EP2605899A1 - Appareil de distribution d'un ruban composite - Google Patents

Appareil de distribution d'un ruban composite

Info

Publication number
EP2605899A1
EP2605899A1 EP11749054.0A EP11749054A EP2605899A1 EP 2605899 A1 EP2605899 A1 EP 2605899A1 EP 11749054 A EP11749054 A EP 11749054A EP 2605899 A1 EP2605899 A1 EP 2605899A1
Authority
EP
European Patent Office
Prior art keywords
tape
molding tool
resin impregnated
prepreg
spool
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP11749054.0A
Other languages
German (de)
English (en)
Inventor
Daniel K. Buckmiller
Rolf M. Johns
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zoltek Companies Inc
Original Assignee
Zoltek Companies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zoltek Companies Inc filed Critical Zoltek Companies Inc
Publication of EP2605899A1 publication Critical patent/EP2605899A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B29C70/388—Tape placement heads, e.g. component parts, details or accessories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0036—Slitting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/243—Partially cured

Definitions

  • the present invention relates to an apparatus for dispensing composite tape, and more particularly, to an apparatus for laying down prepreg tapes with precision.
  • the apparatus can lay down prepreg onto a molding structure having a contoured surface or a flat surface along a linear or non-linear path.
  • a resin preimpregnated web or tape may be used to construct the particular component desired.
  • Prepreg materials consist of aligned reinforcing fibers (typically carbon, glass, or aramid fibers) that are pre-impregnated with a polymer and used as an intermediate product in the molding of composite structures. Very often these fibers are collimated in a unidirectional configuration forming tape-like products that are typically 12 to 60 inches (30.5 to 152.4 cm) wide.
  • the composite structure is built up of successive layers of the tape applied to a working surface such as, for example, a molding tool, mandrel, or any surface used to form composite parts.
  • a working surface such as, for example, a molding tool, mandrel, or any surface used to form composite parts.
  • a composite wind blade, wind blade spar, or wing structures for example, from prepreg tapes
  • long lengths (i.e., greater than 40 meters) of prepreg tape are laid down on a molding tool with great precision. Precise filament alignment is required to achieve the desired composite properties.
  • uniform compaction of the prepreg tape during the laminate build-up is required to minimize entrapped air, which can cause voids in the cured composite laminate. Very slight misalignment of fiber orientation can cause significant loss of critical engineering properties.
  • Voids in the composite can also result in lower composite properties.
  • Greater than 2% voids can cause significant loss of inter-laminar shear strength and can act as sites for damage growth in the composite during service life.
  • Composite wind blade spars are often straight-sided laminates of varying thickness, for example, from approximately 0.1 inch (0.25 cm) to over 1 .5 inches (3.81 cm) thick. They are typically laid up mold surfaces that can range from flat to varying degrees of concave or convex curvature. For example, the wind blade spar may be flat at the tip and curved at the root.
  • This configuration further adds to the complexity of laying down prepreg tapes with extreme precision. Hand layup of these spars with prepreg tapes is extremely difficult and time consuming, and assuring precision is even more difficult. The alternate extreme to hand layup involves the use of automated tape laying machines. These types of machines have been developed for over two decades, primarily for aerospace structures. While these machines are designed to lay down prepreg tapes with extreme precision, these machines are very expensive and overly complex for wind blade spars.
  • the present invention is directed to an apparatus that is capable of laying down a wide prepreg product for a structure having in-plane curvature, while significantly reducing the effects of wrinkling on the inner radius.
  • an apparatus to apply a resin impregnated tape to the surface of a molding tool including: an upper frame rotatably mounted to a base frame, the upper frame having mounted thereon and rotatable therewith a spool holding assembly for holding a spool of resin impregnated tape wound thereon, a tape compaction assembly including a compaction roller configured to conform to the surface of the molding tool for compacting the resin impregnated tape onto the surface of the molding tool, and a tape tensioning system for exerting tension on the resin impregnated tape.
  • the base frame includes a tracking system for tracking the surface of the molding tool, the base frame being reciprocally movable with respect to the surface of the molding tool.
