Abstract: The invention relates to a method for applying a label to an article travelling along an article path, said label being received on a movable surface at an input location to be retained against said surface whilst being glued and advanced to an output location, at which the label is transferred to the article; the article being rotated with a tangential speed about an axis whilst travelling at a speed along the path including providing at least three portions of surface with independent and controllable vacuum means for retaining the label, including curtailing the application of vacuum means at the first portion of the surface upon the first portion reaching the output location and interrupting the application of vacuum means at the third portion of the surface, with the trailing edge of the label being retained at the second portion of the surface.

Abstract: A composite sandwich structure comprises a core sandwiched between composite laminate facesheets. The core includes a plurality of core sections spliced together at joints that incorporate integral features for arresting the propagation of irregularities in the facesheets.

Abstract: A vehicular decorative member is curved as a forward-bulging shape, and includes a transparent base, a transferred layer, a metallic layer, and a base layer. The transparent base includes a front face, and a rear face. The transparent base's rear face has an ordinary section, and a recessed section. The transferred layer, the metallic layer, and the base layer are disposed on the transparent base's rear-face side in this order. The vehicular decorative member further includes a transfer sheet turning into the transferred layer. The transfer sheet includes a support film, and an adhesive layer, a decorative layer and a release layer that are formed on the support film in this order. The transfer sheet makes the transferred layer when the support film is removed from the release layer after pressing the transfer sheet onto the transparent base's ordinary section while heating the transfer sheet.

Abstract: An air filter cartridge is provided including an air filter media construction having a first, outlet end, flow face and an opposite, second, inlet end, flow face. The filter media construction comprises fluted media secured to a facing media sheet. The filter media is closed to flow of unfiltered air completely therethrough. A centerboard is provided. The centerboard has a media portion embedded within the media construction. The centerboard has first and second opposite sides. The media portion that is embedded within the media defines an aperture arrangement extending completely through the centerboard from the first side to the second side. An adhering sealant secures the centerboard to the media construction. At least some adhering sealant extends through the aperture arrangement.

Abstract: A sheath is placed over a crimped scaffold to reduce recoil of the crimped polymer scaffold and maintain scaffold-balloon engagement relied on to hold the scaffold to the balloon when the scaffold is being delivered to a target in a body. The sheath has an opening spanning the length of the sheath. The opening spans an arc length of about 90 degrees with respect to the circumference of the scaffold or balloon. The sheath may be removed from the scaffold by pinching the sheath between a thumb and forefinger, or bending or peeling back the sheath from the edges of the opening using fingertips.

Abstract: Systems and methods for assembling a skin of a composite structure on an outer surface of an inner mold line layup mandrel. The systems and methods include receiving a plurality of ply kits, assembling the plurality of ply kits to form a skin segment that defines a portion of the skin, and affixing the skin segment to the outer surface of the layup mandrel. The assembling includes transferring a respective ply kit of the plurality of ply kits to a non-planar transfer tool, compacting the respective ply kit on the non-planar transfer tool, and repeating the transferring and the compacting for each ply kit in the plurality of ply kits to form the skin segment.

Abstract: A method for forming a tubular construction element built up of longitudinally extending segments joined together in a side-by-side relationship, wherein the length in the longitudinal direction of the tubular construction element is greater than the diameter thereof.

Abstract: The present invention is method for forming a sandwich structure having a pattern of particulate material enveloped between a carrier material and a cover material. The method allows accurate forming of pre-determined pattern at high production speed. Such a method is particularly useful in the manufacture of disposable absorbent articles, such as baby diapers.

Abstract: The invention relates to a method of manufacturing a composite building element that includes a casing material, a bulk material, and a locking element, the method including the steps of: (a) continuously feeding a first sheet of casing material into a filling station; (b) securing the bulk material to the first sheet of casing material; (c) continuously feeding the bulk material and the first sheet of casing material out of the filling station; the method characterised by the step of: (d) securing the locking element to the first sheet of casing material prior to securing the bulk material to the first sheet of casing material.

Abstract: An object of the present invention is to provide a motor rotor support suitable for an axial gap motor and a method for manufacturing the same. The motor rotor support for supporting a magnetic body disposed on a rotor of the motor is configured by laminating single materials each formed from a hot-worked material or a cold-worked material preferably composed of an 18Mn-18Cr nonmagnetic steel.

