US20050238892A1 - Backing film and method for ply materials - Google Patents

Backing film and method for ply materials Download PDF

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Publication number
US20050238892A1
US20050238892A1 US10/829,270 US82927004A US2005238892A1 US 20050238892 A1 US20050238892 A1 US 20050238892A1 US 82927004 A US82927004 A US 82927004A US 2005238892 A1 US2005238892 A1 US 2005238892A1
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United States
Prior art keywords
ply material
ply
backing film
backing
backed
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.)
Abandoned
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US10/829,270
Inventor
Richard Evans
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Boeing Co
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Boeing Co
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Publication date
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Priority to US10/829,270 priority Critical patent/US20050238892A1/en
Assigned to BOEING COMPANY, THE reassignment BOEING COMPANY, THE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: EVANS, RICHARD B.
Publication of US20050238892A1 publication Critical patent/US20050238892A1/en
Priority to US11/528,353 priority patent/US8206540B2/en
Priority to US13/481,705 priority patent/US20120237776A1/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/36Layered products comprising a layer of synthetic resin comprising polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/09Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0004Cutting, tearing or severing, e.g. bursting; Cutter details
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/06Interconnection of layers permitting easy separation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B32B9/007Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/045Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B2037/148Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby layers material is selected in order to facilitate recycling of the laminate
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062Prior to assembly
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/12Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/17Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1702For plural parts or plural areas of single part
    • Y10T156/1705Lamina transferred to base from adhered flexible web or sheet type carrier
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/25Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/26Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/269Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension including synthetic resin or polymer layer or component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31511Of epoxy ether
    • Y10T428/31529Next to metal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31652Of asbestos
    • Y10T428/31663As siloxane, silicone or silane
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31678Of metal
    • Y10T428/31681Next to polyester, polyamide or polyimide [e.g., alkyd, glue, or nylon, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31786Of polyester [e.g., alkyd, etc.]

