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    • 专利摘要:
    This preform (3) defines two parts (21, 23) and comprises: a first group (C1) of layers of warp threads, which is external in the first part, a second group (C2) of warp son layers, which is immediately below this first group, and a first group (T1) of layers of weft threads which is bonded with the first group of warp thread layers, so as to be external in the first part. According to the invention, the first group (C1) of warp layers is absent in the second part and the first group (T1) of layers of weft threads (19) extends into the second part, being bonded with the second group of warp layers in the second part, so that the first group of weft thread layers is external in the second part.
    公开号:FR3055569A1
    申请号:FR1658182
    申请日:2016-09-02
    公开日:2018-03-09
    发明作者:Jean Vincent RISICATO；Patrick VARANIAC
    申请人:Porcher Industries SA；
    IPC主号:
    专利说明:

    055 569
    58182 ® FRENCH REPUBLIC
    NATIONAL INSTITUTE OF INDUSTRIAL PROPERTY © Publication number:
    (to be used only for reproduction orders)
    ©) National registration number
    COURBEVOIE
    ©) Int Cl 8 : B 29 B 11/16 (2017.01), D 03 D 25/00, B 29 C 70/24, B 64 C 1/06
    A1 PATENT APPLICATION
    ©) Date of filing: 02.09.16. © Applicant (s): PORCHER INDUSTRIES Company (30) Priority: anonymous— FR. ©) Inventor (s): RISICATO JEAN VINCENT and VARA- NIAC PATRICK. (43) Date of public availability of the request: 09.03.18 Bulletin 18/10. ©) List of documents cited in the report preliminary research: Refer to end of present booklet (© References to other national documents ©) Holder (s): PORCHER INDUSTRIES Société ano- related: nyme. ©) Extension request (s): ©) Agent (s): LAVOIX.
    PREFORM, FRAME PIECE AND METHOD FOR MANUFACTURING SUCH A PREFORM.
    FR 3 055 569 - A1 (uç) This preform (3) defines two parts (21, 23) and comprises: a first group (C1) of layers of warp threads, which is external in the first part, a second group ( C2) of layers of warp threads, which is located immediately below this first group, and a first group (T1) of layers of weft threads which is linked with the first group of layers of warp threads, so as to be external in the first part. According to the invention, the first group (C 1) of loose wire layouts is absent in the second part and the first group (T1) of weft son layers (19) extends into the second part, being linked with the second group of weft yarn layers in the second part, so that the first group of weft yarn layers is external in the second part.

    Preform, backbone and method of manufacturing such a preform
    The invention relates to a preform, in particular a stiffener, in a three-dimensional fibrous structure, a frame piece, in particular a stiffener, comprising such a preform, as well as a process for manufacturing such a preform.
    The invention relates to the production of parts made of composite material and more particularly of fibrous structures for reinforcing such parts, these fibrous structures being obtained by three-dimensional weaving or 3D weaving. More specifically, the aim is to produce a preform in a fibrous structure, which has a shape or definitive or quasi-definitive dimensions of the part made of composite material to be produced. Such a preform is designed to then be densified, that is to say consolidated, with a resin matrix to form the part made of composite material.
    One field of application of the invention is the production of framework pieces, in particular of beams or stiffeners, in composite material, with fibrous reinforcement and matrix in resin. Such parts, generally of elongated shape, are used in many fields, in particular in aircraft construction. The invention relates in particular to the production of parts having a thin part on at least one longitudinal edge of the structural part.
    In the case of composite parts having thin parts, such as the connecting parts of the stiffeners or the trailing edges of blades of blades for turbomachinery, it is advisable to preserve the three-dimensional structure even in these thin parts while preserving the structural continuity with the thicker parts. The usual practice consisting, during weaving, of removing threads in the warp and / or weft direction, can cause excessively large variations in the fiber content and fraying of the thin parts at their ends.
    W0-A1-2006 / 136755 proposes a reinforcement structure comprising an internal part, or heart, and a part adjacent to an external surface, or skin, the fibrous structure being formed by three-dimensional weaving with heart, skin and heart being formed by different armor. The reduction in thickness of the structure is obtained by a lower number of weft son layers in the thin parts and the document proposes to have a transition zone between thick part and thin part in the form of a partial layer. additional weft yarn, linked by weaving to two complete layers of weft yarn between which it is arranged, using an interlock type weave. The document also mentions, without further details, that the titer of the wires between the heart and the skin may vary. This solution does not make it possible to obtain particularly thin parts such as the ends of the lugs of stiffeners.
    WO-A1-2013 / 088039 proposes a fibrous reinforcement structure produced in a single piece by multilayer weaving, by integrating at least one layer of threads with variable title, each thread of this layer being formed of a separable assembly of fibers, so that, in the thin parts, these threads see their title reduced by elimination of separable fibers. This is combined with a gradual reduction in the number of weft yarn layers in the thin parts. However, the removal of these elementary threads complicates the weaving process.
    The invention therefore aims to provide a new preform, which, while being particularly thin in its thin part (s), presents a particularly reduced risk of fraying in this part and is relatively easy to to manufacture.