Abstract: Two film webs (1), (2) (in each case transfer film or laminating film) with a carrier film (11) and decorative layer (14), in particular metal layer and/or color layer (14), are to be joined to each other. Instead of using a conventional adhesive tape with cold-setting adhesive as hitherto, in the present case a hot-melt adhesive or an adhesive which can be cured using (UV) radiation is used. For example, using hot stamping, a carrier (63) with a PET layer (64) and an adhesive (65) can be applied which joins together two film webs (1, 2) which are in abutment.

Abstract: A method of manufacturing “T” shaped stringers for an aircraft whereby the “T” shaped stringers have a stringer web and a stringer foot, the method comprising: a first step of hot-forming a carbon fiber laminate in order to achieve semi-stringers with an “L” shaped cross-section, a second step of placing together two hot-formed “L” shaped semi-stringers in order to form a “T” shaped stringer, a third step of co-bonding the resulting “T” shaped stringer on a cured skin with an adhesive line between them, and a fourth step of curing the obtained “T” shaped stringer inside a vacuum bag using invar alloy angles as curing tools. The invar alloy angles are cut at a radius area eliminating a part of the invar alloy angles covering the stringer foot in order to define an invar alloy piece having no foot.

Abstract: According to one embodiment, an electrostatic chuck comprises a mount plate, a first layer, and a second layer. The first layer includes a heater. The second layer is provided between the mount plate and the first layer. The second layer transmits heat from the heater to the mount plate. The second layer includes a compressive attachment portion. The compressive attachment portion is formed at the outer edge. The face on the mount plate side of the compressive attachment portion is compressed and attached to the mount plate. The face on the first layer side of the compressive attachment portion is compressed and attached to the first layer.

Abstract: Apparatus for forming composite plies on a contoured tool includes a forming head for forming the composite plies on the tool. The forming head is mounted on a manipulator and includes a compliant nosepiece adapted to conform to the contoured tool.

Abstract: A fiber reinforced resin composite for ballistic protection comprising a plurality of first and second plies wherein the first and second plies further comprise a woven fabric and a polymeric resin. The fabric has a Russell tightness factor of from 0.2 to 0.7 and a cover factor of at least 0.45, The fabric is impregnated with the resin, the resin comprising from 5 to 30 weight percent of the total weight of fabric plus resin. The fabric of each first and second ply comprises regions wherein the fabric is distorted from an orthogonal woven state by a distortion angle of least 30 degrees. The composite may further comprising a third ply having a surface area no greater than 50% of the surface area of a first and second ply. The ratio of the number of first plus second plies to the number of third plies is from 2:1 to 12:1.

Abstract: A method and apparatus for manufacturing a tool for creating composite components. A sheet metal material is secured over a forming tool in an incremental sheet metal forming machine. The sheet metal material is incrementally shaped with a stylus to form a shape for the tool. The tool is removed from the incremental sheet metal forming machine when the shape for the tool is complete. Composite materials on the tool are laid up, wherein the shape of the tool provides a desired shape for a composite component.

Abstract: A seal device or gasket assembly usable with respiration or ventilation mask systems and that is preferably at least one of adhesive or deformable. The gasket is disposed between the mask and the wearer and reduces the escape of respiration gases between the perimeter edge interface of the mask with the anatomy of the wearer and limits exposure of the epidermis located within the perimeter of the mask and between the mask and the wearer to the respiration gas flows. The mask system is particularly useful for improving communication of the respiration gases for those wearers having facial hair, abnormal dontia, and/or other abnormal facial features.

Abstract: A helmet shell is formed having an outer section of fibrous layers, a middle section of fibrous layers and an inner section of fibrous layers. The outer section layers contain high tenacity abrasive fibers in a resin matrix. The middle section layers contain high strength polyolefin fibers and are in the form of woven or knitted fabrics with a resin matrix. The inner section layers contain high strength polyolefin fibers and are in the form of non-woven fabrics with a resin matrix. The helmet is lightweight and resists penetration of rifle bullets.

Abstract: In one embodiment, an implant includes a body member, a first arm member and a second arm member. The body member is formed of a first material and has a first side portion and a second side portion. The body member has a first stiffness and includes multiple apertures through the body member. The first arm member is formed of a second material and is coupled to and extends from the body member. The second arm member is formed of the second material and is coupled to and extends from the body member. The first arm member and the second arm member have a second stiffness, the second stiffness being more than the first stiffness.

Abstract: A composite chassis frame may include a primarily-formed core material having a steel core material and internal composite materials laminated on both surfaces of the steel core material, an internal core material disposed between the primarily-formed core materials, wherein the primarily-formed core materials may be laminated on both surfaces of the internal core material, and a secondarily-formed external composite material covering outer surfaces of the primarily-formed core materials and the internal core material as a skin material.

