EP0204793A1 - A method of making complex shapes from flat fibre reinforced thermoplastics material composites - Google Patents

A method of making complex shapes from flat fibre reinforced thermoplastics material composites

Info

Publication number
EP0204793A1
EP0204793A1 EP86900180A EP86900180A EP0204793A1 EP 0204793 A1 EP0204793 A1 EP 0204793A1 EP 86900180 A EP86900180 A EP 86900180A EP 86900180 A EP86900180 A EP 86900180A EP 0204793 A1 EP0204793 A1 EP 0204793A1
Authority
EP
European Patent Office
Prior art keywords
sheets
fibres
temperature
thermoplastics material
metal mesh
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP86900180A
Other languages
German (de)
French (fr)
Inventor
Thomas Glenville Doe
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.)
HR Smith Technical Developments Ltd
Original Assignee
HR Smith Technical Developments Ltd
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 HR Smith Technical Developments Ltd filed Critical HR Smith Technical Developments Ltd
Publication of EP0204793A1 publication Critical patent/EP0204793A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0003Producing profiled members, e.g. beams
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3404Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
    • B29C65/344Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint being a woven or non-woven fabric or being a mesh
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • B29C66/438Joining sheets for making hollow-walled, channelled structures or multi-tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/524Joining profiled elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00Producing articles with hollow walls
    • B29D24/002Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/004Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having vertical or oblique ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3468Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the means for supplying heat to said heated elements which remain in the join, e.g. special electrical connectors of windings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3472Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint
    • B29C65/3476Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being metallic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114Single butt joints
    • B29C66/1142Single butt to butt joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/54Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7212Fibre-reinforced materials characterised by the composition of the fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7311Thermal properties
    • B29C66/73117Tg, i.e. glass transition temperature
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/92Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools
    • B29C66/929Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools characterized by specific pressure, force, mechanical power or displacement values or ranges
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2071/00Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2077/00Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2081/00Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2101/00Use of unspecified macromolecular compounds as moulding material
    • B29K2101/12Thermoplastic materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25Solid
    • B29K2105/253Preform
    • B29K2105/256Sheets, plates, blanks or films
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00Layered products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00Articles with hollow walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/001Profiled members, e.g. beams, sections
    • B29L2031/003Profiled members, e.g. beams, sections having a profiled transverse cross-section

