Abstract: Provided are a matrix resin composition for fiber reinforced plastic, which comprises a bifunctional or trifunctional liquid diisocyanate, a bifunctional polyol and a bifunctional chain extender containing an active hydrogen group, with a molar ratio of the functional groups of the diisocyanate, polyol and chain extender of 5.0 to 1.0:1.0:4.0 to 0, respectively; and a process for producing fiber reinforced plastic, which comprises impregnating a fibrous material with the resin composition and then curing. The present invention makes it possible to produce a molding containing fibers densely, having excellent strength and inflatability, in the production of an FRP molding by using a thermosetting resin having an extended pot life.

Abstract: A photosensitive epoxy resin adhesive composition which is capable of forming a pattern by exposure to light through a photomask and development, and which, even after having formed a pattern in that manner, may still exhibit high adhesiveness when heated while keeping its pattern as such, as well as a photosensitive adhesive film which comprises the photosensitive epoxy resin adhesive composition. The photosensitive epoxy resin adhesive composition comprises an epoxy resin and a photo-acid generator, wherein the epoxy resin comprises a polyfunctional epoxy resin having an epoxy equivalent of from 100 to 300 g/eq and a polyfunctional epoxy resin having an epoxy equivalent of from 450 to 10000 g/eq.

Abstract: An apparatus for making SMC comprising a conveyor belt assembly having a feed end and a transfer end. The conveyor belt assembly including a belt having an outer surface and an inner surface. A cutting support structure disposed between the feed end and the transfer end, and in contact with the inner surface. A cutting wheel having a perimeter surface and disposed adjacent to the cutting support structure. A feed tension member proximate the outer surface and disposed between the feed end and the cutting wheel. The feed tension member positions the fiber rovings onto the outer surface to be cut by the cutting wheel. The feed tension member, cutting wheel and belt cooperate to feed the fiber rovings at a feed rate, cut the fiber rovings into a plurality of parallel discontinuous fibers, and convey the fibers at substantially the same rate as the feed rate.

Abstract: A polymer optical waveguide includes: a core; and a cladding enclosing the core and extending along a direction of light propagation, the polymer optical waveguide having a substantially rectangular parallelepiped shape, and the polymer optical waveguide having, at least at a position near one end thereof in a longitudinal direction, a groove that has a surface inclined at an angle of 45° with respect to the light propagation direction which reflects light propagating through the core so as to change the light propagation direction by 90°.

Abstract: A transparent reinforced composite material. An illustrative embodiment of the reinforced composite material includes a polymeric matrix, at least one low-density region including a first plurality of glass elements having a first packing density provided in the polymeric matrix and at least one high-density region including a second plurality of glass elements having a second packing density greater than the first packing density provided in the polymeric matrix. A method for reinforcing a composite material is also disclosed.

Abstract: Disclosed is a curable silicone resin composition that is solid at room temperature, the composition including: (A) an organopolysiloxane having a resin structure consisting of specific siloxane units, (B) an organohydrogenpolysiloxane having a resin structure consisting of specific siloxane units, (C) a platinum group metal-based catalyst, (D) either one or both of an opaque pigment and an opaque dye, and (E) a reaction retarder, in which a layer of thickness 100 ?m formed from a cured product of the composition exhibits a light transmittance of not more than 5% across the entire visible light range. The composition is solid at room temperature and therefore easy to handle. Further, the composition is useful for producing an opaque silicone adhesive sheet.

Abstract: An embodiment of the invention includes a composite structure fabricated from at least one pre-cured flat face sheet applied to a core with an adhesive. Once the pre-cured flat face sheet is applied to the core, curing of the adhesive may take place to bond the pre-cured flat face sheet to the core. Before the bonding of the pre-cured flat face sheet to the core takes place, the pre-cured flat face sheet may be prepared by separately curing a composite face sheet.

