法国专利FR3039554A1 PROCESS FOR FIBROUS MATERIAL PRE-IMPREGNATED WITH A THERMOPLASTIC POLYMER USING A LIQUID CRYSTAL POL

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专利摘要:
The present invention relates to a preimpregnated fibrous material, in particular in ribbon form, comprising a fibrous reinforcement, impregnated with a thermoplastic polymer matrix, said preimpregnated fibrous material comprising in its composition: a) a thermoplastic matrix polymer, if amorphous having a Tg> 40 ° C and if semi-crystalline having a Tf> 150 ° C, b) a fibrous reinforcement, c) at least one liquid crystal polymer as an additive at a level ranging from 0.1 to 50% by weight. weight with respect to said polymer a), said additive being able to be premixed with said polymer a) and dispersed in said polymer matrix and d) optionally, carbon charges dispersed in said matrix homogeneously and uniformly. The invention also relates to a specific method for preparing said material, in particular in the form of a calibrated ribbon for use in the manufacture of composite materials.
公开号:FR3039554A1
申请号:FR1557259
申请日:2015-07-29
公开日:2017-02-03
发明作者:Gilles Hochstetter；Patrice Gaillard；Thibaut Savart；Axel Salinier
申请人:Arkema France SA；
IPC主号:

专利说明:

The present invention relates to a pre-impregnated fibrous material, in particular in ribbon form, comprising a fibrous reinforcement, impregnated with a thermoplastic polymer matrix, comprising at least one liquid crystal polymer as an implementation additive and optionally, carbon charges dispersed in said matrix homogeneously and uniformly. The invention also relates to a specific method for preparing said material, in particular in the form of a calibrated ribbon for use in the manufacture of composite parts, in particular in 3D.
In this context, the present invention seeks in particular to improve the state of impregnation of the fibrous reinforcement by said thermoplastic polymer, in the case of semi-crystalline thermoplastic polymers having melting points (melting temperature Tf) greater than 200 ° C and more particularly higher than 250 ° C or thermoplastic polymers of high Tg (glass transition temperature) which have a high melt viscosity and make the high viscosity impregnation of the fibrous reinforcement very difficult and requiring processing temperatures much higher than the melting or softening point to reduce the viscosity but with the risk of thermal degradation of the polymer matrix with consequent loss of mechanical performance of said thermoplastic polymer matrix. On the other hand, it is excluded the use of solvents to reduce the viscosity of the polymer in the molten state during the impregnation stage for reasons of both safety (risk of explosion), health and environment (emission of hot solvent vapors) without considering the plasticizing effect of the residual solvent on the mechanical performance of the polymer matrix and therefore the performance of the final composite material. On the other hand, the solvent microbubbles that may be generated in the thermoplastic polymer matrix in the molten state by volatilization of the solvent are all defects in the structure of the final composite material. Therefore, the use of a solvent or a plasticizer being excluded, the question arises to find other alternative means not having these risks that reduce the viscosity of the thermoplastic matrix polymer in the molten state so to allow an efficient and homogeneous impregnation of the fibrous reinforcement without any negative effect on the final mechanical performance of the thermoplastic polymer matrix and consequently of the resulting composite material. The means proposed by the present invention is the use of a liquid crystal polymer as an additive of said thermoplastic polymer having these processing and viscosity difficulties for an effective and homogeneous impregnation of the fibrous reinforcement.
Then, the other joint objective of the present invention is the obtaining by a specific method of a pre-calibrated tape during its preparation, to the necessary width and in particular less than 100 mm of prepreg fibrous material suitable for the manufacture of composite parts in particular in 3D, without the need for splitting for the manufacture of composite parts in 3D, the tape being suitable for automatic removal by robot.
The manufacture of ribbons of small width, that is to say of width less than 100 mm, generally requires a slitting (that is to say a cut) of strips of width greater than 500 mm, also called tablecloths. The ribbons thus dimensioned are then taken back to be deposited by a robot using a head. In addition, rolls of webs not exceeding a length of about 1 km, ribbons obtained after cutting are generally not long enough to manufacture some large size material during the robot removal. The ribbons must therefore be roped to obtain a longer length, creating extra thicknesses. These extra thicknesses lead to the appearance of heterogeneities that are detrimental to obtaining good quality composite materials.
Indeed, the slitting of the strips of prepregs of greater width (band having a width much greater than 100 mm) leads to the destruction of fibers (less homogeneous performance at slitting points and splits of slit strips) as well as extra thicknesses. affecting the homogeneity of the mechanical performances of the composite parts. On the other hand, the dust generated by this slitting affect the proper functioning of the robots. Thus, additional problems and costs are generated in addition to the technical disadvantages mentioned. No. 5,070,157 and US 5,268,225 (US continuation of the first) describe self-reinforced composites based on a mixture of two liquid crystal polymers (LCP) which are aromatic polyesters, one of which serves as a thermoplastic matrix (TP) with a melting temperature Tf the lowest and the other as a reinforcing agent in the form of unidirectional long fibers created in situ and possibly another reinforcing agent. No. 5,070,157 describes in particular the mixture and US 5,268,225 the self-reinforced composite, including in the form of laminate formed of superimposed sheets of said mixture with processing temperature lower than the Tf of the LCP fibers and greater than the temperature of the polymer of the matrix . No fibrous substrate impregnation process with a mixture of thermoplastic polymer (TP) and liquid crystal polymers (LCP) is described. US 4,728,698 discloses self-reinforced composites from a blend of a conventional flexible-chain thermoplastic polymer and a liquid crystal polymer (LCP) which is an aromatic copolyester, said mixture being homogeneous hot and after cooling allows the in situ creation of the unidirectional oriented fibers of the liquid crystal polymer dispersed in the thermoplastic matrix with mechanical performance being improved with respect to the LCP-free matrix in tensile and impact strength as an improvement in thermal withstand. There is no reference to a process of prepreg fibrous material based on fibers different from LCP and with the presence of LCP acting as a viscosity reducing agent during impregnation. WO 92/011311 discloses semi-finished products such as fabrics impregnated for composites exclusively based on two types of LCP of which one of the lowest Tf serves as a matrix and the other of higher Tf serves as fibrous reinforcement substituting the fibrous reinforcements based on conventional mineral or organic long fibers and at a rate of 20-70% by volume of the finished product. The polymer of the matrix may be in various forms with respect to the LCP reinforcing fibers: in coating form (sheathing) of the highest Tf LCP fibers or in the form of fibers grouped with those of the LCP serving as fibrous reinforcement in the form of wicks woven. No use of other fibrous reinforcement is described nor the use of a LCP polymer as a support agent for the implementation of a thermoplastic polymer, which is not a LCP polymer. The article "Polymer Composites, February 1990, No. 1, p. 10-18 "describes a fast method of composite structure formation using the in situ formation of LCP fibers in a TP thermoplastic matrix which is polystyrene, by a method of" spinning "(spinning) under high shear fibers composites resulting from a melt blend of TP thermoplastic polymer and a LCP polymer which is a polyester-amide aromatic copolymer. A single screw extruder is used for the manufacture of composite fibers. Fibrils are formed in situ in the TP matrix during this "spinning" process. The composite fibers are then aligned to form a fabric in a mold and heated to fuse the TP thermoplastic matrix without melting the fibrils at a lower temperature than the fusion of LCP fibrils. The composite part thus obtained is reinforced by the presence of said LCP polymer fibrils. The fibrous reinforcement in this case is limited to the LCP fibrils generated in situ and no other additional fiber reinforcement is used and therefore the problem of impregnating the fibrous reinforcement other than LCP fibers does not arise as in the case of the present invention. .