Definitions

  • the present invention generally relates to backing materials for sheet and roll stock. More particularly, the present invention pertains to an improved backing material for pre-impregnated ply material.
  • Composite structures are typically constructed from multiple layers or plies. These plies may include a variety of materials such as carbon fiber, various other fibers, metal foils, and the like.
  • the plies may be pre-impregnated with a resin and are often dispensed from a roll or spool.
  • the ply material is referred to as “tape” and typically includes a paper backing film.
  • This backing film generally prevents pre-impregnated ply material (prepreg) from adhering to itself and aids in handling the ply as the ply is applied to the tool and the layup.
  • prepreg pre-impregnated ply material
  • the ply material is generally cut to match the profile of the layup while the backing film is left intact. In this manner, the intact backing film is utilized to guide the severed ply on to the layup.
  • the backing film is removed prior to placement of any subsequent ply.
  • a disadvantage associated with conventional backing film material is that the backing film rips or tears.
  • cuts in the backing film introduced during the ply cutting procedure, often serve as a starting point for a tear.
  • torn backing film may remain on the ply, may foul the ply placement head, and/or may lead to breakage of the backing film.
  • Another disadvantage associated with conventional backing film is that it is usually a relatively thick calendered claycote type paper.
  • the weight and thickness of this paper reduce the yardage of ply material that may be placed on a spool of a given diameter. Reducing the thickness of the conventional backing film in an effort to place more backed ply material on a spool, however, increases the tendency of the backing film to tear.
  • An embodiment of the present invention relates to a layered material.
  • the layered material includes a ply material and a backing film disposed upon the ply material.
  • the backing film includes a polyester film.
  • the apparatus includes a means for disposing a polyester film upon a ply material and a means for generating a roll of the backed ply material by wrapping the backed ply material about a spool.
  • Yet another embodiment of the present invention relates to an apparatus for generating a composite layup.
  • the apparatus includes a means for tacking a ply material having a polyester backing film to a tool.
  • the apparatus further includes a means for disposing the ply material upon the tool along a path and a means for removing the polyester backing film.
  • Yet another embodiment of the present invention relates to a method of generating a composite layup.
  • a ply material having a polyester backing film is tacked to a tool, the ply material is disposed upon the tool along a path, and the polyester backing film is removed.
  • FIG. 1 is perspective view of ply material according to an embodiment of the invention.
  • FIG. 2 is a simplified side view of a tape laying head suitable for use with the ply material according to FIG. 1 .
  • FIG. 3 is a perspective view of a contour tape lamination machine suitable for use with the ply material according to FIG. 1 .
  • FIG. 4 is a flow diagram of a method of placing plies to produce a composite structure or product according to an embodiment of the invention.
  • FIG. 5 is a flow diagram of a method to generate a backed ply material according to FIG. 1 .
  • a backed ply material 10 includes a ply material 12 and a backing 14 .
  • the ply material 12 may include any suitable sheet stock. Examples of suitable sheet stocks include: woven fiber fabric; oriented strand tape; metal foil such as aluminum alloy and titanium foil; composite materials such as titanium graphite composites; and the like.
  • the ply material 12 is a graphite fiber tape pre-impregnated with an epoxy resin (pre-preg).
  • the ply material 12 is an epoxy resin coated titanium foil.
  • the backing 12 is thin.
  • the thickness of this backing 14 is varied depending upon the particular application. For example, according to various embodiments of the invention, for typical composite layup applications, the thickness of the backing 14 is from about 0.001 inches (1 mil) to about 0.004 inches (4 mil). More preferably, the thickness of the backing 14 is about 1 mil to about 2 mil. However, in other embodiments, the thickness of the backing 14 is less than 1 mil.
  • the ply material 12 be approximately 1 mil thick or less and the backing 14 be approximately 0.1 mil thick or less.
  • the thickness of the backing 14 is greater than 4 mil.
  • the backing 14 may be 10 or more mil thick.
  • the backing 14 is typically removed.
  • the backing 14 is tear-resistant.
  • the backing 14 may include a polymeric or otherwise tough resilient material.
  • the backing 14 includes a suitable polyester film. Suitable polyester films include at least polyethylene terephthalate (PET) and heat stabilized PET. In this regard, when applying heat during layup operations, it may be advantageous to utilize a heat stabilized PET.
  • the backing 14 optionally includes a suitable release agent. Suitable release agents include at least silicone release agents applied by Tribex Corp. of Rocklin Calif., USA.
  • the backing 14 is substantially transparent to facilitate inspection of seams between abutting plies. For example, a 2 mil film of PET is essentially transparent.
  • FIG. 2 is a simplified side view of a tape laying head 18 suitable for use with the backed ply material 10 according to FIG. 1 .
  • the tape laying head 18 includes a supply spool 20 , take-up reel 22 , a shoe or compaction roller 24 , cutting assembly 26 , heater assembly 28 , material feeder 30 , and guide chute 32 .
  • the tape laying head 18 dispenses the ply material 12 upon a tool 34 as it moves in direction A relative to the tool 34 . More particularly, the supply spool 20 and the take-up reel 22 rotate in the respectively indicated directions to cause backed ply material 10 to advance through the tape laying head 18 as indicated.
  • the cutting assembly 26 may employ any known cutting device such as various bladed devices, abrasive cutters, high pressure jets, lasers, and the like.
  • the cutting assembly 26 includes an ultrasonic knife that is caused to vibrate by an ultrasonic transducer and controlled to rotate by the action of a motor.
  • the ultrasonic knife is further controlled to traverse the full width of the backed ply material 10 or any portion thereof by the action of a motor configured to rotate a jackscrew.
  • the cutting assembly 26 may employ more than one cutting device.
  • the cutting assembly 26 of an embodiment of the invention includes two cutting devices controlled to perform cutting operations in a substantially simultaneous manner.
  • FIG. 4 illustrates steps involved in a method 44 of placing plies to produce a composite structure or product.
  • a composite product Prior to the initiation of the method 44 , a composite product is designed and a series of computer readable instructions specifying attributes of the composite product is generated. These instructions are utilized to control the operations of the CTLM 38 and construct a form such as the tool 34 . This form is further positioned within the operational area of the CTLM 38 .