Abstract: An article of fiber-reinforced composite material formed by co-curing a lay up under a cycle of heat and pressure. The lay up comprises a first uncured composite layer having at least one uncured resin-impregnated laminate layer. At least one hollow mandrel is provided comprised of a stiffened braided fabric and having an upper, a lower and side surfaces. The mandrel is secured on the upper surface of the first composite layer with the lower surface thereof in engagement with the upper surface of the first composite layer. A second uncured composite layer is positioned over the upper and side surfaces of the hollow mandrel and at least a portion of the upper surface the first uncured composite layer. The second uncured composite layer has at least one uncured resin-impregnated layer. After the cycle of heat and pressure in an autoclave, the hollow mandrel is retained in the co-cured article.

Abstract: A method for producing a reinforced polyester non-woven material suitable for use as a roofing material, comprising: forming a mixture comprising glass fibers and a liquid binder; applying the mixture to a polyester non-woven material; and curing the liquid binder to form a layer comprising glass fibers that is attached to the polyester non-woven material.

Abstract: An article comprising two chemically grafted polymer layers comprising a hydrogel layer and an end-functionalized polyurethane layer. The invention also includes methods of making and using the article.

Abstract: A method for attaching a sealing profile to a vehicle body part includes the steps of pulling the sealing profile from a storage unit; passing the sealing profile through a first buffer which compensates for differences between incoming and outgoing speeds of the sealing profile; attaching an adhesive strip to the sealing profile continuously, the adhesive strip having a first adhesive layer facing the sealing profile and a second adhesive layer facing away from the sealing profile; passing the sealing profile with the attached adhesive strip through a second buffer which compensates for differences between incoming and outgoing speeds of the sealing profile; and rolling the second adhesive layer onto the vehicle body part. The adhesive strip is attached to the sealing strip in an assembly unit which heats the first adhesive layer as it moves around a press roller.

Abstract: A film adhesive for bonding adjacent composite structures.

Abstract: A method of making a repositionable transfer adhesive is provided. The method includes the steps of (a) providing a release liner having opposing first and second surfaces, the first surface having a release value of at least 10 grams per inch, as measured according to the Tape Release Test, lower than the second surface; (b) providing an adhesive composition comprising microsphere adhesive and a binder adhesive; (c) coating the adhesive composition on the first surface of the release liner such that the microspheres protrude from the binder adhesive; (d) drying the adhesive composition to yield a microsphere transfer adhesive; (e) winding the release liner such that the microsphere transfer adhesive is wound inwardly and the second surface of the liner contacts the microspheres; and (f) applying pressure to the second surface of the liner.

Abstract: The present invention is to impart, to a sheet-like soft magnetic material, a configuration in which sheet thickness change is suppressed and in which fluctuation in magnetic permeability is small even under a high-temperature or a high-temperature, high-humidity environment, even when a plurality of thin curable soft magnetic sheets produced by a coating method are laminated. The sheet-like soft magnetic material is formed from a soft magnetic composition which is formed by mixing at least a flat soft magnetic powder, an acrylic rubber, an epoxy resin, a curing agent for the epoxy resin, and a solvent. The flat soft magnetic powder is arranged in an in-plane direction of the sheet-like soft magnetic material. An acrylic rubber having a glycidyl group is used for the acrylic rubber. The weight ratio of the flat soft magnetic powder with respect to the total amount of the acrylic rubber, the epoxy resin, and the curing agent for the epoxy resin is 3.7 to 5.8.

Abstract: A method to join a substrate to an object is disclosed using a curable one or two part adhesive composition comprising an effective amount of a stabilized organoborane amine complex initiator and one or more monomers, oligomers, polymers or mixtures thereof having olefinic unsaturation which is capable of polymerization by free radical polymerization.

Abstract: The present application is directed to systems for controlling the direction of thermal expansion of a composite part during thermal processing. The systems may comprise at least one guiding mechanism capable of being attached to a surface of a tool for fabricating composites and at least one moveable composite insert capable of being attached to a composite part. The moveable composite insert has an opening for receiving the at least one guiding mechanism. The opening is capable of controlling movement of the at least one moveable composite insert in a desired direction during thermal expansion of the composite part, when the guiding mechanism is received by the opening. Methods for controlling the direction of thermal expansion of a composite part during thermal processing are also disclosed.

