A method is provided during which a composite preform is provided that includes an electric heater, fiber-reinforcement and thermoset material. The composite preform is consolidated to provide a composite aircraft component. The consolidating includes heating the thermoset material using the electric heater to cure the thermoset material. The electric heater and the fiber-reinforcement are embedded within the cured thermoset material. The electric heater is configured as a part of a thermal anti-icing system for melting and/or preventing ice accumulation on an exterior surface of the composite aircraft component.

Disclosed is a method of curing a composite article and associated curing apparatus. A heat source is provided for heating the composite article. A temperature related property is detected proximal to the heat source and the heat output is regulated to a predetermined temperature vs. time profile. Heat output vs time data is acquired and functionalised and the curing completion time is determined based on the functionalised heat output vs time data.

The method provides for heating a composite article so as to follow a predetermined temperature vs. time profile (i.e. a cure profile) and avoid excessively high temperatures. The required heat output vs time has also been found to be broadly reproducible, and the curing completion time can be more readily determined from functionalised heat output vs time data, for example by identifying reproducible characteristics of the functionalised data.

The present disclosure is drawn to radiation embossable coated print media. In one example, a radiation embossable coated print medium can include a print substrate, an expanding coating layer on the print substrate, and an ink receiving layer on the expanding coating layer. The expanding coating layer can include a flexible polymer binder and temperature responsive thermoplastic beads in the flexible polymeric binder. The temperature responsive thermoplastic beads can include a propellant encapsulated in a thermoplastic polymer shell.

A thermally expandable sheet includes: a thermally expansive layer formed on a one surface of a base; a first ink receiving layer that is provided on the thermally expansive layer for receiving ink; a film provided on the first ink receiving layer; and a second ink receiving layer that is provided on the film for receiving ink; wherein the first ink receiving layer is formed of a material that provides a texture a different from a texture of the second ink receiving layer.

A composite system for the reinforcement of physical structures includes a plurality of unidirectional fibers arranged with respective longitudinal axes generally parallel to each other over a substantial portion of a length of each unidirectional fiber. The plurality of unidirectional fibers are non-mechanically connected. A resinous material adheres the plurality of unidirectional fibers to each other such that each one of the plurality of unidirectional fiber is adhered to at least one adjacent one of the plurality of unidirectional fibers along a substantial portion of the length of the adjacent one of the plurality unidirectional fibers.

A structure forming method of present invention includes a first step including forming a first pattern serving as a fine pattern using an electromagnetic wave thermal conversion material on a first surface, on the side on which an expansion layer which expands by heating is provided, of a medium including the expansion layer and then irradiating an electromagnetic wave toward the electromagnetic wave thermal conversion material to expand a portion, corresponding to the first pattern, of the expansion layer, and a second step including forming a second pattern including a coarser pattern than the first pattern using an electromagnetic wave thermal conversion material on a second surface, on the opposite side to the side on which the expansion layer is provided, of the medium and then irradiating an electromagnetic wave toward the electromagnetic wave thermal conversion material to expand a portion, corresponding to the second pattern, of the expansion layer.

A method for molding a composite material includes a conductive wire-shaped material arrangement step and a magnetic field application step. The conductive wire-shaped material arrangement step is a step for arranging, in a pre-reaction composite material including reinforcing fibers, a plurality of conductive wire-shaped materials along a direction intersecting the reinforcing fibers with intervals wider than intervals of the reinforcing fibers in a plane on which the reinforcing fibers are arranged. The magnetic field application step is a step for applying a magnetic field in a direction intersecting the plane on which the reinforcing fibers are arranged.

The present disclosure is drawn to methods of embossing print media, printing systems, and printers. In one example, a method of embossing a print medium can include printing a radiation absorbing ink on a coated print medium to form a printed area. The coated print medium can include a print substrate and an expanding coating layer on the print substrate. The expanding coating layer can include a thermal expansion agent having a minimum expansion temperature. The method can further include heating the coated print medium using a heater such that the printed area and unprinted area reach a first temperature from 5 C to 90 C below the minimum expansion temperature. The coated print medium can be irradiated with radiation having a wavelength from 200 nm to 400 nm to selectively heat the print area and expand the thermal expansion agent in the printed area.

The invention relates to a method for creating a surface structure on a mold, wherein first structural elements are created using a laser structuring process in a first step, and second structural elements, which are smaller than the first structural elements, are created using an anodic oxidation process in another step following the laser structuring process. The invention further relates to a mold of said type and finally to a plastic film or a plastic component having a surface structure as well as to a method for the production thereof.

The invention relates to a shaping device (10), which comprises an inductor (14) and one or more shaping half-shells (12, 34), wherein at least one shaping half-shell (12, 34) comprises a bottom shaping element (16) produced from mineral material, and a top shaping element (17), wherein the top shaping element (17) is releasably connected to the bottom shaping element (16) or is formed integrally with it, covers at least parts of an inner surface (16a) of the bottom shaping element (16) and comprises an electrically conductive layer (18), and the inductor (14) is designed to induce eddy currents in the electrically conductive layer (18). The invention further relates to a shaping mould (40) with a part to be formed (38), as well as to a method for heating a shaping surface (17a) of a top shaping element (17) of a shaping half-shell (12, 34) or a shaping surface (38a) of a part to be formed (38).