EP0553000B1 - Process for securing a fibrous structure - Google Patents
Process for securing a fibrous structure Download PDFInfo
- Publication number
- EP0553000B1 EP0553000B1 EP93400059A EP93400059A EP0553000B1 EP 0553000 B1 EP0553000 B1 EP 0553000B1 EP 93400059 A EP93400059 A EP 93400059A EP 93400059 A EP93400059 A EP 93400059A EP 0553000 B1 EP0553000 B1 EP 0553000B1
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- European Patent Office
- Prior art keywords
- thread
- needle
- shuttle
- fibrous
- stitching
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
- D04H3/004—Glass yarns or filaments
Definitions
- the present invention relates to the production of reinforcements for the production of fiber-matrix composite parts with high mechanical and / or thermal performance.
- fibrous reinforcements are produced which are trapped in a hardenable matrix.
- the fibers which can be used for the production of such fibrous reinforcements are for example made of carbon, boron, glass, aramid, etc. In the following, such fibers will be called "technical fibers”.
- the object of the present invention is to remedy these drawbacks and to allow the stitching of parts made of technical fibers by means of threads, also of technical fiber, by using conventional sewing machines, even in the case where said parts are thick.
- the technical fiber thread can not be broken or weakened by the stitching needle.
- the technical fiber thread is only in contact with the auxiliary needle thread, which pulls it into the fibrous part. It will be noted that the present invention goes against the knowledge of those skilled in the art, since the latter has always used as a needle thread, the technical thread with which he wished to piguage (see DE-A-2 704 378).
- auxiliary wire acting only as a means of pulling the wire shuttle in technical fiber, can be formed by any known wire having the tensile strength appropriate to its office. It can, for example, be constituted by a known textile yarn, made of natural or synthetic fiber.
- the sewing machine used to implement the method according to the present invention usually comprises a presser foot for engaging and guiding said fibrous piece in a relative displacement relative to the needle, allowing the production of stitches.
- the presser foot exerts pressure on said fibrous part and therefore a compaction thereof.
- Such packing favors the production of the stitch according to the invention and the thickening of said fibrous part.
- Such a fibrous piece can be intended for producing a composite fiber-matrix piece subjected to a stitching operation using a needle thread and a shuttle thread and remarkable in that it comprises technical fibers passing through it parallel to its thickness and formed by said shuttle wire.
- a composite fiber-matrix part can be produced from such a fibrous part by forming said matrix in the latter.
- said technical fibers are not connected to each other by portions of shuttle wire transverse to the thickness of said fibrous part.
- FIG. 1 is a diagrammatic view, in section, of a fibrous piece, making it possible to illustrate the formation, in known manner, of stitches in said piece using a needle thread and a shuttle wire.
- Figure 2 is a schematic sectional view, similar to Figure 1, illustrating the stitching in accordance with the present invention.
- FIG. 3 shows, in a similar view, the fibrous part of FIG. 2, after elimination of the parts of the needle and shuttle threads external to said fibrous part.
- the part 1, shown in FIGS. 1 to 3, is made up of technical fibers (carbon, glass, aramid, boron, etc.) and it has opposite faces 2 and 3. It can be in the form of a fabric, possibly impregnated with hardenable resin, or else in the form of a mattress in which the fibers, dry or pre-impregnated with hardenable resin, are arranged in an organized fashion, in two or more determined directions or else distributed randomly.
- the fibrous part 1 can even be made up of several individual superposed layers.
- FIG. 1 the process of stitching said fibrous piece 1 is illustrated schematically by means of a needle thread 4 coming from a reel, by means of tension adjustment means, and a thread shuttle 5 from a bobbin, by means of wire braking means.
- a needle thread 4 coming from a reel
- tension adjustment means and a thread shuttle 5 from a bobbin
- wire braking means for clarity, the needle, the shuttle, the needle thread spool, the bobbin, said tension adjustment means and said braking means have not been shown; in addition, it was assumed that a relative movement of displacement existed between the needle and the fibrous part 1, this relative displacement being symbolized by the arrow D.
- the needle through which the needle thread 4 enters the fibrous part 1 through the face 2 thereof crosses said fibrous part parallel to its thickness e and projects outside the face 3 by forming a loop 6 with the needle thread 4.
- the shuttle arranged on the side of the face 3 and containing the shuttle thread bobbin 5, crosses then the loop 6.
- the needle rises, draws with it its own needle thread 4 and tightens the loop 6 which traps the thread 5 coming from the shuttle and pulls it through the needle thread 4. This process is repeated throughout a stitch line thanks to the relative movement of movement D. A series of stitch stitches 7 is thus obtained.
- the needle thread 4 and the shuttle thread 5 each form a loop, respectively 8 and 9, said loops 8 and 9 passing one inside the other and forming a contact point 10 between needle thread 4 and shuttle thread 5.
