FR3111582A1 - Manufacturing process of a thermoplastic material part incorporating heating elements - Google Patents
Manufacturing process of a thermoplastic material part incorporating heating elements Download PDFInfo
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- FR3111582A1 FR3111582A1 FR2006504A FR2006504A FR3111582A1 FR 3111582 A1 FR3111582 A1 FR 3111582A1 FR 2006504 A FR2006504 A FR 2006504A FR 2006504 A FR2006504 A FR 2006504A FR 3111582 A1 FR3111582 A1 FR 3111582A1
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- thermoplastic material
- heating element
- mold
- ribs
- heating
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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
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/0053—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor combined with a final operation, e.g. shaping
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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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/0272—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using lost heating elements, i.e. heating means incorporated and remaining in the formed article
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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
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/18—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression 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
- 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
- B29C45/14065—Positioning or centering articles in the mould
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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
- B29C45/17—Component parts, details or accessories; Auxiliary operations
- B29C45/26—Moulds
- B29C45/2626—Moulds provided with a multiplicity of narrow cavities connected to a common cavity, e.g. for brushes, combs
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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
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/3404—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
- B29C65/344—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint being a woven or non-woven fabric or being a mesh
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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
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/36—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
- B29C65/3604—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint
-
- 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
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/36—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
- B29C65/3604—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint
- B29C65/364—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint being a woven or non-woven fabric or being a mesh
-
- 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
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/36—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
- B29C65/3668—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the means for supplying heat to said heated elements which remain in the join, e.g. special induction coils
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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
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/36—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
- B29C65/3672—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the composition of the elements heated by induction which remain in the joint
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C2035/0211—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould resistance heating
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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
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/08—Transition metals
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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
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/08—Transition metals
- B29K2705/10—Copper
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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
- B29L2031/34—Electrical apparatus, e.g. sparking plugs or parts thereof
- B29L2031/3481—Housings or casings incorporating or embedding electric or electronic elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Textile Engineering (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Thermal Sciences (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
Abstract
Procédé de fabrication d’une pièce en matériau thermoplastique intégrant des éléments chauffants Un procédé de fabrication d’une pièce en matériau thermoplastique apte à être soudée à une autre pièce comprend l’injection ou la compression à chaud d’un matériau thermoplastique (130) dans un moule (50) et le démoulage de la pièce en matériau thermoplastique. Le procédé comprend en outre le placement d’un ou plusieurs éléments chauffants (120) dans le moule (50) avant l’introduction du matériau thermoplastique (130). Le ou les éléments chauffants (120) sont placés dans une ou plusieurs parties du moules correspondant à une ou plusieurs surfaces d’assemblage (101) de la pièce en matériau thermoplastique. Figures pour l’abrégé : Fig. 4 et 5. Process for manufacturing a part in thermoplastic material incorporating heating elements A method of manufacturing a part made of thermoplastic material capable of being welded to another part comprises the injection or hot compression of a thermoplastic material (130) in a mold (50) and the demolding of the part made of thermoplastic. The method further includes placing one or more heating elements (120) in the mold (50) prior to introducing the thermoplastic material (130). The heating element(s) (120) are placed in one or more parts of the mold corresponding to one or more assembly surfaces (101) of the part made of thermoplastic material. Figures for the abstract: Fig. 4 and 5.
Description
La présente invention se rapporte au domaine des pièces en matériau thermoplastique et, plus particulièrement à l’assemblage par soudage de telles pièces.The present invention relates to the field of parts made of thermoplastic material and, more particularly, to the assembly by welding of such parts.
Les matériaux thermoplastiques et en particulier les matériaux composites comprenant des fibres de renfort, par exemple des fibres de carbone et/ou des fibres de verre, dispersées dans une matrice polymère thermoplastique ont de nombreux usages possibles, et notamment, dans le domaine de l’aéronautique.
Pour la réalisation de certaines structures, il peut être nécessaire d’assembler plusieurs pièces en matériau thermoplastique comme, par exemple, pour un volet d’inverseur de poussée, un panneau raidi, des raidisseurs, des parties de carénage, etc.