In the case of the present invention, the LCP polymer serves as an agent for processing the thermoplastic matrix polymer of the composite material (fibrous prepreg) by lowering the viscosity of the thermoplastic polymer + LCP polymer mixture by the intimate mixture of thermoplastic polymer. (TP) and LCP polymer, in order to improve the efficiency and homogeneity of impregnation of the fibrous reinforcement in the form of roving for the manufacture of ribbons pre-calibrated in width, these ribbons being obtained by a specific method allowing ribbons calibrated with uniform and homogeneous performance, in particular a reduced porosity due to the better impregnation of the fibrous reinforcement and the specific calendering that follows this impregnation. These ribbons obtained in the form of coils longer than 1 km in width pre-calibrated according to the use and of uniform thickness are suitable for the manufacture of composite parts 2D and 3D, in particular 3D with automatic removal by robot.
The present invention firstly covers a specific prepreg fibrous material, in particular in the form of a ribbon.
Next, the invention covers a specific process for the preparation of said preimpregnated fibrous material and the use of such a method for the manufacture of calibrated ribbons suitable for the manufacture of 3D composite parts. The invention also covers a ribbon of preimpregnated fibrous material and a 3D composite part.
The first subject of the invention therefore relates to a preimpregnated fibrous material, in particular in ribbon form, comprising a fiber reinforcement (in particular) based on continuous fibers, impregnated with a thermoplastic polymer matrix and comprising in its composition a) a thermoplastic polymer forming said thermoplastic matrix with said polymer, if amorphous having a Tg> 40 ° C, preferably greater than 100 ° C and if semi-crystalline having a Tf> 150 ° C, preferably greater than 200 ° C, b) a fibrous reinforcement, c) as additive, at least one liquid crystal polymer at a level ranging from 0.1 to 50%, preferably from 0.2 to 20%, more preferably from 0.2 to 15%. %, even more preferably from 5 to 15% by weight with respect to said polymer a), said additive being able to be premixed with said polymer a) and dispersed in said polymer matrix, d) optionally, carbon charges, preferably nanofillers carbides dispersed in said matrix homogeneously and uniformly.
Said polymer a) is in particular selected from polyaryl ether ketones (PAEK), in particular polyether ether ketone (PEEK) or from polyaryl ether ketone ketones (PAEKK), in particular polyether ketone ketone (PEKK) or from polyetheretherketone aromatic imides (PEI) or polyaryl sulfones, in particular polyphenylene sulfones (PPS) or from polyarylsulfides, in particular polyphenylene sulfides, or from polyamides (PA) of high Tg, preferably of Tg> 100 ° C.
According to the present invention, said polymer a) may be a single polymer or a mixture of thermoplastic polymers as defined above for the polymer a). Therefore, the term "thermoplastic polymer a)" or "polymer a)" will mean in this application "a single" or "several polymers, that is to say a mixture of polymers".
With regard to said fibrous reinforcement b), it comprises or consists of continuous fibers selected from carbon, glass, silicon carbide, basalt, natural fibers fibers, in particular flax or hemp, sisal, silk or cellulosic and in particular viscose or thermoplastic fibers of Tg or Tf greater than the Tg or Tf of said respectively amorphous or semi-crystalline polymer or of a mixture of two or more of said fibers, preferably said fibrous reinforcement comprising or being made of carbon fibers, glass or silicon carbide or their mixture, in particular of carbon fibers. It is used as a wick (s).
According to the polymer volume ratio a) with respect to the fiber reinforcement b), it is possible to produce pre-impregnated materials known as "ready-to-use" or so-called "dry" prepreg materials.
In pre-impregnated materials known as "ready-to-use", the polymer a) (including a mixture of thermoplastic impregnating polymers) is distributed uniformly and homogeneously around the fibers. In this type of material, the thermoplastic polymer a) impregnating must be distributed as homogeneously as possible within the fibers to obtain a minimum of porosity, that is to say voids between the fibers. Indeed, the presence of porosities in this type of material can act as points of concentration of stress, during a stressing mechanical stress for example and which then form fracture initiation points of the fibrous material pre- impregnated and weakened mechanically. A homogeneous distribution of the polymer or polymer mixture thus improves the mechanical strength and the homogeneity of the composite material formed from these preimpregnated fibrous materials.
Thus, in the case of so-called "ready-to-use" pre-impregnated materials, the volume ratio of the polymer a) with respect to the fiber reinforcement b) varies from 40 to 250%, preferably from 45 to 125% and more. preferably 45 to 80%.
The so-called "dry" prepreg fibrous materials, meanwhile, comprise porosities between the fibers and a smaller amount of thermoplastic polymer a) impregnating which covers the surface fibers to hold them together. These "dry" prepreg materials are suitable for the manufacture of preforms for composite materials. These preforms can then be used to make the infusion of thermoplastic resin or thermosetting resin for example. The porosities in this case make it possible to facilitate the subsequent transport of the infused polymer resin within the preimpregnated fibrous material in order to improve the final properties of the composite material and in particular its mechanical cohesion. In this case, the presence of the thermoplastic polymer a) impregnating the so-called "dry" preimpregnated fibrous material makes it possible to make the infusion resin compatible.
Thus, in the case of so-called "dry" preimpregnated materials, the volume ratio of the polymer a) with respect to the fiber reinforcement b) advantageously varies from 0.2 to 15%, preferably from 0.2 to 10%, and more preferably between 0.2 and 5%. In this case, it is called "polymeric web", of low weight, deposited on the fibrous material to hold the fibers together.
Regarding said liquid crystal polymer c) (LCP), it may be selected from aromatic polyesters obtained by polycondensation of 4-hydroxy benzoic acid or of hydroxy naphthenic acid (6-hydroxy-naphthalene-2 carboxylic acid), copolyesters with based on two previous hydroxy acids or among aromatic copolyesteramides of similar structure. A known example of LCP aromatic copolyester is Vectran®. Preferably, said aromatic copolyesters based on hydroxy benzoic acid and naphthenic hydroxy have a content of hydroxy benzoic acid (hydroxy benzoate) around 70 to 75% by weight and 25-30% by weight of naphthenic hydroxy acid ( hydroxy naphthenate).
