• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
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    • 专利摘要:
    The present invention relates to a method of manufacturing a piece of organic matrix composite material and fibrous reinforcement, the method comprising the following steps: - draping automatically, respectively flat or shaped on a three-dimensional footprint, at least one stratification (30, 31) having at least first and second dry plies, different, at least partially superimposed, so as to form a dry preform, respectively flat or three-dimensional, each ply being fibrous, the plies differing from each other by the structure , the positioning on the preform, the fibers constituting them and / or the geometry of the fold, - thermoforming the preform, the thermoforming taking place when it was draped flat in step a) in a three-dimensional print of a first mold to give it a three-dimensional shape, - impregnate in a mold the preform and thermoformed by at least one polymer , the preform being moved in the case of flat draping in step a) of the first thermoforming mold to a second mold for impregnation.
    公开号:FR3052699A1
    申请号:FR1655722
    申请日:2016-06-20
    公开日:2017-12-22
    发明作者:Matthieu Kneveler；Charles Leroux；Laurent Rota
    申请人:Institut de Recherche Technologique Jules Verne；
    IPC主号:
    专利说明:

    A process for manufacturing a composite material part, a steering column support and a lower crossmember made using such a method
    Field of the invention
    The present invention relates to a method of manufacturing a composite material part with organic matrix and fibrous reinforcement, in particular but not exclusively in the automotive or aeronautical field. The invention also relates to a steering column support and a lower berry rail made in particular using such a manufacturing method.
    Prior art
    In the automotive industry, many parts are made of metal, and is currently seeking to substitute the organic matrix composite material to the metal, in particular to reduce the weight and therefore the fuel consumption of the vehicle or improve the longevity of the batteries in the case of a vehicle with hybrid or electric drive. It is necessary for this purpose that the mechanical performance obtained be comparable, the production rates are high enough to be implemented on an automotive production line and the overall cost is comparatively acceptable or even favorable.
    WO 2013/182521 discloses the replacement of a metal tubular cross member by a fiber composite cross member. Such a crossbar requires a large amount of composite material to obtain the same mechanical properties as the metal cross, which increases the manufacturing costs, weight and volume of the assembly. WO 2015/090989 relates to a dashboard crossmember for a motor vehicle associated with two lateral supports, the crossmember comprising a tube of which at least a part is made of composite plastic material and one of the lateral supports is made of composite plastic, said material composite plastic being reinforced by one or more metal plates bonded to this plastic material by overmolding or gluing. FR 3,014,401 discloses a front apron for a motor vehicle body for separating the engine compartment and the passenger compartment, consisting of the assembly together of a plurality of monolithic unitary parts each formed in a composite material based on a mixture between a reinforcement and a matrix. EP 2 716 527 discloses a device for fixing the steering column of a motor vehicle to the dashboard cross member and to a part of the structure of the vehicle body.
    Also known from FR 2 995 862 a dashboard crossmember for a motor vehicle consists of two tubes axially connected to one another and a strut extending in a direction transverse to the cross, the tubes and the strut being made of composite material. Other patent documents describe composite materials used at least partially for the production of automobile parts such as dashboard, crossbar for dashboard, dashboard, front apron, among which EP 2 597 017, FR 2 975 961 , EP 2 377 747, EP 2 332 809, EP 2 179 910, WO 2010/017254, EP 2 113 448, WO 2005/037632, WO 01/70558. Certain publications specifically describe support structures for a steering column, in particular JP 2015182736 or EP 2,896,545. US Pat. No. 8,623,159 discloses a method comprising the flat embodiment of a preform comprising foam cores.
    Furthermore, in the field of manufacturing processes of parts from preforms, US 2014/0300138 teaches to produce a portion of automotive floor by assembling several dry preforms in a mold before impregnation by infusion of resin. This method of the prior art is difficult to automate and does not achieve economically a high production rate compatible with large series.
    Finally, processes are known for the manufacture of parts based on composite material, such as stamping, resulting in loss of material and requiring very expensive completion steps. This type of process, reserved for high-end parts and small series, is incompatible with the cost constraints of manufacturing large series of parts.
    Despite all this known prior art, there is still a need to achieve achieving a complex piece of organic matrix composite material, at a relatively high production rate if desired and at a lower cost or comparable to that of a room metallic equivalent.
    There is still an interest in expanding the aesthetic possibilities when designing dashboards and reducing the number of parts to assemble in a motor vehicle, the assembly and assembly time of a motor vehicle and / or the volume of storage of prefoimes.
    In a first aspect, the subject of the invention is therefore a process for manufacturing a piece of organic matrix composite material and fiber reinforcement, comprising the following steps: - draper, preferably automatically, respectively flat or shaped on a three-dimensional footprint, at least one lamination comprising at least first and second plies, preferably different dry, at least partially superimposed, so as to form a preform, preferably dry, respectively flat or three-dimensional, each ply being fibrous, the plies differing from each other by the structure, the positioning on the preform, the fibers constituting them and / or the geometry of the ply, - thermoforming the preform, the thermoforming taking place when it has been draped flat in step a) in a three-dimensional imprint of a mold to give it a three-dimensional shape, - impressed In the mold, the preform is thermoformed by at least one polymer, the preform being moved in the case of flat layup in step a) of the first thermoforming mold to a second mold for impregnation.
    Thanks to the invention, there is provided a rapid manufacturing process, from a single preform, the automated draping process, for the production of complex composite parts, including large parts, for example from 5 to 8 m 2, or of complexity of form and / or structure, intended for the automotive, aeronautical or other industrial sector.
    The combination of said at least two different plies in the preform makes it possible to produce a complex preform in one piece, the mechanical characteristics of which are adapted to the subsequent stresses of the part.
    The lamination thus comprises a plurality of plies, at least two of which, at least some of which advantageously have different shapes, in particular of different dimensions, to be positioned at different locations of the preform. This can strengthen certain areas of the room, and / or adapt to a complex form thereof. Thus, the final piece may have reinforced areas compared to other areas. This may also make it possible to adapt or vary locally the elasticity properties or other mechanical properties such as rigidity and deformability, of different areas of the room according to the subsequent mechanical stresses of the piece thus manufactured. It is thus possible to obtain a part with relatively elastic or deformable zones and other rigid non-deformable zones. One can also play on the different nature of the fibers by mixing the glass and carbon fibers in some places depending on the mechanical constraints.