Ces pièces composites peuvent être assemblées par soudage, notamment par une technologie de type :Thermoplastic materials and in particular composite materials comprising reinforcing fibers, for example carbon fibers and/or glass fibers, dispersed in a thermoplastic polymer matrix have many possible uses, and in particular, in the field of aeronautics.
For the realization of certain structures, it may be necessary to assemble several parts in thermoplastic material such as, for example, for a thrust reverser flap, a stiffened panel, stiffeners, fairing parts, etc.
These composite parts can be assembled by welding, in particular by a technology of the type:
- soudage par induction,- induction welding,
- soudage résistif,- resistive welding,
- soudage par chauffe et pression- heat and pressure welding
- soudage par ultrason, soudage laser.- ultrasonic welding, laser welding.
Le document EP 2 907 651 décrit un procédé de soudage par induction dans lequel on soumet à un champ magnétique un ensemble formé de deux pièces à souder en matériau composite à matrice thermoplastique et d’un absorbeur de champ ou suscepteur positionné à l’interface entre les pièces. Le champ magnétique provoque l’élévation en température du suscepteur jusqu’à une température permettant le ramollissement ou la fusion de la résine thermoplastique.
L’interposition d’un suscepteur entre les pièces à souder présente néanmoins l’inconvénient de complexifier techniquement l’opération de soudage par la nécessité de positionner avec précision le suscepteur et de le maintenir en position entre les pièces pendant le soudage. En outre, l’utilisation d’un suscepteur entraîne une augmentation du temps et du coût de fabrication. Par ailleurs, la présence d’un suscepteur à l’interface de liaison entre les deux pièces peut nuire à la tenue mécanique de la structure résultante en service.Document EP 2 907 651 describes an induction welding process in which an assembly formed by two parts to be welded made of composite material with a thermoplastic matrix and a field absorber or susceptor positioned at the interface between rooms. The magnetic field causes the temperature of the susceptor to rise to a temperature allowing the softening or melting of the thermoplastic resin.
The interposition of a susceptor between the parts to be welded nevertheless has the disadvantage of technically complicating the welding operation by the need to position the susceptor with precision and to maintain it in position between the parts during the welding. Further, the use of a susceptor results in an increase in manufacturing time and cost. Furthermore, the presence of a susceptor at the connection interface between the two parts can adversely affect the mechanical strength of the resulting structure in service.
La présente invention a donc pour but principal de proposer une solution pour le soudage d’une pièce en matériau thermoplastique qui ne présente pas les inconvénients précités.The main purpose of the present invention is therefore to propose a solution for welding a part made of thermoplastic material which does not have the aforementioned drawbacks.
Conformément à l’invention, ce but est atteint grâce à un procédé de fabrication d’une pièce en matériau thermoplastique apte à être soudée à une autre pièce, le procédé comprenant l’injection ou la compression à chaud d’un matériau thermoplastique dans un moule et le démoulage de la pièce en matériau thermoplastique, caractérisé en ce qu’il comprend en outre le placement d’un ou plusieurs éléments chauffants dans le moule avant l’introduction du matériau thermoplastique, le ou les éléments chauffants étant placés dans une ou plusieurs parties du moule correspondant à une ou plusieurs surfaces d’assemblage de la pièce en matériau thermoplastique.According to the invention, this object is achieved by means of a process for manufacturing a part made of thermoplastic material capable of being welded to another part, the process comprising the injection or the hot compression of a thermoplastic material in a mold and the demolding of the part made of thermoplastic material, characterized in that it also comprises the placing of one or more heating elements in the mold before the introduction of the thermoplastic material, the heating element(s) being placed in one or more several parts of the mold corresponding to one or more assembly surfaces of the part made of thermoplastic material.