Abstract: A method of forming a consolidated structure. The method comprises placing a thermoplastic material onto a forming tool to form a structure; positioning the structure within a tool; and consolidating the structure to form the consolidated structure. The tool has a number of die liners configured to generate heat in response to a magnetic field. Consolidating comprises applying a magnetic field to the number of die liners to heat the structure to a consolidation temperature.

Abstract: A sandwich structure based on a composite panel made of a thermoplastic core layer connected to at least one fiber-reinforced thermoplastic layer, in particular in-situ manufactured sandwich panels, comprises a thermoplastic core, which is arranged between two cover layers, in which the core is reinforced with fiber-reinforced thermoplastic reinforcing ribs which extend between the cover layers. Preferred methods for the manufacture are also described.

Abstract: A contoured composite structure is fabricated by laying up a composite charge that includes at least one ply formed by uni-directional fiber pre-preg ply segments having substantially constant widths. The ply segments are placed in side-by-side, overlapping relationship with their longitudinal centerlines aligned in a polar orientation related to the contour of the structure. The charge is formed into the shape of the structure and cured.

Abstract: The invention relates to a method for joining plastic-metal hybrid components, in which a metal component (3) is heated up in a heating stage and a plastic component (9) is brought into contact with the heated metal component (3) in a joining stage and joined to the metal component (3) by means of melting in the contact area, wherein in the heating stage the metal component (3) is heated up to a temperature higher than a defined joining temperature, said metal component is cooled down in a subsequent cooling stage in which the temperature of the metal component (3) is recorded by means of at least one temperature measuring device and the joining stage is performed when the defined joining temperature has been reached.

Abstract: A medical device, such as an introducer, includes a shaft having a lumen therethrough. A distal region of the shaft includes both a fixed curve region and a steerable region. According to certain aspects of the disclosure, the fixed curve region is more proximal than the steerable region. The fixed curvature of the distal region is selected to facilitate positioning of the distal end of the medical device in the general vicinity of a target, such as the left atrial appendage, while the steerable region allows for “fine tuning.” The lumen of the shaft is a large bore, typically on the order of about 12F to about 14F, to facilitate passage of larger medical devices, including left atrial appendage occlusion devices.

Abstract: A modular composite manufacturing method. An illustrative embodiment of the method includes providing a plurality of composite modules; inspecting the composite modules; providing a curing tool; and placing the composite modules on the curing tool.

Abstract: A segment of an abradable ring seal for a turbomachine, includes: a reinforcing support; a composite fabric including fibres impregnated with polymerised resin, and a track of abradable material. The composite fabric is interposed between the reinforcing support 71 and the track of abradable material and is bonded to the reinforcing support, on the one side, and to the track of abradable material, on the other side. The segment of an abradable ring seal has a resistance to tearing in a direction perpendicular to the interface between the track of abradable material and the composite fabric, on the one hand, and between the composite fabric and the reinforcing support, on the other hand, greater than 5.106 newtons per square meter. A process for the manufacture of such a segment is also described.

Abstract: This invention provides a method for producing a structural component, particularly in the aerospace sector. An unhardened prepreg fabric is formed from a composite fiber material, hardenable at a first hardening temperature, into a predetermined shape. The unhardened prepreg fabric is then connected to at least one hardening part of a composite fiber material partially hardened at a second hardening temperature for holding the unhardened prepreg fabric in the predetermined shape, wherein the second hardening temperature is lower than the first hardening temperature. In a further method step the unhardened prepreg fabric connected to the at least one holding part is hardened at the first hardening temperature to form the structural component.

Abstract: A method of finishing a fan blade includes bonding a sheath and a cover to an aluminum fan blade with an airfoil, a root, a leading edge and a tip; imparting residual stresses onto the blade; coating the blade to protect exposed areas of the blade; and curing the blade in low-temperature cure cycles to preserve residual stresses imparted.

Abstract: A hybrid tool for curing composite structures for aircrafts, such as stringers, torsion boxes, skin panels, wing surfaces, horizontal tail or vertical stabilizers, etc. The hybrid tool comprises a metallic portion and an elastic portion arranged on a surface of the metallic portion. The elastic portion and the metallic portion are permanently joined to each other so that the metallic portion and the elastic portion together define a surface having a shape which copies at least part of a surface of a piece of composite material to be cured. The tool is capable of satisfactorily curing pieces of composite material which have a minimum thickness and/or a very aggressive change of thickness.

