FR3084012A1 - PROCESS FOR THE MANUFACTURE OF A METAL MATERIAL REINFORCED WITH AN ORGANIC MATRIX COMPOSITE - Google Patents
PROCESS FOR THE MANUFACTURE OF A METAL MATERIAL REINFORCED WITH AN ORGANIC MATRIX COMPOSITE Download PDFInfo
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- FR3084012A1 FR3084012A1 FR1856615A FR1856615A FR3084012A1 FR 3084012 A1 FR3084012 A1 FR 3084012A1 FR 1856615 A FR1856615 A FR 1856615A FR 1856615 A FR1856615 A FR 1856615A FR 3084012 A1 FR3084012 A1 FR 3084012A1
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- metal sheet
- composite
- resin
- fibrous reinforcements
- structural part
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- 238000000034 method Methods 0.000 title claims abstract description 20
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- 239000011159 matrix material Substances 0.000 title claims abstract description 11
- 229910052751 metal Inorganic materials 0.000 claims abstract description 43
- 239000002184 metal Substances 0.000 claims abstract description 42
- 230000002787 reinforcement Effects 0.000 claims abstract description 24
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- 239000011347 resin Substances 0.000 claims abstract description 23
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 239000007788 liquid Substances 0.000 claims abstract description 4
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 4
- 238000000151 deposition Methods 0.000 claims abstract description 3
- 238000009826 distribution Methods 0.000 claims description 8
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- 230000000694 effects Effects 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
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- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 229920006231 aramid fiber Polymers 0.000 claims 1
- 238000003825 pressing Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 13
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- 230000001360 synchronised effect Effects 0.000 description 1
- 235000013311 vegetables Nutrition 0.000 description 1
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Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
Abstract
L'invention concerne un procédé de fabrication d'un matériau métallique renforcé par un composite à matrice organique, le procédé comportant les étapes de : - recouvrir de renforts fibreux une surface supérieure d'une feuille métallique, - déposer une résine thermoplastique liquide sur la surface supérieure de la feuille métallique de façon à noyer les renforts fibreux dans ladite résine pour former un composite à matrice organique, et - chauffer le composite jusqu'à une température prédéterminée avant d'exercer une pression sur le composite en direction de la feuille métallique pour lier ledit composite à ladite feuille métallique.The invention relates to a method of manufacturing a metallic material reinforced with an organic matrix composite, the method comprising the steps of: - covering with fibrous reinforcements an upper surface of a metal sheet, - depositing a liquid thermoplastic resin on the upper surface of the metal sheet so as to embed the fibrous reinforcements in said resin to form an organic matrix composite, and - heating the composite to a predetermined temperature before applying pressure to the composite in the direction of the metal sheet to bond said composite to said metal sheet.
Description
La présente invention concerne un procédé de fabrication d'un matériau métallique renforcé par un composite à matrice organique. L'invention concerne également un procédé d'obtention d'une pièce structurelle dans un matériau issu d'un tel procédé de fabrication.The present invention relates to a method of manufacturing a metallic material reinforced with an organic matrix composite. The invention also relates to a process for obtaining a structural part in a material resulting from such a manufacturing process.
ARRIERE-PLAN TECHNOLOGIQUE DE L'INVENTIONTECHNOLOGICAL BACKGROUND OF THE INVENTION
Avec l'augmentation de leurs dimensions et du nombre d'équipements dont ils sont pourvus, les véhicules ont vu leur poids croître. Or, 75 % de la consommation de carburant est aujourd'hui directement liée à la masse du véhicule. L'allègement des véhicules est donc devenu un objectif incontournable pour tous les constructeurs automobiles, notamment depuis que la règlementation les y pousse. Des normes environnementales exigent en effet la réduction des émissions de polluants, notamment de dioxyde de carbone (CO2).With the increase in their dimensions and the number of equipment with which they are provided, vehicles have seen their weight increase. However, 75% of fuel consumption today is directly linked to the mass of the vehicle. Lightening vehicles has therefore become an unavoidable objective for all car manufacturers, especially since the regulations push them to do so. Environmental standards indeed require the reduction of emissions of pollutants, in particular carbon dioxide (CO2).