Definitions

  • the invention concerns the manufacture of complex shaped structures in fibres reinforced high or low tempe ⁇ rature thermoplastics material.
  • fibres reinforcement encompasses fibres in the form of filaments or tows of filaments, mats of filaments or tows of filaments and cloths made,e.g. by laying up, knitting or weaving, filaments or tows of filaments.
  • thermoplastics materials with or without fibres reinforcement
  • various methods of making them have been proposed.
  • the methods involve matching tools with high temperature and pressure to consolidate the materials in, for example film stacking processes; in which layers of fibres reinforce ⁇ ments (which may or may not be pre-impregnated with the polymer material) are laid up in the mould and one or more layers of the polymer material in sheet form are interposed, if needed, between adjacent ones of the sheets of fibres reinforcements.
  • the fibres are relatively inex- tensible and incompressible and the sheet material containing them cannot be shaped in this way - unless the fibres of the fibres reinforcement extend uni-directionally within the matrix material and the axis of the fold or bend (the axis about which the bend or fold is formed) extends in a direc ⁇ tion parallel to the direction in which the fibres in the fibres reinforcement extend.
  • the invention proposes a novel way of overcoming this problem in thermoplastics materials reinforced with non- unidirectionally arrayed fibres reinforcement and which may with advantage be used in bending or folding thermoplastics materials reinforced with a unidirectionally arrayed fibre reinforcement on an axis not parallel to the direction in which the fibres extend.
  • a first aspect of the invention provides a method of making a complex shaped fibre reinforced thermoplastics material structure in which: a flat sheet of fibres rein- forced thermoplastics material is locally heated to a tem ⁇ perature at which the polymer material therein is plasticised, the sheet thereafter being manipulated so that it is bent or folded at the area at which it was heated with ones of said fibres of said reinforcement extending about the axis of the said bend within the outermost layer of said fibres reinforcement remaining intact and forming, with said polymer material a bead extending along the length of said bend or fold.
  • thermo- plastics matrix material e.g. low temperature thermoplastics materials such as polystyrene
  • high temperature aromatic polymer material materials such as polysulphone, polyethersulphone, polyetheretherketone, a polyamide or the like.
  • the fibres reinforcement may with advantage be of glass, carbon or quartz and the fibres therein may be multi- directionally disposed or uni-directionally disposed and extending in a direction about the axis of the said bend or fold.
  • a second aspect of the invention provides method of making a complex shaped thermoplastics material article formed by joining pre-shaped sheets made in accordance with the above noted first aspect of the invention with other similarly pre-shaped sheets and/or flat sheets.
  • the sheets to be joined are locally heated in the areas at which they are to be joined whilst being held in abutment until those areas are plasticised and then holding those areas together as the sheets cool to a temperature below the glass 5 transition temperature of the thermoplastics matrix material
  • One method in accordance with the second aspect of the invention provides that the local heating is effected by platens held in contact with one or both sides of the sheets to be conjoined.
  • An alternative method in. accordance with the second aspect of the invention provides that the local heating is effected by interposing resistive metal mesh between the areas of the sheets held in abutment and passing to that metal mesh an electric current sufficient to raise the tem- 5 perature thereof above the glass transition temperature of the thermoplastics material being used, after cooling the metal mesh being trimmed such that the portion of the metal mesh left in the complex structure becomes an integral part thereof.
  • a third aspect of the invention provides a complex shaped fibres reinforced thermoplastics material structure made in accordance with the first and second aspects noted above.
  • Figure 1 schematically shows at A an end view, and at B a side view of apparatus used in the method of the invention
  • Figure 2 illustrates schematically the bending of a fibres reinforced plastics material in accordance with the invention.
  • Figure 3 schematically shows an alternative form of the apparatus illustrated in Figure 1 .
  • FIGS 4 to 7 schematically illustrate ways of making various other complex shapes embodying the invention.
  • Figure 1 shows at 10 an electrically resistive heating element coupled via a switch 12 to a low voltage/high current source 14 (such as an arc-welding transformer) by means of which, when switch 12 is closed, element 10 may be heated to a temperature at which the polymer material in a fibres reinforced flat sheet 16 to be worked is plasticised
  • a low voltage/high current source 14 such as an arc-welding transformer
  • One side 18 of the fibres reinforced material sheet 16 is, in accordance with the invention, brought into close proximity - but not into contact - with the element 10. After a time, dependent upon the polymer material and the ⁇
  • the sheet 6 is reversed so that the side 20 thereof is brought into proximity with the element 10 and heated.
  • the sheet 16 may be supported, if desired, on a rigid platform such as shown at 22.
  • thermoplastic material of sheet 16 adjacent the element 10 has been heated to a temperature at which it is plasticised.
  • the material may be folded or bent about an axis C so that its inner surface, e.g. surface 20 is raised to form a bead or roll 24 on the 'inside' of the fold.
