETWEEN CONTINUOUS FILMS - Method and apparatus are described for making e.g. panels by thermoforming outer films ( | 12-10-2009 |
| 20090304988 | HONEYCOMB STRUCTURE - A honeycomb structure has a plurality of honeycomb segments each including porous partition walls that define a plurality of cells communicating with two end surfaces and an outer wall that surrounds the partition walls. The honeycomb segments are combined in a direction perpendicular to the axial directions of the honeycomb segments, and the outer walls of the honeycomb segments are integrally joined by a joint material. The outer wall of each honeycomb segment has corners. A cell in contact with the inner surface of a portion of the outer wall having one of the corners is defined by a plurality of sides including two sides formed by the inner surface and two sides each having one end in contact with the inner surface. An angle θa of the corner formed by the two sides each having the one end in contact with the inner surface is 100 to 150°. | 12-10-2009 |
| 20090311468 | HEATSHIELD USING ABLATIVE MATERIAL AND METHOD OF MAKING SAME - A method of forming a heat shield that involves thermally stabilizing a plurality of phenolic microspheres; mixing the thermally stabilized phenolic microspheres with a phenolic resin to form a phenolic ablative material; compressing the phenolic ablative material into a honeycomb core; and allowing the phenolic ablative material to cure. | 12-17-2009 |
| 20090311469 | Composite Plate and Method of Draining a Composite Plate - The present invention concerns a composite plate ( | 12-17-2009 |
| 20090311470 | DIE FOR EXTRUSION FORMING OF HONEYCOMB FORMED BODY, METHOD OF FORMING HONEYCOMB FORMED BODY, AND HONEYCOMB FORMED BODY - Provided is a die for extrusion forming for extrusion forming of a honeycomb formed body comprising a honeycomb forming die having a structure that there is provided at a surface a groove-like slit in a form of a cell block as well as there is provided at a backside a clay introduction hole in communication with the slit, and a frame-shaped presser plate that is disposed at an outer peripheral portion of the honeycomb forming die and that regulates a shape and dimension of a honeycomb formed body. Among the cell blocks, in an extrusion direction of forming clay, a cell block which end face is positioned to be overlapped with an inner circumferential surface of the presser plate is formed to be shorter than the other cell blocks resided inside the inner circumferential surface of the presser plate. | 12-17-2009 |
| 20100003453 | HONEYCOMB STRUCTURE - A honeycomb structure includes: a periphery-ground article obtained by grinding an outer peripheral portion of a cell structure | 01-07-2010 |
| 20100003454 | HONEYCOMB STRUCTURE - A honeycomb structure 1 includes: a periphery-ground article obtained by grinding an outer peripheral portion of a cell structure 3 where a plurality of honeycomb segments 11 are bonded by means of a bonding layer 12 at an outer wall 10 of each of them, and an outer peripheral coat layer 9 disposed on an outer peripheral face 8 of the periphery-ground article; wherein at least one of the bonding layer 12 and the outer peripheral coat layer 9 is formed by the use of honeycomb-forming slurry containing: biologically soluble fibers containing a metal oxide capable of extricating a metal ion, an inorganic binder containing a colloidal oxide having silica sol, and a chelate compound capable of multi-coordinating with the metal ion or an additive containing a first buffer solution or acid. | 01-07-2010 |
| 20100009117 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A ceramic honeycomb structure comprising a ceramic honeycomb body having cell walls defined by a large number of longitudinally extending cells, and an outer peripheral wall formed on an outer peripheral surface of the ceramic honeycomb body, the outer peripheral wall being formed by coating longitudinally extending grooves defined by cell walls on the outer peripheral surface of the ceramic honeycomb body with a coating material, and the outer peripheral wall having higher hardness in its outer peripheral portion than in its inside portion in a thickness direction. | 01-14-2010 |
| 20100015392 | SYSTEM AND METHOD FOR FORMING PLASTIC PALLETS - A preformed pallet is provided having first and second outer layers that sandwich a cellular or honeycomb shaped core. The peripheral edge of the preformed pallet may be inserted into the molding device having one or more heating elements, which function to focus heat onto the peripheral edge. Once heated, the peripheral edge of the preformed pallet may be reshaped by one or more die sets forming the peripheral edge into an enclosed pallet. | 01-21-2010 |
| 20100021683 | FLEXIBLE HEATED PLANAR ELEMENT - A double-sidedly self-adhesive planar element which is intrinsically heatable in a self-regulating way and at the same time has a particularly high flexibility. The planar element has a layer sequence of a posistor heating layer, a contacting layer and an adhesive layer, the contacting layer being a two-dimensional perforate contacting element which within the planar element is therefore present as a contacting element which has not been applied to a backing. Also disclosed is an adhesively bonded assembly of a bonding substrate and a planar element of the aforesaid kind, a method of producing a planar element of the aforesaid kind, and a method of using a planar element of the aforesaid kind for heating an adhesively bonded assembly. | 01-28-2010 |
| 20100035018 | Sandwich panel - A sandwich panel that has excellent practicality as an inner wall material used in aircraft, for example, whereby the abovementioned requirements of flexural strength, peel strength, and in-plane shear strength can be satisfied while having reduced weight. A sandwich panel in which a middle material | 02-11-2010 |
| 20100035019 | Carbon microtubes - A carbon microtube comprising a hollow, substantially tubular structure having a porous wall, wherein the microtube has a diameter of from about 10 μm to about 150 μm, and a density of less than 20 mg/cm | 02-11-2010 |
| 20100035020 | HONEYCOMB STRUCTURE - Disclosed is a honeycomb structure capable of preventing the generation of cracks in buffer portions and preventing the honeycomb structure from being divided when an operation (regeneration) of burning collected particulate matters is repeated. A honeycomb structure | 02-11-2010 |
| 20100040828 | Latch cover - A lightweight, strong article of manufacture wherein the surfaces are fabricated of an adhesive-impregnated fiber fabric having the desired properties; and where additional stiffness is required, a honeycomb material is sandwiched between the surfaces, greatly increasing the rigidity with only a slight increase in weight. | 02-18-2010 |
| 20100047515 | Honeycomb Core Having a High Compression Strength and Articles Made from the Same - This invention is directed to a honeycomb core structure having a high compression modulus. The core structure comprises (a) a plurality of interconnected walls having surfaces which define a plurality of honeycomb cells, wherein the cell walls are formed from a nonwoven sheet and (b) a cured resin in an amount such that the weight of cured resin as a percentage of combined weight of cured resin and nonwoven sheet is at least 62 percent. The nonwoven sheet further comprises fibers having a modulus of at least 200 grams per denier (180 grams per dtex) and a tenacity of at least 10 grams per denier (9 grams per dtex) wherein, prior to impregnating with the resin, the nonwoven sheet has an apparent density calculated from the equation Dp=K×((dr×(100−% r)/% r)/(1+dr/ds×(100−% r)/% r), where Dp is the apparent density of the sheet before impregnation, dr is the density of cured resin, ds is the density of solid material in the sheet before impregnation, % r is the cured resin content in the final core structure in weight %, K is a number with a value from 1.0 to 1.5. Further, the Gurley porosity of the nonwoven sheet before impregnation with the resin is no greater than 30 seconds per 100 milliliters. The invention is also directed to composite structures incorporating such folded core. | 02-25-2010 |
| 20100055386 | HONEYCOMB STRUCTURE - A honeycomb structure includes at least one honeycomb unit. The at least one honeycomb unit has a longitudinal direction and includes an inorganic binder, a cell wall, and xeolite. The cell wall extends from a first end face to a second end face of the at least one honeycomb unit along the longitudinal direction to define cells. The at least one honeycomb unit includes the zeolite in an amount exceeding approximately 250 g/L per apparent volume. The xeolite is present at a first concentration at a center part of a thickness of the cell wall and at a second concentration at a surface of the cell wall. The second concentration is larger than the first concentration. | 03-04-2010 |
| 20100062211 | EPOXY RESIN COMPOSITION FOR FIBER REINFORCED COMPOSITE MATERIAL - The present invention provides an epoxy resin composition for a fiber reinforced composite material comprising an epoxy resin (A) comprising an epoxy resin (a | 03-11-2010 |
| 20100080953 | Formation of Imprints and Methodology for Strengthening a Surface Bond in a Hybrid Ceramic Matrix Composite Structure - A hybrid ceramic matrix composite structure and method for fabricating such an structure are provided. A ceramic matrix composite substrate | 04-01-2010 |
| 20100086729 | MULTIFUNCTIONAL RADIATION-HARDENED LAMINATE - A multifunctional composite having high strength, low weight, low distortion, low CTE, impact resistance, and multi-faceted radiation protection. | 04-08-2010 |
| 20100086730 | METHOD TO CONNECT BAFFLE & INTERNAL STRUCTURE TO THE OUTER-SHELL OF SLEEPING BAG, INSULATED JACKET AND TENT - A waterproof, insulated multi-layer fabric structure is described, including a first and second layer to bound an interior volume. A baffle layer is located in the bounded volume and undulates between the first layer and second layer. The baffle layer is directly attached to the first layer. Adhesive tape portions are attached to the second layer to eliminate the need of stitching through the second layer, improving the structure's waterproof qualities. The baffle layer is attached to the adhesive tape portions which extend from the second layer. A method for manufacturing the multi-layer structure is also described. | 04-08-2010 |
| 20100086731 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - A honeycomb structure | 04-08-2010 |
| 20100098903 | Honeycomb Structure - There is provided a honeycomb structure in which filtration efficiency of particulate matters (PM) in the exhaust gas is high, initial pressure loss is low and increase in pressure loss in accompanied with the trapping of PMs is suppressed. | 04-22-2010 |
| 20100112277 | Microstructures and methods of fabrication thereof - Microstructures and methods of fabricating microstructures are disclosed. One exemplary microstructure, among others, includes a substrate, an overcoat layer disposed upon the substrate, an air-region within at least a portion of the overcoat layer, and a framing material layer engaging at least a portion of the air-region on the inside of the framing material layer and engaging the overcoat layer on the outside of the framing material layer. | 05-06-2010 |
| 20100112278 | MULTIWALL SHEET, AN ARTICLE, A METHOD OF MAKING A MULTIWALL SHEET - Disclosed herein is a multiwall sheet that comprises a first wall, a second wall, an intermediate wall disposed between the first wall and the second wall, a first set of ribs disposed between the first wall and the intermediate wall, and a second set of ribs disposed between the second wall and the intermediate wall. No ribs are in direct vertical alignment so as to align from the first wall to the second wall and no ribs are on a side of the first wall opposite the intermediate wall or on a side of the second wall opposite the intermediate wall. Also disclosed is a method for making a multiwall sheet. | 05-06-2010 |
| 20100112279 | DIFFUSION-TOLERANT DATA MATRIX DESIGNS - Barcode markings such as two-dimensional data matrices, and methods for using them, according to which ceramic or other articles are imprinted with condensed barcode patterns having printed bars or cells of reduced dimensions as compared with the dimensions of the non-printed bars or cells, and with further processing or use of the articles thereafter causing dilation of the condensed bar or cell patterns to provide patterns with printed and non-printed bars or cells of comparable dimensions. | 05-06-2010 |
| 20100112280 | COATING MATERIAL FOR HONEYCOMB STRUCTURE - There is provided a coating material for a honeycomb structure, the coating material including inorganic particles or organic particles having D90/D10 of 5 to 50 with D10 of 50 μm or less and D90 of 4 μm or more (wherein D10 and D90 are values of 10% diameter and 90% diameter, respectively, in volume-based integrated fraction of a particle diameter distribution measured by a laser diffraction/scattering method from the smaller particle diameter side). | 05-06-2010 |
| 20100119768 | Light-weight thermoplastic olefin truss core for laminated panels for use in the transportation and RV industries - A lightweight thermoplastic core, formed from ThermoPlastic Olefin/ThermoPlastic Vulcanite (TPO/TPV) sheet machined. Said sheet is made of a TPO material that contains fillers to enhance strength and improve Coefficient of Linear Expansion (CLTE). The sheet is heated to thermoforming temperature, then formed by pressure-forming or mechanical pressing the desired shape (truss shape), forming a multi-dimensional core. | 05-13-2010 |
| 20100119769 | BONDING MATERIAL FOR HONEYCOMB STRUCTURE AND HONEYCOMB STRUCTURE UTILIZING THE MATERIAL - A bonding material for a honeycomb structure comprises inorganic particles in which D90/D10 is from 10 to 500, D10 is 100 μm or less and D90 is 4 μm or more, and the D10 and D90 are the values of 10% diameter and 90% diameter from a smaller particle diameter side, respectively, in volume-based integrated fractions of a particle diameter distribution measurement by a laser diffraction/scattering method. | 05-13-2010 |
| 20100129598 | OPTICAL FILM - An optical film includes a number of phosphor layers. The phosphor layers are stacked together, and each of the phosphor layers is excited by an exciting light source and respectively emits a secondary light beam. The secondary light beams emitted by the phosphor layers are in different wavelength ranges. | 05-27-2010 |
| 20100129599 | LOW THERMAL MASS CORDIERITE BODIES AND METHODS FOR MAKING SAME - Disclosed are cordierite bodies having relatively low thermal mass with good mechanical strength. The porous cordierite bodies generally include a primary cordierite ceramic phase as defined herein. Also disclosed are methods for making and using the cordierite bodies. | 05-27-2010 |
| 20100129600 | CORDIERITE FORMING BATCH COMPOSITIONS AND CORDIERITE BODIES MANUFACTURED THEREFROM - Disclosed are cordierite bodies having relatively high porosity and controlled pore size. The porous cordierite bodies generally include a primary cordierite ceramic phase as defined herein. Also disclosed are methods for making and using the cordierite bodies. | 05-27-2010 |
| 20100136285 | POLYURETHANE SYSTEMS FOR PRODUCTION OF POLYURETHANE SANDWICH COMPONENTS - The present invention relates to the use of a polyurethane system, comprising (a) polyisocyanates, (b) at least one compound reactive with isocyanate, (c) at least one reactive chain extender having at least two groups reactive toward isocyanates, where at least one group reactive toward isocyanates is a free, primary NH | 06-03-2010 |
| 20100143645 | DRYING MAT - A drying mat is described. The drying mat includes layers of a microfiber material and a foam layer. The drying mat may be used as dish mat to absorb water from dishes. The drying mat may be used as a shower or bath mat to absorb water from a bather standing upon the drying mat. | 06-10-2010 |
| 20100151185 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A method for producing a ceramic honeycomb structure comprising a ceramic honeycomb body comprising large numbers of axially extending cells defined by cell walls, and an outer peripheral wall formed on an outer peripheral surface of the ceramic honeycomb body, comprising the steps of applying a coating material comprising elongated colloidal silica particles to the outer peripheral surface, and drying the coating material to form the outer peripheral wall. | 06-17-2010 |
| 20100151186 | COMPOSITE ARTICLE INCLUDING VISCOELASTIC LAYER WITH BARRIER LAYER - Fiber reinforced resin matrix composite laminates are provided comprising first and second layers of fiber reinforced resin matrix comprising first and second resin matrices and a viscoelastic construction located between the first and second layers of fiber reinforced resin matrix, bound to the first and second resin matrices, comprising: i) at least one viscoelastic layer; and ii) at least one barrier layer. In some embodiments, the viscoelastic construction comprises at least two barrier layers which differ in composition from at least one viscoelastic layer and wherein the at least two barrier layers are bound to said first and second resin matrices. In some embodiments, the one or more barrier layer(s) may be substantially impermeable to organic solvents, and/or substantially impermeable to water, and/or substantially impermeable to gasses. | 06-17-2010 |
| 20100151187 | Honeycomb structure - A honeycomb structure includes a honeycomb segment joined body comprising a plurality of honeycomb segments unitarily joined at joint faces thereof by means of a bonding material layer, and an outer peripheral coat layer, the honeycomb structure having a plurality of cells functioning as fluid passages disposed in parallel with one another in a central axis direction. A thickness of the outer peripheral coat layer at least at one portion of the portions (portions on end faces) located on end faces in longitudinal direction of the bonding material layer in a cross-section in a direction perpendicular to the central axis direction is larger than an average thickness of the portions other than the portions on end faces. | 06-17-2010 |
| 20100159190 | Method of Making Composite Laminated Product - A method of making a composite light diffusing panel including at least spaced apart lites with a fabric layer applied to an inner surface of at least one of said lites, involves applying a transparent adhesive to the layer of fabric or the lite(s), firmly applying the layer of fabric onto the lite(s) to avoid wrinkling fabric, curing the adhesive to bond the fabric to the lite(s), and assembling the lites to form the light diffusing panel. In this way, a functionally useful product can be obtained that does not suffer from wrinkling and other distracting effects. | 06-24-2010 |
| 20100167005 | DIRECTLY DECORATABLE COMPOSITE MATERIALS, METHOD FOR THEIR MANUFACTURE AND THEIR USE - The invention relates to directly decoratable and/or printable composite materials suitable in particular as materials in interior finishing, for linings, constructions and for the manufacture of furniture and similar products. | 07-01-2010 |
| 20100196656 | COMPOSITE BOARD WITH A HONEYCOMB CARDBOARD - A composite board with a honeycomb cardboard has a top board and bottom board pasted to both sides of the honeycomb cardboard. The honeycomb cardboard, top board, and bottom board form an integrated composite board. The honeycomb cardboard consists of bottom paper, top paper and honeycomb paper. The top paper and bottom paper are pasted to both sides of the honeycomb paper. A fortifier can be added between top board and the bottom board. There is a sealing edge which can adopt different structures and qualities. | 08-05-2010 |
| 20100203284 | SEALING MATERIAL FOR HONEYCOMB STRUCTURE, HONEYCOMB STRUCTURE, AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A sealing material for a honeycomb structure includes inorganic fibers, an oxide sol, inorganic particles, and a metal-containing material. The inorganic fibers include a biosoluble inorganic compound. The metal-containing material contains at least one of Mg, Ca, and Sr. The sealing material is acidic. | 08-12-2010 |
