FR2876945A1 - Reinforced thermoplastic component e.g. for motor vehicle interior load-bearing panel has main body and reinforcing elements of same or compatible thermoplastics - Google Patents
Reinforced thermoplastic component e.g. for motor vehicle interior load-bearing panel has main body and reinforcing elements of same or compatible thermoplastics Download PDFInfo
- Publication number
- FR2876945A1 FR2876945A1 FR0411440A FR0411440A FR2876945A1 FR 2876945 A1 FR2876945 A1 FR 2876945A1 FR 0411440 A FR0411440 A FR 0411440A FR 0411440 A FR0411440 A FR 0411440A FR 2876945 A1 FR2876945 A1 FR 2876945A1
- Authority
- FR
- France
- Prior art keywords
- thermoplastic
- reinforcing element
- fibers
- reinforcing
- reinforcing elements
- 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.)
- Granted
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Classifications
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General 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
- B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
- B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
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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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/481—Non-reactive adhesives, e.g. physically hardening adhesives
- B29C65/4815—Hot melt adhesives, e.g. thermoplastic adhesives
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint 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
- B29C66/112—Single lapped joints
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single 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
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/301—Three-dimensional joints, i.e. the joined area being substantially non-flat
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General 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
- B29C66/51—Joining 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/524—Joining profiled elements
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General 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
- B29C66/51—Joining 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
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/71—General 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
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/72—General 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
- B29C66/721—Fibre-reinforced materials
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/72—General 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
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72141—Fibres of continuous length
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/73—General 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
- B29C66/739—General 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
- B29C66/7392—General 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
- B29C66/73921—General 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
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/08—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/1403—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
- B29C65/1412—Infrared [IR] radiation
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/16—Laser beams
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
- B29C65/20—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools with direct contact, e.g. using "mirror"
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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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
- B29C65/22—Heated wire resistive ribbon, resistive band or resistive strip
- B29C65/221—Heated wire resistive ribbon, resistive band or resistive strip characterised by the type of heated wire, resistive ribbon, band or strip
- B29C65/222—Heated wire resistive ribbon, resistive band or resistive strip characterised by the type of heated wire, resistive ribbon, band or strip comprising at least a single heated wire
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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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General 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
- B29C66/72—General 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
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
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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]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
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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
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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
- B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
- B29K2105/101—Oriented
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3005—Body finishings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Electromagnetism (AREA)
- Toxicology (AREA)
- Manufacturing & Machinery (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
PIECE THERMOPLASTIQUE RENFORCESREINFORCED THERMOPLASTIC PIECE
La présente invention concerne une pièce thermoplastique renforcée adaptée à supporter de fortes charges. Une telle pièce peut être destinée à une utilisation 5 comme pièce d'automobile, de chariot ou de tout autre dispositif nécessitant un renforcement localisé pour supporter de fortes charges. The present invention relates to a reinforced thermoplastic piece adapted to withstand high loads. Such a part may be intended for use as an automobile, trolley or other device requiring localized reinforcement to withstand heavy loads.
Certaines pièces automobiles d'habitacle et de coffre, telles que les planchers de charge ou les tablettes arrière par exemple, doivent pouvoir supporter des charges lourdes comme des bagages et sont soumises à d'importantes contraintes mécaniques, en particulier des contraintes de rigidité, de flèche résiduelle et de résistance au fluage. Pour satisfaire à ces contraintes mécaniques, il est connu de réaliser ces pièces dans des matériaux présentant des modules de Young élevés, comme les matériaux thermodurcissables. Certain automobile interior and trunk parts, such as load floors or rear shelves, for example, must be able to withstand heavy loads such as luggage and are subject to significant mechanical stresses, in particular stiffness, residual arrow and creep resistance. To satisfy these mechanical constraints, it is known to make these parts in materials having high Young's moduli, such as thermosetting materials.
Ces matériaux thermodurcissables à module de Young élevé présentent cependant l'inconvénient de ne pas pouvoir être facilement recyclés. De plus, les pièces précitées étant souvent visibles dans un véhicule automobile, elles sont également soumises à des contraintes esthétiques. Il est alors contraignant pour le concepteur d'être limité dans son choix de matériaux aux seuls matériaux présentant les qualités mécaniques suffisantes. These thermosetting materials with a high Young's modulus, however, have the disadvantage of not being easily recycled. In addition, the aforementioned parts are often visible in a motor vehicle, they are also subject to aesthetic constraints. It is then binding for the designer to be limited in his choice of materials to only materials with sufficient mechanical qualities.
Une solution connue pour réaliser ce type de pièce, dite semi structurelle, est de les fabriquer dans des matériaux ne présentant pas de module Young spécialement élevée, et d'obtenir la rigidité souhaitée grâce à la géométrie de la pièce. Par exemple le brevet FR-A-2 734 201 décrit une tablette double coque constituée de deux parois solidarisées l'une à l'autre en de multiples points ou portions de surface de sorte à ménager des volumes de vide entre lesdites parois. C'est la multiplicité des points ou portions de surfaces de contact entre les parois qui contribue à rigidifier l'ensemble. Une telle tablette mono-matériau peut facilement être recyclée. Mais de telles tablettes présentent un encombrement important en épaisseur, qui n'est pas toujours compatible avec l'espace disponible dans le véhicule. En particulier pour rigidifier un plancher de charge, l'épaisseur nécessaire est telle que cette solution ne peut pas être appliquée. A known solution for producing this type of part, called semi-structural, is to manufacture them in materials that do not have a particularly high Young's modulus, and to obtain the desired rigidity thanks to the geometry of the part. For example FR-A-2,734,201 discloses a double-shell tablet consisting of two walls secured to one another at multiple points or surface portions so as to provide vacuum volumes between said walls. It is the multiplicity of points or portions of contact surfaces between the walls which contributes to stiffening the assembly. Such a mono-material tablet can easily be recycled. But such tablets have a large size in thickness, which is not always compatible with the available space in the vehicle. In particular for stiffening a load floor, the necessary thickness is such that this solution can not be applied.
