WO2006060895A1 - Process and machine for producing lightweight thermoplastic composite products in a continuous manner - Google Patents
Process and machine for producing lightweight thermoplastic composite products in a continuous manner Download PDFInfo
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- WO2006060895A1 WO2006060895A1 PCT/CA2005/001724 CA2005001724W WO2006060895A1 WO 2006060895 A1 WO2006060895 A1 WO 2006060895A1 CA 2005001724 W CA2005001724 W CA 2005001724W WO 2006060895 A1 WO2006060895 A1 WO 2006060895A1
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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/44—Compression means for making articles of indefinite length
- B29C43/46—Rollers
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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/22—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of indefinite length
- B29C43/30—Making multilayered or multicoloured articles
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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/34—Feeding the material to the mould or the compression means
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- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
- B29C70/506—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands and impregnating by melting a solid material, e.g. sheet, powder, fibres
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- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
- B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
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- 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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
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- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/10—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer reinforced with filaments
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- 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
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/44—Compression means for making articles of indefinite length
- B29C43/46—Rollers
- B29C2043/466—Rollers the rollers having specific shape, e.g. non cylindrical rollers, conical rollers
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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
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- 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
- B29K2105/0809—Fabrics
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- 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
- B32B2250/00—Layers arrangement
- B32B2250/40—Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
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- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0207—Elastomeric fibres
- B32B2262/0215—Thermoplastic elastomer fibers
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- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0253—Polyolefin fibres
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- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
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- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
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- B32B2262/106—Carbon fibres, e.g. graphite fibres
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/14—Mixture of at least two fibres made of different materials
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
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- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/31—Heat sealable
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
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- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/552—Fatigue strength
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- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
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- B32B2307/00—Properties of the layers or laminate
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- B32B2607/00—Walls, panels
Definitions
- the present invention relates to a machine and a process for the production of lightweight thermoplastic composite products in a continuous manner.
- thermoplastic (TP) matrices Thermoplastic polymers, in particular semi-crystalline ones, provide a number of significant advantages over their thermosetting counterparts. They exhibit better fraction toughness, there is no need for chemical reaction during processing and therefore no toxicity during processing and application, and they are recyclable.
- the high viscosity of the molten thermoplastic resin imposes many limitations on the manufacturing process with these materials . These are usually related to the need of incorporating the highly viscous polymer into the structure made of continuous reinforcing fibers. Use of commingled yarn is one of the most promising approaches for fast production of TP based composites.
- thermoplastic and reinforcement fibers give a good initial matrix-reinforcement distribution in a non-molten state before processing. This represents a kind of dry impregnation, which circumvents some of the difficulties associated with the high viscosity of the molten polymer.
- Fabric woven from commingled yarn can be processed by application of heat and pressure into composite materials in a manner analogous to that of thermoset based prepregs .
- the relatively uniform commingling of the reinforcing matrix fibers minimizes the distance the molten thermoplastic is required to flow to fill the inter fiber spaces and this allows the material to be consolidated using reasonable pressure even at high fiber content of glass fibers.
- a continuous process also facilitates the production of desired products either by roll forming at the outlet of the continuous process or the production of sandwich panels or sheets of large dimensions which can be used in the manufacture of walls, roof sections, doors, flooring of train cars, automobiles, shipping containers, only to name a few products where reduced weight is of importance to obtain the benefit of reduced gas consumption and consequently the release of hazardous gas emissions.
- By roll forming products can be produced for use in the construction of highway guardrails, which traditionally have been made of corrugated galvanized steel plates and beams.
- Such is prone to corrosion in harsh environments and resulting in loss of strength, durability and deterioration of its appearance.
- Such guardrails also damage vehicles and injure passengers and must be replaced after being impacted by a vehicle.
- thermoplastic composite materials By the use of thermoplastic composite materials, a significant weight reduction with excellent fatigue and impact behaviour, especially at low temperature, can be obtained.
- the present invention provides a machine for producing lightweight thermoplastic composite products in a continuous manner.
- the machine comprises at least one heating- oven for heating a dry unconsolidated fabric sheet of commingled fibers of thermoplastic resin and reinforcing fiberglass or carbon fibers to a temperature sufficient to insure melting and flow distribution of the resin in voids of the commingled fibers.
- This sheet is conveyed through the oven where the fabric sheet is heated up to temperature slightly more than the melting point of the thermoplastic resin, and out of the oven through a first pair of heated rollers with the fabric sheet engaged in a gap between the first pair of heated rollers to maintain pressure.
- the rollers are heated to a predetermined temperature to avoid abrupt cooling at the surface of the laminate.
