US20140110633A1 - Surface Engineering of Thermoplastic Materials and Tooling - Google Patents

Surface Engineering of Thermoplastic Materials and Tooling Download PDF

Info

Publication number
US20140110633A1
US20140110633A1 US14/057,254 US201314057254A US2014110633A1 US 20140110633 A1 US20140110633 A1 US 20140110633A1 US 201314057254 A US201314057254 A US 201314057254A US 2014110633 A1 US2014110633 A1 US 2014110633A1
Authority
US
United States
Prior art keywords
thermoplastic
mold
surface layer
fiber reinforced
layer polymer
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
Application number
US14/057,254
Other languages
English (en)
Inventor
James Francis Pratte
Scott Alfred Rogers
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.)
Cytec Industries Inc
Original Assignee
Cytec Industries 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 Cytec Industries Inc filed Critical Cytec Industries Inc
Priority to US14/057,254 priority Critical patent/US20140110633A1/en
Assigned to CYTEC INDUSTRIES INC. reassignment CYTEC INDUSTRIES INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ROGERS, SCOTT ALFRED, PRATTE, JAMES FRANCIS
Assigned to CYTEC INDUSTRIES INC. reassignment CYTEC INDUSTRIES INC. CORRECTIVE ASSIGNMENT TO CORRECT THE RECEIVING PARTY DATA PREVIOUSLY RECORDED ON REEL 032220 FRAME 0074. ASSIGNOR(S) HEREBY CONFIRMS THE CYTEC INDUSTRIES INC. 5 GARRET MOUNTAIN PLAZA WOODLAND PARK, NEW JERSEY 07424. Assignors: ROGERS, SCOTT ALFRED, PRATTE, JAMES FRANCIS
Publication of US20140110633A1 publication Critical patent/US20140110633A1/en
Priority to US15/045,650 priority patent/US11214019B2/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
    • B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
    • B29B15/10—Coating or impregnating independently of the moulding or shaping step
    • B29B15/105—Coating or impregnating independently of the moulding or shaping step of reinforcement of definite length with a matrix in solid form, e.g. powder, fibre or sheet form
    • 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
    • B32B7/005—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D1/00—Processes for applying liquids or other fluent materials
    • B05D1/02—Processes for applying liquids or other fluent materials performed by spraying
    • B05D1/08—Flame spraying
    • B05D1/10—Applying particulate materials
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/3842—Manufacturing moulds, e.g. shaping the mould surface by machining
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/42—Moulds or cores; Details thereof or accessories therefor characterised by the shape of the moulding surface, e.g. ribs or grooves
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/56—Coatings, e.g. enameled or galvanised; Releasing, lubricating or separating agents
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/56—Coatings, e.g. enameled or galvanised; Releasing, lubricating or separating agents
    • B29C33/60—Releasing, lubricating or separating agents
    • B29C33/62—Releasing, lubricating or separating agents based on polymers or oligomers
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/56—Coatings, e.g. enameled or galvanised; Releasing, lubricating or separating agents
    • B29C33/68—Release sheets
    • 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
    • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0067—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other
    • B29C37/0075—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other using release sheets
    • 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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/0008—Electrical discharge treatment, e.g. corona, plasma treatment; wave energy or particle radiation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered 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
    • B32B7/03—Layered 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 with respect to the orientation of features
    • 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
    • B29K2071/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone or derivatives thereof, as moulding material
    • 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
    • B29K2079/00—Use of polymers having nitrogen, with or without oxygen or carbon only, in the main chain, not provided for in groups B29K2061/00 - B29K2077/00, as moulding material
    • B29K2079/08—PI, i.e. polyimides or derivatives thereof
    • B29K2079/085—Thermoplastic polyimides, e.g. polyesterimides, PEI, i.e. polyetherimides, or polyamideimides; Derivatives thereof
    • 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
    • B29K2101/00—Use of unspecified macromolecular compounds as moulding material
    • B29K2101/12—Thermoplastic materials
    • 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
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0872—Prepregs
    • B29K2105/0881—Prepregs unidirectional
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/26—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer which influences the bonding during the lamination process, e.g. release layers or pressure equalising layers
    • B32B2037/268—Release layers
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31855—Of addition polymer from unsaturated monomers
    • Y10T428/31935—Ester, halide or nitrile of addition polymer