  • the sheet 16 is removed from proximity with element 10 (if necessary being held to retain the shape that has been imparted to it) and allowed to cool to a temperature below its glass transition temperature. Further bends may be formed in the sheet material if desired.
  • the longitu dinal fibres are relatively unaffected by the manipulation and retain the restrictive effect they have on the lateral fibres; the outermost ones of which are merely bent and not stretched whilst those within the outermost layer are all to some extent bent in a sense opposite to that of the bend which has been formed in sheet 16 - the inner- most ones of the lateral fibres in the reinforcement forming a loop which with the polymer material forms the bead or roll 24.
  • the heating element 10 is replaced with two heating elements 26 disposed on either side of the sheet 16 enabling both of its surfaces 18 and 20 to be heated at the same time.
  • the ele ⁇ ments 26 may be coupled to the power supply 14 by a single switch (as described with reference to Figure 1 ) or by two switches 28 as shown in Figure 3. It is thought that such an arrangement has particular advantage when there is a need for the process to be performed relatively quickly (e.g. when making a plurality of similarly formed sheets which are to be further processed) and/or the sheets are thick.
  • thermoplastics material of the flat sheet in place of or in addition to the particular arrangement described above, e.g. the platform 22 may be provided at its edge with embedded heating means - electrical £5 heating elements or channels through which a heating medium (hot oil or the like) is passed.
  • a heating medium hot oil or the like
  • the folded sheet may be joined to other fibres reinforced sheets which may be flat, or of similar or different shaped forms, by any suitable techni-
  • a plurality of flat and/or shaped sheets may be welded together by the method illustrated schematically in Figure 4.
  • a second platen 50' may be located on the other side of the abutting ends of the sheets 42 as 0 shown at the bottom of Figure 4 so that both sides 52 and 54 of the sheets 42 ar directly heated if the desired oper ⁇ ational speed of the process and/or the thickness of the sheets 42 makes it necessary and/or desirable.
  • a sheet 60 which has been bent or folded three times to the particular shape shown is fixed to a flat sheet 62 in the following way.
  • the two sheets 60 and 62 are brought into abutment at the pos ⁇ ition they are to be joined with an interposed layer of a resistive metal mesh 64 (e.g. a 200-200 mesh of 0.002" Dia. Stainless Steel wire).
  • the mesh is coupled to a power supply (e.g. the power supply described with reference to
  • the heat generated in the mesh causes the hermo ⁇ plastics material in the. areas of the sheets contacted by the mesh to be plasticised.
  • Pressure is then applied to the sheets 60 and 62 (e.g. a pressure of the order of 300KPa. for polyethersulphone glass fibres reinforced sheets).
  • the power supply is disconnected and the joint allowed to cool, the pressure is then released, the ends of the mesh are trimmed and a permanent joint has been formed, the remaining mesh in the joint forming an integ- ral part of it.
  • the method illustrated in Figure 6 shows how a complex shape such as an I-beam may be formed.
  • two sheets 66 and 68 pre-formed by the method disclosed above to the 'C shape shown are positioned back- to-back with interposed metal mesh layers 69.
  • Flat sheets 70 and 72 of thermoplastics fibres reinforced material are positioned on the top and bottom respectively of the abutting sheets 66 and 68 as shown with interposed layers of metal mesh 76 and 78 as shown.
  • the various parts of the structure are held in a jig (not shown) and- current is passed to the metal mesh layers 69, 76 and 78. After sufficient heating the power supply to the metal mesh layers is disconnected and the structure allowed to cool. After cooling the structure is removed from the jig and the metal mesh layers trimmed and an I-beam which is in part metal mesh reinforced has been formed.
  • Figure 7 illustrates how complex shapes such as Box- section structures may be formed from flat sheets of thermo ⁇ plastics fibres reinforced materials with interposed sheets which have been pre-formed in accordance with the methods described with reference to figures 1, 2 and 3.
  • flat sheets 80 of thermoplastics fibre reinforced materials are layed up in a jig as shown on top and bottom of pre-shaped sheets 82 and 84 and with interposed metal mesh layers 86 at the areas of contact.
  • the metal mesh layers are heated by passing thereto a current for sufficient time to plasticise the thermoplastics polymer material adjacent the abutting surfaces of the sheets 80, 82 and 84. After heating the power supply is disconnected from the metal mesh and the structure allowed to cool to below its glass transition temperature. Once cool the structure is removed from the jig, the metal mesh trimmed and the complete Box- section article with integral metal mesh reinforced joints has been formed.
  • pre-shaped sheets with other similarly pre-shaped or flat sheets may of course be used, for example the sheets may be joined by chemical/ solvent welding techniques, adhesive bonding or in any other suitable way.
  • thermoplastics matrix material in them and are then held in those relative positions whilst the materials are allowed to cool below the glass transition temperature of the thermoplastics material. It will be appreciated that this can be accomplished in a continuous process in which the various parts are carried through a plant in which the different successive operations are carried out.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

