An aircraft flooring system is provided, made up of a low-weight carpet tile which functions both as a moisture barrier and as the loop part of a hook-and-loop system, for coupling to a hook part of a hook-and-loop system, which is bound to an aircraft floor. Specifically, a barrier backing within the carpet tile, comprising a nonwoven fabric portion, is able to act as the moisture barrier and the loop part, which allows for coupling of the carpet tile with the floor, without the need to add additional loops to the carpet tile, thereby realizing savings in material cost and weight.

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 real wood sheet includes a wood layer, a mesh layer disposed on a surface of the wood layer, and a flexible layer disposed on a surface of the mesh layer such that the mesh layer is disposed between the wood layer and the flexible layer. The wood layer includes a real wood design portion having a real wood pattern processed thereon and an edge portion formed at an edge of the design portion.

The present invention relates to a molding made of expanded bead foam, wherein at least one fiber (F) is partly within the molding, i.e. is surrounded by the expanded bead foam. The two ends of the respective fibers (F) that are not surrounded by the expanded bead foam thus each project from one side of the corresponding molding. The present invention further provides a panel comprising at least one such molding and at least one further layer (S1). The present invention further provides processes for producing the moldings of the invention from expanded bead foam or the panels of the invention and for the use thereof, for example as rotor blade in wind turbines.

An element including: a first electrode; an intermediate layer made of a silicone rubber composition containing a silicone rubber; and a second electrode, where the first electrode, the intermediate layer, and the second electrode are disposed in this order, wherein a peak intensity ratio (1095±5 cm.sup.−1/1025±5 cm.sup.−1) of an infrared absorption spectrum of the intermediate layer varies along a vertical direction relative to a surface of the first electrode, and to a surface of the second electrode.

Composite panels and methods of preparation are described herein. In some embodiments, the composite panel can include a first fiber reinforcement, a polyurethane composite having a first surface and a second surface opposite the first surface, wherein the first surface is in contact with the first fiber reinforcement; and a cementitious material adjacent the first fiber reinforcement opposite the polyurethane composite. The polyurethane composite can be formed from (i) one or more isocyanates selected from the group consisting of diisocyanates, polyisocyanates, and mixtures thereof, (ii) one or more polyols, and (iii) a particulate filler. The fiber reinforcement can be formed from a woven or non-woven material, such as glass fibers. The composite panel can further include a material, such as a second fiber reinforcement and a cementitious layer, in contact with the second surface of the polyurethane composite. Articles comprising the composite panels are also disclosed.

A process for applying an anti-fragmentation system to manufactured articles made of natural stone or ceramic, and a respective manufactured article equipped with such an anti-fragmentation system, which is provided with at least one retaining member having an adhesive surface, and a manufactured article in the form of a slab and having a first, visible surface with a respective ornamental appearance, and a second, non-visible surface opposite to said first surface; the retaining member is associated with the manufactured article by joining the adhesive surface to said second surface.

One aspect of the disclosure is roofing shingle including a shim layer having a top surface, a first side edge, and a second side edge positioned opposite the first side edge. The roofing shingle also includes a top shingle layer at least partially laminated to the top surface of the shim layer, where the top shingle layer includes a first side edge offset a sidelap distance from the first side edge of the shim layer such that a side portion of the top surface of the shim layer is exposed, and a second side edge extending beyond the second side edge of the shim layer so as to overlap the second side edge of the shim layer by the sidelap distance.

Described herein is a multilayer microporous film or membrane that may exhibit improved properties, including improved dielectric break down and strength, compared to prior monolayer or tri-layer microporous membranes of the same thickness. The preferred multilayer microporous membrane comprises microlayers and one or more lamination barriers. Also disclosed is a battery separator or battery comprising one or more of the multilayer microporous films or membranes. The inventive battery and battery separator is preferably safer and more robust than batteries and battery separators using prior monolayer and tri-layer microporous membranes. Also, described herein is a method for making the multilayer microporous separators, membranes or films described herein.

A vehicle interior part includes a substrate, a first outer layer, a second outer layer, an upper reinforcement layer, a lower reinforcement layer, and a bottom fabric layer, where a first surface and a second surface of the substrate are bonded to a first surface of the upper reinforcement layer and a first surface of the lower reinforcement layer, respectively, a second surface of the upper reinforcement layer is bonded to a first surface of the first outer layer, a second surface of the first outer layer is bonded to the second outer layer, and a second surface of the lower reinforcement layer is bonded to the bottom fabric layer.