EP3372718A1 - Method for manufacturing a needled fibrous structure - Google Patents
Method for manufacturing a needled fibrous structure Download PDFInfo
- Publication number
- EP3372718A1 EP3372718A1 EP18159859.0A EP18159859A EP3372718A1 EP 3372718 A1 EP3372718 A1 EP 3372718A1 EP 18159859 A EP18159859 A EP 18159859A EP 3372718 A1 EP3372718 A1 EP 3372718A1
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- EP
- European Patent Office
- Prior art keywords
- needling
- support
- fibrous
- relative
- head
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 12
- 238000006073 displacement reaction Methods 0.000 claims description 17
- 239000002131 composite material Substances 0.000 claims description 8
- 239000000835 fiber Substances 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 6
- 230000002787 reinforcement Effects 0.000 claims description 4
- 239000011159 matrix material Substances 0.000 claims description 3
- 239000004753 textile Substances 0.000 description 3
- 238000000280 densification Methods 0.000 description 2
- 238000010008 shearing Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000287107 Passer Species 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000000306 recurrent effect Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
Images
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
- 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
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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
- D04H18/00—Needling machines
- D04H18/02—Needling machines with needles
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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
- D04H3/105—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 needling
Definitions
- the present invention relates to the general field of processes for manufacturing needled fibrous structures, which can be used for the manufacture of parts made of composite material.
- needling machines are known that can be used to produce needle-punched textile structures.
- a first plane-type machine needling fibrous layers stacked on a table, the table moving in horizontal translation in front of a vertically movable needling head.
- the needling is made of a continuous fibrous layer wound around a rotating mandrel.
- the mandrel has a surface of revolution around which the layer is wound, the layer being located in front of a needling head movable in a direction perpendicular to this surface.
- the fibrous structures obtained obtained have areas of weakness. These areas of weakness are mainly due to recurrent needling on the same area between two consecutive fibrous layers.
- the needling head moves along the fibrous layer to needling (for example by translation of the table or rotation of the mandrel)
- the successive passages of the head between two layers can produce holes aligned in the direction scrolling of the layer (phenomenon called "lineage").
- lineage phenomenon called "lineage"
- the process according to the invention makes it possible to reduce the risk that needles of the needling head may need to point twice the same place between two successive fibrous layers.
- the method according to the invention makes it possible to prevent the formation of needled hole lines ("lineage" phenomenon) between two successive layers and to reduce the problems of fragility caused by them.
- the composite material parts resulting from the subsequent densification of a needled fibrous structure obtained by a method according to the invention thus have improved mechanical strength.
- the support may be a rotary table or mandrel about an axis of rotation.
- the needling head may, during a needling step, move in translation perpendicular to the surface of the table with a vertical movement alternative.
- the table can move in translation in front of the needling head to needle a fibrous layer of larger size than that of the needling head.
- the needling head may, during a needling step, move perpendicularly to the surface of the mandrel with a vertical reciprocating movement, that is to say in a radial direction by relative to the axis of rotation of the mandrel.
- the support may advantageously be a table, mobile or otherwise in translation in front of the needling head.
- the relative displacement of the support relative to the needling head may comprise a relative rotation of the support relative to the needling head.
- the relative rotation of the support relative to the needling head may be a rotation of the support along an axis perpendicular to a surface of the support.
- the support can rotate at a non-zero angle less than or equal to 5 °, for example less than or equal to 2 °.
- a range of angles reduced in this way avoids the presence of so-called “dead zones" where the fibrous layers are not needled.
- the support may advantageously be a mandrel rotating around an axis of rotation and on which a fibrous structure may be wound, a layer of fibrous structure for example making a turn around the mandrel.
- the relative displacement of the support relative to the needling head may comprise a relative translation of the support relative to the needling head.
- the support of the needling machine may be rotatable about an axis of rotation, the relative displacement of the support relative to the needling head then being a relative translation of the needling head relative to the support in a direction parallel to the axis of rotation of the support.
- the needling head or the support can be translated from a non-zero distance of less than or equal to 30 mm, for example less than or equal to 15 mm, in particular to reduce the presence of dead zones in needled layers.
- a plane-type needling machine 100 which comprises a needling head 110 and a support constituted by a table 120.
- the needling head 110 carries a determined number of needles 111 which are provided with barbs, hooks or forks to take fibers from the fibrous layers and transfer them through them as they penetrate them. In a manner known per se, these needles 111 can be arranged in several rows of needles 111.
- the needling head 110 can move vertically, that is to say in the direction Z indicated in the figures, above of the table 120.
