FIBER APPLICATION HEAD WITH AIR BLOWING SYSTEM

Information

  • Patent Application
  • 20200361164
  • Publication Number
    20200361164
  • Date Filed
    November 09, 2018
    6 years ago
  • Date Published
    November 19, 2020
    4 years ago
Abstract
The present application relates, in particular, a fibre application head for producing composite material parts, comprising a compacting system comprising a compacting roller (2) for applying one or more fibres onto an application surface, and a heating system (9) capable of emitting thermal radiation towards the fibre or fibres. Said head further comprises a blowing system (8) comprising an air blowing nozzle (81), said nozzle being arranged upstream from the roller, with respect to the movement direction, and being capable of forming an air knife, parallel to the axis of the roller, towards the nip zone between the compacting roller and the layup surface.
Description

The present invention relates to a fibre application head for a fibre application machine for producing composite material parts, and more particularly to a so-called fibre placement head equipped with a particular application roller. The present invention also relates to a method of manufacturing parts made of composite material by means of a corresponding application head.


There are known fibre application machines, commonly called fibre placement machines, for the application by contact onto a layup tool, such as a male or female mold, of a wide band formed of several continuous flat fibres, of ribbon type, dry or impregnated with thermosetting or thermoplastic resin, in particular carbon fibres consisting of a multitude of carbon threads or filaments.


These machines are used to produce preforms formed of several superposed plies, each ply being formed by laying up onto the mold of one or more bands side by side. In the case of a layup of fibres pre-impregnated with thermoplastic or thermosetting resin, typically of a quantity of at least 40% in weight, the pre-impregnated preform obtained after laying up is hardened or polymerized by passing it through an oven to obtain a composite material part. In the case of so-called dry fibres, which are not pre-impregnated with resins, the fibres comprise a reduced quantity of so-called bonding resin, also called a binder, generally a thermoplastic resin, in a quantity of less than or equal to 5% in weight, to give a tackiness to the fibres during the layup. After layup, the so-called dry preform is subjected to a resin injection or infusion operation before the curing step.


These machines, such as described in the patent document WO2006/092514, typically comprise a fibre application head, a system for moving said head, fibre storage means, and fibre conveying means for conveying the fibres from said storage means to the head. The head typically comprises an application roller, also called a compacting roller, intended to come into contact with the mold for applying the band, and means for guiding the fibres on said application roller.


The head generally further comprises a heating system for heating the fibres. The compacting roller presses the band of fibres against the application surface of the mold, or against the band (s) of fibres previously applied, in order to facilitate the adhesion of the applied bands to each other, as well as to progressively discharge the air trapped between the laid bands. The heating system ensures the heating of the bands of fibres to be applied, and/or of the mold or bands already applied upstream of the compacting roller, just before the compacting of the band, in order to at least soften the pre-impregnation resin or bonding resin, and thus promote adhesion of the bands to one another.


In the case of thermosetting resins, the pre-impregnated fibres are simply heated to soften them, typically at temperatures of about 40° C. The heating system typically comprises an infrared heating system comprising one or more infrared lamps.


In the case of thermoplastic resins, the fibres pre-impregnated or having a binder must be heated at higher temperatures, at least up to the resin melting temperature, being of about 200° C. for nylon type resins, and up to about 400° C. for PEEK type resins.


To achieve these higher temperatures, hot air torch systems have been proposed, and more recently laser type heating systems to achieve accurate and concentrated heating. Due to the higher heating temperatures, the fibre placement heads are typically equipped with metallic compacting rollers, resistant to heat, which can furthermore be cooled by the interior via a water circuit. To be able to adapt itself to the profile of the application surface, segmented metallic compacting rollers have been proposed, comprising several roller segments independently mounted side by side on a same axle, each segment being radially moveable and in an independent manner, and being elastically biased against the application surface. These segmented metallic rollers have proven however to be complex in structure and implementation.


Flexible rollers formed from a so-called high temperature elastomer, including a thermal stabilizer, are also used. These rollers generally comprise an anti-adherent sheath heat-shrunk and glued to the cylinder made of elastomeric material, as described in patent documents FR 2948058 and FR 3009512. To cool them, it has been proposed to equip the placement heads with a cooling system capable of delivering an air flow to cool the roller from the outside or from the inside, as described in the patent document FR 2948058. Despite these cooling systems, flexible rollers can have a tendency to deteriorate when using thermoplastic resins. Depending on the heating temperatures used, the anti-adherent sheath may tend to degrade quickly. Laser heating can tend to deteriorate the glue used for gluing the sheath and lead to a disassembling of the sheath and the cylinder of flexible material. Furthermore, the deteriorated adhesive layer absorbs laser radiation and can rise to high temperatures which can deteriorate the sheath.