Une autre solution connue consiste à réaliser ce type de pièce semi structurelle avec des renforts rapportés. La pièce est alors constituée de deux éléments assemblés, à savoir un corps de pièce, tel qu'un plateau réalisé dans un matériau léger satisfaisant aux contraintes esthétiques mais sans contraintes de rigidité particulières, et des renforts réalisés dans un matériau à module de Young élevé. Ce type de pièce est fréquemment utilisé dans des coffres de véhicule, par exemple pour des tablettes arrière réalisées en polypropylène (PP) avec des renforts métalliques. Another known solution is to make this type of semi structural part with added reinforcements. The part is then composed of two assembled elements, namely a part body, such as a plate made of a light material satisfying the aesthetic constraints but without particular stiffness constraints, and reinforcements made of a high Young's modulus material. . This type of part is frequently used in vehicle trunks, for example for rear shelves made of polypropylene (PP) with metal reinforcements.
R:\Brevets\23100\23148.doc - 27/10/04 - 09:10 - 1/14 De telles pièces satisfont pleinement aux contraintes de rigidité. Cependant, l'utilisation de deux familles de matériaux complique le recyclage de ces pièces: la pièce doit être démontée, les matériaux doivent être séparés, afin que chacun suive la filière de recyclage appropriée. Such parts fully satisfy rigidity constraints. However, the use of two families of materials complicates the recycling of these parts: the part must be dismantled, the materials must be separated, so that everyone follows the appropriate recycling path.
Il existe par ailleurs des éléments de renfort en matériau thermodurcissable présentant un module de Young élevé réalisés par pultrusion d'un matériau composite comprenant des fibres de verre. De tels éléments sont par exemple décrits dans la demande de brevet FR-A-2 483 343 pour un pare-choc et dans la demande de brevet EP-A-O 980 801 pour un renfort d'essuie-glace. Les matériaux composites utilisés dans ces demandes sont obtenus par pultrusion de fibres de verre imprégnées de résine. Ces éléments de renfort ne répondent cependant à aucune contrainte esthétique et sont assemblés avec des pièces intermédiaires aux pièces de véhicule qu'elles renforcent. De tels éléments composites ne peuvent pas être assemblés directement avec une pièce thermoplastique à renforcer. In addition, there are reinforcement elements of thermosetting material having a high Young's modulus produced by pultrusion of a composite material comprising glass fibers. Such elements are for example described in the patent application FR-A-2 483 343 for a bumper and in the patent application EP-A-0 980 801 for a wiper reinforcement. The composite materials used in these applications are obtained by pultrusion of glass fibers impregnated with resin. These reinforcing elements, however, do not meet any aesthetic constraint and are assembled with intermediate parts to the vehicle parts they reinforce. Such composite elements can not be assembled directly with a thermoplastic part to be reinforced.
Il existe donc un besoin pour réaliser des pièces thermoplastiques renforcées qui soient esthétiques, légères, recyclables, d'un encombrement limité et de fabrication simplifiée. There is therefore a need to produce reinforced thermoplastic parts that are aesthetic, light, recyclable, limited space and simplified manufacturing.
A cet effet, l'invention propose une pièce thermoplastique comprenant: un corps constitué d'un matériau comprenant une première matrice thermoplastique; au moins un élément de renfort constitué d'un matériau comprenant une deuxième matrice thermoplastique et des fibres continues et sensiblement parallèles les unes aux autres; les première et deuxième matrices thermoplastiques étant des matériaux de la 25 même famille et ledit au moins un élément de renfort étant associé de façon irréversible au corps de la pièce. For this purpose, the invention provides a thermoplastic part comprising: a body made of a material comprising a first thermoplastic matrix; at least one reinforcing element consisting of a material comprising a second thermoplastic matrix and continuous fibers substantially parallel to each other; the first and second thermoplastic matrices being materials of the same family and said at least one reinforcing element being irreversibly associated with the body of the workpiece.
Selon les modes de réalisation, la pièce thermoplastique de l'invention peut comprendre une ou plusieurs des caractéristiques suivantes: - la famille des première et deuxième matrices est choisie parmi les polypropylènes; les première et deuxième matrices thermoplastiques sont constituées du même matériau; l'élément de renfort est soudé au corps de la pièce; l'élément de renfort est monobloc avec le corps de la pièce; l'élément de renfort présente la forme d'un profilé allongé, les fibres continues étant sensiblement parallèles à l'axe longitudinal du profilé de renfort; R:\ Brevets\ 23100\ 23 I48.doc - 27/10/04 - 09:10 - 2/14 - les fibres constituent entre 20% et 80% en poids de l'élément de renfort; les fibres de l'élément de renfort sont choisies parmi les fibres de verre, les fibres minérales, les fibres d'origine végétale et les fibres 5 synthétiques; - l'élément de renfort présente un module Young à 23 C compris entre 10000 et 50000 MPa; - l'élément de renfort présente une contrainte admissible comprise entre 200 et 900 MPa; - l'élément de renfort comporte un gainage comprenant un matériau thermoplastique; l'élément de renfort présente un profil transversal en forme de , de I , de T , de U , de V , de W , de carré, de rectangle ou de cercle; L'invention concerne aussi un ensemble comprenant: une pièce thermoplastique selon l'invention; - un habillage entourant la pièce. According to the embodiments, the thermoplastic component of the invention may comprise one or more of the following characteristics: the family of the first and second matrices is chosen from polypropylenes; the first and second thermoplastic matrices are made of the same material; the reinforcing element is welded to the body of the piece; the reinforcing element is integral with the body of the part; the reinforcing element has the shape of an elongate section, the continuous fibers being substantially parallel to the longitudinal axis of the reinforcing section; The fibers comprise between 20% and 80% by weight of the reinforcing element; the fibers of the reinforcing element are chosen from glass fibers, mineral fibers, fibers of vegetable origin and synthetic fibers; - The reinforcing element has a Young's modulus at 23 C between 10000 and 50000 MPa; the reinforcing element has a permissible stress of between 200 and 900 MPa; the reinforcing element comprises a cladding comprising a thermoplastic material; the reinforcing element has a transverse profile in the form of, I, T, U, V, W, square, rectangle or circle; The invention also relates to an assembly comprising: a thermoplastic part according to the invention; - a covering surrounding the room.