- the needling head 110 can in particular move up and down and upwards in the vertical direction Z with a vertical reciprocating movement relative to the table 120, as illustrated by the double arrow 112.
- the table 120 extends in turn in horizontal directions X and Y perpendicular to the direction Z.
- the table 120 is here mounted on a pole 130 movable in translation in a rail 140 extending along the direction X, so that the table 120 can be moved in rectilinear translation according to the X direction in front of the needling head 110 (double arrow 131).
- the needling head 110 can not move in the X and Y directions.
- the table 120 is rotatable about an axis A, parallel to the axis Z, and perpendicular to the surface 121 of the table on which the needling fibrous layers will be made. Note that, in an equivalent variant not shown, the table 120 may be fixed in the X direction, while the needling head 110 may be movable in translation in the X direction.
- a first fibrous layer 10 is disposed and held on the table 120.
- the fibrous layer 10 has been needled by the needling head 110, for example by making a round trip to the needling head 110 by moving the table 120 in the rail 140.
- the needling head 110 is driven in a movement along the double arrow 112.
- the needles 111 then enter the fibrous layer or layers present on the table for fibers interpenetrating the different fibrous layers in the direction Z.
- the displacement of the table 120 in front of the head 110 may, during the needling, be carried out step by step, that is to say with an alternation of phases of displacement and stopping phases, the needling being performed by the head 120 during the stopping phases. This advantageously makes it possible to reduce the shearing of the fibrous layer during needling and to further improve the mechanical properties of the part.
- the Figure 1B shows a top view of the first fibrous layer 10 on the table 120, as well as holes 11 corresponding to the location where the needles are retracted into the first fibrous layer 10 during its needling.
- the needles 111 are distributed uniformly over a surface of the needling head 110.
- the needling head 110 is in a first position compared to table 120, illustrated on the Figures 1A, 1B and 2 . This first position is defined here in particular by the orientation of the table 120 relative to the needling head 110.
- a second fibrous layer 20 is positioned on the first fibrous layer 10 which has already been needled.
- the edges of the two fibrous layers 10 and 20 are aligned on the table 120.
- the second layer 20 may be arranged in a different manner on the first layer 10.
- a step of relative displacement of the table 120 (on which the two fibrous layers 10 and 20 are present) relative to the needling head 110 is carried out.
- this step corresponds to a rotation of the table 120 around its axis of rotation A of an angle a, the needling head 110 being here fixed horizontally.
- the angle ⁇ may be less than or equal to 5 ° (that is to say between -5 ° and 5 ° relative to the first position), or even less than or equal to 2 ° (i.e. say between -2 ° and 2 ° relative to the first position), in order to limit the size of the dead zones, that is to say not needled, in the fibrous layers.
- ⁇ is not equal to 0.
- the needling head 110 is thus in a second position, different from the first position.
- the second fibrous layer 20 is needled, the needling head 110 being in the second position at least at the beginning of the needling of the second layer 20.
- the needling of the second fibrous layer 20 may be performed identically to the needling of the first fibrous layer 10.
- the table 120 may also move in front of the needling head 110 in the X direction and can go back and forth to whet all the second layer 20.
- the first position of the table 120 can be seen in dotted lines, and the second position of the table 120 in a solid line.
- the position of the holes 11 made in the first layer 10 during the needling of the first layer is also seen. 10, and the position of the holes 21 made during the needling of the second layer 20. It is thus observed that the needles do not hit the layers 10 and 20 in the same place, which reduces the formation of areas of fragility within the resulting fibrous structure resulting in particular preventing lineage phenomenon.
- FIGS. 4A to 5B illustrate the steps of a method according to a second embodiment of the invention.
- a needling machine 200 of the circular type which comprises a needling head 210 provided with needles 211 and a support here constituted by a mandrel 220 around which a fibrous structure 30 is intended to be wound .
- the mandrel 220 is rotatable about an axis B.
- the needling head 210 can move, during the needling, in a direction Z perpendicular to the surface of the mandrel, this direction also corresponding to a radial direction relative to to the axis B of the mandrel 220.
- the mandrel 220 is only rotatable about the axis B, and the needling head 210 is movable in translation only in the directions X and Z.
- the fibrous structure May be in the form of a fibrous web stored on a mandrel 230.
- the wound portion forms a first fibrous layer 31 on the mandrel 220.
- the portion that covers the first layer 31 forms a second fibrous layer 32 on the mandrel 220.
- the mandrel 220 is rotated progressively (arrow 221) to scroll the first layer 31 in front of the needling head 210.
- the needling head 210 is animated a movement according to the double arrow 212 to needle the entire first layer 31.