    The subject of the invention is a preform, in particular a stiffener, in three-dimensional fibrous structure having a thickness and being woven in a single piece by multilayer weaving of layers of warp threads and layers of weft threads distributed according to the thickness, the preform defining at least a first part and at least a second part extending the first part towards a thin edge of the preform, the preform comprising:
    a first group of successive warp yarn layers, which includes at least one layer of warp yarns and which is external in the first part, a second group of successive warp yarn layers, which includes at least one layer of warp yarns warp and which is located immediately below the first group of weft yarn layers, and a first group of successive weft yarn layers, which includes at least one layer of weft yarn and which is linked in an armor with the first group layers of warp threads, so as to be external in the first part,
    According to the invention, the number of layers of warp yarns forming the second part is reduced compared to the number of layers of warp yarns forming the first part, due to the absence of the first group of layers of warp yarns in the second part, so that the second part has a reduced thickness compared to that of the first part and so that the second group of layers of warp threads is external in the second part.
    In addition, the first group of weft yarn layers extends into the second part, being linked in an armor with the second group of warp yarn layers in the second part, so that the first group of layers of weft yarn is also external in the second part.
    Thanks to the invention, the risk of fraying is reduced even in the case where the second part has a very small thickness, insofar as the first group of layers of weft yarns is disposed outside the first part and the second part without discontinuity. In particular, the preform advantageously has a substantially continuous surface condition at a junction between the first part and the second part. The manufacture of the preform remains relatively simple, however, insofar as the first group of weft son layers can be integrated into the fibrous structure during the three-dimensional weaving of the latter. Furthermore, a three-dimensional loom can be easily configured so that the number of threads in each layer of warp threads is different from one part to another and to link the first group of layers of weft threads at the same time to the second group of warp layers in the second part and to the first group of warp layers in the first part.
    According to other optional and advantageous characteristics of the invention, taken alone or in combination:
    the preform comprises a second group of successive weft yarn layers, which includes at least one layer of weft yarns and which is located immediately below the first group of weft yarn layers in the first part, the second group of layers of weft yarns being absent from the second part, for example by interrupting the weft yarns of this second layer of weft yarns, at a junction of the first part with the second part.
    the weft yarns of the first group of weft son layers have a titer lower than the title of the weft yarns of the second group of weft son layers.
    the warp yarns of the first group of warp yarn layers have a title lower than the title of the warp yarns of the second group of warp yarn layers.
    the preform contains 6K wires and 3K wires.
    the second part comprises at least three layers of warp threads.
    the preform comprises a third part extending the second part in the direction of the thin edge, while the preform comprises a third group of successive layers of warp threads, which includes at least one layer of warp threads and which is located immediately below the first group of layers of warp yarns in the second part, while the number of layers of warp yarns forming the third part is reduced relative to the number of layers of warp yarns forming the second part, due to the absence of the second group of warp yarn layers in the third part, so that the third part has a reduced thickness compared to that of the second part and so that the third group of warp yarn layers is external in the third part , and while the first group of layers of weft threads extends into the third part, being linked in an armor with the tro the third group of weft yarn layers in the third part, so that the first group of weft yarn layers is also external in the third part.
    a plurality of warp threads and / or weft threads of the preform carries a hardened polymer bringing a degree of cohesion to the preform at least in the second part.
    the thin edge is welded by means of said hardened polymer carried by the wires.
    The invention also relates to a framework piece, in particular a stiffener, comprising a preform as defined above, as well as a consolidation material, of the resin type, with which the fibrous structure of the preform is impregnated.
    The invention also relates to a method of manufacturing a preform, in particular a stiffener, in a three-dimensional fibrous structure having a thickness and being woven in one piece, the manufacturing method comprising a step of weaving a multi-layer of layers of threads. of warp and layers of weft yarns distributed along the thickness, in which at least a first part and at least a second part are defined, extending the first part towards a thin edge of the preform, so that the preform includes:
    a first group of successive warp yarn layers, which includes at least one layer of warp yarns and which is external in the first part, a second group of successive warp yarn layers, which includes at least one layer of warp yarns warp and which is located immediately under the first group of layers of warp threads, and a first group of successive layers of weft threads, which includes at least one layer of weft threads and which is linked in an armor with the first group layers of warp threads, so as to be external in the first part,
    According to the invention, to form the second part:
    the number of layers of warp yarns in the second part is reduced relative to the number of layers of warp yarns forming the first part, this reduction being obtained by absence of the first group of layers of warp yarns in the second part, so that the second part has a reduced thickness compared to that of the first part, and so that the second group of layers of warp threads is external in the second part, and the first group of layers of weft threads is bonded , in a weave, with the second group of layers of warp yarns in the second part, so that the first group of layers of weft yarns is also external in the second part.
    Preferably, the preform comprises a second group of weft yarn layers, which includes at least one layer of weft yarn and which is located immediately under the first group of weft yarn layers in the first part, whereas, at the level of the second part, an excess part of the weft threads of the second group of layers of weft threads is taken out of the fibrous structure, and then the excess part is cut.
    The invention will be better understood on reading the description which follows given solely by way of nonlimiting example and made with reference to the drawings in which:
    Figure 1 is a schematic perspective view of a stiffener including a preform in fibrous structure according to a first embodiment of the invention;
    Figure 2 is a section along a plane P2, showing a detail of the preform of Figure 1 on a larger scale; and
    Figure 3 is a section similar to that of Figure 2, showing a detail of a preform according to a second embodiment of the invention.
    The figures are oriented according to an orthonormal reference frame R1, define three directions of space X, Y and Z.