Procédé de fabrication d'une structure de forme complexe en matériau thermoplastique armé de fibres dans lequel: une feuille plate de matériau thermoplastique (16) armé de fibres est chauffée localement à une température à laquelle le matériau polymère qu'elle contient est plastifié, la feuille étant ensuite manipulée de manière à la cintrer ou à la plier au niveau de la zone de chauffage. Après cintrage, certaines desdites fibres d'armature s'étendant autour de l'axe de ladite courbure à l'intérieur de la couche le plus à l'extérieur de ladite armature demeurent intactes et forment, avec ledit matériau polymère, un bourrelet (24) s'étendant sur toute la longueur de ladite courbure ou du pli: sont décrits divers modes de jonctionnement des feuilles ainsi formées avec des feuilles de forme similaire ou des feuilles plates de matériaux thermoplastiques armés de fibres.A method of manufacturing a complex shaped structure of fiber-reinforced thermoplastic material in which: a flat sheet of fiber-reinforced thermoplastic material (16) is locally heated to a temperature at which the polymeric material it contains is plasticized, the sheet then being manipulated so as to bend or fold it at the level of the heating zone. After bending, some of said reinforcing fibers extending around the axis of said curvature inside the outermost layer of said reinforcement remain intact and form, with said polymeric material, a bead (24 ) extending over the entire length of said curvature or of the fold: various modes of joining the sheets thus formed are described with sheets of similar shape or flat sheets of thermoplastic materials reinforced with fibers.