Definitions

  • the subject matter of the present invention relates to fiber reinforced thermoplastic plastic composite materials and particularly to applying a surface layer polymer coating to a composite forming mold tool or to a fiber reinforced thermoplastic prepreg composite material to enhance the first ply laydown of the prepreg onto the composite forming mold tool for prepreg forming or in situ automated laydown tape placement.
  • In situ application of the surface layer polymer coating during or before automated laydown may also provide a beneficial resin rich interlaminar layer between each layer of fiber reinforced thermoplastic composite material.
  • the surface layer polymer coating is preferably thermoplastic particles applied by plasma spraying to the mold tool or prepreg to form a substantially fused layer of thermoplastic particles. More particularly, in certain embodiments the present invention relates to layered fiber reinforced thermoplastic prepreg for use in rapid lamination and forming processes where such fiber reinforced thermoplastic prepreg are useful in aerospace and other high-performance automotive/industrial applications.
  • thermoplastic and thermoset materials have wide application in, for example, the aerospace, automotive, industrial/chemical, and sporting goods industries.
  • Thermosetting resins are impregnated into the fiber reinforcing material before curing, while the resinous materials are low in viscosity.
  • Thermoset composites suffer from disadvantages including processing problems concerned with removing entrained air or volatiles so that a void-free matrix is produced.
  • Thermoset composites made by the prepreg method require lengthy cure times with alternating pressures to control the flow of the resin as it cures to prevent bubbles in the matrix. While traditional fabrication of structures utilized hand placement of thermosetting prepreg plies onto a tool, current fabrication of large structures utilize robotic placement of the thermoset composite material onto the tool to increase production rate.
  • the overall production rate for a structural component is limited by the lengthy cure in the autoclave process step and related operations to prepare the material for that process step.
  • Some high volume processes, such as resin infusion avoid the prepreg step but still require special equipment and materials along with constant monitoring of the process over the length of the cure time (e.g., U.S. Pat. Nos. 4,132,755, and 5,721,034).
  • thermoplastic resin compositions are more difficult to impregnate into the fiber reinforcing material because of their comparatively higher viscosity than thermosetting resin compositions.
  • thermoplastic resin compositions offer a number of benefits over thermosetting resin compositions.
  • thermoplastic prepregs can be more rapidly fabricated into articles and fabrication with fiber reinforced thermoplastic composite materials may utilize robotic automated laydown tape placement of the fiber reinforced thermoplastic composite material onto a mold tool to increase production rate. This may be through a multiple-step robotic arm that pre-heats the prior layer of fiber reinforced thermoplastic composite material before heating and laying the subsequent layer of fiber reinforced thermoplastic composite material on top of it.
  • thermosets have viscosities in the range of 100 to 5,000 centipoise (0.1 to 5 Pa*s)
  • thermoplastics have melt viscosities ranging from 5,000 to 20,000,000 centipoise (5 to 20,000 Pa*s), and more typically from 20,000 to 1,000,000 centipoise (20 to 1000 Pa*s).
  • some processes have been applied to both types of matrices for laminating fibrous materials.
  • Fiber reinforced plastic materials may be manufactured by first impregnating the fiber reinforcement with resin to form a prepreg, then consolidating two or more prepregs into a laminate, optionally with additional forming steps. A few processes apply melt directly to the fibers.
  • a tape can be made by coating a dry web of collimated fibers with the polymer and applying a heated process that forces the polymer into and around the fibers (e.g., see U.S. Pat. Nos. 4,549,920 and 4,559,262).
  • Another process used to coat and impregnate a dry web of collimated fibers is by pulling the web through an aqueous slurry of fine thermoplastic polymer particles whereby the polymer particles are trapped within the filament bundles.
  • thermoplastic and thermoset composites can be formed into thin flexible sheets or strips, referred to as tape.
  • This allows composite components to be formed by laying down the composite tape in a molding tool, with the thickness of the component being locally varied according to the number of layers of composite tape laid down and also the direction of one or more layers of the tape being controllable so as to control the final structural properties of the formed composite component.
  • the laid up components are then “consolidated”, a process which cases involves heating the composite structure so that the thermoset or thermoplastic matrix softens to a sufficient degree to form a single unified matrix, and applying sufficient pressure to the softened matrix to expel any trapped air from the matrix.
  • thermoplastic composites In terms of final structural properties, thermoplastic composites have superior impact and damage resistance properties to those of thermoset composites and are generally tougher and more resistant to chemical attack, all of which are preferable properties within aerospace applications. Furthermore, since thermoplastic composites may be repeatedly reheated and remolded, they are inherently recyclable, which is an increasingly important consideration.
  • thermoset composite tape has one property that, in relation to the laying up process, currently makes it the material of choice for use in aerospace composite components. This property is that the thermoset tape is inherently sticky, or is said to have tack. This tackiness allows the thermoset tape to adhere to both the complex shaped mold surfaces often required for composite components within the aerospace industry, and also for separate layers of the thermoset tape to adhere to one another once the initial layer has been applied to the mold surface, thus making the laying up process relatively easy and convenient to physically manage.
  • thermoplastic composite tape has no tackiness. Consequently, it is problematic to make the thermoplastic composite tape adhere to complex mold surfaces during the lay-up process.
  • Existing lay-up techniques combine local consolidation and melting of the thermoplastic composite material to enable the initial, base layer to be built up only as long as the base layer is firmly held to the surface of the mold tool.
  • Previously proposed solutions to this problem have included applying a separate double-sided adhesive tape as an initial layer to the mold surface to which the first layer of thermoplastic composite tape subsequently adheres. Similarly, it has also been proposed to spray an adhesive to the surface of the mold.
  • thermoset composite materials Whilst both proposed solutions allow the first layer of thermoplastic composite tape to be successfully applied to complex shaped mold surfaces, they introduce their own problem of how to subsequently remove the formed composite component from the mold when the laying up process is complete, since the component is now effectively bonded to the mold surface. Consequently, it is still presently preferred to use thermoset composite materials despite the superior physical properties provided by thermoplastic composite materials.
  • Known methods for fabrication of composite articles include manual and automated fabrication.
  • Manual fabrication entails manual cutting and placement of material by a technician to a surface of the mandrel. This method of fabrication is time consuming and cost intensive, and can possibly result in non-uniformity in the lay-up.
  • Automated fabrication techniques include flat tape laminating machines (FTLM) and contour tape laminating machines (CTLM).
  • FTLM flat tape laminating machines
  • CTLM contour tape laminating machines
  • FTLM and CTLM employ a solitary composite material dispenser that travels over the work surface onto which the composite material is to be applied.
  • the composite material is typically laid down a single row (of composite material) at a time to create a layer of a desired width and length. Additional layers may thereafter be built up onto a prior layer to provide the lay-up with a desired thickness.
  • FTLM's typically apply composite material to a flat transfer sheet; the transfer sheet and lay-up are subsequently removed from the FTLM and placed onto a tool, mold or mandrel.
  • CTLM's typically apply composite material directly to the work surface of a tool, mold or mandrel.
  • FLTM and CTLM machines are also known as automated tape laydown (ATL) and automated fiber placement (AFP) machines, with the dispenser commonly referred to as a tape head.
  • ATL automated tape laydown
  • AFP automated fiber placement
  • the productivity of ATL/AFP machines is dependent on machine parameters, composite part lay-up features, and material characteristics.
  • Machine parameters such as start/stop time, course transition time, and cut/adding plies determine the total time the tape head on the ATL/AFP is laying material on the mandrel.
  • Composite lay-up features such as localized ply build-ups and part dimensions also influence the total productivity of the ATL/AFP machines.
  • thermoplastic parts are in situ fabrication wherein a part is created by robotically placing and consolidating thermoplastic materials onto the molding tool in one step.
  • Thermoplastic composite materials lack tack, which complicates the use of hand and automated lay-up operations, especially of the first ply against the molding tool surface.
  • thermoset resin matrix composites Key material factors that influence ATL/AFP machine productivity are similar for a thermoset resin matrix composite when compared with a thermoplastic matrix composite yet there are a couple of key differences.
  • key factors are impregnation levels, surface resin coverage, and “tack”.
  • Tack is the adhesion level necessary to maintain the position of the tape/tow on the tool or lay-up after it has been deposited on it. Due to the unreacted nature of the thermoset resin, the ATL/AFP process is generally performed at room temperature but in humidity controlled rooms due to the moisture sensitivity on the tack level of the material.
  • tack affects the ability to lay down the first ply of material onto the tool. First ply lay-down of thermoplastic materials is complicated by the lack of tack to hold the first layer down to the tool.
  • the first composite ply to be placed against any tool requires some adhesive or other force to position the material and hold it against gravity or the stiffness of the material.
  • the polymer that is above the T g at the lay-down head will provide this force.
  • the matrix resin is a high performance thermoplastic, this T g temperature is substantially higher and substantially above room temperature. Heating the mold tool, providing a vacuum source, use of a lower temperature film or using a solvated thermoplastic polymer to provide the restraining force are all methods currently used. Each of these methods has limitations in cost, tool complexity, variation to the dimensions of the part or requires hazardous solvents to practice.
  • thermoplastics manufacturing A method known to overcome the limitation of low tack in thermoplastics manufacturing is to provide a mold tool made of a porous material and apply a negative pressure to the porous material so as to create a negative pressure at the mold surface, whereby the thermoplastic composite material is held against the mold surface by virtue of the negative pressure at the mold surface when the initial layer of thermoplastic composite material is laid onto the mold surface.