  • the spool holding assembly includes an alignment system for laterally aligning the spool of prepreg tape relative to the surface of the molding tool.
  • the compaction roller includes a plurality of contiguous disks supported on an axle, the disks having a central bore diameter that is greater than the outer diameter of the axle.
  • the upper frame rotates at least 180° on the base frame to permit changing the direction of application of the resin impregnated tape on the surface of the molding tool.
  • the apparatus may further include a turntable coupled to the upper frame and the base frame to permit rotation of the upper frame on the base frame.
  • the tape tensioning system includes an actuated disk brake. The disk brake may be manually or automatically actuated.
  • the molding tool includes at least one rail and the tracking system includes at least two guide rollers that engage the at least one rail.
  • the surface of the molding tool may include at least one of a convex contour and a concave contour.
  • the width of the resin impregnated tape applied to the molding tool in one embodiment, is within the range of about 1 1 .5 inches (292 mm) to about 60 inches (152.4 cm).
  • that apparatus further includes a slitter for slitting the resin impregnated tape lengthwise into a plurality of strips, the slitter mounted on and rotatable with the upper frame.
  • the slitter may include a plurality of stationary or rotary knives.
  • the plurality of strips of resin impregnated tape is uniform. In another embodiment, the width of the plurality of strips of resin impregnated tape is non-uniform.
  • the apparatus further includes a plurality of accumulator rollers disposed downstream of the slitter, each accumulator roller being
  • the accumulator rollers independently activatable for accumulating and de-accumulating a portion of a respective strip of resin impregnated tape, the accumulator rollers mounted on and rotatable with the upper frame.
  • the apparatus further comprising a controller configured to control at least one of: the placement of the resin impregnated tape on the surface of the molding tool; the tension exerted by the tensioning system on the tape; the direction in which the tape is applied to the surface of the molding tool; and the speed at which the tape is applied to the surface of the molding tool.
  • FIG. 1 is a perspective view of an apparatus for laying down prepreg tape according to an embodiment of the invention.
  • FIG. 2 is a top view of the apparatus of FIG. 1 .
  • FIG. 3 is a front view of the apparatus of FIG. 1 with a spool of prepreg material mounted thereon.
  • FIG. 4 is a side view of the apparatus of FIG. 1 with a spool of prepreg material mounted thereon.
  • FIG. 5 is a perspective view of an embodiment of the apparatus for laying down prepreg tape according to the invention as positioned on a molding tool.
  • FIG. 6 is a front view of the apparatus of FIG. 5.
  • FIG. 7 is a perspective view of the apparatus of FIG. 5, illustrating rotational motion of the upper frame.
  • FIG. 8 is a perspective view of an apparatus for laying down prepreg tape that includes tape slitting and dispensing assemblies in accordance with an embodiment of the present invention.
  • FIG. 9 is a side view of the apparatus of FIG. 8.
  • FIG. 10 is a top view of the apparatus of FIG. 8.
  • FIG. 1 1 is an enlarged top view of the tensioning system of the apparatus of
  • FIG. 12 is a side view of a section of the apparatus of FIG. 8 with a spool of prepreg material mounted thereon.
  • FIG. 13 is a perspective view of the tape alignment assembly of the apparatus of FIG. 8.
  • FIG. 14 is a bottom view of the tape positioning assembly of the apparatus of FIG. 8.
  • FIG. 15A is a schematic drawing illustrating a prepreg tape dispensed using conventional apparatus in a linear direction.
  • FIG. 15B is a schematic drawing illustrating a prepreg tape dispensed using conventional apparatus in a non-linear direction.
  • FIG. 16 is a photograph showing a prepreg tape dispensed using
  • the apparatus of the present invention is useful for forming composite laminated structures by applying tape of continuous fibers that have been
  • an apparatus for laying down a wide, unidirectional prepreg tape for a structure, and in particular, for a wind blade is provided.
  • the apparatus includes a spool holder for demountably holding a spool of a continuous web of prepreg material having a wide width.
  • the apparatus includes a mechanism for properly placing the prepreg on the surface of the molding tool.
  • the apparatus includes a rotatably mounted prepreg tape placement assembly for bi-directional tape placement and compaction.
