An apparatus is provided for forming a composite laminate. The apparatus comprises a mandrel having a surface on which the composite laminate can be formed. The apparatus further comprises an application surface and a conveyor configured to move a composite material piece that has been cut to a desired shape to the application surface. The apparatus also comprises an actuating mechanism for, when actuated, lifting the application surface upward towards the mandrel to apply the composite material piece to the surface of the mandrel to form at least a portion of the composite laminate on the surface of the mandrel.

A process unit and methods are disclosed. One process unit including a pultrusion unit having a pultrusion channel, with the pultrusion channel being limited by at least one shaping wall. The process unit further includes an extrusion unit having an extrusion channel and an opening for removing the extrudate out of the extrusion channel, a cutting unit having a moving cutting element for cutting off the extrudate with the moving cutting element, and a conveying device for conveying a raw extrudate from the pultrusion unit into the extrusion unit. The cutting unit comprises a component that can be caused to move in a rotational manner and the component is mechanically coupled to the cutting element by a mechanical coupling device, such that the rotational movement of the component determines the movement of the cutting element.

A method for producing a functional element of an automobile that can be folded and/or wound up, having the steps of providing a fabric that can be folded and/or wound up, arranging the fabric on an application table or in a casting tool in a level arrangement and molding at least one edge strip made of a polyurethane material to the fabric under atmospheric pressure. Furthermore, a wind deflector element of an automobile is provided to a roller blind panel of an automobile, each comprising a fabric that can be folded and/or wound up and that is provided with an edge strip made of a polyurethane material and forming an edge reinforcement.

A composite member is provided with a bonding member made of a fiber-reinforced resin and a bracket in which the bracket is bonded to the bonding member via a resin. The bracket has a through-hole. The bonding member has a front surface side fiber-reinforced resin sheet and a rear-surface-side fiber-reinforced resin sheet. The front surface side fiber-reinforced resin sheet, the rear surface side fiber-reinforced resin sheet and the bracket are integrally bonded to each other by the resin in a state in which the front surface side fiber-reinforced resin sheet is inserted into the through-hole of the bracket to thereby enhance the bonding strength between the bonding member to the bracket.

A preformed foundation support for a vessel gyro-stabilization system, comprises at least three of a first side support, a second side support, a third side support, and a fourth side support. The side supports define an opening for accommodating at least a portion of a vessel gyro-stabilization system, and the side supports comprise a cuttable portion for custom fitting the preformed foundation support in a vessel. The preformed foundation support structure is installed in the vessel by cutting the cuttable portion of the preformed foundation support for custom fitting the preformed foundation support to the structure support of the vessel. The preformed foundation support structure can be manufactured as a molded fiberglass structure.

Method for manufacturing a wind turbine blade comprising an aerodynamic shell forming an outer surface of the blade and at least one main laminate, the method comprising; providing a mould 13, forming a main laminate 18 in the mould by providing a fibre lay-up comprising a plurality of fibre plies placed on top of each other in the mould 13, dividing the fibre lay-up into at least two segments as seen in the longitudinal direction of the mould by at least one transverse flow barrier 54,55 in the lay-up preventing longitudinal resin flow through the fibre lay-up past the flow barrier 54,55.

A cover for a cushion includes a first panel, a second panel, and a primary receptacle defined between the first panel and the second panel. The primary receptacle may receive a primary cushioning element, such as a pillow, a pillow insert, or a fill material. At least one of the first panel and the second panel includes a secondary cushioning element. The secondary cushioning element may be defined from a compressible, resilient elastomeric material that defines a plurality of thin interconnected walls that in turn define an array of open cells or columns. Each cell or column may have a hexagonal shape, imparting the array of open cells or columns with a honeycomb appearance. Methods for assembling a primary cushioning element with such a cover are also disclosed.

A weight and noise reducing glovebox assembly made of an inner glovebox bin composed of a pair of thermopolymer fiber layers that work in concert to absorb noise and isolate noise and vibration providing a glovebox with improved NVH characteristics. The glovebox bin is formed of a three dimensionally chill formed structural layer composed of PET fiber to which is mated, preferably by needle tacking, an inner carpet layer also composed of PET fiber providing two stage noise, sound and vibration reduction. In a preferred embodiment, the inner PET fiber carpet layer is mated, preferably by needle tacking, to an outer structural moldable PET fiber substrate layer forming a two-stage sound, noise and vibration absorbing and isolating thermoformable blank that is chilled formed into a sound absorbing glovebox bin of one piece flip open construction that is lighter in weight and which has reduced sound and noise generation and transmission compared to conventional hard plastic gloveboxes.

A hybrid material mat for use in the manufacture of fibre-composite articles, in particular parts for wind turbine blades, is described. The mat comprises a plurality of glass fibre rovings provided on top of a relatively thin planar substrate of carbon fibres. Such a hybrid mat construction provides for an improvement in the structural properties of a component manufactured using the mat, as well as allowing for ease of handling and manufacturing of both the mat itself and the component.

Process for producing a fibre-reinforced polymer composition comprising the following steps: a) providing a polymer composition, b) melting the polymer composition in a compounding device, c) feeding a non-woven fabric into the compounding device in the presence of the molten polymer composition, and d) withdrawing the fibre-reinforced polymer composition from the compounding device. Furthermore, the product obtained by the process and the use of a non-woven fabric in an extruder to reinforce a polymer with fibres are disclosed.