En surmoulant ou noyant un ou plusieurs éléments chauffants dans une ou plusieurs parties de la pièce, on s’affranchit des problèmes liés à l’utilisation d’un suscepteur rapporté décrits précédemment. L’intégration d’un ou plusieurs éléments chauffants dans le matériau thermoplastique de la pièce permet de faciliter le positionnement entre les pièces à assembler avec une bonne répétabilité lors d’une production en séries. Le procédé de l’invention permet d’éviter l’utilisation d’un suscepteur qui constitue une opération supplémentaire qui peut être pénalisante techniquement ou économiquement (positionnement manuel pouvant être complexe, coût et pose du composant). La présence du suscepteur peut en outre nuire à la tenue de la pièce en service.By overmolding or embedding one or more heating elements in one or more parts of the part, the problems associated with the use of an attached susceptor described above are overcome. The integration of one or more heating elements in the thermoplastic material of the part facilitates positioning between the parts to be assembled with good repeatability during mass production. The method of the invention makes it possible to avoid the use of a susceptor which constitutes an additional operation which can be technically or economically penalizing (manual positioning which can be complex, cost and installation of the component). The presence of the susceptor may also impair the behavior of the part in service.
Par ailleurs, avec un ou plusieurs éléments chauffants surmoulés ou noyés dans le matériau thermoplastique de la pièce, on contrôle la diffusivité thermique au sein de celle-ci. En effet, il est ainsi possible de chauffer localement le matériau thermoplastique de la pièce au-delà de son point de fusion au niveau de la ou les surfaces d’assemblage de celle-ci tout en conservant dans le reste du matériau de la pièce une température suffisamment basse pour assurer sa stabilité géométrique et un niveau de cristallinité maîtrisé.Furthermore, with one or more heating elements overmoulded or embedded in the thermoplastic material of the part, the thermal diffusivity within the latter is controlled. Indeed, it is thus possible to locally heat the thermoplastic material of the part beyond its melting point at the level of the assembly surface(s) of the latter while maintaining in the rest of the material of the part a temperature low enough to ensure its geometric stability and a controlled level of crystallinity.
Selon un mode de réalisation du procédé selon l’invention, le ou les éléments chauffants sont réalisés en un matériau apte à s’échauffer sous l’effet d’un champ magnétique.According to one embodiment of the method according to the invention, the heating element or elements are made of a material capable of heating up under the effect of a magnetic field.
Selon un autre mode de réalisation du procédé selon l’invention, le ou les éléments chauffants sont de type résistif et sont réalisés en un matériau apte à s’échauffer sous l’effet d’un courant électrique. Dans ce cas, le procédé peut comprendre en outre le placement de connecteurs dans le moule avant l’introduction du matériau thermoplastique, lesdits connecteurs étant reliés électriquement à un ou plusieurs éléments chauffants.According to another embodiment of the method according to the invention, the heating element or elements are of the resistive type and are made of a material capable of heating up under the effect of an electric current. In this case, the method may further comprise the placement of connectors in the mold before the introduction of the thermoplastic material, said connectors being electrically connected to one or more heating elements.
Selon une caractéristique particulière du procédé de l’invention, le ou les éléments chauffants sont réalisés à partir d’un grillage, d’un treillis ou d’un fil en matériau conducteur électriquement et thermiquement. Le matériau conducteur électriquement et thermiquement peut être notamment choisi parmi un des matériaux suivants : cuivre, laiton, bronze, acier, alliage de nickel, titane et fibres de carbone continues. Dans le cas où le ou les éléments chauffants réalisés à partir d’un grillage ou d’un treillis, le grillage ou le treillis présente de préférence une taille de maile supérieure à 1 mm de manière à faciliter le passage du matériau thermoplastique ramolli ou fondu. On favorise ainsi les jonctions entre les chaînes de polymères des pièces assemblées, ce qui renforce la liaison par soudage.According to a particular characteristic of the method of the invention, the heating element or elements are made from a mesh, a mesh or a wire made of an electrically and thermally conductive material. The electrically and thermally conductive material may in particular be chosen from one of the following materials: copper, brass, bronze, steel, nickel alloy, titanium and continuous carbon fibers. In the case where the heating element(s) made from a grid or a mesh, the grid or the mesh preferably has a mesh size greater than 1 mm so as to facilitate the passage of the softened or molten thermoplastic material . This promotes the junctions between the polymer chains of the assembled parts, which reinforces the connection by welding.
