Abstract: A method and apparatus for reworking a composite structure. A composite rework patch system comprises a composite rework patch and a plurality of adhesive layers. The composite rework patch includes a first side having a contour conforming to an inconsistent area on the composite structure. The composite re patch comprises a plurality of regions having different structural properties. The plurality of adhesive layers is on the first side of the composite rework patch. The plurality of adhesive layers change in thickness within at least one region of the composite rework patch to form tapered adhesive sections.

Abstract: A composite comprising adhered components and method of refurbishing such composites are described herein. The composite includes a first component, a second component, and the first component being adhered to the second component using an adhesive stack. The adhesive stack comprises a first adhesive-impregnated scrim layer disposed between the first component and the second component and a bulk adhesive layer disposed between the first component and the second component.

Abstract: The present invention is a method to make an environmentally friendly polyurethane molded article (100) comprising at least 20 percent renewable materials and molded articles made therefrom. Specifically, the method provides for molding a polyurethane coated sandwich structure (40) comprising a honey comb core (30) having fiber reinforcing layers (10, 20) to provide an environmentally friendly polyurethane molded article with a desired shape such as an automobile load floor. The polyurethane coating is derived from a polyurethane—forming mixture comprising an isocyanate component and a polyol component. Specifically, the polyol component comprises one or more natural oil based polyol, preferably comprising at least one of a hydroxymethylated fatty acid or a hydroxymethylated fatty acid (methyl) ester.

Abstract: A device and method to repair a structural component. The device includes a plug that bonds to the structural component. The plug includes a flange and a solid shank extending from the flange, the solid shank being disposable in an opening of the structural component. The device further includes disc that bonds to the structural component such that, when bonded, the disc covers the solid shank of the plug. The method includes bonding the plug to the structural component such that the solid shank of the plug is disposed in the opening of the structural component. The method further includes bonding the disc to the structural component.

Abstract: A method of repairing a composite component having a damaged area including: laying a composite patch over the damaged area; activating the shape memory polymer resin to easily and quickly mold said patch to said damaged area; deactivating said shape memory polymer so that said composite patch retains the molded shape; and bonding said composite patch to said damaged part.

Abstract: Present embodiments include a remanufactured bandage-type medical sensor having an optical assembly with an emitter adapted to transmit one or more wavelengths of light and a photodetector adapted to receive the one or more wavelengths of light transmitted by the emitter. The sensor also includes a laminate assembly having an electrically conductive adhesive transfer tape (ECATT) layer disposed over the photodetector, and the ECATT layer is adapted to shield the photodetector from electromagnetic interference (EMI). A nonconductive layer supports the emitter, the photodetector, and the ECATT layer within the sensor. At least a portion of the optical assembly is from a used bandage-type medical sensor, and at least a portion of the laminate assembly is new.

Abstract: A repair process for a composite material panel that forms part of a fuselage, wings, or stabilizers of an aircraft, with the panel having large dimensions and including irregular contours in some areas and edges prone to damages occurring from handling and assembly of the panel. The process a) locates the damage in the element of the composite material panel; b) sands the area that includes the damage in an area larger than the damage, makes a cut in the panel, having the cut of a same form as a piece that will serve to repair panel; c) places the piece in the cut, so that it is perfectly flush with the panel to be repaired; and d) attaches the piece to the composite material panel.

Abstract: An area of a structure is reworked from one side of the structure using resin infusion of a dry fiber patch. Entrapped air and excess resin is removed from the patch during the infusion process by inserting a vacuum device into the patch, and forcing the area resin through the vacuum device.

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 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: A method for reworking an electrically conductive layer of a composite skin is disclosed in which a patch replaces the altered section of the electrically conductive layer. The method is performed by removing a portion of the electrically conductive layer to reveal the underlying composite skin. A patch is formed, having an electrically conductive section coupled to an adhesive having a low dielectric breakdown strength, and is then introduced over the underlying composite skin such that the adhesive layer covers the underlying composite skin and overlaps an unremoved portion of the electrically conductive layer. The patch is applied such that the electrically conductive section within the patch covers the adhesive layer and overlaps the unremoved section of the electrically conductive layer. The adhesive layer preferably has a low dielectric breakdown strength, so that electricity from lightning which strikes the composite skin may be conducted through the adhesive.