Abstract: A connection between composites with non-compatible properties and a method of preparing of such connections are provided. The composites comprise first and second type fibres, respectively, as well as resin. The connection comprises a transition zone between the composites having a layered structure. The transition zone may optionally comprise a transition member and the transition member may optionally be integrated with one or more of the composites. Examples of non-compatible properties where the present connection will be appreciated are great differences in stiffness, e.g. Young's modulus, or in coefficient of thermal expansion.

Abstract: A laminated structural insulated panel has an inner or core layer, an outer layer on the opposite facing surfaces of the core layer and an adhesive layer between each surface of the core layer and its respective outer laminate layer. To increase the strength and reduce the likelihood of delamination, the present panel is provided with a plurality of perforations in the surface of the core layer that receives the outer and adhesive layers. Each of the perforations form a chamber that receives a portion of the bonding agent or adhesive utilized for the adhesive layer. The bonding agent or adhesive bonds to the side walls of the chamber to mechanically anchor the outer layer to the interior of the core layer by substantially increasing the bonding surface between the adhesive layer and the core layer. In one embodiment, the core layer is an expanded polystyrene or other rigid foam.

Abstract: Preformed compositions in shaped form comprising polymer blends, and the use of these preformed compositions in shaped form to seal apertures are disclosed. In certain embodiments, the preformed compositions are electrically conductive and are capable of shielding EMI/RFI radiation. The polymer blend includes a polysulfide component and a polythioether component.

Abstract: The invention encompasses a handrail for escalators or moving walkways that includes a grip piece of a thermoplastic elastomer including soft segments and hard segments and optionally a sliding layer arranged on the underside of the grip piece relative to the mounting orientation of the handrail. A ratio of the proportions of the soft segments to the hard segments is selected from a range with a lower limit of 1:1 and an upper limit of 9:1, or, in a variation, from a range with a lower limit of 1.5:1 and an upper limit of 6:1, or, in another variation, from a range with a lower limit of 2.5:1 and an upper limit of 4:1.

Abstract: The invention provides a method for imparting topographical or protective features to a substrate by contacting a sheet material comprising a thermosettable layer with a substrate and heating the sheet material to an elevated temperature.

Abstract: In one step of a method of fabricating a composite tube, layers of uncured composite material may be laid over a surface. In another step, spaced-apart strips of at least one of uncured, partially cured, and completely cured composite material may be laid lengthwise over the laid layers of composite material. In still another step, the spaced-apart strips may be compacted against the layers of uncured composite material. In an additional step, the compacted spaced-apart strips and the layers of uncured composite material may be further consolidated and/or cured to form a composite tube.

Abstract: Method for printing objects, whereby these objects (15) are provided with a multi-layered print, characterized in that to this aim, on one hand, two or more layers of printing medium (10-11-12), which at least partially are situated one above the other, are provided on a supple carrier (13) and, on the other hand, these layers (10-11-12) are simultaneously transferred onto the object (15) to be printed by bringing said carrier (13), together with the layers of printing medium (10-11-12) present thereon, and the object (15) into mutual contact.

Abstract: The invention relates to a method of assembling structures and a component for use in such assemblies. The component is an electrically insulant, compressible impermeable cloth. It is formed by impregnating an electrically insulant woven fibre with a sealant, and curing to form the cloth. Structures, such as airframe structures, may be assembled by positioning the cloth between a substructure and an outer skin on at least part of a sub-structure, and then assembling the outer skin to the sub-structure with the cloth located between the substructure and the outer skin. This provides a greater impermeability and insulation across the structural joint. During assemble the cloth may also be compressed, allowing skin panels to be fixed to the substructure within close tolerances, and allowing steps between adjacent panels to be substantially reduced.

