Abstract: The performances and durability of a diaphragm sheet of a solar cell laminator are enhanced, and a favorable lamination work is stably performed over a long period of time. In addition, by stably performing sufficient and uniform lamination over a long period of time, a high-quality module is stably manufactured over a long period of time. A solar cell module is manufactured by using a diaphragm sheet formed of a composition containing an ethylene-propylene-diene rubber (EPDM), which is low in creep deformation and high in durability against an organic peroxide and a silane coupling agent.

Abstract: A method and apparatus for forming a stack of composite layers into a desired shape is present. The stack of composite layers may be positioned on a tool and a number of compressible supports such that the stack of composite layers may be substantially flat on the tool and the stack of composite layers may be substantially flat on the number of compressible supports. A flexible sheet may be placed on top of the stack of composite layers. A vacuum load may be applied on the stack of composite layers on the tool and the number of compressible supports using the flexible sheet such that consolidation of the stack of composite layers occurs to form a desired shape on the tool and the number of compressible supports compress during forming of the desired shape.

Abstract: A composite tool for vacuum bag processing composite parts comprises a plurality of laminated composite plies, including a facesheet adapted to have a composite part placed thereon. A gas impermeable barrier layer sandwiched between the composite plies prevents air leaks through the tool.

Abstract: Individual layers of a high gradient insulator (HGI) are first pre-cut to their final dimensions. The pre-cut layers are then stacked to form an assembly that is subsequently pressed into an HGI unit with the desired dimension. The individual layers are stacked, and alignment is maintained, using a sacrificial alignment tube that is removed after the stack is hot pressed. The HGI's are used as high voltage vacuum insulators in energy storage and transmission structures or devices, e.g. in particle accelerators and pulsed power systems.

Abstract: A method for producing a composite structure comprising fiber reinforced material by means of vacuum assisted resin transfer molding is described. The fiber material is impregnated with liquid resin, and the method comprising the steps of: a) providing a forming structure comprising a rigid mold part and a second mold part, b) placing the fiber material in the rigid mold part, c) sealing the second mold part against the rigid mold part to form a mold cavity, d) connecting a source of uncured fluid resin to at least one resin inlet communicating with the mold cavity, e) connecting at least one vacuum outlet communicating with the mold cavity, f) evacuating the interior of the forming structure through the at least one vacuum outlet, g) supplying uncured resin from the source of uncured resin to the mold cavity through the at least one resin inlet so as to fill the mold cavity with resin, and h) curing the resin in order to form the composite structure.

Abstract: The method comprises the steps of arranging a bunch of cloths stacked onto one another; taking a label (4) containing a respective identifying code of the upper cloth (30) of the bunch, laying onto the label one end (23), provided with a cavity, of a gripping element (21) and creating in the cavity a pressure lower than an ambient pressure, so that the label obstructs the cavity; laying the label onto a labelling area (3b) of the upper cloth, and fixing the label to the upper cloth; moving the labelling area (3b) of the upper cloth by shifting the gripping element (21), maintaining in the cavity a pressure lower than an ambient pressure; increasing pressure in the cavity of the gripping element until the label gets off it, so that the labelling area (3b) of the upper cloth (30) reaches a firm position away from the respective labelling area (3b) of a cloth (31) lying directly below the upper cloth, so as to enable a subsequent application of a respective label (4) onto the respective labelling area (3b) of th

Abstract: A lamination apparatus, including: a substrate support; an adhesive film support that is disposed so as to be spaced from the substrate support; an air injection head that is disposed on a co-plane with the adhesive film support so as to be spaced apart from the substrate support or disposed so as to be further spaced apart from the substrate support than the adhesive film support; an air pump that supplies air to the air injection head; an air supply pipe that connects the air injection head with the air pump, wherein the air injection head includes an ion generation unit.