| 20100209661 | DRYING MAT - A drying mat is described. The drying mat includes layers of a microfiber material and a foam layer. The drying mat may be used as dish mat to absorb water from dishes. The dying mat may be used as a shower or bath mat to absorb water from a bather standing upon the drying mat. | 08-19-2010 |
| 20100215898 | Honeycomb structure and method for producing the same - There is provided a honeycomb structure and a method for producing the honeycomb structure, capable of reducing variance in pore diameter depending on part and capable of increasing the mean pore diameter as a whole. There is provided a method for producing a cordierite honeycomb structure 1 including the step of firing a honeycomb formed body. In the firing step, a temperature rise rate from 1200° C. to 1250° C. is controlled to 40° C./hr or more, a temperature rise rate from 1250° C. to 1300° C. is controlled to 2 to 40° C./hr, and a temperature rise rate from 1300° C. to 1400° C. is controlled to 40° C./hr or more. There is further provided a honeycomb structure having a porosity of 50 to 70%, a mean pore diameter of 15 to 30 μm, a difference in a mean pore diameter of 5 μm or less between in the central portion and in the outer peripheral portion, a thermal expansion coefficient of 1.0×10 | 08-26-2010 |
| 20100221487 | HONEYCOMB COMPOSITE PLATE OF PLASTIC FOAM - A honeycomb composite plate of plastic foam comprises at least a support body and a plastic surface sheet. The support body comprises at least a support core, which has a honeycomb structure and is formed of plastic foam. The plastic surface sheet is fixed to the support body and supported by it. Further, the support core and the plastic surface sheet are fixed together. | 09-02-2010 |
| 20100227116 | THREE-DIMENSIONAL SHEET STRUCTURE, METHOD FOR MAKING SAME, AND SANDWICH-TYPE STRUCTURAL MATERIAL COMPRISING SUCH STRUCTURE - The invention relates to a three-dimensional sheet structure characterised in that it comprises at least: a first sheet ( | 09-09-2010 |
| 20100233425 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A honeycomb structure having a crystal phase composed of aluminum titanate and mullite, which is obtained by sintering a honeycomb molding made of a mixture comprising titania powder, alumina powder, silica powder and mullite powder, the mixture containing 1-10 parts by mass of silica powder and 5-30 parts by mass of mullite powder per the total amount (100 parts by mass) of the titania powder and the alumina powder, and the mullite powder containing 40-60% by mass of particles having particle sizes of 10-50 μm and 5-30% by mass of particles having particle sizes of 3 μm or less, and its production method. | 09-16-2010 |
| 20100239811 | HONEYCOMB STRUCTURE - There is provided a honeycomb structure comprising a plurality of honeycomb segments having porous partition walls separating and forming a plurality of cells and an outer peripheral wall located in the outermost periphery, first cells each open in an end portion on one side and plugged in the other end portion on the other side and second cells each plugged in the end portion on the one side and open in the other end portion on the other side being alternately disposed with the first cells having an area larger than that of the second cells in a cross section perpendicular to the central axial direction, and the outer peripheral wall having protruding portions along an external shape of the first cells and depressed portions along an external shape of the second cells. The honeycomb segments are bonded to each other with a bonding member. | 09-23-2010 |
| 20100239812 | HONEYCOMB STRUCTURE - There is provided a honeycomb structure including a plurality of honeycomb segments having porous partition walls separating and forming a plurality of cells functioning as fluid passages and an outer peripheral wall located in the outermost periphery. The first cells open in an end portion on one side and plugged in the other end portion on the other side and the second cells plugged in the end portion on the one side and open in the other end portion on the other side are alternately disposed. The first cells have an area larger than that of the second cells in a cross section perpendicular to the central axial direction. The outer peripheral wall has protruding portions along an external shape of the first cells and depressed portions along an external shape of the second cells. The honeycomb segments are bonded together with a bonding member. | 09-23-2010 |
| 20100247848 | Sandwich element for sound-absorbing inner cladding of transport means, especially for sound-absorbing inner cladding of aircraft fuselage cells - A sandwich element for a sound-absorbing inner cladding of transport means, such as aircraft fuselage cells, comprising a honeycomb-shaped core structure and cover layers applied to both sides of the core structure. At least one cover layer is constructed as permeable to air at least in sections and a covering is disposed at least in sections on at least one cover layer, wherein a sound absorption layer is disposed at least in sections in the area of at least one cover layer. | 09-30-2010 |
| 20100247849 | ANTISKID DUNNAGE - The dunnage can be used for protecting edges of articles such as wood furniture during shipping and has a honeycomb panel having a first and second opposed faces, and a first and second adjacent panel sections folded relative to each other along a V-groove extending into the first face, a layer of antiskid cohesive material applied on the V-groove and maintaining said first and second adjacent panels in said folded configuration, and also applied on a substantial portion of one of said first and second adjacent panel sections, on the first face. The cohesive on the exposed face of the folded dunnage acts as an antiskid which reduces the likelihood of the dunnage sliding once applied to the edge of the article, and also reduces the abrasiveness of the honeycomb panel. A process of production is also disclosed where the V-groove can be made on line. | 09-30-2010 |
| 20100247850 | METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE AND HONEYCOMB STRUCTURE - There is provided a method for manufacturing a honeycomb structure comprising the steps of: forming kneaded clay containing a forming mixture of cordierite-forming materials and an organic binder to manufacture a honeycomb formed article, and firing the honeycomb formed article. The forming mixture contains at least hydrophilic talc. The method enables to perform extrusion forming at a high rate even without raising an apparatus load in order to improve productivity and can provide a honeycomb structure. | 09-30-2010 |
| 20100247851 | SEALING MATERIAL FOR HONEYCOMB STRUCTURE, HONEYCOMB STRUCTURE, AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A sealing material for a honeycomb structure includes inorganic fibers, inorganic particles, and an ion adsorbent. The inorganic fibers include a biosoluble inorganic compound. The ion adsorbent is in an amount of about 0.1% by weight or more. | 09-30-2010 |
| 20100247852 | HONEYCOMB STRUCTURE AND BONDED TYPE HONEYCOMB STRUCTURE - A honeycomb structure | 09-30-2010 |
| 20100247853 | CERAMIC HONEYCOMB STRUCTURE - There is provided a ceramic honeycomb structure usable as a catalyst substrate and being improved warm-up properties and thermal insulation properties, and being excellent in exhaust gas purification performance; by employing larger heat capacity and larger thermal conductivity compared with a material of the partition walls in at least one of insides and surfaces of the respective partition walls. | 09-30-2010 |
| 20100247854 | BONDED HONEYCOMB SEGMENT ASSEMBLY - A bonded honeycomb segment assembly has plurality of honeycomb segments each including cell structure having plurality of cells as fluid passages partitioned by porous partition walls and provided in parallel with one another, and outer wall provided in the outer periphery of the cell structure. The outer wall of each of the plurality of honeycomb segments is bonded to one another via bonding layers. Relation of M | 09-30-2010 |
| 20100255249 | FILM AND PROCESS FOR PRODUCING THE SAME - A surfactant is added to a polymer solution ( | 10-07-2010 |
| 20100266808 | PROCESS FOR MANUFACTURING A PANEL COMPRISING AT LEAST ONE HONEYCOMB BODY AND A FIRST SKIN MADE FROM A COMPOSITE MATERIAL - The invention relates to a process for manufacturing a sandwich panel comprising a step to bake a stacked structure ( | 10-21-2010 |
| 20100297388 | COMPOSITE PANEL FOR BLAST AND BALLISTIC PROTECTION - A composite panel comprises a single composite layer and the single composite layer includes a thermoplastic resin matrix, reinforcing fiber, and nano-filler particles. The nano-filler particles are dispersed within the thermoplastic resin matrix to define a nano-filled matrix material. The reinforcing fiber is further disposed within the nano-filled matrix material. | 11-25-2010 |
| 20100304082 | Lanthanum-Containing Cordierite Body And Method Of Manufacture - Lanthanum containing cordierite bodies are provided that exhibit high strength, little or no microcracking, and a high thermal shock resistance. Improved maintenance of low microcracking and high strength is obtained even after exposure to high temperatures. | 12-02-2010 |
| 20100310819 | ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE, ITS PRODUCTION METHOD, AND STARTING MATERIAL POWDER FOR PRODUCING SAME - A ceramic honeycomb structure having a large number of flow paths partitioned by porous cell walls, the cell walls comprising at least main crystals of aluminum titanate, in which MgO and SiO | 12-09-2010 |
| 20100310820 | HONEYCOMB PANEL AND ITS PRODUCTION - The invention relates to a method for processing a continuous honeycomb panel, said method comprising the subsequent steps of producing a continuous honeycomb panel from strips of material to form the continuous honeycomb panel in compressed form, at least partially expanding said compressed continuous paper honeycomb, producing a series of spaced cuts in at least one of the edges of said strips, and applying pressure on said at least one cut edge for bending said cut edge. | 12-09-2010 |
| 20100323150 | METHOD FOR PRODUCING A SANDWICH COMPONENT HAVING A HONEYCOMB CORE - A method of producing composite components having a honeycomb core ( | 12-23-2010 |
| 20110020595 | METHOD FOR MANUFACTURING A CORE COMPOSITE PROVIDED WITH COVER LAYERS ON BOTH SIDES AS WELL AS A CORE COMPOSITE - The invention relates to a method for manufacturing a core composite ( | 01-27-2011 |
| 20110027526 | Multi-Functional Aircraft Structures - A method and apparatus for manufacturing a composite structure. A filler material with a barrier material for a channel in the filler material is formed. A composite material and the filler material with the barrier material are laid up onto a tool in a shape of the composite structure. The composite material and the filler material in the shape of the composite structure are cured. | 02-03-2011 |
| 20110045233 | DIMENSIONAL CONTROL DURING FIRING TO FORM ALUMINUM TITANATE HONEYCOMB STRUCTURES - A method for controlling the dimensional shrinkage or growth of AT honeycomb structures during the firing process by control of the alkali metal ion content in the AT-forming batch materials extruded into an AT green body structure that is heated to form the fired AT honeycomb structure. | 02-24-2011 |
| 20110070396 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - A honeycomb structure | 03-24-2011 |
| 20110123761 | BIODEGRADABLE SURFACE PROTECTION SYSTEM MAT - A mat for protecting surfaces from the accumulation of liquids is disclosed. The mat comprises a molded polymeric grid layer made of an elastomeric material having several openings and an absorbent core. The absorbent core comprises a moisture absorbent layer and a moisture barrier layer. The grid layer has a surface engaging perimeter, and the moisture barrier comprises a skid resistant material. The various layers and materials used are either inherently biodegradable or rendered biodegradable through the use of one or more additives. | 05-26-2011 |
| 20110129640 | METHOD AND BINDER FOR POROUS ARTICLES - A method for making porous articles, including: depositing a powder mixture layer comprising a binder powder, and at least one structural powder; contacting the powder mixture layer and an aqueous liquid to selectively activate the binder powder and form a green layer; repeating the depositing and the contacting sequence at least one time; and de-powdering and drying of the resulting green body. The binder powder can include, for example, a protein that is soluble in water at or below about 25° C. The disclosure also provides articles, having high porosity and optionally intricate 3D structures, as defined herein. | 06-02-2011 |
| 20110135873 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A ceramic honeycomb structure having a large number of flow paths defined by porous cell walls having porosity of 45-68% and an average pore size of 15-35 μm, the volume of pores having diameters of more than 50 μm being more than 10% and 25% or less of the total pore volume, the volume of pores having diameters of 100 μm or more being 1-8% of the total pore volume, the volume of pores having diameters of less than 10 μm being 3-10% of the total pore volume, and the pores having a pore size distribution deviation σ [=log(D | 06-09-2011 |
| 20110151181 | Fiber Enhanced Porous Substrate - A porous honeycomb substrate having about 10% to about 60% by volume ceramic fiber is fabricated in a variety of material compositions. The fiber material is combined with particle-based materials to reaction-form composite structures forming a porous matrix. The porous honeycomb substrate exhibits an open pore network of porosity from the fiber component to provide high permeability for various applications such as filtration and catalytic hosting of chemical processes. | 06-23-2011 |
| 20110171420 | AIR CUSHION PAD - An air cushion pad includes at least two sheet members, which are made of resilient materials. Each sheet member forms a plurality of hollow tubes projecting therefrom and the tubes are connected to each other by a substantially flat plate. The tubes of one sheet member and the tubes of the other sheet member are alternately fit to each other in an opposing manner to form the air cushion pad. When an external impact force is applied in a top down manner, the air cushion pad absorbs the impact force and undergoes sideways deformation so as to convert the impact force into a transverse to thereby realize shock absorption and eliminate damage caused by downward action of the impact force to provide the function of protection. | 07-14-2011 |
| 20110171421 | FUSED GRAINS OF OXIDES COMPRISING AL, TI AND MG AND CERAMIC PRODUCTS COMPRISING SUCH GRAINS - The invention relates to a mixture of fused grains mainly comprising or composed of an oxide phase of pseudo-brookite type and comprising titanium, aluminum and magnesium, said fused grains having the following chemical composition, in weight percentages on the basis of the oxides: less than 55% of Al | 07-14-2011 |
| 20110183104 | SANDWICH PANEL WITH INTEGRATED REINFORCING STRUCTURE AND METHOD FOR THE PRODUCTION THEREOF - A Sandwich panel with a core structure, in particular with a honeycomb-shaped core structure, and plane-parallel cover layers applied to both sides of this core structure, to form a floor surface in a fuselage airframe of an aircraft, the core structure having at least one recess into which at least one reinforcing structure is integrated, wherein the at least one reinforcing structure is formed with at least one core, said core having at least one recess into which a stopper is introduced, into which at least one attachment element can be introduced to attach at least one further component to the sandwich panel, and a plurality of prepreg strips which each have a uniform fibre running direction being wound around the core. In addition, the invention relates to a method for the production of a sandwich panel according to the invention. | 07-28-2011 |
| 20110189429 | FABRICATION TECHNIQUES TO ENHANCE PRESSURE UNIFORMITY IN ANODICALLY BONDED VAPOR CELLS - A method of fabricating vapor cells comprises forming a plurality of vapor cell dies in a first wafer having an interior surface region and a perimeter, and forming a plurality of interconnected vent channels in the first wafer. The vent channels provide at least one pathway for gas from each vapor cell die to travel outside of the perimeter of the first wafer. The method further comprises anodically bonding a second wafer to one side of the first wafer, and anodically bonding a third wafer to an opposing side of the first wafer. The vent channels allow gas toward the interior surface region of the first wafer to be in substantially continuous pressure-equilibrium with gas outside of the perimeter of the first wafer during the anodic bonding of the second and third wafers to the first wafer. | 08-04-2011 |
| 20110189430 | Systems and Methods for Providing Vacuum Encapsulation for Climate Control Panels - A climate control system according to implementations of the invention includes one or more vacuum chambers. The vacuum chamber is encompassed by a chamber wall that is substantially impervious to gases. The vacuum chamber houses one of several combinations. In one combination, the near vacuum has yet to be created, and the vacuum chamber houses substantially-pure carbon dioxide and un-reacted carbon dioxide reducing agent. In a second combination, the near vacuum has been created, and the vacuum chamber houses reaction products of a chemical reaction between substantially-pure carbon dioxide and carbon dioxide reducing agent in a near vacuum. Various methods are used for creating vacuum chambers and for generating near vacuum conditions within such chambers. Various systems and structures can utilize such vacuum chambers and panels containing such chambers. | 08-04-2011 |
| 20110200785 | COMPOSITE SHEET HAVING A CORE HAVING END WALLS AND A MAT WITH FIBERS - This invention relates to a composite sheet and a method of making a composite sheet. A core having end walls is provided. Continuous fibers or a continuous fiber mat is secured to the core such that the continuous fibers align with the end walls of the core. Various manufacturing methods are disclosed. | 08-18-2011 |
| 20110200786 | COMPOSITE HONEYCOMB STRUCTURE - Adjoining edges of adjacent honeycomb core panel sections are mechanically interlocked. In one embodiment, the method includes forming a first edge along a first cellular core panel section. The first edge includes a first plurality of edge cell walls along the first edge. The method further includes forming a second edge along a second cellular core panel section, wherein the second edge includes a second plurality of edge cell walls along the second edge. The first edge is positioned proximate to the second edge. At least a portion of at least one of the first plurality of edge cell walls is mechanically interlocked with at least a portion of at least one of the second plurality of edge cell walls to form a joint therebetween. The invention also includes a composite structure at least partially produced by such a method. | 08-18-2011 |
| 20110206894 | Crash Energy Absorbing Furniture Top - Crash energy absorbing furniture top with a top skin, a bottom skin and an energy absorbing material disposed between the top and bottom skin is disclosed. The crash energy absorbing material may be disposed between the top skin and the bottom skin, the crash energy absorbing material being bonded to the top skin in a substantially regular pattern of bonded areas. The energy absorbing furniture top absorbs energy by deforming when an individual collides with the energy absorbing furniture top. The deforming of the crash energy absorbing furniture top reduces the risk of injury to the individual in a collision. | 08-25-2011 |
