A pulforming system for forming a three-dimensional article includes a plurality of fibers, a resin injection system, resin, a preform die, a movable first pulling sled, a movable second pulling sled and a cutting station. The first and second pulling sleds form the fibers and resin into an article using a sequential, continual movement process of back-and-forth translational motion in unison to form an article that is three-dimensional in one or more of a longitudinal or transverse direction.

A method of manufacturing a product including at least two carbon parts including the step of: manufacturing a first carbon part, manufacturing at least a second carbon part, providing on a surface of one of the first carbon part or second carbon part a plurality of protrusions including a carbon resin, joining together the first carbon part and the second carbon part in such a way that the plurality of protrusions is interposed between the first carbon part and second carbon part for providing physical and electrical connection is provided.

A 3D thermoplastic pultrusion system and method based upon a 3D variable die system and including one or more sets of 3D thermoplastic forming machines to continuously produce thermoplastic composite pultrusions with at least one of varying cross-section geometry and constant surface contours, varying cross-section geometry and varying surface contours, and constant cross-section geometry and varying surface contours. The 3D thermoplastic pultrusion system and method including at least one of one or more pairs of shapeable and flexible dual-temperature bands and a rotating assembly that rotates the one or more sets of 3D thermoplastic forming machines to impart a twist to the thermoplastic composite.

A device for coating a thread with a coating material includes a housing, a die body, and a supply line for the coating material. The housing includes a support and a cover mounted on the support, delimiting a chamber. The die body is installed in the chamber, between the support and the cover. The die body includes a lower part and an upper part, with a calibrated die channel being located between the lower and upper parts. Between the support and the cover are an inlet through passage and an outlet through passage. The inlet and outlet passages and the die channel are aligned, so that a thread is able to be passed longitudinally therethrough. The supply line for the coating material includes a lower outlet end located close to the thread, between the inlet or upstream through passage and the die channel.

A method for manufacturing a wind turbine blade, comprising the steps of:

providing one or more individual pultrusions including a first tapering end with a tapering end face terminating in a taper tip, and

arranging the one or more pultrusions in one layer or more stacked layers including at least a bottom layer on a first assembly surface at a first assembly station to provide a pultrusion arrangement extending in a longitudinal direction between a pultrusion root end and a pultrusion tip end, wherein the first tapering end of the one or more pultrusions form the pultrusion root end or the pultrusion tip end of the pultrusion arrangement.

The manufacture of structural elements for aircraft requires the use of complex and costly methods, particularly in the case of parts of elongate overall shape and variable thickness or cross section made of composite material. The disclosure herein proposes to overcome this problem by a method that allows the manufacture of a structural part from a preform made of composite material of simple shape obtained by pultrusion and of one or more reinforcing elements made of composite material and secured by cocuring with the preform to a region of this preform which region is to be reinforced.

A head is disclosed for use with a continuous manufacturing system. The head may have a housing configured to receive a matrix and a continuous fiber, and a diverter located at an end of the housing. The diverter may be configured to divert radially outward a matrix-coated fiber. The head may also include a cutoff having an edge configured to press the matrix-coated fiber against the diverter.

A method is disclosed for continuously manufacturing a composite hollow structure. The method may include continuously coating fibers with a matrix, and revolving matrix-coated fibers about a non-fiber axis. The method may also include diverting the matrix-coated fibers radially outward away from the non-fiber axis, and curing the matrix-coated fibers.

Straight plastic profiles from a plastics material and a continuous reinforcement are predominantly produced continuously in a strand, usually by the pultrusion method. As the plastic profile is pulled through a mold, only straight plastic profiles are formed in known pultrusion methods. In the production of plastic profiles using semi-finished products or complex fibrous constructions, congestion of the fibrous constructions or of the semi-finished products, and thus solidification of the material, may arise when entering the mold, such that the process has to be stopped. A method and a device for the simple production of individually molded plastic profiles is provided in that the mold is formed from at least two mold parts that in relation to the cross section of the plastic profile are split and are moved in a temporally offset manner counter to a production direction of the plastic profile along a portion of the plastic profile.

Disclosed is a part element for a wind turbine blade and a method for manufacturing a part element. The part element comprises a primary sheet having a primary first side and a primary second side. The part element comprises a first fibre thread extending in a primary first direction and forming a first primary loop on the primary first side of the primary sheet from a primary first L1 point to a primary first L2 point. The part element comprises a second fibre thread extending in a primary second direction and forming a second primary loop extending from a primary second L1 point at the primary first side of the primary sheet to a primary second L2 point at the primary first side. A first pre-shaped element is positioned between the first fibre thread and the second fibre thread.