Selon les modes de réalisation, l'habillage est un caisson ou un tissu. L'invention propose aussi un procédé de fabrication d'une pièce 20 thermoplastique renforcée, comprenant les étapes consistant à : - réaliser un corps de pièce comprenant une première matrice thermoplastique; réaliser au moins un élément de renfort comprenant des fibres continues sensiblement parallèles incorporées dans une deuxième 25 matrice thermoplastique, les première et deuxième matrices thermoplastiques étant des matériaux de la même famille; - associer de façon irréversible ledit au moins un élément de renfort au corps pour constituer une pièce renforcée. According to the embodiments, the dressing is a box or a fabric. The invention also provides a method of manufacturing a reinforced thermoplastic member, comprising the steps of: - providing a workpiece body comprising a first thermoplastic matrix; providing at least one reinforcing element comprising substantially parallel continuous fibers incorporated in a second thermoplastic matrix, the first and second thermoplastic matrices being materials of the same family; irreversibly associating said at least one reinforcement element with the body to constitute a reinforced part.
Selon les modes de réalisation, le procédé de l'invention peut comprendre une 30 ou plusieurs des caractéristiques suivantes: - l'étape de réalisation du corps consiste à injecter une matière thermoplastique dans un moule; - l'étape de réalisation de l'élément de renfort comprend des étapes consistant à réunir plusieurs brins de fibres à étirer à travers une filière et à introduire une matière thermoplastique dans la filière; l'étape de réalisation de l'élément de renfort comprend des étapes consistant à réunir plusieurs brins de fibres imprégnés de matière thermoplastique et à étirer lesdits brins de fibre à travers une filière; R:\Brevets\23100\23148.doc - 27/10/04 - 09:10 - 3/14 l'étape de réalisation de l'élément de renfort comprend des étapes consistant à réunir plusieurs brins de fibres et un fil de matière thermoplastique et à étirer lesdits brins et ledit fil simultanément à travers une filière; l'étape d'association de l'élément de renfort au corps comprend une étape de soudage; l'étape d'association de l'élément de renfort au corps comprend une étape de thermocollage; l'étape d'association de l'élément de renfort au corps est conduite simultanément à l'étape de réalisation du corps de la pièce et comprend les étapes consistant à disposer ledit au moins un élément de renfort dans un moule correspondant au corps de la pièce et à thermocomprimer une matière thermoplastique déposée dans le moule. According to the embodiments, the method of the invention may comprise one or more of the following features: the step of producing the body consists in injecting a thermoplastic material into a mold; the step of producing the reinforcing element comprises the steps of joining several strands of fibers to be stretched through a die and introducing a thermoplastic material into the die; the step of providing the reinforcing member comprises steps of joining a plurality of fiber strands impregnated with thermoplastic material and stretching said fiber strands through a die; The step of producing the reinforcing element comprises the steps of joining several strands of fibers and a wire of material. thermoplastic and to stretch said strands and said wire simultaneously through a die; the step of associating the reinforcing element with the body comprises a welding step; the step of combining the reinforcing element with the body comprises a heat-sealing step; the step of combining the reinforcing element with the body is conducted simultaneously with the step of producing the body of the part and comprises the steps of arranging said at least one reinforcing element in a mold corresponding to the body of the piece and thermocompress a thermoplastic material deposited in the mold.
L'invention concerne aussi l'utilisation d'une pièce thermoplastique selon l'invention ou d'un ensemble selon l'invention pour constituer au moins partiellement une pièce automobile ou au moins partiellement une pièce de chariot. The invention also relates to the use of a thermoplastic component according to the invention or an assembly according to the invention for constituting at least partially an automotive part or at least partially a carriage part.
D'autres caractéristiques et avantages de l'invention apparaîtront à la lecture de la description détaillée qui suit des modes de réalisation de l'invention, donnés à titre 20 d'exemple uniquement et en références aux dessins qui montrent: - figure 1, une vue schématique en perspective d'une pièce renforcée selon l'invention; - figure 2, une vue schématique détaillée d'un élément de renfort de la pièce de la figure 1; - figures 3 à 6, des schémas de différents modes d'association des éléments de renfort avec le corps de la pièce; figure 7, une vue schématique détaillée d'un mode d'association d'un élément de renfort avec le corps de la pièce. Other features and advantages of the invention will appear on reading the following detailed description of the embodiments of the invention, given by way of example only and with reference to the drawings which show: FIG. schematic perspective view of a reinforced part according to the invention; - Figure 2, a detailed schematic view of a reinforcing element of the part of Figure 1; - Figures 3 to 6, diagrams of different modes of association of the reinforcing elements with the body of the room; FIG. 7 is a detailed schematic view of a method of associating a reinforcing element with the body of the part.
L'invention propose une pièce thermoplastique comprenant un corps et au moins un élément de renfort. Le corps est constitué d'un matériau comprenant une première matrice thermoplastique et peut présenter les caractéristiques esthétiques et géométriques souhaitées pour la pièce. L'élément de renfort est constitué d'un matériau comprenant une deuxième matrice thermoplastique et des fibres continues et sensiblement parallèles les unes aux autres. L'élément de renfort est associé directement et de façon irréversible au corps de la pièce. The invention provides a thermoplastic component comprising a body and at least one reinforcing element. The body is made of a material comprising a first thermoplastic matrix and may have the desired aesthetic and geometric characteristics for the part. The reinforcing element is made of a material comprising a second thermoplastic matrix and continuous fibers substantially parallel to each other. The reinforcing element is directly and irreversibly associated with the body of the room.