  • the width of the prepreg tape product is typically in the range of about 1 1 .5 inches (292 mm) to about 60 inches (152.4 cm). In one embodiment, the width of the prepreg tape is about 12 inches (30.5 cm) to about 60 inches (152.4 cm), or about 1 1 .5 inches (292 mm) to about 15.75 inches (400 mm). In general, it is advantageous to use wider prepreg tape so as to increase the rate of prepreg tape lay down, and thus increase production efficiency. With the apparatus of the present invention, it is possible to further increase production rates by providing bi-directional tape placement and compaction. Application of the prepreg material on the molding tool may be carried out in the forward direction and in the reverse direction.
  • the prepreg tape laying apparatus is a carriage 10 that includes an upper frame 12 rotatably mounted to a base frame 14. Mounted on the upper frame 12 are a prepreg spool holding assembly 16 and a compaction assembly 18.
  • the base frame 14 includes a tracking system 20 to precisely place the prepreg material on the surface of the molding tool.
  • the spool holding assembly 16 includes a spindle 22 and spool supports 24 mounted on spindle 22.
  • Spool supports 24 include quick-adjust pins 26 that contact the inside of the prepreg spool core to center the spool 80 on the spindle 22.
  • the spool holding assembly 16 enables rapid prepreg spool change-out and positioning.
  • Spindle 22 is supported at each end by trusses 28 on the upper frame 12.
  • the carriage 10 includes a spool positioning system 30 that includes disk 32 and lateral adjustment bracket 34.
  • the spool positioning system 30 controls the lateral position of the spool of prepreg material on the carriage throughout the prepreg dispensing operation.
  • Disk 32 is fixed to spindle 22.
  • the disk 32 is positioned between the arms of a U-shaped bracket 34.
  • a pad 36 coupled to each arm of the bracket 36 contacts the disk 32.
  • small lateral (i.e., perpendicular to the direction of tape application) adjustments in the alignment of the prepreg tape can be made by laterally moving the bracket 34 during tape dispensing as necessary.
  • the carriage 10 includes a tensioning system 38 for maintaining a suitable level of tension on the prepreg material during dispensing operation.
  • a friction adjuster 40 applies pressure to the disk 32 and pads 36 within the bracket 34 to establish a baseline resistance to rotation of the prepreg roll during the dispensing operation.
  • This adjuster 40 can be either manually operated or automatically operated based on feedback from tension monitoring sensors (not shown).
  • the tensioning system 38 includes a spring-loaded arm 42 that provides a measurement of the tension on the prepreg tape.
  • the force of the spring 44 on the spring-loaded arm 42 also compensates for minor fluctuations in force that result from the propulsion of the prepreg dispensing carriage 10 and from the diametric change of the prepreg material as it is dispensed from the spool.
  • the tensioning system may further include sensors for tension monitoring and adjustment.
  • Tension roller 47 attached to lateral bar 46 positions the prepreg tape near the surface of the molding tool in preparation for the compaction step.
  • the compaction assembly 18 acts to press down the prepreg material as it is dispensed onto the surface of the molding tool.
  • the compaction assembly applies compaction pressure regardless of the twist and curvature of the molding tool surface.
  • a compaction roller 48 is made up of a plurality of thin, heavy contiguous disks 50 on a lateral axle 52 with the flat faces of the disks pressed together.
  • the disks 50 have a central bore diameter that is larger than the diameter of the axle 52.
  • the disks 50 have polished faces and/or friction reducing media on the faces of the disks to enable independent movement of each disk.
  • the heavy disks 50 are able to move vertically, so that the edge of each disk contacts the prepreg material to provide compaction.
  • the compaction assembly 18 Adjacent the last disk at each end are retention members 54 on the axle 52 to maintain the lateral position of the disks 50 and limit their motion to rotation about the axle and translation perpendicular to the axle 52. Swing away arm 56 of the compaction assembly 18 is pivotably mounted on the upper frame 12 at pivot point 58. The rotational movement of the compaction assembly 18 enables the operator to lift the compaction assembly off of the prepreg tape when the compaction assembly is not in use.
  • the compaction assembly 18 may optionally include other features, including flexible-urethane or pneumatic shaped rollers, and spring or pneumatic loaded "fingers'Varms (not shown).
  • the prepreg material 82 is unwound from the spool 80, it passes over redirect roller 43 and is then positioned near the surface of the molding tool by tension roller 47.
  • the carriage 10 travels across the surface of the molding tool in the direction indicated by the arrow.