    The stiffener 1 of FIG. 1 constitutes a framework part, that is to say a structural part of the spar, pillar or beam type, for a vehicle, preferably an aircraft. The reference mark R1, attached to the stiffener 1, is oriented so that the direction X is parallel to the longitudinal axis of the stiffener 1, the directions Y and Z to transverse directions of the stiffener 1.
    The stiffener 1 is made of a composite material comprising a preform in three-dimensional fibrous structure, the preform 3 being consolidated, for example by impregnation with a consolidation or reinforcement material 5 forming a matrix, of the resin type. Preferably, the resin is a thermoplastic or thermosetting resin.
    The preform 3 is woven in a single piece using a multi-layer three-dimensional weaving process, including successive layers of warp threads 17, the threads 17 of which extend in the direction X. The layers of weft threads 19 extend either in the direction Y, or in the direction Z, depending on the part of the stiffener considered. In particular, in a part 9, forming a blade of the stiffener 1, the weft threads extend in the direction Y, and the layers of warp threads 17 and weft threads 19 are distributed, that is to say say stacked, in the direction Z, oriented along the thickness of the blade 9, being linked to each other by weaving. Thus, the threads 17 and 19 are wavy and interlaced with one another in one or more predetermined weaving weaves.
    The warp threads 17 and the weft threads 19, are for example made from an organic material, of the polypropylene (PP), viscose, polyamide 6.6 (PA66), polyethylene (PE), polyvinyl acetate (PVA), Para- aramid, or poly (p-phenylene-2,6benzobisoxazole (PBO), or in an inorganic material, such as steel, carbon, silicon carbide, silica, E glass, S glass, or R glass.
    Preferably, the preform 3 is distributed over all or almost all of the volume of the stiffener 1.
    The preform 3, at the end of its weaving, of a possible step of cutting nonwoven yarns and of a possible step of preforming as defined below, advantageously has an identical or almost identical shape to that of the stiffener 1 consolidated with the consolidation material 5. In other words, the concentration of fibrous structure of the stiffener 1 is preferably substantially constant throughout the volume of the stiffener 1, or almost all of this volume. For example, the volume ratio of fibers in the stiffener 1 is between approximately 30% and 80%.
    Alternatively, the concentration of fibrous structure of the stiffener 1 differs in certain areas of the stiffener 1, depending on the desired application.
    Preferably also, the stiffener 1 comprises a single preform 3 made in one piece.
    In practice, the preform 3 forms in itself a stable structure into which the consolidation material 5 is injected, for example into a mold, to form the stiffener 1. Optionally, the preform 3 occupies a space slightly higher than the mold and must be slightly compacted to be introduced into the mold before injection of the consolidation material.
    In practice, the preform 3 is flush with all or part of the external surface of the stiffener 1, which is shown diagrammatically on a local part A1 of the external surface of the stiffener 1 in FIG. 1.
    The stiffener 1 and the preform 3 have a section, taken along the plane YZ, preferably constant in the direction X. At the level of the blade 9, this section along YZ has, along the direction Y, a thickness which varies according to the direction Z. In particular, the blade 9 has a thin edge 7, extending parallel to the direction X. From the thin edge 7, the blade 9 thickens parallel to the direction Y. The blade 9 has a base 8, opposite the thin edge 7, from which rises a wall 11, or rib, of the stiffener 1. In practice, the fibrous structure of the preform 3 is woven flat, that is to say say that the strip 9 and the wall 11 are initially formed horizontally in the same XY plane, itself oriented horizontally. During a preforming step of the preform 3, the orientation and the final shape of the wall 11 is obtained by deformation or deployment of the fibrous structure. The wall 11 is then inclined relative to the blade 9, and extends in the XZ plane, as illustrated in FIG. 1, while the blade extends in the perpendicular XY plane. Thus, all or part of the weft threads of the wall 11 extends perpendicular to the weft threads of the strip 9, and in this case parallel to the direction Z.
    More specifically, before the preforming step, the fibrous structure intended to form the preform 3 comprises at least one debinding in a plane defined between two successive layers of warp and / or weft yarns. "Untying" means that two consecutive layers of yarn, in the thickness direction of the fibrous structure, are not linked together on a certain surface, but joined together where the unbinding stops. Thanks to this unbinding, the two separate parts can be separated from each other, which allows the deployment of the fibrous structure to give it its final preform 3 shape.
    Furthermore, all or a determined fraction of the warp threads and / or the weft threads of the fibrous structure, which is woven flat and which is intended to form the preform 3, carries a heat-sensitive polymer at the surface. During the preforming step, after deployment of the fibrous structure, a heat treatment of the preform 3 is carried out aimed at softening this polymer, then cooling, so as to fix the preformation of the preform 3. The preform 3 then comprises at least one part in which the warp threads 17 and the weft threads 19 are linked at their intersections by polymer, where at least one of the warp threads 17 and / or weft 19 carries polymer. The polymer is in the hardened state. The connection at the intersection points is obtained by softening, then hardening of the polymer by suitable heating.
    The preform can therefore also be defined as comprising a textile structure, the weaving of which has been carried out using warp threads and / or weft threads carrying the heat-sensitive polymer on the surface. The passage to the preform was done by thermoforming at a temperature higher than the softening point of the polymer, followed by cooling, whereby the warp and weft threads are linked at their intersections by polymer there where at least one of the warp and / or weft threads carries polymer.
