Disclosed is a clamping tong for securing a shell part of a wind turbine blade in a mould and a mould comprising a clamping tong. The clamping tong comprises a first tong segment, a second tong segment and a third tong segment. The third tong segment has a clamping surface for applying a clamping force on a mould section, such as a mould flange of the mould. The clamping tong is configured to reposition the clamping surface between a clamping state and a release state. The distance between the clamping surface and the first tong axis in the clamping state is shorter than the distance between the clamping surface and the first tong axis in the release state. Thereby, the clamping surface may provide the clamping force on the mould section in the clamping state. The first tong segment is attachable to the mould.

A method of additively printing an extension segment on a workpiece includes pretreating a workpiece-interface of the workpiece using an energy beam emitted from an energy beam source of an additive manufacturing machine, providing a pretreated workpiece-interface having received a pretreatment, with the pretreatment remediating an aberrant feature of the workpiece and/or the workpiece-interface. The method further includes additively printing an extension segment on the pretreated workpiece-interface using an energy beam emitted from the energy beam source of the additive manufacturing machine. The aberrant feature includes one or more aberrant regions of the workpiece-interface having been determined from a digital representation of the workpiece-interface captured by a vision system. The pretreatment includes heat-conditioning at least a portion of the workpiece-interface including the one or more aberrant regions of the workpiece-interface.

This invention relates to a dispenser device for and a method of applying a structural adhesive to an application surface on a wind turbine blade structure, wherein the dispenser device comprises a housing forming a reservoir configured to hold a surplus of structural adhesive during dispensing. The reservoir is connected to an inlet for supplying the structural adhesive and an outlet for dispensing the structural adhesive. The outlet may be a side opening arranged in an exchangeable housing part. The dispenser device may also comprise an adjustable mechanism connected to a plate member configured to be moved relative to the side opening. The operation of the adjustable mechanism is controlled via a control unit or a control element. The exchangeable housing part or adjustable mechanism enables the cross-sectional profile, the width and/or the height of the dispensed structural adhesive to be changed before or during dispensing.

A modular molding device for creating a mold for a blade segment of a wind turbine blade of a wind turbine, the modular molding device including: a flexible support plate forming the mold for the blade segment, at least one bending apparatus including at least a first end and a second end, the at least one bending apparatus attached to the support plate and configured to bend the support plate from a first support plate shape to at least one second support plate shape, and at least one connection means, which is configured to removably connect the flexible support plate of the modular molding device with at least one connection of a flexible support plate of another modular molding device is provided. Moreover, a molding system and a method for creating a mold for a blade segment of a wind turbine blade of a wind turbine is also provided.

The invention relates to a resin injection regulator for a resin injection circuit in a mould for producing a composite part, in particular a turbine engine composite part, characterised in that it comprises at least one vessel which is connected to said circuit and inside of which a movable wall means can be moved in a sealed manner, said movable wall means defining in said vessel a first cavity which forms a container for accumulation of resin and is designed to be connected to at least one part of said circuit, and a second cavity which is designed to be connected to a source of pressurised fluid, said movable wall means being designed to be urged by the pressurised fluid with which the second cavity is supplied in order to exert a pressure on the resin contained in the first cavity by isolating said resin from said fluid.

A method and system temporarily holds a workpiece, most suitably an aero engine turbine blade element during manufacture. The workholding system includes a support body with a contoured body surface, complementary to a workpiece surface, formed of a transparent material to define a bonding zone. The support body is supported by a base to form a workpiece shuttle, and a bond station receives the workpiece shuttle. Complementary zero-point locating elements on the shuttle and station assure accurate positioning. The bond station further has workpiece locating elements configured to accurately position the workpiece on the shuttle in a predetermined position relative to the zero-point locating elements of the shuttle, thereby compensating for shuttle-to-shuttle variance. An adhesive, such as a UV curable adhesive, is applied to the bonding zone and cured by UV through the transparent material, thereby fixing the workpiece in the predetermined position.

A method of making a wind turbine blade (10) having a shear web (20, 22) bonded between first and second half shells (16, 18) is described. The method involves providing a web locator (40) on an inner surface of a half shell. The web locator has a fixed portion (42) and a spring portion (44) extending from the fixed portion. The spring portion is moveable relative to the fixed portion between compressed and relaxed states.

A rotor blade assembly includes a rotor blade defining a pressure side and a suction side extending between a leading edge and a trailing edge. Further, the rotor blade assembly includes at least one structural feature secured within the rotor blade and spaced apart from the trailing edge to define a void between the pressure side, the suction side, and the trailing edge. Moreover, the rotor blade assembly includes an adhesive filling the void between the pressure side, the suction side, and the trailing edge to provide an adhesive connection between the pressure side, the suction side, the trailing edge, and the structural feature(s). In addition, the adhesive contacts the structural feature(s) at an interface and defines a fillet profile.

Provided herein is a wind turbine blade mold system having built in precision pins to locate structural components (e.g. spar caps) during layup of composite segments. A plurality of pins can be inserted into apertures within the mold, with discs attached to the pins to maintain fixed relative distance to spar caps positioned relative to the pins to ensure precise positioning, thereby preventing/inhibiting movement of the spar cap relative to the mold. The pins can include a first extension that pierce through the layers of composite layups, and protrude above the B-surface of the blade skin. Additionally, the pins can include a marker tip releasably attached to the pin top to provide visual identification of the pin and underlying structural components. The pins can remain embedded within the final molded part.

A blade is provided. The blade comprises a plurality of a first composite fiber plies and a plurality of a second composite fiber plies. Ends of the second fiber plies are staggered such that interlock between the first composite fiber plies and the second composite fiber plies is formed in a region where the second composite fiber plies end and meet with the first composite fiber plies. The blades are used for an engine of an aircraft.