  • the thermoplastic material could thereafter be consolidated and heated to form the thermoplastic composite material (see, e.g., U.S. Patent Application Publication No. 2011/0005666).
  • thermoplastic matrix composites have similar key factors as thermoset matrix composites for ATL/AFP machine productivity, but the thermoplastics polymer tape lack tack at ambient conditions.
  • Thermoplastics generally have low surface energies, a high glass transition temperature (“T g ”), making adhesion at room temperature unlikely.
  • T g glass transition temperature
  • the high performance thermoplastic matrices are in their glass state at room temperature making the molecular diffusion mechanism for tack virtually impossible.
  • tack is achieved in thermoplastic composites by dynamically applying additional energy in the form of thermal, ultrasonic, optical (laser), and/or electromagnetic (induction) to the lay-up and incoming tape to raise the temperature of the materials above their softening and/or melt temperature in order to facilitate molecular diffusion of the polymer chains to occur between the two surfaces.
  • additional energy in the form of thermal, ultrasonic, optical (laser), and/or electromagnetic (induction) to the lay-up and incoming tape to raise the temperature of the materials above their softening and/or melt temperature in order to facilitate molecular diffusion of the polymer chains to occur between the two surfaces.
  • the additional energy added to the materials needs to be removed to a level that will prevent distortion of the laminated lay-up once the lamination pressure from the ATL/AFP head is removed.
  • This rapid flux of energy into and out of the lay-up makes it desirable from an energy usage and lay down speed to perform this process step at the lowest possible temperature and energy without compromising on the temperature performance of the resulting composite part
  • Consolidation is typically necessary to remove voids that result from the inability of the resin to fully displace air from the fiber bundle, tow, or roving during the processes that have been used to impregnate the fibers with resin.
  • the individually impregnated roving yarns, tows, plies, or layers of prepregs are usually consolidated by heat and pressure by compacting in an autoclave.
  • the consolidation step has generally required the application of very high pressures and high temperatures under vacuum for relatively long times.
  • the consolidation process step using an autoclave or oven requires a “bagging” operation to provide the lay-up with a sealed membrane over the tool to allow a vacuum to be applied for removal of air and to provide the pressure differential necessary to effect consolidation in the autoclave.
  • thermoplastic composite it would be advantageous to in-situ consolidate to a low void composite while laminating the tape to the substrate with the ATL/AFP machine.
  • This process is typically referred to as in situ ATL/AFP and the material used in that process called an in situ grade tape.
  • thermoplastic composites have had limited success to date, due to a variety of factors including high processing temperatures (currently around 400° C.), high pressures, and prolonged molding times needed to produce good quality laminates.
  • high processing temperatures currently around 400° C.
  • high pressures high pressures
  • prolonged molding times needed to produce good quality laminates.
  • Most of the efforts have been focused on combining high performance polymers to structural fibers which has only exacerbated the process problems.
  • the length of time typically required to properly consolidate the prepreg plies determines the production rate for the part, it would be desirable to achieve the best consolidation in the shortest amount of time.
  • lower consolidation pressures or temperatures and shorter consolidation times will result in a less expensive production process due to lowered consumption of energy per piece for molding and other manufacturing benefits.
  • thermoplastic materials and methods presently available for producing light-weight, toughened composites require further improvement.
  • Thermoplastic materials having improved process speeds on automated lay-up machines and lower processing temperatures and having no autoclave or oven step would be a useful advance in the art and could find rapid acceptance in the aerospace and high-performance automotive industries, among others.
  • the present invention provides a prepared mold tool having a releasably adhered surface layer polymer coating on the mold surface of the mold tool.
  • the mold tool is a non-porous metal mold tool having a mold surface with a texture and a release film adhered to the textured mold surface of the mold tool and the surface layer polymer coating adhered to the release film.
  • the surface layer polymer coating is preferably a plurality of thermoplastic particles applied to the mold surface by plasma spray creating a substantially fused layer of thermoplastic particles.
  • the prepared mold tool aids placement and adhesion of the first ply of a fiber reinforced thermoplastic composite material such as a thermoplastic prepreg, a thermoplastic unidirectional tape or web, fiber tow/preg, or fabric, or non-woven materials such as a mat or veil.
  • a fiber reinforced thermoplastic composite material such as a thermoplastic prepreg, a thermoplastic unidirectional tape or web, fiber tow/preg, or fabric, or non-woven materials such as a mat or veil.
  • Thermoplastic prepregs are traditionally applied by hand lay-down while thermoplastic unidirectional tapes are applied by in situ automated laydown tape placement against a mold tool.
  • the present invention also involves a method for preparing a prepared mold tool for first ply laydown by providing a solid metal, non-porous mold tool having a mold surface, applying a texture to a mold surface of the mold tool, applying a release film to the mold surface having a texture and finally applying a surface layer polymer coating by plasma spraying thermoplastic particles onto the release film on the mold surface of the mold tool having the texture.
  • a further embodiment of the present invention provides a prepared prepreg having fiber reinforced thermoplastic composite material with a surface layer polymer coating adhered to one or both surfaces of the composite material.
  • the surface layer polymer coating is preferably a plurality of thermoplastic particles applied to the surface of the fiber reinforced thermoplastic composite materials by plasma spray to create a substantially fused layer of thermoplastic particles on the surface.
  • the prepared prepreg aids placement of the first ply of fiber reinforced thermoplastic composite material to a mold surface of a mold tool and may further improve resulting composite part interlaminar properties between plies of composite material.
  • the present invention also involves a method for preparing the prepared prepreg by providing a fiber reinforced thermoplastic composite material such as a thermoplastic prepreg or a thermoplastic unidirectional tape and then applying a surface layer polymer coating by plasma spraying thermoplastic particles onto one or both of the surfaces of the fiber reinforced thermoplastic composite material.
  • a fiber reinforced thermoplastic composite material such as a thermoplastic prepreg or a thermoplastic unidirectional tape
  • the surface layer polymer coating provides a compatible chemistry placed against the mold tool which maintains the dimensions, lowers the temperature requirement for adhesion, and allows the use of hybrid polymer and optional inclusion of conductive coatings for lightning strike in the surface layer polymer coating.
  • This compatible chemistry of the present invention improves adhesion of the first ply of fiber reinforced thermoplastic composite material to the mold surface of the mold tool while maintaining ease of separation of the resulting composite part from the mold tool.
  • the surface layer polymer coating will transfer to the resulting composite part as a surface skin that may impart desirable characteristics to the resulting composite part. Such desirable characteristics such as fire, corrosion or wear protection may come from multi-functional additives to the surface layer polymer coating.
  • the surface layer polymer coating is a high performance thermoplastic such as poly(ether ether ketone) (“PEEK”) or poly(ether ketone ketone) (“PEKK”).
  • PEEK poly(ether ether ketone)
  • PEKK poly(ether ketone ketone)
  • the present invention seeks to improve first-ply lay-down by reducing composite part failure due to material de-bonding against the mold tool during processing, as well as improving chemical compatibility in the high performance thermoplastic polymer.
  • Concepts including fast crystallization or amorphous materials as well as discrete metallic layers and ground fiber mixtures are possible. Furthermore, this discovery also reduces the initial capital and facility cost investment to produce large composites.
  • the present invention also provides methods for manufacturing a resulting thermoplastic composite part with a thickness in the range of 25 to 400 microns that has improved processing times on ATL machines and manufacturing equipment.
  • the invention described in detail herein provides, in one aspect, a prepared mold tool having a surface layer polymer coating of at least one high performance polymer, and a prepared prepreg having surface layer polymer coating on one or both surfaces.
  • the invention relates to articles of manufacture made from the thermoplastic composites according to the invention described herein. Such articles are useful, for example, in the aircraft/aerospace industries among others.
  • thermoplastic composite material tapes for use on an automated tape laydown or automated fiber placement machine are also provided.
  • FIG. 1 a is a side plan view of one embodiment of the present invention illustrating the configuration of the prepared tool ( 10 ) including the non-porous metal mold tool ( 20 ), the textured mold surface ( 30 ) of the mold tool, the release film ( 40 ) and the surface layer polymer coating ( 50 ).
  • FIG. 1 b is a perspective view of the embodiment of FIG. 1 a illustrating the configuration of the prepared tool ( 10 ) including the non-porous metal mold tool ( 20 ), the textured mold surface ( 30 ) of the mold tool, a sealer and the applied release film ( 40 ) and the surface layer polymer coating ( 50 ) shown as substantially fused thermoplastic particles after application by plasma spraying.
  • FIG. 2 a illustrates a perspective view of in situ application of the surface layer polymer coating ( 50 ) from a plasma spray head ( 70 ) onto a non-porous metal tool ( 20 ) followed by application of a first ply thermoplastic fiber reinforced composite material ( 60 ) and compacted by an AFP/ATL laydown roller ( 80 ).
  • FIG. 2 b further illustrates a perspective view of in situ application of the thermoplastic interlaminar layer ( 90 ) (e.g., thermoplastic particles) from a plasma spray head ( 70 ) onto a previously applied thermoplastic composite tape material ( 60 ) followed by application of a subsequent ply thermoplastic fiber reinforced composite material ( 60 ) and compacted by an ATL laydown roller ( 80 ) providing in situ applied thermoplastic interlaminar layer ( 90 ) between layers of thermoplastic fiber reinforced composite material during automated tape lay-down.
  • the thermoplastic interlaminar layer ( 90 ) e.g., thermoplastic particles