Selon une autre caractéristique particulière du procédé de l’invention, le matériau thermoplastique comprend une résine seule ou une résine chargée avec des fibres courtes.According to another particular characteristic of the method of the invention, the thermoplastic material comprises a single resin or a resin filled with short fibers.
Selon un autre mode de réalisation du procédé selon l’invention, le moule présente une pluralité de cavités formant un réseau de nervures, le ou les éléments chauffants étant placés dans le fond des cavités de manière à être présents à un sommet des nervures de la pièce en matériau thermoplastique.According to another embodiment of the method according to the invention, the mold has a plurality of cavities forming a network of ribs, the heating element or elements being placed in the bottom of the cavities so as to be present at a top of the ribs of the piece of thermoplastic material.
L’invention a également pour objet un procédé de fabrication d’une structure comprenant au moins une première pièce en matériau thermoplastique et une deuxième pièce, le procédé comprenant la fabrication d’une première pièce en matériau thermoplastique selon le procédé de fabrication d’une pièce en matériau thermoplastique de l’invention, l’accostage de la ou les surfaces d’assemblage de la première pièce avec une deuxième pièce et l’échauffement du ou des éléments chauffants présents dans la première pièce de manière à souder ladite première pièce à la deuxième pièce.The invention also relates to a method for manufacturing a structure comprising at least a first part made of thermoplastic material and a second part, the method comprising the manufacture of a first part made of thermoplastic material according to the method for manufacturing a part made of thermoplastic material of the invention, the docking of the assembly surface(s) of the first part with a second part and the heating of the heating element(s) present in the first part so as to weld said first part to the second piece.
Selon un mode de réalisation du procédé de fabrication d’une structure selon l’invention, la première pièce en matériau thermoplastique comporte un réseau de nervures, le ou les éléments chauffants étant présents à un sommet des nervures de la pièce en matériau thermoplastique et dans lequel la deuxième pièce correspond à une peau en matériau composite à fibres continues, le sommet des nervures comportant le ou les éléments chauffants étant en contact avec la peau en matériau composite lors de l’échauffement du ou des éléments chauffants de manière à souder la première pièce à ladite peau.According to one embodiment of the method for manufacturing a structure according to the invention, the first part made of thermoplastic material comprises a network of ribs, the heating element(s) being present at a top of the ribs of the part made of thermoplastic material and in which the second part corresponds to a skin made of composite material with continuous fibers, the top of the ribs comprising the heating element(s) being in contact with the skin made of composite material during the heating of the heating element(s) so as to weld the first piece to said skin.
La
Comme illustré sur la
Une fois le grillage 120 mis en place, on ferme le moule 50 avec un couvercle 53 qui comporte des blocs 55 permettant de diviser la cavité de moulage 51 en une pluralité de cavité 56 formant un réseau de nervures (figures 3 et 5).Once the grid 120 has been put in place, the mold 50 is closed with a lid 53 which comprises blocks 55 making it possible to divide the molding cavity 51 into a plurality of cavities 56 forming a network of ribs (FIGS. 3 and 5).
Une fois le moule 50 fermé, on injecte sous pression et à chaud un matériau thermoplastique 130 dans le moule via un port d’injection 54 comme représenté sur les figures 4 et 5.Once the mold 50 is closed, a thermoplastic material 130 is injected under pressure and hot into the mold via an injection port 54 as shown in Figures 4 and 5.