During laying up, combustion of the impregnation resin of the fibres may occur. The combustion fumes tend to form deposits on the sheath. In addition to the problem of fouling the sheath, these deposits absorb laser radiation and can lead to the destruction of the sheath.


In document FR 3009510, it has been proposed to provide blowing nozzles to diffuse an inert gas previously heated, such as nitrogen, to locally form a protective atmosphere and to avoid oxidation of the resins. This diffusion of nitrogen represents a significant cost. Furthermore, this diffusion of nitrogen does not allow the presence of an operator in the layup cell during layup, and requires a renewal of the air in the cell before access is allowed.


The aim of the present invention is to propose a solution to overcome at least one of the aforementioned drawbacks, which in particular enables the use of a wide variety of resins, both thermosetting and thermoplastic, with a substantially uniform compaction of the applied band, and which is simple in design and construction.


To this end, the present invention provides a fibre application head for producing composite material parts, comprising a compacting system comprising a compacting roller, also called application roller, for applying one or more fibres, in particular a band formed of one or more flat fibres, onto an application surface, and a heating system capable of emitting thermal radiation in the direction of the fibre(s) in the direction of the band, preferably just before application by the application roller, characterized in that said head further comprises a blowing system comprising an air blowing nozzle connected to an air supply system, said nozzle being arranged upstream of the roller relative to the movement direction of, and is capable of forming an air knife, preferably parallel to the axis of the roller, in the direction of the nip zone between the compacting roller and layup surface.


According to the invention, the head comprises a blowing nozzle delivering an air knife in the direction of the nip zone, also called the contact zone, so as to limit or even eliminate any deposit of combustion fumes on the external surface of the roller. The air knife enables the combustion flames to be extinguished by being blown out, or even to eliminate the emergence of any combustion flames by blowing them out. According to the invention, it is possible to blow out the flames with an air knife while guaranteeing, despite the high air flow rate, a satisfactory fibre layup quality, and efficient heating of the laid fibre(s), in particular with a laser type heating system, without the need to heat the air beforehand to form the air knife.


This blowing system according to the invention makes it possible to effectively protect the flexible rollers, and in particular their external anti-adherent sheaths, for the application of fibres at high temperatures, in particular above 400° C., in particular for the application of fibres impregnated with thermoplastic resins, in particular with a laser type heating system. The head according to the invention, which comprises a compacting roller of simple design, offers the possibility of using a wide variety of thermosetting or thermoplastic resins combined with a wide variety of fibres, synthetic or natural, hybrid or not, in particular fibres commonly used in the field of composites, such as glass fibres, carbon, quartz, and aramid fibres.


According to one embodiment, the blowing nozzle comprises a longitudinal discharge slot arranged parallel to the axis of the roller, or a purality of outlets arranged along a line parallel to the axis of the roller. This parallel arrangement makes it possible to ensure an air knife at a high flow rate, sufficient to blow out the flames, without altering the quality of the layup of the fibres, in particular without displacing the fibres at the end of the trajectory.


According to one embodiment, the blowing system is capable of forming an air knife having a length at least equal to half the length of the roller, preferably close to the length of the fibre or the bands of fibres laid by the head, the air knife preferably being centred relative to the roller.


According to one embodiment, the blowing system is capable of delivering an air knife at a flow rate of at least 300 Nl/min, preferably at least 500 Nl/min, more preferably at least 600 Nl/min, for example about 700 Nl/min.


According to one embodiment, the blowing system is capable of delivering an air knife at a flow rate of at least 50 Nl/min per centimetre of air knife lengthwise, preferably at least 100 Nl/min, more preferably at least 120 Nl/min


According to one embodiment, the air blowing nozzle is connected to a supply source formed by a source of compressed air or to a turbine, preferably mounted on said head, delivering pulsed air.


According to one embodiment, the blowing system comprises several blowing nozzles arranged side by side, each nozzle being connected to a source of compressed air or to a turbine.