- Further pairs of rollers are provided, and at least one pair of which is operating at a reduced temperature from the first pair and these additional rollers engage the composite sheet in respective gaps whereby to maintain pressure and reduce the temperature of the sheet while controlling the pressure and thickness thereof as the commingled fibers consolidate to form a continuous composite consolidated sheet.
- the machine is also provided with processing means for processing the continuous composite consolidated sheet to progressively form a desired product (profile) using forming rollers.
- thermoplastic composite products comprising the steps of feeding on a continuous basis a sheet of dry unconsolidated commingled fibers of thermoplastic resin and reinforcing fiberglass or carbon fibers in an oven to heat the sheet to a temperature sufficient to insure melting and flow of the thermoplastic resin fibers.
- the sheet is then subjected to further controlled heat and pressure by feeding the sheet from the oven through a gap between a first pair of heated rollers. The rollers are heated to a predetermined temperature and the sheet is compressed in the gap.
- the sheet is then fed through further pairs of rollers, at least one pair of which is a pair of heated rollers operating at a reduced temperature from the first pair of heated rollers to reduce the temperature of the sheet and further maintain the sheet under pressure to ensure full distribution of the resin and to obtain a desired sheet thickness while causing the commingled fibers to consolidate to thereby form a continuous composite consolidated sheet.
- the temperature of the oven, of the heated rollers, and the feed speed of the sheet are all controlled by a computer controller.
- the sheet is then processed progressively to form a desired product by using forming rollers.
- FIG. 1 is a simplified side view illustrating the machine and process of the present invention for the production of lightweight thermoplastic composite material and products in a continuous manner;
- FIG. 2 is a cross-section view illustrating the unconsolidated composite fabric sheet comprised of commingled fibers
- FIG. 3 is a view similar to Figure 2, but illustrating a sandwich panel constructed by the machine and process of the present invention and comprised of a center core material sandwiched between opposed composite consolidated sheets fabricated by the machine and process of the present invention; and FIG. 4 illustrates the construction of a guardrail profile formed at the outlet end of the machine by forming rollers .
- the machine comprises at least one heating oven 11 and there is herein illustrated two such ovens 11 and 11' when fabricating a sandwich product 40 as illustrated in Figure 3.
- a controller device 12 controls the temperature of the ovens 11 and 11'.
- Dry unconsolidated commingled fabrics 13 and 13' are fed to their respective ovens 11 and 11' by suitable feed means.
- the commingled fabric sheets 13 and 13' are guided in their respective ovens 11 and 11' on roller conveyors 14 and 14', respectively.
- Such fabric 13 and 13' may be unwound from supply rolls 15 and 15', respectively. It may also be provided in very long sheet form.
- the fabric sheets 13 and 13' are comprised of dry unconsolidated commingled fibers of thermoplastic resin 16 and reinforcing fibers 17 of fiberglass material or carbon material.
- the fabric sheets 13 and 13' are conveyed through the oven and through the system by drive rollers as will be described later and controlled by the controller device 12.
- the controller device 12 also controls the temperature of the ovens 11 and 11' whereby to heat the fabrics to a temperature sufficient to ensure melting of the thermoplastic resin for it to start flowing between the fibers 17.
- the thermoplastic resin may be, for example, polypropylene, PET or polyamide fibers and they can be of different types or thicknesses.
- the exit temperature from the oven would be higher than the melting point of this resin and therefore above 168 0 C and preferably about 178 0 C. This ensures that the polypropylene has melted and starts flowing in the voids between the reinforcing fib'ers 16 and 17, as illustrated in Figure 2. Accordingly, the fabric sheets 13 and 13' exit their ovens at the outlet 19 and 19' thereof with the thermoplastic resin in molten form.
- the temperature of the ovens is maintained substantially constant by controlling two parallel blocks 20 and 20' of infrared elements. Temperature sensors such as schematically illustrated at 21 provide signals to the controller device 12 to monitor the temperature of each oven and to control the infrared heaters. The controller 12 also controls the feed speed of the fabric sheet 13 being conveyed through the oven.
- the machine 10 as herein illustrated was constructed to fabricate sandwich panels such as illustrated in Figure 3 which is composed of a non-structural core 41 to which is fused two outer composite consolidated sheets 42 and 42' having been processed in the machine 10.
- the core material 41 can be an aluminum or polypropylene prefabricated honeycomb core, as illustrated at 41, or a rigid foam sheet or any suitable material.
- the core material should be a lightweight material capable of supporting shear and compressive stresses and providing good adhesion to the composite consolidated sheets 13". Seeing that the continuous composite consolidated sheets 13" are formed by identical equipment on opposed sides of the core sheet 41, only one side of the apparatus and process will follow. As shown in Figure 1, the core material 41 is fed directly between the ovens and 11 and 11' in a substantially horizontal plane and on opposed sides thereof the composite consolidated sheets 42 are formed.