  • FIG. 3 illustrates a side plan view of a surface layer polymer coating applied to a thermoplastic composite prepreg by plasma spraying a thermoplastic polymer coating ( 50 ) from a plasma spray head ( 70 ) onto one or both surfaces of a composite material ( 60 ) to form a plasma coated thermoplastic composite material ( 100 ).
  • FIG. 4 a illustrates the mean spacing of local peaks of profile of a high temperature mold tool and a thermoplastic surface layer polymer coating using a profilometer.
  • FIG. 4 b illustrates the spacing of peaks in the y-axis.
  • the present invention provides a prepared mold tool having a surface layer polymer coating applied to the release side mold surface of the mold tool to enhance adhesion of the first ply of thermoplastic fiber reinforced composite material to the mold surface.
  • FIG. 1 a illustrates such an embodiment of the present invention providing the configuration of a prepared tool ( 10 ), including the non-porous metal mold tool ( 20 ) with a textured molding surface ( 30 ), a release film ( 40 ) and a surface layer polymer coating ( 50 ) releasably applied to the release film.
  • FIG. 1 b illustrates such an embodiment of the present invention providing the prepared tool ( 10 ) detailing the surface layer polymer coating ( 50 ) shown as substantially fused thermoplastic particles applied by plasma spraying.
  • surface layer polymer coating ( 50 ) may be applied to the release side mold surface of mold tool ( 20 ) through use of plasma spray during in situ automated tape laydown.
  • plasma spray of the surface layer polymer during automated tape laydown on top of a prior ply of fiber reinforced composite material ( 60 ) provides a thermoplastic interlaminar layer ( 90 ) that can impart beneficial properties such as toughening to the resulting composite part.
  • FIG. 2 a illustrates in situ application of the surface layer polymer coating ( 50 ) such as thermoplastic particles from a plasma spray head ( 70 ) onto a non-porous metal mold tool ( 20 ) and then the application of thermoplastic fiber reinforced composite material ( 60 ) and compacted by an ATL laydown roller ( 80 ).
  • the surface layer polymer coating ( 50 ) such as thermoplastic particles from a plasma spray head ( 70 ) onto a non-porous metal mold tool ( 20 ) and then the application of thermoplastic fiber reinforced composite material ( 60 ) and compacted by an ATL laydown roller ( 80 ).
  • FIG. 2 b further illustrates continued plasma spray of the surface layer polymer by plasma spray head ( 70 ) during automated tape laydown thereby providing a thermoplastic interlaminar layer ( 90 ), and then application of a subsequent ply of thermoplastic fiber reinforced composite material ( 60 ) compacted by ATL laydown roller ( 80 ).
  • thermoplastic such as a thermoplastic from a plasma spray head ( 70 ) onto a previously ply of thermoplastic fiber reinforced composite material ( 60 ) and then a subsequent ply of thermoplastic composite material ( 60 ) applied and compacted by an ATL laydown roller ( 80 ) provides an in situ applied interlaminar thermoplastic layer ( 90 ) between the layers of thermoplastic fiber reinforced composite material and subsequently applied thermoplastic fiber reinforced composite material during automated tape lay-down.
  • Thermoplastic interlaminar layer ( 90 ) and surface layer polymer coating ( 50 ) are each high performance thermoplastic polymers, and may be the same or different materials and may contain the same or different multifunctional additives. This versatility in selection of the particular high performance thermoplastic polymer permits selection of the optimal materials for the surface layer coating ( 50 ) and the interlaminar layer ( 90 ).
  • first ply fiber reinforced composite material ( 60 ) and the subsequent plies of fiber reinforced composite material ( 60 ) are each compatible material, but may be the same or different compositions depending upon the properties desired for each layer.
  • the present invention provides prepared prepreg having a surface layer polymer coating applied directly to one or more surfaces of a thermoplastic fiber reinforced composite prepreg material to enhance adhesion of the first ply of the thermoplastic fiber reinforced composite material to the mold surface of the mold tool and to further provide a beneficial interlaminar layer to the resulting composite part.
  • FIG. 3 illustrates a prepreg ( 100 ) prepared by applying a surface layer polymer coating ( 50 ) to both surfaces of a thermoplastic fiber reinforced composite material ( 60 ) by plasma spraying thermoplastic particles from a plasma spray head ( 70 ) onto the surfaces of a fiber reinforced composite material ( 60 ), thereby forming the prepared prepreg ( 100 ).
  • the surface layer polymer coating may be the same or different on each side of the prepared prepreg ( 100 ).
  • Prepared tool ( 10 ) of the present invention incorporates a surface layer polymer coating ( 50 ) that is releasably adhered to the mold surface of a mold tool ( 20 ).
  • a release film ( 40 ) is interposed between the mold surface of the mold tool ( 20 ) and the surface layer polymer coating ( 50 ).
  • the mold surface of the mold tool ( 20 ) is a textured surface ( 30 ).
  • Prepared tool ( 10 ) may be utilized for laydown of fiber reinforced composite material by hand or by ATL as may be desired.
  • Prepared tool ( 10 ) provides optimal controlled adhesion of the first ply fiber reinforced composite material during either hand or ATL application.
  • FIG. 2 a illustrates laydown of a first ply fiber reinforced composite material ( 60 ) by automated tape laydown placement onto the mold surface of mold tool ( 20 ).
  • a plasma spray head ( 70 ) will spray thermoplastic particles onto the mold surface, forming the surface layer polymer coating ( 50 ) on the mold surface for preparation of the mold surface of mold tool ( 20 ).
  • an ATL laydown roller ( 80 ) lays down and releasably adheres the tape prepreg fiber reinforced composite material ( 60 ) onto the surface layer polymer coating ( 50 ) on the mold surface of the mold tool ( 20 ).
  • thermoplastic interlaminar layer ( 90 ) can provide beneficial toughening or other multifunctional benefits as desired.
  • Prepreg ( 100 ) of the present invention is prepared by applying a surface layer polymer coating ( 50 ) to one or both surfaces of a fiber reinforced composite material ( 60 ) directly before or during in situ laydown of the fiber reinforced composite material ( 60 ).
  • a flow of fiber reinforced composite material ( 60 ) is passed between one or more plasma spray heads ( 70 ) that apply surface layer polymer coating ( 50 ) to one or both sides of the composite material ( 60 ), thereby forming the prepared prepreg ( 100 ).
  • This prepared prepreg ( 100 ) can then be directly applied to a mold tool or a prepared tool ( 10 ) by hand laydown or by ATL as desired, and is releasably adhered to the mold surface of the mold tool or prepared tool ( 10 ).
  • Prepared prepreg ( 100 ) can be applied as a tape prepreg by an ATL laydown roller as shown in FIG. 2 a , without the need for a separate plasma spray head ( 70 ) for applying a first ply of fiber reinforced composite material having a surface layer polymer coating ( 50 ) adjacent to the mold surface of the mold tool ( 20 ).
  • the mold surface is preferably a textured mold surface ( 30 ).
  • Prepared prepreg ( 100 ) can save manufacturing costs and create more uniform manufacturing conditions while providing the same potential multifunctional benefits. If the surface layer polymer coating ( 50 ) is applied to both surfaces of a fiber reinforced composite material ( 60 ), the coating ( 50 ) on each surface can have the same or different compositions.
  • surface layer polymer coating ( 50 ) Various methods of applying surface layer polymer coating ( 50 ) are available and known in the art, such as by spraying a solvent based polymer solution onto the mold surface of a metal mold tool, by hand applying a water based slurry, by a plasma spray application, or an electrostatic powder coating and fusing method, among others.
  • One particularly preferred embodiment of the present invention provides for plasma spray application of the surface layer polymer onto the mold surface of a mold tool ( 20 ) forming a prepared tool ( 10 ) as illustrated in FIGS. 1 a and 1 b , or directly onto the fiber reinforced composite material ( 60 ) as depicted in FIG. 3 to form prepared prepreg ( 100 ).
  • the surface layer polymer coating ( 50 ) is applied using a plasma spray gun
  • the surface layer polymer is introduced to the plasma gun in the form of solid particles, preferably thermoplastic particles with a D 90 diameter (wherein ninety percent of the particles are smaller than the number, by volume) from 90 to 180 ⁇ m and more preferably from 150 to 185 ⁇ m.
  • the particles are applied using a low velocity, high temperature plasma.
  • a preferred high performance polymer surface layer polymer particle is PEEK polymer.
  • Surface layer polymer coating ( 50 ) is substantially continuous, but may be discontinuous at lower thickness levels along the mold surface, especially depending upon the level of roughness of textured surface ( 30 ) to which it is applied. It is desired to be continuous over at least 50% of the mold surface, and more preferably at least 90% of the mold surface and optimally, at least 98% of the mold surface.
  • a plasma spray head ( 70 ) to apply the surface layer polymer coating ( 50 )
  • the heated thermoplastic particles impact and adhere to the mold surface as molten particles and the resulting surface layer coating ( 50 ) can appear as a discontinuous plurality of beads that are well fused thermoplastic particles, but not all are melt fused together, forming the partially discontinuous film.
  • the high performance polymer particle size is D 90 of about 100 ⁇ m to about 400 ⁇ m.
  • the polymer particle sizes is in the D 90 range of from about 125 ⁇ m to about 250 ⁇ m, and most preferably from about 150 to about 200 ⁇ m for optimum plasma spray application results.
  • the high performance polymer particles are exposed to a plasma spray head temperature in the range of about 1800° F. to about 2000° F. at a velocity of about 350 to about 400 ⁇ m/second at the vent port nozzle section of the plasma spray applicator.
  • Useful commercially available plasma spray applicator include the Praxair SG 10 plasma spray applicator or a Sulzer Metco plasma spray applicator.
  • the high performance polymer is introduced into the plasma spray head as a solid particle.
  • the plasma spray applicator then directs the solid particles into the plasma jet stream to heat and accelerate the particles to a high velocity.
  • the mold tool ( 20 ) is pre-heated to about 250° F. (121° C.) to aid in adhering the surface layer polymer coating ( 50 ) to the mold surface of the mold tool ( 20 ).
  • plasma spraying should apply surface layer polymer coating ( 50 ) to the mold surface of the mold tool ( 20 ) at a thickness in the range from 0.001 to 0.010 inch thick layer.
  • the thickness of the surface layer polymer coating ( 50 ) is more preferably about 0.002 inches. This thickness is intended to aid in adhesion of the first ply without adding significant weight to the resulting composite part.
  • plasma spraying should apply a surface layer polymer coating ( 50 ) onto a fiber reinforced thermoplastic composite material ( 60 ) at a thickness of from about 0.0005 to about 0.010 inches per layer.
  • the thickness of the surface layer polymer can be from about 0.001 to about 0.008 inches per layer.