According to one embodiment, said compacting roller comprises a rigid central tube by which said roller is rotationally mounted on a support structure of the head and at least one cylindrical part made of a flexible material, elastically deformable, assembled coaxially, directly or indirectly, on said central tube, and an anti-adherent sheath covering the cylindrical part, said anti-adherent sheath has lateral portions extending beyond the cylindrical surface of the cylindrical part in the direction of the rotation axis of the roller, the assembly of said sheath to said cylindrical part being produced by said lateral portions, said lateral portions effecting a blocking of the sheath in translation and rotation relative to said cylindrical part. The protective sheath is assembled by lateral portions, outside the heating zone. This assembly allows to avoid a gluing of the sheath in the heating zone and therefore to avoid any risk of deterioration of the sheath due to a deterioration of the glue due to radiation. This assembly of the sheath combined with the blowing nozzle guarantees good stability of the sheath.


According to one embodiment, said compaction roller comprises a cylindrical part made of an elastomeric material, preferably unexpanded, for example a silicone or a polyurethane, preferably made of silicone, preferably having a hardness of between 25 Shore A and 80 Shore A, preferably at least 40 Shore A, in order to guarantee a good resistance of the sheath over time.


According to one embodiment, the compacting roller comprises a cylindrical part of foam, for example an expanded elastomer such as a polyurethane foam, preferably having a density between 200 kg/m3 and 500 kg/m3.


Said anti-adherent sheath is advantageously formed from a fluoropolymer, preferably a fluoropolymer chosen from the group consisting of a polytetrafluoroethylene (PTFE), a perfluoroalkoxy (PFA), a fluorinated ethylene propylene (FEP), an ethylene tetrafluoroethylene (ETFE), preferably a PFA or a FEP, and a fluoroelastomer, for example an FPM, FFPM or a FEPM, or a polyimide.


According to one embodiment, said anti-adherent sheath is thermoformed on the cylindrical part, preferably heat-shrunk, the thermoformed lateral portions ensuring at least partially the blocking of the sheath in rotation and in translation. The use of a heat-shrinkable sheath enables simple and rapid assembly of the sheath starting from a sheath in the form of a tube which is subsequently heat-shrunk on the cylindrical part.


According to one embodiment, said central tube is provided with radial holes, said cylindrical part of flexible material having fluid communication means capable of putting said radial holes in fluid communication with the external cylindrical surface of the cylindrical part, said head comprising thermal regulation means capable of injecting a thermal regulation gas flow, advantageously a gas at room temperature or cooled, in particular air, in the internal passage of the central tube, said roller comprising a draining intermediate layer interposed between the anti-adherent sheath and the cylindrical part, said intermediate layer ensuring the evacuation of the thermal regulation fluid through the lateral faces of the roller. The use of such a draining layer combined with a by-inside cooling system makes it possible to effectively maintain the sheath and the cylindrical part at reasonable temperatures, below the deterioration temperatures of the materials used.


Said intermediate layer is preferably formed from glass fibres, carbon fibres, metallic fibres or threads, for example copper or stainless steel, or polymer fibres, for example PAN fibres, PEEK fibres, said layer can be in the form of a non-woven fibre felt and/or in the form of a fabric. The thickness and the grammage of the intermediate layer are defined so as to ensure a passage of the gas flow sufficient to remove the calories. In the case of glass fibres, the intermediate layer forms an insulating barrier, limiting the rise in temperature by conduction of the cylindrical part made of flexible material. In the case of metallic fibres, the intermediate layer forms a barrier to the radiation emitted by the heating system.


Preferably, said fluid communication means comprises radial channels, each radial channel opening onto a radial hole in the central tube and onto the external surface of the cylindrical part. The radial holes are distributed over the cylindrical wall of the central tube. The central tube has for example several sets of holes offset longitudinally along the axis of the compacting roller, each set comprising a plurality of holes made at regular angular intervals.


According to the embodiments,

    • said intermediate layer preferably comprises glass fibres in the form of a fabric, for example in the form of a sleeve or braid;
    • the intermediate layer has end portions extending beyond the cylindrical surface of the cylindrical part, so as to guarantee the evacuation of injected gas;
    • each lateral portion of the sheath is assembled by its annular end portion to mechanical assembly means; and/or
    • each lateral portion of the intermediate layer is assembled by its annular end sections to mechanical assembly means, the mechanical means can comprise two washers assembled to each another by assembly means, such as screws, and between which the end section of the sheath and/or of the intermediate layer is enclosed; and/or
    • the roller has at each end a portion defining a curved or inclined surface arranged in the extension of the cylindrical surface, in order to obtain a progressive folding of the sheath, this portion being formed of a part added to the cylindrical part or being integral with the cylindrical portion of the cylindrical part.