| 20110206895 | CARBON FIBER LAMINATE SKI OR SNOWBOARD WITH METAL RIB CORE DAMPENING SYSTEM - A ski or snowboard may be constructed of an elongate body having a front end and a rear end. The body further includes a core with a top side and a bottom side. At least one layer of carbon fiber is laminated to the core at the top side and the bottom side. Also, at least one metal rib extends along the core, with the metal rib being sandwiched between the layers of carbon fiber. | 08-25-2011 |
| 20110212293 | ECO-FRIENDLY INCOMBUSTIBLE BIOCOMPOSITE AND METHOD FOR PREPARING THE SAME - Disclosed is an eco-friendly incombustible biocomposite including: a) a polymer matrix comprising a natural fiber; and b) a ceramic sheet laminated integrally with the polymer matrix. The biocomposite is eco-friendly since the natural fiber is used as a reinforcement material and is incombustible since it is laminated integrally with the ceramic sheet. Further, it has superior storage modulus, dimensional stability and flexural properties and lightweightness, and is processable into various structures. Thus, it is very useful for automotive or building indoor/outdoor materials. | 09-01-2011 |
| 20110229684 | HONEYCOMB STRUCTURE - A honeycomb structure includes a honeycomb block including at least one honeycomb fired body. The at least one honeycomb fired body has cell walls extending along a longitudinal direction of the at least one honeycomb fired body to define cells. The cells include peripheral cells in contact with peripheral walls of the at least one honeycomb fired body and basic cells positioned to be surrounded by the peripheral cells. The peripheral cells include an irregular cell having a cell cross-sectional area larger than a cell cross-sectional area of one of the basic cells. | 09-22-2011 |
| 20110236624 | HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block including at least one honeycomb fired body. The at least one honeycomb fired body has cell walls to define cells and a peripheral wall constituting a periphery of the at least one honeycomb fired body. The cells include peripheral cells in contact with the peripheral wall of the at least one honeycomb fired body constituting a periphery of the ceramic block and basic cells arranged at an inner side of the peripheral cells. The peripheral cells include deformed cells each having a different shape from the basic cells in a cross section perpendicular to a longitudinal direction of the at least one honeycomb fired body. Each of the deformed cells is capable of receiving therein a circle of about 0.9 mm in diameter in the cross section perpendicular to the longitudinal direction. | 09-29-2011 |
| 20110236625 | FORMED ZEOLITE HONEYCOMB ARTICLE AND FIRED ZEOLITE HONEYCOMB ARTICLE - A formed zeolite honeycomb article comprises a formed article obtained by extruding a zeolite raw material containing zeolite particles, an inorganic binding material and a filler constituted of plate-like particles in a honeycomb shape including partition walls disposed to form a plurality of cells, a drying shrinkage of the partition walls in a thickness direction thereof is larger than a drying shrinkage of the partition walls in a cell extending direction thereof and a drying shrinkage of the partition walls in a diametric direction perpendicular to the cell extending direction thereof, and the drying shrinkage of the partition walls in the thickness direction thereof is 1.2 or more times the drying shrinkage of the partition walls in the diametric direction perpendicular to the cell extending direction thereof in the formed zeolite honeycomb article. | 09-29-2011 |
| 20110236626 | HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block including honeycomb fired bodies. The honeycomb fired bodies include outer honeycomb fired bodies and at least one inner honeycomb fired body. At least one of the outer honeycomb fired bodies includes a curved part and a linear part provided in a part of a periphery of the at least one of the outer honeycomb fired bodies which partially constitutes a periphery of the ceramic block. The linear part is substantially parallel to at least one of a first adhesive layer between one of the outer honeycomb fired bodies and an adjacent inner honeycomb fired body, and a second adhesive layer between adjacent outer honeycomb fired bodies. The linear part has a length of from about 5 mm to about 20 mm in a direction substantially perpendicular to the longitudinal direction. | 09-29-2011 |
| 20110236627 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING A HONEYCOMB STRUCTURE - A honeycomb structure includes honeycomb fired bodies, adhesive layers, and edge members. Each of the honeycomb fired bodies has a first end face, a second end face, and side faces. The adhesive layers are disposed on the side faces to bond the honeycomb fired bodies to each other. Each of the side faces has a first side that is one side of one of the first end face and the second end face. The edge members are disposed on the side faces and including an inorganic material. Each of the edge members has a substantially quadrangular pillar shape with a second side that has substantially a same width as the first side and that is disposed such that the second side is in a vicinity of one of the first end face and the second end face. | 09-29-2011 |
| 20110236628 | CERAMIC HONEYCOMB FILTER WITH ENHANCED THERMAL SHOCK RESISTANCE - Thermal shock resistance of a ceramic honeycomb structure is increased through modifications of the cell wall joints. Wall joints can be modified such that a longitudinally-extending opening is created, putting two or more cells that meet at the wall joint in fluid communication through such opening. In such a case, all walls that meet at such a modified joint must join at least one other wall at that joint. Alternatively, wall joints can be modified by providing stress concentrating notches which extend into the joint from two or more cells that share the joint. | 09-29-2011 |
| 20110244175 | Honeycomb Core Having a High Compression Strength and Articles Made from the Same - This invention is directed to a honeycomb core structure having a high compression modulus. The core structure comprises (a) a plurality of interconnected walls having surfaces which define a plurality of honeycomb cells, wherein the cell walls are formed from a nonwoven sheet and (b) a cured resin in an amount such that the weight of cured resin as a percentage of combined weight of cured resin and nonwoven sheet is at least 62 percent. The nonwoven sheet further comprises fibers having a modulus of at least 200 grams per denier (180 grams per dtex) and a tenacity of at least 10 grams per denier (9 grams per dtex) wherein, prior to impregnating with the resin, the nonwoven sheet has an apparent density calculated from the equation Dp=K×((dr×(100−%r)/%r)/(1+dr/ds×(100−%r)/%r), where Dp is the apparent density of the sheet before impregnation, dr is the density of cured resin, ds is the density of solid material in the sheet before impregnation, % r is the cured resin content in the final core structure in weight %, K is a number with a value from 1.0 to 1.35. Further, the Gurley porosity of the nonwoven sheet before impregnation with the resin is no greater than 30 seconds per 100 milliliters. The invention is also directed to composite structures incorporating such folded core. | 10-06-2011 |
| 20110244176 | CERAMIC CLAY, CERAMIC FORMED ARTICLE, AND CERAMIC STRUCTURE, AND MANUFACTURING METHODS THEREOF - The ceramic clay is available by kneading a forming raw material containing a ceramic forming material. The forming raw material contains, in addition to the ceramic forming material, a layered double hydroxide represented by a predetermined chemical formula in an amount of from 0.01 to 5 mass % based on the total amount of them. The layered double hydroxide turns into a gel by dispersing it in water and when it is dispersed in water at a concentration of 6 mass %, it has a viscosity of from 1000 to 20000 mPa·s. | 10-06-2011 |
| 20110244177 | Semi-Open Structure with Tubular Cells - In an at least partially semi-open structure having adjoining, generally tubular open cells, and consisting of sheet material delimiting each of the tubular open cells, having a width (W), a length (L) and a thickness (T) and having multiple spaced corrugations ( | 10-06-2011 |
| 20110250382 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING HONEYCOMB STRUCTURE - A honeycomb structure includes at least one pillar-shaped honeycomb unit and a pair of electrodes. The pillar-shaped honeycomb unit includes an outer peripheral wall and cell walls. The cell walls extend along a longitudinal direction of the honeycomb unit to define cells. The cell walls are composed of a ceramic aggregate having pores. The cell walls contain a substance having an electrical resistivity lower than an electrical resistivity of ceramic forming the ceramic aggregate. The pair of electrodes is arranged at the cell walls and/or the outer peripheral wall. | 10-13-2011 |
| 20110250383 | SHEAR COMPLIANT HEXAGONAL MESO-STRUCTURES HAVING HIGH SHEAR STRENGTH AND HIGH SHEAR STRAIN - A shear layer for a shear band that is used in a tire is provided that has multiple cells or units having an auxetic configuration and that are constructed from aluminum or titanium alloys. The cells may have an angle of −10°. | 10-13-2011 |
| 20110262688 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block including honeycomb fired bodies. The honeycomb fired bodies includes at least one first-shaped unit having a substantially quadrangular shape in a cross section perpendicular to the longitudinal direction. At least one second-shaped unit has a shape that includes at least a first side, a second side making a substantially right angle with the first side, and an inclined side facing the substantially right angle in the cross section. The at least one second-shaped unit is located in a peripheral portion of the ceramic block and is disposed with the second side adjacent to the at least one first-shaped unit. The second side forming a periphery of the at least one second-shaped unit is longer than a longest side of four sides forming a periphery of the at least one first-shaped unit in the cross section. | 10-27-2011 |
| 20110262689 | COMPOSITION FOR EXTRUSION-MOLDED BODIES - A composition for extrusion-molded bodies which comprises | 10-27-2011 |
| 20110262690 | COMPOSITION FOR EXTRUSION-MOLDED BODIES - A composition for extrusion-molded bodies which comprises
| 10-27-2011 |
| 20110262691 | HONEYCOMB STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - A method for manufacturing a honeycomb structure includes extrusion-molding honeycomb molded bodies. The honeycomb molded bodies are fired to form honeycomb fired bodies. A molding frame optionally having a vent portion with air permeability is provided. The honeycomb fired bodies are fixed in the molding frame. A member having an other vent portion with air permeability is optionally disposed on an inner face side of the molding frame. A gap between the honeycomb fired bodies and a gap between the molding frame and the honeycomb fired bodies are filled with a sealing material paste. The sealing material paste includes inorganic particles and/or inorganic fibers. The sealing material paste is dried to solidify the sealing material paste and to form an adhesive layer and a coat layer. The sealing material paste is in contact with at least a part of the vent portion during the drying. | 10-27-2011 |
| 20110262692 | MANUFACTURING METHOD FOR HONEYCOMB-LIKE STRUCTURAL BODY, AND THE HONEYCOMB-LIKE STRUCTURAL BODY - A preform is formed by stacking core elements that are coated with prepregs. By heating the preform at a temperature at which the core elements do not thermally shrink, the prepregs are preliminarily hardened, and prepregs that are in contact with each other are caused to adhered to each other. Then, the prepregs are definitively hardened and the core elements are thermally shrunk by heating the preform at a temperature at which the core elements thermally shrink. | 10-27-2011 |
| 20110268916 | Double Skin Composite Hybrid Structural Insulated Panel - The invention is a structural insulated panel that can be utilized as a building panel. The structural insulated panel has a two part skin system, comprising a semi-flexible or rigid FRP laminate that is adhered to a thicker and usually more rigid material such as cement board or magnesium oxide board. The double skin is adhered to one or both sides of a core material that can comprise one or more plastic foams, natural materials, honeycomb, paper, plastic and aluminum. | 11-03-2011 |
| 20110274873 | COMPOSITE PANELS HAVING IMPROVED FLUID IMPERMEABILITY - A prepreg composite material that includes a fiber layer and a resin comprising a thermoset resin component, a curing agent and a fibrous micropulp. The micropulp component is an aramid fiber having a volume average length of from 0.01 to 100 micrometers. The prepreg is useful in composite panel construction for minimizing fluid permeation into the cured structure. This prepreg is particularly suitable for making honeycomb sandwich panels. Film adhesives, liquid and paste resins containing aramid fiber micropulp are also disclosed. | 11-10-2011 |
| 20110281063 | HONEYCOMB CORE BASED ON CARBON FIBER PAPER AND ARTICLES MADE FROM SAME - This invention relates to a honeycomb core made from paper comprising 20-85 weight percent of carbon fiber floc. The carbon fibers have a non-round cross sectional aspect ratio of at least 1.5:1. The paper has a fiber volume fraction of at least 35%. The arithmetic mean length of the carbon fibers is at least 0.5 mm. and a length weighted mean length of at least 0.9 mm. | 11-17-2011 |
| 20110293882 | CORDIERITE COMPOSITIONS FOR IMPROVED EXTRUSION PROCESS QUALITY - A green ceramic composition and a green ceramic body. The green composition and the body formed therefrom have sufficiently high wet strength to prevent formation of defects due to differential flow. The composition does not include calcined clays and comprises hydrated clays, cordierite precursors such as alumina, talc, and silica, and at least one binder. The binder can be present at a level that ranges from 3 wt % up to 10 wt %. A method of making a cordierite green body is also described. | 12-01-2011 |
| 20110293883 | Cordierite Porous Ceramic Honeycomb Articles - Porous ceramic honeycomb articles for use as particulate filters and processes for making the same are described herein. The porous ceramic honeycomb articles include a fired cordierite body. The fired cordierite body has a microcrack parameter (Nb | 12-01-2011 |
| 20110300329 | AIRFLOW PAD - An airflow pad is disclosed that includes first and second external facings of paper material extending between edge portions of the panel and having interior portions disposed remotely from the edge portions. A low-density core of paper material disposed between and associating the external facings to provide stiffness to the panel. The pad defines a network of channels open at least one of the edge portions and at the interior portion of the first facing allowing airflow therebetween. | 12-08-2011 |
| 20110305868 | Composite thermal insulation material - A composite thermal insulating material comprises a layer ( | 12-15-2011 |
| 20110305869 | VEHICLE OUTER SURFACE COMPONENT COMPRISING A GLASS LENS - The invention relates to a vehicle outer surface component, which may be assembled on the outer surface of a vehicle, comprising a support structure with an outer skin having a lens of glass or a material similar to glass. According to the invention, a simple and economical production of such a vehicle outer surface component may be achieved whereby the support structure is a thermoplastic moulded piece or a lightweight composite structure and the outer skin of an at least partly transparent plastic is directly applied to the support structure by spray coating. | 12-15-2011 |
| 20110311762 | ROOM TEMPERATURE STABLE AGAROSE SOLUTIONS - The present invention provides porous functionalized crosslinked polysaccharide hydrogel coated structures and methods for making the same. The methods include impregnating a porous substrate with a room temperature stable aqueous polysaccharide solution containing, water, a polysaccharide having a concentration in the aqueous solution from about 0.1% to about 20%, a gel-inhibiting agent having a concentration in the aqueous solution from about 18 to about 54%, and an anionic fluorosurfactant having a concentration in the aqueous solution from about 0.001% to about 10% by total weight of the aqueous solution. Followed by evaporating the water from the polysaccharide coating; and exposing the dehydrated polysaccharide coating to a gelling agent form a porous polysaccharide hydrogel coated substrate. The hydrogel coated substrate is exposed to a crosslinking agent to form a porous crosslinked polysaccharide hydrogel coated substrate, which is then functionalized by the attachment of a ligand. | 12-22-2011 |
| 20120003420 | HONEYCOMB STRUCTURE BODY AND METHOD OF PRODUCING THE SAME - A honeycomb structure body has a honeycomb base body and a pair of electrodes composed of conductive ceramic layers and intermediate layers. The honeycomb base body made of porous ceramics containing SiC is comprised of a cell formation part and an outer peripheral part. The outer peripheral part covers the cell formation part. Each electrode is comprised of a conductive ceramic layer and an intermediate layer. The conductive ceramic layers containing SiC, Si and C are formed at two opposite positions on the outer peripheral part observed from a diameter direction. The intermediate layers containing SiC, Si and C are formed in the outer peripheral part at the parts which face the conductive ceramic layers. The honeycomb structure body satisfies a relationship of 0.5≦t/T≦1, where “t” indicates the thickness of the intermediate layer and “T” indicates the thickness of the outer peripheral part. | 01-05-2012 |
| 20120015139 | Void Filler Panel - A void filler panel including a first major wall, a second major wall spaced apart from the first major wall and pillars extending between the first and second major walls, wherein the first major wall, the second major wall and the plurality of pillars are formed from a polymeric material. | 01-19-2012 |
| 20120021167 | ENERGY ABSORBING SYSTEM - A flexible energy absorbing system including a material coated, impregnated and/or combined with a strain rate sensitive substance is disclosed. The flexible energy absorbing system is formed so as to define repeating adjacent cells, each cell having a re-entrant geometry such that, upon impact, the material locally densifies at the impact site. | 01-26-2012 |
| 20120021168 | Structure, Molded Article, and Method for Manufacturing Same - A structure | 01-26-2012 |
| 20120040130 | Minireactor Array | 02-16-2012 |
| 20120064285 | MULTIFUNCTIONAL NANO-SKIN ARTICLES AND METHODS - Methods for vibration and acoustic abatement. The methods comprise providing a substrate with a composite layer deposited thereon, the substrate receiving a vibration energy sufficient to provide at least one bending wave therein, and converting at least a portion of the vibration energy sufficient to cause the at least one bending wave to at least one shear wave in at least a portion of the composite layer. The composite layer comprises an elastomeric polymer matrix comprising carbon nano tubes dispersed or distributed therein. Articles with the composite layer comprising carbon nano tubes disposed thereon are also disclosed and described. | 03-15-2012 |
| 20120064286 | HONEYCOMB STRUCTURAL BODY - A honeycomb structural body includes porous partition walls arranged to form a plurality of cells which become through channels of a fluid, porosities of the partition walls are from 45 to 70%, a pore diameter distribution of the partition walls is measured by mercury porosimetry, the pore diameter distribution indicates a bimodal distribution, in the bimodal distribution, a pore diameter at the maximum peak value of a small pore side distribution is from 1 to 10 μm, and a pore diameter at the maximum peak value of a large pore side distribution exceeds 10 μm, and a ratio between a pore volume of the small pores and a pore volume of the large pores is in a range of 1:7 to 1:1 in the honeycomb structural body. | 03-15-2012 |