Description

A METHOD OF MAKING COMPLEX SHAPES FROM FLAT FIBRE REINFORCED THERMOPLASTICS MATERIAL COMPOSITES.
DESCRIPTION
The invention concerns the manufacture of complex shaped structures in fibres reinforced high or low tempe¬ rature thermoplastics material.
Throughout this specification and in the claims annexed hereto the term fibres reinforcement encompasses fibres in the form of filaments or tows of filaments, mats of filaments or tows of filaments and cloths made,e.g. by laying up, knitting or weaving, filaments or tows of filaments.
The use of thermoplastics materials (with or without fibres reinforcement) to make articles .is well known, and. various methods of making them have been proposed. Genera- lly, the methods involve matching tools with high temperature and pressure to consolidate the materials in, for example film stacking processes; in which layers of fibres reinforce¬ ments (which may or may not be pre-impregnated with the polymer material) are laid up in the mould and one or more layers of the polymer material in sheet form are interposed, if needed, between adjacent ones of the sheets of fibres reinforcements.
The known methods are expensive, and in some cases - particularly when making large 'structures - impracticable. <-.
Flat sheet material is relatively cheap and easy to produce but, to date, the manufacture of useful structures from sheet fibres reinforced material has been a problem, particularly in one respect. When a thick material such as, e.g. metal or polymer without fibres reinforcement is folded or bent, the material 'outside' the median line - the centre line of the sheet- must stretch and the material 'inside' the median line compress to allow the fold to be formed. With fibres rein¬ forced materials, however, the fibres are relatively inex- tensible and incompressible and the sheet material containing them cannot be shaped in this way - unless the fibres of the fibres reinforcement extend uni-directionally within the matrix material and the axis of the fold or bend (the axis about which the bend or fold is formed) extends in a direc¬ tion parallel to the direction in which the fibres in the fibres reinforcement extend.
The invention proposes a novel way of overcoming this problem in thermoplastics materials reinforced with non- unidirectionally arrayed fibres reinforcement and which may with advantage be used in bending or folding thermoplastics materials reinforced with a unidirectionally arrayed fibre reinforcement on an axis not parallel to the direction in which the fibres extend.
A first aspect of the invention provides a method of making a complex shaped fibre reinforced thermoplastics material structure in which: a flat sheet of fibres rein- forced thermoplastics material is locally heated to a tem¬ perature at which the polymer material therein is plasticised, the sheet thereafter being manipulated so that it is bent or folded at the area at which it was heated with ones of said fibres of said reinforcement extending about the axis of the said bend within the outermost layer of said fibres reinforcement remaining intact and forming, with said polymer material a bead extending along the length of said bend or fold.
Although the invention may be used with any thermo- plastics matrix material (e.g. low temperature thermoplastics materials such as polystyrene) we feel that the methods now proposed are of especial advantage with high temperature aromatic polymer material materials such as polysulphone, polyethersulphone, polyetheretherketone, a polyamide or the like.
The fibres reinforcement may with advantage be of glass, carbon or quartz and the fibres therein may be multi- directionally disposed or uni-directionally disposed and extending in a direction about the axis of the said bend or fold.
A second aspect of the invention provides method of making a complex shaped thermoplastics material article formed by joining pre-shaped sheets made in accordance with the above noted first aspect of the invention with other similarly pre-shaped sheets and/or flat sheets. Preferably,in accordance with the second aspect the sheets to be joined are locally heated in the areas at which they are to be joined whilst being held in abutment until those areas are plasticised and then holding those areas together as the sheets cool to a temperature below the glass 5 transition temperature of the thermoplastics matrix material,
One method in accordance with the second aspect of the invention provides that the local heating is effected by platens held in contact with one or both sides of the sheets to be conjoined.
0 An alternative method in. accordance with the second aspect of the invention provides that the local heating is effected by interposing resistive metal mesh between the areas of the sheets held in abutment and passing to that metal mesh an electric current sufficient to raise the tem- 5 perature thereof above the glass transition temperature of the thermoplastics material being used, after cooling the metal mesh being trimmed such that the portion of the metal mesh left in the complex structure becomes an integral part thereof.
- r. A third aspect of the invention provides a complex shaped fibres reinforced thermoplastics material structure made in accordance with the first and second aspects noted above.
Various other aspects, features and advantages of the invention will become apparent from the following descrip¬ tion of various methods embodying the invention now made with reference to the accompanying drawings, in which:-
Figure 1 schematically shows at A an end view, and at B a side view of apparatus used in the method of the invention,
Figure 2 illustrates schematically the bending of a fibres reinforced plastics material in accordance with the invention.
Figure 3 schematically shows an alternative form of the apparatus illustrated in Figure 1 , and
Figures 4 to 7 schematically illustrate ways of making various other complex shapes embodying the invention.
With reference now to Figures 1 and 2 of the drawings.
Figure 1 shows at 10 an electrically resistive heating element coupled via a switch 12 to a low voltage/high current source 14 (such as an arc-welding transformer) by means of which, when switch 12 is closed, element 10 may be heated to a temperature at which the polymer material in a fibres reinforced flat sheet 16 to be worked is plasticised
(e.g. for polyethersulphone fibres reinforced materials a o temperature of 270 -300 C).
One side 18 of the fibres reinforced material sheet 16 is, in accordance with the invention, brought into close proximity - but not into contact - with the element 10. After a time, dependent upon the polymer material and the ς
thickness of the sheet 6 (e.g. for a sheet of polyethersulphone glass fibres reinforced material 3mm thick - after 10 seconds) the sheet is reversed so that the side 20 thereof is brought into proximity with the element 10 and heated. During heating the sheet 16 may be supported, if desired, on a rigid platform such as shown at 22.
Subsequent reversals of the disposition of the sheet may be necessary until the thermoplastic material of sheet 16 adjacent the element 10 has been heated to a temperature at which it is plasticised. Once in this condition the material may be folded or bent about an axis C so that its inner surface, e.g. surface 20 is raised to form a bead or roll 24 on the 'inside' of the fold.
Care is taken in the heating of the sheet to ensure that the area of the sheet being heated is plasticised but the temperature of that area does not rise to a level at which the polymer material therein degrades, for that reason the sheet material must not be allowed to contact the heating element directly and its heating is, desirably, effected by a large number of reversals of its disposition relative to the element 10 so that the temperature of the sheet is slowly raised to a temperature at which it is plasticised and can be worked.
After working, the sheet 16 is removed from proximity with element 10 (if necessary being held to retain the shape that has been imparted to it) and allowed to cool to a temperature below its glass transition temperature. Further bends may be formed in the sheet material if desired.