Mechanical means can be used alone or in combination with the thermoforming of the sheath, to assemble the sheath and/or the draining intermediate layer. According to one embodiment, the sheath is thermoformed and only the intermediate layer is assembled via mechanical means. Separate mechanical means can be used for the sheath and for the intermediate layer. According to another embodiment, the intermediate layer is glued to the cylindrical part, on the cylindrical surface and/or on the lateral faces.


According to one embodiment, the head constitutes a fibre placement head comprising cutting means and a feeding means, and possibly a fibre blocking means . According to one embodiment, the head is used to perform a filament winding type application .


According to one embodiment, the head comprises a laser type heating system , in particular laser diodes, a YAG laser or a fibre laser, capable of emitting a laser beam in the direction of the contact zone between the roller and a layup surface. Despite the high air flow rate of the air knife, efficient heating of the fibres can be obtained by the laser type heating system. Alternatively, the heating system may include one or more infrared lamps.


According to one embodiment, the head further comprises a secondary blowing system comprising a secondary air blowing nozzle, said secondary nozzle being arranged downstream of the roller relative to the movement direction , and is capable of forming an air knife, parallel to the axis of the roller, in the direction of the compacting roller, to cool the roller from the outside and thus to limit the temperature of the roller rising. The use of such an air knife with a high flow rate makes it possible to effectively cool the compacting roller.


The secondary blowing system is similar to or even identical to the aforementioned blowing system arranged upstream of the roller :

    • the secondary nozzle comprises a longitudinal discharge slot arranged parallel to the axis of the roller, or a plurality of outlets arranged along a line parallel to the axis of the roller, and/or is connected to a supply source formed by a source of compressed air or to a turbine delivering pulsed air, and/or
    • the secondary blowing system is capable of forming an air knife having a length at least equal to half the length of the roller, and/or is capable of delivering an air knife at a flow rate of at least 300 Nl/min, preferably at least 500 Nl/min, more preferably at least 600 Nl/min, and/or is capable of delivering an air knife at a flow rate of at least 50 Nl/min per centimetre of air knife lengthwise, preferably at least 100 Nl/min, more preferably at least 120 Nl/min


The present invention also relates to a methodfor manufacturing a composite material part comprising the application of continuous fibres onto an application surface, characterized in that the application of fibres is carried out by means of a fibre application head as described previously, by relative displacement of the application head in relation to the layup surface along layup trajectories, the fibres being compacted during their application by means of said application roller, said nozzle forming an air knife during laying up, in the direction of the nip zone between the compacting roller and the layup surface, so as to blow out the combustion flames, namely to extinguish the combustion flames by blowing, or even to blow out any emergence of combustion flame.


The fibres conventionally used are continuous flat fibres, also called tows, generally unidirectional, and comprising a multitude of filaments. The laid fibres can be dry fibres or fibres pre-impregnated is with thermosetting or thermoplastic resin. The fibres typically have widths of ⅛, ¼ or ½ inch. As used herein, the term “fibres” also refers to fibres of greater width, greater than ½ inch, conventionally called band in placement technology.


The method according to the invention is particularly advantageous in the case of the production of dry preforms produced from dry fibres provided with a binder and/or thermoplastic preforms produced from fibres pre-impregnated with thermoplastic resin, requiring high heating temperatures during layup to at least reach the melting point of the binder and/or the thermoplastic resins.


In the case of a dry preform, the method further comprises a step of impregnating resin into the dry preform, by adding one or more impregnating resins by infusion or injection to the dry preform, and a curing step to obtain a composite material part. In the case of a thermoplastic preform, the preform may possibly be subjected to an additional consolidation step to obtain a final composite material part. In situ consolidation can also be obtained during the application of the fibres.


The application of fibres can be carried out on the application surface of a tool to form a preform, such as described previously, by fibre placement, band placement, and/or winding. According to another embodiment, the application of fibres is carried out directly on the application surface of a prefabricated part, to reinforce this part with unidirectional fibre reinforcements, the prefabricated part being for example a part obtained by injection, molding or additive manufacturing, from one or more thermoplastic and/or thermosetting resins.


