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.

Disclosed is a vacuum apparatus for applying a vacuum to a reinforcement lay-up during in composite manufacture, and a method of use. The vacuum apparatus comprises a vacuum port component (100) having body portion (102) defining a contact surface (104) and an internal cavity. A vacuum port (108) for connection to a vacuum pump is oriented away from the contact surface communicates with the internal cavity. The vacuum port component can be connected to vacuum component (200) body portion also defining a contact surface and an internal cavity (207), and further comprising a plurality of inlet apertures or slots (206) extending therethrough and in communication with the vacuum component internal cavity.

The disclosure relates to a method for producing a component of a rotor blade in that a vacuum film (16) is placed on a positive mould (1), layers (17) are laid on the positive mold (1), a negative mould (3) is pivoted over the occupied positive mold (1), the vacuum film (16) is then sealed from the negative mould (3), a vacuum is then drawn against the negative mold (3), and the negative mould (3) together with the layers (17) is then pivoted back.

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 of heating a tool assembly includes the step of joining a first piece of the tool assembly with a second piece of the tool assembly via a first joint portion and a second joint portion. The method further includes the step of inserting a fastener through the first joint portion and the second joint portion of the tool assembly. The method further includes the step of applying heat to the tool assembly, wherein upon heating, interlock surfaces of the first joint portion and the second joint portion tighten against each other.

An article for damping vibrations by constrained layer damping comprising: a first constraining layer; a second constraining layer; and a damping layer disposed between the first and second constraining layers, wherein the first and second constraining layers each independently comprise a fibre-reinforced composite material, wherein the first and second constraining layers each independently have a thickness from 1.5 to 5 mm, wherein the damping layer comprises a viscoelastic material, wherein the damping layer has a thickness from 1 to 10 mm and wherein the article has a thickness from 6 to 50 mm. The invention also relates to the use of said article for damping vibrations in a vehicle.

According to one implementation, a composite material structure includes a corrugated stringer and a panel. The corrugated stringer has a corrugated structure including portions each having hat-shaped cross section. The corrugated stringer is made of a composite material. The panel is integrated with the corrugated stringer. The panel is made of a composite material. Further, according to one implementation, a manufacturing method of a composite material structure includes: setting a textile on a laminated body of prepregs; and producing the composite material structure by covering the laminated body with a bagging film, forming a vacuum state in a space covered with the bagging film, impregnating the textile with the resin, and thermal curing of the laminated body of the prepregs. The laminated body is a panel before curing. The textile has a structure corresponding to a corrugated stringer.

Provided is a tube body intermediate including: a carbon fiber disposed with respect to an outer circumferential surface of a mandrel so as to extend in an axial direction of the mandrel; and a fixing member having a tubular shape and disposed with respect to the outer circumferential surface of the mandrel so as to cover the carbon fiber. Also provided is a tube body production method including: disposing a fiber body with respect to an outer circumferential surface of a mandrel so that the fiber body extends in an axial direction of the mandrel; disposing a fixing member with a tubular shape with respect to the outer circumferential surface of the mandrel so that the fixing member covers the fiber body; and impregnating the fiber body with a resin on the outer circumferential surface of the mandrel and then heating the resin to mold the resin.

A molding system and methods of forming a structure are presented. The molding system is configured to sequentially form features of a structure. The molding system comprises a first tool comprising a number of features configured to completely form a first set of radii of a structure and a number of partial forming features configured to partially form a second set of radii of the structure, and a second tool comprising a number of completion features configured to complete shaping of the second set of radii.