Liquid crystal polymers have a much lower viscosity than thermoplastic polymers a) whose viscosity is sought to be reduced. Therefore, the addition and intimate mixing of liquid crystal polymers c) (LCP) with said thermoplastic polymer a) first makes it possible to reduce the viscosity of the intimate mixture a) + c) with respect to a). Then, this addition and intimate mixture a) + c) makes it possible to adjust the viscosity of the polymer mixtures a) (in intimate mixture with c)) with carbon charges d) chosen from among the carbon nanofillers by adjusting the level of c ) (LCP). The choice of the nature of the polymer c) (LCP) is a function of the nature of the polymer a) of the thermoplastic matrix in order to optimize the compatibility between the polymer c) (LCP) and the polymer matrix a). The conditions of implementation by the intimate mixing of the polymer a) with the polymer c) (LCP) make it possible to obtain a polymer microstructure c) (LCP) / polymer a) of the matrix which promotes a significant reduction in viscosity with respect to the polymer a) alone and good impregnation of fibers of fiber reinforcement b) but also allow optimal dispersion in the case where said carbon charges d) are carbon nanofillers and more particularly carbon nanotubes. Indeed, the dispersion of said nanofillers in said polymer a) is already difficult because of the high initial viscosity of the polymer a) molten but this (dispersion) becomes even more difficult because of the significant increase in the viscosity of said polymer a) because of the very strong interactions with said nanofillers (because of their nanometric size, the interaction surfaces are larger and consequently the interactions are stronger, thus limiting the level of said nanofillers, dispersion homogeneity without significant reduction of the viscosity of the mixture). Consequently, the addition of said polymer c) (LCP) makes it possible, by reducing the viscosity, to better disperse said nanofillers, which act as reinforcing agents for the thermoplastic polymer matrix a) by interactions at the nanoscale.
According to a particular and preferred option of the invention, said polymer a) comprises carbon charges d), in particular among carbon black and carbon nanofillers and more particularly carbon nanofillers, preferably graphenes and / or nanotubes carbon and / or carbon nanofibrils, more preferably carbon nanotubes. More specifically, said polymer a) comprises said carbon charges d) pre-dispersed in said polymer a) before impregnation of said fibrous reinforcement b) and more particularly said carbon charges d) are dispersed in said polymer a), after intimately mixing said liquid crystal polymer c) (LCP) with said polymer a). The level of said carbon charges d) and preferably carbon nanofillers and more preferably carbon nanotubes (CNTs) may vary from 0.1 to 30% and preferably from 0.3 to 15% by weight relative to said polymer a) constituting the thermoplastic matrix.
Said intimate mixture a) + c) can be done for example in an extruder before mixing with the component c) and before impregnation of said fibrous reinforcement b) to obtain said fibrous material pre-impregnated according to the invention. The more precise method of preparing said preimpregnated fibrous material, in particular in the form of ribbon pre-calibrated in width, is described below according to the second subject of the invention.
This process for preparing the preimpregnated fibrous material, as defined above according to the invention, in particular in the form of a unidirectional ribbon, comprises at least the following step: i) impregnating said fibrous reinforcement, in the form of a single wick or several parallel wicks, by said polymer a) in the molten state and optionally said polymer a) comprising said component d), with said component c) being present in said polymer as a support agent for the implementation for reducing the melt viscosity of said polymer a).
According to a particular option of said method, said component d) is present in said polymer a) in the molten state during said impregnation step i), said component d) being uniformly and uniformly dispersed in said polymer a) fade after a preliminary step of intimately mixing said polymer with said component c).
Preferably, said method comprises, in addition to step i), the following additional steps: ii) shaping said wick or said parallel strands of said fibrous reinforcement impregnated according to step i), by calendering with at least one heating radiator this shaping being in the form of a single unidirectional ribbon calibrated or in the form of multiple unidirectional parallel ribbons calibrated, with in the latter case, said calender heating having multiple calendering grooves, preferably up to 200 calendering grooves, in conformity with the number of said ribbons and with a pressure between the rolls of said calender kept constant by a slave system, iii) winding said ribbon or said parallel ribbons on one or more reels in accordance with the number of said ribbons.
According to a particular option of said method, said impregnation step i) is completed by a step of covering said single wick or said parallel locks after impregnation by said polymer a) melted according to step i), by a molten polymer to ) may be identical or different from said polymer a) impregnating step i), before said calendering step ii), preferably said molten polymer a ') being of the same kind as said polymer a) impregnating the step i), preferably said covering being effected by extrusion at the head of square with respect to said single lock or with respect to said parallel locks.
In said process according to the invention, said fibrous reinforcement b) comprises or consists of continuous fibers selected from carbon, glass, silicon carbide, basalt, natural fibers fibers, in particular flax or hemp, of sisal, silk or from cellulosic fibers and in particular viscose fibers or thermoplastic fibers of Tg or Tf greater than the Tg or Tf of said respectively amorphous or semi-crystalline polymer or a mixture of two or more of said fibers , preferably carbon fibers, glass or silicon carbide or their mixture, in particular carbon fibers.
More particularly, in said method, said heating calender of step ii) is coupled to a rapid complementary heating system, in particular among microwaves or induction, coupled system (linked) to the presence of carbon charges d) and in particular carbon nanofillers in said polymer a) wherein said heating calender is coupled to an infrared heating system (IR) or a laser or heating system by direct contact with a heat source such as a flame.
Said impregnation step i) of said process is carried out more particularly by using a technique chosen from: extrusion, pultrusion, injection-compression or dusting prior to the melting of said polymer a); said polymer a) being in powder form before melting, said powder possibly being (optionally) derived from a compound (melt pre-mixing) of said polymer a) and said carbon charges d). More particularly, said impregnation technique of step i) is extrusion and in particular an extrusion at right angles to said single wick or with respect to said parallel locks or an extrusion-coating on said fibrous reinforcement. one or more parallel locks. The extrusion-coating consists in extruding (melt-casting) said polymer a) followed by coating (melt depositing) on said fibrous reinforcement b). In this case, said polymer a) may be a mixture in the intimate state between said polymer a) and said liquid crystal polymer c) (LCP) and optionally with said component d).
Advantageously, the impregnation is carried out by passing one or more wicks in a continuous impregnation device, this continuous impregnation device comprising an impregnation head also called impregnation die.