Abstract: A composite skin and composite stiffeners are co-cured in an autoclave. Uncured stiffeners are placed in channels of a tool, and an uncured skin is placed on the tool contacting the stiffeners. The vacuum bag is sealed over the tool. Bladders placed in the stiffeners are exposed to autoclave pressure through a manifold system employing vent tubes that pass through the vacuum bag along a side of the tool.

Abstract: The present disclosure is directed to a substrate lamination system and method. A method for laminating substrates may comprise: (a) disposing a pressure-sensitive adhesive later between a substantially planar surface of a first substrate and a substantially planar surface of a second substrate; (b) disposing the first substrate, pressure-sensitive adhesive layer and second substrate within a vacuum chamber; (c) evacuating the vacuum chamber; (d) applying pressure to at least one of the first substrate and the second substrate. A system for laminating substrates may comprise: (a) means for disposing a pressure-sensitive adhesive layer between a substantially planar surface of a first substrate and a substantially planar surface of a second substrate; (b) means for disposing the first substrate, pressure-sensitive adhesive layer and second substrate within a vacuum chamber; (c) means for evacuating the vacuum chamber; (d) means for applying pressure to at least one of the first and second substrates.

Abstract: A method for fabricating a one-piece composite fuselage section that minimizes out-of-plane fiber distortion. This is accomplished by fabricating a mandrel having a coefficient of thermal expansion in the hoopwise direction that is sufficiently greater than that of the laid-up composite ply assembly. As a result of this differential in the coefficients of thermal expansion in the hoopwise direction, the laid-up composite ply assembly is stretched circumferentially as the mandrel expands radially during cure, thereby eliminating or reducing out-of-plane fiber distortion. At the same time, the mandrel and part being fabricated should have substantially the same coefficient of thermal expansion in the lengthwise direction. As the outer surface of the mandrel increases in circumference, the circumferentially oriented reinforcing fibers of the inner plies are stretched, while the circumferentially oriented reinforcing fibers of the outer plies do not reduce in circumference and thus do not form waves or wrinkles.

Abstract: Structural preform layers of multiple rigid unidirectional strength elements or rods are constructed and arranged for use in fabricating load-bearing support structures and reinforcements of wind turbine blades. Individual preform layers include multiple elongate unidirectional strength elements or rods arranged in a single layer along a longitudinal axis of the preform layer. Each preform layer includes one or more fibrous carrier layers to which the multiple strength elements or rods are joined and arranged in the single layer. Each strength element or rod is longitudinally oriented and adjacent to other elements or rods. Individual strength elements or rods include a mass of substantially straight unidirectional structural fibers embedded within a matrix resin such that the elements or rods have a substantially uniform distribution of fibers and high degree of fiber collimation.

Abstract: A protective envelope for a lid of a plastic cup comprises a vacuous plastic film stuck on the top of the lid which was beforehand vaporized by an antiseptic liquid, without alcohol, then dried. The plastic film includes a detachable part, activated by a thread to be pulled, which is positioned above the opening to drink of the lid. So, when a consumer is ready to drink, he removes the detachable part by pulling the thread, so freeing the opening to drink. With such protection the lid is protected from bacteria and virus which can cause diseases. In brief, the steps of conception of the antiseptic lid are: to vaporize the lid with an antiseptic liquid without alcohol, to dry the lid, to put a thin film of plastic onto the lid by positioning the detachable part over the drink opening and to stick the film onto the lid by means of a vacuum.

Abstract: A method of making a compacted composite material preform including providing a pre-impregnated preform comprising a plurality of reinforcing fibers and a polymer matrix and positioning the preform on a base plate. The method includes enclosing the preform inside a vacuum bag defining a first cavity and enclosing the preform and vacuum bag inside a substantially rigid cover defining a second cavity. The method includes drawing a vacuum in the first cavity and the second cavity that is substantially equal or greater than the vacuum in the first cavity to remove air and volatiles from the preform. The method includes drawing a greater vacuum in the first cavity relative to the second cavity to urge the vacuum bag into compressive contact with the plurality of reinforcing fibers and the polymer matrix to a compacted arrangement.

