FR2901730A1 - COMPOSITE STRUCTURE USED TO PRODUCE PIECES OBTAINED BY INJECTION MOLDING AND / OR VACUUM INFUSION PROCESS - Google Patents
COMPOSITE STRUCTURE USED TO PRODUCE PIECES OBTAINED BY INJECTION MOLDING AND / OR VACUUM INFUSION PROCESS Download PDFInfo
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- FR2901730A1 FR2901730A1 FR0604861A FR0604861A FR2901730A1 FR 2901730 A1 FR2901730 A1 FR 2901730A1 FR 0604861 A FR0604861 A FR 0604861A FR 0604861 A FR0604861 A FR 0604861A FR 2901730 A1 FR2901730 A1 FR 2901730A1
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- 239000002131 composite material Substances 0.000 title claims abstract description 29
- 238000000034 method Methods 0.000 title claims abstract description 9
- 238000001746 injection moulding Methods 0.000 title claims abstract description 8
- 238000009755 vacuum infusion Methods 0.000 title claims abstract description 8
- 230000008569 process Effects 0.000 title abstract description 7
- 239000004753 textile Substances 0.000 claims abstract description 28
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 18
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 13
- 238000000465 moulding Methods 0.000 claims abstract description 12
- 239000000463 material Substances 0.000 claims description 26
- 230000004888 barrier function Effects 0.000 claims description 6
- 238000013016 damping Methods 0.000 claims description 5
- 238000013508 migration Methods 0.000 claims description 4
- 230000001681 protective effect Effects 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 239000004744 fabric Substances 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 238000001802 infusion Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000004698 Polyethylene Substances 0.000 description 2
- 230000005012 migration Effects 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- -1 polyethylene Polymers 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
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- 230000036541 health Effects 0.000 description 1
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- 230000000116 mitigating effect Effects 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
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- 238000010186 staining Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
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
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B1/00—Layered products having a non-planar shape
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/02—Layered products comprising a layer of synthetic resin in the form of fibres or filaments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/28—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- 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
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- 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
- B29K2027/00—Use of polyvinylhalogenides or derivatives thereof as moulding material
- B29K2027/06—PVC, i.e. polyvinylchloride
-
- 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
- B29L2009/00—Layered products
-
- 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
- B29L2031/3067—Ships
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Abstract
La présente invention a pour objet une structure composite utilisée pour la réalisation de pièces obtenues par un procédé de moulage par injection et/ou infusion sous vide. Elle concerne le domaine technique du moulage connu sous la dénomination RTM pour ResineTransfert Moulding.Selon l'invention, la structure composite comporte un complexe textile de renfort (3) destiné à être imprégné d'un agent durcisseur, se caractérisant par le fait que ledit complexe textile (3) est arrangé avec un complexe de recouvrement (4) intégrant une peau extérieure de finition (40).La peau extérieure de finition est ainsi directement incorporée dans la structure avant moulage de sorte qu'une pièce finie peut être obtenue directement après le démoulage.The present invention relates to a composite structure used for the production of parts obtained by a process of injection molding and / or vacuum infusion. It relates to the technical field of molding known by the name RTM for ResinTransfer Molding. According to the invention, the composite structure comprises a textile reinforcing complex (3) intended to be impregnated with a hardening agent, characterized in that said textile complex (3) is arranged with a covering complex (4) incorporating an outer skin finish (40) .The outer skin of finish is thus directly incorporated into the structure before molding so that a finished piece can be obtained directly after demolding.
Description
1 Description La présente invention a pour objet une structure compositeThe present invention relates to a composite structure
utilisée pour la réalisation de pièces obtenues par un procédé de moulage par injection et/ou infusion sous vide. used for the production of parts obtained by a process of injection molding and / or vacuum infusion.