  • the method 44 is initiated by turning on the various components of the CTLM 38 described herein above and executing the computer readable instructions.
  • the backed ply material 10 is advanced to an initial point.
  • the take up reel 22 and/or the supply spool 20 may be controlled to advance the backing 14 through the tape laying head 18 until an end of the ply material 12 is positioned between the compaction roller 24 and the tool 34 .
  • the rollers of the material feeder 30 may engage the backed ply material 10 and advance the ply through the tape laying head 18 until the backed ply material 10 is positioned to be applied to the tool 34 , referred to as being tacked.
  • a sensor and/or operator may sense the position of the backed ply material 10 .
  • the location on the tool 34 is determined based upon the series of computer readable instruction and/or the location of a previously positioned ply material 12 .
  • the end of the ply material 12 is, optionally, cut based upon the series of computer readable instruction, the orientation of a previously positioned ply material 12 , and/or the location of a previously positioned ply material 12 .
  • cutting of the ply material 12 may be performed at a controlled depth of cut so as to substantially sever the ply material 12 while leaving the backing 14 substantially uncut.
  • the backed ply material 10 is tacked to the substrate.
  • the backed ply material 10 is tacked by positioning the tape laying head 18 with the CTLM 38 such that the compaction roller 24 or a shoe is controlled to press the backed ply material 10 on to the substrate with sufficient force so as to cause the backed ply material 10 to adhere to the substrate.
  • the backed ply material 10 is dispensed along a path across the tool 34 .
  • this path is typically calculated to coincide with a “natural path” based upon any contours in the tool 34 .
  • the compaction roller 24 is caused to exert sufficient pressure so as to adhere the ply material 12 to the tool 34 .
  • the backed ply material 10 is drawn out of the tape laying head 18 and consolidated on to the tool 34 .
  • composite layups typically include multiple layers of ply material.
  • backed ply material 10 is dispensed upon previously applied ply material.
  • the placement of the backed ply material 10 on the tool 34 is evaluated.
  • a sensor or an operator may sense the relative position of the backed ply material 10 and a previously positioned backed ply material 10 and determine if the distance between these plies is within a predetermined tolerance. If the distance between these plies is not within the predetermined tolerance, an error may be generated at step 56 . If the distance between these plies is within the predetermined tolerance, it is determined if the supply is sufficient at step 58 .
  • the backing 14 is removed from the backed ply material 10 following placement evaluation.
  • the backing 14 need not be removed prior to step 58 , but rather, the backing 14 may be removed at essentially any time prior to placement of a subsequent ply upon the backed ply material 10 .
  • the backing 14 is recyclable. That is, the backing 14 may be collected and submitted to a recycling facility where the PET constituent of the backing 14 may be processed to generate products.
  • the term, “recycling” is defined as the act of collecting the backing 14 for submission to a recycling facility and/or the reprocessing of the backing 14 .
  • step 58 it is determined whether the supply of ply material is sufficient. For example, if it determined that the supply spool 20 contains ply material then, it is determined that sufficient ply material remains. If it is determined that then is an insufficient amount of remaining ply material, the supply spool 20 is replaced at step 60 . If it is determined that a sufficient amount of ply material remains then, it is determined if the end of the path has been reached at step 62 .
  • the supply spool 20 is replaced.
  • a spent supply spool 20 is removed from the tape laying head 18 and a substantially full supply spool 20 may be disposed within the tape laying head 18 .
  • a splice is optionally formed at step 64 .
  • the ply material 12 for the uncompleted path may be removed or, optionally, spliced to the ply material 12 from the new supply spool 20 .
  • the particular steps performed is dependent upon the ply material utilized and the product being laid up. However, in general, the trailing edge of the uncompleted ply and the starting edge of the new ply material are cut to match. These cut edges are abutted and quality control procedure procedures are performed.
  • An advantage of embodiments of the invention over conventional backed ply material is that, due to the relative thinness of the backing 12 , a relatively greater amount of ply material fits on the spool and thus, fewer spool change and tape splicing operations need be performed.
  • step 62 it is determined if the end of the path has been reached. If, based on the series of computer readable instruction, it is determined the tape laying head 18 has not advanced to the end of the path, additional backed ply material 10 is dispensed at step 52 . If, it is determined the tape laying head 18 has advanced to the end of the path, the backed ply material 10 is cut at step 66 .
  • the end of the ply material 12 may be cut based upon the series of computer readable instruction, the orientation of a previously positioned ply material 12 , and/or the location of a previously positioned ply material 12 .
  • step 68 it is determined if the placement of the ply material 12 on the tool 34 has been completed. For example, if all of the computer readable instructions have been completed, it may be determined that the placement of plies for the composite product has been completed and the CTLM 38 may idle until another series of computer readable instructions is initiated. If is determined the placement of plies 12 for the composite product is not completed, an additional ply material 12 placement may proceed at step 48 .
  • the composite product may be cured in any suitable manner.
  • thermoset resins are generally utilized to pre-impregnate ply material. These thermoset resins are typically cured by being held at an elevated temperature for a predetermined amount of time. Times and temperatures may be selected depending on the resin used, the size and thickness of the composite product, and the like.
  • the backed ply material 10 can also be used in other industries that construct composite product. These industries include, but are not limited to, automobile, marine, spacecraft, building, and consumer products.
  • FIG. 5 is a flow diagram of steps performed in a method 70 to generate the backed ply material 10 according to FIG. 1 .
  • the method 70 is initiated in response to a press or other such device being turned on.
  • a variety of tasks may be performed prior to initiation of the method 70 . These tasks include, in no particular order: secure a supply of the ply material 12 within the press; secure a supply of the backing 14 within the press; mount an essentially empty spool downstream of the press; and the like.
  • step 74 sufficient force and/or heat are applied to the ply material 12 and the backing 14 so as to cause the ply material 12 and the backing 14 to adhere.
  • the backed ply material 12 is taken up by the spool.
  • the backed ply material 12 is cut, the essentially full spool is removed, and a substantially empty spool is optionally put in its place.