- the machine and process consist of several stages of fabrication which are completely independent but related in a progressive manner.
- the purpose of the machine and process is to heat and consolidate the commingled fibers in the fabric and then laminate it on opposed sides of the core material 41.
- This continuous process and apparatus can achieve high volume of production and quality composite parts.
- the process offers significant advantages over conventional processing technologies as above-described. Some advantages include a short fabrication cycle, an unlimited length for products and mixed-processing possibilities, such as the construction of sandwich products or shaped products (profiles) are important advantages of this technology.
- the fabric sheet 13 exits with the resin in a molten state and this sheet is immediately fed between a first pair of heated rollers 25 which are mounted on a support frame 26 which is provided with adjustments 27 whereby to adjust the gap 28 and therefore pressure between the rollers. Accordingly, the fabric sheet 13 is placed under pressure in this gap to squeeze the resin in the voids between the fibers.
- the rollers 29 and 29' of the first pair of heated rollers 25 also has the temperature thereof controlled by the controller device 12 , whereby to maintain the sheet at a desired temperature and under pressure whereby to ensure consolidation of the molten resin with the reinforcing fibers and to achieve a composite consolidated sheet of predetermined thickness.
- the temperature of the first pair of heated rollers 25 and 25' is controlled within the range of about 60 to 120°C thereby controlling the cooling rate of the fabric sheet 13.
- the fabric sheet 13 exiting the first pair of heated rollers 25 is then subjected to a second pair of heated rollers 30 which are also mounted on adjustments to control the size of its gap 31.
- the temperature of the second set of heated rollers 30 is also controlled by the controller device 12 and maintained at a temperature which is lower than the first set of rollers 25 and preferably about' 25°C lower. Accordingly, the temperature of the fabric sheet 13 is gradually decreased while maintained under pressure by these two pairs of rollers.
- a still further pair of rollers 33 engages the fabric sheet 13 and its rollers 32 and 32 ' are also adjustable to maintain the fabric sheet 13 under pressure.
- This further set of rollers 33 are not heated and operate at ambient temperature.
- the fabric sheet 13 has now consolidated and it is now fed to processing devices 35 to form desired products. It is pointed out that the fabric sheet 13 is conveyed through the apparatus by the pairs of rollers 25, 30 and 33 which are driven in synchronism. Such drives are well known in the art.
- the pairs of rollers 36, 37 and 38 as illustrated in the processing device 35 may also be driven and also in synchronism. All of these rollers are controlled by the controller device 12.
- the apparatus is structured to form sandwich panels the cross-section of which is illustrated at 40 in Figure 3.
- three pairs of rollers 36, 37 and 38 which maintain pressure on the sandwich which is formed thereunder to ensure that the composite consolidated sheet 13" fed on opposed sides of the core 41 are well bonded thereto.
- the outer faces 43 and 43' of the core sheet 41 are heated by infrared heaters 39 and 39'. These infrared heaters also provide radiant heat, in the order of about 160°C, to the inside surfaces or bonding surfaces 44 and 44' of the composite consolidated sheets 13", respectively. This melts the thermoplastic resin on the surfaces thereof which are to be bonded to the outer surfaces of the core sheet 41.
- the panels may have a thickness of from about 5 mm to about 50 mm.
- the sets of rolls 36, 37 and 38 are adjusted to maintain pressure on this sheet as it cools to rigidly bond to the core material thus producing at its outlet a continuous sheet which can then be cut into sheet sections 45 by a slitter device 46 which moves with the sandwich sheet 40 to cut the sheet transversely thereacross to form individual structural sheets or panels 45 which can then be stacked, as hereinshown on a conveyor means 47 and then automatically transported.
- the slitter 46 is also controlled by the controller device which can adjust the size of the sheets down to narrow panels.
- the core material 41 is constructed of light aluminum or light wood product, then in order to fuse the composite consolidated sheets 13" thereto, there may be interposed between the consolidated sheets and the outer surfaces of the core sheet 41 a binder sheet 48 guided over the infrared heaters 39 by guide rolls 49 to adhere the composite consolidated sheets 13' to opposed surfaces of the core material. If it is desirable to embed a color effect on the opposed faces of the sandwich product 40, then a plastic colored film sheet 50 may be fed over the top surface of the upper composite consolidated sheet 13" as herein illustrated. This sheet would adhere to the top face of the thermoplastic material which is heated and bind thereto by the hot thermoplastic material.