Abstract: 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.

Abstract: A skin adhesion apparatus includes an upper mold half and a lower mold half. The upper mold half and the lower mold half clamps a core material and a skin laid on the core material so that the skin is adhered to a surface of the core material. Disposed along a mold surface of the upper mold half is a tubular member made of elastic material. The skin adhesion apparatus also includes a pump for supplying fluid into the tubular member. When adhering the skin to the core material, the upper mold half is pulled down and then stopped at a predetermined distance above the core material. After then, fluid is supplied into the tubular member so that the fluid pressure inflates the tubular member.

Abstract: Apparatus and methods of forming a molded thermoplastic piece are provided. The molded thermoplastic piece can have an outer layer of one or more sheets of reinforced flexible thermoplastic and a porous layer, such as cork. The outer layer can a mechanical bond with the porous layer.

Abstract: A process for manufacturing a piece made of composite material that includes fibers that are immersed in a resin matrix, whereby the piece is placed in a first chamber with at least one flexible wall. The process includes a thermal cycle with essentially a first phase (50) at a first temperature during which the resin is liquid or in the “gel” state, and then a second phase (52) at a second temperature that is higher than the first during which solidification of the piece takes place by polymerization of the resin. An external pressure is applied to the outside of the first chamber and an internal pressure is generated inside the first chamber, wherein during the first phase (50), the relative internal pressure is less than 0 during a first period, and then greater than 0 during a second period preceding the beginning of the polymerization for reducing the porosity rate.

Abstract: Disclosed are fluid transfer and evacuation structures formed in a vacuum bag operable for use in vacuum-assisted resin transfer molding, debulking, compaction, or similar processes. A reusable vacuum bag can be provided including an elastomeric membrane having a preform-contact surface and at least one textured surface formed in the elastomeric membrane. The textured surface can define a fluid transfer channel. At least one fluid extraction port can be provided in communication with the fluid transfer channel, the fluid extraction port being adapted for engagement to a vacuum pump to remove fluids from the fluid transfer channel. The textured surface defining the fluid transfer channel can be adapted to permit the flow of fluids between the elastomeric membrane and a base mold in communication with the elastomeric membrane when the fluid extraction port is engaged to a vacuum pump.

Abstract: Panels usable for construction of a surface, to provide the surface with a desired appearance, durability, water, air, and fire resistance, dimensions, and weight include a layer of substrate material having first and second sides. Finish elements are positioned on the first side, while a backing material is positioned on the second side, such that the substrate bonds the finish elements to the backing material. Particulate material can also be included, such as within spaces between finish elements. Manufacture of such panels can include use of a vacuum system that acquires finish elements in a selected orientation, acquires particulate material into spaces unoccupied by finish elements, then deposits the arranged finish elements and particulate material into a mold for subsequent manufacturing steps. Use of lightweight, durable materials, such as magnesium oxide, can enable panels having a reduced thickness and weight to be manufactured, without sacrificing durability or longevity.

Abstract: A method for producing, in a composite material, a component that has a re-entrant angle, includes stacking layers of fibres which have been pre-impregnated with a resin so as to obtain a preform and placing the preform in a tooling fixture in order to subject it to a polymerization cycle including a temperature cycle, with a temperature-increase phase and at least one soak at which the temperature is maintained, and a pressure cycle on the outside of the tooling fixture with a pressure-increase phase and a pressure-hold phase, with the layers of pre-impregnated fibres being able to slip against one another when the temperature of the temperature cycle is equal to or higher than a threshold temperature Tf dependent on the resin. The temperature-increase phase includes a soak at a temperature higher than or equal to Tf, the soak beginning before the end of the pressure-increase phase.

