This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.

The invention proposes insulating profiles of a polymer material, and methods for producing the insulating profiles, are disclosed.

The present invention provides a method for post-curing a profile (14) of fibre-reinforced plastic material comprising the steps of: • a supplying the profile, wherein the profile (14) is wound round a winding body (13) and wherein, as a result of the winding in the profile, stresses are present in the profile and said profile comprises a number of fibres extending along one another, which are embedded in a partially cured thermosetting matrix material, • b by means of a heat treatment device, carrying out a heat treatment on the profile (14) while the profile is wound round the winding body (13), and during said heat treatment the matrix material is post-cured, wherein the glass-transition temperature of the matrix material is increased as a result of the heat treatment and wherein the temperature to which the profile is exposed during the heat treatment remains below the glass-transition temperature during the heat treatment, wherein the stresses remain constant and as a result the shape is retained both in cross-section as well as radius of curvature of the profile, at least in the stress-free state, despite the heat treatment and despite winding the profile (14) round the winding body (13) prior to the heat treatment. The present invention also provides a profile manufactured by the method, and use of a profile manufactured by the method.

An electronic display assembly includes a display unit supported by a housing assembly. An upper portion is supported by said housing assembly above, and spaced apart from, the display unit. One or more fans associated with the upper portion move ambient air ingested through one or more intake/exhaust apertures in upper portion housing between an upper cavity and a transition area between the upper portion and the display unit. Ambient air is ingested through one or more intakes at the transition area by one or more fans associated with said display unit and forced though said at least one open loop airflow pathways within said display unit.

Manufacturing structure using a composite material includes: a tapering step for forming a first tapered surface on a first stiffener in an uncured state; a bending step for bending the stiffener such that a second surface is on the inner side; an arranging step for arranging the first stiffener and a skin at prescribed positions; a vacuum suctioning step for vacuum suctioning the first stiffener and the skin; and a bonding step for curing the first stiffener to bond the first stiffener and the skin. In the tapering step, the angle formed between the first tapered surface and the second surface is an acute angle. In the vacuum suctioning step, the first tapered surface is brought into contact with the skin while maintaining contact between the first surface and the skin, and the first stiffener is deformed so that a second tapered surface is formed on the second surface.

Disclosed is a composite beam structure having: an end piece, an end piece outer periphery surface, and an end piece mating end defining an end piece axial boundary, the end piece includes wedge-shaped inner locking features that are formed to project outwardly from the end piece outer periphery surface at the end piece mating end and are spaced apart from one another in the hoop direction; and a composite tube configured to surround at least a portion of the end piece mating end to form a beam joint, wedge-shaped imprints are formed through the composite tube, corresponding to the wedge-shaped inner locking features, the wedge-shaped imprints define respective composite tube wedge-shaped depression surfaces about a composite tube inner periphery and composite tube wedge-shaped boss surfaces about a composite tube outer periphery, and the wedge-shaped inner locking features of the end piece are covered by the composite tube wedge-shaped depression surfaces.

Various embodiments relate to a device for the production of preforms for aircraft structural components, having a supply unit for the continuous supply of a layer structure with at least one fiber layer, having a heating unit with at least one infrared heater which has an infrared radiation source, wherein the supplied layer structure is passed through the heating unit in a conveying direction and can be heated there over at least part of its width in cross section by the at least one infrared heater, a disk which is permeable to infrared radiation being arranged between the layer structure and the infrared heater.

A transfer system which can be used in a flexible manner for transporting or processing, respectively, profiles, in which the injection device comprises a mold for receiving the profile during the injection, wherein the mold has at least two contour parts and the injection device has a closing unit for opening/closing the contour parts, wherein the closing unit is configured for keeping the contour parts open until the profile is enclosed by the contour parts, and wherein the transportation device is configured for moving, preferably not rotating, the profile exclusively parallel to the transportation path, wherein the closing unit and the injection device are assembled so as to be displaceable conjointly with the first feed table, and the first feed table in the direction of the transportation path is displaceable so far until the contour parts enclose the profile.

A universal transition molding for bridging two floor surfaces can include: a substantially symmetrical extruded profile of unitary construction having: (i) a substantially planar central portion, (ii) a pair of downwardly depending substantially planar wings, (iii) a pair of hinge sections joining the wings to opposing edges of the central portion, and (iv) a pair of vertical legs depending from a bottom surface of the central portion. Methods of manufacturing and installing the universal transition molding are described.

The present invention relates to an edge profile for a sheet-like material including a layered structure with a main body made of plastic which has a first base colour tone, with a decorative base material which has a second base colour tone, and with a decorative print. A final decoration which has a third base colour tone is formed at least from decorative base material and decorative print together. The decorative base material is a layer arranged between main body and decorative print. For easier production, the invention proposes that the decorative base layer is a layer of plastic co-extruded with the main body. The invention also relates to a sheet-like material with a corresponding edge profile.