  • Surface layer polymer coating ( 50 ) can be releasably applied to the mold surface of mold tool ( 20 ) to allow effective release of the resulting composite part from the mold surface of the mold tool. While a difficulty with automated tape lay-down of thermoplastic fiber reinforced composite materials is ineffective adhesion of the first ply to the mold surface of the mold tool, the thermoplastic surface layer polymer coating should not adhere so strongly to the mold surface of the mold tool so that when removal is attempted, the thermoplastic surface layer polymer coating is compromised and the resulting thermoplastic composite part is damaged. This is especially important when the thermoplastic surface layer polymer coating contains any multi-functional agent such as described herein to further enhance the surface properties of the resulting thermoplastic composite part.
  • thermoplastic surface layer polymer coating is said to be releasably applied when the resulting thermoplastic composite part made on a mold tool with a thermoplastic surface layer polymer coating releases from the mold tool with slight to modest pressure, while the surface layer polymer coating does not detach during the automated in situ laydown of the thermoplastic fiber reinforced composite material.
  • thermoplastic surface layer polymer ( 50 ) on the mold surface of mold tool ( 20 ) can improve the surface quality and properties of the resulting thermoplastic composite part once it is removed from the mold tool due to the qualities of the resin rich thermoplastic surface layer polymer coating, the enhanced surface texture, and optional multi-functional additives which can be incorporated therein.
  • the surface layer polymer coating ( 50 ) can comprise a high performance polymer chosen from a slow crystallizing, semi-crystalline polymer or an amorphous polymer (or mixtures thereof), such that the thermoplastic surface layer polymer coating ( 50 ) forms a miscible and/or compatible blend with the high performance thermoplastic polymer of the fiber reinforced thermoplastic composite material ( 60 ).
  • the surface layer polymer coating ( 50 ) can be any one of the high performance thermoplastic polymers described herein that is applied to the mold surface of mold tool ( 20 ) for improved processing of first ply laydown as described herein or applied directly to one or both surfaces of thermoplastic fiber reinforced composite material ( 60 ) before application to the mold tool.
  • the morphology of the high performance thermoplastic polymer can be amorphous and/or a slow crystallizing (i.e., low crystallinity—typically less than 20% crystallinity) semi-crystalline polymer. Blends of amorphous and semi-crystalline polymers are also contemplated for use as the surface layer polymer coating ( 50 ).
  • the high performance thermoplastic polymer for thermoplastic surface layer polymer coating ( 50 ) is chosen from polyaryletherketones (PAEK), polyetherimide (PEI), polyimides, PAEK co-polymer with PEI and/or polyethersulfone (PES) and/or polyphenylenesulfide (PPS), and PAEK blends with one or more of PEI, PES, PPS and/or polyimides.
  • PAEK polyaryletherketones
  • PEI polyetherimide
  • PES polyethersulfone
  • PPS polyphenylenesulfide
  • thermoplastic surface layer polymer coating includes PAEK chosen from polyetheretherketone (PEEK) or polyetherketoneketone (PEKK) and blends with, such as, but not limited to, diphenylsulfone.
  • PAEK polyetheretherketone
  • PEKK polyetherketoneketone
  • the T:I ratio of the PEKK ranges from about 0:100 to about 70:30 in order to maintain the slow crystallization rate of the surface layer polymer.
  • the T:I ratio of the thermoplastic surface layer polymer uses CYPEK® DS that has a T:I ratio of from about 0:100 to about 70:30.
  • Suitable PEKK polymers available for use with the present invention include, but are not limited those commercially available from Cytec Industries Inc., Woodland Park N.J., such as CYPEK® DS-E or CYPEK® DS-M and CYPEK® HT.
  • the surface layer polymer coating ( 50 ) can further include one or more multi-functional agents chosen for improving the resulting thermoplastic composite part features, such as electrical conductivity, toughness, oxygen permeability, crystallization rate and/or solvent resistance of the resulting thermoplastic composite part.
  • multi-functional agents may be in the form of a metallic coating and/or micro- and/or nano-particles.
  • the optional surface layer polymer coating ( 50 ) multi-functional agents can include one or more of materials such as, but not limited to, impact modifiers, mold release agents, lubricants, thixotropes, antioxidants, UV absorbers, heat stabilizers, flame retardants, pigments, colorants, layered colorants for impact damage indicators, nonfibrous reinforcements and fillers, nano-graphite platelets, to enhance crystallinity rate and mitigate shrinkage, nano-clays to improve solvent resistance, nano-metals (such as nickel fibrils), particle interleaving for impact toughening, CVD veil fabrics in interleave for OML lightning strike, fiber or polymer veils to improve impact performance, surface finishes to aid in air removal as the pressure is applied by the ATL machine, and high flow surface coatings to speed reptation healing across the inter-ply region.
  • materials such as, but not limited to, impact modifiers, mold release agents, lubricants, thixotropes, antioxidants, UV absorbers, heat stabilizers, flame retardants, pigment
  • the mold tool ( 20 ) can be of any non-porous high temperature tooling including metal.
  • Metal tooling preferably stainless steel, invar or low carbon steel as known to one skilled in the art are all appropriate.
  • the mold surface of the mold tool ( 20 ) can be stainless steel able to withstand the high processing temperatures required for thermoplastic fiber reinforced composite part manufacturing and low CTE, but is preferably invar.
  • High temperature tooling is capable of withstanding processing temperatures up to 800° F. (427° C.).
  • Mold tool ( 20 ) can be a 0.120′′ thick 304 stainless steel plate or 0.063′′ invar 36 .
  • the stainless steel plate may not be as effective as invar due to higher differential CTE, which can cause delamination during processing of the thermoplastic fiber reinforced composite material from the mold surface of the mold tool.
  • the mold tool ( 20 ) should be a solid, impermeable material that is non-porous.
  • the mold tool ( 20 ) should not allow the flow of air or gases through its mold surface.
  • a textured mold surface ( 30 ) is preferably created on the mold surface of the mold tool ( 20 ) in order to improve mechanical adhesion of the surface layer polymer ( 50 ) to the mold tool ( 20 ) in an effort to overcome the CTE differential delaminating the thermoplastic fiber reinforced composite material ( 60 ) and surface layer polymer coating ( 50 ) from the mold surface of mold tool ( 20 ).
  • the textured mold surface ( 30 ) is believed to provide a mechanical interlock between the mold tool ( 20 ) and the surface layer polymer coating ( 50 ), as well as improve adhesion in order to overcome differences in coefficient of thermal expansion between the surface layer polymer coating ( 50 ) and the mold tool ( 20 ).
  • Too little texture and the mechanical interlock will be insufficient to overcome the CTE differential, resulting in the surface layer polymer coating ( 50 ) easily peeling off of the mold tool ( 20 ) during manufacture. Too course of textured mold surface ( 30 ) can result in a surface layer polymer coating ( 50 ) that can be difficult to release and remove without causing damage to the surface layer polymer coating ( 50 ) when trying to remove the resulting composite part from the mold tool.
  • the textured mold surface ( 30 ) cab be added by many means such as sandblasting, milling, Blanchard grinding, glass bead blasting, knurling, or other means to texture the mold surface to accept the release film ( 40 ). Creation of the textured mold surface ( 30 ) can be accomplished by a method such as sandblasting with a grit size from about 20 grit to about 180 grit, and more preferably 40 grit to 120 grit. In particular, about 120 grit aluminum oxide or about 40-60 grit glass beads provide an even texture on the surface and are preferred with the 40-60 grit glass beads being optimal. The preferred methods of applying an appropriate texture is by sandblasting with 120 grit aluminum oxide or 40-60 grit glass beads.
  • the appropriate texture for a particular combination of mold surface of a mold tool ( 20 ) and surface layer polymer coating ( 50 ) can be optimized by one skilled in the art to identify the most appropriate level of texture for a particular surface layer polymer coating ( 50 ) and mold tool ( 20 ).
  • One skilled in the art will be able to identify the most appropriate level of texture for the type of mold tool material and surface layer polymer coating material to overcome the CTE differences involved to support sufficient adhesion while maintaining releasability of the resulting composite part.
  • One method of quantifying an appropriate level of texture is by measuring the profile elements of a textured mold surface ( 30 ). Both a greater mean spacing of profile elements and greater depth of profile elements are appropriate methods of distinguishing preferred levels of texture. Both profile elements need to be appropriate for the texture to be appropriate.
  • the surface profilometer uses a diamond stylus that is moved at a controlled speed over the surface of the sample to detect characteristics of the material. These parameters are measured on a flat sample by resting the device on top of the sample. This is test is performed at standard room temperature and humidity and the mold tool tested should be at room temperature.
  • the profilometer is set onto the sample in the x-direction (defined as parallel to the edge of the test bench) and the test is begun using the play arrow key and all parameters are recorded for the X-direction.
  • the profilometer is then repositioned perpendicular to the previous test and the test is repeated to record all parameters for the Y-direction.
  • the mold release film ( 40 ) can be applied to the mold surface of mold tool ( 20 ) after applying textured mold surface ( 30 ) to the mold tool to evenly and uniformly cover the mold surface of the mold tool ( 20 ).
  • the mold release film ( 40 ) further provides the appropriate releasable adhesion of the surface layer polymer coating ( 50 ) to the mold surface of the mold tool ( 20 ).
  • the mold release film ( 40 ) may only partially cover the textured mold surface ( 30 ) of the mold tool ( 20 ), so long as it covers that recommended by the mold release manufacturer.
  • the mold release film ( 40 ) functions as an interface between the textured mold surface ( 30 ) of the mold tool ( 20 ) and the surface layer polymer coating ( 50 ).
  • the mold release film ( 40 ) also provides a chemical bonding to restrain the surface layer polymer coating ( 50 ) on the mold surface, thereby maintaining optimal adhesion and subsequent releasability of the surface layer polymer coating to the mold surface during application of the thermoplastic fiber reinforced composite material.
  • the mold release film ( 40 ) is also robust enough to survive the intense heat and conditions from the laydown process such that it provides a release layer to separate the surface layer polymer coating ( 50 ) from the mold tool ( 20 ) once the resulting composite part has been cured.
  • Mold release film materials are commercially available and are advertised as capable of releasing the product from a mold tool after processing. Suitable commercial mold release film include Hysol Frekote 800, AXEL 21RM, AXEL 21LS, and AXEL W-4005.
  • the release agent is preferably high temperature AXEL W-4005 applied and seasoned per the manufacturer's specifications.
  • the mold tool ( 20 ) together with the mold release film ( 40 ) can then be heated to “season” as recommended by the supplier.
  • a sealer can optionally be applied to the mold surface of mold tool ( 20 ) as recommended by the mold tool manufacturer prior to application of the mold release film ( 40 ) to further increase the releasable adhesion of the surface layer polymer coating ( 50 ) and allow release of the resulting composite part from the mold surface.