Abstract: A composite comprising a combination of a self-healing polymer matrix and a carbon fiber reinforcement is described. In one embodiment, the matrix is a polybutadiene graft copolymer matrix, such as polybutadiene graft copolymer comprising poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). A method of fabricating the composite is also described, comprising the steps of manufacturing a pre-impregnated unidirectional carbon fiber preform by wetting a plurality of carbon fibers with a solution, the solution comprising a self-healing polymer and a solvent, and curing the preform. A method of repairing a structure made from the composite of the invention is described. A novel prepreg material used to manufacture the composite of the invention is described.

Abstract: The imaging device includes a sensor substrate, a light-blocking substrate, a light-collecting substrate, a sealing material, and a light-transmitting member. The light-transmitting member includes a light-transmitting base disposed to be in contact with either the sensor substrate or the light-blocking substrate, and a light-transmitting resin which is filled between the base and the sensor substrate or the light-blocking substrate. A void is formed in at least a part of a space between the sealing material and the light-transmitting member.

Abstract: To provide a lamination method and a lamination system capable of excellently laminating a film-type laminate without damage even though the semiconductor is a brittle lamination target such as a foil-type semiconductor or a semiconductor made of highly brittle material. In a lamination method for laminating a film-type laminate to a brittle lamination target by overlapping the brittle lamination target and the film-type laminate and heating and pressing the brittle lamination target and the film-type laminate, with respect to the brittle lamination target mounted on a mount member and carried into a lamination device, an eleastic film member is expanded into a vacuum chamber of the lamination device from the above to press and laminate the brittle lamination target and the film-type laminate.

Abstract: A method is disclosed for forming a seal on a vacuum bag used in an infusion molding process. A seal profile having a first part and a second part is attached to a supporting surface and resin is applied to the seal profile to form a mold layer. The mold layer and the seal profile are separated from the supporting surface. The second part of the seal profile is separated from the first part of the seal profile. A silicone resin is applied to the mold layer and the first part of the seal profile to form the seal and the vacuum bag. A vacuum cavity is created between the mold layer and the second resin when the second resin is applied to the first part of the seal profile.

Abstract: The invention relates to a method for the production of sandwich components with an open core structure and a cover layer applied to each side, wherein the cover layers are formed with a curable plastic material, and the sandwich component is cured in a closed device under pressure. A charging gas, which may be nitrogen or air, is introduced to the core structure prior to at least partial solidification of the cover layers, wherein a charging gas pressure p Charging gas is selected that is less than or equal to an operating pressure p operating of the closed device in order to, in particular, at least largely prevent the formation of sink marks in the cover layers. Furthermore, the invention relates to a press for implementing the method.

Abstract: A method for manufacturing a laminated board, comprising: preparing a first and a second prepregs 30a, 30b with a carrier by laminating the carrier with an insulating resin layer in which a fiber cloth is embedded, and laminating the first and the second prepregs 30a, 30b with a carrier by bonding the insulating resin layer in the first prepreg 31a with a carrier and the insulating resin layer in the second prepreg 31b with a carrier directly or via an additional member under reduced pressure and heating it.

Abstract: A V-ribbed belt that includes a ribbed surface covered with fabric is provided. The fabric is stretchable in two predetermined directions. A method for manufacturing the V-ribbed belt is also provided. The method includes placing a belt matrix about a mandrel, placing a fabric about the external circumference of the belt matrix which wraps around the mandrel, placing the mandrel inside a shell having a plurality of grooves on the internal circumference, expanding the belt matrix and the fabric toward the internal circumference of the shell and thus pressing the fabric onto the internal circumference having the multi-ribbed structure, and curing the belt matrix with the fabric. The fabric is stretchable to accommodate itself to the multi-ribbed structure.

Abstract: The present invention relates to a method for the manufacture of a composite article comprising a composite plate (1) and at least one fitting (4). The method is characterized by the steps of arranging at least one former on said composite plate (1), arranging at least one fitting (4) on said composite plate (1), producing a lay-up by applying a composite material layer (9) least partly covering an external surface of the former and of the fitting, and curing the layup in a curing process. After curing, said composite material layer (9) forms the walls of a stiffener and at least partly encloses the fitting so as to support it in a predetermined position.