    The polymer present on the wires is frozen, if it is thermosetting, it is hardened, if it is thermoplastic. It is below its glass transition temperature. Thermosetting or thermoplastic, the polymer has a softening temperature which can correspond to its Tg. The passage of this temperature leads to a reversible softening allowing, on the one hand, the bonding of the coated wires, that is to say the at least one of the warp thread and the weft thread in contact, at their points of intersection, and, on the other hand, to deploy the fibrous structure in its "preform" form. Cooling below this temperature then freezes the preform, ready to be impregnated with consolidation material, and easy to handle.
    The polymer in contact with certain warp and / or weft threads can be chosen from polymers, including copolymers, thermoplastics and thermosets. It can be the same or different from the polymer which will then be injected or infused. Mention may in particular be made of: polyamides (PA), copolyamides (CoPA), ether or ester block polyamides (PEBAX, PEBA), polyphthalamides (PPA), polyesters (in particular polyethylene terephthalate -PET-, polybutylene terephthalate - PBT -), copolyesters (CoPE), thermoplastic polyurethanes (TPU), polyacetals (POM, ...), polyolefins (in particular PP, HDPE, LDPE, LLDPE), polyethersulfones (PES), polysulfones (PSU, ...), sulfonated polyphenylenes (PPSU, ...); polymers of the PAEK family polyaryletherketones comprising in particular polyetheretherketones (PEEK) and polyetherketoneketones (PEKK); poly (phenylene sulfide) (PPS), polyetherimides (PEI), thermoplastic polyimides, liquid crystal polymers (LCP), phenoxys, block copolymers such as styrene butadiene-methyl methacrylate copolymers (SBM), copolymers butyl methyl methacrylate-acrylate-methyl methacrylate (MMA) and mixtures thereof, epoxies, bismaleimide, phenolic polymers.
    Whatever the method for preforming the preform 3, the blade 9 is delimited by a planar surface 13 extending in the XY plane, and by an oblique surface 15, which is curved in the present example. The oblique surface 15 is inclined relative to the XY plane, so that the surfaces 13 and 15 converge towards each other as far as the thin edge 7 by which they end. As a variant, the oblique surface 15 is planar, or of another shape, the projection of which in the YZ plane is monotonous and convergent with respect to the XY plane. Similarly, the surface 13 can be oblique to the XY plane, being planar, curved, or of another shape, the projection of which in the YZ plane is monotonous and convergent with respect to the XY plane.
    FIG. 2 very schematically shows a section along a plane P2 parallel to the plane YZ of an area of the blade 9, on a scale large enough so that the warp threads 17 and the weft threads 19 are visible on this Figure 2. The oblique surface 15 visible in Figure 1 is found at the top of Figure 2. The thin edge 7 and the base 8 are not visible in Figure 2, but are located outside of Figure 2, respectively right and left of the latter, as symbolized by arrows 7 and 8 respectively. The warp threads 17, extending in the direction X, are shown cut by the plane P2, while the weft threads 19 extend along this plane P2, parallel to the direction Y.
    The preform 3 defines a first part 21 and a second part 23 in the direction Y. The part 21 is said to be “thick”, insofar as it has a thickness in the direction Z, the value of which is greater than that of the part 23, which is therefore qualified as "thin". The thin part 23 extends the thick part 21 from a junction 25 of the preform 3. In other words, the thin part 23 continues the thick part 21, the boundary between the thin part 23 and the thick part being located at junction 25. More specifically, junction 25 is located immediately adjacent to the last of the warp threads 17 of the first layer C1. The thin part 23 extends from the junction 25 to the thin edge 7 of the preform 3. The thick part 21 extends from the junction 25 to the base 8 of the blade 9 of the preform 3.
    The preform 3 comprises, at least in the thick part 21 and the thin part 23, a plurality of layers of successive warp threads 17 distributed in the thickness direction of the preform 3, including successive layers C1, C2, C3 , C4, C5, C6, as well as other subsequent layers not visible in FIG. 2. By "successive" is meant that the layer C2 is located immediately below the layer C1, that the layer C3 is located immediately below the layer C2, and so on. By “successive”, it is meant that the designated layers are distributed in the order indicated, from the external part towards the heart of the preform 3. By “immediately”, it is meant that no layer of warp yarns 17 n 'is interposed between a first layer of warp threads 17 and a second layer of warp threads 17 located immediately under this first layer of warp threads 17. On the other hand, weft threads can be interposed between two layers of warp threads immediately one under the other.
    One qualifies with the term "external", or the expression "of skin", a layer or a group of successive layers, for threads of the same direction, either weft or warp, this layer or group being the closest of the surface of the preform 3, in the thickness direction, that is to say in the direction Z in the present example. In contrast, the term “internal” or the expression “at heart” is used to describe any layer or group of successive layers, of threads in the same direction, either weft or warp, layer or group which is separated from the surface of the preform 3 by at least one outer layer of wires in the same direction.
    In the example of FIG. 2, the first layer C1 is external in the thick part 21. Thus, in the thick part 21, the layer C1 extends at the level of the surface 15, and forms a layer of skin of the preform 3.