La structure d'un véhicule, appelée aussi caisse en blanc, est aujourd'hui majoritairement constituée d'acier. Bien que les propriétés mécaniques de l'acier aient évolué, sa densité particulièrement élevée (de l'ordre de 7,8) reste un obstacle majeur à l'allègement de la structure. Réduire le poids de la caisse en blanc passe donc nécessairement par l'introduction de matériaux plus légers et en particulier de composites dont la densité peut être jusqu'à sensiblement cinq fois inférieure à celle de l'acier.The structure of a vehicle, also called a white body, is today mainly made of steel. Although the mechanical properties of steel have changed, its particularly high density (of the order of 7.8) remains a major obstacle to lightening the structure. Reducing the weight of the body in white therefore necessarily involves the introduction of lighter materials and in particular composites whose density can be up to substantially five times lower than that of steel.
Une solution consiste à utiliser, dans les zones les plus sollicitées de la structure, des patchs composites à matrice organique. Ces patchs peuvent être collés, rivetés ou vissés sur la pièce structurelle, une fois celle-ci en forme, pour former des renforts locaux et ainsi se substituer à une augmentation d'épaisseur de la pièce structurelle sur laquelle ils sont fixés.One solution is to use, in the most stressed areas of the structure, composite patches with an organic matrix. These patches can be glued, riveted or screwed onto the structural part, once it is in shape, to form local reinforcements and thus replace an increase in thickness of the structural part to which they are fixed.
Toutefois, cette technique nécessite l'investissement d'outillages spécifiques dédiés à la réalisation de ces renforts. La fabrication de patchs composites peut dès lors s'avérer extrêmement coûteuse, réservant ainsi leur utilisation aux véhicules haut de gamme.However, this technique requires the investment of specific tools dedicated to the production of these reinforcements. The manufacture of composite patches can therefore prove to be extremely expensive, thus reserving their use for high-end vehicles.
Qui plus est, les patchs composites représentent des pièces supplémentaires à fixer sur la structure, ce qui engendre une augmentation du temps d'assemblage et donc du coût du véhicule.What is more, the composite patches represent additional parts to be fixed to the structure, which generates an increase in assembly time and therefore in the cost of the vehicle.
OBJET DE L'INVENTIONOBJECT OF THE INVENTION
L' invention a donc pour objet de proposer un procédé de fabrication de pièces structurelles dans un matériau métallique renforcé qui obvie au moins en partie aux inconvénients précités.The object of the invention is therefore to propose a method of manufacturing structural parts in a reinforced metallic material which at least partly obviates the aforementioned drawbacks.
PRESENTATION DE L'INVENTIONPRESENTATION OF THE INVENTION
A cet effet, l'invention propose un procédé de fabrication d'un matériau métallique renforcé par un composite à matrice organique. Le procédé comporte les étapes de :To this end, the invention provides a method of manufacturing a metallic material reinforced with an organic matrix composite. The process includes the steps of:
- recouvrir de renforts fibreux la surface supérieure d'une feuille métallique,- cover the upper surface with a metal sheet with fibrous reinforcements,
- déposer une résine thermoplastique liquide sur la surface supérieure de la feuille métallique de façon à noyer les renforts fibreux dans ladite résine pour former un composite à matrice organique, etdepositing a liquid thermoplastic resin on the upper surface of the metal sheet so as to embed the fibrous reinforcements in said resin to form an organic matrix composite, and
- chauffer le composite jusqu'à une température prédéterminée pour polymériser la résine sous l'effet d'un catalyseur avant d'exercer une pression sur le composite en direction de la feuille métallique pour adhérer ledit composite à ladite feuille métallique.- Heating the composite to a predetermined temperature to polymerize the resin under the effect of a catalyst before exerting pressure on the composite in the direction of the metal sheet to adhere said composite to said metal sheet.
L'élaboration du composite est ainsi effectuée directement sur la feuille métallique, ce qui permet de diminuer le temps nécessaire à la fabrication du matériau renforcé, mais aussi d'en minimiser les outils nécessaires .The development of the composite is thus carried out directly on the metal sheet, which makes it possible to reduce the time necessary for the manufacture of the reinforced material, but also to minimize the tools required.