Abstract: The present disclosure provides a method of repairing a damaged portion of a panel formed of composite material. The method includes preparing the damaged portion for repair and applying a pressure responsive adhesive layer to substantially cover the damaged portion. The method also includes disposing a vacuum-assisted resin transfer molding repair patch assembly to substantially cover the damaged portion and substantially covering the repair patch assembly with a vacuum bag assembly. Resin is introduced into and impregnates the repair patch assembly. The repair patch assembly is cured after being impregnated.

Abstract: A system for stopping in an opening a flow of a fluid, wherein the system comprises: a kneadable silicon based polymer for fitting in and/or onto the opening so as to block any flow of the fluid through the opening, wherein the silicon based polymer comprises fillers so that the density of the silicon based polymer is higher as compared to the density of the silicon based polymer that does not comprise these fillers, and a silicon based sealant for applying against a dried form of the silicon based polymer, wherein the silicon based sealant is vulcanizable under exposure to humidity.

Abstract: A method of forming a repair patch for repairing a damaged inflatable object is provided. The method comprises forming a backing formed polyimide material and applying as adhesive material to the backing, for securing the polyimide backing material to the inflatable object. The backing may be formed as a thin film of polyimide material and the adhesive may be formed as thin film of adhesive having a high temperature resistance, e.g. 300° F. or higher. The adhesive may be formed of silicon or acrylic contact adhesive having high temperature resistance. The release layer may be applied to the adhesive material.

Abstract: The present invention relates to a method of repairing a fiber composite solid member having a locally deteriorated surface area, such as having cracks or creases. The solid member may e.g. be a mold for the manufacturing of wind turbine blades or such blades. The method comprises machining a surface section comprising the locally deteriorated surface area in order to obtain a recess having a predefined depth and circumferential shape, placing a repair patch having a predefined thickness and circumferential shape matching the recess in the recess, and fastening the repair patch to the solid member by use of a binder material. At least some of the elastic and thermal properties of the repair patch and the binder material are so that after fastening, the repair patch and the binder material in combination have elastic and thermal properties which are substantially the same as the corresponding properties of the surface section before machining.

Abstract: Method and apparatus for the production, forming bonding, joining and repair systems composite and metal components utilizing at least one pressure chamber having a displaceable abutment face, wherein fluid is circulated at an elevated temperature and pressure through the pressure chamber.

Abstract: A system for producing and repairing plastic composite components with a laminate structure includes a prefabricated woven fibre blank, which is enclosed in a safety sleeve, with the safety sleeve is in turn completely enclosed by a processing sleeve. After the safety sleeve is removed from the processing sleeve and a desired cutout contour is marked on the processing sleeve, the woven fibre blank can be replaced in the processing sleeve and impregnated with adhesive there. The advantage of this system is the prefabrication of the woven fibre blank and the almost contactless processing of the woven fibre blank.

Abstract: A method and apparatus for bonding parts. An adhesive and a plurality of beads may be applied onto a first surface of a first part to form a layer of adhesive and beads. The first surface of the first part with the layer of adhesive and beads may be placed in contact with a second surface of a second part to form a structure, wherein the structure may be cured.

Abstract: A method and system for repairing a crack in a concrete structure is provided including securing a plurality of ports at spaced intervals along the crack, adhering a carbon fiber panel to the concrete structure over the top of a crack, and injecting epoxy into each of the plurality of ports to fill the crack while the adhered carbon fiber panel seals the injected epoxy within the crack to provide a reliable epoxy-filled crack repair process.

Abstract: The invention relates to a method for at least partially reworking or replacing a reinforcement element of a fibre composite structure. In a first method step, at least one fibre layer is arranged on a surface section of the reinforcement element and/or at least one replacement section of the reinforcement element of the same material and same layer structure is arranged on a surface reinforcement section of the fibre composite structure. In a second method step, at least a pressure mat adjusted to the contour of the reinforcement element is disposed above the at least one fibre layer and/or the at least one replacement section of the reinforcement element, wherein the at least one pressure mat is supported and fixed in a nominal position by a fixing frame adjusted to the contour of the reinforcement element. In a third method step, the at least one pressure mat is then acted upon by a pressure medium in order to press the same against the reinforcement element and the fixing frame.