  • Fiber reinforced composite material ( 60 ) are structural reinforcement fiber materials, pre-impregnated with an appropriate high performance thermoplastic polymer matrix resin. These are generally categorized as tape, woven cloth, non-woven cloth, paper, and mixtures thereof.
  • Suitable structural reinforcement fibers for fiber reinforcement include any of the commercially available structural fibers such as carbon fibers, Kevlar® fibers, glass fibers, aramid fibers, and mixtures thereof.
  • the fibrous structural reinforcement fiber is a polyacrylonitrile (PAN) based carbon fiber.
  • the fibrous structural reinforcement can be configured in a unidirectional tape (uni-tape) web, non-woven mat or veil, fiber tow, or fabric material.
  • Tape prepreg generally refers to unidirectional structural reinforcement fibers that extend along a single axis of the strip material. Tape prepreg is generally used for ATL laydown applications.
  • the term “cloth” generally refers to structural reinforcement fibers laid along at least two different axes within the strip material. Cloth is commercially available as bi-axial, tri-axial and quad-axial, indicating fibers extending in two, three, or four different axes, respectively. The fibers may optionally be woven with one another, or may be manufactured as non-woven cloth. Cloth prepreg materials are generally used for hand laydown applications.
  • Fiber reinforced composite material ( 60 ) contains any of the fibrous structural reinforcement fiber described herein that has been impregnated with at least one high performance thermoplastic polymer via any manufacturing/impregnation method known to those of skill in the art. Suitable impregnation methods are known to those of ordinary skill in the art and include, for example and without limitation, hot-melt impregnation, aqueous slurry impregnation, powder coating, extrusion film lamination, and combinations thereof.
  • the high performance thermoplastic polymer for the surface layer coating ( 50 ) and the high performance thermoplastic polymer as the matrix resin for the fiber reinforced thermoplastic composite material ( 60 ) can be the same or different materials or combinations thereof.
  • high performance polymer is meant to refer to any thermoplastic polymer that has a melting temperature (Tm) greater than or equal to 280° C. and a process temperature (Tprocess) greater than or equal to 310° C.
  • Tm melting temperature
  • Tprocess process temperature
  • the higher performance polymer is chosen from polyaryletherketones (PAEK), PAEK blends, polyimides, and polyphenylenesulfides (PPS).
  • the PAEK is chosen from polyetheretherketone (PEEK), polyetheretherketoneketone (PEEKK), polyetherketoneketone (PEKK), polyetherketone (PEK), and polyetherketoneketoneetherketone (PEKKEK).
  • the high performance polymer is a PAEK blend having polyetherimide, polyphenylene sulfide and/or polyethersulfone mixed in with one or more polyaryletherketones.
  • Polyaryletherketones are well known to those skilled in the composite arts and include, but are not limited to, APC-2® PEEK, CYPEK®-FC and/or CYPEK®-HT, all commercially available from Cytec Industries Inc., Woodland Park, N.J.
  • Resin content of the high performance thermoplastic polymer resin in the fiber reinforced composite material ( 60 ) ranges from about 26% to about 90% by weight of the total thereby providing composite material ( 60 ) with a resin modulus of 500 ksi or greater and an interlaminar fracture toughness of 600 J/m 2 or greater as measure by G 1c .
  • the viscosity of the high performance polymer is adjusted so that good filament wet out is obtained.
  • the high performance polymer of the fiber reinforced composite material acts as part of a polymer matrix and forms a polymer blend with the surface layer polymer coating ( 50 ) when the materials are contacted.
  • polymer blend includes miscible and compatible polymer blends as those terms are known and understood by those skilled in the art to which the invention pertains.
  • thermoplastic composite parts formed by the present invention can be various articles formed using rapid lamination and forming processes including, but not limited to, in situ thermoplastic tape/tow placement for stiffened wing and fuselage skins, continuous compression molding (CCM) and roll forming process for stiffener fabrication, double belt press to make consolidated flat panels and aircraft floor panels, in situ filament wound cylindrical structures, and fusion bonding and welding of composite assembly.
  • CCM continuous compression molding
  • a formulation of PEI polymer, GE Ultem 1000P at 10% plus Dioxilane at 90% was plasma sprayed onto the mold surface of a steel mold tool which had a release film using an HVLP applicator.
  • an 8 ply quasi-isotropic panel was created using APC PEKK/AS-4 uni-tape material.
  • the panel was processed with a caul plate at an autoclave temperature of 720° F. (382° C.) and 100 psi of N 2 .
  • the panel showed some surface anomalies on the coated face.
  • a direct hand application technique was attempted using a mixture that included surfactant, water, hydrosize (sizing) and thermoplastic, as follows: 1) Sizing 90%/PEKK 10%. 2) D.I water 80%/Surfactant 10%/PEI-Diox. Premix solution 10%. 3) D.I water 80%/Surfactant 10%/PEKK 10%. 4) Sizing 80%/PEI powder 10%/Surfactant 10%).
  • the resulting water based slurry thermoplastic surface layer polymer coating shrank rapidly on the mold surface of the mold tool and did not achieve adequate bonding onto metal mold tool. The surface layer polymer coating flaked off very easily with minimum abrasion.
  • a plasma spray coating was performed using a Praxair SG 100 plasma gun and introduced PEK polymer into the jet stream to heat and accelerate the material to high velocity.
  • PEK polymer Initially there was difficulty maintaining adhesion between the sealed/released tool and the PEK polymer, when the tool was allowed to cool to room temperature, likely caused by the difference in CTE (coefficient of thermal expansion) of the mold tool and the thermoplastic surface layer polymer coating on the smooth mold surface of the mold tool. It appeared that the skin coating released from the tool (Hysol® Frekote® GP sealer agent and release agent Frekote® 800).
  • the resulting panels showed some uneven surface texture and surface layer polymer coating thickness. Some areas of the surface coating could be scraped off the resulting thermoplastic fiber reinforced composite part.
  • the mold surface of the mold tool was clean after the autoclave cycle, indicating the mold release was effective.
  • Plasma spraying was also conducted on APC-uni-tape samples to provide a path to adding material to the outside of a thermoplastic material. Two coated weights were deposited to test the process control. Only one side of the tape was coated. Transverse resin shrinkage and wrinkling of the tape was noted.
  • Metal alloy coatings may provide improved electrical conductivity for lightning strike and edge glow reduction.
  • Thermoplastic composite parts are processed at high temperatures and require stable tooling materials.
  • the processing cycle for PEKK-FC uni-tape panels exceeds 730° F. (388° C.) which necessitates steel alloy tooling.
  • the tooling was 0.120′′ thick 304 stainless steel plate.
  • the default smooth panel was a 0.125′′ thick stainless steel plate that had been sanded with 120 grit sandpaper and solvent cleaned.
  • the textured surface treatments used included 120 grit aluminum oxide and 40-60 c grit glass bead blasting. These surfaces increased the mechanical locking of the first-ply coating to the release-coated material. It is believed that the surface also broke up the resin film by creating thick and thin areas that reduce the effect of the resin shrinkage on tool adhesion.
  • the glass-bead blasted tool is recommended for plasma spraying but had not yet been tried.
  • the benefit of the texture is that it aids retention of the coating during processing.
  • Zyvax Sealer GP was initially used to seal the stainless plates. This was found to interact with the Frekote® 800 to produce a surface with an exceptionally easy release. This causes premature slip of the coating on the tool. After this was discovered, the sealer was mechanically removed from all surfaces and discontinued.
  • the first mold release evaluated was Hysol® Frekote® 800. This solvent-based system is known to offer release at processing temperatures above 400° C. The release was wiped onto the stainless steel surface and allowed to air dry, and then the tools were plasma sprayed with thermoplastic. Initial coating used the PEI/dioxilane spray and showed a tendency to peel off the tool with minimal abrasion. Kant-Stik Cure-Fast mold release was then tried and was also found to have an easy-release surface. This release has proven difficult to process above 750° F. (399° C.).
  • AXEL 21RM mold release was then used without a sealer and appeared to have a “tighter” surface than any of the previous releases. It is a solvent-based system.
  • the Axel 21RM is the preferred available release for this application. It works without a sealer to provide good surface adhesion without being too slippery.
  • a water-based version, W4005 was also tried to compare to the AXEL 21RM, but found to be sensitive to abrasion with small “marbles” of release evident after some finger abrasion of the tool.
  • the tools were heated to the use temperature (735° F., 391° C.) to season the release onto the tool. Seasoning the tool allows the release to be cured onto the tool before entering service. This step was included to prevent solvent from the first ply laydown using the PEI/dioxilane solution from lifting the mold release film.
  • a plasma spray coating was performed using a plasma gun and introduced PEK polymer into the jet stream to heat and accelerate the material to high velocity.
  • the PEK polymer is fed to the plasma gun using a fluidized bed feeder system.
  • the tool was pre-heated to 250° F. (121° C.) to aid in adhering the polymer to the surface of the tool.
  • a Praxair SG 100 plasma gun was used to deposit approximately 2 mils of PEK polymer on to the tool. This temporarily deposits the powder onto the tool.
  • the stainless steel tools with the powder coating were then processed in an electric furnace at 750° F. (399° C.) to melt the polymer and create a melted polymer layer.
  • a subsequent panel was sandblasted using 120 grit aluminum oxide and release coated with Hysol® Frekote® 800.
  • a picture frame of tape was placed on the tool to create a rough center panel and a smooth perimeter. This picture frame was intended to show the effect of surface roughness transitions on the first ply lay-down materials. This also provides a smooth area for masking off tool overspray.
  • an 8-ply quasiisotropic panel was created using APC PEKK/AS-4 uni-tape material.
  • the panel was processed with a caul plate at an autoclave temperature of 720° F. (382° C.) and 100 psi of N 2 .
  • the resulting panel showed somewhat un-even texture and coating thickness.
  • the coated tool surfaces were clean after the autoclave cycle, indicating the mold release was effective.
  • a small press was heated to between 290° C. and 410° C.
  • Kapton film is coated with a release agent and, with the press at the desired temperature; a bi- or tri-layer configuration is sandwiched between two pieces of the release agent coated Kapton film, thereby forming a lay-up.
  • the lay-up is placed between the two 3′′ ⁇ 3′′ stainless steel caul plates of the press along with a thermocouple.
  • the stack is inserted into the press and 1,000 pounds of pressure is applied and held for a period of from 10 to 30 seconds. The pressure and top plate is then released and the stack is removed to cool under a cold press (1000 lbs. for 1 minute).

