Classifications

• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
  • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
  • D04H3/045—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles for net manufacturing
• • 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
  • B29C70/22—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 two directions forming a two-dimensional [2D] structure
  • B29C70/228—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 two directions forming a two-dimensional [2D] structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
• • 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
  • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
  • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
• • 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
  • D04H1/42—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 characterised by the use of certain kinds of fibres insofar as this use has no preponderant influence on the consolidation of the fleece
  • D04H1/4209—Inorganic fibres
  • D04H1/4242—Carbon fibres
• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/002—Inorganic yarns or filaments
• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
  • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
  • D04H3/07—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments otherwise than in a plane, e.g. in a tubular way
• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
  • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
  • D04H3/105—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by needling
• • 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
  • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
  • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
  • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
  • D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
  • F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
  • F16D69/02—Composition of linings ; Methods of manufacturing
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/21—Circular sheet or circular blank
  • Y10T428/213—Frictional
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
  • Y10T428/24033—Structurally defined web or sheet [e.g., overall dimension, etc.] including stitching and discrete fastener[s], coating or bond
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
  • Y10T428/24132—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in different layers or components parallel

Definitions

• the present invention relates to a method for producing annular fibrous structures, in particular preforms intended for the manufacture of annular parts made of composite material.
• a particular, but not exclusive, field of application of the invention is the production of annular preforms for the manufacture of brake or clutch discs in composite material, in particular in carbon-carbon composite material (C / C).
• Annular parts of composite material consist of a fibrous reinforcing structure, or preform, densified by a matrix.
• the preform is made of carbon fibers or fibers of a carbon precursor which is transformed into carbon by heat treatment after production of the preform.
• a carbon precursor available in the form of fibers is in particular the preoxidized polyacrylonitrile (PAN).
• PAN preoxidized polyacrylonitrile
• Densification of the preform can be carried out by liquid-impregnation with a liquid carbon precursor, for example a resin, and transformation of the precursor by heat treatment - or by chemical vapor infiltration, or even by caulking.
• the preform is immersed in a liquid precursor of the matrix and the preform is heated for example by contact with an armature or by direct coupling with an inductor, so that the precursor is vaporized in contact with the preform and can infiltrate to form the matrix by deposition within the porosity of the preform.
• a well-known method for producing fibrous preforms of parts made of composite material consists in superimposing and needlening layers or layers of a two-dimensional fibrous texture.
• the fibrous texture is for example a fabric.
• the fabric is optionally covered with a veil of fibers which provides the fibers capable of being displaced by the needles through the superimposed strata; this is particularly the case when the fabric is made of fibers which are difficult to needleave without being broken, in particular carbon fibers.
• Such a method is described in particular in documents FR-A-2584 106 and FR-A-2584 109 respectively for the production of flat preforms and for the production of preforms of revolution.
• An annular preform for a disc can be cut from a thick plate formed by layers superimposed flat and needled.
• the loss of material is close to 50% which, in the case of preforms made of carbon fibers or of carbon precursor fibers, represents a very significant cost. In order to reduce this loss, it has been proposed in the document
• EP-A-0232059 to produce the preform by superimposing and needling annular layers each formed from several assembled sectors.
• the sectors are cut out in a two-dimensional texture.
• the loss of material is less than in the case of cutting whole rings, but remains significant.
• the process is rather delicate to implement and to automate, in particular because of the need to correctly position the sectors while shifting them from one layer to another so as not to superimpose the lines of separation between sectors .
• Another known technique for producing fibrous preforms for annular parts made of composite material consists in using a textile product in a spiral or helical strip which is wound flat in superimposed turns.
• the textile product can be a fabric formed of helical warp threads and radial weft threads.
• the spiral or helical shape is given to the fabric by calling by means of a tapered roller warp threads unwound from individual spools mounted on a cantre.
• the spacing between the radial weft threads increases over the width of the helical fabric between the inside diameter and the outside diameter.
• fibrous preforms for annular parts of composite material are produced by helical winding of flattened tubular braids.
• the tubular braids can be straight, as described in document EP-A-0528336.
• the braids are then deformed to be wound in a helix.
• Longitudinal wires can be added during the manufacture of the braid in order to improve the dimensional stability of the preform, and to compensate for the variation in surface density between the internal diameter and the external diameter of the flattened braid wound. It has also been proposed to use helical tubular braids in document EP-A-0 683 261.
• an object of the present invention is to provide a method which makes it possible to produce annular preforms for parts made of composite material without causing substantial drops of material and while maintaining a substantially constant surface density between the inside diameter and the outside diameter of the structures.
