Abstract: Resin compositions, layers, and interlayers comprising two or more thermoplastic polymers and at least one RI balancing agent for adjusting the refractive index of at least one of the resins or layers is provided. Such compositions, layers, and interlayers exhibit enhanced optical properties while retaining other properties, such as impact resistance and acoustic performance.

Abstract: A popcorn patch article has a flexible substrate with a sticky surface and a facing surface opposite the sticky surface, and an acoustic texture captured on the facing surface of the substrate.

Abstract: A laminated composite structural panel with fiber reinforcement comprising a skin with a thickness e1 and a localized reinforcement or patch. The skin is made up of a stack of fibrous plies in a matrix made of a thermoplastic polymer. The localized reinforcement or patch is joined to the surface of the skin and rises to a thickness of e2 in a direction that is locally normal to the skin, which is made up of a stack of fibrous plies in a matrix made of thermoplastic polymer. The surface of the plies that make up the patch is decreasing from the ply of the patch in contact with the skin so that the edges of the patch have a slope p greater than 0.5. The patch and the skin is joined by a weld.

Abstract: A method for producing a connector, in particular for repair, in particular in the field of aviation and aerospace, including the steps of: providing a base layer; attaching a first layer of fiber composite material having a first rigidity to the base layer; attaching a second layer of fiber composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.

Abstract: A method and apparatus for managing a rework of a composite structure. Boundary geometries are identified for the layer boundaries in an image of a rework area. The image includes layer boundaries for exposed layers in the rework area. Layer orientations are identified for the exposed layers. A description of a patch for installation in the rework area is generated using the boundary geometries and layer orientations. The patch has plies having ply boundaries with the boundary geometries corresponding to the layer boundaries and ply orientations corresponding to the layer orientations. An operation of a ply cutting system is controlled using the group of files describing the patch, enabling fabricating the patch for the rework area using the group of files describing the patch.

Abstract: A wafer for repairing damage to asphalt shingles comprising a first layer of a rubberized asphalt, a fiber matrix layer and a second layer of the rubberized asphalt. The first and second layers of rubberized asphalt sandwich and are bound to the fiber matrix layer forming an integrated wafer. The wafer is formed in a select shape.

Abstract: A method for producing a molding, the shape of which is adapted to an initial mold, in which method a plurality of layers are deformably placed on top of one another such that the layers can be joined to each other by heat. The layers are deformed by being pressed onto the initial mold and in order to join the layers. Heat is applied in the deformed state. In the arrangement made of layers, at least one converter element is introduced that transforms supplied energy into heat energy and with which at least parts of the layers are heated to join the layers.

Abstract: A method for repairing damaged asphalt shingles includes inserting a tube under the damaged shingle such the terminal end of the tube lies in the vicinity of the damaged area of the shingle, pushing a liquid emulsion through the tube and under the damaged shingle in and around the damaged area, applying a sealant to the upper face of the damaged shingle to fill and seal the damaged area, applying color granules to the sealant to match the granules associated with the damaged shingle, and allowing the sealant and liquid emulsion to seal the damaged area. The method may also include forming a hole in the center of the damaged area of the shingle and applying a sealant through the tube into the hole in sufficient quantity to allow the sealant to spread underneath the damaged shingle and around the damaged area of the shingle, filling the hole with a liquid emulsion, and applying colored granules to the liquid emulsion.

Abstract: The invention relates to an appliance for repairs of local damage of laminated glasses consisting of a body with a base fitted with circumferential elastomer gasket for underpressure suction to the glass. The substance of the invention is that a closing member of an overflow valve for underpressure supply to a repair compartment is arranged so that when closing, it moves in the underpressure suction direction and pushed to a seat by generated pressure. The repair compartment is connected directly with the underpressure source via the overflow valve. A fixing compartment is connected, with the underpressure source independently. To interconnect underpressure/pressure, a lid with boreholes is used as well as a flat gasket with holes and a shape groove.

Abstract: The invention could be a windshield repair kit comprising a laminate having a protective barrier film, an adhesive layer, and a peel-able cover, the protective barrier film having at least one side to which the adhesive layer is applied, the adhesive layer being capable of cured in a presence of a UV light; the peel-able cover removably covering one or more exposed portions of the adhesive layer; a covering that removably receives the laminate, the covering reducing the transmission of UV light to the adhesive layer to a level that prevents the UV activation of the adhesive layer while the laminate is within the covering.

