Provided is a laser marking multilayer film that includes: a layer (X) at least as an outermost layer, the layer (X) being made from a resin composition (x) containing a bisphenol-based polycarbonate (A) and a polyester (B), the polyester (B) containing a predetermined compound as a diol component, the resin composition (x) containing the predetermined compound in an amount of 0.1 to 20 mass %; and at least one layer (Y) made from a resin composition (y) containing the bisphenol-based polycarbonate (A) and a laser beam energy absorber (C). The multilayer film does not contaminate equipment such as a T-die and rolls in melt extrusion molding, brings about good laser marking performance. On the multilayer film, laser-marked information does not fade even in long-term use. In the multilayer film, the base material does not deteriorate.

A method for reducing the resistivity of a carbon nanotube nonwoven sheet includes providing a carbon nanotube nonwoven sheet comprising a plurality of carbon nanotubes and applying pressure to the carbon nanotube nonwoven sheet to reduce air voids between carbon nanotubes within the carbon nanotube nonwoven sheet.

A non-fibrous film has at least one film body that is non-fibrous, and at least one film element that is non-fibrous. The film element is coupled to the film body at an interface that is non-continuous across a film width of the non-fibrous film. The non-fibrous film has at least one of the following characteristics: the interface has at least one mechanical property having a value that is different than the value of the mechanical property of at least one of the film element and the film body, and/or the film element has at least one mechanical property having a value that is different than the value of the mechanical property of the film body.

A method of manufacturing an activated composite web includes laminating a film layer to a nonwoven web to form a composite web, forming a plurality of apertured protuberances in the film layer, and passing the composite web through intermeshing elements to form an activated composite web. The intermeshing elements form a plurality of first lanes, with first widths, substantially unaffected by activation, and a plurality of second lanes, with second widths. The second widths are less than the first widths. Portions of the plurality of apertured protuberances define first apertures in the first lanes and second apertures in the second lanes. The cross-sections of the second apertures are larger than the first apertures. The first apertures have their major axes substantially aligned in the first direction while the second apertures have their major axis substantially aligned in the second direction. An activated composite web also is provided.

A method produces a high-pressure gas storage container that includes a liner and a reinforcing layer. The liner houses a high-pressure gas. The reinforcing layer is formed by winding a plurality of strip-shaped reinforcing members around an outer perimeter surface of the liner. The method includes irradiating plasma on at least a portion of the reinforcing fibers, and adjusting an irradiation intensity of the plasma such that an irradiation amount of the plasma with respect to the reinforcing fibers becomes constant in accordance with changes in a transport speed of the reinforcing fibers.

The present invention relates to a multilayer construction containing a support or frame composed of a nontransparent polymer as layer c) and a transparent layer b) based on a thermoplastic polymer having a solar transmittance TDS of more than 20%, determined in accordance with ISO 13837:2008 at a layer thickness of 4 mm, and a siloxane-based protective layer a) which is applied to layer c) and layer b), wherein the siloxane layer a) is selectively postcured in selected regions by means of ultrashort-wave UV radiation, and to a method for selective surface treatment.

A high-pressure gas storage container includes a liner and a reinforcing layer. The liner houses a high-pressure gas. The reinforcing layer is formed by winding a plurality of strip-shaped reinforcing members around an outer perimeter surface of the liner. The reinforcing members are made of a plurality of reinforcing fibers that are impregnated with a resin. At least a portion of the reinforcing fibers is irradiated with plasma.

A method of making a composite elastic laminate is provided where an elastic layer is stretched in the machine-direction and while in a stretched state is fed into a grooved-roll assembly, together with outer facing layers, for imparting simultaneous cross-direction stretching forces to the superposed layers. The bi-directional stretching forces causes the elastic layer to tear and/or rupture allowing the laminate to be bonded in areas where the elastic layer has been displaced. Upon relaxation, a composite elastic laminate is provided having excellent breathability and elastic properties.

An elastic laminate is provided including outer facing layers of a fabric and, located between the outer facing layers, a series of individual, spaced apart strips of elastic film extending continuously along the direction of elasticity. The film strips are formed by a controlled tearing of a continuous film while the film is biaxially stretched and bonded to the fabric facings. The fabric facings have gathers formed therein that allow the elastic laminate to stretch at least to the extent that the gathers can be pulled flat.

Unit dose packs and methods of producing and using the same are provided. In accordance with one embodiment, a unit dose pack includes a cover that is non-water soluble, and a wash composition encapsulated within the cover to form the unit dose pack. The wash composition is a solid. The cover is stitched together with a thread to form a pouch around the wash composition, and the thread is water soluble.