Selon un mode de réalisation particulier de l'invention, la résine recouvre totalement la surface supérieure de la feuille métallique.According to a particular embodiment of the invention, the resin completely covers the upper surface of the metal sheet.
Selon un autre mode de réalisation de l'invention, la résine recouvre partiellement la surface supérieure de la feuille métallique.According to another embodiment of the invention, the resin partially covers the upper surface of the metal sheet.
De manière particulière, la résine recouvre partiellement la surface supérieure de la feuille métallique dans le sens de la longueur de ladite feuille.In particular, the resin partially covers the upper surface of the metal sheet in the lengthwise direction of said sheet.
Selon un mode de réalisation préféré de l'invention, la feuille métallique est obtenue par découpage d'une bande déroulée d'une bobine.According to a preferred embodiment of the invention, the metal sheet is obtained by cutting an unwound strip from a coil.
Le matériau peut ainsi être réalisé de façon industrielle et continue, c'est-à-dire en étant plus particulièrement compatible avec les cadences de production de l'industrie automobile.The material can thus be produced in an industrial and continuous manner, that is to say being more particularly compatible with the production rates of the automotive industry.
Selon une caractéristique particulière, les renforts fibreux comportent des fibres de carbone et/ou des fibres de verre.According to a particular characteristic, the fibrous reinforcements comprise carbon fibers and / or glass fibers.
De par leur flexibilité et leur résistance élevée à la traction et à la compression, les fibres de carbone, et les fibres de verre permettent d'obtenir un composite ayant de bonnes propriétés mécaniques tout en étant nettement plus léger que le métal correspondant.Due to their flexibility and their high tensile and compressive strength, carbon fibers and glass fibers make it possible to obtain a composite having good mechanical properties while being significantly lighter than the corresponding metal.
Selon un mode de réalisation préféré de l'invention, les renforts fibreux sont issus d'un rouleau de distribution de fibres de verre et/ou de fibres de carbone.According to a preferred embodiment of the invention, the fibrous reinforcements come from a roller for distributing glass fibers and / or carbon fibers.
Les fibres peuvent ainsi être distribuées de façon industrielle et continue, c'est-à-dire en étant plus particulièrement compatible avec les cadences de production de l'industrie automobile.The fibers can thus be distributed in an industrial and continuous manner, that is to say being more particularly compatible with the production rates of the automotive industry.
L'invention concerne également un procédé d'obtention d'une pièce structurelle dans un matériau métallique renforcé issu d'un tel procédé de fabrication.The invention also relates to a process for obtaining a structural part in a reinforced metallic material resulting from such a manufacturing process.
Selon l'invention, le procédé comporte les étapes supplémentaires de :According to the invention, the method comprises the additional steps of:
- découper une portion de matériau métallique renforcé à des dimensions prédéfinies correspondant sensiblement à celles de la pièce structurelle,- cutting a portion of reinforced metallic material to predefined dimensions corresponding substantially to those of the structural part,
- chauffer la portion découpée jusqu'à une température prédéterminée, puis- heat the cut portion to a predetermined temperature, then
- estamper la portion chauffée pour obtenir la forme de la pièce structurelle.- stamp the heated portion to obtain the shape of the structural part.
DESCRIPTION DES FIGURESDESCRIPTION OF THE FIGURES
L'invention sera mieux comprise à la lumière de la description qui suit, laquelle est purement illustrative et non limitative, et doit être lue en regard des figures annexées parmi lesquelles :The invention will be better understood in the light of the description which follows, which is purely illustrative and not limiting, and should be read with reference to the appended figures among which:
- la figure 1 représente schématiquement un procédé de fabrication d'un matériau métallique renforcé selon un mode de réalisation particulier de l'invention,FIG. 1 schematically represents a process for manufacturing a reinforced metallic material according to a particular embodiment of the invention,
- la figure 2 est une vue en perspective d'un matériau issu du procédé illustré à la figure 1,FIG. 2 is a perspective view of a material resulting from the process illustrated in FIG. 1,
- la figure 3 représente schématiquement le procédé d'obtention d'une pièce structurelle dans le matériau illustré à la figure 2,FIG. 3 schematically represents the process for obtaining a structural part in the material illustrated in FIG. 2,
- la figure 4 est une vue en perspective d'une pièce structurelle obtenue dans le matériau illustré à la figure 2.FIG. 4 is a perspective view of a structural part obtained from the material illustrated in FIG. 2.