Each wick to be impregnated is rolled by means of a reel device under the continuous traction generated. Preferably, the reel device comprises a plurality of reels, each reel for unwinding a wick to impregnate. Thus, it is possible to impregnate several strands of fibers simultaneously. Each reel is provided with a brake so as to apply a tension on each strand of fibers. In this case, an alignment module allows to arrange the fiber locks parallel to each other. In this way, the fiber locks can not be in contact with each other, which makes it possible to avoid mechanical degradation of the fibers in particular.
Optionally, the impregnation may be completed by a step of covering said single wick or said parallel multiple wicks after impregnation with said molten polymer, with a molten polymer that may be the same or different from said impregnating polymer i), before calendering step ii). Preferably, the molten polymer is identical to the impregnating polymer and preferably the covering is effected by extrusion at the head of the square with respect to the single wick or with respect to said multiple parallel strands. The use of a different polymer may allow, for example, to add properties to the composite material obtained or to improve its properties, compared to those provided with the impregnating polymer. The angle head is then supplied with thermoplastic polymer a) melted by an extruder. Indeed, such a covering not only makes it possible to complete the fiber impregnation step in order to obtain a final polymer volume content in the desired range, in particular for obtaining "ready-to-use" fibrous materials of good quality. quality, but it also improves the performance of the composite material obtained.
Before passing through the impregnation head, the fiber wick or the parallel fiber locks pass into a heating device whose temperature is controlled and variable, ranging from room temperature up to 1000 ° C. However, this temperature will be reduced for the organic polymers which would degrade completely towards 500 ° C and will have to remain within the limits of the temperature not to be exceeded for the impregnation. This heating temperature will remain below the thermal degradation start temperature of the polymer a) and does not exceed 250 ° C. This heating makes it possible to carry the strands of fibers at a temperature which facilitates their impregnation. Indeed, this heating prior to impregnation thus prevents too rapid recrystallization of the polymer by contact with the locks. This heating device may also make it possible to initiate the polymerization of a material previously deposited on the fiber locks or to modify, or even completely degrade, by thermal means the size of the fibers. Sizing corresponds to the small amount of polymer that generally covers the fiber locks to ensure the binder between these fibers within the wick, but also a compatibility with the polymer matrix a) during a resin infusion process for example. This heating device may, for example, be chosen from the following devices: a microwave or induction device, an IR or laser infrared device or another device allowing direct contact with the heat source such as a flame device . A microwave or induction device is very advantageous, especially when it is coupled to the presence of carbon nanofillers in the polymer a) since the carbon nanofillers amplify the heating effect and transmit it to the core of the material.
At the outlet of this heating device, the different strands of fibers pass through the impregnation head. This impregnation head is composed of an upper part and a lower part for adjusting the opening of the die at the inlet of the fiber locks and at the outlet. The impregnation head is connected to a worm-type polymer extrusion device a) capable of extruding the polymer a) pre-mixed with said polymer c) (LCP) in the molten state, the mixture intimate polymer a) and polymer c) (LCP) giving a melt blend of lower viscosity than that of the polymer a) alone.
Advantageously, the extrusion device of the polymer is composed of a single-screw extruder comprising degassing zones. This extruder is preferably connected to a static mixer, itself connected to a gear pump ensuring a constant polymer flow a) + c) in the die.
After the impregnation step i), there is the shaping step by means of a continuous calendering device comprising one or more heating calandres.
With the prior art, hot calendering could not be envisaged for a shaping step, but only for a finishing step because it did not allow heating at sufficient temperatures, especially when the polymer a) of impregnation is a polymer or comprises polymers with a high melting temperature (> 200 ° C). Said hot calendering not only makes it possible to heat the polymer impregnation mixture a) + polymer c) (LCP) and optionally with the presence of component d) pre-dispersed in a) + c), for said mixture to penetrate, adhere and uniformly covers the fibers of said reinforcement b), but also to control the thickness and width of the tape or tapes of preimpregnated fibrous material and in particular its porosity.
In order to be able to produce a plurality of unidirectional parallel ribbons, that is to say as many ribbons as parallel roving pre-impregnated by the impregnation device, the heating calenders advantageously comprise a plurality of calendering grooves, in accordance with the invention. number of ribbons. This number of grooves may, for example, be up to 200. A slave system also makes it possible to regulate the pressure and / or the spacing between the rolls of the calenders. The regulation of the pressure and / or the spacing between calender rolls is carried out in such a way as to control the thickness of the tapes by a control system controlled by a computer program provided for this purpose.
The calendering device comprises at least one heating calender and, preferably, it comprises a plurality of heating radiators mounted in series. The fact of having several calender in series makes it possible to pack the porosities in the material and to reduce the rate of porosity (fewer defects). This plurality of calenders is therefore important when it is desired to produce so-called "ready-to-use" fibrous materials. On the other hand, to manufacture so-called "dry" fibrous materials, it is possible to be content with a lower number of calenders or even a single calender.
Advantageously, each calender of the calendering device has an integrated heating system by induction or by microwaves and preferably by microwaves, in order to heat the mixture of polymers a) and c) involved in the impregnation of the fibrous reinforcement b ). Advantageously, when said mixture of polymers a) + c) comprises carbonaceous fillers, such as carbon black or carbon nanofillers, preferably chosen from carbon nanofillers, in particular graphenes and / or carbon nanotubes and or carbon nanofibrils or mixtures thereof, the heating effect by microwave or induction is amplified by the presence of these charges which then lead the heat to the heart of the material.
