A flooring arrangement for an aircraft cabin and an aircraft with the flooring arrangement. The flooring arrangement at least one insulating layer for insulating the cabin; a wire mesh disposed above the at least one insulating layer; a carpet layer disposed above the wire mesh, the carpet layer and the wire mesh being in electrically conductive contact; and at least one resistive element connected to the wire mesh, the wire mesh being structured and arranged for being electrically connected to a conductive structure of the aircraft via the at least one resistive element. The resistive element allows transmission, from the wire mesh to the conductive structure, of electrostatic charges developed on the carpet layer, and impedes transmission, from the conductive structure to the wire mesh, of high current events experienced by the aircraft.

A multi-component floor mat has a base or frame layer, intended to be positioned on the floor, that is dimensioned to accommodate a flexible textile mat or rug top layer portion that is releasably held in place on or in the base or frame layer by an attachment coupling feature associated with one or both portions, thereby allowing for the easy removal or replacement of the textile top layer of the mat and its economical laundering.

A flooring product may include an upper flooring material and a glassless wet-laid nonwoven mat. The glassless wet-laid nonwoven mat may include a plurality of polymeric fibers and a binder. The plurality of polymeric fibers have a linear mass density of between about 1.0 denier and 4.0 denier. The plurality of polymeric fibers have lengths of between about 6 mm and 25 mm. The binder has a loss on ignition of at least about 20%. The glassless wet-laid nonwoven mat has a hot-wet % of at least about 20%.

A flooring arrangement for an aircraft cabin and an aircraft with the flooring arrangement. The flooring arrangement at least one insulating layer for insulating the cabin; a wire mesh disposed above the at least one insulating layer; a carpet layer disposed above the wire mesh, the carpet layer and the wire mesh being in electrically conductive contact; and at least one resistive element connected to the wire mesh, the wire mesh being structured and arranged for being electrically connected to a conductive structure of the aircraft via the at least one resistive element. The resistive element allows transmission, from the wire mesh to the conductive structure, of electrostatic charges developed on the carpet layer, and impedes transmission, from the conductive structure to the wire mesh, of high current events experienced by the aircraft.

This disclosure relates to a carpet having fluid barrier properties. The disclosed carpet comprises: (a) a greige good comprising: i) a primary backing material having a face surface and a back surface; ii) a plurality of fibers attached to the primary backing material, wherein a portion of the plurality of fibers extends from the face surface of the primary backing and wherein a second portion of the plurality of fibers are exposed on the back surface of the primary backing in a form of back stitches; b) an adhesive layer comprising a hot melt adhesive composition applied to the back surface of the primary backing material, wherein the adhesive composition is configured to substantially encapsulate at least a portion of the back stitches; and c) a laminated film having fluid barrier properties. Also disclosed are methods for making the carpet described herein.

A multi-component floor mat has a base or frame layer, intended to be positioned on the floor, that is dimensioned to accommodate a flexible textile mat or rug top layer portion that is releasably held in place on or in the base or frame layer by an attachment coupling feature associated with one or both portions, thereby allowing for the easy removal or replacement of the textile top layer of the mat and its economical laundering.

This invention relates to a flooring system comprised of a plurality of washable, multi-component floor mats. The floor mats contain a textile component and a base component. The textile component and the base component are attached to one another by a variety of mechanisms, including magnetic attraction. The magnetic attraction is provided by incorporation of magnetic particles in both the textile and base components. The textile component is designed to be soiled, washed, and re-used, thereby providing ideal end-use applications in areas such as building entryways.

A damping layer comprises a large number of yarns combined to form a textile, wherein at least some of the yarns are foamed synthetic yarns. Such a textile, which consists of a mix of foamed and non-foamed synthetic yarns, is relatively strong and light and can lead to more efficient use of the foamed material. The foamed synthetic yarn may be formed into upstanding loops which provide additional resiliency and damping.

This invention relates to a flooring system comprised of a plurality of washable, multi-component floor mats. The floor mats contain a textile component and a base component. The textile component and the base component are attached to one another by a variety of mechanisms, including magnetic attraction. The magnetic attraction is provided by incorporation of magnetic particles in both the textile and base components. The textile component is designed to be soiled, washed, and re-used, thereby providing ideal end-use applications in areas such as building entryways.

Provided is a method for manufacturing an artificial turf, including: providing a base cloth; providing artificial turf yarns; tufting the artificial turf yarns on the base cloth, and applying an adhesive; and blowing air to the base cloth having the adhesive applied thereto to obtain the artificial turf. According to the manufactured artificial turf, when passing air through the air blowing device, water permeable holes are formed in the bonding layer applied on the base cloth. The water seepage rate of the artificial turf is increased by means of water seepage through the water permeable holes. Moreover, there is no need to pierce the adhesive applied surface of the base cloth during production, thereby avoiding damage to the structure of the artificial turf by piercing. This effectively prevents the artificial turf yarns from loosening and falling off and prolongs the service life of the artificial turf.