  • the compaction assembly 18 is lowered so that compaction roller 48 contacts the prepreg tape 82 and applies compaction pressure to compress the prepreg tape 82 to the surface of the molding tool 60.
  • the carriage 10 may be moved over the surface
  • the carriage 10 may be self-propelled using, for example, an electric motor (not shown). In one embodiment, the carriage 10 is guided by a rail 62 positioned along the surface of the molding tool 60.
  • the components of the tracking system 20 of the carriage 10 are integrated into the carriage 10 and are coordinated with the configuration of the molding tool 60 to assure the proper placement of the prepreg tape.
  • the coordination focuses on a specific feature of the final composite structure.
  • the point where the centerline of a wind blade spar cap contacts the surface of the molding tool 60 may be used as a "key characteristic".
  • Tracking system 20 maintains precise position of the prepreg dispensing carriage relative to the key characteristic.
  • Components of the tracking system 20 may be embedded in the molding tool surface 64 or in a separate guide rail 62 positioned on the edges of planar portions 68 of the molding tool at either side of a central concave portion 66 of the molding tool 60 as shown in FIGS. 5-7.
  • the tracking system 20 includes at least one pair of guide rollers 72 mounted to the end of at least one of the legs 74 of the base frame 14 of the carriage and proximate to wheel 70.
  • the pair of guide rollers 72 are space apart so that they engage both sides of rail 62 and traverse along the axis of the rail 62.
  • a second pair of guide rollers 72 may be mounted to a second leg 74 on the same side of the base frame proximate to the second wheel 70.
  • the guide rollers 72 are coordinated with the molding tool to provide definitive position of the carriage 10; provide proper twist of the carriage 10 to mirror that of the molding tool 60; and maintain contact of the carriage 10 to the molding tool 60 along the entire length of the molding tool. Tracking guide rollers 72 also help to eliminate pull-off of the carriage resulting from forces needed to propel the carriage along the molding tool.
  • the one or more rails are positioned under the molding tool, rather than on the surface of the molding tool.
  • a separate rail is not used to guide the carriage.
  • the molding tool surface itself incorporates key features that are tracked by the carriage so as to assure the proper placement of the prepreg material.
  • the compaction roller 48 exerts a compressive force to the prepreg tape by contacting the top surface of the structural composite being laminated as the tape is deposited on the molding tool.
  • the compaction roller 48 made up of a plurality of thin heavy, contiguous disks 50, is able to conform to the contours of the surface of the molding tool 64, and in particular, is conformable to the concave portion 66 of the molding tool so as to reduce the tendency of the tape to wrinkle when applied to the concave (or convex) portions of the molding tool surface.
  • the prepreg tape can be applied to molding tool surfaces having areas of varying degrees of concave curvature, areas having varying degrees of convex curvature and areas that are flat.
  • the prepreg tape any also be applied along a non-linear path on the molding tool surface.
  • the upper frame 12 is rotatably secured to base frame 14 by turntable 76, which enables rotating the prepreg material by 180 degrees without removing the dispensing carriage 10 from the molding tool 60.
  • the turntable 76 allows the prepreg material to pass through the center of the apparatus 10 during the dispensing operation.
  • the locking member 78 when engaged, prevents rotational movement of the upper frame 12 relative to the base frame 14, and establishes the proper location of the prepreg spool for each direction of dispensing on the molding tool 60.
  • the apparatus of the present invention may further include means for guiding the prepreg lay down to assure controlled fiber alignment.
  • the operation of the carriage assembly 10 may be controlled by a controller (not shown).
  • the carriage may be connected to a controller that is configured to control the placement of the prepreg tape, the tension on the tape, the direction in which the prepreg tape is applied to the surface of the molding tool and the speed at which the prepreg tape is laid down.
  • the carriage assembly 10 may apply the prepreg material tape starting from either end of the molding tool 60 and may start and stop according to predetermined ply locations.
  • a cutter may be used to automatically cut the ply.
  • the carriage assembly 10 may include a laser guide (not shown) for determining the ply locations.
  • the carriage assembly may be removably coupled to a spool loading station.