- the means for adjusting the tension of the needle thread 4 and the braking means for the shuttle thread 5 are adjusted so that the contact points 10 are within the thickness of the fibrous part 1, like this is shown in figure 1.
- the various stitching points 7 are connected to each other by bridges 11 of the needle thread and by bridges 12 of the shuttle thread, said bridges 11 resting on the face 2 of the fibrous part 1, while the bridges 12 rest on the face 3 of the latter.
- the branches 9B of the loops 9 of the shuttle wire 5 are pressed and held in place inside the fibrous part 1 by the fibers constituting the latter.
- FIG. 3 after stitching, it is possible to eliminate, on the side of the face 2, the textile yarn 4 and the ends 9A of the loops 9 of the shuttle yarn 5, and / or, on the side of face 3, the bridges 12 of said shuttle wire 5, without harming the quality of the connection established through the fibrous part 1 by the branches 9B, thus constituting technical fibers transverse to the fibrous part 1.
- transverse fibers 9B can be used to join individual fibrous layers of the fibrous part 1 (to form a thick fibrous element or else to join the overlapping edges of two individual fibrous elements), or even to form technical reinforcing fibers parallel to the thickness of said fibrous part 1.
- the sewing machine used to implement the invention comprises a presser foot intended to guide the fibrous part 1 in its movement D relative to the needle, it is understood that this foot -biche can be used for compaction, parallel to the thickness of the fibrous piece 1, of the fibers constituting the latter, so that this thickness is regulated and that the formation of the stitching point, in accordance with the invention and illustrated by the Figure 2, is facilitated.
- the fibrous part 1 can undergo all the known operations of impregnation and hardening of the matrix. It will also be noted that the elimination of the wire 4, of the ends 9A and / or of the bridges 12 can possibly be carried out after obtaining the composite-matrix part produced from the fibrous part 1.
Description
La présente invention concerne la réalisation d'armatures pour la fabrication de pièces composites fibres-matrice à hautes performances mécaniques et/ou thermiques.The present invention relates to the production of reinforcements for the production of fiber-matrix composite parts with high mechanical and / or thermal performance.
On sait que, pour la réalisation de telles pièces composites, on réalise des armatures fibreuses que l'on emprisonne dans une matrice durcissable. Les fibres susceptibles d'être utilisées pour la réalisation de telles armatures fibreuses sont par exemple en carbone, en bore, en verre, en aramide, etc... Ci-après, de telles fibres seront appelées "fibres techniques".It is known that, for the production of such composite parts, fibrous reinforcements are produced which are trapped in a hardenable matrix. The fibers which can be used for the production of such fibrous reinforcements are for example made of carbon, boron, glass, aramid, etc. In the following, such fibers will be called "technical fibers".
On sait de plus que, dans la réalisation desdites armatures fibreuses, on met souvent en oeuvre des processus de piquage au moyen de telles fibres techniques. En effet, par piquage on peut, par exemple :
- assembler des pièces fibreuses individuelles pour former l'armature désirée :
- lier entre elles des couches de matière fibreuse superposées pour former une pièce fibreuse, à partir de laquelle on réalisera une armature ou un élément d'armature ;
- introduire des fibres de direction désirée dans une pièce fibreuse.
- assemble individual fibrous pieces to form the desired reinforcement:
- bonding superimposed layers of fibrous material together to form a fibrous part, from which a reinforcement or a reinforcement element will be produced;
- introduce desired direction fibers into a fibrous piece.
Les essais de piquage de telles pièces fibreuses avec des fils continus constitués de fibres techniques, par la mise en oeuvre de machines à coudre classiques, se sont révélés décevants, sinon impossibles. En effet, à cause de leur nature, les fils de fibres techniques introduits par l'aiguille de piquage dans lesdites pièces fibreuses sont détériorés par cette aiguille, au point de se rompre fréquemment, arrêtant un processus de piquage en cours. Par ailleurs, la fréquence des ruptures des fils de piquage est alors d'autant plus grande que la pièce fibreuse est plus épaisse, de sorte que le piquage de pièces fibreuses épaisses est impossible.The tests of stitching such fibrous parts with continuous threads made up of technical fibers, by the use of conventional sewing machines, have proved disappointing, if not impossible. Indeed, because of their nature, the technical fiber threads introduced by the stitching needle into said fibrous parts are deteriorated by this needle, at point of breaking frequently, stopping an ongoing stitching process. Furthermore, the frequency of breakage of the stitching threads is then all the greater the thicker the fibrous piece, so that the stitching of thick fibrous pieces is impossible.