It will be appreciated that after formation of the or each bend as described above all the fibres in the rein- forcement in sheet 16 remain intact. That is to say all of the longitudinal fibres (those extending normally of the plane of the drawing) and all of the lateral fibres (those extending in the direction of the arrow X-X) remain intact. The longitu dinal fibres are relatively unaffected by the manipulation and retain the restrictive effect they have on the lateral fibres; the outermost ones of which are merely bent and not stretched whilst those within the outermost layer are all to some extent bent in a sense opposite to that of the bend which has been formed in sheet 16 - the inner- most ones of the lateral fibres in the reinforcement forming a loop which with the polymer material forms the bead or roll 24.
In an alternative arrangement shown in figure 3 the heating element 10 is replaced with two heating elements 26 disposed on either side of the sheet 16 enabling both of its surfaces 18 and 20 to be heated at the same time. The ele¬ ments 26 may be coupled to the power supply 14 by a single switch (as described with reference to Figure 1 ) or by two switches 28 as shown in Figure 3. It is thought that such an arrangement has particular advantage when there is a need for the process to be performed relatively quickly (e.g. when making a plurality of similarly formed sheets which are to be further processed) and/or the sheets are thick.
Other forms of heating the thermoplastics material of the flat sheet in place of or in addition to the particular arrangement described above, e.g. the platform 22 may be provided at its edge with embedded heating means - electrical £5 heating elements or channels through which a heating medium (hot oil or the like) is passed.
Once the folded sheet has cooled, it may be joined to other fibres reinforced sheets which may be flat, or of similar or different shaped forms, by any suitable techni-
10 que. A plurality of flat and/or shaped sheets may be welded together by the method illustrated schematically in Figure 4.
In the arrangement of Figure 4 two pre-shaped sheets 42 (each of which has been folded twice at 44 and 46) are pos¬ itioned with their ends 48 in abutment. Heated platens 50 are
15 then brought into contact with the material of the sheets 42 as shown and after heating the two sheets forced together so that the ends 48 (plasticised by the heat from the platens 50) are welded together. A second platen 50' may be located on the other side of the abutting ends of the sheets 42 as 0 shown at the bottom of Figure 4 so that both sides 52 and 54 of the sheets 42 ar directly heated if the desired oper¬ ational speed of the process and/or the thickness of the sheets 42 makes it necessary and/or desirable.
An alternative method of bonding together flat and/or shaped sheets is shown in Figures 5,6 and 7 in each of which areas of pre-shaped sheets are joined to areas of other pre-shaped or flat fibres reinforced sheets.
In the method illustrated in Figure 5 a sheet 60 which has been bent or folded three times to the particular shape shown is fixed to a flat sheet 62 in the following way. The two sheets 60 and 62 are brought into abutment at the pos¬ ition they are to be joined with an interposed layer of a resistive metal mesh 64 (e.g. a 200-200 mesh of 0.002" Dia. Stainless Steel wire). The mesh is coupled to a power supply (e.g. the power supply described with reference to
Fig.1 ) and the heat generated in the mesh causes the hermo¬ plastics material in the. areas of the sheets contacted by the mesh to be plasticised. Pressure is then applied to the sheets 60 and 62 (e.g. a pressure of the order of 300KPa. for polyethersulphone glass fibres reinforced sheets). After sufficient time, the power supply is disconnected and the joint allowed to cool, the pressure is then released, the ends of the mesh are trimmed and a permanent joint has been formed, the remaining mesh in the joint forming an integ- ral part of it.
The method illustrated in Figure 6 shows how a complex shape such as an I-beam may be formed. In the method of Figure 6 two sheets 66 and 68 pre-formed by the method disclosed above to the 'C shape shown are positioned back- to-back with interposed metal mesh layers 69. Flat sheets 70 and 72 of thermoplastics fibres reinforced material are positioned on the top and bottom respectively of the abutting sheets 66 and 68 as shown with interposed layers of metal mesh 76 and 78 as shown. The various parts of the structure are held in a jig (not shown) and- current is passed to the metal mesh layers 69, 76 and 78. After sufficient heating the power supply to the metal mesh layers is disconnected and the structure allowed to cool. After cooling the structure is removed from the jig and the metal mesh layers trimmed and an I-beam which is in part metal mesh reinforced has been formed.
Figure 7 illustrates how complex shapes such as Box- section structures may be formed from flat sheets of thermo¬ plastics fibres reinforced materials with interposed sheets which have been pre-formed in accordance with the methods described with reference to figures 1, 2 and 3. In the arran- gement of Figure 7 flat sheets 80 of thermoplastics fibre reinforced materials are layed up in a jig as shown on top and bottom of pre-shaped sheets 82 and 84 and with interposed metal mesh layers 86 at the areas of contact. The metal mesh layers are heated by passing thereto a current for sufficient time to plasticise the thermoplastics polymer material adjacent the abutting surfaces of the sheets 80, 82 and 84. After heating the power supply is disconnected from the metal mesh and the structure allowed to cool to below its glass transition temperature. Once cool the structure is removed from the jig, the metal mesh trimmed and the complete Box- section article with integral metal mesh reinforced joints has been formed.
Other ways of joining pre-shaped sheets with other similarly pre-shaped or flat sheets may of course be used, for example the sheets may be joined by chemical/ solvent welding techniques, adhesive bonding or in any other suitable way.
The rolls or beads of material left in making a struc¬ ture embodying the invention add to the rigidity and strength of the finished product.
The above described arrangements are merely exemplary of methods embodying the invention for making fibres rein¬ forced thermoplastics material structures of complex shape.
It is for example, possible in accordance with the invention to make the noted and other complex shaped struc- tures continuously simply by providing that the various parts to be joined are brought into juxtaposition, are heated and held in desired relative positions whilst sufficient heat is applied to them to plasticise the thermoplastics matrix material in them and are then held in those relative positions whilst the materials are allowed to cool below the glass transition temperature of the thermoplastics material. It will be appreciated that this can be accomplished in a continuous process in which the various parts are carried through a plant in which the different successive operations are carried out. It will be appreciated that the use of electrically resistive metal mesh interposed between adjacent layers of fibres reinforced thermoplastics materials to to be conjoined may be used in addition to the use of heated platens should the process, requirements (e.g. the thickness of the sheets) make it desirable and/or necessary.
In the ways described above it is possible to make structurally stiff components of rib/skin box or open girder multispar construction making use of fibres reinforced thermoplastics materials more readily than has until now been possible. As a result of the methods described it is possible to make components of complex form which until now it has been possible to make only of metals (such as aluminium) or in non-reinforced thermoplastics materials.