Après l’injection et le refroidissement du moule, on démoule la pièce en matériau thermoplastique 100 comprenant le réseau de nervures 110 et le grillage 120 surmoulé dans le matériau thermoplastique 130 au niveau du sommet 111 des nervures (
Le matériau thermoplastique utilisé pour former la pièce peut être de différents types. A titre d’exemples non limitatifs, la pièce selon l’invention peut être réalisée avec un des matériaux thermoplastique suivants : PAEK (PolyArylEtherCetone), PEEK (PolyEtherEtherCetone), PEKK (PolyEtherCetoneCetone), PEI (polyétherimide), TPU ou PU (Polyuréthane Thermoplastique), PESU ou PPS (polysulfure de phénylène).Le matériau thermoplastique peut être sous forme d’une résine seule ou d’une résine chargée en particulier avec des fibres courtes qui peuvent être des fibres de carbone, de verre, d’aramide, etc.The thermoplastic material used to form the part can be of different types. By way of non-limiting examples, the part according to the invention can be made with one of the following thermoplastic materials: PAEK (PolyArylEtherCetone), PEEK (PolyEtherEtherCetone), PEKK (PolyEtherCetoneCetone), PEI (polyetherimide), TPU or PU (Thermoplastic Polyurethane ), PESU or PPS (phenylene polysulphide). The thermoplastic material can be in the form of a single resin or a resin filled in particular with short fibers which can be carbon, glass, aramid, etc
La pièce peut également être réalisée par moulage par compression d’un matériau composite à renfort de fibres longues discontinues du type BMC (Bulk Molding Compound), SMC (Sheet Molding Compound) ou DLF (Discontinuous Long Fibers).The part can also be produced by compression molding of a composite material reinforced with discontinuous long fibers of the BMC (Bulk Molding Compound), SMC (Sheet Molding Compound) or DLF (Discontinuous Long Fibers) type.
La taille des fibres est comprise typiquement entre 0,1 mm et 1 mm pour les fibres courtes et entre 1 mm et 50 mm pour les fibres longues.The size of the fibers is typically between 0.1 mm and 1 mm for the short fibers and between 1 mm and 50 mm for the long fibers.
Le ou les éléments chauffants surmoulés dans le matériau thermoplastique de la pièce peuvent être réalisés en un matériau apte à s’échauffer sous l’effet d’un champ magnétique et/ou d’un courant électrique. A titre d’exemples non limitatifs, le ou les éléments chauffants peuvent être réalisés avec un des matériaux suivants : cuivre, laiton, bronze, acier, alliage de nickel, titane et fibres de carbone continues.The heating element(s) molded into the thermoplastic material of the part can be made of a material capable of heating up under the effect of a magnetic field and/or an electric current. By way of non-limiting examples, the heating element(s) can be made from one of the following materials: copper, brass, bronze, steel, nickel alloy, titanium and continuous carbon fibers.
Le ou les éléments chauffants peuvent être réalisés à partir d’un grillage ou treillis comme décrit précédemment ou d’un fil en matériau conducteur électriquement et thermiquement.The heating element(s) can be made from a grid or mesh as described above or from a wire made of an electrically and thermally conductive material.
La
Dans le cas d’un soudage de type résistif, le ou les fils surmoulés dans une pièce en thermoplastique présentent de préférence un diamètre ou section compris entre 10 µm et 2 mm. Ils sont de préférence mais non exclusivement réalisés avec un des matériaux suivants : cuivre, bronze, laiton et acier.In the case of resistive-type welding, the wire or wires overmolded in a thermoplastic part preferably have a diameter or cross-section of between 10 μm and 2 mm. They are preferably but not exclusively made with one of the following materials: copper, bronze, brass and steel.
Dans le cas où le ou les éléments chauffants sont réalisés à partir d’un grillage ou treillis, celui-ci présente de préférence une taille de maille supérieure à 1 mm. En effet, si le grillage ou le treillis est présent en sommet de pièce, comme par exemple en sommet de nervures, et que les mailles sont trop serrées, le matériau thermoplastique fondu ou ramolli peut avoir des difficultés à migrer à l’interface avec l’autre pièce. Cela peut empêcher que les chaines de polymère des deux pièces se mêlent entre elles, ce qui permet d’obtenir un bon soudage.In the case where the heating element or elements are made from a grid or trellis, the latter preferably has a mesh size greater than 1 mm. Indeed, if the mesh or mesh is present at the top of the part, for example at the top of the ribs, and the meshes are too tight, the molten or softened thermoplastic material may have difficulty migrating to the interface with the other room. This can prevent the polymer chains of the two parts from intermingling, resulting in a good weld.