De toute façon, même lorsque le fil en fibre technique ne casse pas lors du piquage, il peut casser après celui-ci, car, à chaque point de couture, une zone fragilisée est créée au croisement du fil d'aiguille et du fil de navette.Anyway, even when the technical fiber thread does not break during the stitching, it can break after it, because, at each stitch, a weakened area is created at the intersection of the needle thread and the shuttle bus.
Cette technique antérieure connue est par exemple décrite dans le document DE-A-2 704 378. On peut y voir que le piquage de la pièce fibreuse est réalisé avec entrelacement d'un fil d'aiguille formé par le fil en fibre technique et d'un fil de navette d'une façon telle que, à chaque point de piqûre, le fil technique est introduit dans ladite pièce fibreuse par une aiguille, qui est animée d'un mouvement alternatif et qui, dans sa course aller, traverse ladite pièce fibreuse en pénétrant par une première face de celle-ci et en en ressortant par une seconde face opposée à la première, ledit fil de navette étant alors entremêlé audit fil technique du côté de ladite seconde face, tandis que, lors de la course de ladite aiguille, le fil de navette est tiré par ledit fil technique à l'intérieur de ladite pièce fibreuse. On remarquera que, pour tenter d'éviter la rupture du fil technique au contact de l'aiguille, le document DE-A-2 704 378 prévoit une aiguille auxiliaire.This known prior art is for example described in document DE-A-2 704 378. It can be seen there that the stitching of the fibrous piece is carried out with interlacing of a needle thread formed by the technical fiber thread and of '' a shuttle thread in such a way that, at each stitching point, the technical thread is introduced into said fibrous part by a needle, which is driven in an alternating movement and which, in its forward stroke, crosses said part fibrous by penetrating by a first face of the latter and by coming out of it by a second face opposite to the first, said shuttle wire then being entangled with said technical wire on the side of said second face, while, during the course of said needle, the shuttle wire is pulled by said technical wire inside said fibrous part. It will be noted that, in an attempt to avoid breaking the technical thread in contact with the needle, document DE-A-2 704 378 provides an auxiliary needle.
Quoi qu'il en soit, dans la réalité industrielle, pour pouvoir piquer une pièce fibreuse avec un fil en fibre technique, on est amené à réaliser des dispositifs de piquage complexes et/ou comportant un support spécial pour la pièce fibreuse à piquer, comme ceux par exemple décrits dans les documents US-A-2 283 802 et US-A-3 322 868.Anyway, in industrial reality, to be able to stitch a fibrous piece with a technical fiber thread, we have to make complex stitching devices and / or comprising a special support for the fibrous piece to stitch, as those for example described in documents US-A-2,283,802 and US-A-3,322,868.
La présente invention a pour objet de remédier à ces inconvénients et de permettre le piquage de pièces en fibres techniques au moyen de fils, également de fibre technique, par la mise en oeuvre de machines à coudre classiques, même dans le cas où lesdites pièces sont épaisses.The object of the present invention is to remedy these drawbacks and to allow the stitching of parts made of technical fibers by means of threads, also of technical fiber, by using conventional sewing machines, even in the case where said parts are thick.
A cette fin, selon l'invention, le procédé pour le piquage, au moyen d'un fil en fibre technique, d'une pièce fibreuse destinée à la réalisation d'une pièce composite fibres-matrice, procédé selon lequel le piquage est réalisé avec entrelacement d'un fil d'aiguille et d'un fil de navette d'une façon telle que, à chaque point de piqûre, le fil d'aiguille est introduit dans ladite pièce fibreuse par une aiguille, qui est animée d'un mouvement alternatif et qui, dans sa course aller, traverse ladite pièce fibreuse en pénétrant par une première face de celle-ci et en en ressortant par une seconde face opposée à la première, ledit fil de navette étant alors entremêlé audit fil d'aiguille du côté de ladite seconde face, tandis que, lors de la course retour de ladite aiguille, le fil de navette est tiré par ledit fil d'aiguille à l'intérieur de ladite pièce fibreuse, est remarquable en ce que :
- ledit fil d'aiguille est constitué par un fil auxiliaire résistant à la traction ;
- ledit fil de navette est constitué par ledit fil en fibre technique ; et
- la tension du fil de navette et la tension du fil d'aiguille sont réglées à des niveaux suffisamment faible et suffisamment élevé, respectivement, pour que, à la fin dudit point de piqûre, ledit fil de navette fasse saillie à l'extérieur de ladite pièce fibreuse, du côté de ladite première face de celle-ci, et ledit fil d'aiguille se trouve complètement à l'extérieur de ladite pièce fibreuse, également du côté de ladite première face de celle-ci.
- said needle thread is constituted by an auxiliary tensile thread;
- said shuttle wire consists of said technical fiber wire; and
- the shuttle thread tension and the needle thread tension are adjusted to sufficiently low and sufficiently high levels, respectively, so that, at the end of said stitching, said shuttle thread protrudes outside said fibrous part, on the side of said first face thereof, and said needle thread is completely outside of said fibrous part, also on the side of said first face thereof.
Ainsi, grâce à l'invention, le fil de fibre technique ne peut être rompu ou fragilisé par l'aiguille de piquage. Le fil de fibre technique n'est qu'au contact du fil auxiliaire d'aiguille, qui le tire dans la pièce fibreuse. On remarquera que la présente invention va à l'encontre des connaissances de l'homme de métier, puisque celui-ci a toujours utilisé comme fil d'aiguille, le fil technique avec lequel il désirait réaliser un piguage (voir DE-A-2 704 378).Thus, thanks to the invention, the technical fiber thread can not be broken or weakened by the stitching needle. The technical fiber thread is only in contact with the auxiliary needle thread, which pulls it into the fibrous part. It will be noted that the present invention goes against the knowledge of those skilled in the art, since the latter has always used as a needle thread, the technical thread with which he wished to piguage (see DE-A-2 704 378).
A cause du réglage particulier des tensions de fils utilisées dans la présente invention, seul le fil de fibre technique est emprisonné à l'intérieur de ladite pièce fibreuse. Le fil auxiliaire est extérieur à celle-ci et ne peut donc constituer une hétérogénéité pour ladite pièce fibreuse. Un tel fil auxiliaire, n'intervenant que comme moyen de traction du fil de navette en fibre technique, peut être formé par tout fil connu présentant la résistance à la traction appropriée à son office. Il peut, par exemple, être constitué par un fil textile connu, en fibre naturelle ou synthétique.Because of the particular adjustment of the thread tensions used in the present invention, only the technical fiber thread is trapped inside said fibrous part. The auxiliary wire is external to it and cannot therefore constitute heterogeneity for said fibrous part. Such an auxiliary wire, acting only as a means of pulling the wire shuttle in technical fiber, can be formed by any known wire having the tensile strength appropriate to its office. It can, for example, be constituted by a known textile yarn, made of natural or synthetic fiber.
De plus, étant extérieur à ladite pièce fibreuse, il peut être facilement éliminé de cette dernière.In addition, being external to said fibrous part, it can be easily eliminated from the latter.
On remarquera, de plus, que, étant donné la texture fibreuse de ladite pièce, les portions du fil de fibre technique se trouvant à l'intérieur de la pièce fibreuse sont maintenues en place par la pression latérale exercée par les autres fibres de ladite pièce. Par suite, il est possible, éventuellement, d'éliminer les parties du fil de fibre technique qui apparaissent sur lesdites première et seconde faces de la pièce fibreuse, sans pour cela nuire à la solidité des points de piqûre.It will also be noted that, given the fibrous texture of said piece, the portions of the technical fiber yarn located inside the fibrous piece are held in place by the lateral pressure exerted by the other fibers of said piece . As a result, it is possible, if necessary, to eliminate the parts of the technical fiber yarn which appear on said first and second faces of the fibrous part, without thereby affecting the solidity of the stitches.
On sait que, sur les machines à coudre classiques, il existe des moyens de réglage de la tension du fil d'aiguille et des moyens de freinage du fil de navette.It is known that, on conventional sewing machines, there are means for adjusting the tension of the needle thread and means for braking the shuttle thread.
Afin d'obtenir le "point" de piqûre conforme à la présente invention, il peut être nécessaire de prévoir des moyens supplémentaires, tels que chicanes, freins de fil à flasques, etc..., pour augmenter jusqu'au niveau approprié la tension du fil textile d'aiguille. En revanche, il peut être nécessaire de diminuer la tension imposée au fil de navette par lesdits moyens de freinage, par exemple en réduisant au maximum les frottements intervenant dans leur fonctionnement.In order to obtain the puncture "point" in accordance with the present invention, it may be necessary to provide additional means, such as baffles, flanged wire brakes, etc., to increase the tension to the appropriate level. needle textile thread. On the other hand, it may be necessary to reduce the tension imposed on the shuttle wire by said braking means, for example by reducing as much as possible the friction involved in their operation.
Par ailleurs, on remarquera qu'il est avantageux que la machine à coudre utilisée pour mettre en oeuvre le procédé conforme à la présente invention comporte, de façon usuelle, un pied-de-biche pour engager et guider ladite pièce fibreuse dans un déplacement relatif par rapport à l'aiguille, permettant la réalisation de suites de points de piqûre. En effet, le pied-de-biche exerce une pression sur ladite pièce fibreuse et donc un tassage de celle-ci. Un tel tassage favorise la réalisation du point conforme à l'invention et la mise à épaisseur de ladite pièce fibreuse.Furthermore, it will be noted that it is advantageous that the sewing machine used to implement the method according to the present invention usually comprises a presser foot for engaging and guiding said fibrous piece in a relative displacement relative to the needle, allowing the production of stitches. Indeed, the presser foot exerts pressure on said fibrous part and therefore a compaction thereof. Such packing favors the production of the stitch according to the invention and the thickening of said fibrous part.
Une telle pièce fibreuse peut être destinée à la réalisation d'une pièce composite fibres-matrice soumise à une opération de piquage à l'aide d'un fil d'aiguille et d'un fil de navette et remarquable en ce qu'elle comporte des fibres techniques la traversant parallèlement à son épaisseur et formées par ledit fil de navette.Such a fibrous piece can be intended for producing a composite fiber-matrix piece subjected to a stitching operation using a needle thread and a shuttle thread and remarkable in that it comprises technical fibers passing through it parallel to its thickness and formed by said shuttle wire.
Une pièce composite fibres-matrice peut être réalisée à partir d'une telle pièce fibreuse par formation de ladite matrice dans cette dernière. De préférence, dans cette pièce composite, lesdites fibres techniques ne sont pas reliées les unes aux autres par des portions de fil de navette transversales à l'épaisseur de ladite pièce fibreuse.A composite fiber-matrix part can be produced from such a fibrous part by forming said matrix in the latter. Preferably, in this composite part, said technical fibers are not connected to each other by portions of shuttle wire transverse to the thickness of said fibrous part.
Les figures du dessin annexé feront bien comprendre comment l'invention peut être réalisée. Sur ces figures, des références identiques désignent des éléments semblables.The figures of the appended drawing will make it clear how the invention can be implemented. In these figures, identical references designate similar elements.
La figure 1 est une vue schématique, en coupe, d'une pièce fibreuse, permettant d'illustrer la formation, de façon connue, de points de couture dans ladite pièce à l'aide d'un fil d'aiguille et d'un fil de navette.FIG. 1 is a diagrammatic view, in section, of a fibrous piece, making it possible to illustrate the formation, in known manner, of stitches in said piece using a needle thread and a shuttle wire.
La figure 2 est une vue en coupe schématique, analogue à la figure 1, illustrant les points de couture conformément à la présente invention.Figure 2 is a schematic sectional view, similar to Figure 1, illustrating the stitching in accordance with the present invention.
La figure 3 montre, en vue analogue, la pièce fibreuse de la figure 2, après élimination des parties des fils d'aiguille et de navette extérieures à ladite pièce fibreuse.FIG. 3 shows, in a similar view, the fibrous part of FIG. 2, after elimination of the parts of the needle and shuttle threads external to said fibrous part.
La pièce 1, montrée sur les figures 1 à 3, est constituée de fibres techniques (carbone, verre, aramide, bore, etc...) et elle présente des faces opposées 2 et 3. Elle peut se présenter sous la forme d'un tissu, éventuellement imprégné de résine durcissable, ou bien sous la forme d'un matelas dans lequel les fibres, sèches ou préimprégnées de résine durcissable, sont disposées de façon organisée, suivant deux ou plusieurs directions déterminées ou bien distribuées de façon aléatoire. La pièce fibreuse 1 peut même être constituée de plusieurs couches individuelles superposées.The
Sur la figure 1, on a illustré schématiquement le processus de piquage de ladite pièce fibreuse 1 au moyen d'un fil d'aiguille 4 provenant d'une bobine, par l'intermédiaire de moyens de réglage de tension, et d'un fil de navette 5 provenant d'une canette, par l'intermédiaire de moyens de freinage de fil. Sur cette figure, à des fins de clarté, on n'a pas représenté l'aiguille, la navette, la bobine de fil d'aiguille, la canette, lesdits moyens de réglage de tension et lesdits moyens de freinage ; de plus, on y a supposé qu'un mouvement relatif de déplacement existait entre l'aiguille et la pièce fibreuse 1, ce déplacement relatif étant symbolisé par la flèche D.In FIG. 1, the process of stitching said
Ainsi, comme cela est illustré schématiquement à l'extrémité de droite de la figure 1, l'aiguille dans laquelle passe le fil d'aiguille 4 pénètre dans la pièce fibreuse 1 à travers la face 2 de celle-ci, traverse ladite pièce fibreuse parallèlement à son épaisseur e et fait saillie à l'extérieur de la face 3 en formant une boucle 6 avec le fil d'aiguille 4. La navette, disposée du côté de la face 3 et contenant la canette de fil de navette 5, traverse alors la boucle 6. Dès que la boucle 6 a ainsi été traversée par le fil de navette 5, l'aiguille se relève, tire avec elle son propre fil d'aiguille 4 et serre la boucle 6 qui emprisonne le fil 5 provenant de la navette et le tire par l'intermédiaire du fil d'aiguille 4. Ce processus est répété tout au long d'une ligne de piqûre grâce au mouvement de déplacement relatif D. On obtient ainsi une suite de points de piqûre 7.Thus, as illustrated diagrammatically at the right end of FIG. 1, the needle through which the needle thread 4 enters the
A chaque point de piqûre 7 terminé, le fil d'aiguille 4 et le fil de navette 5 forment chacun une boucle, respectivement 8 et 9, lesdites boucles 8 et 9 passant l'une dans l'autre et formant un point de contact 10 entre le fil d'aiguille 4 et le fil de navette 5.At each completed stitching point 7, the needle thread 4 and the shuttle thread 5 each form a loop, respectively 8 and 9, said
De façon usuelle, les moyens de réglage de la tension du fil d'aiguille 4 et les moyens de freinage du fil de navette 5 sont réglés pour que les points de contact 10 se trouvent dans l'épaisseur de la pièce fibreuse 1, comme cela est représenté sur la figure 1.Usually, the means for adjusting the tension of the needle thread 4 and the braking means for the shuttle thread 5 are adjusted so that the
Les différents points de piqûre 7 sont reliés l'un à l'autre par des ponts 11 du fil d'aiguille et par des ponts 12 du fil de navette, lesdits ponts 11 reposant sur la face 2 de la pièce fibreuse 1, tandis que les ponts 12 reposent sur la face 3 de cette dernière.The various stitching points 7 are connected to each other by
Si l'on désire introduire dans la pièce fibreuse 1 des fibres techniques par piquage et que, à cet effet, on utilise pour le fil d'aiguille 4 et pour le fil de navette 5 des fils continus constitués de telles fibres techniques, on constate que le fil d'aiguille 4 casse fréquemment, d'autant plus fréquemment que la pièce fibreuse 1 est plus épaisse, rendant le piquage pratiquement impossible. De plus, dans les points 7 réalisés entre deux casses de fil, aux points de contact 10, le fil d'aiguille 4 est grandement fragilisé, de sorte que des ruptures dudit fil d'aiguille 4 peuvent se produire au niveau des points de contact 10 après piquage.If it is desired to introduce technical fibers into the
Pour remédier à cet inconvénient et permettre d'introduire dans la pièce fibreuse 1 des fibres techniques par piquage au moyen d'une machine à coudre ordinaire, selon l'invention :
- on choisit, pour le fil d'aiguille 4, un fil textile classique résistant à la traction ;
- on choisit, pour le fil de navette 5, le fil en fibre technique que l'on veut introduire dans la pièce fibreuse 1 ;
- on règle la tension du fil d'aiguille 4 à un niveau élevé, par réglage adéquat desdits moyens de réglage de tension et, éventuellement, en prévoyant de tels moyens additionnels ; et
- on règle la tension du fil de navette 5 à un niveau faible, par réduction du freinage procuré par lesdits moyens de freinage.
- one chooses, for the needle thread 4, a conventional textile thread resistant to traction;
- we choose, for the shuttle wire 5, the technical fiber wire that we want to introduce into the
fibrous part 1; - the tension of the needle thread 4 is adjusted to a high level, by adequate adjustment of said tension adjustment means and, optionally, by providing such additional means; and
- the tension of the shuttle wire 5 is adjusted to a low level, by reduction of the braking provided by said braking means.
Ainsi, par réglage adéquat des tensions du fil d'aiguille 4 et du fil de navette 5 à ces niveaux, élevé et faible, respectifs, on fait en sorte que, selon l'invention, à la fin d'un point de piqûre (réalisé comme expliqué ci-dessus en regard de la partie droite de la figure 1) :
la boucle 8 du fil d'aiguille 4 disparaît, ledit fil 4 reposant de façon rectiligne sur laface 2 de la pièce fibreuse 1 ; etla boucle 9 du fil de navette 5, traversée par ledit fil 4, est tirée par celui-ci, jusqu'à ce que son extrémité 9A (qui coopère avec le fil d'aiguille 4 pour la traction à travers la pièce fibreuse 1) fasse saillie par rapport à laditeface 2 de la pièce fibreuse 1.
- the
loop 8 of the needle thread 4 disappears, said thread 4 resting rectilinearly on theface 2 of thefibrous part 1; and - the
loop 9 of the shuttle thread 5, crossed by said thread 4, is pulled by the latter, until its end 9A (which cooperates with the needle thread 4 for pulling through the fibrous part 1) protrudes from saidface 2 of thefibrous part 1.
Ainsi, à l'intérieur de la pièce fibreuse 1, seules subsistent les deux branches 9B de chacune des boucles 9, le fil 4 reposant, tendu, sur la face 2 de la pièce fibreuse 1, tandis que, du côté de la face 3 de celle-ci , subsistent des ponts 12. Ceci est illustré schématiquement par la figure 2.Thus, inside the
Les branches 9B des boucles 9 du fil de navette 5 (fil en fibre technique) sont pressées et maintenues en place à l'intérieur de la pièce fibreuse 1 par les fibres constituant celle-ci. Par suite, comme cela est illustré sur la figure 3, après piquage, il est possible d'éliminer, du côté de la face 2, le fil textile 4 et les extrémités 9A des boucles 9 du fil de navette 5, et/ou, du côté de la face 3, les ponts 12 dudit fil de navette 5, sans nuire à la qualité de la liaison établie à travers la pièce fibreuse 1 par les branches 9B, constituant ainsi des fibres techniques transversales à la pièce fibreuse 1.The
De telles fibres transversales 9B peuvent servir à assembler des couches fibreuses individuelles de la pièce fibreuse 1 (pour former un élément fibreux épais ou bien pour solidariser les bords chevauchants de deux éléments fibreux individuels), ou bien encore à former des fibres techniques de renfort parallèlement à l'épaisseur de ladite pièce fibreuse 1.Such
Si, de façon usuelle, la machine à coudre utilisée pour mettre en oeuvre l'invention comporte un pied-de-biche destiné à guider la pièce fibreuse 1 dans son défilement D par rapport à l'aiguille, on comprend que ce pied-de-biche peut servir au tassement, parallèlement à l'épaisseur de la pièce fibreuse 1, des fibres constituant celle-ci, de sorte que cette épaisseur est régulée et que la formation du point de piqûre, conforme à l'invention et illustrée par la figure 2, en est facilitée.If, in the usual way, the sewing machine used to implement the invention comprises a presser foot intended to guide the
Bien entendu, après réalisation du piquage selon l'invention, la pièce fibreuse 1 peut subir toutes les opérations connues d'imprégnation et de durcissement de matrice. On remarquera d'ailleurs que l'élimination du fil 4, des extrémités 9A et/ou des ponts 12 peut être réalisée éventuellement après obtention de la pièce composite-matrice réalisée à partir de la pièce fibreuse 1.Of course, after completion of the stitching according to the invention, the
Claims (4)
- Process for the stitching, by means of an engineering-fibre thread (5), of a fibrous component (1) intended for the production of a fibre/matrix composite component, according to which process the stitching is produced by interlacement of a needle thread (4) with a shuttle thread (5) in such a way that, at each lock stitch (7), the needle thread is inserted into the said fibrous component by a needle which is given an alternating movement and, in its forward stroke, passes through the said fibrous component by penetrating via a first face (2) thereof and by emerging therefrom via a second face (3) opposite the first, the said shuttle thread then being interlocked with the said needle thread on the said second face side, while, during the return stroke of the said needle, the shuttle thread is drawn by the said needle thread into the said fibrous component, the tensions in the said shuttle threads and needle threads being different, characterized in that:- the said needle thread (4) consists of an auxiliary thread strong in tension;- the said shuttle thread (5) consists of the said engineering-fibre thread; and- the tension in the shuttle thread (5) and the tension in the needle thread (4) are adjusted, respectively, to sufficiently low and sufficiently high levels so that, at the end of the said stitch (7), the said shuttle thread (5) projects (at 9A) outside the said fibrous component (1), on the side of the said first face (2) thereof, and the said needle thread (4) lies completely outside the said fibrous component (1) also on the side of the said first face (2) thereof.
- Process according to Claim 1, characterized in that the said auxiliary thread forming the needle thread is a textile thread made of natural or man-made fibre.
- Process according to Claim 2, characterized in that the said auxiliary thread forming the needle thread is removed after stitching the said fibrous component.