- la figure 5 est une vue en perspective d'une pièce structurelle obtenue dans une variante du matériau illustré à la figure 2.FIG. 5 is a perspective view of a structural part obtained in a variant of the material illustrated in FIG. 2.
DESCRIPTION DETAILLEE D'UN MODE DE REALISATIONDETAILED DESCRIPTION OF AN EMBODIMENT
PARTICULIER DE L'INVENTIONPARTICULAR OF THE INVENTION
En référence à la figure 1, une bobine 1 d'une bande de métal est montée mobile en rotation autour d'un axe Y1 orthogonal au plan de ladite figure. Le dévidement de la bobine s'opère suivant un axe XI horizontal pour dérouler la bande suivant le même axe XI pour former une feuille métallique 1.1. L'axe Y1 de rotation de la bobine 1 est orthogonal à l'axe XI de déroulement de la bande.With reference to FIG. 1, a coil 1 of a metal strip is mounted mobile in rotation about an axis Y1 orthogonal to the plane of said figure. The unwinding of the reel takes place along a horizontal axis XI to unwind the strip along the same axis XI to form a metal sheet 1.1. The axis Y1 of rotation of the reel 1 is orthogonal to the axis XI of unwinding of the strip.
De la même manière, un rouleau de distribution 2 de renforts fibreux 2.1 est monté mobile en rotation autour d'un axe Y2 orthogonal au plan de la figure 1. L'axe Y2 de rotation du rouleau de distribution 2 est parallèle à l'axe Y1 de rotation de la bobine 1. Le déroulement des renforts fibreux 2.1 s'opère, en sortie du rouleau de distribution 2, suivant un axe X2 formant un angle a avec l'axe XI de dévidement de la bobine 1. L'angle a est ici sensiblement égal à 50 degrés. Les renforts fibreux comportent par exemple des fibres de carbone et/ou des fibres de verre.In the same way, a distribution roller 2 of fibrous reinforcements 2.1 is mounted so as to be able to rotate about an axis Y2 orthogonal to the plane of FIG. 1. The axis Y2 of rotation of the distribution roller 2 is parallel to the axis Y1 of rotation of the reel 1. The unwinding of the fibrous reinforcements 2.1 takes place, at the outlet of the distribution roller 2, along an axis X2 forming an angle a with the axis XI of unwinding of the reel 1. The angle a is here substantially equal to 50 degrees. The fibrous reinforcements comprise for example carbon fibers and / or glass fibers.
La feuille métallique 1.1 et les renforts fibreux 2.2 se rejoignent alors pour passer ensemble entre un premier cylindre 3.1 et un deuxième cylindre 3.2 destinés à guider le déroulement de la bobine 1 et la distribution des renforts fibreux 2.1 suivant l'axe XI.The metal sheet 1.1 and the fibrous reinforcements 2.2 then meet to pass together between a first cylinder 3.1 and a second cylinder 3.2 intended to guide the unwinding of the coil 1 and the distribution of the fibrous reinforcements 2.1 along the axis XI.