According to one embodiment, the application of fibres is carried out with an air knife at a flow rate of at least 300 Nl/min, preferably at least 500 Nl/min, more preferably at least 600 Nl/min, and/or at a flow rate of at least 50 Nl/min per centimetre of air knife lengthwise, preferably at least 100 Nl/min, more preferably at least 120 Nl/min





The invention will be better understood, and other objectives, details, characteristics and advantages will appear more clearly in the following detailed explanatory description of a currently preferred embodiment of the invention, with reference to the schematic drawings annexed thereto, in which:



FIG. 1 is a schematic side view of a fibre application head according to the invention, illustrating the compacting roller, the heating system and the blowing system;



FIG. 2 is an enlarged partial view of FIG. 1;



FIG. 3 is a schematic perspective view, with a partial cut away, of the compacting roller of FIG. 1;



FIG. 4 is a perspective view of a compacting roller with a partial cut away, according to a second embodiment;



FIG. 5 is a perspective view of a compacting roller according to a third embodiment;



FIG. 6 is a perspective view of a compacting roller, with a partial cut away, according to a fourth embodiment;



FIG. 7 is a perspective view of a compacting roller, with a partial cut away, according to a fifth embodiment;



FIG. 8 is a perspective view of a compacting roller, with a partial cut away, according to a sixth embodiment; and,



FIG. 9 is a view similar to that of FIG. 2, illustrating a fibre application head according to an alternative embodiment, comprising a secondary blowing system.





With reference to FIGS. 1 and 2, the application head 1 comprises a compacting roller 2 which is mounted to rotate around an axis A on a support structure of the head. The head is intended for the application of a band formed of several fibres arranged side by side. The head is mounted by said support structure at the end of a movement system, for example a robot wrist joint. The head further comprises a heating system 9 also mounted on the support structure, upstream of the roller relative to the advancement direction D of the application head during the application of a band of fibres F onto an application surface S. The heating device is for example a laser type heating system, the radiation of which is directed towards the band, just before its compaction, as well as towards the band or bands already laid.


As illustrated in FIG. 1, the radiation 91 is thus directed obliquely towards the nip zone or contact zone between the application roller and the application surface, to heat a section of the band located on the roller, before its compaction by the latter, as well as the application surface and/or one or more bands previously applied.


In the case of a fibre placement machine, the head comprises guiding means 11 which guides the fibres entering the head towards the compacting roller 2 in the form of a band of fibres, the fibres of the band being arranged side by side in a substantially contiguous manner By movement of the head by the robot, the compacting roller is brought into contact with the application surface of a mold S to apply the band.


The fibres are preferably flat continuous fibres, of the tows type, pre-impregnated with a thermosetting resin or a thermoplastic resin, or dry fibres provided with a binder. The binder is in the form of powder and/or one or more veils, preferably of the thermoplastic type.


According to the invention, the head further comprises a blowing system 8, comprising a nozzle 81 also mounted on the support structure, upstream of the roller relative to the advancement direction D, capable of emitting a knife blade of compressed air towards the contact zone. The nozzle forms an air knife, parallel to the axis of the roller, centred along a direction illustrated schematically under the reference 82. The nozzle is for example connected to a compressed air supply circuit.


With reference to FIG. 3, the compacting roller 2 comprises a cylindrical part or body 3 made of a flexible material, elastically deformable by compression. The cylindrical part has a cylindrical central passage for its assembly on a support core formed by a rigid cylindrical central tube 4, for example metallic, such as aluminium. The cylindrical part 3 and the central tube 4 are coaxial and are integral in rotation with one another. The cylindrical part here comprises a single cylindrical part with a cylindrical surface 33 and two lateral faces 34.


The cylindrical part 3 of flexible material gives the compacting roller a crushing capacity which enables the compacting roller to adapt itself to variations in the curvature of the application surface and thus to apply a substantially uniform pressure over the entire laid band. The rigid tube enables the rotary mounting of the roller on the support structure.


The cylindrical part is for example comprised of an unexpanded elastomer, such as a silicone or polysiloxane, or a polyurethane, preferably a silicone, for example a two-component silicone which can be polymerized at room temperature. The cylindrical part has a hardness between 30 Shore A and 70 Shore A, for example 40, 50 or 60 Shore A, is which will be chosen according to the desired crushing rate of the roller for a given compaction force, this crushing rate being defined in particular according to the complexity of the application surface.