  • an apparatus that includes a slitter and accumulator, the apparatus capable of laying down strips of prepreg material formed from a wide prepreg tape product for a structure having in- plane curvature, while significantly reducing the effects of wrinkling on the inner radius.
  • the initial width of the prepreg tape product may be in the range of about 12 inches (30.5 cm) to about 60 inches (152.4 cm).
  • the tapes When building up a composite structure from prepreg tapes, the tapes are usually laid down in straight line directions. Because the tape is being unrolled from a single spool, the fibers cannot stretch in the lay-down process and cannot slide relative to one another. As a result, these prepreg tapes cannot be laid down in an in-plane curvature geometry without creating wrinkling or puckering on the inner radius.
  • a prepreg tape 200 dispensed using conventional apparatus in a linear direction has a plurality of aligned reinforcing fibers 202 that are pre-impregnated with a polymer.
  • the tape 200 When the tape 200 is applied to a flat, linear surface, the tape lies smoothly without wrinkling or puckering.
  • FIG. 15B illustrates a prepreg tape 200 dispensed in a non-linear, curved direction using conventional apparatus. The tape 200 lies smoothly along the outer edge 204 of the curved surface. However, along the inner edge 206, wrinkles 208 are formed.
  • FIG. 16 is a photograph of a 7 inch (17.8 cm) wide strip of prepreg laid down to an in-plane radius of curvature of 130 feet (39.6 m) using a conventional apparatus.
  • the wrinkling and puckering 208 on the inner radius 206 can be clearly seen. This wrinkling creates a loss of orientation of fiber direction and results in loss of composite mechanical properties in this region. Carbon fiber composites are particularly sensitive to loss of compression strength due to such loss of fiber orientation.
  • FIGS. 8-10 another exemplary embodiment of the prepreg tape dispensing apparatus of the present invention is illustrated.
  • the apparatus comprises a movable carriage 10 that includes a spool holding assembly 16 for demountably holding a spool 80 of a continuous web of prepreg tape material 82 having a wide width.
  • this embodiment of the carriage 10 includes an upper frame 12 rotatably mounted to a base frame 14.
  • Mounted on the upper frame 12 are a prepreg spool holding assembly 16 and a compaction assembly 18.
  • the base frame 14 includes a tracking system 20 to precisely place the prepreg material on the surface of the molding tool.
  • the carriage assembly 10 includes turntable 76 which enables upper frame 12 to rotate relative to base frame 14, such that application of the prepreg tape material on the molding tool 60 may be carried out in the forward direction and in the reverse direction.
  • the slitter 90 may include, for example, a plurality of stationary knives 92 or rotary knives.
  • the number of strips and the width of the individual strips 84 depend on the degree of non-linearity of the surface of the molding tool 60 to which the strips 84 are applied.
  • the strips 84 may be uniform in width or may have different widths to accommodate the non-linear path of the molding tool 60. While the description of the apparatus herein refers to a molding tool, it is to be understood that the prepreg material may be applied to the surface of a mold, mandrel, or any other surface used to form the composite structure in the prepreg dispensing operation.
  • the strips 84 are slit during manufacture of the wide prepreg web prior to being wound on a single spool.
  • the spool 80 of pre-slit strips is then mounted on the spool holding assembly 16.
  • the carriage 10 includes a mechanism for taking up the difference in length of the individual strips 84 resulting from the non-linear path of the molding tool 60.
  • an accumulator 94 is used.
  • Accumulator 94 includes a plurality of rollers 96, each strip of prepreg 84 having an associated roller that is independently extendable and retractable as needed to manage the excess length of the individual strip resulting from the non-linear path on the molding tool 60.
  • the accumulator rollers 96 maintain tension in the individual strips 84 so that the individual strips 84 are smoothly applied to the molding tool 60.
  • Extension and retraction of the rollers 96 of the accumulator 94 may be effected by a plurality of actuators 98 coupled to the rollers 96.
  • the actuators 98 include air cylinders.
  • the carriage 10 includes a tensioning system 38 that includes a brake disk 32 fixed to spindle 22, and pneumatically actuated brake pads 100 that apply friction to the disk 32 under programmed control.
  • the prepreg material 82 is unwound from the spool 80, it is advanced to a slitter 90 where it is slit into a plurality of strips 84 of prepreg material.