Les premier et deuxième cylindres 3.1, 3.2 de guidage sont agencés l'un au-dessus de l'autre et sont montés libres en rotation autour d'axes parallèles à l'axe Y1 de rotation de la bobine 1 et de l'axe Y2 de rotation du rouleau de distribution 2. La feuille métallique 1.1 et les renforts fibreux 2.1 sont respectivement en contact avec le premier cylindre 3.1 et le deuxième cylindre 3.2 de guidage. Les renforts fibreuxThe first and second guide cylinders 3.1, 3.2 are arranged one above the other and are mounted free in rotation around axes parallel to the axis Y1 of rotation of the coil 1 and the axis Y2 of rotation of the distribution roller 2. The metal sheet 1.1 and the fibrous reinforcements 2.1 are respectively in contact with the first cylinder 3.1 and the second guide cylinder 3.2. Fibrous reinforcements
2.1 recouvrent ainsi, en sortie des cylindres 3.1, 3.2 de guidage, au moins une partie d'une surface supérieure de la feuille métallique 1.1.2.1 thus cover, at the outlet of the guide cylinders 3.1, 3.2, at least part of an upper surface of the metal sheet 1.1.
Il est à noter que les vitesses de rotation de la bobine 1 et du rouleau de distribution 2 sont coordonnées de façon à ce que la distribution des renforts fibreux en sortie des cylindres de guidages 3.1, 3.2 soit synchronisée avec le déroulement de la feuille métalliqueIt should be noted that the speeds of rotation of the reel 1 and of the distribution roller 2 are coordinated so that the distribution of the fibrous reinforcements at the outlet of the guide cylinders 3.1, 3.2 is synchronized with the unwinding of the metal sheet
1.1 suivant XI.1.1 according to XI.
Un distributeur 4 d'une résine 5 thermoplastique liquide est agencé en sortie des cylindres 3.1, 3.2 de guidage. La résine 5 est déposée par gravité sur la surface supérieure de la feuille métallique 1.1 de façon à imprégner les renforts fibreux 2.1 de ladite résine 5. Les renforts fibreux 2.1 et la résine 5 forment alors un composite à matrice organique. La résine 5 est par exemple de la résine Elium® de la société ARKEMA.A distributor 4 of a liquid thermoplastic resin 5 is arranged at the outlet from the guide cylinders 3.1, 3.2. The resin 5 is deposited by gravity on the upper surface of the metal sheet 1.1 so as to impregnate the fibrous reinforcements 2.1 of said resin 5. The fibrous reinforcements 2.1 and the resin 5 then form a composite with an organic matrix. Resin 5 is for example Elium® resin from the company ARKEMA.
Comme illustré à la figure 2, les renforts fibreux 2.1 forment ici un quadrillage et ne recouvrent, avec la résine 5, que partiellement la surface supérieure de la feuille métallique 1.1. Le composite forme ainsi une bande s'étendant sensiblement au centre et dans le sens de la longueur de la dite feuille 1.1. Comme nous le verrons plus tard, un recouvrement total de la surface supérieure de la feuille métallique 1.1 par le composite est aussi envisageable, tout comme un recouvrement partiel dans le sens de la largueur.As illustrated in FIG. 2, the fibrous reinforcements 2.1 here form a grid and cover, with the resin 5, only partially the upper surface of the metal sheet 1.1. The composite thus forms a strip extending substantially in the center and in the direction of the length of said sheet 1.1. As we will see later, a total covering of the upper surface of the metal sheet 1.1 by the composite is also possible, just like a partial covering in the width direction.
A la suite du distributeur 4 de résine 5 sont agencés des moyens de chauffe 6 pour chauffer le composite jusqu'à une température prédéterminée pour polymériser la résine 5 sous l'effet d'un catalyseur. La température prédéterminée pour la polymérisation de la résine 5 est de préférence comprise entre 50 et 180 degrés Celsius (°C). Les moyens de chauffe 6 peuvent par exemple être de type infrarouge, à air pulsé, voire par induction de la feuille métallique 1.1. La tenue horizontale de la feuille métallique 1.1 et du composite est assurée par des cylindres 7 de convoyage disposés notamment en dessous des moyens de chauffe 6.Following the resin dispenser 4 5 are arranged heating means 6 for heating the composite to a predetermined temperature to polymerize the resin 5 under the effect of a catalyst. The predetermined temperature for the polymerization of the resin 5 is preferably between 50 and 180 degrees Celsius (° C). The heating means 6 can, for example, be of the infrared, forced air type, or even by induction of the metal sheet 1.1. The horizontal behavior of the metal sheet 1.1 and of the composite is ensured by cylinders 7 for conveying arranged in particular below the heating means 6.