Abstract: A label applicator that includes an applicator housing having a flow chamber and a suction side. The suction side has one or more openings that allow air to pass therethrough. The label applicator also includes first and second air flow generators that are fluidly coupled with the flow chamber. The first and second air flow generators are configured to generate first and second air flows, respectively, through the flow chamber. The label applicator also includes a valve mechanism that is positioned in the flow chamber to direct the first and second air flows through the flow chamber of the applicator housing. The valve mechanism includes a diverter valve and an electric actuator. The actuator is configured to move the diverter valve within the flow chamber to different positions during a label application operation.

Abstract: A laminate and a method of forming the laminate, including a fiber reinforced polymer layer and a glassy metal foil layer. The fiber reinforced polymer layer comprises fibers present in a polymer matrix. The glassy metal foil layer comprises an iron based glass forming alloy including nickel, boron, silicon and optionally chromium and exhibits spinodal glass matrix microconstituents including a glass matrix and a semicrystalline/crystalline phase.

Abstract: This present invention provides a masking method for locally treating surface of a workpiece by masking the workpiece. The workpiece has a targeting treatment area and a non-targeting treatment area. The masking method includes: covering a fixture on the non-targeting treatment area of the workpiece to expose the targeting treatment area of the workpiece; by using an adsorbing force existing between the fixture and the workpiece, getting the fixture to closely contact with the non-targeting treatment area of the workpiece and to make an end edge of the fixture correspond to the edge of the targeting treatment area of the workpiece, wherein the adsorbing force is a vacuum adsorbing force or a static electric adsorbing force. Thereby the surface treatment only effects in an area within the range of the targeting treatment area of the workpiece so as to reduce the treatment defect.

Abstract: A method of bonding a film (2) to a curved substrate (1) comprises preforming the film by applying a pneumatic pressure difference between two sides of the film and by heating said film. An intermediate shape is then conferred on the film, which is suitable for applying the film against a curved face of the substrate. This application is carried out, on the one hand, by keeping the film m the intermediate shape by means of an adjusted pressure difference applied between the two sides of the film and, on the other hand, by pressing the substrate against the film by means of a movable support (12-14). Such a method is used to obtain a defect-free ophthalmic lens with a film bonded to it.

Abstract: Apparatus for processing a workpiece comprises a base adapted to have a workpiece placed thereon. A vacuum bag is placed over the workpiece, and the bag is sealed to the base using inner and outer seals. The inner and outer seals are spaced apart from each other to form a channel therebetween. A vacuum port coupled with a vacuum source is used to evacuate air from the channel.

Abstract: A method of manufacturing a flanged composite component is provided. The method includes coupling a composite structure to s first composite material. The method includes coupling a second composite material to the composite structure and placing a first expansion device within the composite structure. A forming element is coupled to at least one of the first composite material, the composite structure, and the second composite material against the mold. The method includes coupling a pressure element to the forming element to define a space among the mold, the forming element, and the pressure element. The method includes expanding the first expansion device to impart a force to the second composite material to move the second composite material away from the composite structure and into the space to facilitate forming a first flange.

Abstract: A setup device for manufacturing a fuselage barrel, made of a fiber composite material, for an aircraft is provided. The setup device for the purpose of reinforcement includes several stringers arranged so as to be spaced apart from each other. The stringers include a base structure to form a load-bearing rigid substructure that is connected to an outwardly curved supporting surface that can be adjusted by means of actuators for the positive setup of the fuselage barrel to be manufactured with the help of form channels for accommodating the stringers. The actuators, designed as pressure-means cylinders, move one or several form channels in radial direction. The form channels are interconnected longitudinally by means of a flexible intermediate element for forming a ring-shaped supporting surface that is closed in a vacuum-tight manner and that overall is able to adjust itself in radial direction.

