An aircraft flap is constructed of nested layers of composite material in the aircraft flap that include an inner layer, a middle layer and an outer layer. The aircraft flap is constructed with the inner layer laid up around a central mandrel, the middle layer laid up around the middle layer and the outer layer laid up around the middle layer. The inner layer, the middle layer and the outer layer are co-cured on the mandrel, removed from the mandrel and then assembled together with the inner layer formed in a folded over configuration around a hollow interior volume of the aircraft flap, the middle layer formed in a folded over configuration over the inner layer, and the outer layer formed in a folded over configuration around the middle layer.

An OLED display panel and manufacturing method are provided. Through disposing a light-shielding film on the packaging cover plate to prevent the laser from illuminating on the electrodes of the MED substrate during the laser scanning of the sealant to effectively protect the electrode. A portion of the light shielding film that overlaps with the thin layer region of the sealant has gradually decreasing light transmittance, which can prevent the problem that the thin layer region of the sealant is scorched by excessive laser energy, sufficiently ensures that the packaging effect, and reduces the generation of particles. In addition, the surface of the light-shielding film irradiated with laser light is a frosted surface, which can cause diffused reflection of the laser light irradiated on the light-shielding film to prevent the laser from directly reflecting on the laser head and protect the laser head from being burned and damaged.

Unidirectional transparent projectile penetration resistant panel assemblies and bidirectional opaque projectile penetration resistant assemblies and systems and methods of forming and mounting the same relative to underlying support structures.

A method for attaching an underlay element to a weight-reduced board element. The method includes providing a board element and an underlay element, wherein a rear side of the board element includes a groove portion and a remaining portion. The groove portion includes at least one groove. An adhesive is applied on at least a portion of the remaining portion and/or on at least a portion of a corresponding residual portion of the underlay element, and the underlay element is arranged on the rear side of the board element, such that the adhesive contacts the underlay element and the rear side.

A paint roller manufacturing system and method are described. In an embodiment, an inner strip of material and an outer strip of material are wound about a mandrel in offset relation. The inner strip of material and the outer strip of material each comprise material that results in a final paint roller which shrinks by less than 2.5 percent of the final paint roller axial length, or which has shrinkage that varies by less +/−0.1%, upon hardening and setting. An adhesive is applied to at least a portion of the outer strip as it is wound about the mandrel. A length of fabric is wound about at least the outer strip to form a paint roller tube, and compression is applied to the paint roller tube while advancing the paint roller tube in a direction parallel to the mandrel. A precision measuring or sensing device is used to control a cutting device causing the cutting device to cut the advancing paint roller tube into pre-selected lengths prior to the paint roller tube hardening and setting.

Embodiments include methods of making a fabric laminates including depositing a first and a second columns of discrete adhesive masses on a first layer of fabric, wherein the first and second columns of discrete adhesive masses are separated by a first gap area, and placing a second layer of fabric on the first layer of fabric sandwiching the first and second columns of discrete adhesive masses, and applying pressure to all layers to form a fabric laminate structure while maintaining the first gap area unobstructed and forming a tunnel area between the first gap area and the first and second fabric layers. In some embodiments, ribbons may be pulled through the tunnels. In some embodiments, the tunnels include batting material. In some embodiments, films are placed on the first or second fabric layer and they imprint their surface finish onto the discrete adhesive masses wetting the surface of the fabric layers.

The present disclosure relates to methods and apparatuses for stretching, transferring, and bonding elastic parts under tension to an advancing carrier substrate during the assembly of absorbent articles. A continuous carrier substrate may be advanced in a machine direction at a first speed, and a discrete elastic part may be cut from a continuous elastic substrate having a direction of stretch in a cross direction. The speed of the discrete elastic part is changed from a second speed to the first speed, and the central region of the discrete elastic part is stretched in the cross direction. The discrete elastic part is bonded with the continuous carrier substrate such that the stretched central region extends in the cross direction between the first and second longitudinal edges of the continuous carrier substrate. The discrete elastic part may also be bonded with the carrier substrate with adhesive and/or mechanical bonds.

The present disclosure relates to absorbent articles having a waist gasketing element, with the gasketing element having an adhesive zone and one or more adhesive-free zones. At least a portion of the waist gasketing element is adhesively attached to a chassis of the absorbent article. Additionally, a portion of the waist gasketing element is mechanically attached to a portion of the absorbent article.

A method of forming a laminate countertop includes a step of providing a laminate countertop with at least one substantially square corner having a curved edge profile extending around the at least one square corner. The method further includes steps of: cutting a first angled slot through a portion of a longitudinal side of the countertop; cutting a second angled slot through a portion of a preformed straight edge member connected to a base support along a latitudinal side of the countertop; and cutting a connecting cut between the slots to form a cutout section of the countertop. The method also includes a step of adhering at least one preformed angled edge member including the curved edge profile into the cutout section of the countertop to form at least one angled corner, thereby forming a laminate countertop having an edge profile extending around the at least one angled corner.

A manufacturing system includes a plurality of lamination heads statically positioned in end-to-end relation to each other and defining a lamination station, and configured to dispense a layup material along a dispensing direction. The manufacturing system also includes a lamination surface movable underneath the lamination station. The lamination heads are configured to sequentially apply the layup material onto the lamination surface and onto previously applied layup material as the lamination surface passes through the lamination station to thereby form a composite laminate having a stack of composite plies arranged in a desired ply stacking sequence defined by positions of the lamination heads relative to each other within the lamination station.