Avant la fin de la polymérisation de la résine 5, l'ensemble feuille métallique/composite passent ensuite entre des cylindres 8 de compactage et d'imprégnation. Les cylindres 8 exercent notamment une pression sur le composite en direction de la feuille métallique 1.1 pour lier ledit composite à ladite feuille métallique et ainsi former un matériau métallique renforcé par un composite à matrice organique. Le matériau se présente alors sous forme d'une bande de largeur sensiblement égale à celle de la feuille métallique 1.1.Before the polymerization of the resin 5 has ended, the metal sheet / composite assembly then pass between compacting and impregnation cylinders 8. The cylinders 8 in particular exert pressure on the composite in the direction of the metal sheet 1.1 to bond said composite to said metal sheet and thus form a metallic material reinforced by an organic matrix composite. The material is then in the form of a strip of width substantially equal to that of the metal sheet 1.1.
Avantageusement, la surface supérieure de la feuille métallique 1.1 a préalablement subi une opération de préparation de surface P permettant d'améliorer l'adhérence entre la résine 5 en phase de polymérisation et la surface supérieure de la feuille métallique 1.1. L'opération de préparation de surface P peut par exemple être réalisée par laser, par abrasion mécanique ou par traitement chimique.Advantageously, the upper surface of the metal sheet 1.1 has previously undergone a surface preparation operation P making it possible to improve the adhesion between the resin 5 in the polymerization phase and the upper surface of the metal sheet 1.1. The surface preparation operation P can for example be carried out by laser, by mechanical abrasion or by chemical treatment.
Un outil de découpe 9 permet de découper une portion 10 dudit matériau à des dimensions prédéfinies correspondant sensiblement à celles d'une pièce structurelle 11. Comme illustré à la figure 3, l'outil de coupe 9 permet par exemple de définir une longueur L de la portion 10 de matériau et de créer des évidements 10.1 latéraux dans des zones non recouvertes par le composite. La largeur 1 de la portion 10 est ici sensiblement égale à celle de la feuille métallique 1.1.A cutting tool 9 makes it possible to cut a portion 10 of said material to predefined dimensions corresponding substantially to those of a structural part 11. As illustrated in FIG. 3, the cutting tool 9 allows for example to define a length L of the portion 10 of material and to create lateral 10.1 recesses in areas not covered by the composite. The width 1 of the portion 10 is here substantially equal to that of the metal sheet 1.1.
Par la suite, la portion 10 découpée est chauffée jusqu'à une température prédéfinie par l'intermédiaire d'un système de chauffage 12 (figure 3). Le réchauffement de la portion 10 découpée permet d'en préparer son estampage sans risquer l'apparition de zones de fatigue voire de rupture du matériau. La température prédéfinie de chauffage dépend des qualités intrinsèques du composite et est de préférence comprise entre 150°C et 350°C.Thereafter, the cut portion 10 is heated to a predefined temperature by means of a heating system 12 (FIG. 3). The heating of the cut portion 10 makes it possible to prepare its stamping without risking the appearance of zones of fatigue or even rupture of the material. The predefined heating temperature depends on the intrinsic qualities of the composite and is preferably between 150 ° C and 350 ° C.
La portion 10 chauffée est ainsi insérée entre une matrice 13.1 et un poinçon 13.2 permettant de donner à ladite portion 10 la forme de la pièce structurelle 11. A titre d'exemple, la pièce structurelle 11 a ici une forme de tunnel dont des extrémités latérales 11.1 ne sont pas recouvertes de composite. Les extrémités latérales 11.1 peuvent avantageusement servir de zones de fixation par soudure de la pièce structurelle il sur un ou des éléments métalliques que ladite pièce structurelle il viendra chevaucher.The heated portion 10 is thus inserted between a die 13.1 and a punch 13.2 making it possible to give said portion 10 the shape of the structural part 11. By way of example, the structural part 11 here has the form of a tunnel whose lateral ends 11.1 are not covered with composite. The lateral ends 11.1 can advantageously serve as areas for fixing by welding the structural part it to one or more metallic elements which said structural part will overlap.