Les première et deuxième matrices thermoplastiques sont choisies telles qu'une association directe et irréversible peut être réalisée entre les éléments de renfort et le R-Brevets\23100\23148.doc - 27/10/04 - 09.10 4/14 corps de la pièce; en particulier, les première et deuxième matrices thermoplastiques sont des matériaux de la même famille. La fabrication de la pièce renforcée est donc simplifiée, ainsi que son recyclage. The first and second thermoplastic matrices are chosen such that a direct and irreversible association can be achieved between the reinforcing elements and the R-Patent. 233/24 - 09/10/04 - 09.10 4/14 body of the part ; in particular, the first and second thermoplastic matrices are materials of the same family. The manufacture of the reinforced part is thus simplified, as well as its recycling.
La figure 1 est une vue en perspective d'une pièce renforcée selon l'invention. Figure 1 is a perspective view of a reinforced part according to the invention.
Une telle pièce pourrait représenter une tablette arrière de véhicule automobile. La pièce thermoplastique comprend un corps 1 constitué d'un matériau comprenant une matrice thermoplastique, par exemple du polypropylène ou tout autre polyoléfine. Des additifs, tels que des pigments de coloration, des charges anti-UV, des agents de texture ou autre, peuvent être ajoutés à la matrice thermoplastique du corps. Le corps 1 de la pièce est représenté comme un plateau, mais il est entendu que toute autre forme pourrait être concernée par l'invention. Such a piece could represent a rear shelf of a motor vehicle. The thermoplastic part comprises a body 1 made of a material comprising a thermoplastic matrix, for example polypropylene or any other polyolefin. Additives, such as color pigments, anti-UV fillers, texturizing agents, or the like, can be added to the thermoplastic matrix of the body. The body 1 of the piece is shown as a tray, but it is understood that any other form could be concerned by the invention.
La pièce comprend également des éléments de renfort 2 en matériau thermoplastique. Les éléments de renfort sont constitués d'un matériau comprenant une matrice thermoplastique et des fibres continues et sensiblement parallèles les unes aux autres. La matrice thermoplastique des éléments de renfort est choisie de la même famille que la matrice constituant le corps de la pièce, par exemple du polypropylène, du polyamide ou tout autre matériau thermoplastique. Il est entendu qu'un même matériau peut être utilisé pour les matrices thermoplastiques des éléments de renfort et du corps de la pièce. Il est ainsi possible de réaliser une association directe et irréversible entre les éléments de renfort et le corps de la pièce. La pièce peut aussi être recyclée sans démontage. The part also comprises reinforcement elements 2 made of thermoplastic material. The reinforcing elements consist of a material comprising a thermoplastic matrix and continuous fibers substantially parallel to each other. The thermoplastic matrix of the reinforcing elements is chosen from the same family as the matrix constituting the body of the part, for example polypropylene, polyamide or any other thermoplastic material. It is understood that the same material can be used for the thermoplastic matrices of the reinforcing elements and the body of the part. It is thus possible to achieve a direct and irreversible association between the reinforcing elements and the body of the part. The part can also be recycled without dismantling.
On entend par association directe et irréversible un assemblage qui présente une adhérence telle que la pièce se casse si l'on tente de désolidariser les éléments de renfort du corps de la pièce. Par exemple, les éléments de renfort 2 peuvent être soudés ou thermocollés au corps 1 de la pièce ou être réalisés monoblocs avec le corps de la pièce. On entend par monobloc dans ce contexte le fait que les éléments de renforts sont assemblés lors de l'étape de formage du corps de la pièce. The term "direct and irreversible association" is understood to mean an assembly that has an adhesion such that the part breaks if one tries to separate the reinforcing elements from the body of the part. For example, the reinforcing elements 2 may be welded or heat-sealed to the body 1 of the part or be made in one piece with the body of the part. Monoblock in this context means that the reinforcing elements are assembled during the forming step of the body of the part.
Les éléments de renfort 2 présentent la forme d'un profilé allongé, c'està-dire avec une longueur plus grande que la largeur et la hauteur, par exemple avec une longueur égale à au moins trois fois la largeur et la hauteur. Les fibres incorporées dans la matrice des éléments de renfort sont disposées sensiblement parallèles à l'axe longitudinal de ce profilé. The reinforcing elements 2 have the shape of an elongated section, that is to say with a length greater than the width and height, for example with a length equal to at least three times the width and height. The fibers incorporated in the matrix of the reinforcing elements are arranged substantially parallel to the longitudinal axis of this profile.
Les fibres incorporées dans la matrice des éléments de renfort sont dites continues, c'est-à-dire qu'elles s'étendent globalement sur toute la longueur du profilé de renfort; elles ne sont pas incorporées en paillettes ou en morceaux dans la matrice thermoplastique. Les fibres sont aussi dites sensiblement parallèles les unes ou autres, c'est-à-dire qu'elles ne sont pas enchevêtrées. The fibers incorporated in the matrix of the reinforcing elements are said to be continuous, that is to say that they extend generally over the entire length of the reinforcement profile; they are not incorporated in flakes or pieces in the thermoplastic matrix. The fibers are also said to be substantially parallel to each other, that is to say that they are not entangled.
