WO2001038074A2 - Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article - Google Patents
Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article Download PDFInfo
- Publication number
- WO2001038074A2 WO2001038074A2 PCT/FR2000/003270 FR0003270W WO0138074A2 WO 2001038074 A2 WO2001038074 A2 WO 2001038074A2 FR 0003270 W FR0003270 W FR 0003270W WO 0138074 A2 WO0138074 A2 WO 0138074A2
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- WO
- WIPO (PCT)
- Prior art keywords
- envelopes
- composite article
- plies
- connecting lines
- article according
- Prior art date
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- Ceased
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three-dimensional [3D] structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/58—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres
- B29C70/66—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres the filler comprising hollow constituents, e.g. syntactic foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/413—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties containing granules other than absorbent substances
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/44—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling
- D04H1/46—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres
- D04H1/498—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres entanglement of layered webs
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/54—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties by welding together the fibres, e.g. by partially melting or dissolving
- D04H1/559—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties by welding together the fibres, e.g. by partially melting or dissolving the fibres being within layered webs
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H13/00—Other non-woven fabrics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B2038/0052—Other operations not otherwise provided for
- B32B2038/008—Sewing, stitching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/026—Porous
Definitions
- the present invention relates to a composite article essentially consisting of parallel fibrous sheets associated by a connecting structure, and in particular, but not limited to, a rigidified article for closing a composite panel.
- the present invention also relates to methods and apparatus for obtaining such articles.
- a method and a device for producing a composite article We know from O-A1-93 / 01342 a method and a device for producing a composite article. We start with two layers that we each converge on one side of a slatted table. The spaces between the slats form slots in the table through which the two sheets are assembled, for example by needling.
- In the lamellae are formed longitudinal conduits through which there is introduced between the two plies and between the connecting lines formed by needling an intermediate component chosen according to the destination of the composite article.
- the purpose of the component is, for example, to stiffen the panel, make it absorbent, strengthen it, cover it with electric cables, etc.
- the qualities required of an article such as a composite panel or a composite web are economy, lightness and mechanical strength.
- the object of the present invention is to improve in this sense the composite article known from WO-A1-93 / 01342.
- the composite article comprising at least two textile plies essentially parallel to one another and spaced from one another, fiber bridges connecting these two plies, and at least an insert component inserts between the sheets and between the fiber bridges, is characterized in that the intermediate component comprises envelopes defining chambers containing a gas.
- the connection structure between the at least two plies is partially hollow.
- the article is impregnated with a material capable of setting, such as a binder or a resin, a substantial saving of resin is achieved since the chambers defined inside the envelopes are not invaded by the resin and remain hollow in the final product which is therefore particularly light in relation to the mechanical resistance which it offers.
- a material capable of setting such as a binder or a resin
- the method for producing a composite panel in which a composite article comprising two elementary fibrous layers associated by a connecting structure at least partially composed of a material capable of making, is placed between two forming plates. taken, in particular a resin, is characterized in that the material traps envelopes defining chambers filled with gas, and in that by compressing the composite article between the plates the gas is put in pressure in the chambers while taking ladi t e material.
- the method for producing a composite article in which at least two elementary plies are connected to one another along longitudinal connecting lines while maintaining them, where the process takes place of connection, spaced apart from each other by mechanical action between the connection lines being formed, and as one connects the two plies, at least one intermediate element is guided between them to introduce it into spaces longitudinal defined between the longitudinal connecting lines by said mechanical action, characterized in that casings containing a gas are introduced as an intermediate component, so as to form an article according to the first aspect.
- Reinforcement fibers in particular organic or inorganic fibers, such as glass fibers, or animal or vegetable fibers, such as flax fibers, can be introduced between the sheets, as a second intermediate component. These fibers will thus be integrated into the article without being directly involved in the bonding process between the two layers. This is advantageous because certain fibers, in particular glass fibers, are difficult to needle.
- the envelopes are preconstituted before being introduced as an intermediate component. They are preferably hermetic so as to constitute sealed chambers in which air or another gas is definitively enclosed.
