Abstract: A panel assembly including a compression-molded, composite panel is provided. The panel has first and second outer layers and a core positioned between the outer layers. The core has a large number of cavities. The outer layers are bonded to the core by press molding. The assembly also includes a component pivotally connected to the panel and a living hinge which allows the component to pivot about a pivot axis between different use positions relative to the panel. The assembly further includes a stiffening support having a support axis substantially parallel to the pivot axis. The support is bonded or joined to the panel to locally reinforce the panel adjacent the living hinge. The stiffening support eliminates the need for a metal hinge and provides for a light weight assembly with improved aesthetics and function.

Abstract: A honeycomb structure has hexagonal cells surrounded by partition walls and a cylindrical outer peripheral wall covering the honeycomb structure. The partition walls have sides and intersection points. Six sides form a hexagonal cell. Three sides as the partition walls are joined to each other at a corresponding intersection point. The sides are divided into sides of basic partition walls and strength reinforcement sides as strength reinforcement partition walls. The strength reinforcement partition wall is thicker than the basic partition wall. Three strength reinforcement sides are joined at a corresponding strength reinforcement intersection point. Each strength reinforcement side in one group joined at one strength reinforcement intersection point is not connected continuously to each strength reinforcement side in another group joined at another strength reinforcement intersection point.

Abstract: 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.

Abstract: A cargo management system including a vehicle load floor having a vehicle component receiving feature is provided. The load floor compartmentalizes a cargo area into an upper compartment and a covered lower compartment. The system includes a first generally planar member having a first depression of a first predetermined depth and a compression-molded, composite, second generally planar member having a second depression of a second predetermined depth. A portion of the second member is locally crushed by press molding to form the second depression. Opposed surfaces of the first and second depressions cooperate to restrain movement of a vehicle component positioned in a cavity defined by the first and second depressions between the first and second members and prevent sudden transfer of vehicle component weight during vehicle acceleration and deceleration.

Abstract: A sandwich-type, structural, composite component including at least one hingedly connected portion which pivots with reduced or eliminated hinge binding and a cargo management system and vehicle load floor utilizing the component are provided. Elongated first and second interior portions of the component are locally crushed by the press molding to form a living hinge having a pivot axis and an elongated depression, respectively. The component includes an elongated cut-out which extends completely through the component at the elongated depression to obtain a clearance between a first portion of the component hingedly connected to a second portion of the component by the living hinge. The living hinge and the clearance allow pivotal movement of the first portion between different use positions relative to the second portion with reduced or eliminated hinge binding during the pivotal movement about the pivot axis.

Abstract: 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.

Abstract: Disclosed are a structure for construction, which includes a hollow structure having a plurality of cells provided therein with hollows, arranged in a set three-dimension pattern, and partitioned by cell walls, and a cover enclosing the outside of the hollow structure, and a method of manufacturing the same. In this way, because the plurality of hollow cells of the hollow structure are partitioned by the cell walls and provided therein with the hollows, the overall weight can be reduced, and the rigidity and strength can be maintained at an adequate level despite the reduced weight. Also, due to the cells installed in the three-dimensional pattern, the growth of cracks or damage caused by impacts can be confined to local areas. Furthermore, since the weight is reduced, distribution and transportation costs can be reduced.

Abstract: Methods for fabricating sub-lithographic, nanoscale microchannels utilizing an aqueous emulsion of an amphiphilic agent and a water-soluble, hydrogel-forming polymer, and films and devices formed from these methods are provided.

Abstract: 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.

Abstract: A structured-core laminate panel can be made in an efficient, structurally sound manner without the use of adhesives (film or liquid forms) using materials with different melt or glass transition temperatures. In one implementation, a manufacturer positions one or more resin substrates about a structured core, which comprises a relatively high melt or glass transition temperature compared with that of the one or more resin substrates. The manufacturer heats the assembly to at least the glass transition temperature of the resin substrates, but not to the melt or glass transition temperature of the structured core. This allows the one or more resin substrates to melt and bond (mechanically, chemically, or both) to the structured core on one side (or inner surface), while maintaining a substantially planar or original conformation on an opposing side (or outer surface).

Abstract: A unitary structural assembly including a first component having a plateau-receiving aperture and a compression-molded, composite second component having a sandwich structure is provided. The second component includes a first outer layer, 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 a press molding. A portion of the second component including the first layer and the core defines a raised plateau having upper and side surfaces. The plateau has a size and shape corresponding to the size and shape of the plateau-receiving aperture. A height of the plateau corresponds to the depth of the plateau-receiving aperture. The plateau is inserted into the plateau-receiving aperture so that corresponding surfaces of the plateau and the plateau-receiving aperture are in abutting engagement to unitarily connect the components and form the assembly.