R: \Brevets\23100\23148.doc - 27/10/04 - 09:10 - 5/14 Les fibres des éléments de renfort peuvent être des fibres de verre. On peut également envisager d'utiliser d'autres types de fibres, telles que des fibres minérales comme le carbone, des fibres d'origine végétale comme le lin, le jute, le chanvre, le sisal, ou encore des fibres synthétiques comme l'aramide. Le choix des fibres de renfort dépend des performances mécaniques attendues pour la pièce. La proportion en masse de fibres de verre dans chaque élément de renfort est comprise entre 20% et 80% en poids. La matrice thermoplastique dans laquelle sont noyées les fibres peut être du polypropylène ou tout autre polyoléfine, du polyester, du polyamide ou tout autre matériau thermoplastique. The fibers of the reinforcing elements may be glass fibers. It is also possible to envisage using other types of fibers, such as mineral fibers such as carbon, plant-based fibers such as linen, jute, hemp, sisal, or synthetic fibers such as aramid. The choice of reinforcing fibers depends on the expected mechanical performance of the part. The proportion by mass of glass fibers in each reinforcing element is between 20% and 80% by weight. The thermoplastic matrix in which the fibers are embedded may be polypropylene or any other polyolefin, polyester, polyamide or any other thermoplastic material.
On a aussi obtenu une pièce thermoplastique renforcée, les éléments de renfort présentant, de par la présence des fibres, un module de Young compris entre 10000 et 50000 MPa, soit un module de Young beaucoup plus élevé que celui du corps de la pièce qui peut être compris entre 500 et 7000 MPa. En outre, la contrainte admissible, c'est-à-dire la force de rupture de l'élément de renfort, se situe entre 200 et 900 MPa. A titre de comparaison, on peut citer les valeurs de l'acier qui présente un module de Young de 200000 MPa et une contrainte admissible de 500 MPa. La combinaison de ces deux caractéristiques, à savoir tenue à la contrainte et élasticité, permet de conférer à la pièce renforcée un rôle de limiteur d'accélération qui trouve des applications particulièrement avantageuses pour des pièces automobiles. A reinforced thermoplastic component has also been obtained, the reinforcing elements having, by the presence of the fibers, a Young's modulus of between 10,000 and 50000 MPa, ie a Young's modulus much higher than that of the body of the part which can be between 500 and 7000 MPa. In addition, the allowable stress, that is to say the breaking strength of the reinforcing element, is between 200 and 900 MPa. By way of comparison, mention may be made of the values of the steel which has a Young's modulus of 200,000 MPa and a permissible stress of 500 MPa. The combination of these two characteristics, namely resistance to stress and elasticity, makes it possible to give the reinforced part a role of throttle limiter which finds particularly advantageous applications for automobile parts.
En cas de choc, l'accélération n'est pas directement transmise aux personnes, biens ou pièces mécaniques en contact avec la pièce renforcée car la pièce renforcée résiste et absorbe une partie du choc. De telles pièces renforcées permettent donc d'améliorer la protection des personnes et des biens en contact avec la pièce et permet de réduire le dimensionnement des pièces adjacentes en limitant les efforts transmis. Le ratio module de Young / contrainte admissible des éléments de renfort est plus favorable qu'un renfort métallique pour la maîtrise des efforts. La protection des personnes et le dimensionnement des structures environnantes sont donc améliorés. In case of shock, the acceleration is not directly transmitted to people, goods or mechanical parts in contact with the reinforced part because the reinforced part resists and absorbs part of the shock. Such reinforced parts thus make it possible to improve the protection of persons and goods in contact with the part and makes it possible to reduce the dimensioning of adjacent parts by limiting the forces transmitted. The Young's modulus ratio / allowable stress of the reinforcement elements is more favorable than a metallic reinforcement for the control of the forces. The protection of people and the dimensioning of the surrounding structures are thus improved.
Selon un mode de réalisation, illustré sur la figure 2, les éléments de renfort 2 peuvent être gainés. Les éléments de renfort 2 peuvent être enrobées au moins partiellement par un gainage 3 constitué d'une matière thermoplastique. Le matériau de gainage comprend une matrice thermoplastique compatible avec la matrice thermoplastique l'éléments de renfort, c'est-à-dire de la même famille organique. Le matériau de gainage 3 peut comprendre des additifs, mais est dénué de fibres. According to one embodiment, illustrated in Figure 2, the reinforcing elements 2 can be sheathed. The reinforcing elements 2 may be at least partially coated by a sheath 3 made of a thermoplastic material. The cladding material comprises a thermoplastic matrix compatible with the thermoplastic matrix and the reinforcing elements, that is to say of the same organic family. The cladding material 3 may comprise additives, but is fiber-free.
L'élément de renfort est alors constitué d'une âme structurelle 2 et d'une peau d'aspect 3. Cette peau peut permettre d'améliorer les qualités sensorielles des renforts, en particulier sur le plan tactile, par exemple pour un toucher soft, et sur le plan visuel, par exemple un gainage translucide. En plus de ces avantages sensoriels, R:\Brevets\23100\23148.doc - 27/10/04 - 09:10 - 6/14 le gainage 3 peut améliorer les propriétés mécaniques du renfort 2, notamment en augmentant la contrainte admissible par le renfort selon une direction perpendiculaire au sens des fibres, ce qui améliore la cohésion du renfort. The reinforcing element then consists of a structural core 2 and an aspect skin 3. This skin can improve the sensory qualities of the reinforcements, particularly on the tactile plane, for example for a soft touch , and visually, for example a translucent cladding. In addition to these sensory advantages, the cladding 3 can improve the mechanical properties of the reinforcement 2, in particular by increasing the permissible stress by the reinforcement in a direction perpendicular to the direction of the fibers, which improves the cohesion of the reinforcement.
