Layers of composite material, such as pre-peg, may be deposited on a reconfigurable polymer mold. An array of actuated pins may deform the polymer mold into a desired 3D shape. The composite material may be inside a cavity formed by the mold and a flexible bag. A vacuum pump may remove air from the cavity, creating a partial vacuum. The partial vacuum may cause the flexible bag to press the composite tightly against the mold, so that the composite conforms to the desired 3D shape. One or more heating elements may be embedded in the mold and may heat the composite to cure the composite. Ball joints may connect the actuated pins to the polymer mold.

A method for forming an object comprises the steps of: providing a mould comprising a first and a second mould part opposite to each other, a part selected from between the first mould part and the second mould part comprising a plurality of sectors for shaping a lateral portion of the object, the sectors delimiting a variable-volume forming region of the mould; positioning a dosed amount of mouldable material between the first and second mould parts while the mould is in an open position; displacing the first mould part and the second mould part towards each other in a moulding direction, to define between the first mould part and the second mould part a closed forming chamber bringing into contact respective abutment surfaces of the first mould part and the second mould part, the abutment surfaces extending transversely to the moulding direction.

A blade mould and a method for manufacturing a blade shell part of a wind turbine blade is disclosed. The blade mould comprises a first mould frame; a mould shell supported by the first mould frame and provided with a moulding surface that defines an outer shape of the blade shell part, wherein the mould shell has a longitudinal direction and comprises a root end mould part at a first end thereof; and a first deformation device for deforming the root end mould part of the mould shell. The method comprises arranging reinforcement material on the moulding surface of the root end mould part; deforming the root end mould part to a receiving configuration; inserting the root end insert in the root end mould part; and bringing the root end mould part to a moulding configuration.

A composite structure forming system configured to form a contoured elongate composite structure in a continuous process is presented. The composite structure forming system comprises a plurality of charge forming stations and a plurality of conveyor systems. The plurality of charge forming stations is configured to operate in parallel, each charge forming station of the plurality of charge forming stations is configured to form a respective composite charge of the contoured elongate composite structure. Each conveyor system of the plurality of conveyor systems is configured to transport a respective composite charge through a respective charge forming station.

A forming tool for forming a semi-finished product comprising reinforcement fibers and being conveyed to the forming tool in a continuous process. The forming tool comprises at least one pressure bag configured to be pressurized during a forming step of the semi-finished product, during which the semi-finished product is sandwiched between a forming surface of a forming element and the at least one pressurized pressure bag, such that the semi-finished product substantially takes on the shape of the forming surface. Further, a forming apparatus and a forming method for forming a semi-finished product comprising reinforcement fibers are provided.

A tool is configured to have a changeable shape. The tool comprises a thermoplastic polymeric material, resistive heating elements within the thermoplastic polymeric material, and a flexible casing encapsulating the thermoplastic polymeric material and resistive heating elements.

The present invention relates to a method and a mould system (66) for manufacturing at least two preforms for moulding a wind turbine blade. The preforms include at least one preform of a first shape and at least one preform of a second shape. The preform mould structure (68) has a moulding surface (70) of variable shape such that the shape of the moulding surface (70) can be varied at least between a first and a second configuration by using actuators.

A system for manufacturing a composite assembly includes a first mandrel, a second mandrel, a first wrap plate, and a second wrap plate. The first wrap plate and the second wrap plate are positionable in side-by-side relation for receiving a wrap material stack. The first wrap plate and/or the second wrap plate are translatable to a wrap plate open position defining a wrap plate gap between the first and second wrap plate surface edge for receiving a bladder. The second mandrel is translatable to a mandrel open position defining a mandrel gap between the first and second mandrel surface edge. The wrap plate gap and the mandrel gap are configured to receive the wrap material stack formed around a bladder. The first and second wrap plate are configured to fold a first and second material stack base portion into overlapping relation with each other on the bladder top.

A manufacturing apparatus includes an arm main body with a long tubular or columnar shape having a uniform lateral cross-section, and attachment interface parts fixed to both sides of the arm main body and attached to another member. The apparatus includes: a pair of fixing parts supporting a part of each of the attachment interface parts and each end of the arm main body and each including a material filling space at least near a joint part between each of the attachment interface parts and the arm main body; a slide mechanism capable of adjusting a distance between the two fixing parts along a longitudinal axis of the arm main body by moving at least one of the fixing parts; and a material injection part injecting a molten material into the space so as to joint each of the attachment interface parts to each end of the arm main body.

Methods and devices of fabricating a stringer for a vehicle. The stringer can be constructed from two charges that are formed together into the stringer. During fabricating, the ends of the charges can be formed in a die cavity. When the ends are misaligned in the die cavity, one of the charges can be moved in the die cavity to align the ends. The device used for fabricating the charges can include a punch with separate punch plates that move the ends of the charges into the die cavity. The punch plates can be separately moved to adjust the position of the charges and align the ends.