    The number of layers of warp threads 17 forming the thin part 23 is reduced compared to the number of layers of warp threads 17 forming the thick part 21, due to the absence of the first layer C1 of warp threads 17 in the thin part 23. Thus the thin part 23 has a reduced thickness compared to the thickness of the thick part 21. In the thin part 23, from the junction 25, the first layer C1 of son of chain 17 is interrupted, or absent. In other words, the preform 3 is devoid of warp threads 17 at the level of the layer C1 in the thin part 23. Thanks to this absence of the layer C1 in the thin part 23, the thickness measured in the direction Z of the thin part 23 is less than the thickness in the direction Z of the thick part 21. Due to this absence of the layer C1 in the thin part also 23, the second layer of warp son C2 is external in the part thin 23, while extending in the thick part 21 under the layer C1, so that the layer C2 is internal in the thick part while being immediately under the layer C1.
    The blade 9 of the preform 3 also comprises a plurality of layers of weft threads 19, including successive layers T1, T2, T3, T4, T5 and T6, visible in FIG. 2, as well as other subsequent layers of threads of weft not visible in FIG. 2. The weft threads 19 of each layer are linked in an armor with at least one of the layers of warp threads 17.
    The second layer T2 of weft yarns is located immediately under the first layer T1 of weft yarns 19 in the thick part 21. The third layer T3 of weft yarns 19 is located immediately under the second layer T2, in the thick part 21 , and immediately under the first layer T1 in the thin part 23. The fourth layer of weft yarns T4 is located immediately under the third layer of weft yarns T3 in the thin part 23 as in the thick part 21. The fifth layer T5 is located immediately below the fourth layer T4, while the sixth layer T6 is located immediately below the fifth layer T5. By "immediately" is meant that no layer of weft yarns 19 is interposed between a first layer of weft yarns 19 and a second layer of weft yarns 19 located immediately under this first layer of weft yarns 19. On the other hand, warp threads can be interposed between two layers of weft threads immediately below one another.
    The first layer T1 of weft threads 19 is linked in an armor with the first layer C1 of warp threads 17, so as to be external in the thick part 21. From the junction 25, the first layer of weft threads T1 descends one row in the thickness direction, so as to extend into the thin part 23, being linked in a weave with the second layer C2 of warp son 17 in the thin part 23. From in this way, the first layer T1 of weft threads 19 is also external in the thin part 23. The first layer T1 thus forms a layer of skin in the direction Y, both in the thick part 21 and in the thin part 23 .
    To obtain this particular arrangement, the second layer T2 of weft threads 19 situated immediately under the first layer T1 of weft threads 19 in the thick part 21, is absent from the thin part 23 from the junction 25. For this, as illustrated in FIG. 2, an excess part 20 of all or part of the weft threads 19 of the second layer T2 advantageously exits outside the fibrous structure of the preform 3 at the junction 25, through the first layer T1 of weft threads 19. In other words, the excess part 20 rotates around the last warp thread 17 of the first layer C1, or of a neighboring warp thread 17, being directed towards the outside of the preform 3. These excess parts 20 are advantageously cut so as to guarantee the regularity of the surface condition of the surface 15. In any event, all or part of the weft threads 19 of the second are interrupted layer T2 from junction 25, in the thin part 23.
    According to a variant not illustrated, all or part of the weft threads 19 of the second layer T2 is not cut, but is woven into the thin part 23, being linked in an armor with this thin part 23, in particular with yarns 17 of the second layer C2 and / or of the third layer C3, this weave being less intertwined than the weave linking this same layer T2 of weft yarns 19 with the warp yarns 17 in the thick part 21. Preferably, in this variant, all or part of the weft yarns 19 of the third layer T3 and possibly other layers of weft yarns 19 below, also have less woven weave in the thin part 23 than in the thick part 21.
    Whatever the variant, a progressive decrease in the thickness of the blade 9 is thus obtained in the direction of the thin edge 7, that is to say a difference in thickness along the direction Z of the three-dimensional structure, at the level of the junction 25. Since the layer T1 forms a skin of the three-dimensional structure, the surface condition of the preform 3 is continuous despite this difference in thickness.
    The preform 3 advantageously comprises a third part, not visible in FIG. 1, extending part 23 in the direction of the thin edge 7 from a junction, not visible in FIG. 1, similar to junction 25. According to a similar diagram to that of FIG. 1 for the junction 25, the number of layers of warp threads 17 forming the third part is reduced compared to the number of layers of warp threads 17 forming the part 23, due to an absence of the second layer C2 of warp threads 17 in the third part. Thus, the third part has a reduced thickness compared to that of the part 230. In addition, the third layer C3 of warp threads 17 is external in the third part. Furthermore, the first layer T1 of weft threads 19 extends as far as the third part, being linked in an armor with the third layer C3 of warp threads 17 in the third part. The first layer T1 is therefore also external in the third part and thus forms a continuous skin along all the parts of the blade 9. According to the same pattern repeated up to the thin edge 7, successive parts which are less and less thick and separated by junctions similar to the above, can be constructed in order to produce a gradual reduction in the thickness of the blade 9 up to the thin edge 7. The obliqueness of the surface 15 relative to the XY plane, as well as the 'possible curvature of the surface 15, are obtained by a succession of junctions 25 similar to that of Figure 2 and advantageously using the aforementioned preforming step, the junctions 25 being distributed in the direction Y. Each of these junctions separates a thicker part from a lower thickness part. As the successive junctions, the thickness in the direction Z of the preform 3 is reduced, in this case one or more layers of son 17 and 19 at each junction 25, the first layer T1 s advantageously extending externally from the base 8 to the thin edge 7. In other words, the first layer T1 forms a continuous layer of skin of the preform 3, from the base 8 to the thin edge 7.