Abstract

A layered material includes a ply material and a backing film to support the ply material. The backing film includes a polyester film. The layered material is generated by disposing the backing film upon the ply material. A composite layup is generated by tacking the layered material to a tool, disposing the layered material upon the tool along a path, and removing the backing film.

Description

    FIELD OF THE INVENTION
  • The present invention generally relates to backing materials for sheet and roll stock. More particularly, the present invention pertains to an improved backing material for pre-impregnated ply material.
  • BACKGROUND OF THE INVENTION
  • Composite structures are typically constructed from multiple layers or plies. These plies may include a variety of materials such as carbon fiber, various other fibers, metal foils, and the like. In addition, the plies may be pre-impregnated with a resin and are often dispensed from a roll or spool. In roll form, the ply material is referred to as “tape” and typically includes a paper backing film. This backing film generally prevents pre-impregnated ply material (prepreg) from adhering to itself and aids in handling the ply as the ply is applied to the tool and the layup. In particular, at the beginning and end of each ply placement, the ply material is generally cut to match the profile of the layup while the backing film is left intact. In this manner, the intact backing film is utilized to guide the severed ply on to the layup. During the layup process, the backing film is removed prior to placement of any subsequent ply.
  • A disadvantage associated with conventional backing film material is that the backing film rips or tears. In particular, cuts in the backing film, introduced during the ply cutting procedure, often serve as a starting point for a tear. As the backing film is removed, torn backing film may remain on the ply, may foul the ply placement head, and/or may lead to breakage of the backing film.
  • Another disadvantage associated with conventional backing film is that it is usually a relatively thick calendered claycote type paper. The weight and thickness of this paper reduce the yardage of ply material that may be placed on a spool of a given diameter. Reducing the thickness of the conventional backing film in an effort to place more backed ply material on a spool, however, increases the tendency of the backing film to tear.
  • Yet another disadvantage associated with conventional backings films is the opaque nature of the paper. This opacity precludes visual inspection of the ply placement until the backing film is removed. Once the backing film is removed from the ply, the handling characteristics of the ply are negatively impacted so, it is difficult or impossible to adjust the ply placement.
  • Accordingly, it is desirable to provide a backing film for pre-impregnated ply material that is capable of overcoming the disadvantages described herein at least to some extent.
  • SUMMARY OF THE INVENTION
  • The foregoing needs are met, to a great extent, by the present invention, wherein in some embodiments an improved backing film for pre-impregnated ply material is provided.
  • An embodiment of the present invention relates to a layered material. The layered material includes a ply material and a backing film disposed upon the ply material. The backing film includes a polyester film.
  • Another embodiment of the present invention pertains to an apparatus for generating backed ply material. The apparatus includes a means for disposing a polyester film upon a ply material and a means for generating a roll of the backed ply material by wrapping the backed ply material about a spool.
  • Yet another embodiment of the present invention relates to an apparatus for generating a composite layup. The apparatus includes a means for tacking a ply material having a polyester backing film to a tool. The apparatus further includes a means for disposing the ply material upon the tool along a path and a means for removing the polyester backing film.
  • Yet another embodiment of the present invention pertains to a method of generating a backed ply material. In this method, a polyester film is disposed upon a ply material.
  • Yet another embodiment of the present invention relates to a method of generating a composite layup. In this method, a ply material having a polyester backing film is tacked to a tool, the ply material is disposed upon the tool along a path, and the polyester backing film is removed.
  • There has thus been outlined, rather broadly, certain embodiments of the invention in order that the detailed description thereof herein may be better understood, and in order that the present contribution to the art may be better appreciated. There are, of course, additional embodiments of the invention that will be described below and which will form the subject matter of the claims appended hereto.
  • In this respect, before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of construction and to the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of embodiments in addition to those described and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein, as well as the abstract, are for the purpose of description and should not be regarded as limiting.
  • As such, those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is perspective view of ply material according to an embodiment of the invention.
  • FIG. 2 is a simplified side view of a tape laying head suitable for use with the ply material according to FIG. 1.
  • FIG. 3 is a perspective view of a contour tape lamination machine suitable for use with the ply material according to FIG. 1.
  • FIG. 4 is a flow diagram of a method of placing plies to produce a composite structure or product according to an embodiment of the invention.
  • FIG. 5 is a flow diagram of a method to generate a backed ply material according to FIG. 1.
  • DETAILED DESCRIPTION
  • The present invention provides, in some embodiments, a backing material, a backed composite ply material, and a method of generating a backed ply material. An embodiment of the invention will now be described with reference to the drawing figures, in which like reference numerals refer to like parts throughout. As shown in FIG. 1, a backed ply material 10 includes a ply material 12 and a backing 14. In various embodiments of the invention, the ply material 12 may include any suitable sheet stock. Examples of suitable sheet stocks include: woven fiber fabric; oriented strand tape; metal foil such as aluminum alloy and titanium foil; composite materials such as titanium graphite composites; and the like. In a particular embodiment, the ply material 12 is a graphite fiber tape pre-impregnated with an epoxy resin (pre-preg). In another particular embodiment, the ply material 12 is an epoxy resin coated titanium foil.
  • In general, the backing 14 lends support to the ply material 12 and aids in handling the ply material 12. As described herein, the backed ply material 10 is typically rolled on to a spool in preparation for dispensing. For a given thickness of the ply material 12 rolled into a given diameter spool, the thickness of the backing 14 has an inversely proportional relationship with the length of ply material 12 that may be placed on the spool. That is, the thinner the backing 14, the more ply material 12 will fit onto the spool. Longer lengths of ply material 12 are generally preferred due to the decreased number of splices that must be prepared, reduced downtime as a result of the decreased number of splices, and reduced number of spool change operation to be performed. Thus, it is preferable that the backing 12 is thin. In addition, the thickness of this backing 14 is varied depending upon the particular application. For example, according to various embodiments of the invention, for typical composite layup applications, the thickness of the backing 14 is from about 0.001 inches (1 mil) to about 0.004 inches (4 mil). More preferably, the thickness of the backing 14 is about 1 mil to about 2 mil. However, in other embodiments, the thickness of the backing 14 is less than 1 mil. For example, when constructing relatively small and/or convoluted items such as, hand held or smaller devices, it may be advantageous that the ply material 12 be approximately 1 mil thick or less and the backing 14 be approximately 0.1 mil thick or less. In yet other embodiments, the thickness of the backing 14 is greater than 4 mil. For example, when constructing items with relatively thick (3 millimeters or more) or otherwise difficult to handle ply material 12, the backing 14 may be 10 or more mil thick.
  • During layup operations, the backing 14 is typically removed. To reduce down time, it is also preferable that the backing 14 is tear-resistant. For example, the backing 14 may include a polymeric or otherwise tough resilient material. According to an embodiment of the invention, the backing 14 includes a suitable polyester film. Suitable polyester films include at least polyethylene terephthalate (PET) and heat stabilized PET. In this regard, when applying heat during layup operations, it may be advantageous to utilize a heat stabilized PET. To further facilitate removal of the backing 14 from the ply material 12, the backing 14 optionally includes a suitable release agent. Suitable release agents include at least silicone release agents applied by Tribex Corp. of Rocklin Calif., USA. Optionally, the backing 14 is substantially transparent to facilitate inspection of seams between abutting plies. For example, a 2 mil film of PET is essentially transparent.
  • FIG. 2 is a simplified side view of a tape laying head 18 suitable for use with the backed ply material 10 according to FIG. 1. As shown in FIG. 2, the tape laying head 18 includes a supply spool 20, take-up reel 22, a shoe or compaction roller 24, cutting assembly 26, heater assembly 28, material feeder 30, and guide chute 32. The tape laying head 18 dispenses the ply material 12 upon a tool 34 as it moves in direction A relative to the tool 34. More particularly, the supply spool 20 and the take-up reel 22 rotate in the respectively indicated directions to cause backed ply material 10 to advance through the tape laying head 18 as indicated. The supply spool 20 and/or the take-up reel 22 are optionally controlled to rotate via the action of, for example, one or more servo axis motors. Following application of the ply material 12 upon the tool 34, the backing 14 is removed and collected by, for example, the take-up reel 22. However, the take-up reel 22 is optional and thus, the backing 14 may be removed in any suitable manner such as, for example, manually, a backing removal device, or the like. Depending upon the particular application, the placement of the ply material 12 may be inspected prior to removal of the backing 14. In this regard, it is an advantage of some embodiments of the invention that the backing 14 is substantially transparent and thus, the placement of the ply material 14 may be plainly visible through the backing 14.