- the needling head 210 is in a first position relative to the mandrel 220 This first position is defined here in particular by the position along the axis X of the needling head 210 with respect to the mandrel 220.
- the movement of the fibrous structure 30 in front of the needling head 210 can be achieved step by step, in particular to reduce the shearing of the fibrous layer during needling.
- Figure 4B shows a view of the first layer 31 at the beginning of its needling and the position of the holes 31a resulting therefrom.
- the relative displacement step of the mandrel 220 (on which the two fibrous layers 31 and 32 are present) is carried out with respect to the needling head 210.
- this step corresponds to a translation of the head of needling 210 of a distance ⁇ X in the X direction parallel to the axis of rotation B of the mandrel.
- the distance ⁇ X may be less than or equal to 30 mm (that is to say that the displacement may be between -30mm and + 30mm relative to the first position), or even less than or equal to 15mm (that is, that is to say between -15mm and + 15mm relative to the first position), in order to limit the size of the dead zones, that is to say not needled, in the fibrous layers.
- ⁇ X is not equal to 0.
- the needling head 210 is thus in a second position, different from the first position.
- the second fibrous layer 32 is needled, the needling head 210 being in the second position at least at the beginning of the needling of the second fibrous layer 32.
- the needling of the second fibrous layer 32 may be performed identically to the needling of the first fibrous layer 31.
- the mandrel 220 can rotate around the axis B so as to scroll the second layer 32 in front of the needling head 210 which is moved back and forth in the direction Z.
- the first position of the head 210 can be seen in dashed lines, and the second position of the head 210 in solid lines.
- the position of the holes 31a made in the first layer 31 during the needling of the first layer is also seen. 31, and the position of the holes 32a made during the needling of the second layer 32. It is thus observed that the needles do not hit the layers 31 and 32 in the same place, which reduces the formation of areas of fragility within the resulting fibrous structure resulting in particular preventing lineage phenomenon.
- the steps of relative movement of the support relative to the needling head correspond to particular movements of the support or the head. , for example a translation or a rotation, particularly adapted to the machine in question.
- the step of relative displacement of the support relative to the needling head successively comprises several types of movements, for example a translation followed by a rotation or vice versa.
- a fibrous layer may for example comprise a unidirectional fiber web, or a textile web having a two-dimensional weave.
- the fibers of the fibrous layer may be fibers of a refractory material such as carbon, or ceramic fibers, for example silicon carbide or glass.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Nonwoven Fabrics (AREA)
- Laminated Bodies (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
Abstract
L'invention concerne un procédé de fabrication d'une structure fibreuse aiguilletée à l'aide d'une machine d'aiguilletage (100) munie d'une tête d'aiguilletage (110), le procédé comprenant au moins les étapes suivantes : le placement d'une première couche fibreuse (10) sur un support (120) ; l'aiguilletage de la première couche, la tête d'aiguilletage étant dans une première position par rapport au support ; le déplacement relatif du support par rapport à la tête d'aiguilletage, réalisé après l'aiguilletage de la première couche, de façon à faire passer la tête d'aiguilletage dans une deuxième position, différente de la première, par rapport au support ; le placement d'une deuxième couche fibreuse (20) sur la première couche; et l'aiguilletage de la deuxième couche fibreuse placée sur la première couche, la tête d'aiguilletage étant dans la deuxième position par rapport au support au début de l'aiguilletage de la deuxième couche.The invention relates to a method of manufacturing a needled fibrous structure using a needling machine (100) provided with a needling head (110), the method comprising at least the following steps: placing a first fibrous layer (10) on a support (120); needling the first layer, the needling head being in a first position relative to the support; relative movement of the support relative to the needling head, made after needling the first layer, so as to pass the needling head in a second position, different from the first, relative to the support; placing a second fibrous layer (20) on the first layer; and the needling of the second fibrous layer placed on the first layer, the needling head being in the second position relative to the support at the beginning of the needling of the second layer.
Description
La présente invention se rapporte au domaine général des procédés de fabrication de structures fibreuses aiguilletées, susceptibles d'être utilisées pour la fabrication de pièces en matériau composite.The present invention relates to the general field of processes for manufacturing needled fibrous structures, which can be used for the manufacture of parts made of composite material.