| 20120082821 | Adhesive label and method of producing the same - An adhesive label ( | 04-05-2012 |
| 20120094061 | Formable Protector - A sandwich construction including a core having inner and outer surfaces and comprising a sheet material oriented extending between the inner and outer core surfaces in a configuration providing resistance to crushing in a direction between the inner and outer surfaces. The formable protector further includes an outer facing layer of a sheet material adhered to the outer surface of the core layer; and an inner facing layer adhered to the core inner surface and being sufficiently deformable to conform to a sharp edge of a protected object when the protector is bent therearound, and being substantially more compressible or stretchable than the outer facing layer. The core has sufficient resistance to crushing and the outer facing layer is sufficiently durable for causing the core to partially crush when the protector is bent around the sharp edge while partially retaining crushing resistance for protecting the sharp edge against impact. | 04-19-2012 |
| 20120100336 | CERAMIC HONEYCOMB STRUCTURE WITH APPLIED INORGANIC SKIN - A skin is applied to a ceramic honeycomb. The skin is formed by applying a skin-forming composition and drying it. The skin-forming composition includes a carrier liquid, colloidal silica and/or colloidal alumina, and an inorganic filler. The filler includes an inorganic fiber. The filler may contain low aspect ratio particles that have the same or nearly the same CTE as the inorganic fiber. The filler may include a small proportion of a low aspect ratio filler particle that has a different CTE than the inorganic fiber. | 04-26-2012 |
| 20120100337 | BOARD STRUCTURE FOR VEHICLE AND MANUFACTURING METHOD OF THE SAME - Provided is a board structure for a vehicle, which includes a durable hinge portion while light weight and high rigidity of the board structure are maintained. The board structure includes: hinge portion | 04-26-2012 |
| 20120114900 | SYSTEM AND METHOD FOR FORMING A SUPPORT ARTICLE - A collapsible support article having a bi-directional corrugated structure is defined by folding along folds lines in an accordion style resulting in peak and valley rows with first and second connections points being defined along the folds lines to generate a second direction of the structure. The first connection points are connected at each peak or valley and each second connection point is connected to adjacent peak or valley rows to define the structural unit. The material used as well as spacing between connection points and the distance between the fold lines determine the strength of and the visibility through the structural unit. The structural unit may be used as a single unit for packing material, as a travel pillow or a plurality of joined structural units to define a sleep suit. Variations in the structural unit may result in a curved support article or a contoured support article. | 05-10-2012 |
| 20120121853 | REINFORCED INJECTION MOLDED THERMOPLASTIC CELLULAR CORE - A reinforced, thermoplastic, injection molded cellular core is provided, wherein the cellular core can include minimum wall thickness sections of less than 1.5 mm and in selected constructions less than 0.5 mm, wherein larger reinforcing pillars at disposed at predetermined locations to form a structural body. A cross sectional shape, sizing and spacing of a plurality of cells within the cellular core can be set in a predetermined configuration to provide for varying density of the cellular core. Reinforcing elements can be uniformly or non-uniformly distributed throughout the cellular core. Stratum can be integrally formed with the cellular core to provide additional performance characteristics. | 05-17-2012 |
| 20120135186 | Cordierite Porous Ceramic Honeycomb Articles With Delayed Microcrack Evolution - A porous ceramic honeycomb article includes a primary cordierite phase and an intercrystalline glass phase. In an as-fired condition, the porous ceramic honeycomb article exhibits microcrack parameter Nb | 05-31-2012 |
| 20120141726 | Thermoplastic Composite Window Panel for Aircraft Applications - An aircraft trim panel structure includes a thermoplastic resinated quadraxial fiberglass lay-up prepreg first open structure skin layer having at least a 28% open area. A thermoplastic resinated quadraxial fiberglass lay-up prepreg second open structure skin layer has at least a 28% open area. An open structure core layer having at least a 28% open area is sandwiched between the first open structure skin layer and the second open structure skin layer. The first open structure skin layer, the second open structure skin layer and the open structure core layer are formed into a three dimensional shape corresponding to the aircraft trim panel. | 06-07-2012 |
| 20120148792 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A ceramic honeycomb structure having a large number of flow paths partitioned by porous cell walls, the cell walls having porosity of 40-60%; pores opening on the cell wall surface having an opening area ratio (the total opening area of pores opening on the cell wall surface per a unit area) of 15% or more; the median opening diameter of the opening pores being 10 μm or more and less than 40 μm, when the opening diameter of each pore opening on the cell wall surface is expressed by an equivalent circle diameter (a diameter of a circle having the same area as the opening area of each pore); the density of pores having equivalent circle diameters of 10 μm or more and less than 40 μm being 350/mm | 06-14-2012 |
| 20120148793 | HONEYCOMB STRUCTURE - A honeycomb structure includes a ceramic block and a sealing material layer. The ceramic block includes a plurality of honeycomb fired bodies each having a large number of cells longitudinally disposed substantially in parallel with one another with a cell wall between the cells, an adhesive layer for bonding side faces of the honeycomb fired bodies, and a cavity-holding member placed between the side faces of the honeycomb fired bodies. The sealing material layer is formed on a peripheral face of the ceramic block. The cavity-holding member includes a nonflammable material and has Young's modulus of at least about 0.001 GPa and at most about 0.07 GPa. | 06-14-2012 |
| 20120156423 | Falling-Film Reactor Fluid Distributors and Methods - A fluid distribution or fluid extraction structure for honeycomb-substrate based falling film reactors is provided, the structure comprising a one or two-piece non-porous honeycomb substrate having a plurality of cells extending in parallel in a common direction from a first end of the substrate to a second and divided by cell walls, and a plurality of lateral channels extending along a channel direction perpendicular to the common direction, the channels defined by the absence of cell walls or the breach of cell walls along the channel direction, the channels being closed or sealed to fluid passage in the common direction but open to the exterior of the structure through one or more ports in a side of the structure, the channels being in fluid communication with the plurality of cells via holes or slots extending through respective cell walls, the holes or slots having a width and a length, the width being equal to or less than the length, and the width at widest being less than 150 μm. Methods of fabrication are also disclosed. | 06-21-2012 |
| 20120164373 | FIRE-RETARDANT COMPOSITE MATERIALS - A prepreg for the manufacture of a fibre-reinforced composite material, the prepreg including:
| 06-28-2012 |
| 20120171412 | ALUMINA TITANATE POROUS STRUCTURE - A porous structure comprising a ceramic material, mainly formed by or consisting of an oxide material comprising titanium, aluminum, zirconium and silicium satisfying the following composition, in wt % on the basis of the oxides:
| 07-05-2012 |
| 20120177875 | High porosity ceramic honeycomb article containing rare earth oxide and method of manufacturing same - The present invention describes a high porosity (% P≧45%), refractory, ceramic article comprising a cordierite ceramic phase and at least about 0.1 wt.% of a rare earth oxide, such as yttrium oxide or lanthanum oxide. When compared to typical high-porosity cordierite articles, the articles of the present invention may exhibit relatively high strength, relatively low microcracking, relatively high strain tolerance (MOR/E), and/or relatively high thermal shock resistance (TSP). | 07-12-2012 |
| 20120177876 | Hollow Article With Pillar Structural Members - A hollow article is provided, comprising a first wall and a second wall, where the first and second walls are positioned in opposing relationship and define a space therebetween. A plurality of protruding structural pillars extend from the second wall and span the space, each of the structural pillars having an end surface integrally bonded with an inside surface of the first wall. | 07-12-2012 |
| 20120177877 | INSULATING HONEYCOMB PANEL - Laminar structures comprising two facing panels separated by a honeycomb structure containing foamed elastomeric material in the cells provide a combination of sound insulation and fire retardancy in a compact light weight foam which can be produced using traditional manufacturing techniques. | 07-12-2012 |
| 20120196079 | COMPOSITE BODY - Composite body having a laminate coating at least partially surrounding a core of the composite body, wherein a positive pressure is present at least in a portion of the core that is at least partially surrounded by the laminate coating, or a positive pressure is achievable at least in said portion of the core, in a delamination-free manner. The core is designed at least partially as open-cell foam, and/or a positive pressure is present in at least a portion of the laminate coating or a positive pressure is achievable at least in said portion of the laminate coating, wherein the core is at least partially designed as open-cell foam. | 08-02-2012 |
| 20120196080 | STIFFENED STRUCTURE INTEGRATING AN OPENING - A stiffened structure includes stiffeners ( | 08-02-2012 |
| 20120196081 | NEW BINDER COMPOSITION - The invention relates to a new binder composition which is particularly suitable for the manufacture of composite materials utilizing such new binder composition in the required nonwoven materials. Composite materials using such new binder composition in their nonwoven part are suitable, in particular, for composites materials for interior construction, for linings, floor coverings, and for the manufacture of furniture and similar products. | 08-02-2012 |
| 20120207967 | CEMENT TO MAKE THERMAL SHOCK RESISTANT CERAMIC HONEYCOMB STRUCTURES AND METHOD TO MAKE THEM - An improved ceramic honeycomb structure is comprised of at least two separate smaller ceramic honeycombs that have been adhered together by a cement layer comprised of a cement layer has at least two regions of differing porosity or cement layer where the ratio of toughness/Young's modulus is at least about 0.1 MPa·m | 08-16-2012 |
| 20120251767 | HONEYCOMB STRUCTURE - A honeycomb structure includes a plurality of honeycomb fired bodies. Each of the plurality of honeycomb fired bodies is combined with one another by an adhesive layer interposed between the honeycomb fired bodies to form a ceramic body. Each of the honeycomb fired bodies has a peripheral wall around each of the honeycomb fired bodies and has a plurality of cells each of which extends along a longitudinal direction of the honeycomb fired body and in parallel with one another. The cells are separated from one another with a cell wall disposed between the cells. The ceramic body includes at least one center-high-heat-capacity honeycomb fired body which is a honeycomb fired body having a heat capacity per unit volume in a central part in a plane perpendicular to the longitudinal direction larger than a heat capacity per unit volume in a peripheral part in the plane. | 10-04-2012 |
| 20120251768 | HONEYCOMB STRUCTURE, MANUFACTURING METHOD THEREOF, AND CATALYST CARRYING HONEYCOMB STRUCTURE - There is disclosed a honeycomb structure onto which a large amount of catalyst can be carried while suppressing an increase in pressure drop. In a honeycomb structure | 10-04-2012 |
| 20120258278 | Waterproof, weather resistant tiled table - A tabletop includes a honeycomb panel including a honeycomb core attached to a top and bottom skin. The top surface of the top skin is decorated with tiles adhered to the panel and waterproofed with a hydrophobic, flexible silicone sealer/adhesive. The sealer/adhesive provides moisture resistance and compensation for the differences in the coefficient of thermal expansion of the honeycomb panel and the tiles adhered to the panel. The honeycomb panel may be a metal, preferably aluminum. | 10-11-2012 |
| 20120263914 | METHOD OF MAKING POLYMERIC BARRIER COATING TO MITIGATE BINDER MIGRATION IN A DIESEL PARTICULATE FILTER TO REDUCE FILTER PRESSURE DROP AND TEMPERATURE GRADIENTS - Ceramic honeycomb structures and methods to make the same are disclosed. The structures may be comprised of at least two separate smaller ceramic honeycombs that have been coated with a polymer to create a polymeric barrier coating and adhered together with a cement comprised of inorganic fibers and a binding phase which is comprised of amorphous silicate, aluminite or alumino silicate glass and other inorganic particles. The polymer is selected such that it is penetratable into or covering the pores in the honeycomb structure to form a thin barrier layer thereon to mitigate migration of the inorganic fibers, binding phase and water into the pores. The polymer is adapted to be burned off or decomposed at or below cement and honeycomb skin firing temperatures, or at or below honeycomb operating temperatures during application to create a honeycomb structure that, when formed into an exhaust filter, does not have any undesired pressure drop increase due to cement migration. | 10-18-2012 |
| 20120276324 | ADDITIVES COMPRISING CELLULOSE ETHERS FOR CERAMICS EXTRUSION - The present invention relates to specific additives comprising cellulose ether for improving the extrudability of ceramic masses and other masses which set as a result of baking or sintering, a corresponding extrusion process, the extrudates and their use. | 11-01-2012 |
| 20120276325 | ALUMINA TITANATE POROUS STRUCTURE - Porous structure comprising an oxide ceramic material comprising, on the basis of the corresponding simple oxides: Al | 11-01-2012 |
| 20120276326 | INSULATING MOLDED PART AND METHOD FOR THE PRODUCTION THEREOF - An insulating molded part, comprising an upper part ( | 11-01-2012 |
| 20120282434 | THERMOSETTING RESIN ADHESIVE CONTAINING IRRADIATED THERMOPLASTIC TOUGHENING AGENT - Thermosetting resins are provided that are toughened with an irradiated thermoplastic toughening agent. The resins have reduced levels of solvent-induced micro crack formation and do not lose their adhesiveness when attacked by solvent. The thermoplastic toughening agent is treated with a sufficient amount of high-energy radiation (e.g. electron beam or gamma rays) to cause reductions in solvent-induced micro crack formation and solvent-induced loss of adhesiveness when compared to the same toughened thermosetting resin in which a non-irradiated version of the thermoplastic toughening agent is used. | 11-08-2012 |
| 20120301664 | HONEYCOMB STRUCTURE COMPRISING AN OUTER CEMENT SKIN AND A CEMENT THEREFOR - Disclosed is a honeycomb catalyst support structure comprising a honeycomb body and an outer layer or skin formed of a cement comprising an amorphous glass powder with a multimodal particle size distribution applied to an exterior surface of the honeycomb body. The multimodal particle size distribution is achieved through the use of a first glass powder having a first median particle size and at least a second glass powder having a second median particle size. In some embodiments, the first and second glass powders are the same amorphous glass consisting of fused silica. The cement may further include a fine-grained, sub-micron sized silica in the form of colloidal silica. The cement exhibits a coefficient of thermal expansion less than 15×10 | 11-29-2012 |
| 20120301665 | SANDWICH PANELS - A structural panel comprising an internal core material having first and second opposing faces, first and second face sheets bonded to the first and second opposing faces respectively, wherein the panel comprises an open-structured sheet, interposed between a first face of the core material and its respective face sheet and the panel comprises less than 200 gsm adhesive. | 11-29-2012 |
| 20120301666 | ALPHA-ALUMINA INORGANIC MEMBRANE SUPPORT AND METHOD OF MAKING THE SAME - Compositions for making alpha-alumina supports for, for example, inorganic membranes are described. Methods for controlling the alumina and pore former particle sizes and other process variables are described which facilitate desirable porosity, pore distribution and strength characteristics of the resulting alpha-alumina inorganic membrane supports. | 11-29-2012 |
| 20120308768 | Moldable Fly-Away Tool Structure System - A composite structure includes a first face sheet, a second face sheet, and a foam member located between the first face sheet and the second face sheet. The foam member has a molded contour, the mold contour being configured to provide tooling surface for at least one of the first face sheet and the second face sheet prior to curing of the composite structure. A method of making the foam member includes creating a mold tool having an interior surface which resembles the desired outer contour of the foam member. A mixture is poured into a pour opening in the mold tool. The mixture is allowed to polymerize into a foam as the foam expands and distributes within the mold tool. Vent openings in the mold tool are selectively tailored to control the density of the foam member. The foam member is cured in the mold tool. | 12-06-2012 |
| 20120308769 | Honeycomb Body Interdigitated Mixers and Methods for Producing - Honeycomb body interdigitating mixers are disclosed along with methods for producing them, the honeycomb body having parallel cells extending along a common direction, the mixer comprising a first fluid path extending within the honeycomb body along a first path direction perpendicular to the common direction, the first fluid path defined within a first plurality of said cells, at least a high aspect ratio portion of the first fluid path having an aspect ratio of height in the common direction to width perpendicular to the common direction and to the first path direction of at least 3:1, and a second fluid path extending within the honeycomb body along a second path direction perpendicular to the common direction, the second fluid path defined within a second plurality of said cells, at least a high aspect ratio portion of the second fluid path having an aspect ratio of height in the common direction to width perpendicular to the common direction and to the second path direction of at least 3:1, wherein the first fluid path is fluidically connected to the second fluid path within their respective high aspect ratio portions via a group of apertures, the group extending in the common direction, the group of apertures taken together having a ratio of height in the common direction to width perpendicular to the common direction of at least 3:1. | 12-06-2012 |
| 20120321840 | THREE-DIMENSIONAL WORKPIECE - A three-dimensional workpiece including a first ductile plate, a second ductile plate and a core layer is provided. The core layer is located between the first ductile plate and the second ductile plate. The first ductile plate, the second ductile plate and the core layer are bound together and have a three-dimensional shape. The first ductile plate has a flat area and a curved area. The core layer has a core flat area and a core curved area. The core flat area is superposed with the plate flat area and the core curved area is superposed with the plate curved area. | 12-20-2012 |