    The term "dry preform" denotes a fibrous preform comprising between about 1% and 20%, in particular less than about 5%, of a thermosetting or thermoplastic polymer, in weight percentage relative to the total mass of the preform. The dry preform is used as reinforcing phase of a composite material, the part corresponding to said preform being obtained by the impregnation, in particular the injection or the infusion, of a polymer in the liquid or pasty state in said dry preform.
    The term "dry fold" designates a fold of fibers impregnated with a small amount of a thermosetting or thermoplastic polymer, a quantity of between 1% and 20%, in particular less than 5% by weight relative to the total mass of the fold. The polymer present in a small amount may be sprinkled as a powder on the fold or may form a web between two fold layers or the like.
    Throughout the text, the term "fingerprint", unless otherwise indicated, refers to both a hollow form and a relief
    Each ply may have a structure selected from the group consisting of a linear structure, especially son or wicks, surface, including nonwovens, fabrics, ribbons or mats, or multidirectional, including braids, complex fabrics , multi-directional weaves, especially three-way or more.
    At least one fold can be arranged in the form of a nonwoven, also called in English Non-Crimp Fabrics (NCF). In this case, the fold comprises a plurality of layers of unidirectional fibers, arranged on each other with a different angular orientation of the fibers. The first and second plies may for example differ in the angular orientation of the layers they contain.
    Alternatively, at least one ply is woven.
    The folds are preferably deformable. The term "deformable fold" refers to a fold composed of continuous fibers arranged in defined directions and assembled in the form of fabric or nonwoven.
    The fibers constituting the plies may be chosen from the group consisting of carbon fibers, glass fibers, aramid fibers, ceramic fibers, polyester fibers, fibers of vegetable origin, especially linseed fibers, preferably the carbon or glass fibers, and a mixture thereof. The fibers can be continuous or short.
    An advantage of the invention is that it can make it possible to use NCF nonwoven fibers, which form a raw material at a lower cost compared with woven fibers. In addition, one can choose the orientation of the fibers for draping, which allows to control the mechanical properties of the room, or to have higher performance. In general, the draping step can be carried out by choosing the orientations of the fibers of the folds so as to obtain the target properties of the different parts of the workpiece.
    The method advantageously comprises a preliminary step of designing the part, so as to predetermine the choice of shape, fiber or fibers, positioning and geometry of each fold, depending on the desired mechanical characteristics for the part.
    The method may include a step of placing at least a portion of the lamination at least one core.
    The method may include the step of draping a second lamination having at least one ply, to at least partially cover the core and the lamination.
    In this case, there is a sandwich structure, for at least part of the room in which the core is present.
    By "sandwich structure" is meant a structure formed of a core or core of a first material, sandwiched between two outer layers of one or more other materials. The core may be light and have, in itself, weak mechanical characteristics, while the outer layers may have strong mechanical characteristics. The thickness of the core may be greater than about ten times the thickness of the outer layers.
    According to a first embodiment, the method according to the invention, for manufacturing a piece made of organic matrix composite material, comprises the following steps: - draping automatically at least one stratification comprising at least a first and a second dry plies different at least partially superimposed, each ply being fibrous, so as to form a dry preform flat, the plies differing from each other by the structure, the positioning on the preform, the fibers constituting them and / or the geometry of the ply - If necessary to assemble said at least two folds, in particular by at least one seam, - position the preform flat in a first mold, - thermoform the preform to give it a three-dimensional shape, - move the preform thus thermoformed in a second mold, impregnating the thermoformed preform with at least one polymer in the second mold in order to produce the part.
    According to a second embodiment, the method according to the invention, for manufacturing a piece made of composite organic matrix material, comprises the following steps: - drape on a three-dimensional non-planar imprint, at least one lamination comprising at least one first and second different plies, at least partially superimposed, each ply being fibrous, so as to form a three-dimensional dry preform, the plies differing from each other by the structure, the positioning on the preform, the fiber or fibers constituting them and / or the geometry of the fold, thermoforming the three-dimensional preform, impregnating the preform with at least one polymer in a mold in order to produce the part.
    Whatever the embodiment, the method may be as defined below.
    Thermoforming, or preforming, that the preform is flat or in three dimensions, can be performed on a single mold, with heating for example by radiant panel at a temperature less than or equal to about 100 ° C, the shaping taking place from preferably under low pressure, for example about 1 bar, which allows to obtain a fibrous structure that can be introduced into a mold for impregnation, for example injection. The mold may be metal such as aluminum or organic matrix composite material or resin.
    Thermoforming compresses the lamination to a final thickness. This operation makes it possible to close the mold for impregnation with the polymer (s).
    In the case of the thermoforming of the preform in three dimensions, this step can take place in the three-dimensional impression used for draping, in the mold used for impregnation or in another mold. The three-dimensional impression may form part of the mold for impregnation with the polymer (s). Alternatively, the preform may be moved from the three-dimensional impression or other mold to a second mold for the impregnation step.
    It should be noted that it is preferable that the mold for thermoforming is different from the mold for impregnation. Indeed, these types of molds are different, not working according to the same ranges of temperature and pressure. Molds for thermoforming are generally much lighter than molds for impregnation.
    The method advantageously comprises the step of consolidating the polymer (s) after the impregnation step, by solidifying the polymer (s) when it is a question of thermoplastic polymers or by baking the polymer (s) when it is is thermosetting polymers, and demolding the piece thus obtained.
    The method can be implemented in several places of the same manufacturing unit or several manufacturing units. It can also be implemented by chaining steps or spacing them, in time. For example, several preforms thermoformed can be made, stored in particular being stacked, and subsequently moved, one by one, in a mold for the impregnation step. The process according to the invention makes it possible, from an industrial point of view, to produce the preform and its impregnation of polymer in remote sites.