  • The cutting assembly 26 may employ any known cutting device such as various bladed devices, abrasive cutters, high pressure jets, lasers, and the like. In a specific example, the cutting assembly 26 includes an ultrasonic knife that is caused to vibrate by an ultrasonic transducer and controlled to rotate by the action of a motor. The ultrasonic knife is further controlled to traverse the full width of the backed ply material 10 or any portion thereof by the action of a motor configured to rotate a jackscrew. Furthermore, the cutting assembly 26 may employ more than one cutting device. For example, the cutting assembly 26 of an embodiment of the invention includes two cutting devices controlled to perform cutting operations in a substantially simultaneous manner.
  • When utilizing specific materials and/or operating conditions in which heating of the material is advantageous, the heater assembly 28 is configured to impart thermal energy upon the backed ply material 10. In this regard, any known device operable to heat the backed ply material 10 in a suitable manner may be utilized by various embodiments of the invention. For example, the heater assembly 28 may include a diverter valve configured to control the flow of heated air directed onto the backed ply material 10. In addition, to the heater assembly 28, the tape laying head 18 may include various supplemental heaters such as, for example, a guide chute heater, a heater following the compactions roller 24, and the like.
  • FIG. 3 is a perspective view of a contour tape lamination machine (CTLM) 38 suitable for use with the backed ply material 10 according to FIG. 1. As shown in FIG. 3, the CTLM 38 is of a gantry-type and, as such, includes a gantry 40, the tape laying head 18, and the tool 34. The gantry 40 is configured to control the movement of the tape laying head 18 in relation to the tool 34 and the ply material 12 laid upon the tool 34. In an embodiment of the invention, the gantry 40 is configured to control ten axis of movement (five axis of the gantry and five axis of the tape laying head 18). However, it is to be understood that the specific number of axis may depend upon the particular operating condition and thus, the number of axis controlled is not critical to the invention.
  • FIG. 4 illustrates steps involved in a method 44 of placing plies to produce a composite structure or product. Prior to the initiation of the method 44, a composite product is designed and a series of computer readable instructions specifying attributes of the composite product is generated. These instructions are utilized to control the operations of the CTLM 38 and construct a form such as the tool 34. This form is further positioned within the operational area of the CTLM 38.
  • At step 46, the method 44 is initiated by turning on the various components of the CTLM 38 described herein above and executing the computer readable instructions.
  • At step 48, the backed ply material 10 is advanced to an initial point. For example, the take up reel 22 and/or the supply spool 20 may be controlled to advance the backing 14 through the tape laying head 18 until an end of the ply material 12 is positioned between the compaction roller 24 and the tool 34. In another example, the rollers of the material feeder 30 may engage the backed ply material 10 and advance the ply through the tape laying head 18 until the backed ply material 10 is positioned to be applied to the tool 34, referred to as being tacked. To ensure the backed ply material 10 has advanced a suitable amount, a sensor and/or operator may sense the position of the backed ply material 10. In addition, the location on the tool 34 is determined based upon the series of computer readable instruction and/or the location of a previously positioned ply material 12. Furthermore, prior to tacking the ply material 12 to the substrate at step 50, the end of the ply material 12 is, optionally, cut based upon the series of computer readable instruction, the orientation of a previously positioned ply material 12, and/or the location of a previously positioned ply material 12. In a particular example, cutting of the ply material 12 may be performed at a controlled depth of cut so as to substantially sever the ply material 12 while leaving the backing 14 substantially uncut.
  • At step 50, the backed ply material 10 is tacked to the substrate. In an embodiment of the invention, the backed ply material 10 is tacked by positioning the tape laying head 18 with the CTLM 38 such that the compaction roller 24 or a shoe is controlled to press the backed ply material 10 on to the substrate with sufficient force so as to cause the backed ply material 10 to adhere to the substrate.
  • At step 52, the backed ply material 10 is dispensed along a path across the tool 34. In order to minimize deformations in the backed ply material 10 (e.g., wrinkles), this path is typically calculated to coincide with a “natural path” based upon any contours in the tool 34. As the tape laying head 18 is controlled along the path across the tool 34, the compaction roller 24 is caused to exert sufficient pressure so as to adhere the ply material 12 to the tool 34. As the tape laying head 18 moves along the path, the backed ply material 10 is drawn out of the tape laying head 18 and consolidated on to the tool 34. In this regard, composite layups typically include multiple layers of ply material. Thus, in subsequent applications of the ply material 12, backed ply material 10 is dispensed upon previously applied ply material.
  • At step 54, the placement of the backed ply material 10 on the tool 34 is evaluated. For example, a sensor or an operator may sense the relative position of the backed ply material 10 and a previously positioned backed ply material 10 and determine if the distance between these plies is within a predetermined tolerance. If the distance between these plies is not within the predetermined tolerance, an error may be generated at step 56. If the distance between these plies is within the predetermined tolerance, it is determined if the supply is sufficient at step 58. In addition, in some embodiments of the invention, the backing 14 is removed from the backed ply material 10 following placement evaluation. However, the backing 14 need not be removed prior to step 58, but rather, the backing 14 may be removed at essentially any time prior to placement of a subsequent ply upon the backed ply material 10. Furthermore, it is an advantage of embodiments of the invention that the backing 14 is recyclable. That is, the backing 14 may be collected and submitted to a recycling facility where the PET constituent of the backing 14 may be processed to generate products. For the purpose of this disclosure, the term, “recycling” is defined as the act of collecting the backing 14 for submission to a recycling facility and/or the reprocessing of the backing 14.
  • At step 58, it is determined whether the supply of ply material is sufficient. For example, if it determined that the supply spool 20 contains ply material then, it is determined that sufficient ply material remains. If it is determined that then is an insufficient amount of remaining ply material, the supply spool 20 is replaced at step 60. If it is determined that a sufficient amount of ply material remains then, it is determined if the end of the path has been reached at step 62.
  • At step 60 the supply spool 20 is replaced. For example, a spent supply spool 20 is removed from the tape laying head 18 and a substantially full supply spool 20 may be disposed within the tape laying head 18. Following replacement of the supply spool 20, a splice is optionally formed at step 64. For example, if the supply of ply material is exhausted during the placement of a ply, the ply material 12 for the uncompleted path may be removed or, optionally, spliced to the ply material 12 from the new supply spool 20. If the splice is performed, the particular steps performed is dependent upon the ply material utilized and the product being laid up. However, in general, the trailing edge of the uncompleted ply and the starting edge of the new ply material are cut to match. These cut edges are abutted and quality control procedure procedures are performed.
  • An advantage of embodiments of the invention over conventional backed ply material is that, due to the relative thinness of the backing 12, a relatively greater amount of ply material fits on the spool and thus, fewer spool change and tape splicing operations need be performed.
  • At step 62, it is determined if the end of the path has been reached. If, based on the series of computer readable instruction, it is determined the tape laying head 18 has not advanced to the end of the path, additional backed ply material 10 is dispensed at step 52. If, it is determined the tape laying head 18 has advanced to the end of the path, the backed ply material 10 is cut at step 66.
  • At step 66, the end of the ply material 12 may be cut based upon the series of computer readable instruction, the orientation of a previously positioned ply material 12, and/or the location of a previously positioned ply material 12.
  • At step 68, it is determined if the placement of the ply material 12 on the tool 34 has been completed. For example, if all of the computer readable instructions have been completed, it may be determined that the placement of plies for the composite product has been completed and the CTLM 38 may idle until another series of computer readable instructions is initiated. If is determined the placement of plies 12 for the composite product is not completed, an additional ply material 12 placement may proceed at step 48.
  • Following the method 44, the composite product may be cured in any suitable manner. In the aerospace industry, thermoset resins are generally utilized to pre-impregnate ply material. These thermoset resins are typically cured by being held at an elevated temperature for a predetermined amount of time. Times and temperatures may be selected depending on the resin used, the size and thickness of the composite product, and the like.
  • Although an example of the tape laying head 18 is shown utilizing the backed ply material 10 for composite products in the airline industry, the backed ply material 10 can also be used in other industries that construct composite product. These industries include, but are not limited to, automobile, marine, spacecraft, building, and consumer products.
  • FIG. 5 is a flow diagram of steps performed in a method 70 to generate the backed ply material 10 according to FIG. 1. As shown in FIG. 5, the method 70 is initiated in response to a press or other such device being turned on. Prior to initiation of the method 70 a variety of tasks may be performed. These tasks include, in no particular order: secure a supply of the ply material 12 within the press; secure a supply of the backing 14 within the press; mount an essentially empty spool downstream of the press; and the like.
  • At step 72 the ply material 12 and the backing 14 are introduced into the press.
  • At step 74 sufficient force and/or heat are applied to the ply material 12 and the backing 14 so as to cause the ply material 12 and the backing 14 to adhere.
  • At step 76 the backed ply material 12 is taken up by the spool. In addition, in response to a sufficient amount of backed ply material 12 being placed upon the spool, the backed ply material 12 is cut, the essentially full spool is removed, and a substantially empty spool is optionally put in its place.
  • The many features and advantages of the invention are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirit and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.