Elle concerne le domaine technique du moulage connu sous la dénomination RTM pour ResineTransfert Moulding, par injection et/ou infusion sous vide. Ce procédé permet la fabrication de pièces composites notamment dans les domaines nautiques, aéronautiques, ferroviaires ou automobiles. L'invention concerne plus particulièrement le domaine technique des structures composites utilisées dans de tels procédés de moulage. It concerns the technical field of molding known by the name RTM for Resin Transfer Molding, by injection and / or vacuum infusion. This process allows the manufacture of composite parts in particular in the nautical, aeronautical, railway or automotive. The invention relates more particularly to the technical field of composite structures used in such molding processes.
Habituellement, lors d'un moulage par injection et/ou infusion sous vide, on applique sur un moule présentant une forme complémentaire à celle de la pièce souhaitée, un complexe textile de renfort positionné a sec. Ce dernier a pour finalité d'assurer les propriétés mécaniques de la pièce. Usually, during an injection molding and / or vacuum infusion, a textile fabric having a position that is complementary to that of the desired part is applied to a mold positioned in a dry position. The purpose of the latter is to ensure the mechanical properties of the part.
Ce complexe textile est recouvert dans le cas de l'infusion d'une bâche étanche et souple, et dans le cas de l'injection d'un contre-moule, ceux-ci étant agencés avec le moule pour former un volume clos, Habituellement, un vide est ensuite appliqué dans ce volume clos en même temps qu'on injecte et/ou infuse un agent durcisseur à l'intérieur du complexe textile. Cette opération permet de répartir de manière homogène l'agent durcisseur dans le complexe textile et de conformer ce dernier à la forme du moule. L'ensemble est alors soumis à des conditions de températures permettant de durcir l'agent durcisseur. À la suite de cette étape, la pièce est refroidie puis démoulée. 2 Ce procédé de moulage permet de réaliser des pièces composites ayant une face parfaitement lisse du côté du moule, mais comportant une face brute de finition du côté de la bâche souple ou du contre-moule. En effet, les défauts du complexe textile apparaissent sur cette face, et en particulier toutes les mailles dudit complexe ressortent. This textile complex is covered in the case of the infusion of a waterproof and flexible tarpaulin, and in the case of the injection of a counter-mold, these being arranged with the mold to form a closed volume, Usually , a vacuum is then applied in this closed volume at the same time that a curing agent is injected and / or infused inside the textile complex. This operation makes it possible to distribute the hardening agent homogeneously in the textile complex and to conform the latter to the shape of the mold. The assembly is then subjected to temperature conditions for hardening the curing agent. Following this step, the part is cooled and demolded. This molding process makes it possible to produce composite parts having a perfectly smooth face on the mold side, but having a rough finish face on the side of the flexible sheet or against the mold. Indeed, the defects of the textile complex appear on this face, and in particular all the meshes of said complex stand out.
Ce résultat nécessite des opérations de finition qui peuvent consister à appliquer contre la face brute de finition une contre-coque, des panneaux ou des tapisseries décoratives, une peinture après ponçage et apprêt, à appliquer des tissus complexes décoratifs ou un vaigrage ou encore toute autre peau de finition équivalente. This result requires finishing operations which may consist of applying a counter-shell, panels or decorative tapes, a paint after sanding and finishing, to apply complex decorative fabrics or a veneer or any other material against the rough surface finish. skin of equivalent finish.
Ces opérations de finitions supplémentaires engendrent une perte de temps quant à la réalisation de la pièce finie, une main d'oeuvre supplémentaire, des surcoûts de fabrication et des risques pour la santé des opérateurs et pour l'environnement, car elles nécessitent l'emploi supplémentaire de solvants contenus dans les différentes colles utilisées. These additional finishing operations cause a loss of time in the production of the finished part, additional labor, additional manufacturing costs and health risks for the operators and the environment, as they require the use additional solvents contained in the various adhesives used.
Face à tous les inconvénients de l'art antérieur, le problème technique que se propose de résoudre l'invention est d'obtenir par un procédé de moulage par injection et/ou infusion sous vide, une pièce composite ne nécessitant aucune finition. Faced with all the disadvantages of the prior art, the technical problem to be solved by the invention is to obtain by a method of injection molding and / or infusion under vacuum, a composite part requiring no finishing.