Abstract: A half closed thermoplastic folded honeycomb structure is described which is produced from a continuous web of material by plastic deformation perpendicular to the plane of the material to thereby form half-hexagonal cell walls and small connecting areas. By folding in the direction of conveyance the cell walls meet to thereby form the honeycomb structure.

Abstract: The present disclosure describes use of filamentous algae to form insulating construction materials which provide thermal and noise insulation. Algae from the order Zygnematales, the Cladophorales, or the Ulotrichales can be dried and formed for use as insulating material. Algae mass can be combined into several layers, using a binder to attach the layers to each other. A composite material of algae mass and an additive can be used and form the body of insulation panels having honeycomb-shaped chambers, which are sealed by a foil that is laminated onto the body.

Abstract: 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).

Abstract: 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.

Abstract: 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.

Abstract: The invention relates to a method for manufacturing flat, single or double curved core composites 1, 23 with at least one folded honeycomb core 4, 19. Prior to applying the initially not yet hardened cover layers 2, 3, 13, 22 a curable and later removable core filler material 15, 16 is introduced into full-length drainage-enabling channels 5, 6 of the folded honeycomb core 4, 19 in order to prevent telegraphing of the cover layers 2, 3, 13, 22 into the channels 5, 6 of the folded honeycomb core when arranging and/or hardening the cover layers 2, 3, 13, 22 and to produce edge-free and polygon-free surfaces of the core composite 1, 23. The core composites 1, 23 made according to the method have optimum structural mechanical properties, an ideal surface quality from the aerodynamic and aesthetic point of view, whereby a direct reprocessing of the core composites 1, 23 is possible without the need for further time and cost-intensive as well as in some circumstances weight-increasing finishing steps.

Abstract: Composite-membrane monoliths include a cordierite monolith having a cordierite-ceramic composite membrane bonded to surfaces thereof with a surface median pore size. The cordierite-ceramic composite membrane has membrane surfaces with a membrane median pore size of 0.3 ?m or less. The cordierite-ceramic composite membrane may be a composite formed by firing the cordierite monolith subsequent to applying a cordierite-ceramic composite slip to surfaces thereof. The cordierite-ceramic slip may include cordierite particles and ceramic particles. The cordierite particles may have a cordierite median particle size smaller than the surface median pore size. The ceramic particles may have a ceramic median particle size smaller than the cordierite median particle size.

Abstract: A method and apparatus comprising a composite panel and a number of structures to reduce noise radiation from the composite panel. The composite panel has a first face sheet, a second face sheet, and a core located between the first face sheet and the second face sheet. The number of structures is associated with the first face sheet. The number of structures has a mass with a configuration to reduce a speed of waves propagating in the composite panel such that noise radiating from the composite panel is reduced.

Abstract: A honeycomb body is formed of at least one at least partially structured sheet-metal foil and has a plurality of channels. The sheet-metal foil has a course or profile direction and includes top-side connecting points and bottom-side connecting points to itself or to at least one additional smooth sheet-metal foil or structured sheet-metal foil. At least the top-side connecting points or bottom-side connecting points form a curved connection line and expansion joints between the respective connection points of the curved connection line. An exhaust-gas treatment unit and a motor vehicle are also provided.

Abstract: 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.

Abstract: A nonwoven web of poly(phenylene-1,3,4-oxadiazole) and polymetaphenylene isopthalamide. was found to have greater retention of tensile strength than kraft paper after immersion in oil at high temperature, making it useful as an insulation material for transformers.

Abstract: A base paper of aramid fiber honeycomb core and its manufacturing method are provided. The base paper comprises 11-90 parts by weight of structural fiber, 10-70 parts by weight of crosslinking fiber, and 0-19 parts by weight of additive fiber, wherein the structural fiber is poly(p-phenylene terephthal amide) fiber, the crosslinking fiber is poly(m-phenylene isophthal amide) fibrid, and the additive is polyester fiber.

Abstract: Embodiments of the present disclosure include a composite panel and a method of manufacturing the composite panel. The composite panel includes first and second fiber reinforced plastic (FRP) layers. The composite panel also includes a core layer disposed between the first and second FRP layers. The core layer includes one of: a honeycomb material and a foam material. The composite panel further includes an exterior layer disposed on a surface of the first FRP layer opposite the core layer and an interior layer disposed on a surface of the second FRP layer opposite the core layer. The layers are cured together in one processing step.