The central tube is provided with radial holes 41, for example cylindrical, traversing the cylindrical wall of the central tube from end to end. The radial holes thus open onto the internal passage 42 of the central tube and onto the cylindrical part. The latter is provided with radial channels 32, aligned with said radial holes 41, having diameters substantially identical to those of said radial holes. Each radial channel 32 opens onto the external cylindrical surface 33 of the cylindrical part 3. By way of example, the central tube comprises six sets of radial holes 41 offset longitudinally along the axis A of the roller, each set comprises a plurality of radial holes arranged at regular angular intervals, for example eight radial holes at 45° to one another. The cylindrical part then comprises six sets of radial channels 32 each comprising eight radial channels at 45° to one another.


The cylindrical part is coated with a draining intermediate layer 5, here formed of a glass fibre fabric, for example in the form of a sleeve or braid. The intermediate layer has a certain elasticity to follow the deformations of the cylindrical part when the roller is pressed against the application surface.


The intermediate layer is externally coated with an external anti-adherent sheath 6, formed here of a heat-shrunk PFA film on the surface of the cylindrical part, with the draining intermediate layer interposed between the cylindrical part and the sheath. The anti-adherent sheath through which the roller is in contact with the band, limits the adhesion of the roller to the fibres, as well as the fouling of the roller.


According to the invention, the anti-adherent sheath has lateral portions 61 extending beyond the cylindrical surface along the lateral faces 34 of the cylindrical part.


The anti-adherent sheath is formed from a tubular film of greater length than that of the cylindrical part, which is fitted onto the cylindrical part then thermoformed, so that the lateral portions are at least partially flattened along the lateral faces. The lateral portions thus heat-shrunk ensure the blocking in translation and in rotation of the anti-adherent sheath and of the intermediate layer on the cylindrical part.


The intermediate layer 5 also has lateral portions 51 extending beyond the cylindrical surface and which are inserted between the lateral faces 34 and the heat-shrunk lateral portions 61 of the sheath.


The mounting of the roller on the head is carried out by means of an axial rod 21 mounted in the internal passage of the central tube 4 by means of two ball bearings 24, the central tube advantageously having a counterbore at each end for the mounting of a bearing. The roller is then mounted by the ends of the axial rod between two flanges 12 of the support structure of the head.


The machine comprises thermal regulation means (not shown), making it possible to inject a gas at room temperature, between 15 and 30° C., or a gas cooled to a temperature below 15° C., in particular air, through one end of the axial rod. The axial rod 21 has an axial passage 22 opening onto one 25 of the ends of the rod, and a radial bore 23 enabling said axial passage 22 and the internal passage 42 of the central tube to be placed in fluid communication, between the two bearings, the two bearings being sealed bearings.


In operation, the air injected through at least the open end of the axial rod, arrives in the internal passage 42 between the two sealed bearings, passes through the radial holes 41 then the radial channels 32 of the cylindrical part, then passes through the draining intermediate layer 5 and escapes laterally through the lateral portions 51. This injected air makes it possible to uniformly cool, the cylindrical part of flexible material, as well as the sheath.


The laser type heating system can comprise laser diodes, arranged in one or more rows, emitting radiation of wavelength(s) between 880 to 1030 nm for example, a fibre optic laser or a YAG laser, emitting a wavelength of around 1060 nm.


The air knife from the blowing system 8 blows out the resin combustion flames, more precisely extinguishes by blowing out the flames that may appear during laser heating, or even eliminates the emergence of any flames by blowing them out. Thus, the air knife makes it possible to limit or even to eliminate any pollution of the sheath linked to combustion.


For example, the head is equipped with a compacting roller having is a length of approximately 6 cm, intended to layup a band of 8 fibres of 6.35 mm (¼″ inch). The nozzle comprises a row of charging outlets forming a knife of approximately 5 cm at the nozzle exit. The nozzle is supplied with compressed air at 5 bars, equivalent to an air knife at a flow rate of approximately 700 Nl/m.



FIG. 4 illustrates a second embodiment of the invention in which the compacting roller 102 comprises as previously a rigid central tube 104 provided with radial holes, a cylindrical part 103 made of elastically deformable flexible material provided with radial channels, an intermediate layer 105 with lateral portions 151, and an anti-adherent sheath 106 thermoformed with lateral portions 161.


In this embodiment, the cylindrical part comprises a central cylindrical part extending laterally via two annular flanges 134 whose outer surfaces form a continuous surface with the cylindrical surface 133. The cylindrical portion and the lateral flanges are molded in one piece, the flanges having a cylindrical outer surface. The lateral portions 151, 161 of the intermediate layer and of the sheath are arranged on said flanges 135. During the thermoforming of the sheath, the flanges progressively fold inwards in the direction of the lateral faces of the cylindrical part, as illustrated in FIG. 4. The flanges allow the sheath and the intermediate layer to be folded over a non-sharp edge at the end of the cylindrical part, and thus to avoid deterioration of the sheath over time at the level of folding.