    When it occurs, the sewing step stabilizes the preform, maintaining the folds in their draping position, allowing to manipulate it without risk of decohesion or misalignment of the folds. The seam makes it possible to bind the folds without unduly hindering their ability to deform. The sewing is advantageously performed according to a predetermined contour, for example according to a folding contour of the preform. The seam can be made zigzag, so as to ensure the cohesion of the different folds of the preform without degrading the deformability of the preform that is conferred by the nature of the deposited folds. The sewing step can take place, when there is a sandwich structure, after the placement of the core (s) and the draping of the second lamination.
    When the draping is performed on a three-dimensional imprint, non-planar, a series of rollers may be provided in the tool to apply the draping on the imprint and gradually form the preform.
    When present, the core (s) may be of foam, in particular of polyethylene terephthalate (PET) foam, preferably molded. PET foam has several advantages including reduced cost, temperature resistance of 200 ° C, ability to be thermoformed, and the possibility of being recycled. The core or cores may be pierced with a plurality of orifices having a diameter of between 1 mm and 5 mm, in order to facilitate the impregnation, in particular injection or infusion, step of polymer through said nuclei.
    Still in this case, said at least one core advantageously has a total outer surface less than that of at least one of the plies so as to cover only certain predetermined areas of the lamination.
    At least one fold can be pre-cut before draping according to predetermined dimensions. Thus, it is possible to avoid losing material by generating waste material that is not used, thereby reducing costs and the quantity of waste. Indeed, in this case, the just needed amount of material is used. Another advantage of this pre-cutting is that it avoids or minimizes the finishing, that is to say the finishing steps of the part, such as deburring, trimming, recovery for drilling, etc., after consolidation of the polymer or polymers, these steps can be long and expensive. Thus, thanks to the invention, the manufacturing time can be reduced, all or part of these completion steps being avoided. Indeed, the piece obtained by the process is called definitive form, called "net-shape" in English, or almost definitive form, called "near net-shape" in English.
    Each ply may comprise a basis weight of between 100 gW and 50,000 g, in particular relatively large, for example greater than 3000 g. This reduces the duration of draping operations. The thickness of a fold can thus be between 0.3 mm and 5 mm, especially greater than 3 mm.
    At least one of the folds can play the role of reinforcement of certain areas of the preform.
    Said at least one polymer impregnating the preform may be chosen from thermosetting resins, such as unsaturated polyester resins, vinylester resins, epoxy resins, acrylic resins, phenolic resins, polyimide resins, bismaleimide resins, resins polystyrylpyridine, and thermoplastic resins such as polycarbonates, polyamides, especially aliphatic polyamides, such as polycaprolactam PA 6, polyhexamethylene adipamide PA 6.6.
    It should be noted that, thanks to the invention, it is possible to use materials, in particular one or more impregnating polymers of the preform, which is inexpensive. For example, thermosetting epoxy resins may be used which are less expensive than high performance thermoplastic resins, it being understood that they may, however, also be used. The step of impregnating the dry preform with a polymer can implement a method selected from the group consisting of resin transfer molding (RTM), light resin transfer molding (RTM Light), molding by high-pressure resin transfer (HP-RTM), thermoplastic resin transfer molding (T-RTM), resin transfer molding with Liquid Molding LCM (RTM / Liquid Compression Molding), thermo thermoplastic stamping, using the dry preform and a thermoplastic matrix in powder or plate form, compression-transfer molding and infusion molding.
    At least one of the draping steps is advantageously implemented by copying a tooling profile or by robot programming. When draping is implemented by copying, the robot is not programmed but follows a mark or profile on the tool. This makes it possible to quickly change the part reference, without having to modify a machine program. It is the tool itself that guides the trajectory of the robot.
    For the realization of possible holes required for fixing other parts, the method may comprise a step of drilling the preform using at least one needle before impregnation of the preform with the polymer. In this case, the impregnating mold may comprise at least one moving needle passing through the stratification (s), and possibly the core. Then, at the level of the bore, a barrel injection resin, pultruded or mechanical. In monolithic areas, the use of needles in the mold allows to make holes directly to the molding. In the case of a sandwich structure, it may be necessary to strengthen the hole. For this, a proposal consists in providing a local recess of the core material which will be filled with polymer to create a binder-bonding binder. It is also possible to equip the core or core material with pultruded drums which will perform the same function.
    Alternatively, one or more inserts, in particular metal or thermoplastic inserts, may be added to the preform.
    Thanks to the method according to the invention, it is possible to produce different parts intended for example for the automotive sector, in an automated manner, at a high rate, with a limited storage space. For example, it is possible to produce a part using the process described above, in a time of between about 2 minutes and 5 minutes, in particular in less than about 200 seconds, of which, for example, 90 seconds for producing the preform and 90 seconds for producing the preform. impregnating the preform with at least one polymer.
    Installation The invention also relates to an installation for implementing the method as defined above. Such an installation comprises, for example, at least one drape area, flat or shaped, a thermoforming zone or preforming and an impregnation zone using at least one polymer, for example by injection.
    Column support The invention further relates, in another of its aspects, independently or in combination with all or part of the foregoing, a steering column support for a motor vehicle, comprising a top part of composite matrix material organic, which may at least partially have a sandwich structure, configured to maintain the front steering column, and shaped to attach to the rear on the lower crossbeam of the vehicle. The upper portion advantageously at least partially a sandwich structure, so as to form a rigid zone ensuring the position of the steering wheel.
    The terms "front" and "rear", "downward" refer to a driver in the final vehicle sitting in the driver's seat facing the steering wheel. The "front" side is thus closest to the driver, while the "back" side is furthest from him, "downward" means a direction towards his feet.
    According to one embodiment, the support is carried out using the method as defined above, in particular comprising the flat layup step. In this case, the support is an example of a part made according to this method.
    The support may comprise, in addition to the upper part, a lower part of organic matrix composite material, extending downward and rearward the upper part and shaped to attach to the vehicle deck and carry the crankset of the vehicle. In this case, the lower part can be made with the upper part in monolithic form. The lower part may not be in the form of a sandwich structure, having no core (x) between the laminations. The lower part can be made to replace part of the deck of the vehicle and have a stiffness similar to that of a steel deck. It can be provided to deform in case of frontal impact.
    The support may comprise a strut, in particular metal, preferably steel, extending downwards between the upper part, at the front, and the apron of the vehicle or the lower part of the support. Such a strut, mechanically fixed to the upper part of the column support, is configured, when present, to take the exceptional forces at the steering wheel, ensure vibration rigidity and this strut is advantageously sized so as to flambé in the event of a frontal impact. The strut may alternatively be made of organic matrix composite material.