Les figures 3 à 6 illustrent plusieurs modes d'association des renforts 2 avec le corps 1 de la pièce. Il est à noter que les éléments de renfort 2 présentent une forme générale de profilé allongé, c'est-à-dire que leur longueur est largement plus grande que leur largeur et hauteur, et la section transversale des éléments de renfort 2 reste sensiblement constante sur toute la longueur mais la forme peut varier. Par exemple, des profils transversaux en forme de Sl ( Oméga ), de I , de T , de U , de V , de W , de cercle, de carré, de rectangle ou toute autre forme de parallélépipède peuvent être envisagés. Figures 3 to 6 illustrate several ways of combining the reinforcements 2 with the body 1 of the room. It should be noted that the reinforcing elements 2 have a generally elongated shape, that is to say that their length is much greater than their width and height, and the cross section of the reinforcing elements 2 remains substantially constant over the entire length but the shape may vary. For example, transverse profiles in the form of Sl (Omega), I, T, U, V, W, circle, square, rectangle or any other parallelepiped shape may be envisaged.
Sur la figure 3, le corps 1 est une pièce sensiblement plane et les éléments de renforts 2 présentent une section transversale en forme de T, la barre horizontale du T étant soudée au corps 1. In FIG. 3, the body 1 is a substantially flat piece and the reinforcing elements 2 have a T-shaped cross-section, the horizontal bar of the T being welded to the body 1.
Sur la figure 4, le corps 1 de la pièce est une pièce présentant des nervures 11 et les éléments de renforts 2 présentent une section transversale en forme de T, la barre horizontale du T étant soudée au fond de la nervure 11 du corps 1. In FIG. 4, the body 1 of the part is a part having ribs 11 and the reinforcing elements 2 have a T-shaped cross section, the horizontal bar of the T being welded to the bottom of the rib 11 of the body 1.
Sur la figure 5, le corps 1 est une pièce présentant des rainures 12 et les éléments de renforts 2 présentent une section transversale en forme de T inversée, la barre verticale du T étant logée dans la rainure 12 du corps 1 et la barre horizontale du T soudée sur l'extrémité des rainures 12. In FIG. 5, the body 1 is a part having grooves 12 and the reinforcing elements 2 have an inverted T-shaped cross section, the vertical bar of the T being housed in the groove 12 of the body 1 and the horizontal bar of the T welded on the end of the grooves 12.
Sur la figure 6, le corps 1 de la pièce est un plateau double coque 13 à l'intérieur duquel sont intégrés les éléments de renfort 2 présentant une section transversale en forme de V inversée. Les renforts 2 sont de préférence soudés de part et d'autre de la coque 13. Le corps 1 de la pièce peut également comprendre des entretoises 14 ajoutées entre les parois de la double coque 13. In Figure 6, the body 1 of the part is a double shell plate 13 inside which are integrated the reinforcing elements 2 having an inverted V-shaped cross section. The reinforcements 2 are preferably welded on either side of the shell 13. The body 1 of the part may also comprise spacers 14 added between the walls of the double shell 13.
Sur la figure 7, une portion du corps 1 présente une forme non plane, éventuellement une forme en trois dimensions, avec des rainures 12. L'élément de renfort 2 présente une section transversale en forme de rectangle soudé sur 30 l'extrémité des rainures. In Figure 7, a portion of the body 1 has a non-planar shape, possibly a three-dimensional shape, with grooves 12. The reinforcing member 2 has a rectangle-shaped cross section welded to the end of the grooves .
Par ailleurs, un ou plusieurs renforts 2 peuvent être galbés longitudinalement, bien que cela ne soit pas illustré sur les figures, par exemple pour s'adapter à un corps 1 galbé. Par exemple, un renfort 2 d'une épaisseur de 1 à 6 mm et d'une largeur quelconque peut être galbé sur toute ou partie de la longueur du corps de pièce. Moreover, one or more reinforcements 2 may be curved longitudinally, although this is not illustrated in the figures, for example to fit a body 1 curved. For example, a reinforcement 2 having a thickness of 1 to 6 mm and any width may be curved over all or part of the length of the workpiece body.
La géométrie du corps 1, celle des éléments de renfort 2 et les géométries d'association qui en découlent, sont laissées à l'appréciation de l'homme du métier, selon les valeurs de résistance à la flexion à obtenir. La géométrie des renforts est R:'Brevets\23100\23148.doc - 27/10/04 - 09:10 7/14 donc choisie en fonction des contraintes mécaniques à respecter, et en particulier la résistance à la flexion à obtenir pour la pièce. Le nombre de renforts, leurs emplacements sur le corps dépendent également de la valeur à respecter en flexion sous charge. The geometry of the body 1, that of the reinforcing elements 2 and the resulting association geometries are left to the appreciation of the skilled person, according to the flexural strength values to be obtained. The geometry of the reinforcements is thus chosen as a function of the mechanical stresses to be respected, and in particular the flexural strength to be obtained for the first time. room. The number of reinforcements, their locations on the body also depend on the value to be respected in flexion under load.
De plus, lors du formage du corps 1 de la pièce, par injection dans un moule par exemple, le corps obtenu peut être déformé par rapport à la forme attendue. L'association des éléments de renfort 2 au corps 1 permet alors de rattraper ces déformations lors du soudage des éléments 2. In addition, during the forming of the body 1 of the part, by injection into a mold for example, the body obtained can be deformed with respect to the expected shape. The combination of the reinforcing elements 2 to the body 1 then makes it possible to compensate for these deformations during the welding of the elements 2.
Il est à noter que la pièce renforcée selon l'invention, comprenant un corps 1 de pièce et un ou des renforts 2, peut être recouverte, totalement ou partiellement, d'un habillage. Un tel habillage peut être un caisson en matériau thermoplastique ou en matériau fibreux ou en tout autre matériau isolant; l'habillage peut aussi être un tissu enveloppant la pièce renforcée, tel qu'un feutre par exemple. It should be noted that the reinforced part according to the invention, comprising a body 1 of part and one or reinforcements 2, can be covered, totally or partially, a covering. Such a covering may be a box made of thermoplastic material or fibrous material or any other insulating material; the covering may also be a fabric wrapping the reinforced part, such as a felt for example.