On connaît plusieurs types de machines d'aiguilletage utilisables pour réaliser des structures textiles aiguilletées. Dans une première machine de type plan, on réalise l'aiguilletage de couches fibreuses empilées sur une table, la table se déplaçant en translation horizontale devant une tête d'aiguilletage mobile verticalement. Dans une deuxième machine de type circulaire, on réalise l'aiguilletage d'une couche fibreuse continue enroulée autour d'un mandrin rotatif. Le mandrin présente une surface de révolution autour de laquelle est enroulée la couche, la couche étant située en face d'une tête d'aiguilletage mobile selon une direction perpendiculaire à cette surface.Several types of needling machines are known that can be used to produce needle-punched textile structures. In a first plane-type machine, needling fibrous layers stacked on a table, the table moving in horizontal translation in front of a vertically movable needling head. In a second machine of the circular type, the needling is made of a continuous fibrous layer wound around a rotating mandrel. The mandrel has a surface of revolution around which the layer is wound, the layer being located in front of a needling head movable in a direction perpendicular to this surface.
En utilisant l'une ou l'autre de ces machines pour aiguilleter plusieurs couches fibreuses superposées, on observe que les structures fibreuses aiguilletées obtenues présentent des zones de fragilité. Ces zones de fragilité sont principalement dues à un aiguilletage récurrent sur une même zone entre deux couches fibreuses consécutives. En particulier, lorsque la tête d'aiguilletage se déplace le long de la couche fibreuse à aiguilleter (par exemple par translation de la table ou rotation du mandrin), les passages successifs de la tête entre deux couches peuvent produire des trous alignés selon la direction de défilement de la couche (phénomène dit de « lignage »). Ces alignements de trous au sein d'une même couche et entre les différentes couches peuvent conduire à la rupture prématurée de la structure fibreuse aiguilletée le long de ces lignes de trous. Par suite, on observe que les pièces en matériau composite résultant de la densification de ces structures fibreuses aiguilletées sont également sujettes à des problèmes de tenue mécanique, ce qui n'est pas souhaitable.By using one or the other of these machines to needle several superimposed fibrous layers, it is observed that the fibrous structures obtained obtained have areas of weakness. These areas of weakness are mainly due to recurrent needling on the same area between two consecutive fibrous layers. In particular, when the needling head moves along the fibrous layer to needling (for example by translation of the table or rotation of the mandrel), the successive passages of the head between two layers can produce holes aligned in the direction scrolling of the layer (phenomenon called "lineage"). These alignments of holes within the same layer and between the different layers can lead to premature failure of the fibrous structure needled along these lines of holes. As a result, it is observed that the composite material parts resulting from the densification of these fibrous needled structures are also subject to mechanical strength problems, which is undesirable.
Il existe donc un besoin pour un procédé de fabrication d'une structure textile aiguilletée sur une machine d'aiguilletage de type plan ou circulaire, qui ne présente pas les inconvénients précités.There is therefore a need for a method of manufacturing a needle-punched textile structure on a planar or circular needling machine, which does not have the aforementioned drawbacks.
La présente invention a donc pour but principal de pallier de tels inconvénients en proposant un procédé de fabrication d'une structure fibreuse aiguilletée à l'aide d'une machine d'aiguilletage munie d'une tête d'aiguilletage, le procédé comprenant au moins les étapes suivantes :
- le placement d'une première couche fibreuse sur un support,
- l'aiguilletage de la première couche fibreuse, la tête d'aiguilletage étant dans une première position par rapport au support au moins à la fin de l'aiguilletage de la première couche,
- le déplacement relatif du support par rapport à la tête d'aiguilletage, réalisé après l'aiguilletage de la première couche, de façon à faire passer la tête d'aiguilletage de la première position à une deuxième position, différente de la première, par rapport au support,
- le placement d'une deuxième couche fibreuse sur la première couche fibreuse aiguilletée, et
- l'aiguilletage de la deuxième couche fibreuse placée sur la première couche fibreuse, la tête d'aiguilletage étant dans la deuxième position par rapport au support au moins au début de l'aiguilletage de la deuxième couche fibreuse.
- placing a first fibrous layer on a support,
- needling the first fibrous layer, the needling head being in a first position relative to the support at least at the end of the needling of the first layer,
- the relative displacement of the support with respect to the needling head, made after the needling of the first layer, so as to pass the needling head of the first position to a second position, different from the first, relative to the support,
- placing a second fibrous layer on the first needled fibrous layer, and
- the needling of the second fibrous layer placed on the first fibrous layer, the needling head being in the second position relative to the support at least at the beginning of the needling of the second fibrous layer.