| 20130011603 | STRUCTURE AND PRODUCTION METHOD THEREFOR - A structure including a substrate and a coating material. The substrate includes a plurality of voids and a surface on which at least the plurality of voids are formed, and is formed such that a void ratio of the plurality of voids decreases one of 2-dimensionally and 3-dimensionally from an inner side of the substrate toward an outer side thereof. The coating material is formed on the surface of the substrate. | 01-10-2013 |
| 20130011604 | TEMPLATED GROWTH OF POROUS OR NON-POROUS CASTINGS - A method of forming a templated casting involves incorporating a liquid feedstock into the channels of a honeycomb substrate to form a feedstock-laden substrate, and directionally solidifying the liquid feedstock within the channels. | 01-10-2013 |
| 20130022780 | THERMOSETTING RESIN COMPOSITION, THERMOSETTING RESIN COMPOSITION FOR FIBER-REINFORCED COMPOSITE MATERIAL, PREPARED USING THE SAME, AND HONEYCOMB SANDWICH PANEL - An object of the present invention is to provide a thermosetting resin composition having superior toughness. The thermosetting resin composition of the present invention includes a thermosetting resin, and an adsorbing filler in which a thermoplastic resin C is adsorbed on a filler, wherein an adsorption coefficient that is greater than 0 and less than or equal to 0.8, defined by Formula 1 below, is satisfied. | 01-24-2013 |
| 20130029088 | HONEYCOMB CATALYST CARRIER - There is provided a honeycomb catalyst carrier provided with porous partition walls containing cordierite or aluminum titanate as a main component and separating and forming a plurality of cells functioning as fluid passages. The partition walls have a porosity of 0.5% or more and 10% or less. The honeycomb catalyst carrier can be warmed up fast, and the temperature of the catalyst loaded on the honeycomb catalyst carrier can be raised faster. | 01-31-2013 |
| 20130040098 | BENZOXAZINE STRUCTURES - Embodiments of the invention are directed toward benzoxazine composite structures and the application thereof. In some embodiments, a radome can be constructed from a benzoxazine composite structure. A benzoxazine structure can include a low density core with one or two benzoxazine composite face skins. The benzoxazine face skins can include reinforcement materials to provide structural strength. Such radomes and/or benzoxazine structures can be used in various maritime, aircraft, rocket, missile, and/or automobile applications. In particular, radomes can be used to house communication equipment such as antennas and the like. | 02-14-2013 |
| 20130045355 | POROUS POLYIMIDE MEMBRANE AND PROCESS FOR PRODUCTION THEREOF - A porous polyimide film having a three-layer structure that comprises two surface layers (a) and (b) and a macrovoid layer sandwiched between the surfaces layers (a) and (b). The macrovoid layer has a partition wall bonding to the surface layers (a) and (b), and multiple macrovoids each surrounded by the partition wall and the surface layers (a) and (b) and having a mean pore size in the film plane direction of from 10 to 500 μm. The partition wall of the macrovoid layer has a thickness of from 0.1 to 50 μm and has multiple pores having a mean pore size of from 0.01 to 50 μm. The surface layers (a) and (b) each have a thickness of from 0.1 to 50 μm, at least one of the surface layers has multiple pores having a mean pore size of from more than 5 μm to 200 μm, and the other surface layer has multiple pores having a mean pore size of from 0.01 to 200 μm. The pores in the partition wall of the macrovoid layer as well as in the surface layers (a) and (b) communicate with each other and further communicate with the macrovoids. The film has a total thickness of from 5 to 500 μm and a porosity of from 60 to 95%. | 02-21-2013 |
| 20130052405 | FABRICATION TECHNIQUES TO ENHANCE PRESSURE UNIFORMITY IN ANODICALLY BONDED VAPOR CELLS - A method of fabricating one or more vapor cells comprises forming one or more vapor cell dies in a first wafer having a first diameter, and anodically bonding a second wafer to a first side of the first wafer over the vapor cell dies, the second wafer having a second diameter. A third wafer is positioned over the vapor cell dies on a second side of the first wafer opposite from the second wafer, with the third wafer having a third diameter. A sacrificial wafer is placed over the third wafer, with the sacrificial wafer having a diameter that is larger than the first, second and third diameters. A metallized bond plate is located over the sacrificial wafer. The third wafer is anodically bonded to the second side of the first wafer when a voltage is applied to the metallized bond plate while the sacrificial wafer is in place. | 02-28-2013 |
| 20130059113 | Structures For Preventing Microorganism Attachment - Methods of making and using substrates having raised structures to inhibit adhesion of microorganisms are described. | 03-07-2013 |
| 20130071608 | HONEYCOMB STRUCTURE - There is provided a honeycomb structure | 03-21-2013 |
| 20130078417 | SEMIFINISHED PRODUCT FOR THE PRODUCTION OF FIBRE COMPOSITE COMPONENTS BASED ON STABLE POLYURETHANE COMPOSITIONS - The invention relates to a semifinished product for the production of fibre composite components, comprising at least two walls of fibre-filled matrix material, which are angled in a meandering manner and are thermally joined to one another to form a symmetrical core structure. The invention addresses the problem of providing a semifinished product which is suitable as a core structure for a fibre composite component in sheet form that has better draping qualities as a result of the not yet cured matrix, but at the same time is sufficiently stable in terms of its shape and composition that it can be easily handled. This problem is solved by using as the matrix material a polyurethane composition which contains as a binder a polymer having functional groups that are reactive with respect isocyanates and contains as a hardener diisocyanate or polyisocyanate that is blocked internally and/or by blocking agents. | 03-28-2013 |
| 20130095284 | COMPOSITE STRUCTURE AND CORE POSITIONING PLY - A composite structure includes a first laminate, a second laminate, and at least one core component located between the first laminate and the second laminate. The at least one core component includes a honeycomb core and at least one locking ply extending from the honeycomb core between the first laminate and the second laminate. The at least one locking ply is configured such that a pressure applied during a cure cycle of the composite structure retains the at least one locking ply between the first laminate and the second laminate thereby preventing movement of core component. | 04-18-2013 |
| 20130122243 | RESILIENCE CUSHION MAT - We provide a cushioned mat with anti-fatigue qualities. In one embodiment the mat includes a PVC base layer reinforced by a polyester layer and having an indentation that holds a woven PVC fabric insert. Glue is applied to the insert and/or the base layer, which is then heat-pressed to complete and enhance the bond. The resulting product has enhanced comfort and durability properties | 05-16-2013 |
| 20130122244 | Aircraft Interior Panels and Methods of Panel Fabrication - A multifunctional fully integral panel system design, a unique material configuration, and a process for fabricating a net shape (or nearly net shape) panel in one production cycle. The panel may comprise a base facing with an outer perimeter, a decorative film applied to the exterior of the base facing, an aft facing having an outer perimeter fused to the base facing, and a reinforcement core disposed between the unfused portions of the base and aft facings, which reinforcement core also acts as acoustic insulation (i.e., a noise attenuator). Alternatively or additionally, a foam core or blanket having thermal and/or acoustic insulation properties is attached to the external surface of the aft facing. The fabrication process involves the application of different heat treatments to panel components having different forming temperature or rubbery/elastic plateaus. | 05-16-2013 |
| 20130136893 | COLD SET COMPOSITION FOR CERAMIC BODIES - Disclosed are ceramic articles comprising ceramic honeycomb bodies and an aqueous composition, for example in the form of a cold-set plug, as well as processes for preparing ceramic articles and processes for making an aqueous composition for use with ceramic articles, for example as a cold-set plug composition. | 05-30-2013 |
| 20130157000 | COMPONENT AND TURBOMACHINE HAVING A COMPONENT - A component, especially contrived and designed for being used in a turbomachine, includes a high-temperature coating being arranged above a base of the component. The base has at least one structural element for connecting it to the high-temperature coating, with the cross-section of the at least one structural element having at least three different widths, i.e. a base width at the lower end of the at least one structural element, a center width above it, and a tip width above that, where on average the center width is greater than or equal to the base width, but less than four times the base width, in particular less than or equal to three times the base width. | 06-20-2013 |
| 20130164494 | AMMONIA OXIDATION CATALYSTS - Ammonia oxidation catalyst units comprising a pair of honeycomb-type blocks having interplaced between them a layer of a gas permeable material performing the function of radially mixing the gas flow, said blocks comprising an ammonia oxidation catalysts, and having height of less than 15 cm and the interplaced layer height of 3 to 0.5 cm. | 06-27-2013 |
| 20130171407 | ACOUSTIC CORE - A panel assembly and method of making the same, whereby the panel assembly includes an adhesive located onto one or more edges of a layered honeycomb structure and a mesh material adhered in between the layered honeycomb structure by the adhesive. | 07-04-2013 |
| 20130183484 | CORE STRUCTURES COMPRISING TANNIN RESIN - This invention is directed to a structural core comprising a fibrous web and a matrix resin, the matrix resin comprising from 15 to 75 weight percent of the weight of web plus resin, the matrix resin contains a first resin comprising tannin in an amount of 10 to 100 weight percent and a second resin in the event tannin is not present in an amount of 100 weight percent, A preferred second resin is phenolic, benzoxazine, polyester, cyanate ester, bismaleimide, epoxy, polyimide or combination thereof. | 07-18-2013 |
| 20130189479 | INFLATABLE PANEL AND METHOD OF MANUFACTURING SAME - An inflatable panel including a first layer formed of a material of low gas permeability and a second layer formed of a material of low gas permeability. The first and second layers are intermittently sealed together via a plurality of first elongated seals, thereby defining a plurality of first tubes between adjacent pairs of the first elongated seals. The panel also includes a third layer of material of low gas permeability. The third and second layers are intermittently sealed together via a plurality of second elongated seals, thereby defining a plurality of second tubes between adjacent pairs of the second elongated seals. Also, the first and second tubes are sealed at front and rear ends thereof, and a gas is provided within each of the tubes, whereby the gas within each of the tubes is prevented from flowing between tubes. | 07-25-2013 |
| 20130189480 | HONEYCOMB COMPOSITE SUPPORT PART AND METHOD FOR COATING IT - A method for coating a cellulose honeycomb composite support part ( | 07-25-2013 |
| 20130196112 | OXIDE MESOSTRUCTURED FILM AND METHOD FOR MANUFACTURING THE SAME - An oxide mesostructured film has a structure in which the orientation direction of cylindrical structures is a given direction throughout in the film plane, at least one peak appears in an angle region corresponding to a plane spacing of 8 nm or more, the number of atoms (X) of silicon to which an alkyl group having 8 or more carbon atoms is bonded to the number of atoms (Y) of silicon or metallic elements among elements constituting oxides of the oxide mesostructured film is 0.1 or more and 0.5 or lower in terms of the atomic number ratio (X/Y). | 08-01-2013 |
| 20130202845 | BUILDING PANEL AS STRUCTURE OF OUTER AND INNER PLATE WITH INTERMEDIATE INSULATION SPACE - The building panel is structure of outer ( | 08-08-2013 |
| 20130216768 | SILICON CARBIDE CERAMIC AND HONEYCOMB STRUCTURE - Provided is a silicon carbide ceramic having a small amount of resistivity change due to temperature change and being capable of generating heat by current application; and containing silicon carbide crystals having 0.1 to 25 mass % of 4H—SiC silicon carbide crystals and 50 to 99.9 mass % of 6H—SiC silicon carbide crystals, preferably having a nitrogen content of 0.01 mass % or less, more preferably containing two or more kinds of silicon carbide particles containing silicon carbide crystals and silicon for binding these silicon carbide particles to each other and having a silicon content of from 10 to 40 mass %. | 08-22-2013 |
| 20130216769 | COMPOSITION FOR EXTRUSION-MOLDED BODIES COMPRISING A METHYL CELLULOSE - A methyl cellulose having a DS(methyl) of from 1.10 to 1.61 is useful for increasing the wet green modulus of an extrusion-molded hollow body, particularly an extrusion-molded hollow body having a ceramic honeycomb structure. | 08-22-2013 |
| 20130224430 | HONEYCOMB STRUCTURE COMPRISING A CEMENT SKIN COMPOSITION WITH CRYSTALLINE INORGANIC FIBROUS MATERIAL - Disclosed is a honeycomb support structure comprising a honeycomb body and an outer layer or skin formed of a cement that includes an inorganic filler material having a first coefficient of thermal expansion from 25° C. to 600° C. and a crystalline inorganic fibrous material having a second coefficient of thermal expansion from 25° C. to 600° C. | 08-29-2013 |
| 20130224431 | DIMENSIONAL CONTROL OF CERAMIC STRUCTURES VIA COMPOSITION - Disclosed herein are methods for controlling and/or predicting the shrinkage and/or growth of a ceramic honeycomb structure between a green body state and a fired state by adjusting the hydrated alumina content of the batch composition. Also disclosed herein is substantially clay-free cordierite honeycombs produced in accordance with such methods. | 08-29-2013 |
| 20130230687 | Glue-free anti-slip polyvinyl chloride floor brick and preparing method thereof - The present invention discloses a glue-free anti-slip polyvinyl chloride floor brick which includes a polyvinyl chloride anti-slip layer having a bottom surface formed with a flexible thermal-pressed pattern by thermal pressing. The thermal-pressed pattern includes a plurality of continuously and repetitively connected, closed and non-equilateral hexagonal protruded ribs, which are characterized with a required flexibility by utilizing a special ingredient amount of the anti-slip layer and provided with an anti-slip coefficient of 1.5 by incorporating with non-equilateral hexagonal anti-slip patterns with special sizes and shapes, thereby enhancing the slip resistance of the floor brick to overcome the bottlenecks in plastic floor brick industries. | 09-05-2013 |
| 20130230688 | Breathable Insulation - The present invention relates to a breathable insulation, could be set on the some part or whole of fabric, cloth, silk, cotton, textile, satin, yarn, linen, wool, synthetic fiber, rayon, polyester fiber, nylon or integrated with part or all of the fabric, cloth, silk, cotton, textile, satin, yarn, linen, wool, synthetic fiber, rayon, polyester fiber, nylon, comprising one or several support units located in the same plane or in different planes to allow air there in convection, with said design, the support units could form three-dimensional spaces to help air convection and to allow warm air come out of human skin. It helps for air distribution and convection, and helps the temperature of the human skin being warm through, not sultry, and achieves the purpose of natural insulation breathable. | 09-05-2013 |
| 20130236687 | HONEYCOMB STRUCTURE AND HONEYCOMB CATALYST - There is disclosed a honeycomb structure usable as a support of a honeycomb catalyst onto which a large amount of catalyst can be loaded and which has a good purification efficiency, and the honeycomb structure includes porous partition walls | 09-12-2013 |
| 20130236688 | SANDWICH COMPONENT AND METHOD FOR PRODUCING SAME - A sandwich component with a moisture barrier and a method for the production thereof. The sandwich component has at least one top layer ( | 09-12-2013 |
| 20130243997 | LATTICE-STRUCTURES AND CONSTRUCTS WITH DESIGNED THERMAL EXPANSION COEFFICIENTS - A thermal expansion-managed lattice structure having a plurality of unit cells each having flexure bearing-mounted tabs supported on a base and actuated by thermal expansion of an actuator having a thermal expansion coefficient greater than the base and arranged so that the tab is inwardly displaced into a base cavity. The flexure bearing-mounted tabs are connected to other flexure-bearing-mounted tabs of adjacent unit cells so that the adjacent unit cells are spaced from each other to accommodate thermal expansion of individual unit cells while maintaining a desired bulk thermal expansion coefficient of the lattice structure as a whole. | 09-19-2013 |
| 20130243998 | SANDWICH COMPONENT - The present invention relates to sandwich component and a method for producing such sandwich component. In addition to a viscoelastic layer disposed between a honeycomb-like core layer and one of two cover layers of the sandwich component a porous layer is provided which is attached the viscoelastic layer at the side of the viscoelastic layer facing away from the cover layer between which and the core layer the viscoelastic layer is disposed. The porous layer has a higher compressive strength than the viscoelastic layer. The sandwich panel may be produced by forming a corresponding layered structure including the layers of the sandwich panel and subsequently applying heat and/or pressure to said layered structure in order to produce the sandwich component. | 09-19-2013 |
| 20130260088 | HONEYCOMB PAPER - A consolidated fibrous mat comprises 20 to 50 weight percent of reinforcing fibers; and a continuous phase connecting the reinforcing fibers, comprising 50 to 70 weight percent of a polymer having a melt temperature at least 20° C. lower than the reinforcing fibers, and 5 to 10 weight percent of a binder having a melt temperature lower than the polymer; wherein the weight percent of each of the reinforcing fibers, the polymer, and the binder is based on the combined total weight of the reinforcing fibers, the polymer, and the binder. | 10-03-2013 |
| 20130260089 | BODY FORMED OF REFRACTORY MATERIAL HAVING STRESS RELIEF SLITS AND METHOD OF FORMING THE SAME - The present invention is directed to a body formed of a refractory material and a method of forming a refractory body. The body formed of a refractory material comprises a plurality of slits formed into one of its surfaces. The slits relieve thermal stress in the body and prevent cracking that would otherwise occur. In one embodiment, the invention can be a body formed of a refractory material comprising: a first surface and an opposing second surface; and a pattern of stress relief slits formed into at least one of the first and second surfaces of the body. | 10-03-2013 |
| 20130280480 | ANTI-WEAR COATING - The invention relates to an anti-wear coating, specifically for components which are subject to erosion under mechanical loading, in particular for gas turbine components, said coating comprising at least two different individual layers which preferably alternate with one another multiply and are applied to a surface of a component which is to be coated. The individual layers comprise a ceramic main layer ( | 10-24-2013 |
| 20130295321 | Multilayered Cellular Metallic Glass Structures - Multi-layered cellular metallic glass structures and methods of preparing the same are provided. In one embodiment, the cellular metallic glass structure includes at least one patterned metallic glass sheet and at least one additional sheet. The at least one patterned metallic glass sheet may include multiple sheets connected together to form a group of sheets, and the structure may include a group of sheets sandwiched between two outer sheets. The patterned metallic glass sheets may be patterned by thermoplastically forming two- and/or three-dimensional patterns in the metallic glass sheets. The metallic glass cellular structures are useful in a wide variety of applications, including but not limited to blast protection applications, energy absorption applications, structural support applications, biomedical implant applications, heat exchanger applications, thermal management applications, electrical shielding applications, magnetic shielding applications, and debris and radiation shielding for aerospace and outer space applications. | 11-07-2013 |