Abstract: A windshield repair apparatus includes a bridge for holding an injector adjacent to a break area of a windshield. The bridge includes a suction cup for mounting the bridge to the windshield. An articulating arm mounts to the bridge for holding equipment, such as a flashlight, a tool holder, and/or a sun blocker. The bridge includes a pivotally mounted arm which allows for pivotal movement of the injector away from the break area, and a registration system which allows for accurate replacement of the injector over the break area following pivotal movement back toward the break area. The arm also is pivotally moveable toward and away from the windshield and is controlled by a threaded adjustment mechanism. The injector is also threadably adjustable vertically relative to the windshield. The articulating arm includes a quick connect/disconnect feature.

Abstract: A method of repairing a composite component having a damaged area including: laying a composite patch over the damaged area; activating the shape memory polymer resin to easily and quickly mold said patch to said damaged area; deactivating said shape memory polymer so that said composite patch retains the molded shape; and bonding said composite patch to said damaged part.

Abstract: One possible embodiment of the invention could be a methodology of preventing an existing crack or break in the vehicle windshield from becoming larger comprising of the steps, providing a laminate with a UV light-permeable barrier film having least one side to which UV light curable adhesive is applied to it, a peel-able cover reversibly applied over the adhesive; providing a windshield with at least a small crack or chip in its surface; removing the peel-able cover from the adhesive; applying the barrier film to the windshield in a manner to cover the crack or chip so that the adhesive comes in contact with the windshield; and transmitting UV light through the film to the adhesive to cure it into a rigid substrate connection between the barrier film and the windshield that resists various forces acting upon the windshield that would otherwise increase the size of crack or chip.

Abstract: A liner assembly and method for lining a damaged pipe junction between a main and lateral pipe is provided. The liner assembly includes a main liner member and a lateral liner tube. A collar disposed near the juncture between the main liner member and lateral liner tube is impregnated with a liquid hydrophobic or hydrophilic material capable of curing in a flexible or rigid state with the material expanding in the presence of water. The hydrophobic or hydrophilic material can also be applied without the use of the collar. When the liner assembly is pressed against the main and lateral pipes, a portion of the hydrophilic or hydrophobic material is forced into the damaged pipe junction.

Abstract: In accordance with various embodiments of the disclosed subject matter, a composite material is provided. The composite material in accordance with some embodiments of the disclosed subject matter includes a high tenacity fiber reinforced polymer fabric and a polyurea coating layer formed on at least one surface of the polymer fabric. The composite material provides significant strength, flexibility, and energy dissipation. In some embodiments, the composite material can be used to reinforce structural and non-structaral substrates.

Abstract: Methods for bonding substrates, forming assemblies using the same, along with improved methods for refurbishing said assemblies are disclosed that take advantage of at least one channel formed in an adhesive utilized to join two substrates to improve fabrication, performance and refurbishment of the assemblies. In one embodiment an assembly includes a first substrate secured to a second substrate by an adhesive layer. The assembly includes a channel having at least one side bounded by the adhesive layer and having an outlet exposed to an exterior of the assembly.

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 pipe or hose composed of a polyamide moulding composition whose molecular weight has been increased by condensation, via addition of a compound having at least two carbonate units in a quantitative proportion of from 0.005 to 10% by weight, based on polyamide, where a) a starting polyamide moulding composition was provided, b) a mixture of the starting polyamide moulding composition and of the compound having at least two carbonate units was produced, c) the premix was, if desired, stored and/or transported, and d) the premix was then processed to give the moulding, this step being the first in which the increase of molecular weight by condensation occurred, the moulding being a pipe or hose whose external diameter is at least 25 mm is used as inliner for a pipeline.

Abstract: A repair patch for reworking an inconsistent area of a composite structure includes a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the second patch region, with the first patch region, the first separation zone and the second patch region having increasing interlaminar fracture toughness from a center to an edge of the patch body; and a layer of adhesive for bonding the patch body to the composite structure.

Abstract: The disclosure provides, in part, adhesive patches for repairing damaged surfaces of health care devices. In one of its aspects the disclosure provides a method of repairing the surface of health care device by applying an adhesive patch over a damaged portion of the surface, the patch comprising a film layer and an adhesive layer. In another one of its aspects, the disclosure provides an adhesive patch for repairing the surface of a health care device comprising a film layer and an adhesive layer.

Abstract: The present system, method and apparatus are adapted for the quick and easy patching of inflatable devices. More specifically, the system, apparatus and methods comprise a tip, a body portion, an adhesive, a patch and a probe, wherein the tip and body portion are inserted into the inflatable device so as to apply the adhesive and patch to the interior of the device to create an air-tight seal. The disclosure thus provides an improved patching system, apparatus and method.