Le procédé selon l'invention permet de réduire le risque que les aiguilles de la tête d'aiguilletage ne viennent aiguilleter deux fois le même endroit entre deux couches fibreuses successives. En effet, l'étape de déplacement relatif du support par rapport à la tête d'aiguilletage, correspondant à un décalage relatif de ces éléments l'un par rapport à l'autre, permet d'éviter que les aiguilles ne frappent globalement au même endroit entre deux couches successives. En particulier, le procédé selon l'invention permet d'empêcher la formation de lignes de trous aiguilletés (phénomène de « lignage ») entre deux couches successives et de réduire les problèmes de fragilité occasionnés par ces dernières. Les pièces en matériau composite résultant de la densification ultérieure d'une structure fibreuse aiguilletée obtenue par un procédé selon l'invention présentent ainsi une tenue mécanique améliorée.The process according to the invention makes it possible to reduce the risk that needles of the needling head may need to point twice the same place between two successive fibrous layers. Indeed, the step of relative displacement of the support relative to the needling head, corresponding to a relative offset of these elements relative to each other, prevents the needles hit globally to the same place between two successive layers. In particular, the method according to the invention makes it possible to prevent the formation of needled hole lines ("lineage" phenomenon) between two successive layers and to reduce the problems of fragility caused by them. The composite material parts resulting from the subsequent densification of a needled fibrous structure obtained by a method according to the invention thus have improved mechanical strength.
Le support peut être une table ou un mandrin rotatif autour d'un axe de rotation. Quand le support est une table, la tête d'aiguilletage peut, lors d'une étape d'aiguilletage, se déplacer en translation perpendiculairement à la surface de la table avec un mouvement vertical alternatif. En outre, la table peut se déplacer en translation devant la tête d'aiguilletage afin d'aiguilleter une couche fibreuse de taille plus importante que celle de la tête d'aiguilletage. Quand le support est un mandrin rotatif, la tête d'aiguilletage peut, lors d'une étape d'aiguilletage, se déplacer perpendiculairement à la surface du mandrin avec un mouvement vertical alternatif, c'est-à-dire selon une direction radiale par rapport à l'axe de rotation du mandrin.The support may be a rotary table or mandrel about an axis of rotation. When the support is a table, the needling head may, during a needling step, move in translation perpendicular to the surface of the table with a vertical movement alternative. In addition, the table can move in translation in front of the needling head to needle a fibrous layer of larger size than that of the needling head. When the support is a rotating mandrel, the needling head may, during a needling step, move perpendicularly to the surface of the mandrel with a vertical reciprocating movement, that is to say in a radial direction by relative to the axis of rotation of the mandrel.
Dans les exemples de réalisation qui suivent, le support peut être avantageusement une table, mobile ou non en translation devant la tête d'aiguilletage.In the following exemplary embodiments, the support may advantageously be a table, mobile or otherwise in translation in front of the needling head.
Dans un exemple de réalisation, le déplacement relatif du support par rapport à la tête d'aiguilletage peut comprendre une rotation relative du support par rapport à la tête d'aiguilletage.In an exemplary embodiment, the relative displacement of the support relative to the needling head may comprise a relative rotation of the support relative to the needling head.
En particulier, la rotation relative du support par rapport à la tête d'aiguilletage peut être une rotation du support selon un axe perpendiculaire à une surface du support.In particular, the relative rotation of the support relative to the needling head may be a rotation of the support along an axis perpendicular to a surface of the support.
Dans un exemple de réalisation, le support peut effectuer une rotation d'un angle non nul inférieur ou égal à 5°, par exemple inférieur ou égal à 2°. Une plage d'angles réduite de la sorte permet d'éviter la présence de zones dites « mortes » où les couches fibreuses ne seraient pas aiguilletées.In an exemplary embodiment, the support can rotate at a non-zero angle less than or equal to 5 °, for example less than or equal to 2 °. A range of angles reduced in this way avoids the presence of so-called "dead zones" where the fibrous layers are not needled.
Dans les exemples de réalisation qui suivent, le support peut être avantageusement un mandrin rotatif autour d'un axe de rotation et sur lequel on peut enrouler une structure fibreuse, une couche de structure fibreuse faisant par exemple un tour autour du mandrin.In the following exemplary embodiments, the support may advantageously be a mandrel rotating around an axis of rotation and on which a fibrous structure may be wound, a layer of fibrous structure for example making a turn around the mandrel.
Dans un exemple de réalisation, le déplacement relatif du support par rapport à la tête d'aiguilletage peut comprendre une translation relative du support par rapport à la tête d'aiguilletage.In an exemplary embodiment, the relative displacement of the support relative to the needling head may comprise a relative translation of the support relative to the needling head.
En particulier, le support de la machine d'aiguilletage peut être rotatif autour d'un axe de rotation, le déplacement relatif du support par rapport à la tête d'aiguilletage étant alors une translation relative de la tête d'aiguilletage par rapport au support selon une direction parallèle à l'axe de rotation du support.In particular, the support of the needling machine may be rotatable about an axis of rotation, the relative displacement of the support relative to the needling head then being a relative translation of the needling head relative to the support in a direction parallel to the axis of rotation of the support.