L'invention a ainsi pour objet une structure composite pour la réalisation de pièces obtenues par moulage par injection et/ou infusion sous vide, ladite structure comportant un complexe textile de renfort destiné à être imprégné d'un agent durcissant, se caractérisant par le fait que ledit complexe textile est arrangé avec un complexe de recouvrement intégrant une peau extérieure de finition. The subject of the invention is thus a composite structure for producing parts obtained by injection molding and / or vacuum infusion, said structure comprising a textile reinforcing complex intended to be impregnated with a hardening agent, characterized by the fact that said textile complex is arranged with a covering complex incorporating an outer skin finish.
Ainsi, la peau extérieure de finition est directement incorporée dans la structure avant moulage de sorte qu'une pièce finie puisse être obtenue directement après le démoulage. -3 Selon une caractéristique préférée de l'invention permettant de protéger la peau extérieure de finition contre d'éventuelles déformations ou retraits de matière, le complexe de recouvrement comporte une couche d'un matériau apte à amortir les contraintes mécaniques auxquelles est soumise ladite peau extérieure lors du moulage. Thus, the outer skin finish is directly incorporated into the structure before molding so that a finished part can be obtained directly after demolding. According to a preferred characteristic of the invention making it possible to protect the external finishing skin against any deformations or withdrawals of material, the covering complex comprises a layer of a material capable of damping the mechanical stresses to which said skin is subjected. outside when molding.
Selon une autre caractéristique préférée de l'invention, le complexe de recouvrement comporte une couche de matériau formant une barrière anti-migration de l'agent durcisseur. Cette caractéristique permet d'isoler le complexe de recouvrement et en particulier la peau extérieure de finition contre d'éventuelles contraintes chimiques. According to another preferred feature of the invention, the covering complex comprises a layer of material forming a barrier against migration of the curing agent. This characteristic makes it possible to isolate the covering complex and in particular the outer skin of finish against possible chemical constraints.
Selon une autre caractéristique préférée de l'invention permettant d'atténuer l'apparition de plis au niveau de la peau extérieure de finition, le complexe de recouvrement comporte un matériau destiné à niveler les imperfections. According to another preferred feature of the invention for mitigating the appearance of folds at the outer skin finish, the covering complex comprises a material for leveling imperfections.
Selon une caractéristique avantageuse de l'invention permettant de préserver au mieux les propriétés du matériau destiné à niveler les imperfections, ce dernier est disposé entre le matériau élastique et déformable et la peau extérieure de finition. According to an advantageous characteristic of the invention to best preserve the properties of the material for leveling imperfections, the latter is disposed between the elastic and deformable material and the outer skin finish.
Selon une autre caractéristique préférée de l'invention permettant de protéger la peau extérieure de finition, cette dernière est recouverte d'un film de protection. According to another preferred feature of the invention for protecting the outer skin finish, the latter is covered with a protective film.
D'autres avantages et caractéristiques de l'invention apparaîtront mieux à la lecture de la description du mode de réalisation préférée qui va suivre, en référence à la figure 1 annexée, réalisée à titre d'exemple indicatif et non limitatif et représentant une vue schématique en coupe de la structure complexe objet de l'invention. -4 La structure complexe objet de l'invention représentée sur la figure 1 est destinée à être utilisée dans un procédé de moulage par injection et/ou infusion de résine sous vide, dans le but de fabriquer des panneaux de décoration, des coques de navires, des accessoires pour avions, trains ou automobiles, ou toutes autres pièces composites équivalentes. On l'utilise particulièrement pour réaliser le vaigrage d'un bateau. Other advantages and characteristics of the invention will appear better on reading the description of the preferred embodiment which follows, with reference to the appended FIG. 1, carried out as an indicative and nonlimiting example and showing a schematic view. in section of the complex structure object of the invention. The complex structure which is the subject of the invention shown in FIG. 1 is intended to be used in a vacuum resin injection and / or infusion molding process, for the purpose of manufacturing decoration panels, hulls of vessels. , accessories for aircraft, trains or automobiles, or any other equivalent composite parts. It is particularly used to make the surfacing of a boat.