Claims

1. A method of making a complex shaped fibre reinforced thermoplastics material structure in which: a flat sheet of fibres reinforced thermoplastics material is locally heated to a temperature at which the polymer material therein is plasticised, the sheet thereafter being manipulated so that it is bent or folded at the area at which it was heated with ones of said fibres of said reinforcement extending about the axis of the said bend within the outermost layer of said fibres reinforcement remaining intact and forming, with said polymer material a bead extending along the length of said bend or fold.
2. A method as claimed in claim 1 , wherein the thermo¬ plastics material is a high temperature aromatic polymer material.
3. A method as claimed in claim 2, wherein the thermo¬ plastics material is one of polysulphone, polyethersulphone, polyetheretherketone, and a polyamide.
4. A method as claimed in any one of the preceeding claims wherein, the fibres reinforcement is of glass, carbon or quartz.
5. A method of making a complex shaped thermoplastics material article in which the article is formed by joining pre-shaped sheets made in accordance in any one of the preceeding claims with other similarly pre-shaped sheets and/or flat sheets of fibres reinforced thermoplastics material.
6. A method as claimed in claim 5, wherein the sheets to be joined are locally heated in the areas at which they are to be joined whilst being held in abutment until those areas are plasticised those areas then being held together as the sheets cool to a temperature below the glass transition temperature of the thermoplastics matrix material.
7. A method as claimed in claim 6, wherein the local heating is effected by platens held in contact with one or both sides of the sheets to be conjoined.
8. A method as claimed in claim 6, wherein the local heating is effected by interposing electrically resistive metal mesh between the areas of the sheets held in abutment and passing to that metal mesh an electric current sufficient to raise the temperature thereof above the temperature at which the thermoplastics matrix material is plasticised, and after cooling to below the glass transition temperature of the thermoplastics material the metal mesh is trimmed such that the portion of the metal mesh left in the complex structure becomes an integral part thereof.
9. A complex shaped fibres reinforced thermoplastics material structure made in accordance with the method of any one of the preceeding claims.
10. A method of making a complex shaped fibres reinforced thermoplastics material structure as claimed in any one of the preceeding claims and substantially as herein described.
11. A complex shaped fibres reinforced thermoplastics material structure made in accordance with any one of the preceeding claims and substantially as herein described with reference to Figures 2, 4, 5, 6, and 7 of the accompanying drawings.
EP86900180A 1984-12-10 1985-12-06 A method of making complex shapes from flat fibre reinforced thermoplastics material composites Withdrawn EP0204793A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8431086 1984-12-10
GB848431086A GB8431086D0 (en) 1984-12-10 1984-12-10 Complex shapes from thermoplastics material composites

Publications (1)

Publication Number Publication Date
EP0204793A1 true EP0204793A1 (en) 1986-12-17

Family

ID=10570935

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86900180A Withdrawn EP0204793A1 (en) 1984-12-10 1985-12-06 A method of making complex shapes from flat fibre reinforced thermoplastics material composites

Country Status (4)