  • the prepreg strips 84 travel over the rollers 96 of the accumulator 94, the path each strip independently controlled to manage any excess length of the individual strip resulting from the non-linear path on the molding tool 60 to which the strip is applied. From the accumulator rollers 96, the strips proceed to guide rollers 102 which position the strips near the surface of the molding tool.
  • the compaction roller 48 contacts the prepreg strips 84 and applies compaction pressure to compress the prepreg strips 84 to the surface of the molding tool 60.
  • the surface of the molding surface 60 may include concave and/or convex areas having varying degrees of curvature, and/or flat areas.
  • the path of the individual prepreg strips 84 on the surface of the molding tool may be nonlinear or curved, the apparatus 10 is able to lay down the strips with little or no wrinkling of the prepreg layers and/or gaps between the strips on the mold.
  • FIGS. 12-14 illustrate the steps involved in the positioning the tape on the molding tool.
  • the tape 82 Before being slit into strips 84, the tape 82 is guided by the threading guide 104 along the tape path as shown in FIG. 12, with the slitter 90 inactivated.
  • the tape 82 is clamped or held to the surface of the mold tool 60.
  • the slitter 90 is then activated and the carriage 10 begins to move forward (in the direction indicated by the arrow), pulling the tape 82 until the slit portion of the tape (i.e., the strips 84) have extended past the compaction roller 48.
  • the tape 84 is then cut laterally and the carriage 10 advances out of the way so the tape just laid down can be pulled up and discarded.
  • the carriage 10 then moves to the programmed start position for the next layer to be applied, and the compaction roller 48 is lowered to begin adhering the prepreg strips 84 to the molding tool surface 64. From this point, the prepreg strips 84 are aligned by the crowned accumulator rollers 96 and the crowned guide roller 102. As the carriage 10 transitions from straight portions of the molding surface 64 to swept portions, or from one radius of sweep to another, the cross carriage 106 is shifted laterally by the cross carriage drive motor 104 to keep the center of the tape aligned with the center of the molding surface. In this embodiment, the amount of shift is previously input as offset data points into a table in the controller 1 12.
  • This same cross carriage 106 is used to move the carriage an additional or lesser distance as needed to track the tape 82 coming off the spool 80, as detected by the web edge sensor 1 10. This is done to provide a degree of compensation for tape not evenly wound on the spool 80, or tape 82 that has shifted on the spool 80 during transport.
  • the operation of the carriage assembly may be controlled by a controller 1 12.
  • the carriage 10 may be connected to a controller 1 12 that is configured to control the placement of the prepreg tape 82 or strips 84, the tension on the tape or strips, the direction in which the prepreg tape or strips are applied to the surface of the molding tool 60 and the speed at which the prepreg tape or strips are laid down.
  • the carriage assembly 10 may apply the prepreg material tape 82 or strips 84 starting from either end of the molding tool 60 and may start and stop according to predetermined tape or strip locations.
  • a cutter such as an ultrasonic knife (not shown) may be used to automatically cut the tape or strips.
  • the carriage assembly may include a laser guide for determining the tape or strip ply locations.
  • the prepreg tape material 82 on the spool 80 may have a liner or backing layer adhered to the prepreg tape 82.
  • the liner or backing layer of the prepreg material is removed from the underside of prepreg web prior to laying down the tape 82 or individual strips 84 of prepreg material, and is taken up on liner take-up roll.
  • the prepreg material web 82 includes a liner on the upper surface of the web that is removed prior to laying down the web.
  • the carriage assembly may further include means for detecting incomplete removal of the liner or backing from the prepreg material web.
  • the carriage assembly 10 may be removably coupled to a spool loading station.
  • a four wheeled cart was constructed to hold a spool of prepreg material having an outside diameter of up to 32 inches (81 .3 cm) and an inside diameter of 12 inches (30.5 cm), and having a length of approximately 1800 feet (549 m).
  • a 600 miNinneter wide web of prepreg was slit into twelve strips of 2 in. (50.8mm) in width with stationary knives mounted on the cart.
  • the apparatus and process of the present invention is particularly useful for the construction of wind turbine components.
  • the apparatus and process can also be used for, for example, in the construction of structural and aerodynamic components for airplanes, helicopters, automobile bodies, rail cars, marine crafts and the like.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