Abstract: 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.

Abstract: A grid type element (1) of fiber composite structure, comprising a plurality of open polygonal cells (5) made of at least three core segments (16), said open polygonal cells (5) being stringed together alongside said ribs (16) to form a grid structure, and an essentially planar skin sheet (4), said essentially planar skin sheet (4) being attached unilaterally to the grid structure. A multipartite core (6) is provided, said core segments (6a, 6b, 6c) with respectively rectangular cross sections being formed of said multipartite core (6). Said at least three core segments (6a, 6b, 6c) are pivotable interconnected with at least two reduced cross sections (9) between two of said at least three core segments (6a, 6b, 6c) and at least one fiber composite layer (8, 7) is provided with said multipartite core (6), said at least one fiber composite layer (8, 7) sheathing at least partly said multipartite core (6). The invention is as well related to a method of manufacturing such grid type elements.

Abstract: The invention is related to a grid type fiber composite structure (1) comprising a grid of polygon cell modules (5) comprising at least three substantially u-shaped ribs made of fiber composite layer (8, 13) and a foam core (9) provided inside each cell module (5) for support of said u-shaped ribs. Said foam core (9) is along a base essentially in line with one of said flat cap sections (11, 12). At least one layer of strip (2, 3) is provided outside said flat cap sections (11, 12) and a skin sheet (4) is unilaterally attached to said cell modules (5) essentially in line with one of said flat cap sections (11, 12). The invention is as well related to a method of manufacturing such a grid type fiber composite structure (1).

Abstract: The cargo loading and transport system, particularly for barrels for hazardous materials such as e.g. chemicals, comprises a carrier plate (38) provided to support cargo (40) for transportation, and angle-section bar elements (10) comprising cardboard material, for arrangement on upper outer edges (41) of the cargo (40) facing away from the carrier plate (38). The cargo loading and transport system further comprises lashing straps (44) to be strapped around the carrier plate (38), the angle-section bar elements (10) and the cargo (40) arranged therebetween.

Abstract: A packaging material for protecting a packaged product is disclosed. The packaging material includes a core material having a plurality of cells with open tops and bottoms A first reinforcing layer covers the open tops of the cells of the core material. A second reinforcing layer covers the open bottoms of the cells of the core material. A layer of anti-abrasive material is attached to the first reinforcing layer. A second layer of anti-abrasive material may be attached to the second reinforcing layer. The packaging material may be formed into angle pads, corner pads and channel protectors also.

Abstract: 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.

Abstract: 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.

Abstract: 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 fiber 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.

Abstract: A unitary structural assembly including a first component having a plateau-receiving aperture and a compression-molded, composite second component having a sandwich structure is provided. The second component includes a first outer layer, 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 a press molding. A portion of the second component including the first layer and the core defines a raised plateau having upper and side surfaces. The plateau has a size and shape corresponding to the size and shape of the plateau-receiving aperture. A height of the plateau corresponds to the depth of the plateau-receiving aperture. The plateau is inserted into the plateau-receiving aperture so that corresponding surfaces of the plateau and the plateau-receiving aperture are in abutting engagement to unitarily connect the components and form the assembly.

Abstract: Novel method of preserving the internal environmental air temperature and thereby stabilizing the temperature within the cargo compartment of a transport container, and thereby protecting the cargo itself from degradation due to temperature fluxuations, including a freeze and heat barrier attained through the characteristics of the article of manufacture, composition of matter, and method of preservation of the internal environmental air temperature and proximate cargo within said cargo compartment; along with a machine or devise that is used as either a stand-alone container, or as an insert to retrofit existing containers so as to make said retrofitted devices capable of providing cooling over an extended period of time are disclosed. The inserted cargo compartments described herein are particularly useful for temperature-stabilizing cargo compartment shipping containers that are required to maintain a temperature below ambient for a time sufficient to complete delivery of the container and its contents.

Abstract: 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.

Abstract: An object of the invention is to provide a honeycomb structure that has excellent NOx purification performance and can suppress the breakage of a honeycomb unit due to the adsorption or desorption of water, a method for manufacturing the honeycomb structure, and an exhaust gas purifying apparatus including the honeycomb structure. In addition, the honeycomb structure of the invention includes a honeycomb unit provided with a plurality of through holes arrayed in a longitudinal direction with a partition wall therebetween, in which the honeycomb unit is produced by extruding and firing raw material paste containing silicoaluminophosphate particles and an inorganic binder, and the silicoaluminophosphate particles have a ratio of an amount of Si to a sum of amounts of Al and P in a range of 0.16 to 0.33, a specific surface area in a range of 200 m2/g to 400 m2/g, and an average diameter of original silicoaluminophosphate particles in a range of 2.0 ?m to 6.0 ?m.