    To obtain the obliquity of the surface 13, a similar diagram can be applied, in particular symmetrically.
    Preferably, the weft threads 19 of the first layer T1 of weft threads 19 have a titer lower than the title of the weft threads 19 of the second layer C2 of weft threads 19. Similarly, the warp threads 17 of the first layer C1 have a title lower than the title of the warp threads 17 of the second layer C2. In a manner known per se, the title or titration of a wire corresponds to the size of the wire, which can be defined in many ways, in particular by the number of filaments which compose it. In this case, the thread title is expressed in "K" which corresponds to the number in thousands of filaments per thread. In a manner known per se, the title of a wire can alternatively be defined in particular by its linear mass or other similar or equivalent quantities.
    For example, the wires of the preform 3 which have a lower titer have a titer which is less by a ratio of at least 1.5 compared to the other wires of the preform 3, in particular a ratio of around 2, 5 or 3, in the case of carbon threads. In a particularly preferred manner, the preform 3 contains wires 3K, which form the wires of lower title, and wires 6K, which form the wires of higher title.
    In general, the layers of warp threads 17 and weft threads 19 which are located near the layers C1 and T1, as well as these layers C1 and T1, have threads whose titer is lower than other threads the preform 3 located more at the heart, that is to say included in internal layers close to a median distance, parallel to the direction Z, between the surfaces 15 and 13. This variation in the titer of the wires of the preform 3 provides a particularly small thickness, especially near the thin edge 7 where the number of internal layers is reduced.
    In the example of FIG. 2, the thin part 23 comprises at least five layers of warp threads 17. Alternatively, the thin part 23 can comprise fewer or more layers of warp threads 17. In any event, the thin part 23 comprises at least three layers of warp threads 17.
    Preferably, the number of layers of weft threads 19 corresponds to the number of layers of warp threads 17. However, a number of layers of warp threads 17 may be lower or higher than that of the layers of weft threads 19, with a difference of one or more layers, depending in particular on the weaving weaves used. Some threads may be unbound, at least in part, but nevertheless trapped by the neighboring layers of thread.
    A plurality of warp threads 17 and / or weft threads 19 of the preform 3 preferably carrying a hardened polymer bringing a degree of cohesion to the preform 3, at least in the part 23, the thin edge 7 is preferably welded by means of this polymer carried by the wires.
    To make this preform 3, a manufacturing process is implemented comprising a step of multilayer weaving of the warp son layers 17 and the weft son layers 19, by distributing them according to the thickness of the preform 3. This step can be carried out using an automatic three-dimensional weaving machine, of the weaving loom type. The thick part 21 and the thin part 23 are thus produced, which is in the direction of the thin edge 7 of the preform 3. The weaving machine is programmed so that the preform includes the different layers of warp thread 17 and weft thread 19 above, linked and arranged as defined above.
    Preferably, once the weaving step has been carried out, the excess parts 20 are cut, as well as any non-woven threads. Optionally, all or part of the weft threads 19 of the second layer T2 is also woven in part 23 with a less interwoven weave than in part 21, as described above.
    FIG. 3 represents a second embodiment of a preform 30 according to the invention, similar to the preform 3 of FIGS. 1 and 2. The preform 30 has characteristics similar to those of the preform 3, which are designated on the Figure 3 by reference signs multiplied by 10 compared to the reference signs of Figures 1 and 2 associated with the corresponding characteristics.
    In this embodiment of FIG. 3, the preform 30 is made of a three-dimensional fibrous structure having a thickness, measured in the direction Z, and being woven in one piece by multilayer weaving of successive layers C10A, C10B, C20A, C20B, C30 and C40 of warp threads 170 and of successive layers T10A, T10B, T20A, T20B, T30 and T40 of weft threads 190 distributed according to the thickness. The preform 30 defines at least one thick part 210 and at least one thin part 230 extending the thick part towards a thin edge 70 of a blade 90 of the preform 30. The thin edge 70, not visible in FIG. 3 , is located outside of FIG. 3 to the right, as symbolized by an arrow 70. The blade 90 also includes an opposite base 80, not visible in FIG. 3, and symbolized by an arrow 80. The preform 30 comprises two first layers C10A and C10B of warp threads 170, the layer C10B being located immediately under the layer C10A, the two layers C10A and C10B forming an external group of successive layers. The preform 30 also comprises two successive layers C20A and C20B of warp threads 170, the layer C20A being located immediately under the layer C10B, forming another group of layers of warp threads. The preform 30 further comprises two first layers T10A and T10B of weft threads 190 forming a first group of layers of weft threads, which is external in the thick part 210. The layers T10A and T10B are linked, in this example, according to armor, respectively with layers C10A and C10B of warp threads 170.