L'invention concerne un appareil pour appliquer un ruban imprégné de résine sur la surface d'un outil de moulage (60), l'appareil comprenant : un cadre supérieur (12) monté de manière rotative sur un cadre de base (14), le cadre supérieur présentant, un ensemble de support de bobine (16) avec lequel il peut tourner pour supporter une bobine de ruban imprégné de résine enroulée sur celui-ci, un ensemble de compression du ruban (18) comprenant un rouleau compresseur (48) configuré pour se conformer à la surface de l'outil de moulage pour compresser le ruban imprégné de résine sur la surface de l'outil de moulage, et un système de tension du ruban (38) pour exercer une tension sur le ruban imprégné de résine. Le cadre de base comprend un système de suivi (20) pour suivre la surface de l'outil de moulage, le cadre de base étant mobile selon un mouvement alternatif par rapport à la surface de l'outil de moulage.
EP11749054.0A 2010-08-17 2011-08-17 Appareil de distribution d'un ruban composite Withdrawn EP2605899A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US37458010P 2010-08-17 2010-08-17
US201161430427P 2011-01-06 2011-01-06
PCT/US2011/048051 WO2012024377A1 (fr) 2010-08-17 2011-08-17 Appareil de distribution d'un ruban composite

Publications (1)

Publication Number Publication Date
EP2605899A1 true EP2605899A1 (fr) 2013-06-26

Family

ID=44513199

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11749054.0A Withdrawn EP2605899A1 (fr) 2010-08-17 2011-08-17 Appareil de distribution d'un ruban composite

Country Status (7)