Abstract: A method of manufacturing a case frame is provided. The method includes forming a mold for forming an ultraviolet molding pattern layer, laminating a hard coating layer on a transfer resin film, laminating an ultraviolet molding pattern layer on the hard coating layer, laminating a deposition layer on the ultraviolet molding pattern layer, laminating a printing layer on the deposition layer, and performing transfer IMD on an injection product using a transfer resin film, on which the printing layer, the deposition layer, the ultraviolet molding pattern layer, and the hard coating layer are successively laminated.

Abstract: The invention relates to a vapour barrier collar (1) comprising a number of sheet elements (2, 3, 4, 5) including side sheet elements (2, 3), which extend substantially along a longitudinal axis (L), and top (4) and bottom (5) sheet elements, respectively, which extend substantially along a lateral axis (A), which is perpendicular to the longitudinal axis (L). Each sheet element (2, 3, 4, 5) has two end edges (6) adjacent to a first edge (7) of the sheet element (2, 3, 4, 5). The sheet elements (2, 3, 4, 5) are mutually joined together in joints (8) extending along the end edges (6), and mounting means (9) are provided along the first edges (7) of the sheet elements (2, 3, 4, 5). The mounting means (9) extend uninterruptedly along the entire length of the first edge (7) of each sheet element (2, 3, 4, 5).

Abstract: A substrate de-bowing mechanism, system and method are described. The mechanism can include a substrate support, one or more stationary contact members, and one or more dynamic or movable contact members that are adapted to contact the substrate and bend the substrate in a desired direction to reduce or eliminate bowing of the substrate. The mechanism is controlled by a CPU or other controller that can adjust the de-bow parameters of the de-bowing mechanism based on input settings that can be dynamic and/or static settings. The mechanism can be used to de-bow a variety of substrates including plastic cards, passports, and passport pages.

Abstract: A method of manufacturing as absorbed article includes a first absorption layer-forming step of forming a first absolution layer configuring the absorber, and a second absorption layer-forming step of forming a second absorption layer configuring the absorber, and laminated on to the first absorption layer. In the first absorption layer-forming step, a first absorption layer is formed while forming the curving unit in symmetry with respect to a virtual central line dividing a width of the absorber in the widthwise direction into two, and extending in the longitudinal direction, and in the second absorption layer-forming step, the second absorption layer is formed without providing the curving unit in a crotch region that is adapted to be in contact with a crotch of the wearer.

Abstract: There is provided a decorative panel comprising: a backing layer having a back face for abutting a panel-receiving surface and a front face opposite to the back face; a relief decorative layer attached to the front face of the backing layer and comprising: a layer of a base polymer attached to the front face of the backing layer and substantially covering the front face of the backing layer; and a relief element made of a layer of an overlay polymer attached to the layer of base polymer and covering a portion thereof.

Abstract: The invention which relates to a wheel rim having a rim base (3) of fiber composite material and a wheel disk (2) connected to the rim base (3) in a radial marginal section is based on the problem of improving the connection between the rim base (3) and the wheel disk (2) and of providing a method for producing a wheel rim having an improved connection between the rim base (3) and the wheel disk (2). The radial marginal section of the wheel disk (2) comprises at least two partial layers (4, 5) on each of which a contoured joining zone (6, 7) which extends substantially axially, is provided, said joining zone being flat connected to the rim base (3).

Abstract: A composite structure is fabricated by staging at least a portion of an uncured, first composite component. The first composite component is assembled with a second composite component, and the staged portion of the first composite component is cocured with the second composite component.

Abstract: The disclosed embodiments provide a battery cell. The battery cell includes a set of layers including a cathode with an active coating, a separator, and an anode with an active coating. The battery cell also includes a pouch enclosing the layers, which contains a first layer of polyether ether ketone (PEEK).

Abstract: The present invention generally pertains to an enclosure constructed from homopolymer and/or copolymer thermal plastic, preferably polypropylene members and a method of construction therefore. Particularly, such enclosures are utilized in the construction of vending machines, product dispensing machines and the like. The polymer members used for the enclosure material are at least partially formed from homopolymer material, or copolymer material, or a combination of homopolymer and copolymer materials.

Abstract: A system comprising: a vacuum roll configured to receive a material, wherein the vacuum roll defines a peripheral surface having a contoured portion; and an element forming a nip with the vacuum roll so that the material can be applied to a substrate advancing through the nip.

Abstract: A curved bullet-proof composite comprising: a glass or glass-ceramic external strike-face layer having been subjected to an ion exchange process and which is mechanically curved; at least one glass or glass-ceramic intermediate layer; an internal plastic layer; and an adhesive material between the strike-face layer, the at least one intermediate layer and the internal plastic layer.