Claims (23)

1. A layered material comprising:
a ply material; and
a backing film disposed upon the ply material, the backing film comprising a polyester film.
2. The layered material according to claim 1, wherein the backing film further comprises:
a release coating to facilitate removal of the backing film from the composite ply material.
3. The layered material according to claim 2, wherein the release coating comprises silicone.
4. The layered material according to claim 1, wherein the backing film is about 0.001 to about 0.004 inches thick.
5. The layered material according to claim 4, wherein the backing film is about 0.001 to about 0.002 inches thick.
6. The layered material according to claim 1, wherein the backing film is substantially transparent.
7. The layered material according to claim 1, wherein the backing film comprises polyethylene terephthalate.
8. The layered material according to claim 1, wherein the backing film is heat stabilized.
9. The layered material according to claim 1, wherein the ply material comprises graphite fibers.
10. The layered material according to claim 1, wherein the ply material comprises a metal foil.
11. The layered material according to claim 10, wherein the ply material comprises a titanium foil.
12. The layered material according to claim 11, wherein the ply material comprises a titanium graphite composite.
13. The layered material according to claim 1, wherein the backing film is recyclable.
14. An apparatus for generating backed ply material, the apparatus comprising:
means for disposing a polyester film upon a ply material; and
means for generating a roll of the backed ply material by wrapping the backed ply material about a spool.
15. The apparatus according to claim 14, wherein the polyester film is substantially transparent.
16. An apparatus for generating a composite layup, the apparatus comprising:
means for tacking a ply material having a polyester backing film to a tool;
means for disposing the ply material upon the tool along a path; and
means for removing the polyester backing film.
17. The apparatus according to claim 16, further comprising:
means for cutting the ply material in response disposing the ply material at an end of the path.
18. A method of generating a backed ply material, the method comprising:
disposing a polyester film upon a ply material.
19. The method according to claim 18, further comprising:
generating a roll of the backed ply material by wrapping the backed ply material about a spool.
20. The method according to claim 18, wherein the polyester film is substantially transparent.
21. A method of generating a composite layup, the method comprising:
tacking a ply material having a polyester backing film to a tool;
disposing the ply material upon the tool along a path; and
removing the polyester backing film.
22. The method according to claim 21, further comprising:
cutting the ply material in response disposing the ply material at an end of the path.
23. The method according to claim 21, further comprising:
recycling the polyester backing film in response to the removing step.
US10/829,270 2004-04-22 2004-04-22 Backing film and method for ply materials Abandoned US20050238892A1 (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006035847A1 (en) * 2006-08-01 2008-02-14 Airbus Deutschland Gmbh Wing section producing method for e.g. aircraft, involves laying structural arrangement on laminating apparatus by tape-laying machine, and curing structural arrangement to form wing section
US20100084087A1 (en) * 2006-11-20 2010-04-08 The Boeing Company Apparatus and method for composite material trim-on-the-fly
US20120086150A1 (en) * 2010-10-08 2012-04-12 Airbus Operations Process for manufacturing a stiffener of composite material
US20130065068A1 (en) * 2008-02-18 2013-03-14 Hexcel Composites Limited Composite Tape For Use In Tape Laying Machines
US20140374003A1 (en) * 2012-08-31 2014-12-25 General Electric Company Methods and systems for automated ply layup for composites
CN111136992A (en) * 2018-11-01 2020-05-12 波音公司 Self-penetrating lamination head and method