Country Link
EP (1) EP0204793A1 (en)
AU (1) AU5234286A (en)
GB (2) GB8431086D0 (en)
WO (1) WO1986003451A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2215262B (en) * 1986-07-23 1991-09-18 Superplank Pty Limited Method of constructing a scaffold plank
GB8622988D0 (en) * 1986-09-24 1986-10-29 Westland Plc Joining thermoplastic materials
US4887880A (en) * 1988-08-31 1989-12-19 Raynet Corporation Optical fiber connector structure
US5076873A (en) * 1988-11-04 1991-12-31 The Boeing Company Method for forming and curing an I-section workpiece
US7126096B1 (en) 1991-04-05 2006-10-24 Th Boeing Company Resistance welding of thermoplastics in aerospace structure
FR2691099B1 (en) * 1992-05-13 1997-07-04 Dassault Aviat DEVICE FOR SOLIDARIZING OBJECTS MADE OF COMPOSITE MATERIALS THROUGH SIMULTANEOUS APPLICATION OF HEAT AND PRESSURE.
AU5317896A (en) * 1995-06-06 1996-12-24 Boeing Company, The Resistance welding of thermoplastics in aerospace structure
US6036802A (en) * 1996-09-13 2000-03-14 The Boeing Company Thermoplastic panel bending
FR2876945B1 (en) * 2004-10-27 2008-10-10 Mecaplast Sa Monegasque REINFORCED THERMOPLASTIC PIECE
EP1808285B1 (en) * 2006-01-17 2010-03-17 Mecaplast Sam Reinforced plastic piece

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1482569A (en) * 1922-01-16 1924-02-05 Berthold A Lange Box corner
US1872482A (en) * 1930-04-17 1932-08-16 Bull Dog Electric Products Com Process of bending laminated sheets
US2765716A (en) * 1955-04-12 1956-10-09 Andersson Nils Matrix for creasing paperboard for cartons
US3384695A (en) * 1965-04-26 1968-05-21 Impact Plastics Inc Method of making lug straps
US3329555A (en) * 1965-07-26 1967-07-04 Owens Corning Fiberglass Corp Postformed resin shapes
US3731600A (en) * 1971-03-16 1973-05-08 Ex Cell O Corp Resilient female scoring
CH547692A (en) * 1972-09-27 1974-04-11 Benone Ag METHOD FOR MANUFACTURING HOLLOW PROFILES, DEVICE FOR CARRYING OUT THE METHOD AND HOLLOW PROFILE MANUFACTURED BY THE METHOD.

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8603451A1 *

Also Published As

Publication number Publication date
WO1986003451A1 (en) 1986-06-19
GB2168643B (en) 1988-09-28
AU5234286A (en) 1986-07-01
GB8530088D0 (en) 1986-01-15
GB2168643A (en) 1986-06-25
GB8431086D0 (en) 1985-01-16

Similar Documents

Publication Publication Date Title
US5919543A (en) Composite sine wave spar
CA2688093C (en) Method for manufacturing an object from a sandwich structure having a reinforced corner and an object of this type
US7126096B1 (en) Resistance welding of thermoplastics in aerospace structure
JP5583969B2 (en) Method for making a composite fiber component using a foldable molded core and the molded core
NO931928L (en) PROCEDURE FOR PREPARING UNIFORM TERMOPLASTIC CELL LAYER STRUCTURE WITH DIFFERENT PHYSICAL PROPERTIES
EP0204793A1 (en) A method of making complex shapes from flat fibre reinforced thermoplastics material composites
BE1028283B1 (en) BIKE FRAME AND MANUFACTURING PROCEDURE
US7138031B2 (en) Mandrel and method for manufacturing composite structures
AU2023202622A1 (en) Manufacturing fibre-reinforced composite structures
RU2027604C1 (en) Elongate composite structure forming apparatus
WO1987006186A1 (en) Lightweight high temperature thermoplastics material structures
CA2030418C (en) Method of making an article from a thermoplastic sandwich material
US20230415428A1 (en) Beaded panels and systems and methods for forming beaded panels
EP3670158B1 (en) Method for forming a bicycle frame component made of thermoplastic composite laminates and the bicycle frame for the same
EP0375280A1 (en) Method for forming components from fibre-reinforced thermoplastic materials
JPH06344477A (en) Laminated molded product and production thereof
US5458476A (en) Apparatus for shaping fiber reinforced resin matrix materials
FR2626212A1 (en) Method and device for moulding and curing a composite material for forming a reinforced skin panel
JP3723659B2 (en) Method for forming honeycomb core material
JPH04189535A (en) Method of manufacturing thermoplastic sandwich material product
EP0830283A1 (en) Resistance welding of thermoplastics in aerospace structure
CN115816839A (en) Lapping forming method for annular plastic fiber board skin ring
JPS6411447B2 (en)

Legal Events

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

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19861112

RIN1 Information on inventor provided before grant (corrected)

Inventor name: DOE, THOMAS, GLENVILLE