FIG. 5 illustrates a third embodiment of the invention in which the compacting roller 202 comprises as previously a rigid central tube 204 provided with radial holes, a cylindrical part 103 of elastically deformable flexible material provided with radial channels, an intermediate layer 205 with lateral portions 251, and an anti-adherent sheath 206 thermoformed with lateral portions 261.


In this embodiment, as a replacement for the aforementioned flanges, the roller comprises a O-ring seal or part 235 arranged against each lateral face 234 of the cylindrical part, and the anti-adherent sheath 206 is heat-shrunk over said seals . The seals have an outside diameter equal to the outside diameter of the cylindrical part and enable the sheath and the intermediate layer to be folded over a non-sharp angle at the end of the cylindrical part. Preferably, the cylindrical part has a small flange at the end to ensure perfect surface continuity between the cylindrical surface of the cylindrical part and the seals.


Furthermore, the assembly by heat-shrinking is here completed by mechanical assembly by means of two washers 271, 272 assembled together by means of screws 273 by enclosing the annular end sections of the lateral portions 251, 261 of the sheath and of the intermediate layer between them.


The washers are pressed one against the another by contact zones angularly spaced to one another, to enable the evacuation of the air flow by the lateral portions of the intermediate layer between two contact zones. For this purpose, at least one or both of the washers are ringed, or one or both of the washers have on their opposing faces bosses or studs distributed at regular angular intervals, for example at the holes of the outer washer and/or the threads of the inner washer which serve for screwing in the screws, the washers being pressed one against the other by said bosses when tightening the screws.



FIG. 6 illustrates a fourth embodiment of a compacting roller 302 which differs from the preceding compacting roller 202 in that the two annular washers 371 have tabs 371a arranged at regular angular intervals and extending radially towards the exterior, the two washers are assembled to each other by means of screws 373 screwed into said tabs, enclosing between them the end portions of the anti-adherent sheath and of the intermediate layer. Thus in this embodiment, the air injected from inside the tube escapes through each zone of lateral portions of the intermediate layer arranged between two adjacent tabs.



FIG. 7 illustrates a fifth embodiment of a compacting roller 402 which differs from the compacting roller 102 illustrated in FIG. 4 by the fact that, on each side of the roller, the annular flange 435, the lateral portion 451 of the intermediate layer 405, as well as the lateral portion 461 of the sheath 406 are assembled together by mechanical means. These mechanical means comprise an outer washer or crown 471 provided with inclined tabs 471a at regular angular intervals, and a washer or inner ring 472 provided with an inclined annular surface 472a, the crown and the ring being assembled to each another by screws 473, so that the flange and the two lateral portions 451, 461 are enclosed is between the inclined tabs and said inclined surface of the ring.



FIG. 8 illustrates a sixth embodiment which differs from the embodiment of FIG. 3 by the fact that, on each side of the roller 502, the central tube 504 has an end section 543 extending beyond the lateral face 533 of the cylindrical part 503, the lateral portion 551 of the intermediate layer 505 extends beyond the lateral portion 461 of the thermoformed anti-adherent sheath 506, over the whole of the lateral face of the cylindrical part 533, and is blocked on the end section 543 of the tube by means of a ring 571. For example, the ring is crimped or screwed onto the tube, or is formed of two half-rings assembled by screwing.


In this embodiment, the sheath is held in place only by thermoforming, only the intermediate layer is assembled by mechanical means.



FIG. 9 illustrates an alternative embodiment in which the head further comprises a secondary blowing system 7, comprising a secondary nozzle 71 mounted on the support structure, downstream of the roller relative to the advancement direction D, capable of emitting a knife of compressed air towards the roller. The secondary nozzle forms an air knife, parallel to the axis of the roller centred along a direction illustrated schematically under the reference 72. The secondary nozzle is for example identical to the nozzle 81 arranged upstream of the roller, and is connected to the same compressed air supply circuit, the nozzle being for example supplied with compressed air at 5 bars.


Although the invention has been described in connection with various particular embodiments, it is obvious that it is in no way limited thereto and that it includes all the technical equivalents of the means described as well as their combinations if these are within the scope of the invention.