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7455742B2 (en) * 2005-02-16 2008-11-25 The Boeing Company Slit-course ply placement device and method
US8999098B2 (en) 2010-02-05 2015-04-07 Orbital Atk, Inc. Backing for pre-preg material
US9321220B2 (en) 2010-04-13 2016-04-26 Orbital Atk, Inc. Automated bias-ply preparation device and process
US20140087198A1 (en) 2012-09-26 2014-03-27 Web Industries, Inc. Prepreg tape slitting method and apparatus
KR101422129B1 (en) * 2013-05-16 2014-07-22 재단법인 중소조선연구원 high speed laminated molding appartus using rotating mold
US11059235B2 (en) 2018-09-28 2021-07-13 The Boeing Company Reconfigurable manufacturing system and method for manufacturing composite laminates
US10994502B2 (en) 2018-11-01 2021-05-04 The Boeing Company Lamination system and method using a plurality of static lamination heads
US10926492B2 (en) 2018-11-01 2021-02-23 The Boeing Company Bi-directional lamination head and method
US10960615B2 (en) 2018-11-13 2021-03-30 The Boeing Company System and method for laminating a composite laminate along a continuous loop lamination path
US11396143B2 (en) 2019-06-21 2022-07-26 The Boeing Company System and method for manufacturing a composite assembly
US11148373B2 (en) 2019-07-01 2021-10-19 The Boeing Company System and method for laying up a composite laminate having integrally laminated filler elements
US11052454B2 (en) 2019-07-23 2021-07-06 The Boeing Company Dynamic collar swage conformance checking based on swage tool parameters
EP4008530A1 (en) 2020-12-04 2022-06-08 The Boeing Company Lamination head having self-threading capability
EP4008529B1 (en) 2020-12-04 2024-01-31 The Boeing Company Lamination head having bi-directional capability

Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3971866A (en) * 1974-06-07 1976-07-27 Minnesota Mining And Manufacturing Company Thermoformable release liner
US4029838A (en) * 1975-09-24 1977-06-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hybrid composite laminate structures
US4319750A (en) * 1979-04-30 1982-03-16 Aldila, Inc. Golf shaft having controlled flex zone
US4683018A (en) * 1984-12-06 1987-07-28 Rolls-Royce Plc Composite material manufacture by shaping individual sheets followed by consolidating the sheets
US4867834A (en) * 1986-04-07 1989-09-19 Hercules Filament winding system
US4876153A (en) * 1987-04-09 1989-10-24 Basf Corporation Process for the preparation of cyanate resin-based prepregs and films which maintain their tack
US4938824A (en) * 1987-01-23 1990-07-03 Thiokol Corporation Method for making a composite component using a transverse tape
US5043032A (en) * 1989-02-17 1991-08-27 Bell Helicopter Textron Inc. Method for detecting protective layer on composite materials
US5173138A (en) * 1990-08-08 1992-12-22 Blauch Denise A Method and apparatus for the continuous production of cross-plied material
US5496602A (en) * 1994-11-22 1996-03-05 Dow-United Technologies Composite Products, Inc. Low resin content unidirectional fiber tape
US5589115A (en) * 1987-11-16 1996-12-31 Corning Incorporated Method for making fiber-reinforced ceramic matrix composite
US5667889A (en) * 1995-11-21 1997-09-16 Imperial Chemical Industries Plc Polymeric film
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6013376A (en) * 1997-12-09 2000-01-11 3M Innovative Properties Company Metal fibermat/polymer composite
US6133167A (en) * 1992-07-30 2000-10-17 Ciba Specialty Chemicals Corp. Fibre reinforced resin composite products
US6163957A (en) * 1998-11-13 2000-12-26 Fujitsu Limited Multilayer laminated substrates with high density interconnects and methods of making the same
US6242090B1 (en) * 1993-07-26 2001-06-05 Hexcel Corporation Fibre reinforced resin composite products
US6523258B2 (en) * 2000-03-13 2003-02-25 Matsushita Electric Industrial Co., Ltd. Method of manufacturing printed circuit board

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3775219A (en) * 1971-04-05 1973-11-27 Goldsworthy Eng Inc Composite-tape placement head
GB1587536A (en) * 1977-07-05 1981-04-08 Ciba Geigy Ag Expoxide resin-impregnated composites
US4588466A (en) * 1983-04-08 1986-05-13 Vektronics Manufacturing, Inc. Tape laying method and apparatus
US4637943A (en) * 1984-09-17 1987-01-20 Simmonds Precision Sealed split instrument housing with foil-backed acrylic transfer adhesive tearband
US4732814A (en) * 1985-10-03 1988-03-22 Toray Industries, Inc. Polyester film with smooth and highly adhesive surface and method of making same
US5117348A (en) * 1986-03-28 1992-05-26 The Ingersoll Milling Machine Company Method for alignment of a representative surface to an actual surface for a tape laying machine
US4861406A (en) * 1987-08-17 1989-08-29 The Boeing Company Method and apparatus for handling plies of composite material
US4990213A (en) * 1988-11-29 1991-02-05 Northrop Corporation Automated tape laminator head for thermoplastic matrix composite material
EP0541795B1 (en) * 1989-01-25 1998-04-01 Asahi Kasei Kogyo Kabushiki Kaisha New prepreg and composite molding, and production of composite molding
TW289900B (en) * 1994-04-22 1996-11-01 Gould Electronics Inc
US5700347A (en) * 1996-01-11 1997-12-23 The Boeing Company Thermoplastic multi-tape application head
US6692681B1 (en) * 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
US6596391B2 (en) * 1997-05-14 2003-07-22 Honeywell International Inc. Very ultra thin conductor layers for printed wiring boards
JP2001225418A (en) 2000-02-17 2001-08-21 Teijin Ltd Release film and protective film for prepreg using the same
US8017531B2 (en) * 2001-09-18 2011-09-13 Elkcorp Composite material
JP4213887B2 (en) * 2001-10-26 2009-01-21 日東電工株式会社 Transparent adhesive composition and adhesive sheet thereof
TWI289155B (en) * 2002-04-03 2007-11-01 Tomoegawa Paper Co Ltd Adhesive sheet for producing semiconductor devices
JP2003308016A (en) * 2002-04-16 2003-10-31 Nitto Denko Corp Tacky adhesive label for display
US6919405B2 (en) * 2002-12-31 2005-07-19 3M Innovative Properties Company Release compositions and articles made therefrom
JP4614126B2 (en) * 2005-02-21 2011-01-19 リンテック株式会社 LAMINATED SHEET, LAMINATED SHEET WIND AND PROCESS FOR PRODUCING THEM
JP4986423B2 (en) * 2005-08-03 2012-07-25 日東電工株式会社 Peeling treatment substrate and method for producing the same
US20100136265A1 (en) * 2007-04-13 2010-06-03 Everaerts Albert I Antistatic optically clear pressure sensitive adhesive