• Another object of the present invention is to provide such a method, the cost of implementation of which is substantially lower than that of the methods of the state of the art capable of providing similar results.
• a method of producing an annular fibrous structure is proposed by flat helical winding of a fibrous texture in the form of a deformable strip, the method comprising the steps which consist in:
• the directions of the two plies make with the longitudinal direction of the strip angles of absolute value preferably between 30 ° and 60 °, in order to provide a capacity for deformation of the elementary meshes in longitudinal direction and in transverse direction.
• these angles are equal to + 45 ° and -45 °.
• the connection of the sheets between them is carried out while preserving the possibility of deformation of the elementary meshes at their tops, for example by sewing or by knitting by means of threads passing from one face to the other of the texture, or even by pre- needling or localized needling.
• Such a texture is particularly advantageous by its deformation capacity allowing it to be wound in a flat helix without forming any surface thicknesses or undulations and with a substantially uniform distribution of the fibrous elements of the plies giving the helix a surface density whose variation between its inside and outside diameters can remain within acceptable limits, without it being necessary to compensate for it.
• the turns superimposed flat formed by winding the helical texture are linked together.
• the connection between the turns is for example carried out by needling. Needling can be done after winding and possibly compression of the annular structure, or during winding.
• the stripe-like texture can be deformed by passing between two rotating discs, maintaining the texture between the discs, for example by clamping, along its longitudinal edges, or by calling on at least one frustoconical roller.
• FIG. 1 is a very schematic view of an installation allowing the realization of 'A fibrous texture in the form of a deformable strip usable for the implementation of a method according to the invention
• FIGS. 2, 3A, 3B and 3C are views illustrating the production of a knitting connection of a fibrous texture usable for the implementation of a method according to the invention
• 5A, 5B and 5C are views illustrating the production of another knitting connection of a fibrous texture usable for the implementation of a method according to the invention
• FIG. 6 is a schematic detail view which shows how a fibrous texture, such as that produced by means of the installation of Figure 1, deforms when it is wound flat helically;
• FIG. 7A and 7B are schematic views illustrating a helical winding device of a fibrous texture for the implementation of a method according to the invention
• FIG. 8A and 8B are schematic views illustrating two other helical winding devices of a fibrous texture for the implementation of a method according to the invention
• FIG. 9 is a schematic view illustrating an embodiment of a method for producing an annular fibrous structure in accordance with the invention: and - Figure 10 is a schematic view illustrating another embodiment of a method for producing an annular fibrous structure according to the invention.
• the fibrous texture used in a process according to the invention is formed by superposition and bonding of two unidirectional sheets made up of fibrous elements parallel to each other.
• a unidirectional ply can be obtained by spreading-lapping a cable or, as envisaged in the detailed description below, by placing in parallel wires from different coils. It will be noted that a process for producing a multi-axial fibrous texture from unidirectional plies obtained by spreading cables is described in the French patent application filed on March 28, 1997 under No. 97 03 832 and entitled “Process and machine for producing multiaxial fibrous webs ", the content of which is incorporated herein by reference. FIG.
• the constituent fibers of the unidirectional sheets 10, 12 are made of a material chosen according to the use envisaged for the strip-like texture. They may be organic or mineral fibers, for example carbon or ceramic fibers, or carbon or ceramic precursor. It will be noted that the constituent fibers of the two layers may be of different natures. It is even possible to use fibers of different natures in each tablecloth.
• the strip is formed by bringing successive segments of the ply 10 making an angle of + 45 ° relative to the longitudinal direction of the strip to be produced, and by juxtaposing these segments in this direction. Each segment is brought over a length such that it extends from one longitudinal edge of the strip to the other longitudinal edge. Similarly, successive segments of the ply 12 are brought at an angle of -45 ° relative to the longitudinal direction of the strip to be produced and are juxtaposed, the ply segments 12 being arranged above the ply segments 10.
• the wires 11, 13 constituting each ply 10, 12 are stretched between two endless chains with pins 20, 22 moved in synchronism.
• the ends of the plies 10, 12 are guided by carriages, respectively 14, 16 receiving the wires 11, 13 from respective coils (not shown) and driven back and forth between the longitudinal edges of the strip to be produced.
• the plies are turned around around pins of the corresponding pin chain.
• the advance of the studded chains 20, 22 is controlled continuously or discontinuously, in relation to the supply of the plies 10, 12, so as to juxtapose the successive ply segments.
• An installation of this type is known, for example from document US-A-4 677 831, so that a more detailed description is not necessary.