Abstract: The present disclosure relates to a system for monitoring a structural component. The system may include an electromechanical device to generate guided waves having a measurement surface and a bonding agent disposed on the measurement surface and configured to engage with the surface of the structural component. The system may also include a heating element for heating the measurement surface, the bonding agent, and capable of heating a portion 100 of the structural component surface. In addition, the system may include a clamp for retaining the measurement surface relative to the structural component.

Abstract: The present disclosure relates to a method for repairing a portion of an acoustic panel for a nacelle of an aircraft turbojet engine. The panel includes an acoustic skin in which a plurality of acoustic holes are drilled, a solid skin, and a cellular acoustic structure. The cellular acoustic structure, being arranged between the acoustic skin and the solid skin, has a plurality of cells, each of which has one or more drainage openings arranged in one or more of the walls forming each cell. The method includes a step of: defining a part of the acoustic panel to be cut; forming a cutting area closed by the acoustic skin; injecting a resin through the acoustic holes; positioning a replacement cellular acoustic structure in the cutting area and on the acoustic skin; forming a solid replacement skin on the replacement cellular acoustic structure.

Abstract: Method for manufacturing a continuous composite tube comprising translating a tube liner through a manufacturing station wherein the manufacturing station comprises a winding station and a consolidation station located at a distance downstream of the winding station; winding a composite tape on the tube liner at the winding station for forming a tape layer; consolidating the composite tape on the tube liner at a consolidation zone of the consolidation station by pressing and heating to the tape.

Abstract: A method is provided for repairing an aircraft structural component which has a component fault in a portion adjoining a cavity of the aircraft structural component. The method includes removing a region of the aircraft structural component that has the component fault, introducing an expansion body into the cavity of the aircraft structural component through an opening that has been formed by the removal of the region of the aircraft structural component having the component fault, wherein the expansion body while being introduced into the cavity of the aircraft structural component is in a non-expanded state, converting the expansion body that has been introduced into the cavity of the aircraft structural component to an expanded state, and closing the opening by means of a repair material.

Abstract: A surrogate patch assembly for a rework area of a structure comprises a surrogate patch body which may be formed of a material for drawing moisture from the rework area. The patch assembly may include a sensor mounted to the surrogate patch body. The sensor may comprise a thermal sensor for sensing the temperature of the rework area and the surrogate patch body. The sensor may comprise a moisture sensor for sensing moisture drawn into the surrogate patch body.

Abstract: Embodiments disclosed herein relate to one or more embodiments of and methods to repair a flexible pipe. A method to repair damaged flexible fiber-reinforced pipe which includes a plurality of helically-wrapped stacks of laminated strips of material is disclosed. The method includes removing a portion of existing stacks from a damage location, applying an adhesive to a surface of replacement stacks, installing the replacement stacks to the damage location, binding the replacement stacks to remaining existing stacks with the applied adhesive, and installing a replacement jacket over the replacement stacks.

Abstract: A repair patch for reworking an inconsistent area of a composite structure includes a patch body adapted to cover the inconsistent area and having a first patch region, a second patch region outside the first patch region and a first separation zone between the first patch region and the second patch region, with the first patch region, the first separation zone and the second patch region having increasing interlaminar fracture toughness from a center to an edge of the patch body; and a layer of adhesive for bonding the patch body to the composite structure.

Abstract: Disclosed is a soundproof material fabricated using recycled polyurethane foam from waste seats and a process of fabricating the same, and more particularly, a soundproof material fabricated by stacking a thermoplastic polymer on a sound absorbing material including recycled polyurethane foam from seats from end-of-life vehicles and a process of fabricating the same. Use of recycled resources provides an eco-friendly impact, reduces manufacturing costs for parts, and allows for improved mechanical rigidity and sound insulating properties. The soundproof material may be applied to various automobile parts such as package trays, luggage coverings, covering shelves, and isolation pads.

Abstract: An apparatus for lining a pipe, comprising a liner having a non-everted portion and an everted portion, and a stretching device. The stretching device includes at least two stretch members secured to the everted portion on substantially opposing sides, and a force mechanism to facilitate movement of the stretch members away from each other in order to stretch the evert portion of the liner. Preferably, the liner comprises an inner layer and an outer layer, and the stretch members are positioned between the inner and outer layers. In another aspect, the present invention provides a method of everting a liner into a pipe. The method includes flipping an open end of the liner inside out to create an everted portion, engaging a sidewall of the liner at two opposing locations on the everted portion, and applying a force at the two locations to stretch the everted portion of the liner.