Claims
  • 1. Fibre application head for producing composite material parts, comprising a compacting system comprising a compacting roller (2,102, 202, 302, 402, 502) for the application of one or more fibres onto an application surface (S), and a heating system (9) capable of emitting thermal radiation in the direction of the or fibre(s), characterized in that said head further comprises a blowing system (8) comprising an air blowing nozzle (81), said nozzle being arranged upstream of the roller with respect to the movement direction, and is capable of forming an air knife, parallel to the axis of the roller, in the direction of the nip zone between the compacting roller and the layup surface.
  • 2. Application head according to claim 1, characterized in that the blowing nozzle comprises a longitudinal discharge slot arranged parallel to the axis of the roller, or a plurality of outlets arranged in a line parallel to the axis of the roller.
  • 3. Application head according to claim 1 or 2, characterized in that the blowing system is capable of forming an air knife having a length at least equal to half the length of the roller.
  • 4. Application head according to one of claims 1 to 3, characterized in that the blowing system is capable of delivering an air knife at a flow rate of at least 300 Nl/min, preferably at least 500 Nl/min, more preferably at least 600 Nl/min.
  • 5. Application head according to claims 1 to 4, characterized in that the blowing system is capable of delivering an air knife at a flow rate of at least 50 Nl/min per centimetre of air knife lengthwise, preferably at least 100 Nl/min, more preferably at least 120 Nl/min
  • 6. Application head according to one of claims 1 to 5, characterized in that the air blowing nozzle (81) is connected to a supply source formed by a source of compressed air or to a turbine delivering pulsed air.
  • 7. Application head according to one of claims 1 to 6, characterized in that the said compacting roller comprises a rigid central tube (4) and at least one cylindrical part (3, 103, 203, 403, 503) made of a flexible material, elastically deformable, assembled on said central tube, and an anti-adherent sheath (6, 106, 206, 406, 506) covering the cylindrical part, said anti-adherent sheath has lateral portions (61, 161, 261, 461, 561) extending beyond the cylindrical surface (33) of the cylindrical part in the direction of the rotation axis (A) of the roller, the assembly of said anti-adherent sheath with said cylindrical part being carried out by said lateral portions.
  • 8. Head according to claim 7, characterized in that said anti-adherent sheath (6, 106, 206, 406, 506) is thermoformed on the cylindrical part, the thermoformed lateral portions ensuring at least partially the blocking of the sheath in rotation and in translation.
  • 9. Head according to claim 7 or 8, characterized in that said central tube (4) is provided with radial holes (41), said cylindrical part of flexible material having fluid communication means (32) capable of putting said radial holes in fluid communication with the external cylindrical surface (33) of the cylindrical part, said head comprising thermal regulation means capable of injecting a thermal regulated gas flow into the internal passage of the central tube,said roller comprises a draining intermediate layer (5, 105, 205, 405, 505) interposed between the anti-adherent sheath and the cylindrical part, said intermediate layer ensuring the evacuation of the thermal regulation fluid through the lateral faces of the roller.
  • 10. Head according to one of claims 1 to 9, characterized in that it comprises a laser type heating system capable of emitting a laser beam in the direction of the contact zone between the roller and a layup surface.
  • 11. Head according to one of claims 1 to 10, characterized in that it further comprises a secondary blowing system (7) comprising a secondary air blowing nozzle (71), said secondary nozzle being arranged downstream of the roller relative to the movement direction, and is capable of forming an air knife, parallel to the axis of the roller, in the direction of the compacting roller.
  • 12. Method for manufacturing a composite material part comprising the application of continuous fibres onto an application surface, characterized in that this application of fibres is carried out by means of a fibre application head according to one of claims 1 to 10, by relative movement of the application head in relation to the layup surface along layup trajectories, said nozzle forming an air knife during laying up, parallel to the axis of the roller, in the direction of the nip zone between the compacting roller and the layup surface, so as to blow out the combustion flames.
  • 13. Method according to claim 12, characterized in that the application of fibres is carried out with an air knife at a flow rate of at least 300 Nl/min, preferably at least 500 Nl/min, more preferably at least 600 Nl/min.
  • 14. Method according to claim 12 or 13, characterized in that the application of fibres is carried out with an air knife at a flow rate of at least 50 Nl/min per centimetre of air knife lengthwise, preferably of at least 100 Nl/min, more preferably at least 120 Nl/min
Priority Claims (1)
Number Date Country Kind
17 71204 Nov 2017 FR national
PCT Information
Filing Document Filing Date Country Kind
PCT/FR2018/000246 11/9/2018 WO 00