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Coating Of Shaped Articles Made Of Macromolecular Substances (AREA)
  • Reinforced Plastic Materials (AREA)
US14/057,254 2012-10-18 2013-10-18 Surface Engineering of Thermoplastic Materials and Tooling Abandoned US20140110633A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US14/057,254 US20140110633A1 (en) 2012-10-18 2013-10-18 Surface Engineering of Thermoplastic Materials and Tooling
US15/045,650 US11214019B2 (en) 2012-10-18 2016-02-17 Surface engineering of thermoplastic materials and tooling

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261715438P 2012-10-18 2012-10-18
US14/057,254 US20140110633A1 (en) 2012-10-18 2013-10-18 Surface Engineering of Thermoplastic Materials and Tooling

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US15/045,650 Division US11214019B2 (en) 2012-10-18 2016-02-17 Surface engineering of thermoplastic materials and tooling

Publications (1)

Publication Number Publication Date
US20140110633A1 true US20140110633A1 (en) 2014-04-24

Family

ID=49546614

Family Applications (2)

Application Number Title Priority Date Filing Date
US14/057,254 Abandoned US20140110633A1 (en) 2012-10-18 2013-10-18 Surface Engineering of Thermoplastic Materials and Tooling
US15/045,650 Active 2036-02-22 US11214019B2 (en) 2012-10-18 2016-02-17 Surface engineering of thermoplastic materials and tooling

Family Applications After (1)

Application Number Title Priority Date Filing Date
US15/045,650 Active 2036-02-22 US11214019B2 (en) 2012-10-18 2016-02-17 Surface engineering of thermoplastic materials and tooling

Country Status (14)

Country Link
US (2) US20140110633A1 (fr)
EP (1) EP2909011B1 (fr)
JP (2) JP2015534913A (fr)
KR (1) KR102085024B1 (fr)
CN (1) CN104736328B (fr)
AU (1) AU2013331261B2 (fr)
BR (1) BR112015008752B1 (fr)
CA (1) CA2888615C (fr)
ES (1) ES2859507T3 (fr)
MX (1) MX2015004899A (fr)
MY (1) MY183181A (fr)
RU (1) RU2622306C2 (fr)
TW (1) TWI596010B (fr)
WO (1) WO2014062900A1 (fr)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140335216A1 (en) * 2011-08-19 2014-11-13 Sueddekor Gmbh Strip-shaped mold cavity for producing surface materials and method for producing a strip-shaped mold cavity
US20150282358A1 (en) * 2014-03-28 2015-10-01 Mark E. Sprenger Composite chassis with cosmetic finish
US20160076552A1 (en) * 2014-09-16 2016-03-17 General Electric Company Composite airfoil structures
JP2016049760A (ja) * 2014-09-02 2016-04-11 日産自動車株式会社 複合材料の成形方法および成形装置
DE102015113686A1 (de) 2014-12-23 2016-06-23 East-4D Carbon Technology Gmbh Verfahren und Vorrichtung zur Herstellung zylinderförmiger Faserverbundkörpern mit sprunghaften Änderungen ihres Profils entlang der Längsachse
US20160243806A1 (en) * 2015-02-19 2016-08-25 Rohr, Inc. Method for manufacturing a nacelle strake
WO2017051081A1 (fr) * 2015-09-25 2017-03-30 Coriolis Composites Procédé de réalisation de pièces métalliques renforcées de fibres thermoplastiques continues
WO2017079103A1 (fr) * 2015-11-02 2017-05-11 Toho Tenax America, Inc. Procédé de traitement par fusion in-situ de composite thermoplastique pour outils enveloppés de composite
US20170341312A1 (en) * 2016-05-25 2017-11-30 Airbus Helicopters Method and a thermoplastic blade
CN108794786A (zh) * 2017-05-01 2018-11-13 波音公司 用热塑性薄膜涂层固化的复合材料
DE102017009986A1 (de) * 2017-10-26 2019-05-02 Senvion Gmbh Herstellungsvorrichtung und Herstellungsverfahren für ein Verbund-Bauteil
EP3505260A1 (fr) * 2017-12-28 2019-07-03 RAantec GmbH & Co.KG Procédé et dispositif de scellement d'une fente d'assemblage
US11027856B2 (en) 2015-11-30 2021-06-08 Cytec Industries Inc. Surfacing materials for composite structures
US11065827B2 (en) * 2015-11-02 2021-07-20 Teijin Carbon America, Inc. Thermoplastic composite in-situ melt processing method for composite overwrapped tools
US11254048B2 (en) * 2017-02-21 2022-02-22 Kansas State University Research Foundation Additive manufacturing of continuous fiber thermoplastic composites
CN116552024A (zh) * 2023-06-29 2023-08-08 东莞市聚力复合材料科技有限公司 一种高强度轻量化的机械臂及其制造工艺与制造模具
US11745468B2 (en) 2016-09-27 2023-09-05 3M Innovative Properties Company Protection film
FR3142119A1 (fr) * 2022-11-17 2024-05-24 Safran Piece en materiau composite et son procede de fabrication
US12043003B2 (en) 2022-01-18 2024-07-23 Rohr, Inc. Assemblies and methods for forming fiber reinforced thermoplastic structures
US12115738B2 (en) 2022-01-18 2024-10-15 Rohr, Inc. Assemblies and methods for forming fiber-reinforced thermoplastic structures with lightning strike protection

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2725922C2 (ru) * 2015-08-24 2020-07-07 Сайтек Индастриз Инк. Композитный материал и композиция смолы, содержащая метастабильные частицы
US10906211B2 (en) * 2015-12-22 2021-02-02 Cytec Industries Inc. Mold-releasable surfacing materials for composite parts
EP3397489B1 (fr) * 2015-12-30 2022-02-09 Cytec Industries Inc. Particules de polymère traitées en surface, bouillie comprenant les particules, et leur utilisation
US20180029317A1 (en) * 2016-07-26 2018-02-01 The Boeing Company Metal-modified, plasma-treated thermoplastics for improved electrical performance
GB201620227D0 (en) * 2016-11-29 2017-01-11 Cytec Ind Inc Automated fabrication of fibrous preform
CN110325355A (zh) * 2017-02-26 2019-10-11 陶氏环球技术有限责任公司 具有降低的表面粗糙度的纤维复合材料及其制造方法
JP6884650B2 (ja) * 2017-06-22 2021-06-09 三菱重工業株式会社 複合材構造物の製造方法
FR3071184B1 (fr) * 2017-09-18 2021-11-19 Arkema France Procede d'impregnation de fibres de renfort avec des polyarylethercetones et semi-produits ainsi obtenus
US11147749B2 (en) 2017-10-04 2021-10-19 Mana Products, Inc. Dry composition for removing oils from hair and methods for fabrication of dry compositions
DE102018201902A1 (de) 2018-02-07 2019-08-08 Ford Global Technologies, Llc Vorrichtung und Verfahren zur Serienfertigung von zumindest teilweise faserverstärkten Spritzgussbauteilen
EP3873401A4 (fr) * 2018-10-31 2022-10-19 George Lambridis Composition sèche pour éliminer des huiles de cheveux et procédés de fabrication de compositions sèches
WO2020178949A1 (fr) * 2019-03-04 2020-09-10 日本飛行機株式会社 Support de gabarit
EP4130106A4 (fr) * 2020-03-24 2023-12-13 Mitsubishi Chemical Corporation Matériau composite renforcé par des fibres et corps lié
CN112812351B (zh) * 2021-02-23 2022-06-10 吉林大学 一种连续纤维增强结晶性聚芳醚酮树脂基单向带预浸料、制备方法及其应用
CN113715382A (zh) * 2021-09-01 2021-11-30 中山市富达运动器材有限公司 一种运动鞋底复合成型工艺
FR3132459B1 (fr) * 2022-02-10 2023-12-29 Coriolis Group Procédé de réalisation d’une pièce en matériau thermoplastique

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110097575A1 (en) * 2009-09-24 2011-04-28 Cytec Technology Corp. Thermoplastic Composites and Methods of Making and Using Same

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5539663B2 (fr) 1972-05-23 1980-10-13
GB1596793A (en) * 1977-06-28 1981-08-26 Secr Defence Laminating apparatus
US4132755A (en) 1977-07-22 1979-01-02 Jay Johnson Process for manufacturing resin-impregnated, reinforced articles without the presence of resin fumes
US4559262A (en) 1981-01-21 1985-12-17 Imperial Chemical Industries, Plc Fibre reinforced compositions and methods for producing such compositions
US4549920A (en) 1981-07-28 1985-10-29 Imperial Chemical Industries, Plc Method for impregnating filaments with thermoplastic
US4792481A (en) 1986-11-28 1988-12-20 Phillips Petroleum Company Reinforced plastic
US4883552A (en) 1986-12-05 1989-11-28 Phillips Petroleum Company Pultrusion process and apparatus
EP0274899B1 (fr) * 1986-12-25 1994-02-09 Toray Industries, Inc. Matériaux composites tenaces
US5094883A (en) 1989-04-17 1992-03-10 Georgia Tech Research Corporation Flexible multiply towpreg and method of production therefor
US5589249A (en) * 1993-01-08 1996-12-31 Poly-Bond, Inc. Medical composite with discontinuous adhesive structure
US6027794A (en) * 1993-01-14 2000-02-22 Toray Industries, Inc. Prepregs, processes for their production, and composite laminates
DE4325260A1 (de) 1993-07-28 1995-02-02 Hoechst Ag Verfahren zur Herstellung faserverstärkter Verbundwerkstoffe
EP0661147B1 (fr) 1993-12-29 1999-09-15 Toho Rayon Co., Ltd. Procédé et appareil pour la fabrication d'un objet cylindrique en matériau composite fibreux
JP2772388B2 (ja) * 1994-09-08 1998-07-02 東邦レーヨン株式会社 繊維強化熱可塑性樹脂パイプの製造方法および製造装置
JPH08258165A (ja) * 1995-03-27 1996-10-08 Daiwa Seiko Inc 管状体とその製造方法
DE69532142T2 (de) 1994-12-06 2004-04-15 Daiwa Seiko, Inc., Higashikurume Rohrförmige Substanz und Verfahren zur seiner Herstellung
US5958325A (en) 1995-06-07 1999-09-28 Tpi Technology, Inc. Large composite structures and a method for production of large composite structures incorporating a resin distribution network
ATE236772T1 (de) 1998-02-20 2003-04-15 Arova Schaffhausen Ag Herstellung von unidirektional faserverstärkten thermoplasten
US6174405B1 (en) * 1998-09-11 2001-01-16 Northrop Grumman Corporation Liquid crystal polymer in situ coating for co-cured composite structure
US6203404B1 (en) 1999-06-03 2001-03-20 Micron Technology, Inc. Chemical mechanical polishing methods
US20040234707A1 (en) * 2003-05-23 2004-11-25 Dimarzio Don Method of multi-axial crystalline thermoplastic coating of composite structures
US6974606B2 (en) * 2003-05-23 2005-12-13 Northrop Grumman Corporation Thermoplastic coating for composite structures
WO2005033393A1 (fr) * 2003-09-30 2005-04-14 Fabrics Technologies Llc Materiaux composites thermoplastiques renforces par des fibres et leur procede de fabrication
US8865042B2 (en) * 2006-05-02 2014-10-21 Mitsubishi Engineering-Plastics Corporation Mold for thermoplastic resin molding, cavity mold, and process for producing the cavity mold
JP5076996B2 (ja) * 2008-03-19 2012-11-21 オムロンヘルスケア株式会社 血圧情報測定装置
GB0807398D0 (en) 2008-04-23 2008-05-28 Airbus Uk Ltd Improved method of tape laying of thermoplastic composite materials
CN105295025A (zh) * 2009-02-05 2016-02-03 阿科玛股份有限公司 包含聚醚酮酮结系层的组件
WO2011117314A2 (fr) 2010-03-24 2011-09-29 Limo Patentverwaltung Gmbh & Co. Kg Dispositif de soumission à l'action d'un faisceau laser ainsi que dispositif pour reproduire une répartition de lumière en forme de ligne
ES2378129B1 (es) * 2010-04-30 2013-03-25 Airbus Operations, S.L. Proceso de aplicación de resina sobre una superficie tratada con sustancias desmoldeantes de un útil base de moldeo para obtener cuerpos de material compuesto.
CA2845504A1 (fr) * 2011-08-29 2013-03-07 Cytec Technology Corp. Trempe interlaminaire de thermoplastiques

