EP0424216A1 - Composite material, its fabricating process and use of the material - Google Patents
Composite material, its fabricating process and use of the material Download PDFInfo
- Publication number
- EP0424216A1 EP0424216A1 EP90402823A EP90402823A EP0424216A1 EP 0424216 A1 EP0424216 A1 EP 0424216A1 EP 90402823 A EP90402823 A EP 90402823A EP 90402823 A EP90402823 A EP 90402823A EP 0424216 A1 EP0424216 A1 EP 0424216A1
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- EP
- European Patent Office
- Prior art keywords
- resin
- threads
- fabric
- composite material
- composite
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Laminated Bodies (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Glass Compositions (AREA)
- Woven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
La présente invention concerne un matériau composite, son procédé de réalisation et utilisation dudit matériau.The present invention relates to a composite material, its production method and use of said material.
Le matériau composite est une substance hétérogène comportant généralement des fibres, des fils, libres ou assemblés en couches, noyés dans une résine.The composite material is a heterogeneous substance generally comprising fibers, threads, free or assembled in layers, embedded in a resin.
Ces matériaux composites se présentent généralement sous forme de grandes plaques épaisses assez rigides. Elles sont de plus en plus utilisées dans l'industrie notamment dans l'industrie de construction de matériels de biens d'équipement, de transport, etc... pour réaliser des carosseries, des planchers, etc.These composite materials are generally in the form of large, fairly rigid thick plates. They are more and more used in industry, especially in the industry of construction of equipment, capital goods, transport, etc. to make bodywork, floors, etc.
Ces plaques sont transformées, selon les techniques traditionnelles par moulage par contact ou sous vide, par injection et selon une technique plus récente, par estampage.These plates are transformed, according to traditional techniques by contact or vacuum molding, by injection and according to a more recent technique, by stamping.
Généralement un procédé de réalisation consiste à assembler en couches ou strates des étoffes textiles de fibres ou de fils de renfort à hautes caractéristiques mécaniques telles que : verre, silice, carbure de silicium, carbone, céramique, aramides, polyéthylène haut module, etc, et à les noyer dans une matrice de résine. Plus précisément, on coule dans un moule de la dimension d'une plaque un fond de résine et d'agent de démoulage; par dessus on pose une première couche d'étoffe, en fils de fibres de renfort par exemple, que l'on recouvre de résine; par dessus on pose une seconde couche d'étoffe en fils de renfort à haute résistance, que l'on recouvre également de résine; ainsi de suite on "empile" plusieurs couches, par exemple cinq ou six que l'on recouvre de résine, et on achève l'empilage par une dernière couche de résine et un agent de démoulage. On fait ensuite subir à cet ensemble une action de compression destinée à éliminer le maximum d'air et à faire pénétrer la résine dans les couches d'étoffes, puis un traitement thermique qui réticule ou polymérise la résine afin d'obtenir un composite rigide et un ensemble le plus homogène possible. Ces matériaux composites peuvent comporter jusqu'à plus de quarante couches chacune d'une épaisseur de l'ordre de 0,1 à 0,2 millimètre: les plus courants comptent de une à quinze couches et sont d'épaisseur totale moyenne entre 3 et 5 millimètre après compression et prêts à l'emploi. Leur poids est de l'ordre de 200 grammes/m2 pour une couche de 0,1 mm d'épaisseur en verre. Le matériau obtenu est un produit composite à haute résistance notamment aux chocs, à la traction, à la compression.Generally, a production process consists in assembling in layers or strata textile fabrics of fibers or reinforcing threads with high mechanical characteristics such as: glass, silica, silicon carbide, carbon, ceramic, aramids, high modulus polyethylene, etc., and to drown them in a resin matrix. More precisely, a base of resin and release agent is poured into a mold the size of a plate; above, a first layer of fabric is laid, made of reinforcing fiber threads for example, which is covered with resin; above, a second layer of fabric is placed in high-resistance reinforcing threads, which are also covered with resin; so on we stack several layers, for example five or six that are covered with resin, and we finish the stack with a last layer of resin and a release agent. This assembly is then subjected to a compression action intended to eliminate the maximum of air and to make the resin penetrate into the layers of fabrics, then a heat treatment which crosslinks or polymerizes the resin in order to obtain a rigid composite and the most homogeneous whole possible. These composite materials can comprise up to more than forty layers each with a thickness of the order of 0.1 to 0.2 millimeters: the most common have from one to fifteen layers and are of average total thickness between 3 and 5 mm after compression and ready to use. Their weight is around 200 grams / m2 for a 0.1 mm thick layer of glass. The material obtained is a composite product with high resistance, in particular to impact, traction, compression.