Dans un exemple de réalisation, la tête d'aiguilletage ou le support peut être translaté d'une distance non nulle inférieure ou égale à 30 mm, par exemple inférieure ou égale à 15 mm, afin notamment de réduire la présence de zones mortes dans les couches aiguilletées.In an exemplary embodiment, the needling head or the support can be translated from a non-zero distance of less than or equal to 30 mm, for example less than or equal to 15 mm, in particular to reduce the presence of dead zones in needled layers.
L'invention vise aussi, selon un autre aspect, un procédé de fabrication d'une pièce en matériau composite comprenant un renfort fibreux densifié par une matrice, le procédé comprenant au moins les étapes suivantes :
- la fabrication d'une structure fibreuse aiguilletée destinée à former le renfort fibreux de la pièce par un procédé tel que celui décrit précédemment, et
- la formation d'une matrice dans la porosité de la structure fibreuse aiguilletée de façon à obtenir la pièce en matériau composite.
- the manufacture of a fibrous needled structure intended to form the fibrous reinforcement of the part by a process such as that described above, and
- the formation of a matrix in the porosity of the fibrous structure needled to obtain the composite material part.
D'autres caractéristiques et avantages de la présente invention ressortiront de la description faite ci-dessous, en référence aux dessins annexés qui en illustrent un exemple de réalisation dépourvu de tout caractère limitatif. Sur les figures :
- les
figures 1A à 3B illustrent les étapes d'un procédé selon un premier mode de réalisation de l'invention, mettant en oeuvre une machine d'aiguilletage du type plan, et - les
figures 4A à 5B illustrent les étapes d'un procédé selon un deuxième mode de réalisation de l'invention, mettant en oeuvre une machine d'aiguilletage du type plan.
- the
Figures 1A to 3B illustrate the steps of a method according to a first embodiment of the invention, implementing a needling machine of the planar type, and - the
Figures 4A to 5B illustrate the steps of a method according to a second embodiment of the invention, implementing a needling machine of the planar type.
Les
Sur la
La
A la
Puis, comme illustré sur la
Après déplacement relatif de la table 120 par rapport à la tête d'aiguilletage 110, on réalise l'aiguilletage de la deuxième couche fibreuse 20, la tête d'aiguilletage 110 étant dans la deuxième position au moins au début de l'aiguilletage de la deuxième couche 20. L'aiguilletage de la deuxième couche fibreuse 20 peut être réalisé de manière identique à l'aiguilletage de la première couche fibreuse 10. En particulier la table 120 peut aussi se déplacer devant la tête d'aiguilletage 110 dans la direction X et peut faire un aller-retour pour aiguilleter toute la deuxième couche 20.After relative movement of the table 120 with respect to the needling
Sur la
Les
Dans la suite, on considère que lorsque la structure fibreuse 30 est enroulée avec moins d'un tour sur le mandrin 220, la portion enroulée forme une première couche fibreuse 31 sur le mandrin 220. Lorsque la structure 30 est enroulée avec plus d'un tour et moins de deux tours, la portion qui recouvre la première couche 31 forme une deuxième couche fibreuse 32 sur le mandrin 220.In the following, it is considered that when the
De façon connue, pour aiguilleter la première couche 31, on fait tourner le mandrin 220 progressivement (flèche 221) pour faire défiler la première couche 31 devant la tête d'aiguilletage 210. Dans le même temps, la tête d'aiguilletage 210 est animée d'un mouvement selon la double flèche 212 afin d'aiguilleter l'ensemble de la première couche 31. Suite à l'aiguilletage de cette première couche 31, la tête d'aiguilletage 210 se trouve dans une première position par rapport au mandrin 220. Cette première position est définie ici notamment par la position selon l'axe X de la tête d'aiguilletage 210 par rapport au mandrin 220. Comme pour l'exemple précédent, le défilement de la structure fibreuse 30 devant la tête d'aiguilletage 210 peut être réalisé pas à pas, afin notamment de réduire le cisaillement de la couche fibreuse lors de l'aiguilletage.In known manner, to needle the
De manière similaire à l'exemple précédent, la
Puis, comme illustré sur la