Advantageously, the heating calenders of the calendering device are coupled to a rapid heating device which makes it possible to heat the material not only at the surface but also at the core. The mechanical stress of the calenders coupled to these rapid heating devices first makes it possible to control the porosities and more particularly to minimize until the presence of porosities is eliminated and the polymer is distributed homogeneously, especially when the preimpregnated fibrous material is a so-called "ready-made" material. These rapid heating devices are located before and / or after each calender, in order to quickly transmit thermal energy to the material. The rapid heating device may for example be chosen from the following devices: a microwave or induction device, an IR or laser infrared device or other device allowing direct contact with the heat source such as a flame device. According to an alternative embodiment, it is also possible to combine several of these heating devices.
Optionally, a subsequent step is to wind the prepreg and shaped ribbons. For this, the method comprises a winding device comprising as many reels as ribbons, a coil being assigned to each ribbon. A splitter is generally provided to deflect the pre-impregnated ribbons to their respective coils, while preventing the ribbons from touching to avoid any degradation.
Regarding the heating grille, it comprises an upper roll and a lower roll. One of the rollers, for example the upper roll, comprises a crenellated portion, while the other lower roll comprises a grooved portion, the shape of the grooves being complementary to the shape of the projecting portions of the upper roll. The spacing between the rollers and / or the pressure exerted by the two rollers against each other makes it possible to define the dimensions of the grooves and in particular their thickness and their width. Each groove is designed to house a bit of fiber which is then pressed and heated between the rollers. The wicks then turn into parallel unidirectional ribbons whose dimensions, thickness and width are calibrated accurately by said grooves of the calenders. Each calender comprises in particular a plurality of grooves, the number of which can be up to 200, so as to produce as many ribbons as there are grooves and pre-impregnated locks. The calendering device further comprises the servo system for simultaneously regulating the pressure and / or spacing of the calendering rollers of all calenders of the unit.
The one-way ribbon (s) thus manufactured has (s) a width and a thickness adapted to a deposit by robot in the manufacture of composite parts, in particular in three dimensions (3D), without the need for slitting. The width of the ribbon (s) may be between 5 and 100 mm, preferably between 5 and 50 mm and even more preferably between 5 and 10 mm.
The process for the preparation of a preimpregnated fibrous material which has just been described thus makes it possible to produce preimpregnated fibrous materials with high productivity while permitting homogeneous impregnation of the fibers and the control and reproducibility of the porosity and thus the control and reproducibility of the performances of the final composite article in question. The homogeneous impregnation around the fibers and the absence of porosities are ensured by the impregnation step using the polymer a) in the molten state in intimate mixture with the liquid crystal polymer c) (LCP) which helps to the implementation by reducing the melt viscosity of said polymer a) and the use of a mechanical stress shaping device (heating calendering), itself coupled to rapid heating devices which allow to heat the material both surface and heart. The preimpregnated fibrous materials thus obtained are semi-finished products in the form of ribbons calibrated in thickness and width and which are used for the manufacture of structural parts in three dimensions in the transport sectors such as automotive, civil aviation or military, nautical or railway, renewable energies, sports and leisure, health and medical, weapons and missiles, security and electronics, by a process including the removal assisted by a robot head by example and known as the AFP method (from the acronym "Automatic Fiber Placement").
This method thus makes it possible to continuously produce ribbons of calibrated dimensions and of great length, so that it avoids slitting and splicing steps which are costly and detrimental to the quality of the composite parts manufactured subsequently. The economics of eliminating the slitting step is about 30-40% of the total cost of producing a ribbon of preimpregnated fibrous material. The combination of rapid heating devices with hot calenders facilitates the shaping of the ribbons to the desired dimensions and makes it possible to significantly increase the rate of production of these ribbons compared to conventional shaping methods. Moreover, this combination makes it possible to densify the material by completely eliminating the porosities in so-called "ready-to-use" fibrous materials.
This specific process combining a specific composition with specific impregnation and shaping steps by specific calendering also makes it possible to use many polymer grades, even the most viscous ones, which makes it possible to cover all ranges of resistance. mechanics desired.
For the specific manufacture of ribbons of so-called "dry" fibrous materials, the impregnation step according to the present invention makes it possible to obtain a uniformly distributed weight of polymer, with a preferred level of deposited polymer of the order of 5. at 7 g / m which allows a good penetration of the resins used to make, for example, infusion on preforms.
Another subject of the invention concerns a ribbon of preimpregnated fibrous material, in particular ribbon wound on a reel, which is based on a preimpregnated fibrous material as defined above according to the invention or which is obtained by a process as defined according to the invention above. More particularly, said ribbon has a width and a thickness suitable for robot placement of fiber placement, in the manufacture of parts in 2D or 3D, in particular 3D, without slitting and preferably it has a width not exceeding 20 mm, preferably not exceeding 12.70 mm (0.5 inches), more preferably not exceeding 6.35 mm (0.25 inches).
Another object of the invention relates to the use of the method as described above according to the invention for the manufacture of calibrated ribbons suitable for the manufacture of composite parts in 2D or 3D, preferably in 3D, by automatic removal. robot said ribbons. Said strips pre-calibrated width during their preparation according to the method of the invention no longer require slitting, as is the case with prepreg strips of width much greater than 100 mm.
Also part of the invention is the use of the ribbon of preimpregnated fibrous material as defined according to the invention in the manufacture of composite parts in 2D or 3D and preferably in 3D. Preferably, said manufacture of said composite parts concerns the automobile, civil or military aeronautics, energy and in particular wind and tidal energy, energy storage devices, thermal protection panels, panels solar, ballistics, in particular weapons and missile parts, boating, sports and leisure.
Finally, the invention relates to a composite part in 2D or in 3D, in particular in 3D, which results from the use of at least one ribbon of preimpregnated fibrous material, as defined above according to the invention.
Regarding the method used to determine the glass transition temperature Tg, it is measured using a differential scanning calorimeter (DSC) after a second heat-up according to ISO 11357-2 with a speed heating of 20 ° C / min.
Regarding the melting temperature Tf, it is measured by DSC according to the ISO 11357-3 standard with a heating rate of 20 ° C / min.