La pièce thermoplastique renforcée selon l'invention peut être fabriquée de la 15 manière suivante. The reinforced thermoplastic part according to the invention can be manufactured in the following manner.
On réalise un corps 1 de pièce comprenant une matière thermoplastique par injection thermoplastique, soufflage, thermoformage, rotomoulage, thermocompression, ou toute autre technologie courante de formage de pièces en matériaux thermoplastiques. Les dimensions et formes du corps de la pièce peuvent être très variables selon les applications envisagées. A body 1 comprising a thermoplastic thermoplastic injection molding, blowing, thermoforming, rotational molding, thermocompression, or other common technology for forming parts made of thermoplastic materials is produced. The dimensions and shapes of the body of the part can be very variable according to the envisaged applications.
La matière du corps 1 de la pièce peut contenir des charges minérales, comme du talc ou du verre, ou végétales. Les charges peuvent être des fibres naturelles cellulosiques, comme le lin, le jute, le sisal, dans des proportions variant entre 30% et 70%, et préférentiellement 50/50. Dans une variante, le corps 1 comprend au moins une couche de matériau non-tissé, un feutre par exemple, et une couche de matière thermoplastique, ceux deux couches étant liées par chauffage puis compactage. Le matériau ainsi obtenu présente un module Young compris entre 500 et 7000 MPa à 23 C (1MPa = 1 N/mm2). The material of the body 1 of the part may contain mineral fillers, such as talc or glass, or vegetable. The fillers may be natural cellulosic fibers, such as flax, jute or sisal, in proportions varying between 30% and 70%, and preferably 50/50. In a variant, the body 1 comprises at least one layer of nonwoven material, a felt for example, and a layer of thermoplastic material, those two layers being bonded by heating then compacting. The material thus obtained has a Young's modulus of between 500 and 7000 MPa at 23 ° C. (1 MPa = 1 N / mm 2).
On réalise aussi au moins un élément de renfort 2 comprenant des fibres continues sensiblement parallèles incorporées dans une matrice thermoplastique. At least one reinforcement element 2 is also made comprising substantially parallel continuous fibers incorporated in a thermoplastic matrix.
Par exemple, les éléments de renfort 2 peuvent être obtenus par pultrusion. Plusieurs brins de fibres continus sont réunis parallèlement et introduit dans une filière. Une matière thermoplastique peut être introduite dans la filière pendant que les fibres sont étirées pour former l'élément de renfort 2. La forme de la section transversale de l'élément de renfort 2 est fonction du calibre de la filière utilisée. On peut également utiliser un fil composite réunissant des brins de fibre et de matière thermoplastique comme décrit dans la demande de brevet FR-A-2 638 467 et chauffer la ligne en amont de la filière pour ramollir la matière thermoplastique afin R:\Brevets\23100\23148.doc - 27/10/04 - 09:10 - 8/14 d'incorporer les fibres dans le plastique. On peut aussi utiliser des brins de fibres et un fil de matière thermoplastique introduit dans la filière en même temps que les brins de fibres. La matière thermoplastique est chauffée avant introduction dans la filière et les fibres sont incorporées dans le plastique en sortie de la filière. For example, the reinforcing elements 2 can be obtained by pultrusion. Several continuous fiber strands are joined in parallel and introduced into a die. A thermoplastic material may be introduced into the die while the fibers are stretched to form the reinforcing member 2. The shape of the cross section of the reinforcing member 2 is a function of the size of the die used. It is also possible to use a composite yarn joining fiber and thermoplastic fiber strands as described in the patent application FR-A-2,638,467 and heating the line upstream of the die to soften the thermoplastic material in order to: 23100 \ 23148.doc - 27/10/04 - 09:10 - 8/14 to incorporate the fibers into the plastic. It is also possible to use fiber strands and a wire of thermoplastic material introduced into the die at the same time as the fiber strands. The thermoplastic material is heated before introduction into the die and the fibers are incorporated into the plastic at the outlet of the die.
Dans le cas d'un élément de renfort gainé, comme illustré sur la figure 2, on forme d'abord un profilé dans lequel les fibres et la matière thermoplastique sont rassemblées parallèlement et on introduit ce profilé dans une filière calibrée dans laquelle on introduit simultanément au moins une deuxième matière thermoplastique fondue au contact du profilé pour constituer le gainage. In the case of a sheathed reinforcing element, as illustrated in FIG. 2, a profile is firstly formed in which the fibers and the thermoplastic material are brought together in parallel, and this profile is introduced into a calibrated die into which at the same time at least one second molten thermoplastic material in contact with the profile to form the cladding.
On associe alors les éléments de renfort au corps pour constituer la pièce renforcée. Une association directe et irréversible peut être obtenue par un soudage, de préférence sans contact tel qu'un soudage par rayonnement infrarouge. The reinforcing elements are then associated with the body to form the reinforced part. A direct and irreversible association can be obtained by welding, preferably without contact such as infrared radiation welding.
Dans un soudage sans contact, la soudure se fait par rayonnement. De l'énergie sous forme de chaleur est apporté au niveau de la surface de contact pour provoquer une fusion superficielle de la matière. La source d'énergie peut être un laser, un fil émissif infrarouge, un émetteur ultrasons ou haute fréquence, ou autre. Lors de la mise en contact des pièces à souder, il y a interpénétration des surfaces de contact, ce qui se traduit au niveau moléculaire par un enchevêtrement des chaînes de polymères. Au moment du refroidissement, les chaînes de polymères adoptent une nouvelle structure tridimensionnelle assurant ainsi une association directe et irréversible des pièces soudées. Le soudage se fait uniquement par fusion des deux pièces à assembler, sans apport de matières supplémentaire. In contactless welding, the welding is done by radiation. Energy in the form of heat is provided at the contact surface to cause surface melting of the material. The energy source may be a laser, an infrared emissive wire, an ultrasonic or high frequency emitter, or the like. When the parts to be welded come into contact, the contact surfaces interpenetrate, which is reflected at the molecular level by entanglement of the polymer chains. At the time of cooling, the polymer chains adopt a new three-dimensional structure thus ensuring a direct and irreversible association of the welded parts. The welding is done only by merging the two parts to be assembled, without adding additional materials.
