A pultrusion process for making a strip for an elongate reinforcing structure of a wind turbine blade, the process comprising drawing fibres (42) and resin through a pultrusion die (40) in a process direction to form a strip (102); and applying an infusion-promoting layer (110) to a surface of the strip down-stream from the die in the process direction. A pultrusion apparatus is also disclosed.

Method for testing a fiber composite component, in particular a body component for a vehicle, wherein the fiber composite component comprises a sensor device which is integrated in the fiber composite component, wherein the sensor device comprises a flexible circuit carrier having a sensor module, in particular having a micromechanical sensor module, for ascertaining an acceleration value, said method comprising the steps: setting the fiber composite component into a test vibration, in particular by applying a test pulse to a test site of the fiber composite component; capturing a response signal using the sensor device; and comparing the response signal with a reference signal.

A hockey stick with a co-molded structure and method where the blade member is formed by a molding process onto a preformed shaft member, where the preformed shaft member has a contoured tip at the blade end. The contoured tip helps to secure the blade member to the shaft member in conjunction with the molded composite layers, and in one example, the contoured tip has a width that is greater than the width of the shaft member at the blade-starting region.

A method of forming parts uses a forming tool having a forming surface, and an ultrasonic transducer array on the forming surface.

A high pressure container has enhanced pressure resistant strength, and a method for manufacturing such high pressure container. The high pressure container includes a sealable hollow liner and a reinforcement layer including a composite carbon fiber bundle covering an outer surface of the hollow liner, wherein the reinforcement layer is wound around the outer surface of the hollow liner and fixed with a cured product of thermosetting resin, and a stress relaxation portion including the cured product of thermosetting product and a plurality of carbon nanotubes between a carbon fiber contained in one composite carbon fiber bundle and a carbon fiber contained in the other composite carbon fiber bundle.

A conduit embedded in thermoplastic and adhered to a pipeline with a porous material assisting in the adhesion. The porous material is adhered to the pipeline, the porous material having at least some pores occupied by the thermoplastic. The porous material may be a sleeve of fibrous material. The adhesion may be accomplished by positioning a sleeve of fibrous material around a guide, bringing the thermoplastic into contact with the sleeve and heating the thermoplastic to cause the thermoplastic to enter pores of the sleeve. The guide forms a barrier preventing the thermoplastic from reaching a portion of the sleeve, and that portion is adhered to the object. This method may also be applied to adhere a thermoplastic, with or without a conduit, to any object.

A tank manufacturing method includes the steps of (a) forming a reinforcing layer before hardening, (b) embedding at least a part of a label into the reinforcing layer before hardening, and (c) winding glass fiber with thermosetting resin before hardening impregnated so as to cover the label to form a surface layer before hardening. The step (a) includes (a1) forming an inner layer before hardening, and (a2) forming an outer layer before hardening having a cover rate lower than the inner layer before hardening and lower than 100%, the outer layer before hardening being arranged on the inner layer before hardening.

A composite material structural member including a core member, composite material members, and at least one composite material sheet. The members are disposed around the core member and are adhered to each other to form a hollow space. The composite material sheet is disposed between the core member and the members so as to overlap the bonded portion between the members. The composite material sheet forms a hollow composited structure together with the members.

A unitary reinforced composite based panel component, and methods of construction thereof is provided. The unitary reinforced panel component eliminates the need for adhesively joining an offset piece to the backside of a panel, to provide additional reinforcing strength thereby improving efficiency and eliminating bond-line read-through (BLRT). A vehicle component is prepared with resort to a preform made of selective comingled fiber bundle positioning (SCFBP) to selectively place co-mingled fibers that are enriched in carbon fiber as a reinforcement relative to other region that rely on a relatively higher percentage of glass fiber reinforcement to create such a preform.

The present invention relates to a novel process for the production of novel fibre-reinforced profile materials filled with a rigid foam core, especially a PMI foam core. In particular, the present invention relates to a novel process which, in various versions, provides a particularly high throughput and allows a very wide range of shaping options. One step here continuously produces a complex fibre-reinforced profile material and simultaneously inserts the rigid foam core into same. In addition, in the same process step, very good binding of the rigid foam core to the fibre-reinforced profile material is assured. Shaping further takes place in two or more moulds simultaneously to achieve a particularly high throughput and simultaneously produce profile materials differing in shape.