权利要求:
Claims (19)
[1" id="c-fr-0001]
1. Prepreg fibrous material, in particular in ribbon form, comprising a fiber reinforcement (in particular) based on continuous fibers, impregnated with a thermoplastic polymer matrix and comprising in its composition: a) a thermoplastic polymer forming said thermoplastic matrix with said polymer, if amorphous having a Tg> 40 ° C, preferably greater than 100 ° C and if semi-crystalline having a Tf> 150 ° C, preferably greater than 200 ° C, b) a fibrous reinforcement, c) as an additive, at least one liquid crystal polymer at a level ranging from 0.1 to 50%, preferably from 0.2 to 20%, more preferably from 0.2 to 15% and even more preferentially from 5 to 15% by weight with respect to said polymer a), said additive being able to be premixed with said polymer a) and dispersed in said polymer matrix, d) optionally, carbon fillers, preferably carbon nanofillers dispersed in said matrix of homogeneous and uniform way.
[2" id="c-fr-0002]
2. fibrous material according to claim 1, characterized in that said polymer a) is selected from polyaryl ether ketones (PAEK), in particular polyether ether ketone (PEEK) or from polyaryl ether ketone ketones (PAEKK), in particular the polyether ketone ketone (PEKK) or from aromatic polyether-imides (PEI) or polyaryl sulphones, in particular polyphenylene sulphones (PPS) or from polyarylsulphides, in particular polyphenylene sulphides or from polyamides (PA) of high T g, preferably Tg> 100 ° C.
[3" id="c-fr-0003]
3. fibrous material according to claim 1 or 2, characterized in that said polymer a) is a polymer or a mixture of thermoplastic polymers as defined according to claim 1 or 2.
[4" id="c-fr-0004]
4. fibrous material according to one of claims 1 to 3, characterized in that said fibrous reinforcement b) comprises or consists of continuous fibers selected from carbon fibers, glass, silicon carbide, basalt, natural fibers , in particular flax or hemp, sisal, silk or cellulosic material and in particular viscose or thermoplastic fibers of Tg or Tf greater than the Tg or Tf of said respectively amorphous or semi-crystalline polymer or of a mixture two or more of said fibers, preferably said fibrous reinforcement comprising or consisting of carbon fibers, glass or silicon carbide or their mixture, in particular carbon fibers.
[5" id="c-fr-0005]
5. fibrous material according to one of claims 1 to 4, characterized in that said polymer comprises carbon fillers, in particular from carbon black and carbon nanofillers and more particularly carbon nanofillers, preferably graphenes and / or or carbon nanotubes and / or carbon nanofibrils, more preferably carbon nanotubes.
[6" id="c-fr-0006]
6. Process for preparing a preimpregnated fibrous material, as defined according to one of claims 1 to 5, in particular in the form of a unidirectional ribbon, characterized in that it comprises at least the following step: impregnating said fibrous reinforcement, in the form of a single wick or several parallel locks, with said polymer a) in the molten state and optionally said polymer a) comprising said component d), with said component c) being present in said polymer as an application aid for reducing the melt viscosity of said polymer a).
[7" id="c-fr-0007]
7. Method according to claim 6, characterized in that said component d) is present in said polymer a) in the molten state during said impregnation step i), said component d) being homogeneously and uniformly dispersed in said molten polymer after a prior step of intimately mixing said polymer with said component c).
[8" id="c-fr-0008]
8. A method according to claim 6 or 7, characterized in that it comprises in addition to step i) the following additional steps: ii) shaping said wick or said parallel locks of said fibrous reinforcement impregnated according to step i), by calendering by at least one heating calender, this shaping being in the form of a single unidirectional calibrated ribbon or in the form of multiple unidirectional parallel calibrated ribbons, with in the latter case said heating calender comprising multiple calendering grooves, preferably up to 200 calendering grooves, in accordance with the number of said ribbons and with a pressure between the rolls of said calender kept constant by a slave system, iii) winding said ribbon or said parallel ribbons on one or more coils in accordance with the number of said ribbons.
[9" id="c-fr-0009]
9. Method according to claim 8, characterized in that said impregnation step i) is completed by a step of covering said single wick or said parallel locks after impregnation with said polymer a) melted according to step i), by a molten polymer a ') which may be identical or different from said impregnating polymer a) i), before said calendering step ii), preferably said molten polymer a') being of the same nature as said impregnating polymer a) ), preferably said covering being effected by extrusion head-square with respect to said single wick or with respect to said parallel locks.
[10" id="c-fr-0010]
10. Method according to one of claims 6 to 9, characterized in that said fiber reinforcement b) comprises or consists of continuous fibers selected from carbon fibers, glass, silicon carbide, basalt, natural fibers, in particular flax or hemp, sisal, silk or from cellulosic fibers and in particular viscose or thermoplastic fibers of Tg or Tf greater than the Tg or Tf of said polymer respectively if amorphous or semi-crystalline or a mixing two or more of said fibers, preferably carbon fibers, glass or silicon carbide or a mixture thereof, in particular carbon fibers.
[11" id="c-fr-0011]
11. Method according to one of claims 8 to 10, characterized in that said heating shell of step ii) is coupled to a rapid complementary heating system, in particular among microwaves or induction system coupled to the presence of carbon charges d) and in particular carbon nanofillers in said polymer a) or an infrared heating system (IR) or a laser or by direct contact with a heat source such as a flame.
[12" id="c-fr-0012]
12. Method according to one of claims 6 to 11, characterized in that said impregnation step i) is carried out using a technique among: extrusion, pultrusion or injection-compression or by dusting prior to the melting of said polymer a) said polymer a) being in the form of a powder before melting, said powder optionally being derived from a compound of said polymer a) and said carbon charges d).
[13" id="c-fr-0013]
13. The method of claim 12, characterized in that said impregnation technique i) is the extrusion and in particular an extrusion head-square with respect to said single wick or with respect to said parallel locks or extrusion-coating on said fibrous reinforcement in one or more parallel locks.
[14" id="c-fr-0014]
14. Ribbon of preimpregnated fibrous material, in particular tape wound on a reel, characterized in that it is based on a preimpregnated fibrous material as defined in one of claims 1 to 5 or that it is obtained by a process as defined according to one of claims 6 to 13.
[15" id="c-fr-0015]
15. Tape according to claim 14, characterized in that it has a width and a thickness suitable for the fiber placement robot removal, in the manufacture of 2D or 3D parts, in particular 3D, without the need for splitting and preferably it has a width not exceeding 20 mm, preferably not exceeding 12.70 mm (0.5 inches), more preferably not exceeding 6.35 mm (0.25 inches).
[16" id="c-fr-0016]
16. Use of the method as defined according to one of claims 6 to 13, for the manufacture of calibrated ribbons suitable for the manufacture of composite parts in 2D or 3D, preferably in 3D, by automatic robot application of said ribbons.
[17" id="c-fr-0017]
17. Use of the ribbon of preimpregnated fibrous material as defined in claims 14 or 15, in the manufacture of composite parts in 2D or in 3D, in particular in 3D.
[18" id="c-fr-0018]
18. Use according to claim 17, characterized in that said manufacture of said composite parts relates to the automobile, civil or military aviation, energy and in particular wind and tidal energy, energy storage devices. , thermal protection panels, solar panels, ballistics, in particular parts for weapons or missiles, boating, sports and leisure.
[19" id="c-fr-0019]
19. Composite part in 2D or in 3D, in particular in 3D, characterized in that it results from the use of at least one ribbon of preimpregnated fibrous material, as defined according to claim 14 or 15.

