The invention relates to a method of manufacturing high durability timber product, the method comprising: a) selecting a durable substrate timber; b) selecting a veneer of high-performance timber; and c) gluing the veneer of high-performance timber to the face of the durable substrate 5 timber, wherein the resulting manufactured high durability timber product is suitable for long-term use in exterior applications at a lower cost than that of the same thickness timber product if made of high-performance timber alone.

A wood or engineered wood structural panel, such as, but not limited to, OSB (“oriented strand board”) or plywood, that is both fire-resistant and water resistant. The panel is factory-coated with a product that provides fire resistance. The treatment gives it a Fire-Resistant (FR) performance (for use in a one- or two-hour rated assembly). The panel also is overlaid or coated in a factory setting with a weather/water resistive barrier (WRB). The structural panel thus combines a fire-resistant structural sheathing and WRB product in one integrated panel produced at a factory prior for installation at a job site.

Provided in the embodiments of the present disclosure are a support sheet for supporting a flexible display screen, a flexible display screen and an electronic device. The flexible display screen support sheet includes a carbon fiber substrate and an epoxy resin adhesive. The carbon fiber substrate includes first carbon fibers in a first direction and a second carbon fibers in a second direction, and the first direction being different from and angled with the second direction.

A multilayer film comprising, in this order: (a) a biaxially oriented polyethylene terephthalate layer, (b) a pressure sensitive adhesive layer, (c) an elastic polyurethane dispersion, and (d) a biaxially oriented polyethylene terephthalate layer.

Layer (d) preferably has the structure A:B:A:C; where A and B preferably comprise crystalline PET and antiblocking particles and C is preferably an amorphous, heat-sealable copolyester.

A multilayer film comprising, in this order: (a) a biaxially oriented polyethylene terephthalate layer, (b) a pressure sensitive adhesive layer, (c) an elastic polyurethane dispersion, and (d) a biaxially oriented polyethylene terephthalate layer.

Layer (d) preferably has the structure A:B:A:C; where A and B preferably comprise crystalline PET and antiblocking particles and C is preferably an amorphous, heat-sealable copolyester.

At least one braided composite layer configured to form a first ply may be provided. A plurality of slit tapes may be arranged and aligned such that each slit tape is adjacent to one another and non-overlapping, to form a second ply. A hybrid composite laminate may be formed by stacking a plurality of plies that includes at least one first ply and at least one second ply. Each slit tape may be a steered unidirectional composite slit tape that is aligned along an axis, contour line, or curve of the hybrid composite laminate, a mold/tooling used to shape the laminate, or the resulting composite part. Hybrid composite laminates may be formed by stacking at least one first ply formed of a braided composite layer and at least one second ply formed from a plurality of slit tapes. Composite parts may be formed by consolidating such hybrid composite laminates.

At least one braided composite layer configured to form a first ply may be provided. A plurality of slit tapes may be arranged and aligned such that each slit tape is adjacent to one another and non-overlapping, to form a second ply. A hybrid composite laminate may be formed by stacking a plurality of plies that includes at least one first ply and at least one second ply. Each slit tape may be a steered unidirectional composite slit tape that is aligned along an axis, contour line, or curve of the hybrid composite laminate, a mold/tooling used to shape the laminate, or the resulting composite part. Hybrid composite laminates may be formed by stacking at least one first ply formed of a braided composite layer and at least one second ply formed from a plurality of slit tapes. Composite parts may be formed by consolidating such hybrid composite laminates.

Various embodiments for configuring LC cells, LC panels, and methods of manufacturing LC panels are provided, comprising: providing a first glass layer and a second glass layer; wherein the first glass layer has first and second surfaces and the second glass layer has first and second surfaces; and at least one of: surface polishing a surface of the first glass layer and second glass layer; and selectively positioning the first glass layer and second glass layer such that, after lamination, based on the positioning or polishing of the glass layers, the resulting LC panel is configured with uniform transmission.

Various embodiments for configuring LC cells, LC panels, and methods of manufacturing LC panels are provided, comprising: providing a first glass layer and a second glass layer; wherein the first glass layer has first and second surfaces and the second glass layer has first and second surfaces; and at least one of: surface polishing a surface of the first glass layer and second glass layer; and selectively positioning the first glass layer and second glass layer such that, after lamination, based on the positioning or polishing of the glass layers, the resulting LC panel is configured with uniform transmission.

A grid and skin assembly for use in a composite laminate structure is described. The assembly includes a metallic grid having a plurality of intersecting ribs oriented in at least two distinct rib directions offset at a grid angle relative to one another and defining respective intersection points; and a composite laminate skin having a plurality of ply layers comprising a plurality of tapes oriented in at least two distinct tape directions offset at a ply angle relative to one another. The grid angle is at least 25 degrees, the intersection points define glueless joints of the metallic grid, and the grid is a non-aluminum-based material. A grid and method of manufacturing the grid and skin assembly is also described. The method includes a water jet cutting procedure and glueless joint formation due to differing thermal expansion characteristics of the grid and skin.