Abstract: A surgical table width extender having an angled tang structure for engaging the gap formed between a standard table and its stand-off-mounted side rail. The tang structure contacts portions of the rail and portions of the table edge to enhance the load-carrying capability of the table side rail assembly. The extender further provides its own stand-off-mounted rail and a quick release clamp for securing the extender to the table. The tang structure is formed to allow a single extender to be used on either side of a surgical table where the stand-offs are not evenly spaced apart. The extender body is formed from a lightweight, strong carbon fiber composite material. Further enhancements protect exposed comers of the extender and protect potential high stress surfaces. An angularly orientable attachment is provided for use when two width extenders are used simultaneously on opposite sides of the table. In a lowered, horizontal orientation the attachment acts as a table length extender.

Abstract: Described herein are composites that are composed of a plurality of plies with a stiffening grid intimately embedded within the composite. The composite structures have the improved buckling performance characteristics of known isogrid and orthogrid composite structures and yet have a significantly higher damage tolerance that permits such structures to be used in the formation of aircraft and spacecraft designs. Also described herein are methods for making the composites.

Abstract: In one embodiment, the invention is a composition comprising: a) one or more film forming resins having at least one functional group capable of polymerization; b) one or more adhesion promoters comprising compounds containing one or more unsaturated groups capable of free radical polymerization and one or more trialkoxy silane groups; c) one or more fillers capable of imparting abrasion resistance to the composition when cured; d) one or more compounds which is reactive with the film forming resin which also contains an acidic moiety; and e) one or more compounds comprising a siloxane backbone and one or more active hydrogen groups capable of reacting with the functional groups on a glass bonding adhesive, one or more second adhesion promoters comprising one or more silicon, titanium, zirconium, aluminum, or metal containing compounds, organic materials having reactive groups which are reactive with reactive groups on the surface of substrates or adhesives to which the composition of the invention will be

Abstract: The invention relates to a jig (9) for manufacturing composite material parts out-of-autoclave, comprising a base (11) the upper surface of which includes a stacking table (13) having a rotating movement and a shifting movement in the laminating direction, and a head (15) supported on a portal frame (17) through means allowing the shift perpendicular to the laminating direction on the mentioned table (13), the head (15) in turn comprising: automatic means (21) for placing tapes or roves of composite material in the form of prepreg; compacting means (23) for compacting the composite material and curing means (25) for polymerizing the composite material. The invention also relates to an out-of-autoclave process for manufacturing composite material structures.

Abstract: A method of making an insulation product is provided. An uncured or partially cured mat containing randomly oriented inorganic fibers and a heat curable binder agent is formed. The mat has a pair of side portions and a first and second major surfaces thereon. A nonwoven sheet is applied to the first major surface. The nonwoven sheet comprises randomly oriented glass fibers. The uncured or partially cured mat is heated with the nonwoven sheet, wherein the mat is cured to form a low density mat and the nonwoven sheet is bonded to the first major surface by the heat curable binder agent.

Abstract: The present invention provides a new antistatic method and its application to members. The present invention is an antistatic method featured to mount multiple resin based composites with different triboelectric series order on the surface and members featured to have multiple resin based composites with different triboelectric series order on the surface. The members are resin based sheets, resin based films or resin molded materials. The resin based composites are adhesives, bonding agents, printing ink or paint.

Abstract: An apparatus for the production of sandwich composite elements which includes at least two feed apparatus for facings, to which an application apparatus for an adhesion promoter, an application apparatus for a core layer, a conveying apparatus and a cutting apparatus are connected one after the other. The application apparatus for the adhesion promoter includes at least one feed line for the adhesion promoter, a rotary table with at least one lateral outlet orifice and a drive for the rotary table.

Abstract: A method for manufacturing a textile composite intended for mechanical reinforcement of a bitumen or synthetic-based waterproof coating. The composite comprises a first layer of a non-woven fabric material based on synthetic fibres that is puncture resistant; a second layer of a non-woven fabric material based on mineral or synthetic fibres that is fire resistant; a grid structure placed between the first and second layers, the warp yarns and weft yarns of which are connected to each other at the points where they cross by means of an adhesive that also ensures bonding of the first and second layers on the grid.

Abstract: A process for production of a self-adhesive sheet, comprising following stages: predisposing a front layer and a support layer; spreading silicone on an upper surface of the support layer; polymerizing the silicone; applying the front layer to the upper surface of the support layer, interposing an adhesive substance between the layers.

