B32B38/0012

High Opacity Laminate Surface
20230143935 · 2023-05-11 ·

A decorative and/or functional laminate using a nonwoven glass fibre material impregnated and or coated with a novel mixture of at least styrene maleic anhydride copolymer amic acid and cyanuric acid and melamine to provide opacity and a laminate surface suitable for printing or painting and/or sealing.

Method and apparatus for assembling absorbent articles

The present disclosure relates to methods for assembling elastic laminates that may be used to make absorbent article components. Particular aspects of the present disclosure involve providing a first substrate and a second substrate, the first substrate and the second substrate, each having a width in a cross direction; providing an activated elastic material; elongating the activated elastic material; and ultrasonically bonding the first substrate together with the second substrate with the elongated activated elastic material positioned between the first substrate and the second substrate.

NON-STRETCH BONDED STRAND AND FILM ELASTICS
20230147078 · 2023-05-11 ·

A laminate includes a core structure having a first surface and a second surface, the core structure including an elastic core layer and a plastic core layer, wherein the elastic core layer is one of a film, a plurality of strands, and a plurality of strips, and wherein the plastic core layer is one of a film layer, a plurality of strands, and a plurality of strips, the plastic core structure reinforcing the core layer in the machine direction, and a nonwoven first facing layer affixed to the first surface.

COMPOSITE PANEL AND METHOD FOR MAKING COMPOSITE PANEL
20170368789 · 2017-12-28 · ·

A composite panel includes a core having at least one core element. The core element includes a shell defining a cavity. A pair of skins sandwich the core. Each skin has a first face facing away from the core and an opposed second face facing the core. The second face has a plurality of barbs extending therefrom. The barbs penetrate the shell to secure the core element between the skins. A method for making a composite panel includes positioning a core element against a barbed face of a first skin, where the core element includes a shell defining a cavity, and pressing the core element and first skin together to force barbs of the barbed face to penetrate the shell.

Method of Making an ARTICLE OF FOOTWEAR
20230200493 · 2023-06-29 ·

A method of manufacturing a panel for an article of apparel includes stretching a base layer from a resting configuration to a stretched configuration. The method further includes coupling a reinforcement layer to the base layer when the base layer is in the stretched configuration. The method also includes applying an auxetic structure to the reinforcement layer when the base layer is in the stretched configuration. The auxetic structure includes a plurality of interconnected members defining a repeating pattern of voids, and each void has a reentrant shape. The method further includes releasing the base layer to allow the base layer to return to the resting configuration.

COMPOSITE MATERIAL STRUCTURE AND PROCESSING METHOD THEREOF
20230202140 · 2023-06-29 ·

A composite material structure includes a first metal member and a second metal member bonding to the first metal member. A bonding surface is formed therebetween. A first hole is through the first metal member. A circular bonding line is formed at a junction of a wall of the first hole and the bonding surface. A sleeve protrudes from the second metal member into the first hole, and covers the bonding line. A groove indents from the first metal member. The groove has a bottom surface located in the same plane with a top surface of the sleeve. A processing method of the composite material structure is also provided. The sleeve covers the bonding line between the first metal member and the second metal member, which allows the composite material structure to provide an improved sealing performance.

Process for the production of a structured film

The present invention relates to a process for the formation of a structured film, a structured film as such, an article comprising the structured film, a device for the continuous formation of such a structured film and a composite comprising the structured film.

LIGHTNING STRIKE DISPERSION FOR COMPOSITE AIRCRAFT STRUCTURES
20170361944 · 2017-12-21 · ·

A lightning strike dispersion structure may include a composite component having an outboard surface, wherein the composite component is electrically nonconductive. The lightning strike dispersion structure may include a metal sheet coupled to and extending across a minority portion of the outboard surface of the composite component, wherein the metal sheet is electrically conductive. The lightning strike dispersion structure may also include a metal stud coupled to and in electrical contact with the metal sheet, the metal stud extending completely through the composite component, wherein the metal stud is electrically conductive.

ADHESIVE STRIP FOR APPLICATION TO AN OBJECT, METHOD OF MANUFACTURING SUCH AN ADHESIVE STRIP AND METHOD OF APPLYING SUCH AN ADHESIVE STRIP TO AN OBJECT

An adhesive strip for application to an object, more particularly for application to an object with a strongly curved and/or angled surface or an object with a large surface area is disclosed. Methods of manufacturing and applying such an adhesive strip are disclosed as well. The adhesive strip includes a carrier structure with two opposite main expansion surfaces. At least one main expansion surface has an adhesive. Formed in the carrier structure are several weakened points penetrating the carrier structure from one main expansion surface in the direction of the other main expansion surface. The carrier structure is expandable in one tangential plane of one of the main expansion surfaces.

METHOD OF FORMING A GLASS ARTICLE AND THE GLASS ARTICLE FORMED THEREBY

A method of forming a glass article includes providing a first glass sheet. The first glass sheet is heated to a temperature suitable for shaping. The first glass sheet is deposited on a first bending tool. An edge portion of the first glass sheet is disposed over a shaping surface of the first bending tool. The shaping surface of the first bending tool is configured to provide in the first glass sheet a compression area and a tension area. The first glass sheet is shaped on the first bending tool and the compression area is formed in the edge portion of the first glass sheet. The compression area includes a first portion and a second portion. The first portion has a width which is greater than a width of a second portion.