| 20130316129 | SILICON CARBIDE MATERIAL, HONEYCOMB STRUCTURE, AND ELECTRIC HEATING TYPE CATALYST CARRIER - A silicon carbide material according to the present invention includes a substrate containing, as a main component, silicon carbide or containing, as main components, silicon carbide and metallic silicon, and a film covering at least a portion of the surface of the substrate. The film contains, as a main component, a phase including at least four elements: lithium (Li), aluminum (Al), silicon (Si), and oxygen (O). One example of such a silicon carbide material includes a substrate having a structure in which silicon carbide particles are bonded by metallic silicon, and a lithium aluminosilicate film covering at least a portion of the surface of the silicon carbide particles. Such a silicon carbide material can be used for a DPF, an electric heating type catalytic converter, or the like. | 11-28-2013 |
| 20130316130 | HONEYCOMB STRUCTURE BODY - There is disclosed a honeycomb structure body having joining material layers of a stress relaxing function and joining strength equivalent to those of joining material layers of a conventional honeycomb structure body, and having an excellent heat shock resistance. A honeycomb structure body includes a plurality of honeycomb segments and joining material layers having a plurality of pores and joining the plurality of honeycomb segments in a state where the honeycomb segments are arranged adjacent to each other so that side surfaces of the honeycomb segments face each other. A ratio of the number of pores having a value of 1.2 or less which is obtained by dividing a maximum diameter of each of the pores by a minimum diameter of the each of the pores is 60% or more of the number of all the pores of each of the joining material layers. | 11-28-2013 |
| 20130330504 | POROUS CARBON AND METHOD OF MANUFACTURING SAME - A porous carbon that has an extremely high specific surface area while being crystalline, and a method of manufacturing the porous carbon are provided. | 12-12-2013 |
| 20130337223 | SANDWICH STRUCTURE WELDED BY HIGH-FREQUENCY INDUCTION HEATING, AND METHOD FOR MANUFACTURING SAME - According to one embodiment of the present invention, a sandwich structure welded by high-frequency induction heating comprises: a honeycomb core; a first skin sheet and a second skin sheet formed at either side of the honeycomb core, respectively; and conductors to be heated, which are arranged at one side of each of the first skin sheet and second skin sheet, and which melt the interfaces of the first skin sheet and second skin sheet by high-frequency induction heating so as to enable the first skin sheet and second skin sheet to be adhered to either side of the honeycomb core, respectively. | 12-19-2013 |
| 20130344283 | HONEYCOMB STRUCTURE - There is disclosed a honeycomb structure including: a plurality of honeycomb segments each having porous partition walls, and plugged portions arranged in open frontal areas of the predetermined cells; joining portions in which the plurality of honeycomb segments are joined; and an outer peripheral wall, and having: an aspect ratio (a long axis/a short axis) of 1.2 or more, wherein corners which are regions of the joining portions in the region of 10 mm or less from each intersection between the joining portion and the outer peripheral wall along a direction of the short axis are present in the region of 25 mm or less, and a thickness of each of the joining portions is 0.5 mm or more and 5 mm or less, and a thickness of each of the other joining portions is 1.5 mm or less. | 12-26-2013 |
| 20140004299 | CELLULAR STRUCTURE FOR DOUBLE CURVATURE PANEL | 01-02-2014 |
| 20140023821 | MAGNETIC COMPOSITE AND METHOD OF MANUFACTURING THE SAME, AND ARTICLE AND DEVICE INCLUDING THE SAME - A magnetic composite including a magnetic material; and a binder including a metallic glass, a glass frit, or a combination thereof. | 01-23-2014 |
| 20140030476 | POLYMER COMPOSITE STRUCTURE AND METHOD - An assembly including a first component having a first side and a second side opposite the first side, the first side having at least one bonding structure extending therefrom and spaced from an outer perimeter of the first component, and a second component having a first side and a second side opposite the first side, the second component thermally bonded to the first component along at least one interior interface including said bonding structure, said interface fully enclosed between the first and second components. At least a portion of at least one of the first or second components is laser transparent to allow passage of laser energy through said laser transparent portion to a laser opaque portion of the interface, said laser opaque portion configured to absorb laser energy to facilitate bonding. | 01-30-2014 |
| 20140037893 | HYDRATION INHIBITOR COATING FOR ADHESIVE BONDS - An adhesively bonded article includes a metallic substrate that has an oxide layer thereon, a phosphonate bond promoter coating on the oxide layer, an adhesive material on the bond promoter coating, and a component bonded to the metallic substrate by way of the adhesive material. | 02-06-2014 |
| 20140065350 | HONEYCOMB STRUCTURE - A honeycomb structure | 03-06-2014 |
| 20140065351 | FORMING CELLULAR MATERIAL BY MELT-STRETCHING MELT-STRETCHABLE MATERIAL - A material with a cellular structure is formed from melt-stretched granules. Granules compressed between stretching surfaces are melted to form viscous molten layers attaching ends of the granules to the surfaces. Melted central portions of the granules are stretched by moving the surfaces away from one another. A cellular structure is thus formed between the molten layers, both of which are solidified to form a solid material. A cellular material may also be formed by melting a melt-stretchable material to form a sheet of viscous molten mass formed of opposite surface layers connected by a central portion, stretching the central portion by pulling the surface layers away from one another to generate air cells randomly distributed throughout the central portion, and solidifying the cellular core and the skins formed from the central portion and the surface layers. | 03-06-2014 |
| 20140087127 | DEVICE AND METHOD FOR PRODUCING A HONEYCOMB STRUCTURE AND A HONEYCOMB STRUCTURE - The invention relates to a device for producing a honeycomb structure from strip material comprising a supply and forming device, which forms a structured strip from the strip material and additionally determines a conveying speed of the structured strip, and a stop device comprising a feed channel, wherein the stop device is disposed downstream of the forming device such that the structured strip can be supplied to the feed channel, and wherein the honeycomb structure comprises a stop edge, which runs parallel to the feed channel, and wherein the stop device comprises a stop and stop means, which are designed in a movable manner such that the structured strip can be connected to a stop edge of the honeycomb structure. | 03-27-2014 |
| 20140087128 | HONEYCOMB STRUCTURE - There are disclosed a honeycomb structure hardly generates ring cracks; and a honeycomb structure | 03-27-2014 |
| 20140106114 | Artwork Surface and Method of Use - The present invention relates, in general, to a novel artwork surface and, in particular, to an ultra lightweight dispersed solid artwork surface and methods of creating artwork structures. Techniques are described herein that are capable of creating an innovative artwork structure. For example, a method of preparing a dispersed solid artwork surface, applying said medium to said dispersed solid artwork surface, finishing said dispersed artwork surface to create an artwork structure, and displaying said artwork structure. | 04-17-2014 |
| 20140106115 | Structure of Handgrip Cushion Pad - A handgrip cushion pad includes two ciliated bodies that are made of an elastic material and each have a surface on which a plurality of uniaxial pouches is formed to be arranged in an alternate form. The uniaxial pouches of the first ciliated body have a height that is greater than a height of the uniaxial pouches of the second ciliated body. The second ciliated body includes through holes formed therein to respectively correspond to the uniaxial pouches of the first ciliated body. To assemble, the two ciliated bodies are attached to each other with the pouched surfaces facing each other and top ends of the uniaxial pouches of the first ciliated body penetrating through and projecting beyond the through holes. The top ends of predetermined ones of the pouches are each provided with an expanded flange, which is forced through the through hole to form a retention engagement therewith. | 04-17-2014 |
| 20140113104 | FIBER-RESIN COMPOSITE SHEET AND ARTICLE COMPRISING THE SAME - A fiber-resin composite sheet comprises a reinforcing substrate of high tenacity fibers and a resin coated onto or into the substrate, the resin comprising a first thermoplastic polymer and a second thermoplastic polymer wherein, (i) the first and second polymers form a two phase blend, (ii) the first polymer is thermoplastic has a melting point of from 75 to 400 degrees C. and forms a continuous or co-continuous phase with the second polymer, (iii) the second polymer is particulate having an effective diameter of from 0.01 to 15 micrometers, has a melting point of from 25 to 350 degrees C. and is dispersed in the continuous or co-continuous phase of the first polymer and (iv) the first polymer comprises from 35 to 99 weight percent of the combined weight of first and second polymers in the blend, | 04-24-2014 |
| 20140113105 | STRUCTURE AND METHOD OF PRODUCING THE SAME - [Object] To provide a structure of a novel shape and a method of producing it. | 04-24-2014 |
| 20140113106 | METHOD OF MANUFACTURING HONEYCOMB STRUCTURE AND HONEYCOMB STRUCTURE - A honeycomb structure mainly composed of cordierite and obtained by forming and firing a forming material containing a layered clay mineral whose layer charge (X) is 0.2| 04-24-2014 | |
| 20140120303 | High-Quality Flame-Retardant Decorative Finish for Interior Panels - A high-quality, fire-resistant, decorative finish for panels made of composite material, such as aircraft interior panels. Starting with a flat or complex contoured panel, a flame-retardant filler primer is applied to the panel surface. This filler primer is then sanded to a very smooth solid surface. In a separate process, a polymeric film is printed with a desired pattern or image. The polymeric film is then bonded to the primed panel surface using an adhesive. The non-printed side of the polymeric film is bonded to the panel. A thin highly durable polymeric coating (clear or tinted) is then applied to the exposed printed side. | 05-01-2014 |
| 20140120304 | INSULATION MATERIAL - A flexible or rigid heat-insulation material consisting of a sheet of at least one layer of closed-cell gas bubbles 1/16 inch to 1 inch in size filled with a gas selected from helium, argon, neon, krypton, xenon, carbon dioxide, and chlorodifluoromethane, and mixtures thereof. At least one heat reflective layer of aluminum film is adhesively attached to the layer of gas bubbles or an aluminum film is vapor-deposited on the layer of gas bubbles. | 05-01-2014 |
| 20140127452 | HONEYCOMB CORE, METHOD OF PRODUCING A HONEYCOMB CORE, AND SANDWICH PANEL COMPRISING A HONEYCOMB CORE - A honeycomb core having a lattice structure which includes a resin-impregnated matrix, a method for producing such a honeycomb core, a sandwich panel having such a honeycomb core, and use of such a honeycomb core or such a sandwich panel in automobile construction. The matrix is impregnated inhomogeneously with the resin. | 05-08-2014 |
| 20140127453 | SEALED HONEYCOMB STRUCTRURE - A sealed honeycomb structure may include porous walls dividedly forming inlet cells and outlet cells extending from an end surface of an inlet side to an end surface of an outlet side, an outlet side sealing portion, and an inlet side sealing portion, wherein at least one outlet cell is a reinforced cell, where a reinforced part for reinforcing the outlet cell is formed at at least one corner portion at which the walls on a cross-section vertical to an extending direction of the cell cross each other, and wherein the inlet cell is a non-reinforced cell where the reinforced part is not formed at all the corner portions at which the walls on the cross-section vertical to the extending direction of the cell cross each other. | 05-08-2014 |
| 20140127454 | Hollow Body Arrangement and Method for Producing Same - A building element | 05-08-2014 |
| 20140134392 | COMPOSITE STONE PANELS - A composite stone panel can comprise a stone slab. A partially metallic panel backer is coupled to the stone slab and can further comprise a core material layer, a first interface layer disposed on a first surface of the core material layer, and a second interface layer disposed on a second surface of the core material layer opposite the first metal interface layer. The stone slab can further comprise a length greater than 1.2 meters (m), a width greater than 0.6 m, and a thickness in a range of 0.2-1.5 centimeters (cm). The core material layer can comprise a thickness greater than 3.75 millimeters and can further comprise polyethylene and optional fibers. The first and second interface layers can comprise a thickness of aluminum in a range of 0.21 millimeters (mm) to 0.30 mm. Accordingly, the composite stone panel can comprises a thickness in a range of 0.6-3.0 cm. | 05-15-2014 |
| 20140134393 | STRUCTURE, MOLDED ARTICLE, AND METHOD FOR MANUFACTURING SAME - A structure | 05-15-2014 |
| 20140147621 | HONEYCOMB STRUCTURE COMPRISING A MULTILAYER CEMENT SKIN - Disclosed is a ceramic honeycomb structure comprising a honeycomb body and a multilayered outer layer formed of a thick core layer applied and rapidly dried and a thin clad layer dried more gently to form a crack free dual skin layer. The core layer may have properties that are closer to those of the ceramic honeycomb body in service than the clad layer that may provide a tough outer shell to withstand handling and assembly. | 05-29-2014 |
| 20140147622 | SANDWICH-TYPE, STRUCTURAL, COMPOSITE PANEL HAVING A PATTERN OF DEPRESSIONS FORMED AT A LOWER OUTER SURFACE THEREOF AND STIFFENING SUPPORTS RECEIVED AND RETAINED THEREIN - A sandwich-type, structural, composite panel having a pattern of depressions formed at a lower outer surface thereof and stiffening supports received and retained therein is provided. The panel includes a first outer layer having a first outer surface, a second outer layer having a second outer surface and a core positioned between the outer layers and having a large number of cavities. The outer layers are bonded to the core by press molding. Crushed portions of the panel having a reduced thickness form the pattern of depressions at the second outer surface of the second outer layer. The stiffening supports are bonded or joined to the second outer layer within the pattern of depressions. The stiffening supports are sized, shaped and arranged within the pattern of depressions to provide the panel with strength to resist deflection from a load at various positions and orientations at the first outer surface. | 05-29-2014 |
| 20140154460 | COMPRESSION-MOLDED COMPOSITE COMPONENT HAVING A SANDWICH STRUCTURE AND HAVING INTEGRALLY FORMED STRENGTHENING STRUCTURES - A compression-molded, composite component having a sandwich structure and having integrally formed strengthening structures is disclosed. The component includes a first outer layer having an outer surface, a second outer layer, and a core positioned between the outer layers and having a large number of cavities. The outer layers are bonded to the core by press molding. Portions of at least one of the outer layers are sized, shaped and arranged laterally adjacent to each other in a pattern to provide the component with strength to resist deflection from a load at various positions and orientations at the outer surface. | 06-05-2014 |
| 20140154461 | SANDWICH-TYPE COMPOSITE COMPONENT HAVING IMPRINTED 3-D STRUCTURES WHICH PROVIDE AT LEAST ONE PATTERN AT AN OUTER SURFACE OF THE COMPONENT - A sandwich-type composite component having imprinted 3-D structures which provide at least one pattern at an outer surface of the component is provided. The component includes a first outer layer having an outer surface, a second outer layer and a core positioned between the outer layers and having a large number of cavities. The outer layers are bonded to the core by press molding. The first outer layer comprises an integral, unitary structure including 3-D structures imprinted by the press molding. The 3-D structures are sized, shaped and arranged in one or more patterns at the outer surface. The one or more patterns may form a textural surface finish, a logo or indicia such as instructions at the outer surface. The component may be a vehicle interior component such as a vehicle load floor component. | 06-05-2014 |
| 20140170372 | GRID TYPE FIBER COMPOSITE STRUCTURE AND METHOD OF MANUFACTURING SUCH GRID TYPE STRUCTURE - The invention is related to a grid type fiber composite structure ( | 06-19-2014 |
| 20140170373 | GRID TYPE ELEMENT OF OPEN POLYGONAL CELLS - A grid type element ( | 06-19-2014 |
| 20140170374 | Core of Sheet Structural Material and Assembly Process - A core of sandwich structural material comprising an assembly of several sheets comprising a first sheet and a second sheet that are provided on one of the faces thereof with of periodically distributed polygonal-based pyramid frustums, the superposition of these sheets in the thickness direction forming a three-dimensional network of hollow tubular channels which extend from one face of one sheet to one face of another sheet along a channel direction, and that are each defined by a peripheral wall, this peripheral wall being provided both by the first sheet and by the second sheet. | 06-19-2014 |
| 20140186576 | INSULATING MATERIAL CONTAINING NANOCELLULOSE - A nonwoven web of unmodified or cyanoethylated nanocellulose was found to have greater strength than kraft paper after immersion in oil at high temperature, making it useful as an insulation material for transformers. A mixture of nanocellulose and polymetaphenylene isophthalamide has further improved properties for use as an insulating material. | 07-03-2014 |
| 20140205794 | HONEYCOMB STRUCTURAL BODY - A honeycomb structural body has a central part, an outer-circumferential part and a boundary-partition wall. The central part has central basic-cell walls and central reinforced-cell walls. The outer-circumferential part has outer-circumferential basic-cell walls and outer-circumferential reinforced-cell walls. The body satisfies R1/P1≧0.5, R2/P2≧0.5, T10≧T20, T11>T21, T3>T10, T3>T20, T3≧T11 and T3>T21, where R1 indicates a distance from the boundary-partition wall toward a radially-inward direction of the body, P1 indicates an average cell-pitch in the central part, R2 indicates a distance from the boundary-partition wall toward a radially outward direction of the body, P2 indicates an average cell-pitch in the outer-circumferential part, T10 indicates an average-thickness of the central basic-cell walls, T20 indicates an average-thickness of the outer-circumferential basic-cell walls, T11 indicates an average-thickness of the central reinforced-cell walls, T21 indicates an average-thickness of the outer-circumferential reinforced-cell walls, and T3 indicates an average-thickness of the boundary-partition wall. | 07-24-2014 |