L'association des éléments de renfort 2 avec le corps 1 de la pièce peut être réalisée par toute autre technique de soudage appropriée, tels que le soudage miroir ou le soudage par vibration par exemple, et peut également être faite par collage, notamment par collage à chaud (hotmelt). On préférera cependant le soudage au collage car le soudage ne nécessite aucun apport de matière extérieure alors que le collage nécessite une enduction de colle thermoplastique sur au moins l'une des pièces à assembler. The combination of the reinforcing elements 2 with the body 1 of the part can be achieved by any other suitable welding technique, such as mirror welding or vibration welding for example, and can also be done by gluing, especially by gluing. hot (hotmelt). However, bonding welding is preferred because welding does not require any addition of external material, whereas bonding requires a coating of thermoplastic adhesive on at least one of the parts to be assembled.
Si les éléments de renforts 2 sont gainés 3, le soudage ou le collage sera fait entre cette gaine 3 thermoplastique et le corps 1. If the reinforcing elements 2 are sheathed 3, the welding or bonding will be done between this thermoplastic sheath 3 and the body 1.
Dans un mode de réalisation particulier, lorsque le corps 1 est réalisé par thermoformage ou thermocompression, l'association des éléments de renfort 2 au corps peut se faire directement lors de la mise en forme du corps. On parle alors de procédé en une seule étape, ou one shot . In a particular embodiment, when the body 1 is made by thermoforming or thermocompression, the association of the reinforcing elements 2 to the body can be done directly during the shaping of the body. This is called a one-step process, or one shot.
Les éléments de renfort 2 sont fabriqués selon l'un des modes de réalisation précités ou toute autre mode approprié. Les éléments 2 sont ensuite déposés dans le moule destiné à former le corps 1 de la pièce. Le matériau constituant le corps est R:\ Brevets\ 23100\23148.doc - 27/10/04 - 09:10 - 9/14 chauffé au dessus de sa température de fusion et déposé dans le moule froid. Le matériau du corps est alors thermocomprimé dans le moule afin de former le corps en_ assemblant simultanément les éléments de renfort. La surface des renforts 2 destinée à être adjacente au corps de pièce peut être réactivée, c'est-à-dire chauffée, avant leur mise en place dans le moule pour améliorer l'adhérence entre les renforts et le corps de pièce. The reinforcing elements 2 are manufactured according to one of the aforementioned embodiments or any other appropriate mode. The elements 2 are then deposited in the mold intended to form the body 1 of the part. The material constituting the body is heated above its melting point and deposited in the cold mold. The body material is then thermocompressed in the mold to form the body while simultaneously assembling the reinforcing members. The surface of the reinforcements 2 intended to be adjacent to the workpiece body can be reactivated, that is to say heated, before they are put into place in the mold to improve the adhesion between the reinforcements and the workpiece body.
La pièce thermoplastique renforcée selon l'invention peut être utilisée pour les applications suivantes. The reinforced thermoplastic part according to the invention can be used for the following applications.
La pièce peut constituer au moins partiellement une pièce automobile, telle qu'un hayon de coffre, une tablette arrière, un plancher de coffre, un plancher d'habitacle, un écran sous moteur, une portière, des barres de toit, des barres antiintrusion, ou toute autre pièce ayant à répondre à un cahier des charges de tenue mécanique ou de résistance aux chocs. The part can be at least partially a car part, such as a tailgate, a rear shelf, a trunk floor, a cockpit floor, a screen under engine, a door, roof bars, anti-extrusion bars , or any other part having to meet a specification of mechanical strength or impact resistance.
La pièce peut aussi constituer au moins partiellement une pièce de chariot, par exemple un fond ou une poignée, en particulier une poignée télescopique. The part may also be at least partially a carriage part, for example a bottom or a handle, in particular a telescopic handle.
Le nombre de renforts et leur emplacement dépend directement de la rigidité souhaitée pour la pièce semi- structurelle. Par exemple, une tablette autoporteuse de dimension 1000 mm * 500 mm * 65 mm sera ainsi avantageusement rigidifiée par deux éléments d'au moins 900 mm de long placés à 200 mm de distance l'un de l'autre. The number of reinforcements and their location depends directly on the desired rigidity for the semi-structural part. For example, a self-supporting tablet of size 1000 mm * 500 mm * 65 mm will thus be advantageously stiffened by two elements of at least 900 mm long placed at 200 mm distance from one another.
R:\Brevets\23100\23148.doc - 27/10/04 - 09:10 - 10/14 R: \ Patents \ 23100 \ 23148.doc - 27/10/04 - 09:10 - 10/14
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Cited By (6)
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EP1808285A1 (en) * | 2006-01-17 | 2007-07-18 | Mecaplast Sam | Reinforced plastic piece |
DE102006041653A1 (en) * | 2006-08-24 | 2008-02-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Composite structure and method of making a composite structure |
EP2006066A2 (en) * | 2007-06-22 | 2008-12-24 | Ford Global Technologies, LLC. | Moulded-in-colour panel and method for moulding such |
EP2134533A2 (en) * | 2007-03-29 | 2009-12-23 | Carbone Forge | Method for making a thermoplastic composite part by moulding |
US8343409B2 (en) | 2007-06-22 | 2013-01-01 | Ford Global Technologies, Llc | Molding system and molded-in-color panel |
US9090003B2 (en) | 2007-02-12 | 2015-07-28 | Ford Global Technologies, Llc | Molded-in-color vehicle panel and mold |
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