La structure composite objet de l'invention est destinée à être agencée entre un moule 1 et soit un contre-moule et /ou une bâche souple 2, ces deux éléments étant combinés pour former un volume clos à l'intérieur duquel va être appliqué un vide et va être injecté et/ou infusé un agent durcisseur du type résine thermodurcissable. The composite structure which is the subject of the invention is intended to be arranged between a mold 1 and either a counter-mold and / or a flexible sheet 2, these two elements being combined to form a closed volume within which a vacuum and will be injected and / or infused a curing agent of the thermosetting resin type.
La structure composite est formée d'un complexe textile de renfort 3 arrangé avec un complexe de recouvrement 4 intégrant une peau extérieure de finition 40. The composite structure is formed of a reinforcing textile complex 3 arranged with a covering complex 4 incorporating an outer finishing skin 40.
De manière connue en soi, le complexe textile de renfort 3 est formé de plusieurs couches textiles en contact avec des fibres tissées ou non tissées. Il assure le renforcement mécanique de la pièce composite. En pratique, le complexe textile de renfort utilisé est du type intégrant des couches de tissus de verre traditionnels. On peut également employer un complexe textile intégrant des couches de tissus non tissé à base de polyester. In a manner known per se, the reinforcing textile complex 3 is formed of several textile layers in contact with woven or non-woven fibers. It provides the mechanical reinforcement of the composite part. In practice, the textile reinforcement complex used is of the type incorporating layers of traditional glass fabrics. It is also possible to use a textile complex incorporating layers of nonwoven fabric based on polyester.
Le complexe textile de renfort 3 intègre avantageusement une structure drainante ayant pour fonction d'améliorer la diffusion de l'agent durcisseur et d'assurer une répartition homogène de ce dernier dans le complexe textile. Un tel complexe textile est par exemple décrit dans le document FR2.870.861 (CHOMARAT). On peut également employer une structure à base de fibres de verre drainantes UNIFILO . The reinforcing textile complex 3 advantageously incorporates a draining structure whose function is to improve the diffusion of the hardening agent and to ensure a homogeneous distribution of the latter in the textile complex. Such a textile complex is for example described in the document FR2.870.861 (CHOMARAT). It is also possible to use a structure based on draining glass fibers UNIFILO.
En se rapportant à la figure 1, lorsque le vide est réalisé entre l'espace étanche défini par le moule 1 et la bâche souple et / ou le contre-moule 2, l'agent durcisseur est injecté dans le complexe textile de renfort 3 et se diffuse dans ce dernier comme indiqué par les flèches. Referring to FIG. 1, when the vacuum is formed between the sealed space defined by the mold 1 and the flexible sheet and / or the counter-mold 2, the hardening agent is injected into the reinforcing textile complex 3 and spreads in the latter as indicated by the arrows.
En se rapportant à la figure annexée, le complexe de recouvrement 4 est arrangé au-dessus du complexe textile de renfort 3. Ces deux éléments sont solidarisés entre eux par un tricot tridimensionnel classique, ou par l'utilisation d'un adhésif. De manière préférée, 10 on utilise une liaison thermochimique du type polyuréthane à chaud Referring to the attached figure, the covering complex 4 is arranged above the reinforcing textile complex 3. These two elements are joined together by a conventional three-dimensional knit, or by the use of an adhesive. Preferably, a thermochemical bond of the hot polyurethane type is used.