Abstract: Nanoporous three-dimensional networks of polyurethane particles, e.g., polyurethane aerogels, and methods of preparation are presented herein. Such nanoporous networks may include polyurethane particles made up of linked polyisocyanate and polyol monomers. In some cases, greater than about 95% of the linkages between the polyisocyanate monomers and the polyol monomers are urethane linkages. To prepare such networks, a mixture including polyisocyanate monomers (e.g., diisocyanates, triisocyanates), polyol monomers (diols, triols), and a solvent is provided. The polyisocyanate and polyol monomers may be aliphatic or aromatic. A polyurethane catalyst is added to the mixture causing formation of linkages between the polyisocyanate monomers and the polyol monomers. Phase separation of particles from the reaction medium can be controlled to enable formation of polyurethane networks with desirable nanomorphologies, specific surface area, and mechanical properties.

Abstract: 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.

Abstract: The present disclosure relates to a substrate comprising nanomaterials for treatment of gases, washcoats for use in preparing such a substrate, and methods of preparation of the nanomaterials and the substrate comprising the nanomaterials. More specifically, the present disclosure relates to a substrate comprising nanomaterial for three-way catalytic converters for treatment of exhaust gases.

Abstract: 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.

Abstract: A structure 1 is provided with a core layer 2 where a plurality of polygonal-cylindrical or circular-cylindrical cells S are disposed adjoiningly inside and skin layers 3, 4 that are provided on the upper and lower surfaces of the core layer 2. Communication portions 6 for communicating with adjacent cells S are formed in the core layer 2. A molded article is formed by providing a bent portion to the structure 1.

Abstract: 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.

Abstract: 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 comprising porous partition walls by which a plurality of cells that become through channels of a fluid are partitioned and in which a plurality of pores are formed. In each of the partition walls, pores having pore diameters larger than a thickness of the partition wall in a section thereof which is perpendicular to an extending direction of the cells are formed so as to occupy 4 to 11% of the total volume of the pores formed in the partition walls.

Abstract: A honeycomb body for an exhaust-gas purification system may be used, for example, as a carrier body for catalytically acting coatings or as a filter, absorber or mixer in the exhaust system of an internal combustion engine. The honeycomb body has channels, an axial main direction, a planar front surface, a planar end surface and a circumferential surface disposed parallel to the axial main direction. The front surface and/or the end surface are disposed obliquely with respect to the axial main direction. Such a honeycomb body is advantageous, in particular, for applying reducing agent to the oblique end or front surface. A method for producing a honeycomb body, an exhaust line section and a motor vehicle are also provided.

Abstract: A freeze dryer shelf with opposed, parallel first and second plates is disclosed. The plates have at least one flow channel located therebetween for conveying a diathermic fluid between the plates. One of the plates has a surface treated to inhibit the sticking to the shelf of a rubber stopper pressed against that surface during the application of pressure to the stopper to push the stopper into a container.

Abstract: 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.

Abstract: A building element 1 consists of several individual layers 2, 3, 4 and is designed as a honeycomb construction with partial hollow bodies 26, 27 protruding over the basic construction 16. Surfaces 10, 11 of adjoining individual layers 2, 3, 4 together form a wall of a small thickness. Individual surfaces 10, 11 of the individual layers 2, 3, 4 have a pre-stressing for improving the connection with adjoining surfaces.

Abstract: 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.

Abstract: 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.

Abstract: A honeycomb structure includes: a honeycomb structural portion having porous partition walls functioning as fluid passages and separating and forming a plurality of cells extending from one end face to the other end face. The partition walls and the outer peripheral wall contain silicon carbide particles as a framework and silicon as a binder for binding the silicon carbide particles. The honeycomb structure has a partition walls thickness of 50 to 200 ?m, a cell density of 40 to 150 cells/cm2, and an average particle diameter of the silicon carbide as a framework of 3 to 40 ?m. The honeycomb structural portion has a volume resistivity of 1 to 40 ?cm at 400° C., and the volume resistivity of the electrode portion at 400° C. is not more than 40% of the volume resistivity of the honeycomb structural portion at 400° C.