Cependant un tel procédé présente de nombreux inconvénients:
- 1- il est coûteux : le matériel nécessaire à sa mécanisation est très coûteux, et généralement les opérations sont manuelles, ce qui suppose une main-d'oeuvre importante; d'autre part il est long : les étapes de réalisation sont nombreuses;
- 2- le matériau obtenu présente une faible résistance au cisaillement : on observe du délaminage. Le phénomène s'explique par le fait que les couches de tissus renferment des bulles d'air qui ne sont pas chassées par la résine. Ces bulles forment autant de petits matelas d'air qui réduisent le contact couche-résine et l'adhérence entre les couches.
- 3- l'homogénéité recherchée par le traitement thermique, (imprégnation, polymérisation) est difficile à obtenir en une durée raisonnable, du fait de l'épaisseur du matériau ce qui accentue le délaminage.
- 1- it is expensive: the equipment necessary for its mechanization is very expensive, and generally the operations are manual, which supposes a significant manpower; on the other hand it is long: the stages of realization are numerous;
- 2- the material obtained has a low shear strength: delamination is observed. The phenomenon is explained by the fact that the layers of tissue contain air bubbles which are not expelled by the resin. These bubbles form as many small air mattresses which reduce the layer-resin contact and the adhesion between the layers.
- 3- the homogeneity sought by the heat treatment (impregnation, polymerization) is difficult to obtain in a reasonable time, due to the thickness of the material which accentuates delamination.
D'autre part et d'une manière très générale un tissu est une structure textile formée d'un assemblage de fils dits de chaîne assemblés dans des fils dits de trame. Cette structure s'étend dans un plan, dont l'épaisseur est limitée à celle du ou des fils utilisés, dimension négligeable relativement à la surface du tissu. Une des caractéristiques habituelles des tissus est leur indéformabilité dans le plan, qui peut être une qualité ou un défaut selon l'utilisation qui en est faite. On sait bien que la déformation d'un tissu pour lui donner une forme, produit des plis, le tissu n'étant pas susceptible de se déformer élastiquement de par sa structure. La confection est alors l'art d'assembler des pièces de tissu de manière à détenir des formes, que ce soit dans l'industrie vestimentaire ou toute autre industrie. C'est pourquoi, lorsque l'on réalise des matériaux composites, l'assemblage des couches de tissus consiste également à disposer des bandes de tissus de manière à favoriser la réalisation de formes, sans produire de plis.On the other hand and in a very general way, a fabric is a textile structure formed by an assembly of so-called warp threads assembled in so-called weft threads. This structure extends in a plane, the thickness of which is limited to that of the wire or wires used, dimension negligible in relation to the surface of the fabric. One of the usual characteristics of fabrics is their non-deformability in the plane, which can be a quality or a defect depending on the use made of them. It is well known that the deformation of a fabric to give it a shape produces folds, the fabric not being capable of deforming elastically due to its structure. Confection is then the art of assembling pieces of fabric so as to hold forms, whether in the clothing industry or any other industry. This is why, when making composite materials, assembling the layers of fabrics also consists in arranging strips of fabrics so as to promote the production of shapes, without producing folds.
La présente invention a pour objectif de réaliser un matériau composite selon un procédé qui résoud l'ensemble des difficultés exposées : mécanisation, rapidité de réalisation, grande déformabilité, résistance au délaminage, homogénéité, coûts.The aim of the present invention is to produce a composite material according to a process which resolves all the difficulties exposed: mechanization, speed of production, high deformability, resistance to delamination, homogeneity, costs.
L'invention a pour objet un matériau composite d'épaisseur substantielle caractérisé en ce qu'il est constitué d'un seul ensemble de fils de renfort associés à une résine thermosplastique, tissés en trois dimensions.The subject of the invention is a composite material of substantial thickness, characterized in that it consists of a single set of reinforcing threads associated with a thermosplastic resin, woven in three dimensions.
Elle a encore pour objet l'utilisation d'un métier à tisser muni de plusieurs chaines de fils de renfort afin de réaliser un revêtement composite d'épaisseur substantielle.It also relates to the use of a weaving loom provided with several chains of reinforcing threads in order to produce a composite coating of substantial thickness.
Afin de mieux comprendre l'invention on a représenté au dessin annexé un exemple non limitatif de matériau selon l'invention.In order to better understand the invention, there is shown in the accompanying drawing a non-limiting example of material according to the invention.
Comme on le voit sur le dessin, le tissu 1 comporte plusieurs séries de 2 fils de chaîne 2 s'étendant parallèlement les uns des autres. Dans l'exemple le tissu comporte 5 séries de fils de chaîne 2a à 2f. Chaque chaîne est horizontale, les séries se superposent verticalement, formant une feuille épaisse, qui s'étend dans les trois dimensions. Les fils de trame 3 sont passés alternativement dans ces fils de chaîne et, selon le choix, alternent entre le fil du premier niveau 2a et le fil du second 2b, ou du troisième 2c etc.As can be seen in the drawing, the fabric 1 comprises several series of 2
Le tissage peut être modulé selon l'effet que l'on veut donner au tissu.The weaving can be modulated according to the effect which one wants to give to the fabric.