    The column support can be pre-assembled with the vehicle crankset and / or the steering column, before mounting in the vehicle.
    In another aspect of the invention, the invention further relates, independently or in combination with all or part of the foregoing, to a lower berry beam intended to extend over the entire width of the part. interior of a vehicle, made of a composite material with a polymer matrix, which may at least partially have a sandwich structure, made according to the method as defined above.
    To obtain such a piece, the method implemented may include draping on a three-dimensional footprint having the desired shape for the piece. The shape of the lower berry beam may be constrained by the double curvature shape of the windshield, which may prevent flat draping. The development of the lower berry beam is advantageously constant, which can make it possible to perform the draping automatically.
    The lower berry beam is advantageously intended to be fixed to the rear of the upper part of the steering column support as defined above.
    The lower berry beam advantageously has a sandwich structure in the area of attachment with the column support. Under this fixing area. the lower berry beam is advantageously extended by a portion, not sandwich structure, more flexible, which portion can bend in case of frontal impact.
    The invention further relates, in another of its aspects, independently or in combination with all or part of the above, to a steering column support assembly as defined above. upper and lower crossbar bay as defined above, intended to be mounted in a motor vehicle.
    In this case, the support can be pre-mounted with the pedal and / or the steering column before attachment to the bottom rail of the bay, or not. Motor vehicle The invention further relates, in another of its aspects, independently or in combination with all or part of the above, a motor vehicle comprising a steering column support as defined above and a lower rail of bay as defined above, secured together, the column support extending over only a portion of the length of the lower berry rail.
    The invention also relates to any part made using the method as described above, for the automotive, aeronautical, shipbuilding or other industrial sector. In particular, the part may consist of a composite spring leaf articulated for connection to the ground of a motor vehicle.
    Fi2ures The invention will be better understood on reading the following description, non-limiting examples of implementation thereof, and on examining the appended drawing, in which: FIG. schematically and in perspective an exemplary steering column support according to the invention, pre-assembled, - Figure 2 shows schematically and partially, in perspective, the pre-mounted column support of Figure 1 with a Beam lower cross member according to the invention, - Figure 3 shows schematically and partially in perspective, the column support assembly and cross bottom bay of Figure 2 mounted on the deck of a vehicle. FIG. 4 is a cross-section, schematically and partially, of an example of column support and lower rack crossmember according to the invention mounted together; FIG. 5 is a diagrammatic and partial representation of the column support and the FIG. 6 shows another example of column support and lower rack crossmember according to the invention after assembly; FIG. 7 shows the column support assembly and lower crossmember; Figure 8 shows the assembly of Figure 4 after a front impact, - Figures 9 to 12 show schematically and partially the method of manufacturing the column support of Figure 1 FIG. 13 represents the piercing step of the manufacturing process of the part, FIG. 14 schematically represents in perspective the preform after FIG. 13 is a diagrammatic and perspective view of the industrial plant for carrying out the process of FIGS. 9 to 12, FIG. 16 is an enlarged view of a portion of FIG. FIG. 17 is an isolated, diagrammatic and cross-sectional view of the lower crossmember according to the invention; FIGS. 18 to 21 diagrammatically show the various steps of the process; FIG. 22 shows the different stages of manufacture of the lower belly beam, schematically and in perspective, FIG. 23 is a diagrammatic representation of FIG. perspective, the draping tool used for the realization of the lower cross-bay, - Figure 24 represents, schematically and in perspective, the install for the implementation of the method of FIGS. 18 to 21, and FIG. 25 is an enlarged view of a portion of the installation of FIG. 24.
    FIG. 1 shows a steering column support 1 according to an exemplary embodiment of the invention, intended for a motor vehicle, on which the crankset P of the vehicle and the steering column C of the vehicle have been preassembled.
    The steering column support 1, in this example, is made of organic matrix composite material, according to the manufacturing method described hereinafter.
    The column support 1 comprises an upper portion 2 of organic matrix composite material having in this example at least partially a sandwich structure, configured to maintain the front 3 of the steering column C. As shown in Figure 2, the part upper 2 is also shaped to attach to the rear 4 on the lower crossbar bay 5 of the vehicle. In this example, the upper portion 2 is L-shaped with a relatively flat portion 6 extending from the front 3 to the rear 4 and a portion 7 extending rearwardly downwardly.
    The support 1 also comprises, in the extension of the portion 7, in this example, a lower portion 8 substantially shaped curved cross, arranged to carry the pedal, as shown in Figures 1 to 3. The lower portion 8 is realized made of organic matrix composite material not in the form of a sandwich structure but in the form of stacked lamination made monolithically with the upper part 2. This lower part 8 replaces in this example a part of the steel deck of the vehicle for which it is intended to to set and advantageously has a stiffness comparable to that of a steel deck.
    Also shown in the drawing a lower crosspiece bay 5 according to an exemplary embodiment, visible in Figures 2 and 3, fixed to the support 1. The bottom cross member 5 extends transversely across the width of the vehicle, has a double curvature shape matching that of the windshield of the vehicle. Fixing between the support 1 and the bottom crossbar 5 is advantageously by screwing and / or bonding.
    FIG. 3 represents, arranged in a vehicle V represented very partially, the assembly 10 formed by the support 1, preassembled in this example with the pedal P and the steering column C, and the lower rail of the bay 5. The whole is mounted on the deck T. It should be noted that the shape and mechanical properties of the lower cross member 5, whose shape is a hollow body, can dispense with a metal crossbar, which allows to imagine new dashboard designs.
    Moreover, compared to sets made from metal parts, the number of parts needed to perform the same functions is lower.
    The lower crosspiece 5 is made of an organic matrix composite material, in this example partially sandwich structure incorporating one or more cores over all or part of its length. As can be seen in FIG. 4, the lower rack beam 5 has a substantially hollow U-shaped cross-sectional shape throughout its length.
    As can also be seen in FIG. 4, the column support 1 comprises a strut 12, made at least partially in this example of a metallic material such as steel, fixed in this example on the one hand by an upper end 16, at the upper part 2 of the column support 1 via a fastening system 13 and secondly, by a lower end 17, to the lower part 8 of the column support 1.