Country Link
EP (1) EP2605899A1 (fr)
KR (1) KR20130138747A (fr)
CN (1) CN103068559A (fr)
BR (1) BR112013003473A2 (fr)
CA (1) CA2808293A1 (fr)
MX (1) MX2013001588A (fr)
WO (1) WO2012024377A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MX2015001369A (es) * 2012-08-06 2015-05-11 Zoltek Companies Inc Aparato para dispensacion de cinta compuesta.
US10875287B2 (en) 2012-09-18 2020-12-29 Vestas Wind Systems A/S Wind turbine blades
DE102012219224B3 (de) 2012-10-22 2014-03-27 Repower Systems Se System und Verfahren zum Herstellen eines Rotorblattgurtes
DE102015007801A1 (de) 2015-06-19 2016-12-22 Senvion Gmbh Verfahren zur Herstellung eines Bauteils eines Rotorblattes einer Windenergieanlage
EP3597412B1 (fr) * 2017-03-17 2022-10-05 Subaru Corporation Dispositif de façonnage pour matériau fibreux et procédé de façonnage pour matériau fibreux
US10391723B2 (en) * 2017-08-31 2019-08-27 The Boeing Company Rotary compaction tool
FR3071187B1 (fr) * 2017-09-19 2021-02-12 Nimitech Innovation Systeme autonome d'execution de taches sur une surface et procede de realisation de piece utilisant un tel systeme
KR102363931B1 (ko) * 2020-11-27 2022-02-16 (주)휴먼컴퍼지트 대형 풍력 복합재 블레이드의 스파캡 소재 자동 적층 시스템
CN113561544B (zh) * 2021-09-26 2021-12-10 南通骏标自密封安全轮胎科技有限公司 自密封安全轮胎胶片滚压式覆胶机及其轮胎覆胶方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3810805A (en) * 1972-04-14 1974-05-14 Goldsworthy Eng Inc Geodesic path length compensator for composite-tape placement head
IL96489A0 (en) * 1989-12-06 1991-08-16 Du Pont Method for laying down tapes
US5431749A (en) * 1993-09-30 1995-07-11 The Ingersoll Milling Machine Company Tape laying head with curved tape laying capability and improved adaptive steering
ES2112088B1 (es) * 1993-11-30 1998-11-01 Torres Martinez M Cabezal de encintado para la aplicacion de cinta de fibra de carbono o similar.
ES2144900B1 (es) * 1996-07-25 2001-02-01 Torres Martinez M Cabezal para la aplicacion de tiras de composite.
US6390169B1 (en) * 2000-02-23 2002-05-21 The Boeing Company Conformable compaction apparatus for use with a fiber placement machine
EP1731291B1 (fr) * 2005-06-08 2008-09-24 Saab Ab Appareil de positionnement automatique de bandes et procédé utilisant cet appareil
US7810539B2 (en) * 2005-08-25 2010-10-12 Ingersoll Machine Tools, Inc. Compaction roller for a fiber placement machine
US8042594B2 (en) * 2006-06-28 2011-10-25 Alliant Techsystems Inc. Compaction device for fiber placement using interdependent segment travel
ES2331825B1 (es) * 2007-10-08 2010-07-22 Manuel Torres Martinez Perfeccionamientos en cabezales de aplicacion de cintas de fibra.

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2012024377A1 *

Also Published As

Publication number Publication date
BR112013003473A2 (pt) 2019-09-24
WO2012024377A1 (fr) 2012-02-23
CA2808293A1 (fr) 2012-02-23
CN103068559A (zh) 2013-04-24
KR20130138747A (ko) 2013-12-19
MX2013001588A (es) 2013-04-29

Similar Documents

Publication Publication Date Title
EP2605899A1 (fr) Appareil de distribution d'un ruban composite
US8641847B2 (en) Composite lamination using array of parallel material dispensing heads
US10987882B2 (en) Material preparation device and related methods
CN104812553B (zh) 将薄膜材料施加到伸长构件的方法和装置
US8578995B2 (en) Parallel configuration composite material fabricator and related methods
US4588466A (en) Tape laying method and apparatus
US8048253B2 (en) System and method for the rapid, automated creation of advanced composite tailored blanks
US11565485B2 (en) System, method, and apparatus for use in ply compaction in forming a composite structure
CA2880919A1 (fr) Appareil de distribution de bande composite
US11865825B2 (en) System, method, and apparatus for use in ply compaction in forming a composite structure
US20130126095A1 (en) Apparatus for composite tape dispensing
US20210107182A1 (en) System, method, and apparatus for use in forming a composite structure
JP7224348B2 (ja) 複合構造、成形機器ならびに関連したシステムおよび方法
US11660831B2 (en) Lamination head having bi-directional capability
CN118810201A (zh) 多机器高速复合材料铺设

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20130215

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN

18W Application withdrawn

Effective date: 20150513