- the envelopes can for example be formed by two films in the form of a ribbon, glued one against the other except on certain surfaces, for example circular, where the two films separate from one another to form "bubbles" . It can also be a tubular film defining a shape chamber inside. general continuous cylindrical, or preferably a tubular film having from place to place transverse welds isolating from each other the successive individual chambers. It can also be foams or particles, such as balls which are introduced in bulk between the two layers or in certain longitudinal corridors formed between the two layers. Various expanded synthetic materials can be used for the balls or foams such as polystyrene, polyethylene, PVC or polyurethane. Mineral materials can also be used such as glass or clay.
- the device for manufacturing a composite article comprising means for guiding at least two elementary plies parallel to one another, with mechanical means for defining a spacing between them, means to connect the two plies along longitudinal connecting lines in the vicinity of said mechanical means, and introduction means for guiding at least one intermediate component between the two plies as they advance parallel to each other to introduce this constituting in longitudinal corridors defined by the mechanical means between the longitudinal connecting lines, is characterized in that the introduction means comprise means for guiding as intermediate component envelopes defining chambers filled with a gas.
- FIG. 1 is an elevation view of a manufacturing device according to the invention
- Figure 2 is a view of a detail of Figure 1, on an enlarged scale
- Figure 3 is a sectional view along III-III of Figure 2
- - Figure 4 is a sectional view along IV-IV of Figure 2
- Figure 5 is a schematic cross-sectional view of the article obtained at the outlet of the lamella table
- - Figure 6 is a cross-sectional view of the article obtained after forming
- Figures 7, 9 and 11 are schematic views in longitudinal section of three different embodiments for the envelopes defining the chambers
- Figures 8 and 10 are partial perspective views of the envelopes of Figures 7 and 9 respectively
- Figures 12 and 13 are views similar to Figures 1 and 3 respectively, but relating to a second embodiment
- Figures 14, 15, 16, 17 are views similar to Figures 1, 2, 3 and 4 respectively, but relating to a third embodiment
- the device according to the invention comprises a frame 1 rigidly supporting a vertical table 2 having two opposite guide faces 3.
- the table 2 is formed of strips 4.
- the lamellae 4 have an elongation direction which is vertical in the example (FIG. 2), have a flattened rectangular profile in planes perpendicular to the guide faces 3, which are defined by the small faces or edges of the lamellae.
- the frame 1 further comprises means 6 for supporting, on either side of the plane of the table 2, two coils 7 for supplying layers of textile fibers.
- the sheet 8 supplied by each coil 7 can be composed of fibers distributed at random, for example by the technique known as "pneumatic lapping", or of fibers having predetermined general orientations, obtained for example by means of a lapper spreader. These plies can be consolidated or preconsolidated in a known manner, in particular by needling or pre-needling.
- the frame 1 still carries different means 9, 11, 13 which will not be described in detail, intended to make the two plies 8 converge towards the table 2.
- the two plies 8 join the table 2 at the same height 31 then are guided parallel to each other downwards, each between a guide face 3 of the table 2 and a counterplate 14.
- the outgoing product 16 comprising the two plies 8 associated by a connecting structure as will be said later, passes between two drive rollers 17 rotating in opposite directions to pull the product 16 and therefore the two layers 8 along the route which has just been described.
- Each plywood 14 is located between table 2 and a respective needle board 18.
- Each board 18 carries vertical rows of needles 19 oriented perpendicularly towards the guide faces 3 of the table 2.
- the needles 19 are arranged in correspondence with slots 21 of the plywoods 14 and with intervals 22 , relatively narrow, between the lamellae 4.
- the rows of needles 19 are grouped in pairs.
- Each group of two rows of needles 19 is associated with two defined intervals 22 between a group of three strips 4.
- This pattern of needles 19 and strips 22 is repeated at regular intervals here according to the width of the table 2 with, between two successive patterns, an area without needles or strips. There is thus a corridor 23 between the lamellae of two successive patterns.
- the needle boards 18 are each connected to a mechanism of a type known for needling machines, intended to animate these needle boards with an alternating reciprocating movement 24 in a direction perpendicular to the guide faces 3 of the table 2. This movement alternately penetrates the needles 19 between the slats 4 as far as beyond the guide face 3 opposite the needle board 18 considered, then pull the needles 19 out of the slat table 2.
- FIG. 4 illustrates that the strips 4 of the same pattern can be produced in a single block with a common support 26 located upstream.