Abstract: A method and apparatus for manufacturing. A fiber layer and a porous bonding layer are formed to form a unidirectional lay-up of fibers. The lay-up of fibers is heated under pressure to form a unidirectional composite tape of desired thickness to substantially maintain the fibers in a desired configuration. The unidirectional composite tape is slit to a desired width, and the slit unidirectional composite tape is loaded into a multiaxial fabric machine. A first layer is built from the composite tape in the multiaxial machine, and a second layer is built from the composite tape on the first layer at a predetermined angle from the first layer in the multiaxial machine. The first and second layers are consolidated to form a composite fabric in a continuous process.

Abstract: A composite member with a reinforced rampdown or taper has a composite noodle bonded to an end of a core to fill the taper.

Abstract: The invention relates to a process for the manufacture of a ballistic-resistant molded article in which a stack of monolayers is formed, each monolayer containing unidirectionally oriented reinforcing fibers and at most 30 mass % of a plastic matrix material, the reinforcing fibers being highly-drawn polyethylene fibers, and with the fiber direction in each monolayer being rotated with respect to the fiber direction in an adjacent monolayer, the stack then being compressed at a pressure of more than 25 MPa and a temperature between 125 and 150° C., and the plastic matrix material having a 100% modulus of at least 3 MPa.

Abstract: The use of a film for adhesively bonding two substrates, wherein the film comprises a layer which is composed of more than 30% by weight of a heat-activatable polyurethane (PU layer for short).

Abstract: Moisture-curing compositions include at least one silane-functional polymer P with at least two terminal groups of formula (I) and at least one reaction product R which is produced from at least one aminosilane AS with at least one primary amino group and at least one silane group-free alkene M which is capable of entering in 1,4 addition reactions with primary amino groups. The compositions have improved adhesive properties and are especially suitable for use as adhesives, sealing materials or coatings, especially as elastic adhesive or sealing materials.

Abstract: A sandwich component assembly (10) with an L-shaped element comprises a first sandwich panel (12) with a first honeycomb core (14), the upper and lower sides of which are provided with respective cover layers (16, 18), one of which cover layers forms an inner cover layer (16) and the other cover layer an outer cover layer (18), and a second sandwich panel (20) with a second honeycomb core (22), the upper and lower sides of which are provided with respective cover layers (24, 26), one of which cover layers likewise forms an inner cover layer (26) and the other cover layer an outer cover layer (24). At least one edge of the second sandwich panel (20) is connected to the first sandwich panel (12) to form an L-shaped element.

Abstract: Techniques and apparatus for providing a fly away caul plate are disclosed. In an embodiment, a method for curing a composite structure includes placing a pre-cured caul plate proximate an uncured composite lay-up, the lay-up may or may not include one or more stiffeners extending substantially perpendicular to the lay-up surface, the caul plate including an aperture for receiving the at least one stiffener. A force may be exerted against the caul plate to engage the composite lay-up. Heat and/or pressure may be applied to the composite lay-up to cure the stiffener panel and co-bond the caul plate to the composite lay-up.

Abstract: Composite articles having a cosmetic layer, a structural layer comprising a fiber reinforced resin, and a compressible layer positioned between the cosmetic layer and the structural layer are described. The cosmetic layer has a Young's modulus of at least 1.0 GPa and the compressible layer has a Young's modulus of less than or equal to 50 MPa. Print-through control layers having a compressible layer and at least one skin coat are also described, as are methods of forming composite articles and methods of controlling print through.

Abstract: A surface covering such as a lay flat flooring product having an upper show surface disposed in overlying relation to a single or multi-layer, preferably flexible, heavy, thin, resilient backing. A fibrous backing sheet may be disposed across an underside of the backing. The surface covering may be, for example, a tile or roll goods. The show surface may be a decorative textile or carpet layer.

