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.

Floor element comprising a top layer (102) attached to a substrate layer (104), in which the top layer (102) is itself layered, the top layer (102) comprising: —an optional backing layer (122) made of flexible polymer, —a flexible or semi-rigid polymer layer (124), onto or into which optionally at least one reinforcing layer (126) is attached or embedded, and —a finishing layer comprising a decorative layer (132), a wearing layer (134) thereon and optionally a coating (136) thereon; the substrate layer (104) being a rigid substrate layer.

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 multilayered textile sleeve for routing and protecting elongate members and method of construction thereof are provided. The multilayered textile sleeve includes a plurality of textile layers overlying one another to form a multilayered tubular wall extending lengthwise about a central axis between opposite open ends. The plurality of textile layers include a textile innermost layer and a textile outer layer. At least one silicone layer is sandwiched between the textile innermost layer and the textile outer layer.

A composite material provided in the form of a sheet material includes at least one textile layer as a cover for an airbag. The cover is arranged to form at least one flap with a hinge which includes a hinge region. One side or both sides of the at least one textile layer includes a plastics coating. A melting point of the plastics coating is lower than a melting point of the at least one textile layer. The hinge region is arranged to form at least one single or double fold along the hinge so that the sheet material contacts itself once or twice. In a region of the at least one single or double fold, areas of the plastics coating are arranged to contact each other and, via a prior introduction of heat or a subsequent introduction of heat, are melted onto each other.

A stiffener 100 comprises a first stiffener portion (102), having a first cross-sectional profile (104) that is constant along the first stiffener portion (102). The stiffener 100 also comprises a second stiffener portion (106), having a second cross-sectional profile (108) that is constant along the second stiffener portion (106). The second cross-sectional profile (108) of the second stiffener portion (106) is different from the first cross-sectional profile (104) of the first stiffener portion (102). The stiffener 100 additionally comprises a transition stiffener portion (110) tapering from the second stiffener portion (106) to the first stiffener portion (102).

A seamless tubular liner for repairing an underground or surface pipe is disclosed, including circumferential wefts consisting of slivers comprising a plurality of staple fibers bundled together, the slivers adapted to elongate through disentanglement of the bundled staple fibers when the seamless tubular liner is subjected to an inflation pressure such that the diameter of the tubular liner is able to expand to accommodate variations of diameter of the pipe being repaired.

Curable prepregs possessing enhanced ability for the removal of gases from within prepregs and between prepreg plies in a prepreg layup prior to and/or during consolidation and curing. Each curable prepreg is a resin-impregnated, woven fabric that has been subjected to a treatment to create an array of openings in at least one major surface. Furthermore, the location of the openings is specific to the weave pattern of the fabric.

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.

The present invention provides a sheet-type beauty pack having a convenient use and expected to provide moisture and nutrients to the skin of the face and the like, has a sufficient far infrared ray effect due to a natural material containing minerals, removes impurities, and has a wrinkle alleviation effect due to skin lifting, by applying a beauty pack, which uses a cosmetic material of a natural material containing minerals, in a paste state to a sheet such as nonwoven fabric. The sheet-type beauty pack comprises: a first release paper; a nonwoven fabric of which one surface is laminated with the first release paper and of which the other surface is coated with a cosmetic material in the paste state; and a second release paper laminated on the other surface, coated with the cosmetic material, of the nonwoven fabric.