Abstract: A repair solution for a wind turbine blade is described. The repair solution includes the application of a layer of viscous coating material to the section of the blade to be repaired, which is cured to form a repaired surface. The layer of viscous coating material may be temporarily covered during the curing process using a film of Low Surface Energy material, to prevent defects in the repaired surface from dust, insects, etc. Additionally or alternatively, a temporary shield may be erected adjacent the curing layer of coating material, to allow for the control of the temperature and/or humidity levels of the region adjacent the curing material, to provide for more effective control of the curing process and to allow for repairs to be carried out for a wider process window.

Abstract: The present application relates to a system for supporting a roof of a portion of a mine. The system includes a first plurality of stabilizing members disposed above the roof at a first elevation. The first plurality of stabilizing members originate from a first common location and terminate at a second elevation that is higher than the first elevation. The system further includes a second plurality of stabilizing members disposed above the roof and the first plurality of stabilizing members at a third elevation. The second plurality of stabilizing members originate from a second common location and terminate at a fourth elevation that is higher than the third elevation. The second plurality of stabilizing members are disposed generally perpendicular to the first plurality of stabilizing members.

Abstract: A method of repairing a composite material is provided in which a frustum-shaped portion of a composite material is removed, and the composite material and a repair material are bonded with each other while evacuating. The repair method includes step S2 of removing a damaged part 11 from the front side so as to pass through in the thickness direction while leaving a support wall protruding inward in the radial direction from the periphery of the top face of the frustum-shaped portion; step S3 of sealing the back side by placing a sealing plate, which is inserted from the front side into a through hole formed by the removing step, on the support wall; step S5 of placing the repair material through an adhesive on the composite material where the frustum-shaped portion has been removed; and step S6 of evacuating in a state in which the front side is sealed.

Abstract: A cartridge detachably mountable to a main assembly of an image forming apparatus includes: a frame; a flexible container, provided with an opening at a side thereof and provided inside the frame, for accommodating a developer; and a sealing member for sealing the opening. The sealing member is removable when being used. The flexible container includes a bottom portion forming a bottom thereof. The bottom portion is provided vertically above a lower end of the opening in a state in which the cartridge is mounted in the main assembly.

Abstract: Techniques are disclosed for a cutting apparatus that can be used to cut a target layer within a display module, e.g., a liquid crystal display that includes a protective cover glass. The cutting apparatus includes a platform that supports a track. The cutting apparatus also includes a linear slide that is configured to both hold the display module in place and travel along the track, where the movement of the linear slide along the track is driven by a mass that is in free fall. The cutting apparatus further includes a cutting wire, where the cutting wire is positioned relative to the target layer and oscillates to cut the target layer as the linear slide moves along the track. Additional techniques are disclosed and directed toward a method for operating the cutting apparatus described above.

Abstract: A method for a repair of materials used in the manufacture of non-structural aircraft interior components includes the steps of laying fiberglass over a damaged surface and adhering the fiberglass with a fast-adhering glue, that includes at least one of cyanoacrylate and a cyanoacrylate activator for repairing the surface, to the damaged surface. A related method that includes applying a cyanoacrylate activator is used for removing pen and pencil marks for a synthetic leather material.

Abstract: A stacked semiconductor package includes a first semiconductor chip having one surface, and an other surface which faces away from the one surface, and first through electrodes which pass through the one surface and the other surface and project out of the other surface; a second semiconductor chip stacked over the one surface of the first semiconductor chip and having second through electrodes which are connected with the first through electrodes; a heat dissipation member disposed over the second semiconductor chip; and a first heat absorbing member disposed to face the other surface of the first semiconductor chip and defined with through holes into which projecting portions of the first through electrodes are inserted.

Abstract: A method and a device for recycling labeled plastic articles are described. Accordingly, the labels are detached from the plastic articles and the plastic articles treated in this way are sorted in particular automatically. During sorting, plastic articles from which the labels have not been properly detached are sorted out and again subjected to the treatment for detaching the labels.

Abstract: Optical materials including polymerizable compositions and oligomeric and polymeric material formed therefrom. The oligomer or polymer material include structural repeat units. The optical material has low or substantially no absorbance of wavelengths in at least one of the spectral regions of interest. Optical components include adhesives, waveguides, spherical or non-spherical optical lenses, architectural articles, automotive components, laminated structures and composites.

