B29C31/08

Tape-laying device and tape-laying method for flexibly and quickly laying tapes with different widths

A tape-laying apparatus includes a material feeder configured to feed tapes, and a laying device configured for picking up and placing tapes onto a laying table. The laying device includes a transporter and a vacuum. The vacuum is connected to the transporter such that at least one tape is configured to be held on the transporter by a negative pressure generated by the vacuum. The transporter includes at least two endless transport belts, which circulate around deflection rollers. The transport belts run parallel to one another in a same transport plane.

Tape-laying device and tape-laying method for flexibly and quickly laying tapes with different widths

A tape-laying apparatus includes a material feeder configured to feed tapes, and a laying device configured for picking up and placing tapes onto a laying table. The laying device includes a transporter and a vacuum. The vacuum is connected to the transporter such that at least one tape is configured to be held on the transporter by a negative pressure generated by the vacuum. The transporter includes at least two endless transport belts, which circulate around deflection rollers. The transport belts run parallel to one another in a same transport plane.

APPARATUS AND METHOD FOR CORRECTING MISALIGNMENT OF A STRIP
20200407180 · 2020-12-31 ·

Disclosed is an apparatus and method for correcting misalignment of a strip, wherein the apparatus includes a correction device with an alignment surface for supporting a strip in a support plane, wherein the support plane extends at a support angle with respect to a first vertical plane in a range of five to thirty degrees, wherein the support plane intersects with a second vertical plane that is perpendicular to the first vertical plane at an intersecting line, wherein the correction device further includes one or more correction elements for exerting a displacement force onto said strip in a correction direction parallel to the support plane and transverse to the intersecting line.

Wind turbine blades
10875287 · 2020-12-29 · ·

A method of making a wind turbine blade having at least one pultruded strip of fibrous reinforcing material integrated with a shell of the blade is described. The method comprises the steps of: providing at a first location a feed apparatus for dispensing a pultruded strip of fibrous reinforcing material; supporting a coiled pultruded strip of fibrous reinforcing material for rotation in the feed apparatus; causing the coiled strip to rotate in the feed apparatus at the first location; and feeding a free end of the strip from the feed apparatus in a feed direction towards a second location remote from the first location. An associated feed apparatus for use in the method is also described.

Production system for laying fibre tapes

The invention relates to a production system (1) for laying fiber tapes (2), said production system (1) comprising: a laying device (5) having at least two roll-out devices (9); an application device (6) having an application surface (32) for receiving the fiber tape (2), wherein the fiber tape (2) can be rolled out in strips onto the application surface (32); a manipulation device (7) for manipulating the fiber tape (2) applied to the application device (6), wherein the manipulation device (7) has a receiving surface (59) for receiving the fiber tape (2). The application surface (32) of the application device (6) is divided into at least two sub-regions (35) when seen over the width (34) of the application device (6), wherein each of the sub-regions (35) is assigned to a roll-out device (9) and wherein the at least two sub-regions (35) of the application surface (32) and the respective related roll-out device (9) of the laying device (5) can be moved relative to one another in the longitudinal extension (33) of the application surface (32) independently of the further roll-out device (9) and the further sub-region (35).

SYSTEM AND METHOD FOR MANUFACTURING A COMPOSITE ASSEMBLY

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.

Conveyance device and conveyance head

A conveyance device includes a plurality of holding mechanisms and one or more pressing mechanisms, the holding mechanisms each include a holder that holds a molding material and a holder movement mechanism that moves the holder, and the pressing mechanisms each include a pusher that comes into contact with and pushes the molding material and a pusher movement mechanism that moves the pusher.

Conveyance device and conveyance head

A conveyance device includes a plurality of holding mechanisms and one or more pressing mechanisms, the holding mechanisms each include a holder that holds a molding material and a holder movement mechanism that moves the holder, and the pressing mechanisms each include a pusher that comes into contact with and pushes the molding material and a pusher movement mechanism that moves the pusher.

COMPOSITE STRUCTURE FABRICATION SYSTEMS AND METHODS

Composite structure fabrication systems and methods. The systems include a plurality of ply carriers, each of which is configured to support at least one ply segment, and an elongate forming mandrel, which defines an elongate ply forming surface that is shaped to define a surface contour of the composite structure. The systems further include a carrier transfer device, which is configured to selectively convey a selected ply carrier from a ply kitting area to an intermediate location, and a forming machine, which is configured to deform the selected ply carrier and a respective ply segment over a selected portion of the elongate ply forming surface. The forming machine further is configured to separate the selected ply carrier from the respective ply segment and return the selected ply carrier to the carrier transfer device. The methods include methods of operating the systems.

COMPOSITE STRUCTURE FABRICATION SYSTEMS AND METHODS

Composite structure fabrication systems and methods. The systems include a plurality of ply carriers, each of which is configured to support at least one ply segment, and an elongate forming mandrel, which defines an elongate ply forming surface that is shaped to define a surface contour of the composite structure. The systems further include a carrier transfer device, which is configured to selectively convey a selected ply carrier from a ply kitting area to an intermediate location, and a forming machine, which is configured to deform the selected ply carrier and a respective ply segment over a selected portion of the elongate ply forming surface. The forming machine further is configured to separate the selected ply carrier from the respective ply segment and return the selected ply carrier to the carrier transfer device. The methods include methods of operating the systems.