On décrit maintenant un procédé de fabrication d’une structure conformément à un mode de réalisation de l’invention entre la pièce en matériau thermoplastique 100 décrite précédemment et une peau 300. Le procédé débute, comme illustré sur la
Une fois les pièces 100 et 300 positionnées l’une par rapport à l’autre en maintenant la surface d’assemblage 101 de la pièce 100 en contact avec la surface d’assemblage 301 de la pièce 300, on procède à l’opération de soudage comme illustré sur la
Sous l’effet du champ magnétique, le grillage 120 présent au niveau de la surface d’assemblage 101 s’échauffe de manière à faire fondre localement le matériau thermoplastique de la pièce 100 au plus près de l’interface d’assemblage entre les deux pièces et souder ces dernières entre elles. On applique de préférence une pression P entre sur deux pièces pendant le soudage.Under the effect of the magnetic field, the mesh 120 present at the level of the assembly surface 101 heats up so as to locally melt the thermoplastic material of the part 100 as close as possible to the assembly interface between the two parts and weld them together. Preferably, a pressure P between is applied to two parts during welding.
On obtient alors une structure 500 comprenant une peau 300 solidaire d’un réseau de nervures correspondant à la pièce 100. Les portions de jonction entre les nervures 110 de la pièce 100 et la peau 300 présentent des bourrelets 112 résultant du ramollissement ou de la fusion du matériau thermoplastique au niveau de l’interface d’assemblage. Les bourrelets 112 permettent de renforcer la liaison soudée entre la pièce 100 et la peau 300. La structure 500 peut notamment constituer tout ou partie d’un volet d’inverseur de poussée, d’un panneau raidi, d’une pièce de fuselage ou de carénage, d’une structure de type sandwich notamment pour des traitements acoustiques, etc.A structure 500 is then obtained comprising a skin 300 secured to a network of ribs corresponding to the part 100. The junction portions between the ribs 110 of the part 100 and the skin 300 have beads 112 resulting from the softening or fusion thermoplastic material at the assembly interface. The beads 112 make it possible to reinforce the welded connection between the part 100 and the skin 300. The structure 500 can in particular constitute all or part of a thrust reverser flap, of a stiffened panel, of a fuselage part or of fairing, of a structure of the sandwich type in particular for acoustic treatments, etc.
La pièce en matériau plastique selon l’invention peut comprendre plusieurs éléments chauffants. Plusieurs éléments chauffants identiques ou différents peuvent être placés au même endroit de la pièce afin d’augmenter la température de chauffage locale si nécessaire. Plusieurs éléments chauffants identiques ou différents peuvent également être placés à des endroits différents de la pièce afin de former plusieurs surfaces d’assemblage dans la pièce et permettre par exemple le soudage de la pièce avec plusieurs autres pièces.The part made of plastic material according to the invention may comprise several heating elements. Several identical or different heating elements can be placed in the same place in the room in order to increase the local heating temperature if necessary. Several identical or different heating elements can also be placed at different places in the part in order to form several assembly surfaces in the part and allow, for example, the welding of the part with several other parts.
En surmoulant ou noyant un ou plusieurs éléments chauffants dans une ou plusieurs parties de la pièce, on contrôle la diffusivité thermique dans celle-ci. Il est ainsi possible de chauffer localement le matériau thermoplastique de la pièce au-delà de son point de fusion au niveau de la ou les surfaces d’assemblage de celle-ci tout en conservant dans le reste du matériau de la pièce une température suffisamment basse pour assurer sa stabilité géométrique et un niveau de cristallinité maîtrisé.By overmolding or embedding one or more heating elements in one or more parts of the part, the thermal diffusivity in the latter is controlled. It is thus possible to locally heat the thermoplastic material of the part beyond its melting point at the assembly surface(s) of the latter while maintaining a sufficiently low temperature in the rest of the material of the part. to ensure its geometric stability and a controlled level of crystallinity.