Abstract: A method for recovering uncured rubber from unused electron beam pre-cured rubber stock used in the manufacture of pneumatic tires. A first layer of the pre-cured rubber stock having cured rubber is skived with a band knife cutter blade from a second layer of the pre-cured rubber stock having uncured rubber. The band knife cutter blade is lubricated so as to avoid adhesion of the uncured rubber to a leading cutting edge of the cutter blade. After the first layer of cured rubber is removed from the pre-cured rubber stock, the uncured rubber in the second layer is reworked into at least one tire component.

Abstract: A pipe lining composition and a method for installing the pipe lining composition into a pipeline requiring repair is provided. The lining composition is a layered lining composite formed of alternating plies of felt and carbon fiber strand reinforcing such that layers of carbon fiber reinforcing strands are trapped between layers of felt. Once the composite is laid up the composite is preferably stitched to provide stability and to maintain the layers relative to one another and then formed into a tube. In accordance with the method, the lining tube is then sequentially filled resins of increasing viscosity as it is drawn through rollers in a manner that fully wets out the carbon fiber before it is placed into the pipe to be lined.

Abstract: A method of restoring a section of a composite includes the steps of removing an undesirable section of a perforated composite and depositing a repair material in the location of the removed, undesirable section. The repair material is then cured. Before completing the curing step, one or more opening are formed through the repair material to produce one or more perforations through the repair material upon completing the curing step.

Abstract: A method of joining a fibre reinforced laminate layer to a surface (3), including applying a layer of melted resin on to the surface (3), the resin displacing air from the surface and solidifying upon cooling on the surface to thereby form a layer of solidifled resin (7) thereon, applying a composite lay-up (13) over the resultant layer of solidified resin, and heating and melting the resin so that the composite lay-up is submerged in the melted resin and the resin is subsequently cured to thereby form the laminate layer (19).

Abstract: A system and method for recycling and repurposing a synthetic turf field cover including a pre-existing mixture of rubber and sand particles embedded in the turf material. The system utilizes an aspirating machine for removing and separating the existing rubber and sand particles. The removed rubber particles are reused, and can be cleaned and sterilized prior to reinstallation. A method of recycling a synthetic turf field cover includes the steps of removing the existing synthetic turf field cover, aspirating pre-existing rubber and sand particles, sterilizing the rubber particles, reapplying the sterilized, reused rubber particles and applying additional rubber particles and sand to a replaced or reinstalled field turf cover.

Abstract: A system for stopping in an opening a flow of a fluid, wherein the system comprises: a kneadable silicon based polymer for fitting in and/or onto the opening so as to block any flow of the fluid through the opening, wherein the silicon based polymer comprises fillers so that the density of the silicon based polymer is higher as compared to the density of the silicon based polymer that does not comprise these fillers, and a silicon based sealant for applying against a dried form of the silicon based polymer, wherein the silicon based sealant is vulcanizable under exposure to humidity.

Abstract: A patch for reworking an inconsistent area in a composite structure includes a composite laminate patch adapted to cover the inconsistent area and bonded to the structure by a layer of adhesive. The patch includes a plurality of composite plies having a tapered cross section, and at least first and second regions respectively having differing fracture toughnesses.

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 UV-IR combination curing system and method for manufacture and repair of composite parts, such as for use in wind blade manufacture and repair. The system and method utilize UV and IR dual radiation sources to cure glass fiber reinforced laminates containing a photo initiator. The UV and IR dual radiation sources can be configured as discrete stand-alone UV and IR lamps used in a side by side configuration, a plurality of UV lamps with thermal IR radiation, a combined UV/IR lamp, or other forms of light sources providing both UV and IR radiation. To achieve high glass transition and complete curing of thick laminates, the IR radiation source is initially turned on to heat the laminate to close to 40° C.-100° C. before the UV radiation source is turned on. The IR radiation source can be turned off after UV radiation source is activated.

Abstract: A composite laminate patch for reworking an inconsistent area in a structure has inner and outer control regions possessing differing interlaminar fracture toughnesses for controlling the advance of a disbond in the patch. One or more separation zones in the patch between the control regions aids in diffusing the fracture energy of the disbond as the disband advances from the inner region to the outer region.