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同族专利:

公开号 | 公开日

WO2017017388A1|2017-02-02|

FR3039554B1|2018-12-07|

引用文献:

公开号 | 申请日 | 公开日 | 申请人 | 专利标题

US5039572A|1989-07-24|1991-08-13|Phillips Petroleum Company|High strength thermoplastic resin/carbon fiber composites and methods|

GB2424890A|2005-04-06|2006-10-11|Victrex Mfg Ltd|Polymeric material|

JP2010163552A|2009-01-16|2010-07-29|Toray Ind Inc|Fiber-reinforced composite material and method for producing the same|

JP2015094995A|2013-11-08|2015-05-18|富士通株式会社|Housing component and manufacturing method of the same|WO2018234441A1|2017-06-22|2018-12-27|Arkema France|Fibrous material impregnated with reactive thermoplastic prepolymer|

US10675785B2|2017-06-22|2020-06-09|Arkema France|Fibrous material impregnated with thermoplastic polymer|

CN107471679B|2017-08-08|2020-05-15|惠州市海龙模具塑料制品有限公司|Method for manufacturing carbon fiber composite material|

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优先权:

申请号 | 申请日 | 专利标题

FR1557259A|FR3039554B1|2015-07-29|2015-07-29|PROCESS FOR FIBROUS MATERIAL PRE-IMPREGNATED WITH A THERMOPLASTIC POLYMER USING A LIQUID CRYSTAL POLYMER|

FR1557259|2015-07-29|FR1557259A| FR3039554B1|2015-07-29|2015-07-29|PROCESS FOR FIBROUS MATERIAL PRE-IMPREGNATED WITH A THERMOPLASTIC POLYMER USING A LIQUID CRYSTAL POLYMER|

PCT/FR2016/051980| WO2017017388A1|2015-07-29|2016-07-29|Method for preparing a fiber material, pre-impregnated by a thermoplastic polymer, using a liquid crystal polymer|

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