- the machine as herein illustrated is to construct the sandwich panel product 40 as illustrated in Figure 3, the machine can operate with simply the upper part thereof with a single oven and sets of rolls 25, 30 and 33 whereby to produce a single composite consolidated sheet 13" which is then processed by the processing device 35 which may consist of sets of forming rolls 52 as illustrated in Figure 4 whereby to shape the continuous composite consolidated sheet 13" as illustrated in Figure 4 to form a desired profile.
- the profile being formed is that for use in the construction of guardrails and many of these wave shapes can be formed across the sheet and then cut into long strip sections of shaped products .
- These forming rolls 52 would progressively shape the sheet which is still hot and malleable prior to complete cooling thereof.
- These shaped sheets could also be cut by the device 46.
- the cutter device 46 can have various forms and could be a laser cutting machine or other suitable cutter devices.
- the conveying means consist of the pairs of rollers 25, 30, 33 and also rollers 36, 37, 38 if provided. These rolls are connected to variable speed drive motors, not shown, but obvious to a person skilled in - li ⁇
- the art which are automatically controlled by the controller device whereby to adjust the feed speed of the fabric sheet to ensure full consolidation. Also, the adjustment of the gaps between these rollers can be adjusted mechanically or automatically.
- thermoplastic composite products comprises the steps of feeding on a continuous basis the sheet 13 of the dry unconsolidated commingled fibers of thermoplastic resin and reinforcing fiberglass or carbon fibers through various controlled process stages.
- the first stage comprises an oven 11 to heat the sheet to a temperature sufficient to ensure the melting of the thermoplastic resin fibers.
- the sheet 13 is then subjected to further controlled heat and pressure treatment by a first pair of heated rollers 25 which have the gap thereof adjusted depending on the thickness of fabric sheet 13 fed to rollers to squeeze the resin within the voids between the reinforcing fibers.
- the speed is also controlled in accordance with the characteristics of that sheet.
- the rollers 25 are heated to a predetermined temperature, whereby the temperature of the heated sheet can be controlled and compressed between the rolls to ensure full consolidation of the resin with the structural fibers.
- the sheet is also fed through a second set of heated rollers which maintain the sheet at a reduced temperature and continuously under pressure to assure that the resin flows into the interstices of the fibers in the fabric sheet and full consolidation.
- the last set of rollers 33 operate at ambient temperature and at that stage the fabric sheet 13 has almost fully consolidated and it is now ready to be treated in the processing device to fabricate desired products as above-described. As shown in Figure 1, it is also envisaged that a color may be imparted to at least one face of the composite consolidated sheet.
- a hopper 60 is provided at the inlet of the top oven 20 whereby to deposit on the unconsolidated fabric sheet 13 a colored plastic powder material 61 which will melt in the oven and flow in the sheet to provide a color effect at the surface of the top consolidated sheet 13".
- this hopper 60 may be installed after the oven or at any other stages between the consolidation rollers depending on the type of powder and application.
Abstract
Description
Claims
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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US11/006,707 | 2004-12-08 | ||
US11/006,707 US7429305B2 (en) | 2004-12-08 | 2004-12-08 | Process and machine for producing lightweight thermoplastic composite products in a continuous manner |
CA2,492,560 | 2005-01-13 | ||
CA2492560A CA2492560C (en) | 2004-12-08 | 2005-01-13 | Process and machine for producing lightweight thermoplastic composite products in a continuous manner |
Publications (1)
Publication Number | Publication Date |
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WO2006060895A1 true WO2006060895A1 (en) | 2006-06-15 |
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ID=36577625
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/CA2005/001724 WO2006060895A1 (en) | 2004-12-08 | 2005-11-14 | Process and machine for producing lightweight thermoplastic composite products in a continuous manner |
Country Status (1)
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WO (1) | WO2006060895A1 (en) |
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DE102010006805A1 (en) * | 2010-02-04 | 2011-08-04 | Audi Ag, 85057 | Method for manufacturing component e.g. shell part of car body, in automobile industry, involves discontinuously manufacturing complex component from preform, and introducing preform into press, and pressing preform |
EP3069843A1 (en) * | 2015-03-19 | 2016-09-21 | Fuji Jukogyo Kabushiki Kaisha | Composite material shaping device and composite material shaping method |
KR101730606B1 (en) | 2015-11-13 | 2017-04-26 | 주식회사 한국이엔티 | Reinforced panel forming apparatus |
CN110774511A (en) * | 2019-10-23 | 2020-02-11 | 安徽华宏机械设备有限公司 | Steel wire rope core conveyer belt blank preheating cold press molding device |
US11155049B2 (en) | 2016-02-23 | 2021-10-26 | Subaru Corporation | Composite material shaping device and composite material shaping method |
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