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110097575A1 (en) * 2009-09-24 2011-04-28 Cytec Technology Corp. Thermoplastic Composites and Methods of Making and Using Same

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140335216A1 (en) * 2011-08-19 2014-11-13 Sueddekor Gmbh Strip-shaped mold cavity for producing surface materials and method for producing a strip-shaped mold cavity
US20150282358A1 (en) * 2014-03-28 2015-10-01 Mark E. Sprenger Composite chassis with cosmetic finish
JP2016049760A (ja) * 2014-09-02 2016-04-11 日産自動車株式会社 複合材料の成形方法および成形装置
US20160076552A1 (en) * 2014-09-16 2016-03-17 General Electric Company Composite airfoil structures
US10099434B2 (en) * 2014-09-16 2018-10-16 General Electric Company Composite airfoil structures
DE102015113686A1 (de) 2014-12-23 2016-06-23 East-4D Carbon Technology Gmbh Verfahren und Vorrichtung zur Herstellung zylinderförmiger Faserverbundkörpern mit sprunghaften Änderungen ihres Profils entlang der Längsachse
DE102015113686B4 (de) 2014-12-23 2023-01-05 East-4D Carbon Technology Gmbh Verfahren und Vorrichtung zur Herstellung von zylinderförmigen Faserverbundkörpern mit sprunghaften Änderungen ihres Profils entlang der Längsachse
US9937998B2 (en) * 2015-02-19 2018-04-10 Rohr, Inc. Method for manufacturing a nacelle strake
US20160243806A1 (en) * 2015-02-19 2016-08-25 Rohr, Inc. Method for manufacturing a nacelle strake
FR3041660A1 (fr) * 2015-09-25 2017-03-31 Coriolis Composites Procede de realisation de pieces metalliques renforcees de fibres thermoplastiques continues
WO2017051081A1 (fr) * 2015-09-25 2017-03-30 Coriolis Composites Procédé de réalisation de pièces métalliques renforcées de fibres thermoplastiques continues
US11738522B2 (en) 2015-11-02 2023-08-29 Teijin Carbon America, Inc. Thermoplastic composite in-situ melt processing method for composite overwrapped tools
WO2017079103A1 (fr) * 2015-11-02 2017-05-11 Toho Tenax America, Inc. Procédé de traitement par fusion in-situ de composite thermoplastique pour outils enveloppés de composite
EP3370956A4 (fr) * 2015-11-02 2019-07-10 Teijin Carbon America, Inc. Procédé de traitement par fusion in-situ de composite thermoplastique pour outils enveloppés de composite
US11065827B2 (en) * 2015-11-02 2021-07-20 Teijin Carbon America, Inc. Thermoplastic composite in-situ melt processing method for composite overwrapped tools
US11027856B2 (en) 2015-11-30 2021-06-08 Cytec Industries Inc. Surfacing materials for composite structures
US20170341312A1 (en) * 2016-05-25 2017-11-30 Airbus Helicopters Method and a thermoplastic blade
US10654225B2 (en) * 2016-05-25 2020-05-19 Airbus Helicopters Method and a thermoplastic blade
US11745468B2 (en) 2016-09-27 2023-09-05 3M Innovative Properties Company Protection film
US11254048B2 (en) * 2017-02-21 2022-02-22 Kansas State University Research Foundation Additive manufacturing of continuous fiber thermoplastic composites
US11260423B2 (en) 2017-05-01 2022-03-01 The Boeing Company Composite materials cured with thermoplastic thin film coating
CN108794786A (zh) * 2017-05-01 2018-11-13 波音公司 用热塑性薄膜涂层固化的复合材料
DE102017009986A1 (de) * 2017-10-26 2019-05-02 Senvion Gmbh Herstellungsvorrichtung und Herstellungsverfahren für ein Verbund-Bauteil
EP3505260A1 (fr) * 2017-12-28 2019-07-03 RAantec GmbH & Co.KG Procédé et dispositif de scellement d'une fente d'assemblage
US12043003B2 (en) 2022-01-18 2024-07-23 Rohr, Inc. Assemblies and methods for forming fiber reinforced thermoplastic structures
US12115738B2 (en) 2022-01-18 2024-10-15 Rohr, Inc. Assemblies and methods for forming fiber-reinforced thermoplastic structures with lightning strike protection
FR3142119A1 (fr) * 2022-11-17 2024-05-24 Safran Piece en materiau composite et son procede de fabrication
CN116552024A (zh) * 2023-06-29 2023-08-08 东莞市聚力复合材料科技有限公司 一种高强度轻量化的机械臂及其制造工艺与制造模具

Also Published As

Publication number Publication date
WO2014062900A1 (fr) 2014-04-24
TW201422435A (zh) 2014-06-16
EP2909011B1 (fr) 2021-01-20
KR20150074056A (ko) 2015-07-01
ES2859507T3 (es) 2021-10-04
CA2888615A1 (fr) 2014-04-24
CN104736328A (zh) 2015-06-24
CN104736328B (zh) 2017-06-13
CA2888615C (fr) 2020-03-31
BR112015008752B1 (pt) 2021-02-23
MX2015004899A (es) 2015-10-29
US20160221223A1 (en) 2016-08-04
EP2909011A1 (fr) 2015-08-26
JP2015534913A (ja) 2015-12-07
TWI596010B (zh) 2017-08-21
KR102085024B1 (ko) 2020-03-05
RU2015118348A (ru) 2016-12-10
BR112015008752A2 (pt) 2017-07-04
MY183181A (en) 2021-02-18
JP6387142B2 (ja) 2018-09-05
JP2017159660A (ja) 2017-09-14
US11214019B2 (en) 2022-01-04
AU2013331261B2 (en) 2017-10-19
AU2013331261A1 (en) 2015-04-30
RU2622306C2 (ru) 2017-06-14

Similar Documents

Publication Publication Date Title
US11214019B2 (en) Surface engineering of thermoplastic materials and tooling
CA2775053C (fr) Composites thermoplastiques et procedes pour leur realisation et leur utilisation
EP2804894B1 (fr) Pré-imprégné intervenant dans la fabrication de matériaux composites
AU761069C (en) Moulding materials
JPWO2013115337A1 (ja) ランダムマットおよび繊維強化複合材料
JPWO2018147331A1 (ja) 繊維強化樹脂シート
AU2010298260B2 (en) Thermoplastic composites and methods of making and using same
JP2023021876A (ja) 熱可塑性樹脂プリプレグ、及びその製造方法
WO2019148084A1 (fr) Agent poisseux pour procédés de famille d'infusion de résine

Legal Events

Date Code Title Description
AS Assignment

Owner name: CYTEC INDUSTRIES INC., CONNECTICUT

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:PRATTE, JAMES FRANCIS;ROGERS, SCOTT ALFRED;SIGNING DATES FROM 20140206 TO 20140211;REEL/FRAME:032220/0074

AS Assignment

Owner name: CYTEC INDUSTRIES INC., NEW JERSEY

Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE RECEIVING PARTY DATA PREVIOUSLY RECORDED ON REEL 032220 FRAME 0074. ASSIGNOR(S) HEREBY CONFIRMS THE CYTEC INDUSTRIES INC. 5 GARRET MOUNTAIN PLAZA WOODLAND PARK, NEW JERSEY 07424;ASSIGNORS:PRATTE, JAMES FRANCIS;ROGERS, SCOTT ALFRED;SIGNING DATES FROM 20140206 TO 20140211;REEL/FRAME:032265/0798

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION