FR2584106A1 - METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS - Google Patents
METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS Download PDFInfo
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- FR2584106A1 FR2584106A1 FR8509820A FR8509820A FR2584106A1 FR 2584106 A1 FR2584106 A1 FR 2584106A1 FR 8509820 A FR8509820 A FR 8509820A FR 8509820 A FR8509820 A FR 8509820A FR 2584106 A1 FR2584106 A1 FR 2584106A1
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- needling
- needles
- fibrous material
- fibers
- carbon
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
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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
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/44—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling
- D04H1/46—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres
- D04H1/498—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres entanglement of layered webs
-
- 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
- D04H18/00—Needling machines
- D04H18/02—Needling machines with needles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B2038/0052—Other operations not otherwise provided for
- B32B2038/008—Sewing, stitching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/105—Ceramic fibres
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Nonwoven Fabrics (AREA)
- Laminated Bodies (AREA)
Abstract
DES BANDES PLANES 20 DE MATERIAU FIBREUX SONT SUPERPOSEES SUR UN PLATEAU 10 EN AIGUILLETANT CHAQUE NOUVELLE BANDE SUR LA PRECEDENTE JUSQU'A OBTENTION DE L'EPAISSEUR DESIREE, ET LA DISTANCE ENTRE LE PLATEAU ET LES AIGUILLES EST MODIFIEE A CHAQUE FOIS QU'UNE NOUVELLE BANDE EST AMENEE SUR L'EMPILEMENT, DE MANIERE A REALISER UN AIGUILLETAGE SENSIBLEMENT UNIFORME DANS TOUTE L'EPAISSEUR DE LA STRUCTURE. LE PLATEAU ET LES AIGUILLES SONT MUTUELLEMENT ECARTES A CHAQUE AMENEE D'UN NOUVELLE BANDE, D'UNE DISTANCE EGALE A L'EPAISSEUR DE LA BANDE UNE FOIS AIGUILLETEE.PLANAR STRIPS 20 OF FIBROUS MATERIAL ARE OVERLAYED ON A TRAY 10 NEEDLEING EACH NEW STRIP ON THE PREVIOUS ONE UNTIL THE DESIRED THICKNESS IS OBTAINED, AND THE DISTANCE BETWEEN THE TRAY AND THE NEEDLES IS CHANGED EVERY TIME. IS BROUGHT ON THE STACKING, TO MANUFACTURE A SUBSTANTIALLY UNIFORM NEEDLE THROUGHOUT THE THICKNESS OF THE STRUCTURE. THE TRAY AND THE NEEDLES ARE MUTUALLY SPACED EACH EACH OF A NEW STRIP, EQUAL TO THE THICKNESS OF THE STRIP WHEN NEEDED.
Description
Procédé de fabrication de structures tridimensionnelles par aiguilletageMethod for manufacturing three-dimensional structures by needling
de couches planes de matériau fibreux superposées et matériau fibreux utilisé pour la mise en oeuvre du procédé La présente invention concerne la fabrication de structures tridimensionnelles formées par des couches planes superposées de matériau fibreux liées entre elles par aiguilletage. Le domaine d'application de l'invention est plus particulièrement, mais non exclusivement, la fabrication de structures de renfort tridimensionnelles destinées à la réalisation de pièces en matériau composites par densification des structures de renfort, notamment pour fabriquer des disques de freins, tuiles composites, etc. Un procédé connu de fabrication de structures planes par aiguilletage de couches superposées de matériau fibreux est décrit dans le certificat d'utilité FR 2 196 966. Selon ce procédé connu, des couches planes unidirectionnelles sont superposées en étant croisées puis sont aiguilletées. Bien qu'aucune limitation ne soit donnée quant au nombre de couches superposées, ce document est silencieux sur les moyens à utiliser pour réaliser une structure épaisse avec des caractéristiques homogènes dans toute la structure. Le brevet FR 2 414 574 décrit quant à lui un procédé de fabrication de renfort fibreux pour disques de frein par formation d'anneaux de feutre par aiguilletage, empilement des anneaux les uns sur les autres jusqu'à obtention de l'épaisseur souhaitée, et maintien de l'empilement en vue de la densification. Il est indiqué que l'ensemble des anneaux empilés peut être aiguilleté, The present invention relates to the manufacture of three-dimensional structures formed by superimposed planar layers of fibrous material bonded together by needling. The field of application of the invention is more particularly, but not exclusively, the manufacture of three-dimensional reinforcement structures intended for the production of parts made of composite material by densification of the reinforcement structures, in particular for manufacturing brake discs, composite tiles , etc. A known method of manufacturing planar structures by needling superimposed layers of fibrous material is described in the utility certificate FR 2 196 966. According to this known method, planar unidirectional layers are superimposed by being crossed and then needled. Although no limitation is given as to the number of superimposed layers, this document is silent on the means to be used to achieve a thick structure with homogeneous characteristics throughout the structure. The patent FR 2 414 574 describes a process for manufacturing fibrous reinforcement for brake discs by forming felt rings by needling, stacking the rings on top of each other until the desired thickness is obtained, and maintenance of the stack for densification. It is indicated that all of the stacked rings can be needled,
mais sans décrire le mode opératoire. but without describing the procedure.
Les deux documents ci-dessus évoqués, de même que le brevet US 3 772 115 divulguent en fait des techniques d'aiguilletage pour des faibles épaisseurs, et il s'avère que ces techniques ne sont pas telles quelles transposables pour les fortes épaisseurs. Une raison tient à ce que, à partir d'une certaine pénétration dans les couches superposées, les aiguilles perdent de leur agressivité en raison du bouchage de leurs aspérités par des morceaux de fibres arrachés des couches de matériau déjà traversées; les aiguilles ne peuvent alors remplir correctement leur fonction, rendant impossible l'obtention des mêmes caractéristiques d'aiguilletage dans toute l'épaisseur de l'empilement. Or, pour des matériaux destinés à être exposés à des contraintes thermomécaniques sévères, il est important de maintenir les propriétés constantes dans toute la masse afin, par The two documents mentioned above, as well as US Pat. No. 3,772,115 in fact disclose needling techniques for small thicknesses, and it turns out that these techniques are not as such transposable for large thicknesses. One reason is that, from a certain penetration in the superimposed layers, the needles lose their aggressiveness due to the blocking of their roughness by pieces of fibers torn from the layers of material already crossed; the needles cannot then correctly fulfill their function, making it impossible to obtain the same needling characteristics throughout the thickness of the stack. However, for materials intended to be exposed to severe thermomechanical stresses, it is important to maintain the properties constant throughout the mass so, by
exemple, d'éviter des délaminages. example, to avoid delamination.
Aussi, selon l'un de ses aspects, la présente invention a- Also, according to one of its aspects, the present invention has-
t-elle pour but de fournir un procédé permettant de réaliser des structures tridimensionnelles épaisses par aiguilletage de couches planes superposées avec une densité d'aiguilletage constante dans does it aim to provide a method for producing thick three-dimensional structures by needling superimposed planar layers with a constant needling density in
toute l'épaisseur.the entire thickness.
Ce but est atteint grâce à un procédé selon lequel, conformément à l'invention, des bandes planes de matériau fibreux sont superposées sur un plateau en aiguilletant chaque nouvelle bande sur la précédente jusqu'à obtention de l'épaisseur désirée, et la distance entre le plateau et les aiguilles est modifiée à chaque fois qu'une nouvelle bande est amenée sur l'empilement, de manière a réaliser un aiguilletage sensiblement uniforme dans This object is achieved by a process according to which, in accordance with the invention, flat strips of fibrous material are superimposed on a plate by needling each new strip on the previous one until the desired thickness is obtained, and the distance between the plate and the needles are modified each time a new strip is brought onto the stack, so as to achieve a substantially uniform needling in
toute l'épaisseur de la structure.the entire thickness of the structure.
Le plateau et les aiguilles sont mutuellement écartés, à chaque amenée d'une nouvelle bande, d'une distance égale à The plate and the needles are separated from each other, each time a new strip is brought in, by a distance equal to
l'épaisseur de la bande une fois aiguilletée. the thickness of the strip once needled.
A chaque passe d'aiguilletage, les aiguilles traversent plusieurs bandes superposées. Aussi, afin d'obtenir un matériau homogène dans toute son épaisseur, des passes d'aiguilletage de finition sont réalisées après l'amenée et l'aiguilletage de la dernière bande, de manière que la densité d'aiguilletage dans les couches supérieures soit sensiblement égale à celle dans les autres couches. Après chaque passe de finition, le plateau et les aiguilles sont mutuellement déplacés comme si une nouvelle bande était amenée. Du fait qu'elles effectuent une partie de leur course dans l'air au cours des passes de finition, les aiguilles sont plus agressives vis à vis des couches supérieures de l'empilement que si elles avaient dû préalablement traverser d'autres couches avec bouchage plus ou moins important de leurs aspérités. Pour cette raison, le nombre de passes de finition est de préférence inférieur à celui nécessaire pour arriver jusqu'au moment o les aiguilles n'atteignent plus la dernière couche de l'empilement. Selon un autre de ses aspects, la présente invention vise un matériau fibreux apte à être utilisé pour la mise en oeuvre du procédé. Le choix du matériau fibreux est guidé par l'application envisagée, tout en faisant en sorte que la texture aiguilletée se prête à l'opération de densification, c'est-à-dire présente une At each needling pass, the needles pass through several superimposed bands. Also, in order to obtain a homogeneous material throughout its thickness, finishing needling passes are carried out after the feeding and needling of the last strip, so that the needling density in the upper layers is substantially equal to that in the other layers. After each finishing pass, the platter and the needles are moved to each other as if a new strip has been fed. Because they perform part of their course in the air during the finishing passes, the needles are more aggressive towards the upper layers of the stack than if they had previously had to cross other layers with capping more or less important of their roughness. For this reason, the number of finishing passes is preferably less than that necessary to arrive until the point where the needles no longer reach the last layer of the stack. According to another of its aspects, the present invention relates to a fibrous material capable of being used for the implementation of the method. The choice of fibrous material is guided by the intended application, while ensuring that the needled texture lends itself to the densification operation, that is to say has a
porosité ouverte assez importante.fairly large open porosity.
Par exemple, la bande de matériau pourra comprendre au moins une couche formée de fibres seules discontinues, obtenue par cardage ou une couche de fibres continues obtenue par nappage de For example, the strip of material may comprise at least one layer formed of single staple fibers, obtained by carding or a layer of continuous fibers obtained by coating
câbles ou de fils suivi d'un pré-aiguilletage. cables or wires followed by a pre-needling.
Lorsqu'une plus grande tenue mécanique est exigée, on pourra utiliser un complexe constitué d'un tissu (toile ou satin) sur lequel a été aiguilletée une nappe de fibres, un tissu constitué en chaîne et en trame de fils formés de filaments continus ou discontinus, ou encore un tissu constitué en chaîne de fils formés de filaments continus ou discontinus et en trame d'une When greater mechanical strength is required, a complex made of a fabric (canvas or satin) may be used, on which a web of fibers has been needled, a fabric made of warp and weft of threads formed of continuous filaments or discontinuous, or a fabric consisting of a warp of threads formed of continuous or discontinuous filaments and in a weft of
mèche de filature.spinning wick.
Par ailleurs, le matériau doit se prêter à l'aiguilletage, ce qui n'est guère le cas des fibres de carbone ou céramiques entrant dans la composition des matériaux composites utilisés actuellement pour des applications demandant une haute tenue thermomécanique. Dans ce dernier cas, une partie au moins des fibres constitutives du matériau sont des fibres précurseurs de carbone ou de céramiques qui se prêtent bien à l'aiguilletage et qui sont ultérieurement transformées en fibres de carbone ou céramique par Furthermore, the material must be suitable for needling, which is hardly the case for carbon or ceramic fibers used in the composition of the composite materials currently used for applications requiring high thermomechanical strength. In the latter case, at least part of the constituent fibers of the material are carbon or ceramic precursor fibers which lend themselves well to needling and which are subsequently transformed into carbon or ceramic fibers by
traitement de la structure.treatment of the structure.
D'autres particularités et avantages du procédé selon Other features and advantages of the process according to
l'invention ressortiront à la lecture de la description faite ci- the invention will emerge on reading the description given below
après, à titre indicatif, mais non limitatif, en référence aux dessins annexés sur lesquels: - la figure 1 est une vue illustrant, très schématiquement un dispositif pour la mise en oeuvre du procédé selon l'invention, et - les figures 2 à 4 illustrent, en coupe, différents stades de la réalisation d'une structure avec le procédé selon l'invention. Sur un plateau horizontal 10 sont amenées, une par une, des bandes 20 de matériau fibreux de largeur et longueur after, for information, but not limitation, with reference to the accompanying drawings in which: - Figure 1 is a view illustrating, very schematically a device for implementing the method according to the invention, and - Figures 2 to 4 illustrate, in section, different stages in the production of a structure with the method according to the invention. On a horizontal plate 10 are fed, one by one, strips 20 of fibrous material of width and length
déterminées en fonction des dimensions de la structure à réaliser. determined according to the dimensions of the structure to be produced.
Les bandes 20 sont empilées les unes sur les autres et liées entre The strips 20 are stacked on top of each other and linked between
elles par aiguilletage au moyen d'une planche à aiguilles 12. them by needling by means of a needle board 12.
Celle-ci est située au-dessus du plateau 10 et s'étend parallèlement à l'un des côtés du plateau 10, et sur une longueur sensiblement égale à cellede ce côté, avec les aiguilles 13 This is located above the plate 10 and extends parallel to one of the sides of the plate 10, and over a length substantially equal to that of this side, with the needles 13
dirigées verticalement vers le bas. directed vertically downwards.
La planche à aiguilles 12 est solidaire d'un dispositif d'entraînement (non représenté) qui, de façon bien connue en soi, The needle board 12 is integral with a drive device (not shown) which, in a manner well known per se,
communique aux aiguilles un mouvement alternatif vertical. communicates to the hands a vertical reciprocating movement.
La planche à aiguilles 12 et l'empilement de bandes 20 sont mobiles l'un par rapport à l'autre en direction horizontale et en direction verticale. Horizontalement, le plateau 10 est par The needle board 12 and the stack of strips 20 are movable relative to each other in the horizontal direction and in the vertical direction. Horizontally, the plate 10 is by
exemple mobile par rapport à une table support 14, perpendiculai- example movable relative to a support table 14, perpendicular to
rement à la planche 12, sous l'action de moyens d'entratnement(non représentés) montés sur la table 14. Verticalement, le déplacement mutuel du plateau 10 et de la planche 12 est par exemple réalisé par entratnement de la table 14 au moyen de vis sans fin ou autre dispositif d'accouplement avec un moteur (non représenté) fixé au rement to the board 12, under the action of drive means (not shown) mounted on the table 14. Vertically, the mutual displacement of the plate 10 and the board 12 is for example achieved by driving the table 14 by means worm or other coupling device with a motor (not shown) fixed to the
bâti de support de la planche à aiguilles. needle board support frame.
La fabrication d'une structure est réalisée comme suit. The fabrication of a structure is carried out as follows.
Une première bande de matériau est placée sur le plateau , puis une seconde lui est superposée et est aiguilletée sur la premiere, la planche à aiguilles 12 étant animée en permanence d'un mouvement vertical alternatif tandis que le plateau est déplacé horizontalement sur une longueur au moins égale à celle des bandes 20 pour faire défiler cellesci sur toute leur longueur en regard de la planche 12. Lorsque le plateau 10 est parvenu à une extrémité de sa course, une nouvelle bande 20 est empilée sur les précédentes puis la table 14 est descendue d'une distance correspondant à l'épaisseur e d'une bande aiguilletée avant de réaliser une nouvelle passe d'aiguilletage par déplacement du plateau 10 jusqu'à l'autre extrémité de sa course. On procède ainsi en alimentant le plateau 10 en nouvelles bandes à chaque extrémité de sa course horizontale, jusqu'à atteindre la hauteur A first strip of material is placed on the plate, then a second is superimposed on it and is needled on the first, the needle board 12 being continuously driven in an alternating vertical movement while the plate is moved horizontally over a length at less equal to that of the strips 20 to scroll these over their entire length opposite the board 12. When the plate 10 has reached an end of its travel, a new strip 20 is stacked on the previous ones then the table 14 is lowered by a distance corresponding to the thickness e of a needled strip before making a new needling pass by moving the plate 10 to the other end of its travel. This is done by supplying the plate 10 with new strips at each end of its horizontal travel, until reaching the height
désirée pour la structure.desired for structure.
A chaque pénétration des aiguilles, les aspérités (ou barbes) de cellesci entraînent des fibres du matériau des bandes traversées, lesquelles fibres réalisent les liaisons verticales Each penetration of the needles, the roughness (or barbs) of the latter entrain fibers of the material of the crossed bands, which fibers make the vertical connections.
entre les bandes superposées.between the overlapping bands.
Les figures 2 et 3 montrent les aiguilles respectivement en position haute et en position basse. Les aiguilles pénètrent dans la texture sur une profondeur égale à plusieurs fois l'épaisseur d'une bande 20 aiguilletée (par exemple 8 fois). La profondeur d'aiguilletage est maintenue constante pendant toute l'opération du fait de l'abaissement progressif de la structure par rapport aux aiguilles. Afin de pouvoir aiguilleter les premières bandes sur le plateau 10, il est nécessaire de prévoir des moyens permettant d'éviter que les aiguilles 13 viennent buter contre la surface dure du plateau 10. A cet effet, le plateau 10 est recouvert d'un revêtement 11 dans lequel les aiguilles peuvent pénétrer sans être endommagées et sans ramener de particules ou Figures 2 and 3 show the needles respectively in the high position and in the low position. The needles penetrate the texture to a depth equal to several times the thickness of a needled strip (for example 8 times). The needling depth is kept constant throughout the operation due to the gradual lowering of the structure relative to the needles. In order to be able to needle the first strips on the plate 10, it is necessary to provide means making it possible to prevent the needles 13 from abutting against the hard surface of the plate 10. For this purpose, the plate 10 is covered with a coating 11 in which the needles can penetrate without being damaged and without bringing back particles or
fibres au sein de la structure à fabriquer. fibers within the structure to be manufactured.
Le revêtement 11 peut par exemple être constitué d'une feuille 11a d'élastomère armé (par exemple de l'Hypalon" armé d'un tissu de "Nylon") fixée au plateau 10 et sur laquelle est collée une couche llb formée d'un feutre d'embase (par exemple The coating 11 can for example consist of a sheet 11a of reinforced elastomer (for example of Hypalon "reinforced with a" Nylon "fabric) fixed to the plate 10 and on which is glued a layer llb formed of a base felt (for example
2584'1062584'106
feutre de polypropylène) d'épaisseur suffisante pour que les aiguilles, lors de la première passe d'aiguilletage puissent pénétrer sur la profondeur d'aiguilletage prévue sans toucher le plateau 10. Sur le feutre d'embase est collée une autre feuille 11c, par exemple en polychlorure de vinyle. Au cours de l'aiguilletage, la feuille 11c est traversée par les aiguilles mais évite que trop de fibres provenant du matériau des bandes 20 ne s'incrustent dans le feutre d'embase et compliquent polypropylene felt) of sufficient thickness so that the needles, during the first needling pass can penetrate the planned needling depth without touching the plate 10. On the base felt is another sheet 11c, by example in polyvinyl chloride. During needling, the sheet 11c is crossed by the needles but prevents too much fiber from the material of the strips 20 from becoming encrusted in the base felt and complicating
l'enlèvement de la structure terminée. removal of the completed structure.
On notera, en variante, qu'il est possible soit de maintenir le plateau immobile horizontalement et donc de déplacer la planche à aiguilles, soit de réaliser l'aiguilletage sur un plateau perforé avec des perforations correspondant aux aiguilles de la planche 12. Dans ce cas, il n'est pas utile de munir le plateau d'un revêtement de surface tel que le revêtement 11. Le plateau est immobile par rapport à la planche à aiguilles en direction horizontale et c'est donc l'empilement de bandes qui est déplacé horizontalement sur le plateau à chaque passe d'aiguilletage. Afin d'obtenir une densité d'aiguilletage constante dans toute l'épaisseur de la structure, il est nécessaire de procéder à des passes d'aiguilletage de finition après mise en place et aiguilletage de la dernière bande. On procède comme si de nouvelles bandes étaient mises en place. Du fait que les aiguilles traversent alors une certaine distance d dans l'air avant d'atteindre la structure et de parvenir en fin de descente (figure 4), leurs aspérités sont moins bouchées que si elles avaient dû traverser une même distance d à travers le matériau fibreux. Les aiguilles présentent ainsi une agressivité croissante au cours des passes de finition. Pour éviter alors un aiguilletage plus dense dans les couches supérieures, le nombre de passes de finition réalisé (par exemple quatre) est inférieur à celui (huit) qui aurait été nécessaire pour parvenir jusqu'au moment o les It will be noted, as a variant, that it is possible either to keep the plate stationary horizontally and therefore to move the needle board, or to carry out the needling on a perforated plate with perforations corresponding to the needles of the board 12. In this In this case, it is not useful to provide the tray with a surface coating such as the coating 11. The tray is stationary relative to the needle board in the horizontal direction and therefore it is the stacking of strips which is moved horizontally on the table with each needling pass. In order to obtain a constant needling density throughout the thickness of the structure, it is necessary to carry out finishing needling passes after the last strip has been put in place and needled. We proceed as if new bands were put in place. Because the needles then cross a certain distance d in the air before reaching the structure and reaching the end of descent (Figure 4), their roughness is less blocked than if they had to cross the same distance d through the fibrous material. The needles thus exhibit increasing aggressiveness during the finishing passes. To avoid then a more dense needling in the upper layers, the number of finishing passes carried out (for example four) is less than that (eight) which would have been necessary to arrive until the moment when the
aiguilles n'atteignent plus la bande déposée en dernier. needles no longer reach the last deposited strip.
La bande en matériau fibreux peut se présenter sous The strip of fibrous material may be present under
2584 1062584 106
différentes formes, notamment en fonction de l'application envisagée. Ainsi, le matériau fibreux peut être au moins en partie constitué par une couche de fibres discontinues obtenue par cardage (voile de carde), ou par une couche de fibres continues obtenue par croisement de nappes unidirectionnelles de câbles ou fils continus et aiguilletage à faible densité (pré-aiguilletage) des nappes entre elles. Dans ce dernier cas, le croisement pourra être réalisé comme connu en soi par nappage; l'une des nappes de câbles ou fils unidirectionnelles est alimentée en continu tandis qu'une autre nappe de câbles ou fils unidirectionnelle lui est superposée par va-et-vient en direction perpendiculaire au déplacement de la première nappe. Du fait du déplacement relatif entre les nappes unidirectionnelles, on obtient en fait trois nappes superposées formant entre elles des angles différents de different forms, in particular depending on the intended application. Thus, the fibrous material can be at least partially constituted by a layer of staple fibers obtained by carding (carding web), or by a layer of continuous fibers obtained by crossing unidirectional layers of continuous cables or wires and needling at low density. (pre-needling) of the plies together. In the latter case, the crossing may be carried out as known per se by coating; one of the plies of unidirectional cables or wires is supplied continuously while another ply of unidirectional cables or wires is superimposed on it back and forth in a direction perpendicular to the movement of the first ply. Due to the relative displacement between the unidirectional plies, three superimposed plies are in fact obtained, forming between them angles different from
, par exemple environ 60 . , for example about 60.
Lorsqu'une tenue mécanique supérieure est demandée à la structure notamment en fonction des propriétés souhaitées du matériau composite final à fabriquer, le matériau fibreux est constitué par au moins une couche tissée par exemple: - un complexe constitué d'un tissu de fils continus ou discontinus (satin ou toile) sur lequel a été aiguilletée avec une faible densité d'aiguilletage une nappe de fibres discontinues obtenue par cardage (voile de carde) ou une nappe de fibres continues, ces nappes étant déposées sur le tissu par nappage, - un tissu seul constitué en chaîne et en trame de fils formés de filaments continus ou discontinus, ou - un tissu seul constitué en chaîne de fils formés de filaments continus ou discontinus et en trame d'une mèche de When a higher mechanical strength is requested from the structure, in particular as a function of the desired properties of the final composite material to be manufactured, the fibrous material consists of at least one woven layer for example: - a complex consisting of a fabric of continuous threads or discontinuous (satin or fabric) on which a web of staple fibers obtained by carding (carding veil) or a web of continuous fibers has been needled with a low needling density, these plies being deposited on the fabric by coating, - a single fabric consisting of warp and weft of threads formed of continuous or discontinuous filaments, or - a single fabric consisting of warp of threads formed of continuous or discontinuous filaments and weft of a wick of
filature.spinning.
Les fibres constituant les matériaux décrits ci-dessus peuvent être toutes fibres naturelles, artificielles ou synthétiques, organiques ou minérales, telles quelles ou traitées thermiquement, le choix de la nature des fibres dépendant de The fibers constituting the materials described above can be any natural, artificial or synthetic, organic or mineral fiber, as it is or heat treated, the choice of the nature of the fibers depending on
l'application envisagée.the intended application.
S'agissant de la réalisation de structures de renfort pour matériaux composites destinés à supporter des efforts thermomécaniques importants, les fibres les plus intéressantes sont les fibres de carbone et les fibres céramiques (alumine, carbure de silicium,...) ainsi que les fibres précurseurs de ces fibres ou toutes fibres constituant un intermédiaire entre fibres As regards the production of reinforcement structures for composite materials intended to withstand significant thermomechanical forces, the most interesting fibers are carbon fibers and ceramic fibers (alumina, silicon carbide, etc.) as well as the fibers precursors of these fibers or any fibers constituting an intermediate between fibers
précurseurs et les fibres complètement traitées thermiquement. precursors and fibers completely heat treated.
Lorsque la structure tridimensionnelle est réalisée totalement ou en partie à partir de fibres précurseurs ou intermédiaires, elle subit ultérieurement le traitement thermique When the three-dimensional structure is produced wholly or in part from precursor or intermediate fibers, it subsequently undergoes heat treatment
destiné à conférer aux fibres les propriétés mécaniques optimales. intended to give fibers the optimal mechanical properties.
Cette dernière façon de procéder permet de ne pas briser les fibres lors de l'aiguilletage dans le cas o les fibres traitées thermiquement ont des modules trop élevés et des résistances transversales trop faibles pour être aiguilletées sans This last way of proceeding makes it possible not to break the fibers during needling in the case where the heat treated fibers have too high moduli and too low transverse resistances to be needled without
dommage, comme c'est le cas des fibres carbone et céramiques. damage, as is the case with carbon and ceramic fibers.
Ainsi, les matériaux décrits plus haut pourront être constitués au moins en partie avec des fibres précurseurs de carbone ou de céramique, le reste éventuel des fibres étant en carbone ou en Thus, the materials described above can be made at least in part with carbon or ceramic precursor fibers, the possible remainder of the fibers being carbon or
céramique.ceramic.
Par exemple, le matériau fibreux destiné à l'aiguilletage est constitué par un complexe formé d'un tissu de fibres de carbone haute résistance pré-aiguilleté avec un voile de carde de fibres de P.A.N. (polyacrylonitryle, précurseur du carbone) stabilisé. Dans ce complexe, le tissu apporte la tenue mécanique désirée tandis que la nappe de fibres autorise un aiguilletage non destructeur des bandes superposées car les barbes des aiguilles, se couvrant de P.A.N. stabilisé, ne blessent pas gravement les fibres de carbone. Par souci d'économie, le tissu sera choisi le plus léger possible compte-tenu des propriétés mécaniques désirées, par exemple avec une masse surfacique comprise entre 100 For example, the fibrous material intended for needling consists of a complex formed from a fabric of high-strength carbon fibers pre-needled with a veil of carding fibers from P.A.N. (polyacrylonitryl, carbon precursor) stabilized. In this complex, the fabric provides the desired mechanical strength while the fiber web allows non-destructive needling of the superimposed bands because the barbs of the needles, covering themselves with P.A.N. stabilized, do not seriously injure carbon fibers. For the sake of economy, the fabric will be chosen as light as possible, taking into account the desired mechanical properties, for example with a surface mass of between 100
et 600 g/m2.and 600 g / m2.
Dans l'exemple précédent, on pourra bien entendu remplacer indépendamment fibres et/ou précurseurs de carbone par fibres et/ou précurseurs de céramique. Et, inversement, un tissu en fibres précurseurs de carbone ou céramique peut être combiné avec In the previous example, it is of course possible to independently replace fibers and / or carbon precursors with fibers and / or ceramic precursors. And, conversely, a fabric of carbon or ceramic precursor fibers can be combined with
un voile de carde en fibres carbone ou céramique. a carbon or ceramic fiber card veil.
De la même manière, fibres de carbone ou céramique et fibres précurseurs de carbone ou céramique peuvent être combinées en formant indépendamment l'une de l'autre la chaîne et la trame d'un tissu constitué, en chaîne, de fils de filaments continus ou discontinus et, en trame, d'une mèche de filature ou de fils de Likewise, carbon or ceramic fibers and carbon or ceramic precursor fibers can be combined by forming, independently of each other, the warp and the weft of a fabric made up, in warp, of continuous filament yarns or discontinuous and, in the weft, of a spinning wick or
filaments continus ou discontinus.continuous or discontinuous filaments.
Claims (13)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8509820A FR2584106B1 (en) | 1985-06-27 | 1985-06-27 | METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS |
DE3620611A DE3620611C2 (en) | 1985-06-27 | 1986-06-20 | Process for the production of three-dimensional, fibrous laminates and suitable fiber materials |
US06/877,254 US4790052A (en) | 1983-12-28 | 1986-06-23 | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
IT20881/86A IT1204405B (en) | 1985-06-27 | 1986-06-23 | PROCESS OF MANUFACTURING OF THREE-DIMENSIONAL STRUCTURES BY SEWING LAYERS OF FLAT LAYERS OF FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCEDURE |
GB8615602A GB2177345B (en) | 1985-06-27 | 1986-06-26 | Process for manufacturing three-dimensional structures of fibrous material |
JP61149880A JPH0759782B2 (en) | 1985-06-27 | 1986-06-27 | Method for stacking and puncturing flat layers of fibrous material to produce a three-dimensional structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8509820A FR2584106B1 (en) | 1985-06-27 | 1985-06-27 | METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2584106A1 true FR2584106A1 (en) | 1987-01-02 |
FR2584106B1 FR2584106B1 (en) | 1988-05-13 |
Family
ID=9320736
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8509820A Expired FR2584106B1 (en) | 1983-12-28 | 1985-06-27 | METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPH0759782B2 (en) |
DE (1) | DE3620611C2 (en) |
FR (1) | FR2584106B1 (en) |
GB (1) | GB2177345B (en) |
IT (1) | IT1204405B (en) |
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DE4139848A1 (en) * | 1990-12-03 | 1992-06-04 | Europ Propulsion | METHOD FOR PRODUCING A FIBROUS PREFORM WITH EXTENDABLE THICKNESS FOR PRODUCING A WORKPIECE FROM COMPOSITE TYPE OF A CARBON OR CERAMIC MATRIX |
DE4139714A1 (en) * | 1990-12-03 | 1992-06-04 | Europ Propulsion | DEVICE FOR THE PRODUCTION OF FIBROUS, NEEDLEED PREFORMS FOR THE PRODUCTION OF WORKPIECES FROM COMPOSITE MATERIAL |
WO1995011869A1 (en) * | 1993-10-27 | 1995-05-04 | Societe Europeenne De Propulsion | Chemical vapour infiltration process of a material within a fibrous substrate with creation of a temperature gradient in the latter |
US5490892A (en) * | 1993-02-17 | 1996-02-13 | Societe Europeenne De Propulsion | Method of fabricating a composite material part, in particular a sandwich panel, from a plurality of assembled-together preforms |
WO1996037646A1 (en) * | 1995-05-24 | 1996-11-28 | Societe Europeenne De Propulsion | Hybrid yarn for the fabrication of fibre preforms of composite parts, and method for its preparation |
FR2738303A1 (en) * | 1995-08-30 | 1997-03-07 | Europ Propulsion | TURBINE OF THERMOSTRUCTURAL COMPOSITE MATERIAL, ESPECIALLY A SMALL DIAMETER, AND PROCESS FOR PRODUCING THE SAME |
FR2738304A1 (en) * | 1995-08-30 | 1997-03-07 | Europ Propulsion | TURBINE OF THERMOSTRUCTURAL COMPOSITE MATERIAL, IN PARTICULAR A LARGE DIAMETER, AND PROCESS FOR MANUFACTURING THE SAME |
EP1424423A3 (en) * | 1994-07-25 | 2007-11-28 | Goodrich Corporation | An improved process for forming fibrous preform structures |
WO2012143658A1 (en) | 2011-04-19 | 2012-10-26 | Snecma Propulsion Solide | Process for preparing a monolithic catalysis element comprising a fibrous support and said monolithic catalysis element |
US10589474B2 (en) | 2011-01-12 | 2020-03-17 | Compagnie Chomarat | Methods for manufacturing sublaminate modules and forming composite laminated structures from the same |
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US5882781A (en) * | 1986-01-28 | 1999-03-16 | Aerospace Preforms Limited | Shaped fibrous fabric structure comprising multiple layers of fibrous material |
US5388320A (en) | 1987-01-27 | 1995-02-14 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5705264A (en) * | 1987-01-27 | 1998-01-06 | Aerpspace Preforms Limited | Production of shaped filamentary structures |
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JPH0713344B2 (en) * | 1989-08-28 | 1995-02-15 | 東レ株式会社 | Method for manufacturing sheet material |
EP0546001B2 (en) * | 1990-08-31 | 2003-08-20 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5846611A (en) * | 1993-10-27 | 1998-12-08 | Societe Europeene De Propulsion | Chemical vapor infiltration process of a material within a fibrous substrate with creation of a temperature gradient in the latter |
DE4343271A1 (en) * | 1993-12-17 | 1995-06-22 | Jacob Emendoerfer Nachf Baur V | Strong, low density multilayer fibre, esp. wool, fleece strip |
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EP0842038B2 (en) * | 1995-07-28 | 2004-11-03 | SAERTEX Wagener GmbH & Co. KG | Method of producing a reinforcement for thermoplastic and thermosetting matrices |
JP2004060058A (en) * | 2002-07-24 | 2004-02-26 | Mitsubishi Heavy Ind Ltd | Fiber substrate for composite material |
WO2003013817A1 (en) * | 2001-08-02 | 2003-02-20 | Mitsubishi Heavy Industries, Ltd. | Composite material-use fiber base material |
JP2003039429A (en) * | 2001-08-02 | 2003-02-13 | Mitsubishi Heavy Ind Ltd | Fiber base for composite material |
FR2858318B1 (en) * | 2003-07-31 | 2007-03-02 | Snecma Propulsion Solide | PROTECTION AGAINST OXIDATION OF COMPOSITE MATERIALS CONTAINING CARBON AND PARTS THUS PROTECTED |
JP7287162B2 (en) | 2019-07-19 | 2023-06-06 | 株式会社豊田自動織機 | Fiber structures and fiber reinforced composites |
CN111676598A (en) * | 2020-06-24 | 2020-09-18 | 浙江星辉新材料科技股份有限公司 | Flat prefabricated body needle loom of carbon fiber |
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DE4139714A1 (en) * | 1990-12-03 | 1992-06-04 | Europ Propulsion | DEVICE FOR THE PRODUCTION OF FIBROUS, NEEDLEED PREFORMS FOR THE PRODUCTION OF WORKPIECES FROM COMPOSITE MATERIAL |
DE4139714C2 (en) * | 1990-12-03 | 2000-10-26 | Const De Moteurs D Aviat Paris | Device for the production of fiber-containing needled preforms for the production of workpieces from a composite material |
DE4139848A1 (en) * | 1990-12-03 | 1992-06-04 | Europ Propulsion | METHOD FOR PRODUCING A FIBROUS PREFORM WITH EXTENDABLE THICKNESS FOR PRODUCING A WORKPIECE FROM COMPOSITE TYPE OF A CARBON OR CERAMIC MATRIX |
DE4139848C2 (en) * | 1990-12-03 | 1998-02-19 | Europ Propulsion | Method for producing a fibrous preform with an expandable thickness for producing a workpiece from a composite material of the carbon or ceramic matrix type |
US5490892A (en) * | 1993-02-17 | 1996-02-13 | Societe Europeenne De Propulsion | Method of fabricating a composite material part, in particular a sandwich panel, from a plurality of assembled-together preforms |
WO1995011869A1 (en) * | 1993-10-27 | 1995-05-04 | Societe Europeenne De Propulsion | Chemical vapour infiltration process of a material within a fibrous substrate with creation of a temperature gradient in the latter |
FR2711645A1 (en) * | 1993-10-27 | 1995-05-05 | Europ Propulsion | Method of chemical vapor infiltration of a material within a fibrous substrate with establishment of a temperature gradient therein. |
EP1424423A3 (en) * | 1994-07-25 | 2007-11-28 | Goodrich Corporation | An improved process for forming fibrous preform structures |
US6051313A (en) * | 1995-05-24 | 2000-04-18 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Hybrid yarn for the fabrication of fibre preforms of composite parts, and method for its preparation |
WO1996037646A1 (en) * | 1995-05-24 | 1996-11-28 | Societe Europeenne De Propulsion | Hybrid yarn for the fabrication of fibre preforms of composite parts, and method for its preparation |
FR2734581A1 (en) * | 1995-05-24 | 1996-11-29 | Europ Propulsion | HYBRID WIRE FOR THE MANUFACTURE OF FIBROUS PREFORMS OF COMPOSITE MATERIAL PIECES AND PROCESS FOR PREPARING THE SAME |
US6228786B1 (en) | 1995-05-24 | 2001-05-08 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Hybrid yard for the fabrication of fiber preforms of composite parts, and method for its preparation |
EP0761978A1 (en) * | 1995-08-30 | 1997-03-12 | Societe Europeenne De Propulsion | Thermostructural composite material rotor, particularly of large diameter and its method of manufacturing |
US5845398A (en) * | 1995-08-30 | 1998-12-08 | Societe Europeenne De Propulsion | Turbine of thermostructural composite material, in particular a turbine of large diameter, and a method of manufacturing it |
US5944485A (en) * | 1995-08-30 | 1999-08-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Turbine of thermostructural composite material, in particular a turbine of large diameter, and a method of manufacturing it |
US6029347A (en) * | 1995-08-30 | 2000-02-29 | Societe Europenne De Propulsion | Method of manufacturing a turbine of thermostructural composite material, in particular of small diameter |
US5775878A (en) * | 1995-08-30 | 1998-07-07 | Societe Europeene De Propulsion | Turbine of thermostructural composite material, in particular of small diameter, and a method of manufacturing it |
EP0761977A1 (en) * | 1995-08-30 | 1997-03-12 | Societe Europeenne De Propulsion | High temperature composite material impellor, particularly of small diameter, and its manufacturing method |
FR2738304A1 (en) * | 1995-08-30 | 1997-03-07 | Europ Propulsion | TURBINE OF THERMOSTRUCTURAL COMPOSITE MATERIAL, IN PARTICULAR A LARGE DIAMETER, AND PROCESS FOR MANUFACTURING THE SAME |
FR2738303A1 (en) * | 1995-08-30 | 1997-03-07 | Europ Propulsion | TURBINE OF THERMOSTRUCTURAL COMPOSITE MATERIAL, ESPECIALLY A SMALL DIAMETER, AND PROCESS FOR PRODUCING THE SAME |
US10589474B2 (en) | 2011-01-12 | 2020-03-17 | Compagnie Chomarat | Methods for manufacturing sublaminate modules and forming composite laminated structures from the same |
WO2012143658A1 (en) | 2011-04-19 | 2012-10-26 | Snecma Propulsion Solide | Process for preparing a monolithic catalysis element comprising a fibrous support and said monolithic catalysis element |
Also Published As
Publication number | Publication date |
---|---|
GB2177345A (en) | 1987-01-21 |
GB8615602D0 (en) | 1986-07-30 |
FR2584106B1 (en) | 1988-05-13 |
JPS626956A (en) | 1987-01-13 |
IT1204405B (en) | 1989-03-01 |
JPH0759782B2 (en) | 1995-06-28 |
IT8620881A0 (en) | 1986-06-23 |
DE3620611A1 (en) | 1987-01-08 |
DE3620611C2 (en) | 1997-09-25 |
GB2177345B (en) | 1989-07-12 |
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