Le complexe de recouvrement 4 comporte une peau extérieure de finition 40 en T.E.P (Tissu Enduit Plastique), cuir, bois, éponge, tissu de décoration, vaigrage pour bateau, silicone, formée d'un film PVC dense recouvert d'une 15 enduction polyuréthane, etc. Cette peau extérieure a pour objectif de réaliser la finition de la pièce composite du côté de la face de la structure complexe en contact avec la bâche souple et/ou le contre-moule 2. On peut également prévoir de disposer des peaux extérieures de finition au niveau de chaque face de la structure 20 complexe. Selon un mode préféré de réalisation, la peau extérieure de finition 40 est constituée d'un film homogène présentant une résistance mécanique et chimique spécifique contre les tâches ou le nettoyage. En fonction de l'utilisation de la pièce, la peau extérieure de finition est spécialement traitée 25 pour répondre à différentes normes de sécurité, comme les normes anti-feu. The covering complex 4 has an outer skin 40 of TEP (Plastic Coated Fabric), leather, wood, sponge, decorative fabric, boat coating, silicone, formed of a dense PVC film coated with a polyurethane coating. etc. This outer skin is intended to achieve the finishing of the composite part on the side of the face of the complex structure in contact with the flexible sheet and / or the against-mold 2. It is also possible to have the outer skin finish of the level of each face of the complex structure. According to a preferred embodiment, the external finish skin 40 is made of a homogeneous film having a specific mechanical and chemical resistance against staining or cleaning. Depending on the use of the workpiece, the outer finish skin is specially treated to meet different safety standards, such as fire standards.
Le complexe de recouvrement 4 est avantageusement conçu pour amortir les déformations intervenant lors de la mise sous vide de la structure composite objet de l'invention. En effet, lors de cette étape, il se crée un vide 30 dans l'espace clos et la bâche souple et/ou le contre-moule 2 comprime la structure contre le moule 1, ce qui est susceptible d'endommager la peau extérieure de finition 40. 6 De plus, lors du durcissement de l'agent durcisseur, des phénomènes de retraits ou de mouvements peuvent apparaître et sont susceptibles de dégrader l'aspect esthétique de la peau extérieure de finition 40 après démoulage. Selon le mode préféré de réalisation représenté sur la figure 1, le complexe de recouvrement 4 comporte donc avantageusement une couche d'un matériau 41 apte à amortir les contraintes mécaniques auxquelles est soumise la peau extérieure de finition 40 lors du moulage. Cette couche est disposée entre la peau extérieure de finition 40 et le complexe textile de renfort 3. The covering complex 4 is advantageously designed to damp the deformations occurring during the evacuation of the composite structure object of the invention. Indeed, during this step, a vacuum 30 is created in the enclosed space and the flexible sheet and / or the counter-mold 2 compresses the structure against the mold 1, which is likely to damage the outer skin of the mold. In addition, during hardening of the curing agent, shrinkage or movement phenomena may occur and are liable to degrade the aesthetic appearance of the external finish skin 40 after demolding. According to the preferred embodiment shown in Figure 1, the covering complex 4 thus advantageously comprises a layer of a material 41 adapted to dampen the mechanical stresses to which the external finish skin 40 is subjected during molding. This layer is disposed between the external finish skin 40 and the reinforcing textile complex 3.
En pratique, on utilise un matériau élastique et déformable, avantageusement un matériau non tissé à base de polyester ayant une densité comprise entre 200 gr/m2 et 250 gr/m2. In practice, an elastic and deformable material is used, advantageously a non-woven material based on polyester having a density of between 200 g / m 2 and 250 g / m 2.