Patent Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3971866A (en) * 1974-06-07 1976-07-27 Minnesota Mining And Manufacturing Company Thermoformable release liner
US4029838A (en) * 1975-09-24 1977-06-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hybrid composite laminate structures
US4319750A (en) * 1979-04-30 1982-03-16 Aldila, Inc. Golf shaft having controlled flex zone
US4683018A (en) * 1984-12-06 1987-07-28 Rolls-Royce Plc Composite material manufacture by shaping individual sheets followed by consolidating the sheets
US4867834A (en) * 1986-04-07 1989-09-19 Hercules Filament winding system
US4938824A (en) * 1987-01-23 1990-07-03 Thiokol Corporation Method for making a composite component using a transverse tape
US4876153A (en) * 1987-04-09 1989-10-24 Basf Corporation Process for the preparation of cyanate resin-based prepregs and films which maintain their tack
US5589115A (en) * 1987-11-16 1996-12-31 Corning Incorporated Method for making fiber-reinforced ceramic matrix composite
US5043032A (en) * 1989-02-17 1991-08-27 Bell Helicopter Textron Inc. Method for detecting protective layer on composite materials
US5173138A (en) * 1990-08-08 1992-12-22 Blauch Denise A Method and apparatus for the continuous production of cross-plied material
US6133167A (en) * 1992-07-30 2000-10-17 Ciba Specialty Chemicals Corp. Fibre reinforced resin composite products
US6242090B1 (en) * 1993-07-26 2001-06-05 Hexcel Corporation Fibre reinforced resin composite products
US5496602A (en) * 1994-11-22 1996-03-05 Dow-United Technologies Composite Products, Inc. Low resin content unidirectional fiber tape
US5667889A (en) * 1995-11-21 1997-09-16 Imperial Chemical Industries Plc Polymeric film
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6013376A (en) * 1997-12-09 2000-01-11 3M Innovative Properties Company Metal fibermat/polymer composite
US6163957A (en) * 1998-11-13 2000-12-26 Fujitsu Limited Multilayer laminated substrates with high density interconnects and methods of making the same
US6523258B2 (en) * 2000-03-13 2003-02-25 Matsushita Electric Industrial Co., Ltd. Method of manufacturing printed circuit board

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8709188B2 (en) 2006-08-01 2014-04-29 Airbus Operations Gmbh Lay-up arrangement and structural arrangement and method for producing a component for aerospace
US20090269596A1 (en) * 2006-08-01 2009-10-29 Olaf Rocker Lay-up arrangement and structural arrangement and method for producing a component for aerospace
DE102006035847B4 (en) * 2006-08-01 2009-11-19 Airbus Deutschland Gmbh Structural arrangement and method for producing a component for aerospace
DE102006035847A1 (en) * 2006-08-01 2008-02-14 Airbus Deutschland Gmbh Wing section producing method for e.g. aircraft, involves laying structural arrangement on laminating apparatus by tape-laying machine, and curing structural arrangement to form wing section
US20100084087A1 (en) * 2006-11-20 2010-04-08 The Boeing Company Apparatus and method for composite material trim-on-the-fly
US20110192545A1 (en) * 2006-11-20 2011-08-11 Mccowin Peter D Composite material layup including trim-on-the-fly
US8640757B2 (en) * 2006-11-20 2014-02-04 The Boeing Company Composite material layup including trim-on-the-fly
US7879177B2 (en) 2006-11-20 2011-02-01 The Boeing Company Apparatus and method for composite material trim-on-the-fly
US20130065068A1 (en) * 2008-02-18 2013-03-14 Hexcel Composites Limited Composite Tape For Use In Tape Laying Machines
US9333678B2 (en) * 2008-02-18 2016-05-10 Hexcel Composites, Limited Composite tape for use in tape laying machines
US20120086150A1 (en) * 2010-10-08 2012-04-12 Airbus Operations Process for manufacturing a stiffener of composite material
US8985995B2 (en) * 2010-10-08 2015-03-24 Airbus Operations (S.A.S.) Process for manufacturing a stiffener of composite material
US20140374003A1 (en) * 2012-08-31 2014-12-25 General Electric Company Methods and systems for automated ply layup for composites
US9421744B2 (en) * 2012-08-31 2016-08-23 General Electric Company Methods and systems for automated ply layup for composites
CN111136992A (en) * 2018-11-01 2020-05-12 波音公司 Self-penetrating lamination head and method

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