    The lower part 8 is, in turn, fixed to the metal deck T of the vehicle as visible in particular in Figure 5.
    In this example, the lower rack crosspiece 5 has a sandwich structure attachment portion 15 which, at the rear 4 of the upper part 2 of the column support 1, forms the shape thereof. This fixing portion 15 is substantially vertical. The lower bay crossbar 5 further comprises a substantially horizontal upper portion 19, in the extension of the flat portion 6 of the upper portion 2, and a reinforced portion sandwich structure 22 extending rearwardly downwardly. under the windshield of the vehicle. Fixing and assembling between the different parts is done according to the arrows of Figure 5, by gluing and / or mechanical fastening, in particular by screwing.
    As illustrated in Figure 8, the strut 12 is configured to flare in the event of a frontal impact, and the lower portion 8 of the column support 1 is provided to deform as well.
    Another example of a support 1 and a lower crossbeam 5 has been illustrated in FIGS. 6 and 7. In this example, the lower crossbeam 5 comprises a single sandwich structure zone 25 extending under the support 1, which comprises only an upper portion 2 and a strut 12. In this example, the strut 12 is fixed by its upper end 16 to the fastening system 13 and its lower end 17 to the deck T. Similarly, the lower rail 5 is fixed to the support 1 and the apron T as visible in FIG.
    FIGS. 9 to 14 show the various steps of the process for manufacturing a complex piece made of organic matrix composite material, presenting in this example at least partially a sandwich structure, such as the illustrated column support 1 in Figures 1 to 3.
    In FIG. 9, a flat layup step a) is shown of a lamination comprising a first deformable dry ply of rectangular shape with predetermined dimensions. Step b) also illustrated in Figure 9 is to drape flat a second crease 31 deformable dry with several pieces of predetermined dimensions and positioning and corresponding to the desired shape. As visible, the second fold 31 covers only partially the first fold 30 and the orientation and shape of the pieces is different from it. The second ply 31 may be identical in nature and weight to the first ply 30, depending for example on the desired mechanical properties. The lamination is, for example, maintained on the table of the vacuum draper. Step c) consists in placing a polyethylene terephthalate foam core 32 on a predetermined part of the surface of the lamination constituted by the folds 30 and 31. The core (s) 32 may be glued to the lamination.
    It is not beyond the scope of the invention if the core is not PET foam or if there is no core. Any other material suitable for the process may be used, including a metal insert, for example made from shaped sheets and / or foundry, so as to have a function suitable for the application; damping material, resistance, sound or thermal insulation, conductive or insulating material for example. Step d) which follows consists of draping a second laminate flat again comprising a deformable dry fold 33 corresponding to the fold 31, at least for the form.
    In a step e), a crushable dry ply 34, identical at least for the shape to the ply 30, is draped flat, forming with the ply 33 the second lamination. The relative flexibility of the core does not hinder the draping of these folds 33 and 34. According to an alternative embodiment, the folds 33 and 34 constituting the second lamination are stabilized on the preform by the thermal activation of a polymer, for example a thermoplastic polymer, powdered on said plies, or by glue spraying. At this step e), it is clearly visible that one part, in this case the upper part 2 of the column support 1 is made in the form of a sandwich structure while the other, namely the lower part 8 of the support 1 column, is made monolithically with the upper part 2 but devoid of core and therefore sandwich structure.
    The folds 30, 31, 33 and 34 are advantageously, in this example, non-woven folds of NCF, of grammage chosen so as to obtain the desired rigidity without multiplying the number of folds required. For example, a fold of NCF, used for producing the column support 1 or for any other part made according to the process according to the invention, comprises a first layer of carbon fibers oriented at + 45 °, a second layer of fibers 0 ° oriented aramid, a third layer of carbon fibers oriented at -45 ° without this example being limiting or exhaustive Thus, the nature of the draped fibers is adapted to meet the needs of mechanical strength vis-à-vis solicitations during the use of the part produced and the needs in situations of exceptional stress, such as in the presence of shock or penetration of a foreign body. It is not beyond the scope of the invention if the preform comprises for example glass fibers, carbon, kevlar or natural fibers, among others.
    In a step f), at least one seam of the pleats is made so as to hold the two laminates together. The seam 35, preferably made in a zigzag fashion, may follow the contour of the nucleus (s) so as to enable the stratifications to be separated on either side of the nucleus (s) by reinforcing this separation zone with respect to the peel. Alternatively or additionally, the seam 35 may constitute one or more fold lines of the preform. The location of the seam 35 is determined for example by experience or simulation. Sewing can be done by a sewing system binding the folds together to fix their position. Such a system may be two-needle or a curved needle. In both cases, there is a buffer zone under the preform capable of accommodating the needles. The speed of realization of the seam can be about 1400 points / min, about 10 cm / s.
    In an alternative embodiment not shown, the seam or most stressed are covered by unidirectional fiber strips, for example carbon fibers to strengthen them. The fibers of said strips are oriented substantially parallel to the general direction of progression of the seams they cover.
    A flat dry preform 36 is then obtained. As illustrated in FIG. 10, the flat dry preform 36 obtained in step f) is moved into a three-dimensional cavity E of a mold and a radiant panel R is heated at temperature. about 100 ° C, so that, as illustrated in Figure 11, the preform matches the shape of the footprint E.
    The thermoformed preform 37 thus obtained is then moved into a second mold, not visible in the figures, in which it is impregnated with at least one polymer in order to produce the part, visible in FIG. 12, constituting in this example the support 1 previously described. The impregnation step may, in a manner known per se, consist of a material injection molding step, of RTM resin transfer molding type, light resin transfer molding (RTM light), high pressure HP-RTM molding. by thermoplastic resin transfer T-RTM or other. The molding may also be of the transfer-compression type, for example using one or more thermoplastic polymers made of sheet or powder, or of another type, comprising, for example, an infusion step.
    The polymer used for the impregnation may be a thermosetting or thermoplastic resin.