Après déplacement relatif du mandrin 220 par rapport à la tête d'aiguilletage 210, on réalise l'aiguilletage de la deuxième couche fibreuse 32, la tête d'aiguilletage 210 étant dans la deuxième position au moins au début de l'aiguilletage de la deuxième couche fibreuse 32. L'aiguilletage de la deuxième couche fibreuse 32 peut être réalisé de manière identique à l'aiguilletage de la première couche fibreuse 31. En particulier le mandrin 220 peut tourner autour de l'axe B de façon à faire défiler la deuxième couche 32 devant la tête d'aiguilletage 210 qui est animée d'un mouvement de va et vient selon la direction Z.After relative displacement of the
Sur la
Des exemples de procédés selon l'invention ont été décrits en lien avec une machine d'aiguilletage de type plan 100 et avec une machine d'aiguilletage de type circulaire 200. Dans l'une ou l'autre de ces machines 100 et 200, les étapes de déplacement relatif du support par rapport à la tête d'aiguilletage correspondent à des mouvements particuliers du support ou de la tête, par exemple une translation ou une rotation, adaptés notamment à la machine considérée. Bien entendu, on ne sort pas du cadre de la présente invention lorsque l'étape de déplacement relatif du support par rapport à la tête d'aiguilletage comprend successivement plusieurs types de mouvements, par exemple une translation suivie d'une rotation ou vice versa.Examples of processes according to the invention have been described in connection with a plane-
Une couche fibreuse peut par exemple comprendre une nappe de fibres unidirectionnelles, ou une nappe textile présentant un tissage bidimensionnel. Les fibres de la couche fibreuse peuvent être des fibres d'un matériau réfractaire comme du carbone, ou des fibres céramiques, par exemple en carbure de silicium ou en verre.A fibrous layer may for example comprise a unidirectional fiber web, or a textile web having a two-dimensional weave. The fibers of the fibrous layer may be fibers of a refractory material such as carbon, or ceramic fibers, for example silicon carbide or glass.
En outre, pour des raisons de simplification, les exemples de procédés selon l'invention ont été décrits avec l'aiguilletage de seulement deux couches fibreuses empilées, mais il est évident que l'invention s'applique à l'aiguilletage d'un nombre plus important de couches fibreuses, qui peuvent être de formes et de dimensions variées. Aussi, lorsque l'on aiguillette une couche fibreuse, elle est généralement présente sur une autre couche fibreuse sous-jacente. Dans les exemples illustrés, la couche fibreuse sous-jacente à la première couche 10 ou 21 n'a pas été représentée. On notera que dans certains cas, il est possible d'aiguilleter une couche fibreuse seule sans qu'une couche fibreuse sous-jacente ne soit présente. Dans ce dernier cas, on pourra interposer une couche de feutre (non représentée) entre la table ou le mandrin et la première couche fibreuse.In addition, for reasons of simplification, the examples of processes according to the invention have been described with the needling of only two stacked fibrous layers, but it is obvious that the invention applies to the needling of a number more important fibrous layers, which can be of various shapes and sizes. Also, when we need a fibrous layer, it is usually present on another underlying fibrous layer. In the illustrated examples, the fibrous layer underlying the
Par ailleurs, lorsque le procédé selon l'invention est répété, par exemple lorsque l'on empile une troisième couche fibreuse sur la deuxième, puis une quatrième sur la troisième, etc. il peut être avantageux de choisir de façon aléatoire la valeur de l'angle de rotation α ou de la distance de translation ΔX pour chaque étape de déplacement relatif du support par rapport à la tête d'aiguilletage qui est réalisée entre chaque étape d'aiguilletage.Moreover, when the process according to the invention is repeated, for example when a third fibrous layer is stacked on the second, then a fourth on the third, etc. it may be advantageous to choose randomly the value of the angle of rotation α or of the translation distance ΔX for each step of relative displacement of the support relative to the needling head which is performed between each needling step .
Dans le présent exposé, il faut entendre l'expression « compris entre ... et ... » comme incluant les bornes.In this presentation, the expression "between ... and ..." is to be understood as including the terminals.