Un tel procédé donne un tissu épais, homogène dans son épaisseur puisque réalisé d'un seul tenant. D'autre part, le fait de tisser en trois dimensions confère à ce tissu une grande déformabilité, par déformation interne.Such a process gives a thick fabric, homogeneous in its thickness since it is made in one piece. On the other hand, the fact of weaving in three dimensions gives this fabric great deformability, by internal deformation.
Dans une première variante de réalisation les fils sont préalablement associés à la résine, c'est-à-dire qu'ils comprennent à la fois des fibres de renfort et leur matrice ou résine. Cet "enresinement" est obtenu soit par mélange intime dans le fil, de fibres de renfort et de résine présentée sous forme de fibres, soit par enrobage de fils de renfort par une gaine de résine.In a first alternative embodiment, the wires are previously associated with the resin, that is to say that they comprise both reinforcing fibers and their matrix or resin. This "entrainment" is obtained either by intimate mixing in the yarn, of reinforcing fibers and of resin presented in the form of fibers, or by coating of reinforcing yarns with a sheath of resin.
Dans une deuxième variante le tissage est réalisé avec des fils ne comportant que des fibres de renfort, exempts de résine. L'association fils-résine, ou "enresinement" est ici un enrobage du tissu; il est réalisé après passage dans le métier à tisser par application au pinceau, pulvérisation, injection, ou toute autre technique connue.In a second variant, weaving is carried out with threads comprising only reinforcing fibers, free of resin. The son-resin association, or "enresinement" is here a coating of the fabric; it is produced after passing through the loom by application with a brush, spraying, injection, or any other known technique.
La première variante est avantageuse en ce qu'elle donne en une seule opération un matériau souple qui peut être immédiatement enroulé, ou découpé en panneaux, et constitue un produit fini prêt à être utilisé.The first variant is advantageous in that it gives, in a single operation, a flexible material which can be immediately wound up, or cut into panels, and constitutes a finished product ready to be used.
Le revêtement obtenu doit ensuite subir un traitement thermique suivi ou non d'un compactage destiné à faire fondre la résine, à donner à ce revêtement la forme désirée et à lui donner ensuite une grande rigidité.The coating obtained must then undergo a heat treatment followed or not by compaction intended to melt the resin, to give this coating the desired shape and then to give it great rigidity.
A titre d'exemple de réalisation on a réalisé un tissu en trois dimensions avec des fils composites à 60% de verre, 40% PEEK, et le traitement à chaud et un estampage donne des plaques de blindage.As an example of an embodiment, a three-dimensional fabric was produced with composite yarns of 60% glass, 40% PEEK, and the heat treatment and stamping gives armor plates.
L'invention apporte entre autre les avantages considérables suivants :
- l'ensemble tridimensionnel est d'une parfaite homogénéité;
- le tissage en profondeur supprime les couches successives il ne peut plus y avoir de délaminage;
- après traitement thermique la présence de bulles d'air entre les fils tissés n'a pas d'influence défavorable sur les caractéristiques de résistance : cette opération peut alors être considérablement simplifiée.
- le matériau peut être plus ou moins comprimé ce qui permet de réaliser très facilement des empreintes qui restent souples;
- le matériau est d'une très grande légèreté; par rapport aux matériaux traditionnels à épaisseur comparable. On peut estimer un gain de poids de l'ordre de 20%.The invention provides, among other things, the following considerable advantages:
- the three-dimensional assembly is perfectly homogeneous;
- deep weaving removes successive layers, there can no longer be delamination;
- After heat treatment, the presence of air bubbles between the woven threads does not have an unfavorable influence on the resistance characteristics: this operation can then be considerably simplified.
- The material can be more or less compressed which makes it very easy to make imprints which remain flexible;
- the material is very light; compared to traditional materials of comparable thickness. We can estimate a weight gain of around 20%.