| 20140205795 | THREE DIMENSIONAL NEGATIVE POISSON'S RATIO SPACER KNITTED FABRIC AND METHOD FOR MAKING THE SAME - This present application relates to a three dimensional negative Poisson's ratio spacer knitted fabric and a method for making the same; the fabric includes a first surface layer fabric, a second surface layer fabric, and a spacer yarn layer connecting the first surface layer fabric with the second surface layer fabric, both the first surface layer fabric and the second surface layer fabric are bi-dimensional structures having the negative Poisson's ratio effects; the method is to compress and/or stretch a three dimensional mesh spacer knitted base fabric along one or two plane directions to form a structures having the negative Poisson's ratio effects. The advantages of the present application include low making cost, simple operation method, significant negative Poisson's ratio effects, good elastic recovery, and high practical application value. | 07-24-2014 |
| 20140212622 | Multi-Segmented Structured Ceramic Packing - A multi-segmented monolith (MSM) which can be used as a structured packing in mass-transfer and catalytic operations is disclosed. The MSM comprises a series of longitudinally attached segments. The length of each segment is between 0.2 to 5 inches. Each segment has flow passages which extend from the inlet flow face to the outlet flow face. The segments are located such that the outlet of a flow passage on a segment is in flow communication with the inlet of a flow passage on an adjacent attached segment. The segments are attached to each other either in the green state or with an adhesive, such as sodium silicate. Alternately, the segments are attached to each other by a mechanical means, such as a tie-rod or a dowel pin. The MSM further includes a spacer means between adjacent segments. A plurality of MSMs are further assembled into a Compound MSM (CMSM). | 07-31-2014 |
| 20140220294 | CATALYST SUPPORTING BODY AND METHOD OF MANUFACTURING THE SAME - A catalyst supporting body has a porous honeycomb base body having a porosity within a range of 40 to 60 vol. %. The body has a plurality of cells partitioned by cell walls arranged in a lattice-like shape. A coated catalyst layer made of a porous body having a void fraction of void spaces within a range of 53 to 63 vol. % is particularly supported on surfaces of the cell walls and in pores formed in the cell walls by a filling rate of not less than 40 vol. %. In an immersing step of a manufacturing method, a combination of a kind of catalyst slurry and the porous honeycomb base body is selected so that a cumulative-frequency at an intersection point between a pore distribution map and a particle size distribution map becomes not less than 80%. The pore distribution map indicates a relationship between pore sizes of pores in the porous honeycomb base body and a cumulative-frequency of the pores. The particle size distribution map indicates a relationship between particle size in the catalyst slurry and a cumulative-frequency of the particles. | 08-07-2014 |
| 20140242327 | FIBER-REINFORCED CERAMIC COMPOSITE MATERIAL HONEYCOMB AND METHOD FOR PREPARING THE SAME - Disclosed herein is a fiber-reinforced ceramic composite material honeycomb, including: a plurality of inner tubes, each of which is made of a fiber-reinforced ceramic composite material; and an outer shell which is made of a fiber-reinforced ceramic composite material and which surrounds the plurality of inner tubes. | 08-28-2014 |
| 20140272275 | MICRO-TRUSS MATERIALS HAVING IN-PLANE MATERIAL PROPERTY VARIATIONS - A micro-truss sheet having material properties varying across the sheet. The sheet may include a plurality of truss members intersecting at nodes. The diameter of the truss members at one point in the sheet may differ from the diameter of the truss members at another point in the sheet. In one embodiment the spacing between adjacent truss members may be different in one part of the sheet from the spacing between adjacent truss members in another part of the sheet. | 09-18-2014 |
| 20140272276 | Cellular Ceramic Article and Method For Manufacturing The Same - A method and apparatus to treat a dried unfired article comprising a ceramic precursor composition substantially held together by a binder, to be resistant to binder soluble solvent based processing. The method includes depositing a fluid on the article surface, and polymerizing the deposited fluid to form a polymer thin layer on the surface. The fluid may be an aerosol, a vapor, a fog, a mist, a smoke, or combinations thereof. An apparatus to perform the method and an article resistant to binder soluble solvent based processing are also provided. The article can be an unfired honeycomb body that includes a dried composition of ceramic precursor substantially held together by a binder and a layer disposed on a surface of the unfired honeycomb body. The surface to be exposed in the green state to a binder soluble solvent and the layer protects the binder from solubilization by the solvent. | 09-18-2014 |
| 20140272277 | CONSTRAINED MICROLAYER CELLULAR MATERIAL WITH HIGH STIFFNESS AND DAMPING - Composite materials with high damping and high stiffness at relatively low density. These materials include three-dimensional structures of interconnected ligaments, which have multiple concentric layers alternating between stiff constraining layers and soft damping layers, so that bulk deformation of the structure results in high local shear strain and correspondingly high bulk damping. | 09-18-2014 |
| 20140295132 | PRODUCTION METHOD OF CERAMIC HONEYCOMB STRUCTURE, AND CERAMIC HONEYCOMB STRUCTURE - A method for producing a ceramic honeycomb structure comprising a ceramic honeycomb body having large numbers of longitudinal cells partitioned by porous cell walls having porosity of 50% or more, and a peripheral wall formed on a peripheral surface of the ceramic honeycomb body, comprising the steps of extruding moldable ceramic material to form a honeycomb-structured ceramic green body; machining a peripheral portion of the green body or a sintered body obtained from the green body to remove part of cell walls in the peripheral portion to obtain a ceramic honeycomb body having longitudinal grooves on a peripheral surface; applying colloidal metal oxide to a peripheral surface of the ceramic honeycomb body and drying it, and then applying a coating material comprising ceramic aggregate having an average particle size of 1 μm or more to form the peripheral wall. | 10-02-2014 |
| 20140302277 | Panel and Use of Such a Panel As A Scaffolding Board or a Building Panel - The present invention relates to a panel comprising two parallel skin plates made of wood or a wood material, between which ribs extend for stiffening the panel, wherein the ribs are at least substantially made of wood or a wood material. The present invention further relates to the use of such a panel as a scaffolding board or a construction element and to scaffolding provided with such panels. | 10-09-2014 |
| 20140314987 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and binder ingredient such that raw material paste including the titania particles, alumina particles and binder ingredient is prepared, forming a body made of the raw material paste and having a honeycomb structure such that the body has the honeycomb structure having through-holes extending in the longitudinal direction of the body and partition portions between the through-holes, positioning on a base having zirconia granules the body made of the raw material paste and having the honeycomb structure such that the zirconia are interposed between the body and the base, and sintering the body made of the raw material paste and having the honeycomb structure on the base with the zirconia granules interposed between the body and the base such that a ceramic body having the honeycomb structure is formed on the base with the zirconia granules. | 10-23-2014 |
| 20140314988 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and binder ingredient such that raw material paste including the titania particles, alumina particles and binder ingredient is prepared, forming a body made of the raw material paste and having a honeycomb structure such that the body has the honeycomb structure having through-holes extending in the longitudinal direction of the body and partition portions between the through-holes, positioning the body on a base such that one end surface of the body in the longitudinal direction faces the base and a space is formed between the base and the end surface of the body, and sintering under oxygen atmosphere the body on the base with the space between the base and the body such that a ceramic body having the honeycomb structure is formed on the base. | 10-23-2014 |
| 20140322484 | Shock Resistant Member - A shock resistant member which is lightweight and has a high degree of freedom in shape, and excellent shock resistance, is provided. | 10-30-2014 |
| 20140335306 | 3D Fiber Composite - A composite having a core containing a cellular structure, reinforcing fibers, an upper face sheet, and a lower face sheet is provided. The cellular structure is a honeycomb structure containing strips of carrier material arranged in an x direction in an x-y plane, adhered together, and expanded in the x direction after adhesion. The reinforcing fibers are externally bonded onto the outer walls of each of the cells of the cellular structure in a z direction. The upper face sheet and the lower face sheet are configured to be bonded to the upper portion and the lower portion of the reinforcing fibers that extend outwardly from the upper edges and the lower edges of the cells of the cellular structure respectively, thereby establishing a three dimensional continuity of the reinforcing fibers between a surface of contact between the core, the upper face sheet, and the lower face sheet. | 11-13-2014 |
| 20140342117 | HEAT CONDUCTIVE ADHESIVE FILM, METHOD FOR MANUFACTURING THE SAME AND OLED PANEL - A method for manufacturing a heat conductive adhesive film includes: forming a non-solid heat conductive adhesive layer with cured particles on a substrate; forming several bumps on the non-solid heat conductive adhesive layer while performing curing, so as to yield the heat conductive adhesive film with several bumps. A heat conductive adhesive film and an OLED panel are provided. Several bumps are formed on a flat surface of the heat conductive adhesive film, thus increasing the surface area of the heat conductive adhesive film such that heat from the heat generating unit can be duly discharged. | 11-20-2014 |
| 20140356570 | HONEYCOMB ELEMENT WITH REINFORCED CORNERS - A monolithic honeycomb element includes a collection of adjacent ducts of mutually parallel axes separated by walls made of a porous material, the element having, in transverse cross section, a polygonal, notably quadratic cross section delimited by exterior wall elements, wherein at least one corner of the polygon, has, along the bisector of the angle at the corner, an additional thickness, such that the total thickness of the external wall, likewise measured along the bisector of the angle at the corner, is greater than the mean thickness of the exterior walls by a factor of at least 1.43, the additional thickness being obtained at least in part by an additional quantity of porous material on the external face of the corner. | 12-04-2014 |
| 20140363616 | HONEYCOMB STRUCTURE - There is disclosed a honeycomb structure in which a ring crack is not easily generated. A honeycomb structure includes a honeycomb substrate, and a bulging portion continuously or intermittently surrounding, in a ring shape, at least a part of an outer periphery of the honeycomb substrate. The outer periphery of the honeycomb substrate has one or a plurality of stress relaxing portions which are crevices each having an open end in the surface over a region of −5 to +10 mm or less from a reference bonded portion to a tapered surface, and a total of lengths of all the stress relaxing portions is 3% or more of a circumferential length of the honeycomb substrate. | 12-11-2014 |
| 20140363617 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and a binder such that a raw material paste containing the titania particles, the alumina particles and the binder is prepared, forming a body made of the raw material paste and having the honeycomb structure, and sintering the body having the honeycomb structure such that a ceramic body having the honeycomb structure and made of aluminum titanate is formed. The kneading includes combining the binder, a titania powder containing the titania particles and an alumina powder containing the alumina particles, and the titania powder includes sodium in an amount of from 200 ppm to 1,000 ppm with respect to the titania powder in a weight ratio based on conversion from Na | 12-11-2014 |
| 20140363618 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and a binder such that a raw material paste containing the titania particles, the alumina particles and the binder is prepared, forming a body made of the raw material paste and having the honeycomb structure, and sintering the body having the honeycomb structure such that a ceramic body having the honeycomb structure and made of aluminum titanate is formed. The kneading includes combining the binder, a titania powder containing the titania particles and an alumina powder containing the alumina particles, and the titania powder includes potassium in an amount of from 100 ppm to 600 ppm with respect to the titania powder in a weight ratio based on conversion from K | 12-11-2014 |
| 20140363619 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and a binder such that a raw material paste containing the titania particles, the alumina particles and the binder is prepared, forming a body made of the raw material paste and having the honeycomb structure, and sintering the body having the honeycomb structure such that a ceramic body having the honeycomb structure and made of aluminum titanate is formed. The kneading includes combining the binder, a titania powder containing the titania particles and an alumina powder containing the alumina particles, and the titania powder includes magnesium in an amount of 500 ppm or less with respect to the titania powder in a weight ratio based on conversion from MgO. | 12-11-2014 |
| 20140363620 | METHOD FOR MANUFACTURING ALUMINUM-TITANATE-BASED CERAMIC HONEYCOMB STRUCTURE - A method for manufacturing a ceramic honeycomb structure includes kneading titania particles, alumina particles and a binder such that a raw material paste containing the titania particles, the alumina particles and the binder is prepared, forming a body made of the raw material paste and having the honeycomb structure, and sintering the body having the honeycomb structure such that a ceramic body having the honeycomb structure and made of aluminum titanate is formed. The titania particles are secondary titania particles each comprising primary titania particles aggregated such that the secondary titania particles have a mean volume particle diameter in the range of from 5 μm to 20 μm, and the alumina particles have a mean volume particle diameter in the range of from 2 μm to 5 μm. | 12-11-2014 |
| 20140370232 | POROUS MATERIAL, HONEYCOMB STRUCTURE, AND PRODUCTION METHOD FOR POROUS MATERIAL - There is disclosed a porous material containing aggregates; and a composite binding material which binds the aggregates to one another in a state where pores are formed and in which mullite particles that are reinforcing particles are dispersed in cordierite that is a binding material, and a content of metal silicon is smaller than 15 mass %. Preferably, to a total mass of the aggregates, the composite binding material and the metal silicon, a lower limit value of a content of the composite binding material is 12 mass %, and an upper limit value of the content of the composite binding material is 50 mass %. Preferably, to the total mass, a lower limit value of a content of the mullite particles is 0.5 mass %, and an upper limit value of the content of the mullite particles is 15 mass %. A porous material having a high thermal shock resistance is provided. | 12-18-2014 |
| 20140370233 | POROUS MATERIAL AND HONEYCOMB STRUCTURE - There are disclosed a porous material having a high thermal shock resistance and a honeycomb structure. The porous material contains main aggregates and auxiliary aggregates as aggregates, the main aggregates are silicon carbide particles, the auxiliary aggregates are at least either of mullite particles or alumina particles, the aggregates are bound to one another via a binding phase, so as to form pores, and the binding phase is at least one of an amorphous phase and a cordierite phase, and a porosity is from 40 to 90%. Furthermore, the honeycomb structure is constituted of such a porous material, and includes partition walls defining and forming a plurality of cells extending from one end face to the other end face. | 12-18-2014 |
| 20150017383 | PYRAMIDAL KAGOME STRUCTURE AND ITS FABRICATING METHOD - The present invention relates to a pyramidal kagome structure and more particularly, to a pyramidal kagome structure having a broaden contact area with a plate member and its fabricating method. According to the invention, a lattice mesh is formed with a plate so that continuous and mass-production is permitted and the produced pyramidal truss structures are assembled into a pyramidal kagome truss structure by combining the apexes of the pyramidal truss structures, whereby improved mechanical strength is obtained. Furthermore, the connecting of the pyramidal truss structures is facilitated due to the broadened contact area with the top and bottom plate member and an improved stability after combining is obtained. | 01-15-2015 |
| 20150024163 | FORCE SPUN SUB-MICRON FIBER AND APPLICATIONS - A process of forming a non-woven web including spinning continuous polymeric filaments including one selected from a poly(phenylene ether) component, a poly(phenylene ether)-polysiloxane block copolymer, and combinations thereof. The filaments can have a length to diameter ratio that is more than 1,000,000, and a diameter ranging from 50 nanometers to 5 microns. The spinning can include passing a polymer through a spinneret having a plurality of orifices in a non-electrospinning environment. The process can further include chopping the plurality of continuous filaments and obtaining a plurality of chopped nano-fibers and forming the nano-fibers into a nonwoven web. The spinning can be conducted at a rate of at least 300 grams/hour/spinneret. | 01-22-2015 |
| 20150030806 | SANDWICH TYPE LOAD BEARING PANEL - A sandwich type load bearing panel ( | 01-29-2015 |
| 20150037531 | METHOD FOR MAKING POROUS MULLITE-CONTAINING COMPOSITES - Porous aluminum-containing ceramic bodies are treated to form acicular mullite crystals onto the surfaces of their pores. The crystalsare formed by contacting the body with a fluorine-containing gas or a source of both fluorine and silicon atoms to form fluorotopaz at the surface of the pores, and then decomposing the fluorotopaz to form acicular mullite crystals. This process allows the surface area of the ceramic body to be increased significantly while retaining the geometry (size, shape, general pore structure) of the starting body. The higher surface area makes the body more efficient as a particulate filter and also allows for easier introduction of catalytic materials. | 02-05-2015 |
| 20150044415 | Articles of Cellulose and Methods of Forming Same - The present invention follows from a number of recent discoveries relating to cellulose fibrils and crystals. Unique properties of these compositions provide for novel structural materials that exhibit extremely high strength per unit of mass. Structures and articles first taught herein may be formed by computer numerically controlled processing, extruding, molding, shearing, weaving, and various additive manufacturing techniques, as well as by other more traditional procedures. These structures and articles may be used as a skin or core in composite constructions. These structures and articles can be used as free standing shells or panels. They may be made into intricate forms, particularly in three spatial dimensions with sonic elements in tension and some elements in compression to realize high performance functionalities. Cellulose matter is a dominate part of these compositions, making the articles fully biodegradable. One can make entirely renewable and nontoxic products depending on the presence of necessary additives. | 02-12-2015 |