Abstract: A substrate sealing apparatus includes a chamber, at least one lower compressing member, and at least one lower compressing member. The lower compressing member includes a lower compressing surface for emitting heat, is configured to be elevated up and lowered down in a vertical direction with respect to the compressing surface, and rotates about the vertical direction. The upper compressing member includes a lower compressing surface for emitting heat, and is configured to be elevated up and lowered down in the vertical direction.

Abstract: A pressure debulking system includes a debulking chamber having a debulking chamber interior, a pressure bladder having a bladder interior provided in the debulking chamber interior, a vacuum port disposed in fluid communication with the debulking chamber interior and a pressure port disposed in fluid communication with the debulking chamber interior. A pressure debulking method is also disclosed.

Abstract: A portable air clamp for use during lamination of substrates is provided. The clamp includes a top clamp plate, a bottom clamp plate and at least one flexible, expandable tube within a housing of the clamp. The top clamp plate is adjacent to a top housing and the bottom clamp plate is adjacent to a bottom housing. An expandable tube or bladder may be disposed in the top housing or the bottom housing. The clamp may also include alignment devices and mechanisms for ensuring proper alignment of the substrates during the laminating procedure. The clamp is adapted to provide uniform pressure along the surfaces of the substrates to be laminated.

Abstract: A method of manufacturing a cell array structure includes a first step of laminating a deformable layer capable of causing plastic deformation on a substrate, the substrate being formed with plural, mutually separated depressions on a top surface thereof, such that the deformable layer forms a mutually isolated space in each of the plural depressions; and a second step of extending the space in each of the plural depressions by causing plastic deformation in the deformable layer, such that there are formed plural columnar cells respectively in correspondence to the plural depressions.

Abstract: Methods for assembling diaper pants are disclosed herein. Each diaper pant may include a chassis and two side panels extending from the chassis. The side panels join a first waist region and a second waist region of the chassis. The methods may include the step of transferring the chassis to a rotating drum including a chassis folding member, a first panel folding member and a second panel folding member. The chassis may be folded about a lateral axis by the chassis folding member. The first and second folding members may also move toward each other and radially outward relative an outer surface of the rotating drum to position second end regions of the side panels in contact with a second waist region of the chassis. The second end regions of the side panels may be connected with the second waist region.

Abstract: A flexible compaction sheet is used to compact uncured composite plies onto the surface of a ply layup. The compaction sheet includes a peripheral seal that seals the perimeter of the sheet to the surface of the part layup and forms a vacuum chamber over the plies which is evacuated through the sheet to apply compaction pressure to the plies.

Abstract: A caul plate system for a laminate structure includes a plurality of layers of curable caul plies disposed over a laminate structure and substantially conforming to a surface of the laminate structure. A resin is applied to the plurality of layers of caul plies. Co-curing of the plurality of layers of caul plies with the laminate structure hardens the plurality of layers of caul plies such that a normal pressure is applied to the laminate structure during cure of the laminate structure.

Abstract: Provided herein is a blend composition useful as a cross-linkable encapsulant layer and consisting essentially of two ethylene copolymers and optionally one or more additives. The first ethylene copolymer comprises copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a second olefin having the formula CH2?C(R3)COOH. The second ethylene copolymer consists essentially of copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a third olefin having the formula CH2?C(R4)D. R1, R3 and R4 represent hydrogen or an alkyl group; R2 represents an alkyl group; and D represents a moiety containing an epoxy group. Further provided are solar cell modules comprising the encapsulant layer. The encapsulant layer comprises the blend composition or the product of cross-linking the blend composition, in which some acid groups of the second olefin have reacted with some epoxy groups of the third olefin.

Abstract: Provided herein is a blend composition useful as a cross-linkable encapsulant layer and consisting essentially of two ethylene copolymers and optionally one or more additives. The first ethylene copolymer comprises copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a second olefin having the formula CH2?C(R3)COOH. At least a portion of the carboxylic acid groups have been neutralized to form carboxylate salts. The second ethylene copolymer consists essentially of copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a third olefin having the formula CH2?C(R4)D. R1, R3 and R4 represent hydrogen or an alkyl group; R2 represents an alkyl group; and D represents a moiety containing an epoxy group. Further provided are solar cell modules comprising the encapsulant layer.