Lors de la mise sous vide de la structure composite objet de l'invention, l'agent durcisseur qui imprègne le complexe textile de renfort 3 est susceptible de migrer vers le complexe de recouvrement 4 du fait de la compression des différentes couches. Les adjuvants et/ou solvants contenus dans l'agent durcisseur peuvent alors altérer les propriétés du complexe de recouvrement 4. Pour éviter cela, le complexe de recouvrement 4 comporte une couche de matériau 42 formant une barrière anti-migration de l'agent durcisseur. Afin de préserver au mieux l'intégrité du complexe de recouvrement 4, cette couche de matériau 42 formant barrière est disposée directement au contact du complexe textile de renfort 3. En pratique, on utilise un film de polyéthylène ou de PVC ayant une 25 épaisseur comprise entre 100 pm et 200pm, avantageusement 120 pm. During the evacuation of the composite structure which is the subject of the invention, the hardening agent which impregnates the reinforcing textile complex 3 is capable of migrating towards the covering complex 4 because of the compression of the various layers. The adjuvants and / or solvents contained in the curing agent can then alter the properties of the covering complex 4. To avoid this, the covering complex 4 comprises a layer of material 42 forming a barrier against migration of the curing agent. In order to better preserve the integrity of the covering complex 4, this layer of barrier material 42 is placed directly in contact with the reinforcing textile complex 3. In practice, a polyethylene or PVC film having a thickness of between 100 pm and 200 pm, advantageously 120 pm.
En fonction de la forme de la pièce à réaliser et/ou du type de complexe textile 3 utilisé (notamment selon sa capacité à absorber l'agent durcisseur), il arrive que la peau extérieure de finition 40 présente des plis après le 30 démouiage. Pour remédier à cet état des choses, le complexe de recouvrement 4 comporte une couche d'un matériau 43 destiné à niveler les imperfections, 7 avantageusement disposée entre le matériau 41 apte à amortir les contraintes mécaniques et la peau extérieure de finition 40. En pratique, le matériau 43 destiné à niveler les imperfections est une émulsion expansée de PVC à cellules fermées ayant une densité comprise entre 700 gr/m2 et 1500 gr/m2. En jouant sur la densité de ce matériau, on peut améliorer l'atténuation des plis. Depending on the shape of the part to be made and / or the type of textile complex 3 used (in particular according to its capacity to absorb the hardening agent), it sometimes happens that the outer finishing skin 40 has folds after demouiage. To remedy this state of affairs, the covering complex 4 comprises a layer of a material 43 intended to level the imperfections, 7 advantageously arranged between the material 41 capable of damping the mechanical stresses and the outer skin of finish 40. In practice , the imperfection-leveling material 43 is an expanded closed-cell PVC emulsion having a density of from 700 gr / m2 to 1500 gr / m2. By varying the density of this material, it is possible to improve the attenuation of the folds.
Lors de la mise sous vide de la structure composite, il peut apparaître des bavures d'agent durcisseur au niveau de la peau extérieure de finition 40. Également, lors de la manipulation de la pièce démoulée, la peau extérieure peut être salie ou être soumise à des chocs. Pour se prémunir de cela, le complexe de recouvrement 4 comporte un film de protection 44 qui recouvre ladite peau. En pratique, on utilise un film polyéthylène d'environ 20 pm qui adhère à la peau extérieure de finition 40 par phénomène électrostatique. When evacuating the composite structure, bursts of hardening agent may appear at the level of the outer finishing skin 40. Also, when handling the demolded part, the outer skin may be soiled or subjected to to shocks. To guard against this, the covering complex 4 comprises a protective film 44 which covers said skin. In practice, a polyethylene film of about 20 μm is used which adheres to the external finish skin 40 by electrostatic phenomena.
Les différentes couches de matériaux constitutifs du complexe de recouvrement 4 sont solidarisées entre elles par un tricot tridimensionnel classique, ou par l'utilisation d'un adhésif ou encore, et de manière préférée, par l'intermédiaire d'une liaison thermochimique du type polyuréthane à chaud. The different layers of materials constituting the covering complex 4 are joined to each other by a conventional three-dimensional knit, or by the use of an adhesive or, more preferably, via a thermochemical bond of the polyurethane type. hot.
La structure complexe objet de l'invention se présente sous la forme d'une bande ayant une épaisseur totale d'environ 4 mm et dont la longueur et la largeur varient selon les dimensions de la pièce composite à réaliser. The complex structure which is the subject of the invention is in the form of a strip having a total thickness of approximately 4 mm and whose length and width vary according to the dimensions of the composite part to be produced.