Claims (5)
dans lequel (i) le déplacement relatif comprend une rotation relative du support (120) par rapport à la tête d'aiguilletage (110), ou (ii) le support (220) est un mandrin rotatif et le déplacement relatif est une translation relative de la tête d'aiguilletage (210) par rapport au support selon une direction (X) parallèle à un axe (B) de rotation du support.A method of manufacturing a needled fibrous structure using a needling machine (100; 200) provided with a needling head (110; 210) comprising a plurality of needles, the method comprising at least the following steps:
wherein (i) the relative displacement comprises a relative rotation of the support (120) with respect to the needling head (110), or (ii) the support (220) is a rotating mandrel and the relative displacement is a relative translation the needling head (210) relative to the support in a direction (X) parallel to an axis (B) of rotation of the support.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR1751830A FR3063745B1 (en) | 2017-03-07 | 2017-03-07 | PROCESS FOR MANUFACTURING A NEEDLE FIBROUS STRUCTURE |
Publications (2)
Publication Number | Publication Date |
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EP3372718A1 true EP3372718A1 (en) | 2018-09-12 |
EP3372718B1 EP3372718B1 (en) | 2020-01-01 |
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EP18159859.0A Active EP3372718B1 (en) | 2017-03-07 | 2018-03-05 | Method for manufacturing a needled fibrous structure |
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US (1) | US10704171B2 (en) |
EP (1) | EP3372718B1 (en) |
FR (1) | FR3063745B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020212113A1 (en) * | 2019-04-17 | 2020-10-22 | Andritz Asselin-Thibeau | Needling machine or needling line with multi-needle boards |
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EP0683261A2 (en) * | 1994-05-17 | 1995-11-22 | The B.F. Goodrich Company | Near net shaped fibrous structures and methods of making |
WO1997020092A1 (en) * | 1995-11-27 | 1997-06-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Method for making fibrous preforms for producing annular parts from a composite material |
EP2816147A1 (en) * | 2013-06-20 | 2014-12-24 | Messier-Bugatti-Dowty | A table and a method for needling a textile structure formed from an annular fiber preform, with radial offsetting of the needling head |
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US3431611A (en) | 1966-09-16 | 1969-03-11 | Gen Electric | Method for forming nonwoven electric blanket shells |
US3909891A (en) * | 1972-01-18 | 1975-10-07 | Dilo Kg Oskar | Needling Apparatus |
US3845529A (en) | 1972-08-31 | 1974-11-05 | Riegel Textile Corp | Apparatus and process for tacking fabrics |
FR2557550B1 (en) * | 1983-12-28 | 1986-05-30 | Europ Propulsion | METHOD AND APPARATUS FOR THE MANUFACTURE OF THREE-DIMENSIONAL REVOLUTION STRUCTURES |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
US4878278A (en) * | 1987-08-05 | 1989-11-07 | Wangner Systems Corporation | Method for manufacture of paper making fabrics |
AT400852B (en) * | 1994-05-02 | 1996-04-25 | Fehrer Textilmasch | DEVICE FOR NEEDING A CIRCULAR, IN PARTICULAR CIRCULAR FIBER PAD |
US6568050B2 (en) | 2001-02-26 | 2003-05-27 | Messier-Bugatti | Method and installation for advancing a needled fiber plate |
FR2824084B1 (en) * | 2001-04-30 | 2003-08-01 | Messier Bugatti | NEEDLE FEEDER BY CONTINUOUS SPIRAL BAND |
US7430790B1 (en) | 2005-04-26 | 2008-10-07 | Don Bowles | Felting machine |
ATE485414T1 (en) | 2007-08-09 | 2010-11-15 | Dilo Kg Maschf Oskar | SYSTEM AND METHOD FOR NEEDLING A NON-WOVEN WEB |
CN105899341A (en) * | 2013-05-31 | 2016-08-24 | 先进碳技术有限责任公司 | Methods of manufacturing low density cloth preform |
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2017
- 2017-03-07 FR FR1751830A patent/FR3063745B1/en active Active
-
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- 2018-03-05 EP EP18159859.0A patent/EP3372718B1/en active Active
- 2018-03-06 US US15/913,370 patent/US10704171B2/en active Active
Patent Citations (3)
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EP0683261A2 (en) * | 1994-05-17 | 1995-11-22 | The B.F. Goodrich Company | Near net shaped fibrous structures and methods of making |
WO1997020092A1 (en) * | 1995-11-27 | 1997-06-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Method for making fibrous preforms for producing annular parts from a composite material |
EP2816147A1 (en) * | 2013-06-20 | 2014-12-24 | Messier-Bugatti-Dowty | A table and a method for needling a textile structure formed from an annular fiber preform, with radial offsetting of the needling head |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020212113A1 (en) * | 2019-04-17 | 2020-10-22 | Andritz Asselin-Thibeau | Needling machine or needling line with multi-needle boards |
FR3095214A1 (en) * | 2019-04-17 | 2020-10-23 | Andritz Asselin-Thibeau | Needling machine or multi-needle board needling line |
US11946180B2 (en) | 2019-04-17 | 2024-04-02 | Andritz Asselin-Thibeau | Needling machine or needling line with multi-needle boards |
Also Published As
Publication number | Publication date |
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FR3063745B1 (en) | 2021-06-11 |
FR3063745A1 (en) | 2018-09-14 |
US10704171B2 (en) | 2020-07-07 |
US20180257331A1 (en) | 2018-09-13 |
EP3372718B1 (en) | 2020-01-01 |
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