Abstract: The invention relates to a method of producing reinforced, formed fabrics, consisting in producing a continuous fabric alternated with a membrane (34) containing embedded reinforcing elements, which is prepared in overlapping portions on a conveyor belt (29) which passes over a preparation table (25). The membrane (34) and the reinforcing elements are then positioned under a press consisting of an upper air-filled chamber (1), the lower part thereof comprising a flexible element (4), and a lower water-filled chamber (14), the upper part thereof comprising a flexible element (17). According to the invention, a forming bar (10) is adjustably mounted in the upper chamber (1). When the aforementioned forming bar (10) is adjusted to adopt a particular shape, the different flexible elements can deform at the forming bar and the membrane and the reinforcing elements are hot pressed with a portion corresponding to the forming bar having a three-dimensional shape, thereby defining the form of the fabric produced.

Abstract: The invention relates to a process for the production of post-crosslinkable thermoplastic resins by bulk-polymerizing a polymerizable composition (A) comprising (I) a monomer fluid containing a cyclic olefin (?) having two or more metathetical ring-opening reaction sites in the molecule in an amount 10 wt % or above based on the total amount of the monomers or a monomer fluid containing a norbornene monomer and a crosslinking agent, (II) a metathetical polymerization catalyst, and (III) a chain transfer agent; thermoplastic resins obtained by this process; and a process for producing crosslinked resins or crosslinked resin composite materials which comprises laminating such a thermoplastic resin with a substrate at need and then crosslinking the thermoplastic resin. According to the invention, thermoplastic resins which are free from odor due to residual monomers and excellent in storage stability can be efficiently obtained by a simple process of bulk-polymerizing the composition (A).

Abstract: The present disclosure is drawn to embodiments of dies having polymer ribs.

Abstract: A method for making a panel comprising the steps of providing a plurality of waveguides including an optical core layer having a first and a second surface coated with a cladding material that forms a cladding layer, positioning a thermosetting adhesive between the plurality of waveguides, wherein the thermosetting adhesive includes a thermosetting resin, and curing the thermosetting adhesive.

Abstract: An integral composite rocket motor nozzle. The novel nozzle includes a first layer of a first reinforcement material, a second layer of a second reinforcement material, and a common matrix material surrounding the first and second reinforcement materials such that the reinforcement materials and matrix material form a single integral composite structure. In an illustrative embodiment, the first reinforcement material includes graphite fibers for providing structural support, and the second reinforcement material includes glass or quartz fibers for providing thermal insulation on a first side of the first layer. The nozzle may also include a third layer of a third reinforcement material for providing thermal insulation on a second side of the first layer. In a preferred embodiment, the first layer is shaped to form an integrated dome and nozzle structure.

Abstract: Carbon nanotube interlayer assemblies, methods of manufacturing carbon nanotube interlayer assemblies, and methods of manufacturing composite parts with carbon nanotube interlayer assemblies are disclosed herein. In one embodiment, a method of manufacturing a composite structure in accordance with an embodiment of the invention includes producing a plurality of carbon nanotubes on one or both sides of a substrate, and attaching the substrate to a first fiber layer. The method can further include positioning a second fiber layer adjacent to the first fiber layer to position the plurality of carbon nanotubes between the first and second fiber layers. The method can additionally include infusing the first and second fiber layers with resin, and curing the resin. In one embodiment, the carbon nanotube substrate can be attached to the first fiber layer by melt-bonding. In another embodiment, the carbon nanotube substrate can be attached to the first fiber layer with stitches.

Abstract: Composite laminates used in structural applications include an interlayer of soft material that provides damping action to reduce noise and vibration. The interlayer may comprise a viscoelastic material which deforms under stress caused by shock, noise or vibration. A reinforcement may be embedded in the viscoelastic material to maintain the mechanical strength and stiffness of the laminate. The reinforcement may include individual or woven fibers or ridged tubes that provide the interlayer with stiffness.

Abstract: Configurable layup tooling is used to fabricate reinforced composite parts have a common shape but varying features. The tooling includes a tool base, multiple mandrels and optionally, a tool insert, all of which may be used to form a portion of the common shape. The mandrels have differing tool geometries for forming the varying features of the commonly shaped parts. The tool base may be used as a bonding jig to assemble and bond assemblies that include the fabricated parts.