25 En se rapportant à la figure 1, elle est préférentiellement réalisée par la superposition successive des couches suivantes : complexe textile de renfort 3 ; - matériau 42 formant une barrière anti-migration de l'agent durcisseur ; 30 - matériau 41 apte à amortir les contraintes mécaniques auxquelles est soumise la peau extérieure de finition 40 lors du moulage ; - le matériau 43 destiné à niveler les imperfections ; - 8 - peau extérieure de finition 40 ; - film de protection 44.Referring to FIG. 1, it is preferentially produced by the successive superimposition of the following layers: reinforcement textile complex 3; material 42 forming an anti-migration barrier for the hardening agent; Material 41 capable of damping the mechanical stresses to which the external finishing skin 40 is subjected during molding; the material 43 intended to level the imperfections; Outer skin of finish 40; - protective film 44.
Claims (10)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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FR0604861A FR2901730B3 (en) | 2006-05-31 | 2006-05-31 | COMPOSITE STRUCTURE USED TO PRODUCE PIECES OBTAINED BY INJECTION MOLDING AND / OR VACUUM INFUSION PROCESS |
PCT/FR2007/000904 WO2007138196A1 (en) | 2006-05-31 | 2007-05-31 | Multilayer composite structure for making parts obtained by vacuum injection and/or infusion molding |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0604861A FR2901730B3 (en) | 2006-05-31 | 2006-05-31 | COMPOSITE STRUCTURE USED TO PRODUCE PIECES OBTAINED BY INJECTION MOLDING AND / OR VACUUM INFUSION PROCESS |
Publications (2)
Publication Number | Publication Date |
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FR2901730A1 true FR2901730A1 (en) | 2007-12-07 |
FR2901730B3 FR2901730B3 (en) | 2008-10-10 |
Family
ID=38608866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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FR0604861A Expired - Fee Related FR2901730B3 (en) | 2006-05-31 | 2006-05-31 | COMPOSITE STRUCTURE USED TO PRODUCE PIECES OBTAINED BY INJECTION MOLDING AND / OR VACUUM INFUSION PROCESS |
Country Status (2)
Country | Link |
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FR (1) | FR2901730B3 (en) |
WO (1) | WO2007138196A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012136235A1 (en) * | 2011-04-02 | 2012-10-11 | Daimler Ag | Composite fibre multi-coat bodywork component and method for producing same |
EP2730396A1 (en) * | 2012-11-08 | 2014-05-14 | Volkswagen Aktiengesellschaft | Process for manufacturing a molded part comprising a layer made of a fibre composite plastic layer and a surface coating consisting of a moulded plastic component |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3873406A (en) * | 1972-12-22 | 1975-03-25 | Toray Industries | Synthetic leather and method of preparing the same |
US5580621A (en) * | 1990-04-30 | 1996-12-03 | American Standard Inc. | Polyester backed acrylic composite molded structure and method of manufacturing thereof |
DE4132461C2 (en) * | 1991-09-30 | 1995-01-26 | Peter Forster | Process for making a kitchen sink |
-
2006
- 2006-05-31 FR FR0604861A patent/FR2901730B3/en not_active Expired - Fee Related
-
2007
- 2007-05-31 WO PCT/FR2007/000904 patent/WO2007138196A1/en active Application Filing
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012136235A1 (en) * | 2011-04-02 | 2012-10-11 | Daimler Ag | Composite fibre multi-coat bodywork component and method for producing same |
EP2730396A1 (en) * | 2012-11-08 | 2014-05-14 | Volkswagen Aktiengesellschaft | Process for manufacturing a molded part comprising a layer made of a fibre composite plastic layer and a surface coating consisting of a moulded plastic component |
Also Published As
Publication number | Publication date |
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FR2901730B3 (en) | 2008-10-10 |
WO2007138196A1 (en) | 2007-12-06 |
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