Abstract: A method and apparatus are used to fit a metallic or composite doubler on an uneven surface. A three dimensional digital map of the gap between the doubler and the uneven surface is generated by digitally scanning the uneven surface. The digital map is then used to fabricate a stack of adhesive plies tailored to substantially fill the gap between the doubler and the uneven surface.

Abstract: The invention relates to a device for tensioning the fabric of a device for restoring a removable panel, characterized in that it comprises at least one structure, a thermal chamber arranged inside said structure and able to heat said flexible fabric, an internal frame elastically secured to said thermal chamber, and at least one actuator secured to the structure and able to move the thermal chamber so that, on the one hand, the thermal chamber is moved between a fabric at rest position and a fabric stretched position and, on the other hand, to move the internal frame between a fabric at rest position and an intermediate position located between said fabric at rest and fabric stretched positions, the flexible fabric resting on part of the thermal chamber and being held by its peripheral edge between the internal frame and the structure. The invention also proposes a method for coating a removable panel that uses the tensioning device.

Abstract: A patch is used to rework an area of a structure. The patch is bonded to the structure by a layer of adhesive. A spacer placed between the patch and the structure is used to control the thickness of the adhesive and/or a bondline.

Abstract: A method for adhesive application in vehicle construction during joining of joining partners which are subject to tolerances comprises the following steps: detecting the geometric data of the joining partners in an automated manner, detecting the joint gap dimensions of the joining partners from the detected geometric data, joining the joining partners in the joining position thereof, and applying the adhesive in the joint gap.

Abstract: When a bridge pier is reinforced or repaired by wrapping a reinforcement around the pier, a waterproof sheet having a sufficient flexibility to attach to and cover the interface between the pier and the reinforcement in a liquid-tight manner is useful. The waterproof sheet is attached to the interface between the pier and the reinforcement to prevent water from penetrating into the interface for thereby preventing the reinforcement from deterioration.

Abstract: A repair part enables rapid and efficient repair of damaged metal structures, in particular airframe fuselage skins having internal and external faces, without necessitating any additional thickness compromising the transmission of waves. To this end, the repair part includes a double internal/external plate adapted to be fastened to the internal face and the external face of the metal structure, respectively. The repair part also includes a central hub connecting the internal plate and the external plate and forming a groove between the plates. The part is constituted of a single composite material block, and a glass ply, lining the groove, may be positioned between the plates and the structure. The hub may have passing through it at least one orifice adapted to allow connections to pass through the structure.

Abstract: An article comprises a multi-directional textile of first reinforcing fiber tows extending in a first direction and second reinforcing fiber tows extending in a second direction. Filaments in the first fiber tows extend past a boundary of the textile and are spread. The tows are embedded in resin.

Abstract: An in-situ double vacuum debulk (DVD) composite repair system designed to produce partially or fully cured autoclave-quality hot-bond composite repairs on contoured structures. The system provides vacuum pressure for hot bond repairs to be performed on flat and contoured structures using one set-up capable of debulking (partially curing) and then fully curing composite repairs on composite and metallic aircraft structures. The use of in-situ DVD also eliminates handling of the patch/adhesive when transferring from an off-aircraft DVD chamber to the repair site on the aircraft. This can increase the probability of successful repairs because the possibility of contaminating and misaligning the adhesive and repair patch are eliminated.

Abstract: A polyurethaneurea system that includes in some embodiments Parts A and B reaction components for a polyurethaneurea, wherein an exemplary embodiment provides a Part A that comprises between 55 and 75 wt. % of an oligomeric polyol, between 3 and 7 wt. % of an aromatic diamine chain extender, and between 0.1 and 1.5% of a reactivity catalyst; Part B includes between 1 and 15 wt. % of a short aromatic diisocyanate and between 5 and 35 wt. % of an aromatic diisocyanate prepolymer that is the reaction product of a short aromatic diisocyanate and a diol. The polyurethaneurea system may further comprise an elastomer-surface activator comprising a second short aromatic diisocyanate and a second aromatic diisocyanate prepolymer, wherein at least one of the second diisocyanates may be the same as at least one of the diisocyanates of Part B.