    In this embodiment of FIG. 3, the number of layers of warp threads
    170 forming the thin part 230 is reduced compared to the number of layers of warp threads 170 forming the thick part 210, due to the absence of the first two layers C10A and C10B of warp threads 170 in the thin part 230. Thus , the group formed by layers C20A and C20B of warp threads is external in the thin part 230. In addition, the first two layers T10A and T10B of weft threads 190 extend as far as the thin part 230, being linked according to an armor, respectively with the layers C20A and C20B of warp threads 170 in the thin part 230, so as to form an external group of successive warp threads also in the thin part 230. At a junction 250 between the thick part 210 and thin part 230, the excess parts 200 of the weft threads 190 of two successive layers T20A and T20B have been cut, the layer T20A being situated immediately under the layer T10B, and the layer T20B immediately s or the T20A layer. The layers T20A and T20B form a second group of successive layers of weft yarns 190.
    If in the aforementioned examples, the preforms 3 and 30 are used in the production of a stiffener 1, such preforms can also be used in the production of any other part, preferably for a framework, the part being produced in a composite material including the preform and having a thin edge. For example, this part is used within the framework of a land, naval or air vehicle, or of a building.
    Armor different from that shown in the figures can be used.
    The characteristics of each embodiment or variant described above can be incorporated into any embodiment or variant described above, provided that this is technically possible. In particular, the same preform may include both junctions similar to that of junction 25 of FIG. 2 and junctions similar to junction 250 of FIG. 3, in particular for the purpose of creating curvatures for the surfaces of the blade of a preform.
    权利要求:
    Claims (12)
    [1" id="c-fr-0001]
    1. - Preform (3; 30), in particular of stiffener (1), in three-dimensional fibrous structure having a thickness (Z) and being woven in one piece by multi-layer weaving of warp son layers (17; 170) and of weft son layers (19; 190) distributed according to the thickness, the preform defining at least a first part (21; 210) and at least a second part (23; 230) extending the first part towards an edge thin (7; 70) of the preform, the preform comprising:
    a first group (C1; C10A, C10B) of successive warp yarn layers, which includes at least one layer of warp yarns and which is external in the first part,
    a second group (C2; C20A, C20B) of successive chain son layers, which includes at least one layer of warp son and which is located immediately below the first group of chain son layers, and
    a first group (T1; T10A, T10B) of successive weft yarn layers, which includes at least one weft yarn layer and which is linked in an armor with the first group of warp yarn layers, so as to be external in the first part, the preform being characterized in that:
    - the number of layers of warp threads (17; 170) forming the second part (23; 230) is reduced compared to the number of layers of warp threads forming the first part (21; 210), due to a absence of the first group (C1; C10A, C10B) of warp layers in the second part, so that the second part has a thickness (Z) reduced compared to that of the first part and so that the second group (C2; C20A, C20B) of layers of warp thread is external in the second part, and
    - the first group (T1; T10A, T10B) of weft yarn layers (19; 190) extends into the second part, being linked in a weave with the second group of warp yarn layers in the second part, so that the first group of weft thread layers is external also in the second part.
    [2" id="c-fr-0002]
    2. - Preform (3; 30) according to claim 1, characterized in that the preform comprises a second group (T2; T20A, T20B) of successive weft son layers (19; 190), which includes at least one layer of weft threads and which is located immediately below the first group (T1; T10A, T10B) of layers of weft threads in the first part (21; 210), the second group of layers of weft threads being absent from the second part (23; 230), for example by interrupting the weft threads of this second layer of weft threads, at a junction (25; 250) of the first part (21; 210) with the second part (23; 230) .
    [3" id="c-fr-0003]
    3, - Preform (3; 30) according to any one of claims 1 or 2, characterized in that the weft threads (19; 190) of the first group (T1; T10A, T10B) of weft thread layers have a title lower than the title of the weft yarns of the second group (T2; T20A, T20B) of weft yarn layers.
    [4" id="c-fr-0004]
    4, - Preform (3; 30) according to any one of claims 1 to 3, characterized in that the warp threads (17; 170) of the first group (C1; C10A, C10B) of layers of warp threads have a title lower than the title of the warp yarns of the second group (C2; C20A, C20B) of layers of warp yarns.
    [5" id="c-fr-0005]
    5, - Preform (3; 30) according to claim 4, characterized in that the preform contains 6K wires and 3K wires.
    [6" id="c-fr-0006]
    6, - Preform (3; 30) according to any one of the preceding claims, characterized in that the second part (23; 230) comprises at least three layers of warp son (17; 170).
    [7" id="c-fr-0007]
    7, - Preform (3; 30) according to any one of the preceding claims, characterized in that:
    the preform comprises a third part extending the second part (23; 230) in the direction of the thin edge (7; 70),
    - the preform comprises a third group (C3; C30) of successive warp son layers (17; 170), which includes at least one warp son layer and which is located immediately below the second group of layers (C2; C20A , C20B) of warp threads in the second part,
    - the number of layers of warp yarns forming the third part is reduced compared to the number of layers of warp yarns forming the second part (23; 230), due to the absence of the second group of layers of warp yarns in the third part, so that the third part has a thickness (Z) reduced compared to that of the second part and so that the third group of layers of warp threads is external in the third part, and
    - the first group (T1; T10A, T10B) of weft yarn layers (19; 190) extends into the third part, being linked in a weave with the third group of warp yarn layers in the third part, so that the first group of weft thread layers is external also in the third part.