| 20150064394 | COMPUTING DEVICE COVER - Techniques for forming portions of a computing device are described herein. The techniques include a method including forming a first portion of a computing device, the first portion composed of a metal. A nanostructure layer of the first portion is formed, and a second portion of the computing device is formed, wherein the second portion composed of a polymer. The method includes coupling the first portion to the second portion by injection molding the polymer of the second portion onto the nanostructure layer. | 03-05-2015 |
| 20150064395 | Formed Articles Comprising Carbon And Natural Fibers, Methods Of Manufacture And Use Thereof - A fiber mat comprising a first fiber layer, the first fiber layer formed by combining 45-55% by weight of synthetic polymer fibers; 35-45% by weight of natural fibers; and 5-15% by weight of carbon fibers, as well as a formed article comprising a molded substrate formed from a fiber mat, the fiber mat comprising a first fiber layer formed by combining 45-55% by weight of synthetic polymer fibers; 35-45% by weight of natural fibers; and 5-15% by weight of carbon fibers. | 03-05-2015 |
| 20150072103 | LINKED ARRAYS OF VOID CELLS - Implementations described and claimed herein include methods of manufacturing related to a spaced array of individually formed void cells, which are linked together. The void cells are protruding, resiliently compressible cells manufactured by thermoforming, extrusion, injection molding, laminating, and/or blow molding processes. The individual void cells are molded and arranged in an array. A separate, porous binding layer is attached to the individual void cells in the array. In one implementation, two arrays may each comprise of linked individually formed void cells, wherein each array is aligned with the other array, and linked individually formed void cells of one array are positioned opposite the linked individually formed void cells of the other array, sharing the same binding layer. In another implementation, multiple arrays can be stacked upon one another. In another implementation, the linked individually formed void cells have substantially different force-deflection characteristics. | 03-12-2015 |
| 20150086748 | HONEYCOMB STRUCTURE - In a cross section of a honeycomb structure body, shape of the cells is polygonal, and the honeycomb structure body is constituted so that thickness of partition walls in circumferential region is larger than in central region. In the cross section, when among the cells arranged on a first line segment passing the center of gravity and extending in a direction perpendicular to the partition walls each constituting one side of the cells, cell pitch of the respective five or less cells each arranged on the first line segment toward each of the central region side and the circumferential region side from boundary between the central region and the circumferential region has a size of 70% or more and 95% or less to cell pitch in the extending direction of the first line segment of the cells in the central region of the honeycomb structure. | 03-26-2015 |
| 20150104605 | HONEYCOMB CORE STRUCTURE - A thermoplastic honeycomb core structure comprises from 40 to 90 weight percent of an aliphatic polyamide polymer and from 10 to 60 weight percent of discontinuous fibers distributed evenly throughout the polymer wherein (i) the honeycomb is free of fused cell walls, (ii) the fibers are carbon, glass, para-aramid or a combination thereof, and (iii) the fibers have a length of from 0.5 to 10 mm. | 04-16-2015 |
| 20150104606 | TRANSLUCENT COMPOSITE STONE PANELS - A translucent composite stone panel can comprise a translucent stone slab of onyx or travertine. The composite stone panel can comprise a length greater than or equal to 1.2 m, a width greater than or equal to 0.6 m, and a thickness in a range of 0.2-1.5 cm. The translucent stone slab can further comprise a length greater than or equal to 2.4 m and a width greater than or equal to 1.2 m. The translucent composite stone panel can further comprise a translucent honeycomb panel backer comprising a length greater than or equal to 1.2 m, a width greater than or equal to 0.6 m, a thickness in a range of 0.2-1.5 cm that is coupled to the translucent stone slab. The translucent honeycomb panel backer can further comprises a length greater than or equal to 2.4 m and a width greater than or equal to 1.2 m. | 04-16-2015 |
| 20150110998 | GLASS-CERAMICS SUBSTRATES FOR GRAPHENE GROWTH - An insulating glass-ceramic substrate for synthesizing graphene includes discrete, crystalline, nanophase metallic regions capable of catalyzing graphene growth. The nanophase regions may be formed by thermal treatment of a glass-ceramic substrate containing the corresponding metal oxide. Single layer and double layer graphene are prepared on the modified glass-ceramic substrate in a vacuum chemical vapor deposition (CVD) process from hydrocarbon precursors. The graphene-coated glass-ceramic substrate is electrically conductive. | 04-23-2015 |
| 20150125653 | COMPOSITION FOR EXTRUSION-MOLDED BODIES - A composition for extrusion-molded bodies which comprises
| 05-07-2015 |
| 20150290574 | Honeycomb Body Made Of Ceramic Material - A honeycomb body of ceramic material for use in installations for cleaning and/or regenerating gases, comprising a prismatic body, which is penetrated by many rectilinear gas-flow channels parallel to one another, which discharge into both face ends of the honeycomb body, wherein the honeycomb body ( | 10-15-2015 |
| 20150328845 | MANUFACTURE OF A RESIN INFUSED ONE-PIECE COMPOSITE TRUSS STRUCTURE - A composite truss structure may have a first facesheet, a second facesheet, and a plurality of truss elements joined with the first facesheet and the second facesheet at nodes to form a one-piece structure. The composite truss structure may be formed by a method comprising preparing a dry fabric mold by: 1) placing a first dry fabric layer on a tool, 2) placing a first layer of fabric-loaded mandrels on the first dry fabric layer, 3) placing a second layer of the fabric-loaded mandrels on the first layer of fabric-loaded mandrels, and 4) placing a second dry fabric layer over the fabric-loaded mandrels. The method may further comprise infusing the dry fabric mold with a resin, and curing the resin to provide the nonflexible composite truss structure. | 11-19-2015 |
| 20150336350 | Sandwich Component and Method for Producing a Sandwich Component - A sandwich component and method of producing the sandwich component are provided, wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced thermoplast material having greater resistance to a certain solvent and, fused therewith, an inner layer made of a thermoplast material having lower resistance to the solvent. The core has outer layers, each of which is formed from a thermoplast material having lower resistance to the solvent, and an inner structure, which is formed entirely or partially from a thermoplast material having greater resistance to the solvent. The inner layers of the cover layers were each fused with one of the outer layers of the core with the use of the solvent. | 11-26-2015 |
| 20150336352 | Sandwich Component and Method for Producing a Sandwich Component - A sandwich component and method of producing the sandwich component are provided wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced high-melting-point thermoplast material and, fused therewith, an inner layer made of a low-melting-point thermoplast material. The core has outer layers, each of which is formed from a low-melting-point thermoplast material, and an inner structure, which is formed entirely or partially from a high-melting-point thermoplast material. The inner layers of the cover layers were each fused with one of the outer layers of the core. | 11-26-2015 |
| 20150367335 | CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD - A ceramic honeycomb structure comprising large numbers of cells partitioned by porous cell walls, the cell walls having (a) porosity of 50-80%, and when measured by mercury porosimetry, (b) a median pore diameter being 25-50 μm, (c) (i) a cumulative pore volume in a pore diameter range of 20 μm or less being 25% or less of the total pore volume, (ii) a cumulative pore volume in a pore diameter range of more than 20 μm and 50 μm or less being 50% or more of the total pore volume, and (iii) a cumulative pore volume in a pore diameter range of more than 50 μm being 12% or more of the total pore volume. | 12-24-2015 |
| 20150377109 | HONEYCOMB STRUCTURE BODY AND METHOD OF DESIGNING HONEYCOMB STRUCTURE BODY - A honeycomb structure body has main cells having a tubular shape and main cell walls. Each main cell is surrounded by the main cell walls. A virtual base structure body has base cell walls and base cells. The honeycomb structure body has an improved structure obtained by modifying a structure of the virtual base structure body. Each base intersecting point, at which base cell walls intersect, is determined by a polar coordinate (r, θ) using a radius vector r and a deflection angle θ. Each main intersecting point is formed on a polar coordinate (r′, θ) using the deflection angle θ and a main radius vector r′ which is obtained by multiplying the radius vector r and a constant magnification without changing the deflection angle θ. A cell density varying section varies its cell density and is formed in at least a part of the honeycomb structure body. | 12-31-2015 |
| 20160009033 | Method and Resulting Product of Thermoplastic Material Comprising a Fibre Reinforcement | 01-14-2016 |
| 20160046098 | DUAL LAYER SANDWICH FOR THERMAL MANAGEMENT - A thermal protection system including a plurality of layers. A first layer includes a passive insulation material. A second layer includes a phase change insulation material. A third layer is positioned between the first layer and the second layer to separate the passive insulation material from the phase change insulation material. A structural system extends through the first layer, the second layer, the third layer, or a combination thereof. | 02-18-2016 |
| 20160046531 | JOINED BODY AND METHOD FOR PRODUCING THE SAME - A joined body | 02-18-2016 |
| 20160067941 | CONSTRAINED MICROLAYER CELLULAR MATERIAL WITH HIGH STIFFNESS AND DAMPING - Composite materials with high damping and high stiffness at relatively low density. These materials include three-dimensional structures of interconnected ligaments, which have multiple concentric layers alternating between stiff constraining layers and soft damping layers, so that bulk deformation of the structure results in high local shear strain and correspondingly high bulk damping. | 03-10-2016 |
| 20160076179 | HONEYCOMB STRUCTURE MADE OF A NON-WOVEN MADE OF RECYCLED CARBON FIBERS - A honeycomb structure comprising carbon-fiber non-woven, sandwich structure comprising the said honeycomb structure, and process for the production of the said honeycomb structure. | 03-17-2016 |
| 20160082148 | FILM - Disclosed is a film which is able to suppress agglutination by being continuously adhered to an adhesion target portion in a biological body while suppressing a position shift. A film includes an adhesive and an adhesion inhibiting layer. The adhesive layer absorbs and maintains a liquid in a plurality of pores which are opened in one film surface and has a capillary force for adhering the adhesive layer to a first-cell group. The adhesive layer is formed of a biodegradable polymer. The adhesion inhibiting layer configures the other film surface, and inhibits adhesion between a second-cell group which is different from the first-cell group and the adhesive layer. In the adhesive layer, the pore is formed not to be penetrated in a thickness direction of the film, and thus the first-cell group and the second-cell group are separated into the one film surface side and the other film surface side. | 03-24-2016 |
| 20160083072 | AIRCRAFT CABIN PRESSURE REGULATING SUBFLOOR - An aircraft cabin subfloor construction has flow paths through the subfloor that vent air pockets trapped beneath an air impermeable floor mat on the subfloor where, due to a difference in pressure in the air pockets trapped beneath the floor mat and the air in the aircraft cabin above the floor mat, the air pockets would create bubbles or buckling in the floor mat. The venting of the air pockets beneath the floor mat by the flow paths eliminates the problem of bubbling or buckling in the floor mat. | 03-24-2016 |
| 20160096777 | HONEYCOMB STRUCTURAL BODY AND METHOD FOR MANUFACTURING THE SAME - A honeycomb structural body | 04-07-2016 |
| 20160097162 | HONEYCOMB CORE HAVING A HIGH COMPRESSION STRENGTH - This invention pertains to a method of making a fiber-reinforced composite structure comprising the steps of (i) forming a paper sheet having a Gurley air resistance at least 200 seconds per 100 milliliters, the sheet comprising from 30 to 70 weight percent p-aramid fiber, (ii) depositing on both surfaces of the paper sheet a compression enhancing layer in a quantity up to 5 weight percent based on the weight of the paper, (iii) forming a honeycomb from the sheet of step (ii), and (iv) applying a matrix resin coating to the honeycomb of step (iii). | 04-07-2016 |
| 20160102018 | COMPOSITIONS, PANELS AND SHEETS COMPRISING MINERAL FILLERS AND METHODS TO PRODUCE THE SAME - There are provided gypsum panels, sheets and multi-layer sheets as well as methods of preparation thereof. For example, there are provided cellulose filament-reinforced gypsum panels, sheets and multi-layer sheets and methods of preparation thereof. For example, in such gypsum panels, sheets and multi-layer sheets gypsum is bound with cellulose filaments to strengthen the gypsum panels, sheets and multi-layer sheets. The cellulose filament-reinforced gypsum panel can be, for example, a core comprising a honeycomb or corrugated structure. There are also provided aqueous suspensions comprising cellulose filaments and CaSO | 04-14-2016 |
| 20160123160 | Thermal-Sprayed Bonding of a Ceramic Structure to a Substrate - A thermal barrier system includes a protective coating on a substrate, and a ceramic feature layer attached to the protective coating via an adhesive spray coat. | 05-05-2016 |
| 20160129433 | High Capacity Structures and Monoliths Via Paste Imprinting - The disclosure relate generally to structures, forms, and monoliths, and methods of preparing the same. This disclosure can produce uniform structured passageways or channels of active material, including adsorbent or catalyst, by imprinting or molding features into a paste on a support that can be subsequently assembled into a gas or liquid treating structure, i.e. a monolith. The paste, which can include an active material, binder, and other potential additives, can be applied to the support or pushed through a support (as in a mesh) as a thin film. The paste can be imprinted, stamped, shaped or otherwise handled to give features of desired height, shape, width, and positioning. When stacked or rolled, the features of one layer contact a subsequent layer, which seal to form passageways. The resulting structure can have high cell-density (>1000 cells per square inch) and a large volume fraction of active material. | 05-12-2016 |
| 20160136633 | HONEYCOMB FORMED BODY EXTRUDING DIE - A die has two surfaces, in a forming material supplying surface which is one surface, a plurality of back holes to introduce a forming material of a honeycomb formed body into the die are formed, and in a honeycomb formed body extruding surface which is the other surface, lattice-shaped slits corresponding to cell partition walls are formed, the back holes communicate with the slits in slit intersecting portions of the slits, polygonal cell blocks defined by the slits include chamfered portions in which parts of corner portions and the like are chamfered at a chamfering angle θ of 1.0 to 8.0° to the extruding direction, from the honeycomb formed body extruding surface toward a slit depth direction, and straight portions which are not chamfered, and a ratio of a length L of the straight portion to a slit depth D is from 20 to 60%. | 05-19-2016 |
| 20160137255 | CARDBOARD-BASED UNIT - The present disclosure provides a cardboard-based unit, structural elements comprising said unit and land-vehicles comprising said units and structural elements. | 05-19-2016 |
| 20160144592 | COMPOSITE HONEYCOMB STRUCTURE - Adjoining edges of adjacent honeycomb core panel sections are mechanically interlocked. In one embodiment, the method includes forming a first edge along a first cellular core panel section. The first edge includes a first plurality of edge cell walls along the first edge. The method further includes forming a second edge along a second cellular core panel section, wherein the second edge includes a second plurality of edge cell walls along the second edge. The first edge is positioned proximate to the second edge. At least a portion of at least one of the first plurality of edge cell walls is mechanically interlocked with at least a portion of at least one of the second plurality of edge cell walls to form a joint therebetween. The invention also includes a composite structure at least partially produced by such a method. | 05-26-2016 |
| 20160151992 | High-Quality Flame-Retardant Decorative Finish for Interior Panels | 06-02-2016 |
| 20160159028 | ACOUSTICAL STRUCTURE - A light-weight acoustical substrate is disclosed. In one embodiment, the substrate includes a substantially open core and outer facing layers. The core is comprised of a plurality of open, cells which extend between the facing layers. The cells may have numerous configurations, including honeycomb. The facing layers may be non-woven or woven glass scrims in some embodiments, A multi-layered acoustical structure is provided which in one non-limiting embodiment is comprised of two cores with outer facing layers and an interlayer between the cores. | 06-09-2016 |
| 20160167332 | COMPOSITE MATERIAL INCORPORATING WATER INGRESS BARRIER | 06-16-2016 |
| 20160167333 | METHOD OF MAKING CORE-STIFFENED STRUCTURE | 06-16-2016 |
| 20160176140 | SEMI-FINISHED HONEYCOMB PART AND SANDWICH PART | 06-23-2016 |
| 20160176149 | VEHICLE FLOOR SYSTEM | 06-23-2016 |
| 20160176153 | METHOD AND APPARATUS FOR MANUFACTORING A SANDWICH PART AND SANDWICH PART | 06-23-2016 |
| 20160176157 | SANDWICH COMPONENT | 06-23-2016 |
| 20160250577 | CORDIERITE-TYPE CERAMIC HONEYCOMB STRUCTURE AND ITS PRODUCTION METHOD | 09-01-2016 |
| 20160250820 | ARCHITECTED MATERIALS FOR ENHANCED ENERGY ABSORPTION | 09-01-2016 |
| 20160251249 | CERAMIC COMPOSITE BEADS AND METHODS FOR MAKING SAME | 09-01-2016 |
| 20160375649 | OPEN AREA CORE WITH CHOPPED FIBER REINFORCED SKIN - A process for forming a composite sandwich panel assembly is provided that includes positioning a top sheet and a bottom sheet on opposing sides of an open pore matrix core. The top sheet, bottom sheet, and core are exposed to a heat source with the application of a clamping pressure to the top and the bottom sheet. The heat source is then removed and the clamping pressure maintained for a period of time. The clamping pressure is removed when the top sheet, bottom sheet, and core have cooled and fused together. An assembly formed by such a process is also provided. | 12-29-2016 |
| 20170238369 | HEATED AIRCRAFT FLOOR PANELS | 08-17-2017 |
| 20190143629 | Panel and Method of Forming Same | 05-16-2019 |
| 20220134324 | METHOD FOR PRODUCING MOTOR VEHICLE EXHAUST GAS CATALYSTS - The present invention is directed to a method and a device for coating substrates of motor vehicle exhaust gas catalysts. In this respect, the substrates can be flow-though substrates or filter systems (“wall flow”). The invention particularly describes an improvement in such coating processes in which a suspension (washcoat) containing the catalytically active material is applied to or delivered onto such a vertically oriented substrate (monolithic substrate) from above (“metered charge” process). | 05-05-2022 |