    According to a non-illustrated embodiment, the second mold comprises two parts and sealing means so that, when the mold is closed, said two parts define a sealed cavity in which the dry preform is located. The mold comprises vacuum drawing means of said cavity, and according to an exemplary embodiment, means for heating each part of the mold. According to different exemplary embodiments, the heating of the two parts of the mold is achieved by the circulation of a fluid, by electrical resistances or by induction. The preform being drawn by vacuum into the cavity of the mold, channels make it possible to inject a polymer into the preform, so as to impregnate it. This injection is carried out at a temperature adapted to the polymer used. The injection may be carried out under high pressure, for example about 30 bar, and at high temperature, especially between 120 ° C and 180 ° C. The mold may be metallic, in particular steel. According to an exemplary embodiment, polymers of different types are injected into the upper part and into the lower part of the mold and / or into specific areas of the upper and / or lower parts, so as to confer properties adapted to the part in question. depending on the modes of solicitation it undergoes.
    After consolidation of the piece 1 by the solidification of the polymer when it is a thermoplastic polymer or by baking the polymer when it is a thermosetting polymer, the part 1 is demolded. A simple deburring, not a machining, can be done to finish the piece 1.
    With such a method, the production rate of a part can be lower, in cumulative time, to 200 s, the draping and impregnation steps, including injection, each requiring 90 s.
    FIGS. 13 and 14 show a step for drilling the preform that can take place during the manufacture thereof. The mold M comprises a movable needle A which is inserted through the folds 30 and 34 and possibly the core 32 as visible. During the injection of material, the impregnating polymer forming the matrix 41 of the part 1 also creates a fut 40 surrounding the drilling. 14 shows the drilling locations 42 provided in the part 1 and may, in another embodiment, be made by placing metal inserts, pre-existing in the material or the cores.
    An installation D for carrying out the process of FIGS. 9 to 14 has been illustrated in FIGS. 15 and 16. In FIG. 15, a first flat layup zone 45, a second preforming zone 46 or thermoforming zone are shown. and finally a third impregnation zone 47 with a polymer, for example an injection polymer. The flat layup zone 45 is more visible in FIG. 16, illustrating in particular the fact that four preforms can be produced, in particular draped, simultaneously with this installation D, thanks to the use in this example of an injection press 300t.
    An RI robot lays flat lay automatically. A second robot R2 visible in FIG. 15 makes it possible to move the preforms flat in the second zone 46, for example by a gripper, needle or vacuum effector, preferably with needles.
    In the third zone 47, in addition to a robot R3 arranged for the displacement of the thermoformed preforms towards the third zone 47, a tooling O including the mold for the impregnation, in particular by injection, of polymer in the preform has been represented. In this example, the tooling is an injection device such as a press. In Figure 17, there is shown separately the bottom cross member 5, in cross section. It has a hollow form, open section. The sandwich structure makes it possible to impart stiffness to the workpiece by choosing the carbon fibers for the most stressed parts or parts and the glass fibers for the least stressed parts or parts.
    The manufacturing method thereof has been illustrated in Figures 18 to 23. In Figure 18, there is shown a step 1) of draping shaped on a footprint E 'having a three-dimensional surface. The draping is carried out automatically using small rollers S draping little by little and in the form of a lamination comprising in this example a first crease 51 dry deformable NCF. In step m), second plies 52, constituting reinforcements, are positioned on certain areas of the first ply 51. These plies 52 are made for example of carbon fiber woven fabric.
    Then, in step n), cores 53, two in number in this example, are positioned on a part of the first lamination 51, in this case on the folds 52. In step o), a second lamination 54, comprising in this example a deformable dry fold of NCF, is performed automatically using the rollers S. It should be noted that the folds 52 have previously been also deposited above the cores 53, as visible at this stage o).
    A preforming step, or thermoforming, under low pressure, of the order of 1 bar, and at a low temperature, less than 100 ° C., is carried out after step o), in a simple mold, for example in aluminum or composite material with organic matrix, or resin, or other.
    The three-dimensional preform 55 obtained is visible in perspective in FIG. 19. The preform 1 is moved into another mold where, as shown in FIG. 20, a counter-mold M 'is disposed on the preform 55. At the illustrated step in Figure 21, a thermosetting resin is injected into the mold so as to impregnate the preform 55 with a polymer. After consolidation, in this example by baking the resin, the part can be demolded.
    It should be noted that the characteristics described above for the preform, the materials used, the steps of the method as well as the tooling, with reference to FIGS. 9 to 12, even if not repeated in the description, may be identical, at least for part of them, to those of the preform, materials, tools, steps of the process of Figures 18 to 21.
    FIG. 22 illustrates the same steps as those illustrated in FIG. 18, although the part is viewed in perspective. We see the draping tool then the draping step in the form of the first fold 51 and the laying of the second folds 52 and the addition of the cores 53 and finally the draping in the form of a second stratification with the folds 52 and 54 .
    An example of tooling that can be used for the form layup is shown in FIG. 23. For draping this complex shape, an automatic draping is preferably used by indexing the lateral displacement of the rolls of fabrics in a groove of the tooling, adapted profile, rather than programming the robot. This simplifies the programming of the means and the part reference change process. The overall installation illustrated in FIG. 24 makes it possible to simultaneously produce two preforms of lower bay cross-section. The drape zone 60 is juxtaposed with an injection zone 61, a robot R5 making it possible to move, with a gripping effector, the preforms produced by the tooling D.
    The method, the steps of which are illustrated in FIGS. 9 to 12 and 18 to 21, may be implemented for the production of parts other than a steering column support or a lower rack crossmember.
    In particular, such a method can enable the high-speed production of all complex parts made of organic matrix composite material that may comprise at least one part in a sandwich structure, whether they are intended for the automotive, aeronautical or other industrial sectors. .
    It should be noted that the steps of the method according to the invention for producing the preform (s) can be implemented independently of the final stage of impregnation with a polymer in order to produce the part. The dry preforms can be stored, stacked to reduce the storage area. The final step of the process can be carried out later after a lapse of time of for example from 1h up to one year. As a variant, all the steps of the method can be implemented successively, without delay, that is to say less than about 1 hour, in particular of the order of a few minutes maximum.