    [8" id="c-fr-0008]
    8. - Preform (3; 30) according to any one of the preceding claims, characterized in that a plurality of warp threads (17; 170) and / or weft threads (19; 190) of the preform carries a hardened polymer bringing a degree of cohesion to the preform at least in the second part (23; 230).
    [9" id="c-fr-0009]
    9. - Preform (3; 30) according to claim 8, characterized in that the thin edge (7; 70) is welded by means of said cured polymer carried by the son.
    [10" id="c-fr-0010]
    10. - Frame part, in particular a stiffener (1), comprising a preform (3; 30) according to any one of the preceding claims, as well as a consolidation material (5), of the resin type, with which the fibrous structure of the preform is impregnated.
    [11" id="c-fr-0011]
    11. - Method of manufacturing a preform (3; 30), in particular of stiffener (1), in three-dimensional fibrous structure having a thickness (Z) and being woven in one piece, the manufacturing method comprising a step of multilayer weaving of layers of warp threads (17; 170) and layers of weft threads (19; 190) distributed according to the thickness, in which at least a first part (21; 210) and at least a second are defined part (23; 230) extending the first part towards a thin edge (7; 70) of the preform, so that the preform comprises:
    a first group (C1; C10A, C10B) of successive warp yarn layers, which includes at least one layer of warp yarns and which is external in the first part,
    a second group (C2; C20A, C20B) of successive chain son layers, which includes at least one layer of warp son and which is located immediately below the first group of chain son layers, and
    - A first group (T 1; T10A, T10B) of successive weft yarn layers, which includes at least one weft yarn layer and which is linked in an armor with the first group of warp yarn layers, so to be external in the first part, the method being characterized in that, to form the second part (23; 230):
    - the number of layers of warp yarns (17; 170) in the second part is reduced relative to the number of layers of warp yarns forming the first part (21; 210), this reduction being obtained by absence of the first group ( C1; C10A, C10B) of warp layers in the second part, so that the second part has a thickness (Z) reduced compared to that of the first part, and so that the second group (C2; C20A , C20B) of layers of warp yarn is external in the second part, and
    - the first group (T1; T10A, T10B) of weft son layers (19; 190) is linked, according to a weave, with the second group (C2; C20A, C20B) of warp son layers (17; 170 ) in the second part, so that the first group of weft thread layers is external also in the second part.
    [12" id="c-fr-0012]
    12, - Manufacturing process according to claim 11, characterized in that:
    - the preform (3; 30) comprises a second group (T2; T20A, T20B) of weft son layers (19; 190), which includes at least one layer of weft son and which is located immediately under the first group (T1; T10A, T10B) of weft son layers in the first part (21; 210),
    - at the second part (23; 230), an excess part (20; 200) of the weft threads of the second group of layers of weft threads is removed from the fibrous structure, and
    - the excess part is cut.
    1/3
    NOT
    2/3
    ΓΤ pu lt ”> o
    Vj Vj Vj Vj Vj tu
    3/3 t
    δ you
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    同族专利:
    公开号 | 公开日
    US11173633B2|2021-11-16|
    US20190224885A1|2019-07-25|
    CN109843565A|2019-06-04|
    EP3507085A1|2019-07-10|
    ES2826723T3|2021-05-19|
    PT3507085T|2020-11-03|
    WO2018041992A1|2018-03-08|
    EP3507085B1|2020-07-29|
    FR3055569B1|2019-11-22|
    CN109843565B|2021-04-13|
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    WO2013088038A2|2011-12-14|2013-06-20|Snecma|Fiber structure intended to reinforce composite material parts and including a portion having a reduced thickness|CN113365802A|2019-01-30|2021-09-07|赛峰航空器发动机|Shell made of composite material with local thickness variation|US6972144B2|2002-04-19|2005-12-06|Hunter Paine Enterprises, Llc|Composite structural material and method of making same|
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    法律状态:
    2017-08-24| PLFP| Fee payment|Year of fee payment: 2 |
    2018-03-09| PLSC| Publication of the preliminary search report|Effective date: 20180309 |
    2018-08-24| PLFP| Fee payment|Year of fee payment: 3 |
    2019-08-22| PLFP| Fee payment|Year of fee payment: 4 |
    2020-08-12| PLFP| Fee payment|Year of fee payment: 5 |
    2021-08-11| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1658182A|FR3055569B1|2016-09-02|2016-09-02|PREFORM, CORRECTION PIECE AND METHOD OF MANUFACTURING SUCH A PREFORM|
    FR1658182|2016-09-02|FR1658182A| FR3055569B1|2016-09-02|2016-09-02|PREFORM, CORRECTION PIECE AND METHOD OF MANUFACTURING SUCH A PREFORM|
    ES17765118T| ES2826723T3|2016-09-02|2017-09-01|Preform, frame part and manufacturing process of said preform|
    US16/329,822| US11173633B2|2016-09-02|2017-09-01|Preform, framework part, and method for producing such a preform|
    EP17765118.9A| EP3507085B1|2016-09-02|2017-09-01|Preform, framework part, and method for producing such a preform|
    CN201780065173.3A| CN109843565B|2016-09-02|2017-09-01|Preform, frame part and method for producing such a preform|
    PCT/EP2017/071949| WO2018041992A1|2016-09-02|2017-09-01|Preform, framework part, and method for producing such a preform|
    PT177651189T| PT3507085T|2016-09-02|2017-09-01|Preform, framework part, and method for producing such a preform|
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