Abstract: A slide-room for installation in a recreational vehicle or other structure is disclosed. The slide-room comprises a shell, which can be constructed from fiberglass. The shell comprises an end wall, a ceiling, a floor, two opposing side walls, and a flange extending from the end wall, wherein the end wall, the ceiling, the floor, the side walls and the flange comprise a one-piece, unitary construction. Also disclosed are methods for molding composite components, such as slide-room. In one specific implementation, the shell for a slide-room is formed from fiberglass using a vacuum assisted resin transfer process.

Abstract: The present invention is a process for performing a planarization treatment of pressure-sensitive adhesive (PSA). The process includes positioning a first substrate onto a support surface of a planarization tool. The process further includes placing at least one layer of PSA onto the first substrate. The process further includes positioning a second substrate onto the layer(s) of PSA. The process further includes applying a pressure to the second substrate via a flexible membrane, said pressure being applied in a generally uniform, unidirectional and localized manner. Further, the applied pressure flattens the PSA between the first substrate and the second substrate for promoting suitability of the PSA for use in rigid-to-rigid lamination processes.

Abstract: A safety laminate comprises an interlayer that comprises a crosslinkable blend of ethylene copolymers. The first ethylene copolymer comprises copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a second olefin having the formula CH2?C(R3)COOH. The first ethylene copolymer is optionally at least partially neutralized. The second ethylene copolymer consists essentially of copolymerized units of ethylene, optionally a first olefin having the formula CH2?C(R1)CO2R2, and a third olefin having the formula CH2?C(R4)D. R1, R3 and R4 represent hydrogen or an alkyl group; R2 represents an alkyl group; and D represents a moiety containing an epoxy group. The crosslinkable blend is useful as an interlayer in safety laminates. Methods for preparing the safety laminates are also provided.

Abstract: A manufacturing method for a composite sheet which includes: conveying a first continuous sheet in a first direction so as to abut a depressed surface of a mold member; forming an absorbent body by depositing liquid-absorbent particles on a portion of the first sheet proximal to a suction hole of the mold; and joining a second sheet over the first sheet having the absorbent body that is deposited therebetween, the second sheet being continuously transported in the first direction. A plurality of opposed slope members guide the liquid-absorbent particles onto the first sheet located on the mold member. At least one of the plurality of slope members causes the liquid-absorbent particles to reverse their falling direction from an upper slope member.

Abstract: In order to produce photovoltaic modules or modules bearing functional coatings, a strand (3) composed of sealing composition is arranged along the outer edge of a glass sheet (1) and at least one photovoltaic cell (11) and/or at least one functional coating, for example a light-emitting coating, are/is applied within the strand (3). As a next step, a composition (13) is applied to the glass sheet (1) within the strand (3). A second glass sheet (3) is then placed onto the strand (3) at a distance from the free surface (5) of the strand (3) and the arrangement is evacuated. The evacuated arrangement is compressed in a heating press, such that the entire interior space (9) between the glass sheets (1) and (2) and within the sealing strand (3) is filled by composition (13), which is a pasty gel-like composition e.g. a resin, or a silicone-based composition.

Abstract: A substrate-bonding apparatus for a display device, and which includes a chamber unit configured to bond a carrier substrate to a substrate for manufacturing the display device; a first surface plate provided inside the chamber unit and configured to support the substrate; a supporting unit provided inside the chamber unit and configured bring the carrier substrate into contact with the substrate supported by the first surface plate; and a pressure-adjusting unit communicating with the chamber unit and configured to change a vacuum pressure from a low vacuum pressure to a high pressure in multiple steps inside the chamber unit while the carrier substrate is brought into contact with the substrate to bond the carrier substrate to the substrate without adhesive material between the carrier substrate and the substrate.