Provided is a method of manufacturing a wind turbine rotor blade spar cap, which method includes providing a plurality of carbon profile elements; providing a number of adhesive film layers; preparing a spar cap assembly by arranging the carbon profile elements in a stack and arranging an adhesive film layer between adjacent carbon profile elements of the stack; and curing the spar cap assembly. The embodiments further describe a wind turbine rotor blade spar cap, and a wind turbine rotor blade including such a spar cap.

A method for producing a fiber composite component assembly having at least first and second plate-shaped composite structures made from synthetic resin embedded fibers, the at least first and second fiber composite components having a plurality of partial regions not containing synthetic resin is described. The method includes positioning the at least first and second fiber composite components, the partial regions having been brought to flush conformity with each other, bonding the at least first and second positioned fiber composite components by the adhesive layer arranged in between, placing mechanical reinforcement means through the partial regions, infusing the dry partial regions with synthetic resin, and curing the synthetic resin placed in the partial regions.

A layered composite assembly may include a plurality of composite fiber layers stacked onto one another. Each of the plurality of composite fiber layers may include a main body including a plurality of composite fibers. The main body may be pre-impregnated with at least one resin. Each composite fiber layer also includes a plurality of layer-securing pins secured to the main body. The layer-securing pins are configured to mechanically connect the main body to an adjacent composite fiber layer.

Methods for manufacturing elongated structural elements are provided. Such methods provide composite material having optimal properties such as weight and strength which can be produced at much lower costs compared to conventional methods. Composite materials including such elements are also provided. In addition, commercial products incorporating such structural elements are provided.

A method for manufacturing a pneumatic tire may include lap-splicing end parts of a laminate sheet in which a sheet obtained from a thermoplastic resin or a thermoplastic resin composition of a thermoplastic resin blended with an elastomer is laminated with a rubber that undergoes vulcanizing adhesion with the thermoplastic resin or the thermoplastic resin composition. After the sheet obtained from the thermoplastic resin or the thermoplastic resin composition is cut into lengths to be supplied for lap-splicing, and at a stage before tire vulcanization molding, distal end parts of the sheet obtained from the thermoplastic resin or the thermoplastic resin composition are sharpened with a thermal treatment.

A method is provided in one example embodiment and may include assembling a first component and a second component together using, at least in part, a first adhesive film on the first component and a second adhesive film on the second component, wherein the first component and the second component are fully cured and the first adhesive film and the second adhesive film are at least partially uncured; and curing the first adhesive film and the second adhesive film to form a bonded structure.

The invention relates to a method for producing a fiber-composite hollow component from a fiber-composite material which contains at least one fibrous material and one matrix material, wherein the fiber-composite hollow component is formed from at least two fiber-composite half-shells which in a joining edge region of the fiber-composite half-shells are joined to one another such that a cavity is configured between the joined-together fiber-composite half-shells, wherein the method comprises the following steps: providing a first fiber-composite half-shell formed from the fibrous material of the fiber-composite material, and at least one second fiber-composite half-shell formed from the fibrous material of the fiber-composite material; assembling the first fiber-composite half-shell and the at least second fiber-composite half-shell so as to form the fiber-composite hollow component; wherein at least one spacer element is inserted in the joining edge region between the first fiber-composite half-shell and the at least second fiber-composite half-shell; incorporating an internal vacuum cover in the cavity formed by the assembling of the fiber-composite half-shells, and incorporating the assembled fiber-composite half-shells in an external vacuum cover such that a component cavity having the fibrous material of the fiber-composite hollow component to be produced is formed between the internal vacuum cover and the external vacuum cover; evacuating the component cavity having the fibrous material; and curing the matrix material which embeds the fibrous material of the fiber-composite half-shells, in order for the fiber-composite hollow component to be produced.

Disclosed is joining device for joining a trailing end of a first strip to a leading end of a second strip to form a tire component. The joining device includes a support member with a support surface and a retaining member with a retaining surface for retaining the second strip. The joining device is arranged for positioning the leading end of the second strip in a joining orientation in which said leading end is closer to the support plane than the rest. The joining device also includes a control unit for controlling a relative movement between the support member and the retaining member with a first component in a placement direction to place the leading end of the second strip and a second component in a joining direction to bring the leading end of the second strip into contact with the trailing end of the first strip.

A composite panel is constructed by preparing a panel assembly layup including a first prepreg layer having reinforcement material, a first layer of a resin formulation upon a first outer surface, and a second layer of the resin formulation upon an opposing outer surface, where the first layer is thinner than the second layer, and the first layer is presented toward a mold. The layup includes a core layer directly abutting the second layer. They layup includes a second prepreg layer having a first layer of the resin formulation upon a first outer surface, and a second layer of the resin formulation upon an opposing outer surface, where the first layer is thinner than the second layer, and the second layer directly abuts the core layer. The panel assembly is cured in the mold.

Method for manufacturing stiffened panels comprising the following steps: forming a first and a second wet skin, each comprising a plurality of plies of preimpregnated composite material; forming a plurality of pairs of wet stringers, comprising a plurality of plies of preimpregnated material, wherein forming each pair of wet stringers comprises a) forming an assembly having a central web extending between opposite end flanges, and b) cutting the assembly along a median plane so as to form a pair of wet stringers, placing the pairs of wet stringers on the first wet skin by means of removable supporting members; turning the second wet skin over and placing it on the pairs of stringers, so as to obtain a pair of wet panels arranged above each other; and subjecting the pair of wet panels to a same curing cycle.