- FIG. 5 illustrates fiber bridges 27 each produced by the working of the needles 19 in one of the intervals 22 between two neighboring strips. Each bridge 27 visible in FIG. 5 corresponds to a row of bridges or connecting line between the two layers, oriented longitudinally relative to the direction of travel of the layers along the table 2. The penetration of the needles 19 into the table 2 entrains fibers of the ply 8 closest to the needle board considered and comes to intertwine these fibers with those of the other ply 8.
- the penetration of the needles on either side of the table can be simultaneous if the needles are shifted from one board to another, or on the contrary alternated in which case the needles of the two boards can be exactly aligned.
- the guide surfaces 3 defined by the edges of the strips prevent the plies 8 from being driven by the needles.
- the plywoods 14 which prevent the plies 8 from being driven by the needles 19.
- An intermediate component 28 is inserted between the two plies 8 in the corridors 23 defined between the lamella patterns 4.
- this component 28 is found in the product 16 trapped on the one hand between the plies 8 and on the other hand between the groups of bridges 27 which have been formed by needling.
- the intermediate component 28 is composed of envelopes containing a gas.
- these envelopes have the shape of balls of relatively small dimension, of the order of a millimeter or a few millimeters, which are hermetic, free from one another, and sent in bulk, by gravity, in the corridors 23 so as to fill them.
- the table 2 is mounted in a contiguous manner between two plates 29 extending as far as the zone 31 where the two plies 8 arrive, just upstream of the two counterplates 14.
- FIG. 5 represents in the right part the product 16 obtained in cross section with the groups of bridges 27 and the balls 28.
- the article 16 thus obtained can for example be subjected to a waterproofing treatment to form a floating wall an inflatable structure, serving as both a structural and thermally insulating wall.
- the product 16 can also be impregnated with resin.
- the resin will invade the entire space outside the envelopes formed by the balls 28.
- the product is compressed in the direction of its thickness. This has the double effect of reducing the space available for the resin and therefore the quantity of resin consumed as well as the weight of the finished product.
- the intermediate component 28 compensates for its compression in the thickness direction by compression of the gas contained in the envelopes but also by lateral expansion. This leads to a deformation of the bridges 27 in the form of an arc.
- the bridges 27 are kept under mechanical tension despite the mutual ratment of the two main faces of the article 16 which has become a composite panel.
- the resin impregnation can be done through the two main faces of the product 16.
- the resin impregnation and the pressing can be done after cutting off the product 16 leaving the machine 1 in a mold essentially comprising two pressing faces, flat or shaped for a particular use of the panel, to get a shape panel.
- the impregnation and pressing steps can also be carried out continuously before cutting off the product.
- the resin used can be a thermoplastic, thermoformable, thermosetting resin, or an expandable resin, for example an epoxy resin or foam.
- the expandable resins fill the space better and give an even lighter final product.
- FIG. 6 also illustrates that the finish can be improved on at least one of the faces of article 16 by laminating a coating 30 on this face. In Figure 6, the coating 30 is shown slightly spaced from the corresponding face of the article 16 for clarity.
- one or more finishing coatings could not be counter-coiled but integrated into the product upstream of the assembly operation of the layers, the resin then injected ensuring in this case the cohesion of the coatings.
- FIG. 7 illustrates that a chain 23a of generally cylindrical envelopes 31 separated by welds 32 can be used as an intermediate component instead of the balls 28.
- the intermediate component 28a can be produced by means of a flexible plastic film tube inflated with air or other gas and which is closed at regular intervals by the transverse welds 32.
- the film may for example be made of plastic such as polyethylene 7 / 100mm. If resin is subsequently injected, the film will be chosen according to the nature of the resin because it must be capable of withstanding the temperature of the exothermic reaction of the resin used.
- the intermediate component 28b is produced by means of two flexible films 33, in the form of a tape, glued or adhered against each other except in certain locations regularly distributed longitudinally where the one of the films 33 forms pockets 34 closed by the other film and containing air or other gas.
- the process for producing such an intermediate component is similar to that which is used for producing packaging films having "bubbles" of padding intended to protect the packaged object against impact during transport.
- the casing 28c is a simple continuous flexible tubular film. Compared to the embodiments of FIGS. 7 to 10, this tubular film is more economical but has the drawback of not hermetically trapping air or other gas. On the other hand, a puncture of the tubular film affects a great length of the article during production.
- Figures 7 to 10 are advantageous because the strings 28a or 28b are positively driven with the article 16 during production.