- Process according to either of Claims 1 and 2, characterized in that those parts (9A, 12) of the shuttle thread which appear on the said first and second faces (2, 3) of the said fibrous component (1) are removed after stitching the latter.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9200761 | 1992-01-24 | ||
FR9200761A FR2686627B1 (en) | 1992-01-24 | 1992-01-24 | METHOD FOR STITCHING A FIBROUS PIECE, FIBROUS PIECE THUS OBTAINED AND FIBER-MATRIX COMPOSITE PIECE OBTAINED FROM SAID FIBROUS PIECE. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0553000A1 EP0553000A1 (en) | 1993-07-28 |
EP0553000B1 true EP0553000B1 (en) | 1996-11-06 |
Family
ID=9425940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP93400059A Expired - Lifetime EP0553000B1 (en) | 1992-01-24 | 1993-01-13 | Process for securing a fibrous structure |
Country Status (6)
Country | Link |
---|---|
US (1) | US5333562A (en) |
EP (1) | EP0553000B1 (en) |
JP (1) | JP3396244B2 (en) |
CA (1) | CA2086568C (en) |
DE (1) | DE69305755T2 (en) |
FR (1) | FR2686627B1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2718802B1 (en) * | 1994-04-18 | 1996-06-14 | Aerospatiale | Rod made of composite material and process for its manufacture. |
FR2718757B1 (en) * | 1994-04-18 | 1996-06-14 | Aerospatiale | Method and machine for producing a plate-shaped reinforcement for a piece of composite material. |
US6676785B2 (en) | 2001-04-06 | 2004-01-13 | Ebert Composites Corporation | Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate |
US7785693B2 (en) | 2001-04-06 | 2010-08-31 | Ebert Composites Corporation | Composite laminate structure |
US20050025948A1 (en) * | 2001-04-06 | 2005-02-03 | Johnson David W. | Composite laminate reinforced with curvilinear 3-D fiber and method of making the same |
US7056576B2 (en) * | 2001-04-06 | 2006-06-06 | Ebert Composites, Inc. | 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates |
US7731046B2 (en) * | 2001-04-06 | 2010-06-08 | Ebert Composites Corporation | Composite sandwich panel and method of making same |
US7105071B2 (en) | 2001-04-06 | 2006-09-12 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US6645333B2 (en) | 2001-04-06 | 2003-11-11 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US20050118448A1 (en) * | 2002-12-05 | 2005-06-02 | Olin Corporation, A Corporation Of The Commonwealth Of Virginia | Laser ablation resistant copper foil |
IL163135A (en) * | 2004-07-21 | 2010-02-17 | Yair Eilam | Sewing machine for stitching with a composite thread |
ITMI20050119A1 (en) * | 2005-01-28 | 2006-07-29 | Top Glass Spa | PANEL STRUCTURE AND ITS CONSTRUCTION PROCEDURE |
DE102013218572A1 (en) | 2013-09-17 | 2015-03-19 | Audi Ag | Method for joining preform structures |
JP6187410B2 (en) * | 2014-08-04 | 2017-08-30 | 豊田合成株式会社 | Stitch line formation method |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US298053A (en) * | 1884-05-06 | Eduaed bally | ||
US795290A (en) * | 1904-02-23 | 1905-07-25 | George A Lowry | Fabric and method of making same. |
US2283802A (en) * | 1941-09-20 | 1942-05-19 | Clair H Gingher | Fabric making machine |
US3322868A (en) * | 1963-07-02 | 1967-05-30 | Douglas Aircraft Co Inc | Three dimensional reinforced structure |
US3291085A (en) * | 1964-08-14 | 1966-12-13 | Levy David | Method of sewing a footwear construction |
US3533893A (en) * | 1966-11-22 | 1970-10-13 | Fred W Hartstein | Decorative tufted fabric |
US3921085A (en) * | 1973-11-23 | 1975-11-18 | William J Keane | Frequency discriminator apparatus |
FR2315562A1 (en) * | 1975-06-26 | 1977-01-21 | Commissariat Energie Atomique | METHOD AND DEVICES FOR MANUFACTURING BODIES OR PARTS FROM THREE-DIMENSIONAL FABRICS |
FR2355936A1 (en) * | 1976-02-03 | 1978-01-20 | Commissariat Energie Atomique | PROCESS FOR MANUFACTURING PARTS IN THREE-DIMENSIONAL FABRICS |
FR2565262B1 (en) * | 1984-05-29 | 1986-09-26 | Europ Propulsion | METHOD FOR MANUFACTURING A MULTI-DIRECTIONAL FIBROUS TEXTURE AND DEVICE FOR CARRYING OUT THIS METHOD |
JPS63165562A (en) * | 1986-12-27 | 1988-07-08 | 電気化学工業株式会社 | Heat resistant inorganic fiber molded body and its production |
US5038693A (en) * | 1989-09-21 | 1991-08-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Composite flexible blanket insulation |
-
1992
- 1992-01-24 FR FR9200761A patent/FR2686627B1/en not_active Expired - Fee Related
- 1992-12-21 US US07/993,704 patent/US5333562A/en not_active Expired - Lifetime
- 1992-12-31 CA CA002086568A patent/CA2086568C/en not_active Expired - Fee Related
-
1993
- 1993-01-13 EP EP93400059A patent/EP0553000B1/en not_active Expired - Lifetime
- 1993-01-13 DE DE69305755T patent/DE69305755T2/en not_active Expired - Fee Related
- 1993-01-22 JP JP00901193A patent/JP3396244B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0553000A1 (en) | 1993-07-28 |
DE69305755T2 (en) | 1997-03-20 |
JP3396244B2 (en) | 2003-04-14 |
DE69305755D1 (en) | 1996-12-12 |
CA2086568C (en) | 2000-09-26 |
US5333562A (en) | 1994-08-02 |
FR2686627B1 (en) | 1995-06-16 |
CA2086568A1 (en) | 1993-07-25 |
JPH0686877A (en) | 1994-03-29 |
FR2686627A1 (en) | 1993-07-30 |
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