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8913477 | 1989-10-16 | ||
FR8913477A FR2653141B1 (en) | 1989-10-16 | 1989-10-16 | COMPOSITE MATERIAL AND ITS MANUFACTURING METHOD. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0424216A1 true EP0424216A1 (en) | 1991-04-24 |
EP0424216B1 EP0424216B1 (en) | 1995-01-11 |
Family
ID=9386420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90402823A Expired - Lifetime EP0424216B1 (en) | 1989-10-16 | 1990-10-10 | Composite material, its fabricating process and use of the material |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0424216B1 (en) |
AT (1) | ATE117029T1 (en) |
DE (1) | DE69015962T2 (en) |
FR (1) | FR2653141B1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0570318A1 (en) * | 1992-05-15 | 1993-11-18 | AEROSPATIALE Société Nationale Industrielle | Process for weaving thick reinforcement with several undelaminable layers for composite material and loom for its manufacture |
FR2702222A1 (en) * | 1993-03-03 | 1994-09-09 | Cotton Freres Cie | Three-dimensional multiaxial fabric and its manufacturing process. |
WO2002103098A2 (en) * | 2001-06-15 | 2002-12-27 | Lockheed Martin Corporation | Three-dimensional weave architecture |
FR2917099A1 (en) * | 2007-06-06 | 2008-12-12 | Ensait | METHOD FOR MANUFACTURING A COMPOSITE MATERIAL, IN PARTICULAR FOR BALLISTIC PROTECTION, AND COMPOSITE MATERIAL OBTAINED |
WO2018041990A1 (en) | 2016-09-02 | 2018-03-08 | Porcher Industries | Fibrous structure and 3d preform for a composite part |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3619319A (en) * | 1967-07-05 | 1971-11-09 | Alkor Werk Karl Lissman Kg | Method of making a composite reinforced synthetic resin sheet material |
EP0258102A2 (en) * | 1986-08-01 | 1988-03-02 | Brochier S.A. | Multidimensional textile structure reinforced with stratified material, and its manufacture |
FR2610951A1 (en) * | 1987-02-17 | 1988-08-19 | Aerospatiale | WOVEN REINFORCEMENT FOR COMPOSITE MATERIAL |
-
1989
- 1989-10-16 FR FR8913477A patent/FR2653141B1/en not_active Expired - Fee Related
-
1990
- 1990-10-10 AT AT90402823T patent/ATE117029T1/en not_active IP Right Cessation
- 1990-10-10 DE DE69015962T patent/DE69015962T2/en not_active Expired - Fee Related
- 1990-10-10 EP EP90402823A patent/EP0424216B1/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3619319A (en) * | 1967-07-05 | 1971-11-09 | Alkor Werk Karl Lissman Kg | Method of making a composite reinforced synthetic resin sheet material |
EP0258102A2 (en) * | 1986-08-01 | 1988-03-02 | Brochier S.A. | Multidimensional textile structure reinforced with stratified material, and its manufacture |
FR2610951A1 (en) * | 1987-02-17 | 1988-08-19 | Aerospatiale | WOVEN REINFORCEMENT FOR COMPOSITE MATERIAL |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0570318A1 (en) * | 1992-05-15 | 1993-11-18 | AEROSPATIALE Société Nationale Industrielle | Process for weaving thick reinforcement with several undelaminable layers for composite material and loom for its manufacture |
FR2691174A1 (en) * | 1992-05-15 | 1993-11-19 | Aerospatiale | A method for weaving multiple layers of indelaminable thickeners for composite materials and a weaving machine for its implementation. |
US5353844A (en) * | 1992-05-15 | 1994-10-11 | Societe Nationale Industrielle Et Aerospatiale | Warp handling arrangement for weaving a multi-dimensional thick fabric |
FR2702222A1 (en) * | 1993-03-03 | 1994-09-09 | Cotton Freres Cie | Three-dimensional multiaxial fabric and its manufacturing process. |
WO1994020658A1 (en) * | 1993-03-03 | 1994-09-15 | C.T.M.I. Cotton Textiles Pour Materiaux Innovants | Multiaxial three-dimensional fabric and process for its manufacture |
WO2002103098A2 (en) * | 2001-06-15 | 2002-12-27 | Lockheed Martin Corporation | Three-dimensional weave architecture |
WO2002103098A3 (en) * | 2001-06-15 | 2003-12-18 | Lockheed Corp | Three-dimensional weave architecture |
FR2917099A1 (en) * | 2007-06-06 | 2008-12-12 | Ensait | METHOD FOR MANUFACTURING A COMPOSITE MATERIAL, IN PARTICULAR FOR BALLISTIC PROTECTION, AND COMPOSITE MATERIAL OBTAINED |
WO2008152337A1 (en) * | 2007-06-06 | 2008-12-18 | Ensait | Method of manufacturing a composite, especially a bulletproof composite, and composite obtained |
WO2018041990A1 (en) | 2016-09-02 | 2018-03-08 | Porcher Industries | Fibrous structure and 3d preform for a composite part |
US11383406B2 (en) | 2016-09-02 | 2022-07-12 | Porcher Industries | Fibrous structure and 3D preform for a composite part |
Also Published As
Publication number | Publication date |
---|---|
FR2653141B1 (en) | 1992-04-17 |
FR2653141A1 (en) | 1991-04-19 |
EP0424216B1 (en) | 1995-01-11 |
DE69015962T2 (en) | 1995-08-24 |
DE69015962D1 (en) | 1995-02-23 |
ATE117029T1 (en) | 1995-01-15 |
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