- the balls 28 on the contrary require monitoring for the proper filling of each lane 23. They can on the other hand be advantageous in order to give the article better resistance to compression in the sense of its thickness.
- Figures 4, 5 and 6 illustrate the operation of the device of Figure 1 with the different types of envelopes 28c, 28a, 28b, 28 from the left of each figure, respectively. This is purely illustrative. In practice, the same type of envelopes will generally be used in all the corridors 23 for a given production.
- the frame 1 comprises means 6a for supporting a third ply coil 7a delivering a third ply 8a.
- the needles 19, in the position of maximum penetration can reach the opposite outer ply 8 or, on the contrary, preferably, only reach the central ply 8a.
- the article advances in a horizontal plane during its production.
- the back and forth movement 24 of the needles is therefore vertical.
- corridors 23 and 23a there are two types of corridors 23 and 23a.
- the corridors 23, of larger dimension, are as in the previous embodiment intended for the introduction of the intermediate components 28.
- the corridors 23a are occupied by resin injection nozzles 36 which are supplied from a reservoir 37 ( Figure 14) and a pump 38 and open between the two plies 8 beyond the downstream end of the table 2 ( Figure 17).
- the resin 39 dispensed by the nozzles 36 drowns the plies 8 and the interval between them except for the chambers 41 defined inside the envelopes 28.
- the product 16 can be subjected to the setting operation of the resin also in the process. It passes for this purpose between two forming plates 42, possibly heating, the mutual distance of which is calculated to compress the product and give it an internal configuration similar to that shown in FIG. 6. Extractor rollers 43 are provided downstream of the plates 42.
- a chainsaw 44 delivers the article 16 into individual panels 46 which are, for example received on a stacking device which is only suggested.
- the resin 39 can be chosen from the same varieties as those mentioned above.
- the corridor 23 is produced in a similar manner to that described for the previous examples, between two successive patterns of lamellae.
- the corridor 23a located right next to it is produced in a similar manner.
- the other corridors are defined by the inner face of tubular strips of square or rectangular sections 47, two opposite faces of which help define the guide faces 8 and two other opposite faces delimit some of the intervals intended for the needles.
- the slat table is more expensive to produce but the plies are better guided and supported against the forces due to the needling.
- nozzles 36 are components of relatively low value which can be replaced independently of the table 2 and in particular, if necessary, of the tubular strips 36a of the table 2 in which they extend.
- At least one second intermediate component in particular reinforcing fibers, in particular organic or inorganic, such as glass fibers, or animal or vegetable fibers, such as flax fibers, instead some of the envelopes or together with envelopes in the same corridor. This is particularly advantageous if the product is then impregnated as described.
- the material capable of setting can be injected in the form of a powder, for example a plaster, a cement, or can be an elastomer. Instead of needling, one can use a sewing or welding step.
- the tubular films can be inserted in the deflated state between the two layers, then inflate them before resinating, at a pressure which determines the place left for the resin, and which may differ from 'one tube to another, to distribute the resin in greater quantity in the less swollen areas. It is also possible to produce a flexible and inflatable and deflatable structure by mounting a valve at the end of each tube or a valve common to all the tubes.
- the structure can be made waterproof by laminating a waterproof film such as PVC on at least one side, generally on both sides.
- the support 26 then remaining only as a guide beyond the needles.