    权利要求:
    Claims (14)
    [1" id="c-fr-0001]
    1. A method of manufacturing a part (1; 5) of organic matrix composite material and fibrous reinforcement, the method comprising the following steps: drape automatically, respectively flat or shaped on a three-dimensional footprint (E ') at least one lamination (30, 31; 51, 52) having at least first and second dry plies, different, at least partially superimposed, so as to form a dry preform, respectively flat or three-dimensional, each ply being fibrous , the plies differing from each other by the structure, the positioning on the preform, the fibers constituting them and / or the geometry of the fold, thermoforming the preform, the thermoforming taking place when it was draped flat in step a ) in a three-dimensional impression of a first mold in order to give it a three-dimensional shape, impregnating a preform thus thermoformed with at least one polymer in a mold, the preform being moved in the case of flat draping in step a) of the first thermoforming mold to a second mold for impregnation.
    [2" id="c-fr-0002]
    2. A method of manufacturing a piece of organic matrix composite material, comprising the following steps: drape automatically flat at least one lamination comprising at least a first and second dry plies different at least partially superimposed, each ply being fibrous, so as to form a dry preform flat, the plies differing from each other by the structure, the positioning on the preform, the fibers constituting them and / or the geometry of the fold, if necessary to assemble said at least two folds, in particular by at least one seam, position the preform flat in a first mold, thermoform the preform to give it a three-dimensional shape, move the preform thus thermoformed in a second mold, impregnate the preform thermoformed with at least one polymer in the second mold in order to make the piece.
    [3" id="c-fr-0003]
    3. Method according to claim 1 or 2, each fold being in a structure selected from the group consisting of a linear structure, including son or wicks, surface, including non-woven fabric, fabrics, ribbons or mats. or multidirectional, especially braids, complex fabrics, multidirectional weaves, in particular tri-directional or more, at least one fold being preferably in the form of nonwoven (NCF), at least one ply preferably being pre-cut before layup according to predetermined dimensions.
    [4" id="c-fr-0004]
    4. Process according to any one of claims 1 to 3, the fibers constituting the plies being chosen from the group consisting of carbon fibers, glass fibers, aramid fibers, ceramic fibers, polyester fibers, fibers of vegetable origin, especially flax fibers, and a mixture thereof.
    [5" id="c-fr-0005]
    5. Method according to any one of the preceding claims, comprising a step of placing on at least a portion of the lamination at least one core, said at least one core (32; foam, especially polyethylene terephthalate (PET) foam, having a total outer surface less than that of at least one of the plies so as to cover only certain predetermined areas of the lamination (30, 31; 51, 52).
    [6" id="c-fr-0006]
    6. Method according to the preceding claim, comprising the step of draping a second lamination comprising at least one fold (33, 34; 52, 54) to cover at least partially the core and the lamination.
    [7" id="c-fr-0007]
    7. Process according to any one of the preceding claims, the polymer impregnating the preform being chosen from thermosetting resins, such as unsaturated polyester resins, vinylester resins, epoxy resins, acrylic resins, phenolic resins, polyimide resins, bismaleimide resins, polystyrylpyridine resins, and thermoplastic resins such as polycarbonates and polyamides.
    [8" id="c-fr-0008]
    8. A method according to any one of the preceding claims, the step of impregnating the preform with a polymer implementing a method selected from the group consisting of resin transfer molding (RTM), light resin transfer molding. (RTM Light), high-pressure resin transfer molding (HP-RTM), thermoplastic resin transfer molding (T-RTM), resin transfer molding with open-mold liquid resin deposition (RTM / Liquid Compression Molding LCM), thermoplastic thermo-stamping, compression-transfer molding and infusion molding.
    [9" id="c-fr-0009]
    9. Installation for implementing the method according to any one of claims 1 to 8, the installation comprising at least one drape zone (45; 60), flat or shaped, a thermoforming zone, and a impregnation zone (47; 61) using at least one polymer.
    [10" id="c-fr-0010]
    10. Support (1) for a steering column for a motor vehicle, comprising an upper part (2) of organic matrix composite material, configured to hold the steering column (C) at the front, and shaped to attach to the steering column. rearwardly on the lower bolster of the vehicle (5), the carrier (1) being preferably produced by means of the method according to any one of claims 1 to 8.
    [11" id="c-fr-0011]
    11. Column support according to claim 10, comprising a lower portion (8) of organic matrix composite material, extending downwardly and rearwardly the upper portion (2) and shaped to attach to the deck (T). of the vehicle and carry the pedal (P) of the vehicle, the lower part (8) being preferably made with the upper part (2) in monolithic form.
    [12" id="c-fr-0012]
    12. Support column according to any one of claims 10 and 11, comprising a strut (12), in particular metal, preferably steel, extending downwardly between the upper portion (2), the before, and the apron (T) of the vehicle.
    [13" id="c-fr-0013]
    13. Lower berry crossbar (5), intended to extend over the entire width of the inner part of a vehicle, made of a composite material with a polymer matrix, produced according to the method as defined in any one of the Claims 1 to 8, and preferably configured to be secured to the rear of the upper portion (2) of the steering column support (1) as defined in any one of Claims 10 to 12.
    [14" id="c-fr-0014]
    14. A motor vehicle (V) comprising a steering column support (1) as defined in any one of claims 10 to 12 and a lower rack beam (5) as defined in claim 13, secured together, the support (1) column extending over only a portion of the length of the lower bay rail (5).
