An adhesive composition comprising a solids component, said solids component including a rubber component that includes polychloroprene; and a solvent component, said solvent component including t-butyl acetate.

A lightweight composite material includes a substrate and a carbon fiber layer. The substrate has a first surface and a second surface opposite to each other, and is prepared by impregnating glass fibers with a resinous matrix which is formed by mixing hollow glass microspheres with a thermosettable resin material. The carbon fiber layer is bonded to one of the first and second surfaces of the substrate by thermosetting the thermosettable resin material.

An object is to provide a composite material manufacturing method for improving interlayer strength. The present disclosure provides a composite material manufacturing method of laminating a plurality of prepregs (10) formed of a fiber reinforced base material impregnated with an uncured matrix resin and performing hot molding, the method including: using the prepregs (10) each provided with a gap layer (12) that does not contain a resin and is continuous in an in-plane direction and resin layers (11a, 11b) disposed on both surfaces of the gap layer; disposing a plurality of short fibers (13) on facing surfaces of the prepregs (10) that are adjacent to each other; and evacuating the laminated prepregs (10) to degas the gap layer (12) and then performing hot molding.

The present invention relates to a method for producing an engineered wood, comprising the steps of: (a) breaking down a veneer to increase its porosity; (b) impregnating the veneer from step (a) with an adhesive material; (c) drying the veneer from step (b) to a predetermined moisture content level; (d) arranging a plurality of the veneers from step (c) in a mould; and (e) pressing the plurality of the veneers in the mould. The engineered wood has an appearance of natural timber, and is able to withstand extreme weather conditions and have minimum warping, rotting and termite infestation.

A method is provided for managing the temperature of heat sensitive material located near a repair patch being thermally cured on a composite skin using a heating blanket. The method comprises configuring an assembly of thermally conductive cooling blocks to fit within a space between the heating blanket and the heat sensitive material. The assembly of thermally conductive cooling blocks is then installed against the skin within the space, forming a heat sink that conducts a portion of heat out of the composite skin away from the heat sensitive material.

To provide an apparatus such as an image display device with which extrusion of a curing resin from a prescribed place can be prevented and display failure and contamination of surroundings do not occur. A molding member exhibiting liquid repellency is disposed in an outer circumference part of the surface of a cover plate, a light-shielding part, and a base unit to be the laminating surfaces to prevent extrusion of the curing resin used for lamination and to improve generation of display failures and contamination of surroundings which may be caused by assembling failures of the apparatus such as the image display device.

An instrument panel structure includes: a base material that has both end portions in the longitudinal direction bent toward the lower face side to form a side face portion; a foamed material that covers a surface of the base material; and a skin that covers a surface of the foamed material. The instrument panel structure also includes a sealing rib that protrudes outward in the longitudinal direction from the side face portion in an arrangement position spaced apart by a predetermined gap toward the lower face side from a bent position of the base material, and to which an end portion of the skin is joined. The instrument panel structure also includes a widening rib that protrudes outward in the longitudinal direction from the side face portion on an upper face side of the arrangement position of the sealing rib on the side face portion, and is covered with the foamed material.

A honeycomb core construction that includes at least two honeycomb cores and a connection layer that is disposed between the honeycomb cores. The connection layer is configured so as to be gas-permeable, and has an adhesive for adhesively bonding to the honeycomb cores only in a region of the webs of the honeycomb cores.

Disclosed are thermoset/thermoplastic composites that include a thermoset component directly or indirectly bonded to a thermoplastic component via a crosslinked binding layer between the two. The crosslinked binding layer is bonded to the thermoplastic component via epoxy linkages and is either directly or indirectly bonded to the thermoset component via epoxy linkages. The composite can be a laminate and can provide a route for addition of a thermoplastic implant to a thermoset structure.

A heater panel includes a core and a heater/dielectric layer including a positive thermal coefficient (PTC) heater layer between a pair of dielectric layers. A structural facing is included, wherein the heater/dielectric layer is bonded directly between the core and the structural facing. A second structural facing can be bonded to the core opposite the heater/dielectric layer. An impact layer can be bonded to the structural facing, e.g., the first structural facing described above, opposite the heater/dielectric layer.