- the resin such as phenolic
- the resin can be introduced between the layers, in the form of a powder. The powder is activated by passing it through the oven, in particular a steam oven.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Nonwoven Fabrics (AREA)
Abstract
Description
Claims
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2001221772A AU2001221772A1 (en) | 2000-11-24 | 2000-11-24 | Composite articles with fibrous laps, method and device for obtaining same |
| PCT/FR2000/003270 WO2001038074A2 (fr) | 1999-11-25 | 2000-11-24 | Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR99/14822 | 1999-11-25 | ||
| FR9914822A FR2801613B1 (fr) | 1999-11-25 | 1999-11-25 | Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article |
| PCT/FR2000/003270 WO2001038074A2 (fr) | 1999-11-25 | 2000-11-24 | Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2001038074A2 true WO2001038074A2 (fr) | 2001-05-31 |
| WO2001038074A3 WO2001038074A3 (fr) | 2001-12-13 |
Family
ID=26212257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/FR2000/003270 Ceased WO2001038074A2 (fr) | 1999-11-25 | 2000-11-24 | Article composite a nappes fibreuses, procede et dispositif d'obtention d'un tel article |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO2001038074A2 (fr) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005007962A1 (fr) * | 2003-07-11 | 2005-01-27 | Nonwovens Innovation & Research Institute Limited | Textile non-tisse a espaces intermediaires |
| WO2006008166A1 (fr) * | 2004-07-23 | 2006-01-26 | Alfonso Branca | Procede et installation de fabrication d'un panneau multicouche et panneau multicouche ainsi produit |
| EP1686210A1 (fr) * | 2005-02-01 | 2006-08-02 | Guy Le Roy | Panneau composite, dispositif et procédé pour fabriquer un tel panneau |
| WO2008065174A1 (fr) | 2006-11-30 | 2008-06-05 | Airbus Deutschland Gmbh | Structure principale et procédé de production d'une structure principale |
| WO2010110660A1 (fr) * | 2009-03-23 | 2010-09-30 | Lantor B.V. | Matériau de noyau conducteur |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1504196B2 (de) * | 1965-12-16 | 1971-02-18 | Deutsche Tafelglas AG Detag 8510Furth | Verfahren zur herstellung von ebenen oder raeumlich ge kruemmten plattenfoermigen koerpern aus mit fluessigem haertbarem kunstharz getraenkten fasermaterial |
| US5140721A (en) * | 1990-10-25 | 1992-08-25 | Kauffeld Robert C | Thermal protective diving undergarments made with plastic bubble packing sheets |
| FR2678547B1 (fr) * | 1991-07-03 | 1995-03-10 | Guy Leroy | Procede et dispositif pour la realisation de nappes composites et composites obtenus. |
| FI89471C (fi) * | 1991-09-12 | 1993-10-11 | Finnclever Oy | Foerfarande foer framstaellning av en armerad fiberkonstruktion som skall lamineras och motsvarande armerad fiberkonstruktion |
| FR2700140B1 (fr) * | 1993-01-07 | 1995-01-27 | Guy Le Roy | Procédé et dispositif pour la réalisation de nappes composites avec constituant intercalaire initialement semi-fluide et composites obtenus. |
| EP0714755A1 (fr) * | 1994-11-15 | 1996-06-05 | Klaus Kurt Kölzer | Charge légère comprimée pour matériaux thermoduresesables et procédé pour sa fabrication |
-
2000
- 2000-11-24 WO PCT/FR2000/003270 patent/WO2001038074A2/fr not_active Ceased
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005007962A1 (fr) * | 2003-07-11 | 2005-01-27 | Nonwovens Innovation & Research Institute Limited | Textile non-tisse a espaces intermediaires |
| US7718249B2 (en) | 2003-07-11 | 2010-05-18 | Nonwovens Innovation & Research Institute Limited | Nonwoven spacer fabric |
| US7814625B2 (en) | 2003-07-11 | 2010-10-19 | Nonwovens Innovation & Research Institute Limited | Nonwoven spacer fabrics |
| WO2006008166A1 (fr) * | 2004-07-23 | 2006-01-26 | Alfonso Branca | Procede et installation de fabrication d'un panneau multicouche et panneau multicouche ainsi produit |
| EP1686210A1 (fr) * | 2005-02-01 | 2006-08-02 | Guy Le Roy | Panneau composite, dispositif et procédé pour fabriquer un tel panneau |
| FR2881442A1 (fr) * | 2005-02-01 | 2006-08-04 | Roy Guy Le | Panneau composite, dispositif et procede pour fabriquer un tel panneau |
| WO2008065174A1 (fr) | 2006-11-30 | 2008-06-05 | Airbus Deutschland Gmbh | Structure principale et procédé de production d'une structure principale |
| CN101616786B (zh) * | 2006-11-30 | 2012-11-07 | 空中客车德国运营有限责任公司 | 芯结构以及制造芯结构的方法 |
| US8365412B2 (en) | 2006-11-30 | 2013-02-05 | Airbus Operations Gmbh | Core structure and method for producing a core structure |
| WO2010110660A1 (fr) * | 2009-03-23 | 2010-09-30 | Lantor B.V. | Matériau de noyau conducteur |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2001038074A3 (fr) | 2001-12-13 |
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