Abstract: A doubler repair apparatus includes a composite structure having a repair area, a susceptor having an adhesive film and at least one magnetic component extending within the adhesive film on the repair area, a repair doubler patch on the susceptor and a heat source having an induction coil generally above the repair doubler patch.

Abstract: A method for joining, by adhesive bonding, at least two large joining partners in vehicle construction, in particular in aircraft construction, comprises the following steps: detecting the geometric data of the joining partners in an automated manner, detecting the joint gap dimensions of the joining partners from the geometric data, applying adhesive to one or both joint faces of the two joining partners to be joined as a function of the joint gap dimensions, joining the joining partners in the joining position, and sequentially applying joining pressure to the joint faces along the joint gap to bring the joining partners into the final joining position.

Abstract: A method for repairing a sound attenuation panel is disclosed. The panel includes a structuring skin in metal material, a resistive layer in metal material and a honeycomb structure as acoustic absorption material directly added onto the structuring skin and resistive layer. The method includes a step in which one reinforcing pin is inserted into the thickness of the attenuation panel and a step in which the reinforcing pin is secured by welding in a controlled atmosphere to the structuring skin and resistive layer respectively.

Abstract: An attachment method for securing elements to one another. The attachment method includes providing an inanimate object. The attachment method also includes providing a repair wrap. The repair wrap includes a fabric. The fabric includes one or more fibers and the one or more fibers are knit to form the fabric. The repair wrap also includes a hardening material. The attachment method further includes wrapping the fabric about a portion of the inanimate object. The attachment method additionally includes curing the hardening material.

Abstract: A repair wrap for repairing or strengthening an item. The repair wrap includes a fabric, where the fabric includes one or more fibers. The repair wrap also includes a film disposed laterally within the fabric. The repair wrap further includes a hardening material disposed in the fabric. The fabric is configured to be wrapped around a portion of an item. Curing the hardening material is configured to form a shell about the portion of the item.

Abstract: A method consistent with certain implementations involves installing a protective film on a display panel by: placing a sheet of protective film adjacent a front surface of a display panel, where the front surface comprises a surface of the display panel that is displayed when in use, and where the display panel has an edge around a periphery of the display panel; drawing protective film into full contact with the front surface of the display panel; sealing the protective film to the front surface of the display panel at a location at or near the edge of the display panel around the periphery thereof to produce a peripheral sealed edge. The protective film can be drawn into full contact with the display panel by using a vacuum. This abstract is not to be considered limiting, since other embodiments may deviate from the features described in this abstract.

Abstract: The described embodiments relate generally to methods to enhance cosmetic surfaces of friction stir processed parts. More specifically a method for applying cold spray over a weld line generated by the friction stir processing is disclosed. Methods are also disclosed for blending the cold spray applied over the weld line in with a cosmetic surface portion of friction stir processed parts. In some embodiments cold spray can be used to on its own to create a cosmetic joint between various parts. Structural joints between first and second substrates may also be formed via solid state deposition. Such joints may be strengthened through use of a hidden weld, mechanical interlocking between the substrates, and/or coupling via fasteners.

Abstract: A melamine resin decorative sheet of the present invention includes a laminate structure of a surface layer and a core layer, in which the surface layer is configured of a surface layer material composed of a surface layer base material which carries a resin containing a melamine resin on a first surface side that serves as a design surface and which carries a solid content of a thermoplastic emulsion resin on a second surface side that contacts with the core layer, and in which the core layer is configured of a heat dissipative material layer.

Abstract: An adhesive sheet for protecting the back face of a solar battery module includes a synthetic resin substrate layer, and an adhesive compound layer laminated on the back face side of the substrate layer, and the adhesive compound layer having an average thickness of 0.01 mm or greater and 1 mm or less.

Abstract: A method of processing a patch includes mounting the patch on a surface of a caul plate having at least one suction hole, and drawing a vacuum through the suction hole to maintain the patch in contact with the caul plate.

Abstract: A pattern is transferred to a surface of an object via dip transfer printing. Dip transfer printing can leave a void in the pattern on the surface of the object. An ink based label is used to repair (i.e., cover or fill) the void. The ink based label includes an ink layer and an adhesive layer. The ink layer includes a printing of each color of a four-color printing process forming an image representative of a major element of the pattern. The adhesive layer attaches the ink layer to the void in the pattern on the surface of the object. Optionally, the ink based label includes a backing layer between the ink layer and the adhesive layer.

