Described is a composite made from a woven fabric, a non-woven fabric, or a knitted face fabric and a non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric is needle punched such that fibers protrude into the non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric has a first polymer having a first melting point and a second polymer having a second melting point being higher than the first melting point. The nonwoven backing material comprises a third polymer having a third melting point and a fourth polymer having a fourth melting point being higher than the third melting point. The woven fabric, the non-woven fabric, or the knitted face fabric is further bonded to the nonwoven backing material applying heat to at least partially melt or soften the first polymer and the third polymer such that they bond together.

Described herein are methods of preparing continuous polyolefin textiles laminated to a physically crosslinked, closed cell continuous foam sheet. The methods can include extruding a foamable sheet through a nip while simultaneously feeding a polyolefin textile into the nip to laminate the textile to the foamable sheet, irradiating the laminate, and foaming the laminate

A woven EMI sleeve has a wall with opposite edges extending lengthwise between opposite ends. The wall is wrapped about a central longitudinal axis into a tubular configuration bounding an enclosed cavity sized for receipt of an elongate member therein. The wall is woven with warp filaments extending generally parallel to the central longitudinal axis and weft filaments extending generally transversely to the warp filaments. The warp filaments include conductive filaments provided as wire filaments and separate non-conductive warp filaments. The weft filaments include heat-set filaments that are heat-formed to bias the wall into the tubular configuration and to bias opposite edges into overlapping relation with one another. The weft filaments also include conductive filaments.

Provided are a core material (10) formed in a structure in which a fiber glass (10A) and an aramid (10B) are woven and stacked; an outer cover member (20) formed by attaching high-density polyethylene (20A) and impregnated kraft paper (20B) to an outside of the core material (10); and a non-flammable member (30) formed by attaching an acrylic resin (30A) and a ceramic coating material (30B) to at least one surface of the outer cover member (20). Therefore, it is possible to prevent deterioration of bulletproof power due to detachment and breakage caused by bullets in the event of a gun accident, and to enhance non-flammability and eco-friendliness to expand the internal and external fields of a building, thereby enhancing product competitiveness and increasing usability.

A commingled fiber preform is provided. The commingled fiber preform includes at least one first fabric layer and a second fabric layer. The second fabric layer is positioned on top of the at least one first fabric layer. The second fabric layer is joined to the at least one first fabric layer via through thickness reinforcement (TTR) using a commingled thread. A transport depth of the TTR penetrates completely through a thickness of the second fabric layer and an entirety of the at least one first fabric layer. The commingled thread comprises carbon fibers commingled with fugitive fibers. The fugitive fibers are pyrolyzed from the commingled fiber preform to create a path through the thickness for infiltration of fluids.

A composite sheet is provided. The composite sheet includes one or more outer fiber reinforcement layers and one or more intermediate structural support layers. At least one surface of the composite sheet is an outer fiber reinforcement layer of the one or more outer fiber reinforcement layers. The one or more outer fiber reinforcement layers include at least one of an aramid fiber cloth layer, an aramid carbon fiber blend layer, an aramid glass fiber blend layer, and a natural plant fiber layer. The one or more intermediate structural support layers include at least one of a carbon fiber cloth layer and a carbon glass fiber blend layer. The composite sheet may be used to make watch straps.

A commingled fiber preform is provided. The commingled fiber preform includes a plurality of first fabric layers and a second fabric layer. The second fabric layer is positioned on top of the plurality of first fabric layers. The second fabric layer is joined to the plurality of first fabric layers via through thickness reinforcement (TTR) using a commingled thread. A transport depth of the TTR penetrates completely through a thickness of the second fabric layer and partially through a thickness of the plurality of first fabric layers. The commingled thread comprises carbon fibers commingled with fugitive fibers. The fugitive fibers are pyrolyzed from the commingled fiber preform to create a path through the thickness for infiltration of fluids.

Composite materials are described herein. An example composite material may comprise a shell fiber layer. The example composite material may comprise a membrane disposed adjacent the shell fiber layer.

A woven fabric prepreg for constructing a composite laminate comprises two sheets of fabric woven from tows of fibres, impregnated with a polymer matrix and adhered together. Each sheet is woven in a satin weave such that the tows create long floats on at least one side of the sheet. The sheets are positioned face-to-face with the long floats parallel, such that the tows pack together and the space between the sheets is minimised.