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WO2025032294A1 (en) | 2023-08-07 | 2025-02-13 | Safran | Method for welding parts made of thermoplastic-matrix composite material |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3871822T2 (en) * | 1987-03-04 | 1993-01-14 | Shinsozai Sogo Kenkyusho Kk | MEDICAL BAG AND MANUFACTURING METHOD. |
JPH0531808A (en) * | 1991-07-31 | 1993-02-09 | Nissha Printing Co Ltd | Manufacture of plastic joint product |
FR2742691A1 (en) * | 1995-12-22 | 1997-06-27 | Etex De Rech Tech Soc | Joining element |
EP0959526A2 (en) * | 1998-05-15 | 1999-11-24 | TOHOKU MUNEKATA Co., Ltd. | Joining components of thermoplastic resin by fusion |
JP2001208274A (en) * | 1999-11-19 | 2001-08-03 | Buraunii:Kk | Pipe joining method and device, and pipe |
US20040031798A1 (en) * | 2002-08-16 | 2004-02-19 | Fox Robert W. | Multi-component packaging system and method for manufacture |
GB2431135A (en) * | 2005-10-11 | 2007-04-18 | Uponor Innovation Ab | Heated wire thermoplastic and elastomer bonding |
US20090256349A1 (en) * | 2006-05-05 | 2009-10-15 | Pierre Strubin | Method and device for connecting tubes made out of thermoplastic material |
US20140158684A1 (en) * | 2004-11-23 | 2014-06-12 | Arrow Innovations, Llc | Container Closure With Segmented Fusion Ring |
EP2907651A1 (en) | 2014-02-18 | 2015-08-19 | Airbus Operations (S.A.S) | Method and device for induction welding of parts made of composite materials |
CN103527885B (en) * | 2012-07-05 | 2015-12-16 | 孙志强 | Plastic pipe electrofusion connecting piece having mesh-structured electric heating element and preparation method thereof |
-
2020
- 2020-06-22 FR FR2006504A patent/FR3111582B1/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3871822T2 (en) * | 1987-03-04 | 1993-01-14 | Shinsozai Sogo Kenkyusho Kk | MEDICAL BAG AND MANUFACTURING METHOD. |
JPH0531808A (en) * | 1991-07-31 | 1993-02-09 | Nissha Printing Co Ltd | Manufacture of plastic joint product |
FR2742691A1 (en) * | 1995-12-22 | 1997-06-27 | Etex De Rech Tech Soc | Joining element |
EP0959526A2 (en) * | 1998-05-15 | 1999-11-24 | TOHOKU MUNEKATA Co., Ltd. | Joining components of thermoplastic resin by fusion |
JP2001208274A (en) * | 1999-11-19 | 2001-08-03 | Buraunii:Kk | Pipe joining method and device, and pipe |
US20040031798A1 (en) * | 2002-08-16 | 2004-02-19 | Fox Robert W. | Multi-component packaging system and method for manufacture |
US20140158684A1 (en) * | 2004-11-23 | 2014-06-12 | Arrow Innovations, Llc | Container Closure With Segmented Fusion Ring |
GB2431135A (en) * | 2005-10-11 | 2007-04-18 | Uponor Innovation Ab | Heated wire thermoplastic and elastomer bonding |
US20090256349A1 (en) * | 2006-05-05 | 2009-10-15 | Pierre Strubin | Method and device for connecting tubes made out of thermoplastic material |
CN103527885B (en) * | 2012-07-05 | 2015-12-16 | 孙志强 | Plastic pipe electrofusion connecting piece having mesh-structured electric heating element and preparation method thereof |
EP2907651A1 (en) | 2014-02-18 | 2015-08-19 | Airbus Operations (S.A.S) | Method and device for induction welding of parts made of composite materials |
Non-Patent Citations (1)
Title |
---|
ALI YOUSEFPOUR: "Fusion Bonding/Welding of Thermoplastic Composites", JOURNAL OF THERMOPLASTIC COMPOSITE MATERIALS,, vol. 17, no. 4, 1 January 2004 (2004-01-01), pages 303 - 341, XP009100998, ISSN: 1530-7980, DOI: 10.1177/0892705704045187 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2025032294A1 (en) | 2023-08-07 | 2025-02-13 | Safran | Method for welding parts made of thermoplastic-matrix composite material |
FR3151983A1 (en) | 2023-08-07 | 2025-02-14 | Safran | Welding process between parts made of thermoplastic matrix composite material |
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