Abstract: A method of covering an anomaly in a wall substantially to match a pre-existing texture pattern surrounding the anomaly comprises the following steps. A valve is supported on a container assembly to define a main chamber. Contained material comprising wall material concentrate and propellant material is disposed within a main chamber defined by a valve and a container assembly. An actuator relative is arranged relative to the container assembly such that displacement of a button changes the valve from a closed configuration to an open configuration. A first portion of the contained material is applied to the anomaly. A second portion of the contained material is applied to the base coat. The second portion of the contained material forms a desired texture pattern on the base coat that substantially matches the pre-existing texture pattern.

Abstract: A patch may be used to rework a composite structure in the field. The patch is bonded to the structure by a layer of adhesive and includes perforations that allow the escape of air from the adhesive as the patch is compressed against the structure. A spacer may be introduced between the patch and the structure to control the thickness of the adhesive layer.

Abstract: A method for preventive maintenance of a boat hull to restore the integrity of a fiberglass boat hull and prevent new water infiltration damage to a boat hull. The wet area repair guidelines using a surface moisture meter. Any balsa cored area reading 15% or above is considered a wet area. Any wood cored area reading 20% or above is considered a wet area. The preventive maintenance steps involve removing all through-hull fittings or hardware. Wet core areas are then dried out using heat lamps, lights or heaters, hot-vac systems, or octopus vacuum with grid system. If necessary, any area not drying out is de-cored and repaired accordingly. After repairs are finished, all through-hull fillings or hardware is reinstalled using new sealant.

Abstract: A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

Abstract: The present invention relates to a repair method using a pre-cured repairing patch, and a repaired product obtained from repairing using the repairing patch, and the present invention securely bonds a repairing patch, where an out-of-plane stiffness is required, to a repair target. In order to cover a repair target portion 23 formed in an outer panel 2 with a repairing patch 30, and bond the repairing patch 30 to a repair target, repairing plates 31, 32 that are formed of fibers and thermosetting resin, and pre-cured before repairing are used as the repairing patch 30, and a laminating step S4 of laminating the repairing plates 31, 32, and a bonding step S7 of bonding the repairing plates 31, 32 to each other are performed.

Abstract: A method for repairing a honeycomb core sandwich structural body according to the present invention is a method in which a damaged portion that is formed in a honeycomb core sandwich structural body where a honeycomb structured core is held between a first outer skin and a second outer skin and that reaches the core through the first outer skin is repaired, the method including: a repair material mounting step of mounting a repair material on the damaged portion, the repair material including a patch that covers an opening of the damaged portion, and one or a plurality of braces that support the patch; a patch bonding step of bonding the patch to the first outer skin; and a brace bonding step of bonding the brace to the second outer skin or the core.

Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.

Abstract: To reduce a time required for repairing a honeycomb core sandwich panel. A repair method according to the present invention is a repair method, in which a repair patch 20 is disposed on a repair target portion that exists on the side of a repair surface 1A of a honeycomb core sandwich panel 1, the honeycomb core sandwich panel 1 being formed by sandwiching a honeycomb structured core 10 with a plurality of cells between skins 11 and 12, the method including: a heating step of heating the repair patch 20; and a cooling step of cooling the honeycomb core sandwich panel 1 from the side of a second surface 1B opposing the repair surface 1A of the honeycomb core sandwich panel 1.

Abstract: The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes a repairing material disposing step of disposing a repairing patch 20 and an adhesive 21A to the repair target portion 14; and a heating-hardening step of heating and hardening the adhesive 21A by irradiating it with electromagnetic waves.

Abstract: A composite fabric includes: a fabric backing; an adhesive layer; a midlayer barrier bonded to the fabric backing by the adhesive layer; and an external barrier bonded to the midlayer barrier, wherein the composite fabric has a hydrostatic pressure resistance of at least 100 psi and is sufficiently flexible such that it can be formed into a tube and everted. A process and an apparatus for producing the composite fabric are also disclosed. The composite fabric is particularly suitable for use as a liner in a cured-in-place pipe repair method.

Abstract: Interlaminar features of a composite structure are laid up by placing and steering individual chopped fiber pre-preg segments onto a substrate.