Laminated parts are described that include a core, a fiber layer arranged on each side of the core and impregnated with a polyurethane resin, and an outer layer that at least partially coats at least one of the polyurethane impregnated fiber layers, in which the outer layer is the cured reaction product of a reaction mixture that includes: (1) a polyisocyanate, (2) a polyether polyol having a molecular weight of 800 Da to 25,000 Da and a functionality of 2 to 8, and (3) a fatty acid ester having isocyanate-reactive functionality. Methods of producing such laminated parts are also described.

Described herein is a 3D spacer fabric reinforced composite, a process for producing it, a method of using it in footwear, and a footwear including it.

Described herein is a 3D spacer fabric reinforced composite, a process for producing it, a method of using it in footwear, and a footwear including it.

A method for manufacturing a wind turbine blade, including the step of monitoring a process of infusing and/or curing a fiber lay-up with resin in a mold, wherein the monitoring is based on sensor data obtained from the resin infusion and/or curing process displayed in an augmented reality device, is provided. Displaying sensor data obtained from the resin infusion and/or curing process in an augmented reality device allows to better monitor the resin infusion and/or curing process. Thus, the quality of the manufactured wind turbine blade can be improved.

A liquid composite molding method includes the steps of providing a part mold that has an inlet gate and an exit gate, placing a fabric preform over the part mold, placing a membrane over the fabric preform and securing a pressure cap to the part mold. The pressure cap and part mold together form a pressure chamber with a headspace between the membrane and the pressure cap. The method further includes the step of filling the fabric preform with liquid resin under the membrane while applying pressure within the headspace over the membrane. The method may be practiced with an apparatus that has a pressure chamber, a fabric preform inside the pressure chamber, a membrane over the fabric preform, a resin injection assembly, and a resin extraction assembly. The pressure chamber includes a part mold and a pressure cap. A headspace is formed above the membrane within the pressure chamber.

A liquid composite molding method includes the steps of providing a part mold that has an inlet gate and an exit gate, placing a fabric preform over the part mold, placing a membrane over the fabric preform and securing a pressure cap to the part mold. The pressure cap and part mold together form a pressure chamber with a headspace between the membrane and the pressure cap. The method further includes the step of filling the fabric preform with liquid resin under the membrane while applying pressure within the headspace over the membrane. The method may be practiced with an apparatus that has a pressure chamber, a fabric preform inside the pressure chamber, a membrane over the fabric preform, a resin injection assembly, and a resin extraction assembly. The pressure chamber includes a part mold and a pressure cap. A headspace is formed above the membrane within the pressure chamber.

The present disclosure provides for a root plate assembly system, an axially adjustable, rigid connection between a metallic (e.g. steel) root plate and a composite root flange of a wind turbine blade mold. The system includes a root plate including a flange portion with at least one aperture disposed therein. The system includes a sealing collar disposed within the aperture in the root plate. The system includes at least one washer having a larger diameter than the aperture in the root plate. The system includes a threaded collar having a longitudinally extending channel and threads on an outer surfaces thereof. The system includes a fastener disposed at least partially within the longitudinally extending channel of the threaded collar. The system includes a locknut disposed above the fastener abutting the fastener and a bolt cover disposed over the locknut, the bolt cover abutting the collar.

A system for constructing a composite structure includes a braiding machine, a winding tool and a forming machine. The composite structure is constructed of a wound tubular braiding. The wound tubular braiding is constructed of a biaxial or triaxial tubular braid of unidirectional tape.

A method for closing an injection mold for manufacturing a revolution part made of composite material, the mold including a mandrel supporting a fiber preform and angular sectors comprising an annular base to come into contact with the fiber texture, the annular base extending between first and second side edges along a circumferential direction. The method includes successive positioning and fixing the angular sectors on the mandrel, the annular base of each sector compacting the fiber preform portion present oppositely, the side edges of the annular base of each angular sector being in contact with the side edges of the annular base of the adjacent sectors. Before the positioning and fixing of the angular sectors on the mandrel, strip s are placed on the exposed surface of the fiber preform, each strip covering an area of the fiber preform located facing a junction area between two adjacent angular sectors.

A process for manufacturing a blade made of composite material for a turbomachine is provided. The blade includes an airfoil having a pressure side and a suction side which extend from a leading edge to a trailing edge of the airfoil. The blade further includes a metal sheath that extends along the leading edge of the airfoil. The process includes the steps of: a) placing a preform, made by three-dimensionally weaving fibers, in a mold, a polymerizable adhesive being inserted between the sheath and the edge of the preform; and b) injecting polymerizable resin into the mold to impregnate the preform so as to form the airfoil after solidifying, wherein the resin is injected within a time interval during which the adhesive reaches a freezing point.