• the strip formed by superposition of the plies 10, 12 is removed from the chains with pins 20, 22 at the downstream end of their upper strand to be admitted into a binding device 30.
• the binding is carried out by needling by means of a needle board 32 which extends over the entire length of the strip in formation, the latter passing over a perforated plate 34, the perforations of which are located to the right of the needles of the board 32.
• the distribution of the needles on the needle board 32 is determined to perform a localized needling so that the binding of the two plies defines elementary deformable stitches for example in the manner of parallelograms.
• the bonding between the layers gives the fibrous texture in the form of a strip 50 obtained sufficient cohesion to be stored on a roller 38 driven by a motor 40 in synchronism with the pin chains 20, 22. Between the binding device 30 and the roller 38, the edges of the strip 50 are cut by means of rotary knobs 36a, 36b_.
• FIGS. 2, 3A and 3B illustrate a preferred variant embodiment of the binding of the sheets.
• the binding is carried out not by needling but by knitting.
• the superimposed layers taken from the spiked chains 20, 22 are received by a knitting device 42 which produces a knitting, that is to say a two-dimensional structure, by means of a thread passing from one face to the other.
• texture 50 ( Figure 2).
• FIG. 3A shows in detail the knitting stitch used 44, while FIGS. 3B and 3C show the right and wrong sides of the texture 50 bonded by knitting.
• the knitting stitch forms intertwined loops 44a, elongated in the longitudinal direction of texture 50 by forming several parallel rows, and V or zig-zag paths 4412 which connect the loops between neighboring rows .
• the texture 50 is located between the paths 44b_ located on the right side ( Figure 3B) and the loops 44a located on the reverse side ( Figure 3C), giving the knitted fabric the appearance of a zigzag stitch on one side and d 'a chain stitch on the other side.
• the knitting stitch includes several threads of each tablecloth, depending on the gauge chosen.
• connection points between the paths 44b_ in a zigzag and the loops 44a such as the points A, B, C, D of FIGS. 3B and 3C, define summits of elementary deformable meshes. That is to say, in this case, that are deformable both the meshes defined by the knitting stitch, and meshes defined by crossing points between son of the plies and forming deformable parallelograms.
• FIG. 4 illustrates another variant according to which the connection between the plies is also carried out by knitting.
• the overlapped plies taken from the spike chains 20, 22 are received by a knitting device 46 which links the plies along several lines parallel to the longitudinal edges of the texture 50.
• the knitting stitch 48 is a stitch chain with loops 48a linked by rectilinear segments 48b_, the texture 50 is located between the segments 48b_, visible on the right side of the texture
• the knitting yarn for the embodiments of FIGS. 2 and 4 can be made of a fugitive material, that is to say a material capable of being removed later without damaging the fibers making up the plies.
• a fugitive material that is to say a material capable of being removed later without damaging the fibers making up the plies.
• son of a material capable of being removed by heat without leaving a residue or son of a material capable of being removed by a solvent, for example son of polyvinyl alcohol soluble in water .
• a knitting yarn made of a material compatible with the subsequent use envisaged for the texture may be used.
• the knitting or sewing thread may be made of a material compatible with the material of the matrix of the composite material, that is to say preferably say of the same nature or miscible in the matrix without reacting chemically with it.
• Other modes of connection by knitting or also by sewing can be chosen.
• the strip-like texture obtained is particularly advantageous because of its deformation capacity allowing it to be wound in a flat helix without causing surface deformation (slippage or undulations), this because the elementary meshes 52 of the texture 50 behave like deformable parallelograms whose deformation is not hampered by the mode chosen binding mode, the knitting mode illustrated by Figures 2, 3A, 3B and 3C being preferred in this regard.
• the elementary meshes 52 ′ located in the vicinity of the internal diameter of the propeller being formed are deformed by elongation in the radial direction and narrowing in the longitudinal direction, while the elementary meshes 52 "located in the vicinity of the outer diameter of the propeller are deformed by narrowing in the radial direction and elongation in the longitudinal direction.
• the surface density of fibers remains substantially constant or slightly variable between the inner diameter and the outer diameter, which is particularly advantageous for developing homogeneous preforms intended for the manufacture of parts made of composite material
• the dashed line 54 shows the deformation of one of the initial directions of the strip 50.
• the deformation of the elementary stitches formed by the threads of the texture is accompanied by a deformation of the knitting or sewing points.
• the deformation results in an elongation or a shortening of the parts of the thread forming the loops of the chains and by an opening or a closing of the angles which the zigzag paths form.