Abstract: A container for food products is defined by a cup-shaped basket, which is made of a first polymeric material, and is provided with a gripping handle connected to the basket in rotary manner by means of two coupling elements, which are made of a second polymeric material, and are welded to the basket itself.

Abstract: The present invention relates to a multi-layered structural component (10), in particular for a motor vehicle, preferably a floor component for a motor vehicle, comprising at least two fibre layers (14) which each include a fibre material and a thermoplastic binder and are arranged one above the other in a stacking direction (S), and at least one metal layer (12) having a thickness (d) of at most 1 mm which is arranged between the two fibre layers (14), wherein the fibre layers (14) each have, at least in certain regions, a porosity of at least 75%, and wherein the structural component (10) comprises at least three metal layers (12) which are arranged one above the other in a stacking direction (S) and each have a thickness (d) of at most 1 mm, with each of the two fibre layers (14) being arranged between two metal layers (12) that are adjacent to one another in the stacking direction (S).

Abstract: A three-sided reflected is formed to include a front and two adjacent sides that are sized to encompass a sign post. This three-sided reflector is then attached to the sign post so that the front faces in the same direction as a front of the sign post. A highly visible material having a bright or fluorescent color and optionally including retro reflectors is disposed on each of the outer surfaces of the front and the two adjacent sides of the reflector so that incident light is reflected back toward a driver of a vehicle that is approaching the front or either side of the sign post. The reflected light greatly increases the visual perception of the sign post by a driver of the vehicle so that it much less likely that the driver will strike the sign post with the vehicle.

Abstract: A hybrid turbine blade and method of fabrication, comprising a shank portion and an airfoil portion. The airfoil portion comprising a composite outer structure having a recess formed therein and an alternating stack of at least one composite section and at least two insert sections disposed in the recess. The outer composite structure and the at least one composite section having a first density. The at least two insert sections having a second mass density, which is less than the first mass density. The composite outer structure and the alternating stack of at least one composite section and at least two insert sections together define an airfoil portion that meets all mechanical load carrying requirements of said hybrid turbine blade such that no load transfer needs to occur through said at least two insert sections.

Abstract: A bicycle wheel includes a hub. The wheel also includes a fully asymmetric carbon fiber rim. The carbon fiber rim includes a curved sidewall and a straight sidewall, the straight sidewall being thicker than the curved sidewall. The wheel also includes a number of symmetric left and right spokes connecting the hub to the rim.

Abstract: A method of fabricating an elastomeric structure, comprising: forming a first elastomeric layer on top of a first micromachined mold, the first micromachined mold having a first raised protrusion which forms a first recess extending along a bottom surface of the first elastomeric layer; forming a second elastomeric layer on top of a second micromachined mold, the second micromachined mold having a second raised protrusion which forms a second recess extending along a bottom surface of the second elastomeric layer; bonding the bottom surface of the second elastomeric layer onto a top surface of the first elastomeric layer such that a control channel forms in the second recess between the first and second elastomeric layers; and positioning the first elastomeric layer on top of a planar substrate such that a flow channel forms in the first recess between the first elastomeric layer and the planar substrate.

Abstract: A method of manufacturing a tampon includes transporting a web of material in a machine direction. The web of material has a base web and an absorbent web. The absorbent web has a free end and a bonded end wherein the bonded end is bonded to the base web. At least the free end of the absorbent web of the web to is controlled to inhibit movement of the absorbent web relative to the base web. The web of material is cut into discrete web segments while controlling at least the free end of the absorbent web. The discrete web segments is bonded to a substrate.

Abstract: Methods of the present disclosure can facilitate creating a piece of furniture entirely made of glass. In some embodiments, the system includes a digital glass printer, a glass tempering machine, and an assembler. The digital glass printer may be configured to print a pattern on a first component of a plurality of components of the piece of furniture. The glass tempering machine may be configured to temper the first component. The assembler may be configured to assemble the components. At least one of the components may serve as a structural element of the piece of furniture.

Abstract: A method and apparatus for producing a radio frequency absorbing (RFA) or perfect microwave absorbing (PMA) printed circuit board (PCB) is described herein. A metamaterial layer may be applied to a low dielectric substrate. Resistive and capacitive components may then be added to the metamaterial layer. The metamaterial layer may then be formed into an RFA or PMA PCB, which may comprise a multi-layered assembly for absorption of electromagnetic radiation in a targeted frequency range such as the microwave frequency range in the PCB.