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    同族专利:
    公开号 | 公开日
    EP3708348A1|2020-09-16|
    FR3052699B1|2019-08-16|
    WO2017220562A1|2017-12-28|
    EP3471948A1|2019-04-24|
    US20190232578A1|2019-08-01|
    US20200230897A1|2020-07-23|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE102011111743A1|2011-08-24|2013-02-28|Daimler Ag|Fiber-reinforced plastic-component i.e. control housing module, for use in internal combustion engine of motor vehicle, has molded rib structures connected with frame and made from milled fibers with reinforcement material|
    WO2015170016A1|2014-05-09|2015-11-12|Coriolis Composites|Method and machine for creating preforms by compactionless application of oriented fibers|
    DE19922799B4|1999-05-18|2014-06-12|Bayerische Motoren Werke Aktiengesellschaft|Process for producing a plastic molding|
    US6517744B1|1999-11-16|2003-02-11|Jsr Corporation|Curing composition for forming a heat-conductive sheet, heat-conductive sheet, production thereof and heat sink structure|
    FR2806366B1|2000-03-20|2002-07-26|Valeo Climatisation|STRUCTURING TRANSVERSE BEAM AND METHOD OF MAKING|
    EP1675766B1|2003-10-14|2007-09-19|Behr GmbH & Co. KG|Composite part, especially cross member|
    WO2009006163A2|2007-06-29|2009-01-08|Itt Manufacturing Enterprises, Inc.|Thermally conductive structural composite material and method|
    DE102007057110B4|2007-11-26|2012-12-13|Eurocopter Deutschland Gmbh|Process for producing an endless, three-dimensional closed fiber composite semifinished product|
    DE102008021103B4|2008-04-28|2013-10-24|International Automotive Components Group Gmbh|Integrated composite component of a motor vehicle and method for producing an integrated composite component|
    WO2010017254A2|2008-08-08|2010-02-11|Dow Global Technologies Inc.|Integrated cockpit and front module assembly and method|
    US8424207B2|2008-10-27|2013-04-23|Honda Motor Co., Ltd.|Method of making a composite component and apparatus|
    FR2953795B1|2009-12-14|2011-11-25|Renault Sa|LOWER BAY TRAVERSE IN COMPOSITE MATERIAL|
    EP2377746A1|2010-04-15|2011-10-19|LANXESS Deutschland GmbH|Cross-member module for a motor vehicle|
    FR2975961B1|2011-06-06|2013-07-05|Peugeot Citroen Automobiles Sa|VEHICLE BOARD REINFORCING PART, IN PARTICULAR AUTOMOBILE AND REINFORCED REINFORCEMENT BOARD.|
    DE102011052513A1|2011-08-09|2013-02-14|Rehau Ag + Co.|Battery housing part for receiving a traction battery of an electric vehicle and method for producing the battery housing part|
    FR2983161B1|2011-11-24|2013-11-08|Rehau Sa|LIGHTWEIGHT COMPOSITE TUBULAR TRAVERSE FOR AUTOMOTIVE VEHICLE DASHBOARD.|
    DE102011089044A1|2011-12-19|2013-06-20|Bayerische Motoren Werke Aktiengesellschaft|Motor vehicle body with a rear floor and a cross member|
    FR2991656B1|2012-06-07|2014-06-20|Peugeot Citroen Automobiles Sa|FIBER COMPOSITE MATERIAL FOR VEHICLE DASHBOARD AND METHOD FOR MANUFACTURING THE SAME|
    FR2995862B1|2012-09-24|2014-09-19|Peugeot Citroen Automobiles Sa|AUTOMOTIVE VEHICLE DASHBOARD TRAVERSE CONSISTING OF TWO TUBES AND A FORCE LEG IN COMPOSITE MATERIAL|
    FR2996204B1|2012-10-03|2014-09-19|Peugeot Citroen Automobiles Sa|DEVICE FOR FASTENING THE STEERING COLUMN OF A MOTOR VEHICLE TO THE DASHBOARD TRAVERSE AND TO A PART OF THE STRUCTURE OF THE VEHICLE BOX|
    FR3014401B1|2013-12-10|2017-04-07|Renault Sas|FRONT APRON BY COMPOSITE PART ASSEMBLY|
    FR3014818B1|2013-12-18|2016-02-05|Peugeot Citroen Automobiles Sa|ASSEMBLY COMPRISING A DASHBOARD TRAILER FOR A MOTOR VEHICLE AND TWO SIDE MOUNTS FOR ATTACHING IT TO THE VEHICLE BODY|
    EP2896545A1|2014-01-17|2015-07-22|Ford Motor Company|Mounting structure for a steering column|
    JP2015182736A|2014-03-26|2015-10-22|フタバ産業株式会社|Support structure of steering column|
    WO2016003339A1|2014-07-03|2016-01-07|Saab Ab|A composite article having multifunctional properties and method for its manufacture|US11192595B2|2018-01-09|2021-12-07|Faurecia Emissions Control Technologies, Usa, Llc|Overmolded brackets for composite shock tower|
    KR20200072731A|2018-12-13|2020-06-23|현대자동차주식회사|Light Weight Cowl cross bar for vehicle|
    FR3089843B1|2018-12-14|2022-02-18|Centre Techn Ind Mecanique|Process for producing a composite part and implementation installation|
    CN111516761A|2020-04-20|2020-08-11|重庆长安汽车股份有限公司|Carbon fiber composite material automobile front floor, manufacturing method and automobile|
    法律状态:
    2017-05-30| PLFP| Fee payment|Year of fee payment: 2 |
    2017-12-22| PLSC| Search report ready|Effective date: 20171222 |
    2018-06-29| PLFP| Fee payment|Year of fee payment: 3 |
    2019-06-28| PLFP| Fee payment|Year of fee payment: 4 |
    2020-04-27| PLFP| Fee payment|Year of fee payment: 5 |
    2021-04-28| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1655722A|FR3052699B1|2016-06-20|2016-06-20|METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART, STEERING COLUMN BRACKET, AND LOWER BAY TRAVERSE PRODUCED BY SUCH A METHOD|
    FR1655722|2016-06-20|FR1655722A| FR3052699B1|2016-06-20|2016-06-20|METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART, STEERING COLUMN BRACKET, AND LOWER BAY TRAVERSE PRODUCED BY SUCH A METHOD|
    EP17730212.2A| EP3471948A1|2016-06-20|2017-06-20|Method for producing a composite material part, steering column support member and lower space cross member produced by such a method|
    PCT/EP2017/065061| WO2017220562A1|2016-06-20|2017-06-20|Method for producing a composite material part, steering column support member and lower space cross member produced by such a method|
    US16/312,116| US20190232578A1|2016-06-20|2017-06-20|Method for producing a composite material part, steering column support and lower space cross member produced by such a method|
    EP20160344.6A| EP3708348A1|2016-06-20|2017-06-20|Method for manufacturing a part made of a composite material with organic matrix and fibrous reinforcement for battery|
    US16/840,965| US20200230897A1|2016-06-20|2020-04-06|Method for producing a composite material part, steering column support and lower space cross member produced by such a method|
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