A multiaxial product including at least three thread layers, each of the thread layers being formed by multi-filament reinforcing yarns which are arranged within thread layers so as to be mutually parallel and next to one another so as to be adjacent, at least two thread layers being arranged within multiaxial product wherein thread layers define a 0° direction within multiaxial product and the at least one further thread layer being arranged at an angle of more than±10° with respect to 0° direction within multiaxial product, the at least two thread layers in 0° direction directly following one after the other, based on relative arrangement of the at least three thread layers within multiaxial product, without a further layer of multi-filament reinforcing yarns therebetween. Further, a method for producing multiaxial product, further relating to composite produced from multiaxial product and to a method for producing composite from multiaxial product.

The present invention generally relates to fiber-reinforced composites, including carbon-fiber composites. These materials are useful in load-bearing components for mechanical systems, and other applications. Surprisingly, the carbon fibers can be aligned using an applied magnetic field applied directly to the carbon fibers, rather than to magnetic materials that are used to indirectly align the carbon fibers. For example, the carbon fibers may exhibit an anisotropic diamagnetic response in response to a magnetic field, which can be used to align the fibers. In some cases, the carbon fibers may be relatively pure, and/or have a relatively high modulus, which may result in diamagnetic properties. Other embodiments are generally directed to systems and methods for making or using such composites, kits involving such composites, or the like.

A flow-enhancing fabric extends in a longitudinal direction and in a transverse direction. The fabric includes a plurality of fibre layers including a first fibre layer and a second fibre layer arranged upon each other, the first fibre layer has a first plurality of fibre bundles oriented in parallel in a first fibre direction and has a plurality of first glass fibre bundles and a number of first carbon fibre bundles. The second fibre layer has a second plurality of fibre bundles oriented in parallel in a second fibre direction different from the first direction and has a plurality of second glass fibre bundles and a number of second carbon fibre bundles. At least a number of first carbon fibre bundles intersect and contact a number of second carbon fibre bundles. The fabric has a plurality of monofilaments arranged between the first and second fibre layer along the transverse direction.

Disclosed herein are systems and techniques for producing complex components using a reinforced thermoplastic material. The complex components can include contoured or curved outer surfaces, and in some cases define a cavity. In certain examples, one or more thermoplastic materials are arranged to form a wheel component, such as that adapted to define a rim of the bicycle. Thermal bonding can be used to join multiple reinforced thermoplastic materials to one another in order to form a cavity of the wheel component or other complex shape. In certain examples, a portion of a tooling assembly can be pressurized to maintain a shape of the cavity during thermal bonding and cooling. This can remove the need for a sacrificial bladder or other structure that would maintain the shape of the cavity, allowing for a seamless final component, optionally absent indicia of bladder exit or other seams.

The present disclosure provides for a reinforced elastomeric blade having a plurality of laminated layers. The laminated layers can include at least two layers of elastomeric material at least partially separated by a fiber reinforced laminate layer or an embedded metal layer.

A manufacturing line for manufacturing layered products, comprising a plurality of manufacturing stations disposed along a transportation track of a transportation system. The plurality of manufacturing stations includes a number of layer dispensing stations, the transportation system comprising a plurality of product holders that are each arranged to be moved individually along the transportation track to visit manufacturing stations along the transportation track. The product holders are arranged to hold a stack of layers, and the transportation track includes a loop and a router. The router is arranged to route product holders to revisit manufacturing stations via the loop in the transportation track.

The method of forming reinforced fiber base material is provided with: arranging, on the mold having a projection with a upper surface, a platform that is adjacent to the projection and has a flat upper surface at the same height as the upper surface of the projection; forming the laminate by placing reinforced fiber base material in layers on the upper surface of the projection; placing an end of the laminate in the width direction extending out of the upper surface of the projection, on the upper surface of the platform, with the end of the laminate in the width direction sandwiched in a vertical direction by a pair of the films of which outer ends in the width direction are fixed to each other; and removing the platform and pulling out the pair of the films while shaping the laminate along the projection.

Described are methods and systems for a composite structure that allows for out of autoclave curing. Due to the layout of the composite structure, voids within the composite structure, formed out of autoclave, is reduced. The composite structure includes a composite laminate and one or more infusion films. The composite laminate includes a plurality of fiber tows that each include a plurality of fiber strands and a resin. The resin has a first viscosity within a first temperature range. The infusion film is disposed on a surface of the composite laminate and has a second viscosity lower than the first viscosity within the first temperature range. Methods of curing the composite structure are also described.

A manufacturing method for incorporating holes in composite laminates (e.g., structural composites) is disclosed. Also described is a hole-making method for composite laminates prepared using heat vacuum assisted resin transfer molding (HVARTM) technique. In one example, the method comprises providing one or more layer of fibers; inserting one or more pins in the one or more layers of fiber; contacting the one of more layers of fiber with a resin for forming the polymeric matrix; curing the resin to form the polymeric matrix; and removing the one or more pins, thereby preparing a composite wherein the composite comprises one or more holes extending from an outer surface of the composite toward or all the way to an opposite outer surface of the composite. Composite materials produced by the method are also disclosed.

Disclosed herein are systems and techniques for producing complex components using a reinforced thermoplastic material. The complex components can include contoured or curved outer surfaces, and in some cases define a cavity. In certain examples, one or more thermoplastic materials are arranged to form a wheel component, such as that adapted to define a rim of the bicycle. Thermal bonding can be used to join multiple reinforced thermoplastic materials to one another in order to form a cavity of the wheel component or other complex shape. In certain examples, a portion of a tooling assembly can be pressurized to maintain a shape of the cavity during thermal bonding and cooling. This can remove the need for a sacrificial bladder or other structure that would maintain the shape of the cavity, allowing for a seamless final component, optionally absent indicia of bladder exit or other seams.