La figure 5 illustre une pièce structurelle 11' de forme similaire à la pièce structurelle il précédemment décrite. La différence réside notamment dans le fait que la pièce structurelle 11' est issu d'un matériau dans lequel le composite recouvre la totalité de la feuille métallique 1.1.FIG. 5 illustrates a structural part 11 ′ of shape similar to the structural part 11 previously described. The difference lies in particular in the fact that the structural part 11 ′ is made from a material in which the composite covers the entire metal sheet 1.1.
Bien entendu, l'invention n'est pas limitée au mode de réalisation décrit mais englobe toute variante entrant dans le champ de l'invention telle que définie par les revendications.Of course, the invention is not limited to the embodiment described but encompasses any variant coming within the scope of the invention as defined by the claims.
Bien qu'ici les renforts fibreux comportent des fibres de carbone et/ou de verre, ils peuvent aussi comporter d'autres types de fibres comme par exemple des fibres végétales, des fibres d'aramide ou de polypropylène...Although here the fibrous reinforcements comprise carbon and / or glass fibers, they can also comprise other types of fibers such as for example vegetable fibers, aramid or polypropylene fibers ...
Claims (9)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1856615A FR3084012B1 (en) | 2018-07-17 | 2018-07-17 | PROCESS FOR MANUFACTURING A METAL MATERIAL REINFORCED BY A COMPOSITE WITH AN ORGANIC MATRIX |
| PCT/EP2019/068296 WO2020016044A1 (en) | 2018-07-17 | 2019-07-08 | Method for producing a metal material reinforced with an organic matrix composite |
| EP19735360.0A EP3823829A1 (en) | 2018-07-17 | 2019-07-08 | Method for producing a metal material reinforced with an organic matrix composite |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1856615 | 2018-07-17 | ||
| FR1856615A FR3084012B1 (en) | 2018-07-17 | 2018-07-17 | PROCESS FOR MANUFACTURING A METAL MATERIAL REINFORCED BY A COMPOSITE WITH AN ORGANIC MATRIX |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3084012A1 true FR3084012A1 (en) | 2020-01-24 |
| FR3084012B1 FR3084012B1 (en) | 2020-09-18 |
Family
ID=63963168
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1856615A Active FR3084012B1 (en) | 2018-07-17 | 2018-07-17 | PROCESS FOR MANUFACTURING A METAL MATERIAL REINFORCED BY A COMPOSITE WITH AN ORGANIC MATRIX |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP3823829A1 (en) |
| FR (1) | FR3084012B1 (en) |
| WO (1) | WO2020016044A1 (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5149394A (en) * | 1988-10-14 | 1992-09-22 | Kurt Held | Method and apparatus for continuously fabricating laminates |
| EP2633979A1 (en) * | 2012-02-28 | 2013-09-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Semi-finished product for the production of a fiber composite metal hybrid laminate and method for producing such a semi-finished product |
| US9902096B2 (en) * | 2014-05-06 | 2018-02-27 | Evonik Degussa Gmbh | Production of fibre composite component part based on aluminium and polyurethane |
-
2018
- 2018-07-17 FR FR1856615A patent/FR3084012B1/en active Active
-
2019
- 2019-07-08 EP EP19735360.0A patent/EP3823829A1/en not_active Withdrawn
- 2019-07-08 WO PCT/EP2019/068296 patent/WO2020016044A1/en unknown
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5149394A (en) * | 1988-10-14 | 1992-09-22 | Kurt Held | Method and apparatus for continuously fabricating laminates |
| EP2633979A1 (en) * | 2012-02-28 | 2013-09-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Semi-finished product for the production of a fiber composite metal hybrid laminate and method for producing such a semi-finished product |
| US9902096B2 (en) * | 2014-05-06 | 2018-02-27 | Evonik Degussa Gmbh | Production of fibre composite component part based on aluminium and polyurethane |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2020016044A1 (en) | 2020-01-23 |
| EP3823829A1 (en) | 2021-05-26 |
| FR3084012B1 (en) | 2020-09-18 |
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