• Winding with deformation of the texture 50 in a flat helix can be achieved by passing the texture between two discs or annular flanges 60, 62 while maintaining the texture between the discs along its longitudinal edges (FIG. 7A).
• the texture is maintained for example by clamping its edges between circular ribs 64, 66 formed on the internal faces of the disks 60, 62, or at least on the internal face of one of the disks (FIG. 7B).
• the winding with deformation of the texture is produced by passing the latter over at least one frustoconical roller.
• the number of rollers and their apex angles are chosen according to the degree of deformation desired.
• two identical tapered rollers 70, 72 are used which are rotated by respective motors (not shown).
• the texture is forced to follow a part of the periphery of at least one of the rollers.
• the texture is forced to pass between a first rotary tapered roller 74 and a smooth support plate 75 and between a second rotary tapered roller 76 and a smooth support plate 77.
• the rollers driven in rotation by respective motors (not shown) deform the texture by friction.
• An annular fibrous structure can be produced by superimposing flat the turns formed by the helical winding of the texture 50 and bonding the turns together by needling as the winding takes place (FIG. 9).
• the texture 50 deformed, for example by passing between two discs, as in the case of FIG. 5, is wound in turns superimposed flat on a rotating plate 80.
• the plate 80 is mounted on a vertical axis 82 secured to a support 84.
• the support 84 further carries a motor 86 which drives the plate 80 in rotation about its vertical axis 90 (arrow f 1), by means of a belt 88.
• the assembly comprising the support 84 and the plate 80 is movable vertically along a fixed central guide tube 92 of axis 90. At its upper end, the tube 92 supports the device for deformation of the helical strip.
• the support 84 rests on vertical telescopic rods 94, the vertical movement of the support 84 being controlled by one or more jacks 96.
• the band 50 is needled by means of a board 100 carrying needles
• the movement of the needle board is controlled by a motor 104, via a connecting rod-crank type transmission.
• the motor 104 is carried by the support 84.
• the needling of the strip 50 is carried out with a substantially constant surface density and depth.
• the needle board 100 has a sector shape, corresponding to a sector of an annular layer of fabric, sector on which the needles are distributed uniformly, while the plate 80 supporting the structure 110 being developed is rotated at constant speed.
• the needling depth that is to say the distance over which the needles 102 penetrate each time into the structure 110, is kept substantially constant, and equal for example to the thickness formed by a few overlapping layers of fabric.
• the strip 50 is wound on the plate 80, the latter is moved vertically downwards by the desired distance so that the relative position between the surface of the preform and the needle board, at one end of its vertical stroke, remains unchanged.
• several needling passes are carried out while continuing to rotate the plate 80 so that the volume density of needling in the layers of surface tissue is substantially the same as in the rest of the preform.
• a progressive lowering of the plate 80 can be controlled, as in the previous phases.
• This principle of needling at constant depth by progressive lowering of the support of the preform and with final needling passes is known and described in particular in the document FR-A-2 584 106 already cited.
• the plate 80 is coated with a protective layer 106 in which the needles can penetrate without being damaged during the needling of the first turns of tape 50.
• the protective layer 106 can be formed of a felt of base, for example a polypropylene felt, covered with a sheet of plastic material, for example polyvinyl chloride which avoids, when the needles rise, entraining in the preform 110, fibers taken from the base felt .
• the turns formed by helically winding the deformed texture are applied against each other and the fibrous structure is compressed by means of a tool comprising a base plate 130 and a upper plate 132 (FIG. 10).
• the compression is carried out so as to obtain a desired volume ratio of fibers.
• the turns can then be linked together by needling by means of a needle board 134, the needles 136 of which pass through perforations in the upper plate 132 and penetrate the entire thickness of the structure 110. Perforations can be formed also in the base plate 130 to the right of the hands.
• annular fibrous structure obtained as described above can be used as a preform for the manufacture of an annular piece of composite material, for example a brake disc.
• the elimination of the wire is carried out by dissolution or heat treatment before densification of the preform.
• the material constituting the fibers of the fibrous structure obtained is a precursor to that of the fibrous reinforcement of the composite material
• the transformation of the precursor is carried out before densification of the preform, or during the rise in temperature preceding densification.
• the densification of the preform is carried out in a known manner by the liquid route or by chemical vapor infiltration in order to form within the accessible porosity of the preform a deposit of the material constituting the desired material.
• deformable fibrous texture consisting of two linked unidirectional sheets forming angles of + 45 ° and -45 ° relative to the longitudinal direction of the strip
• the method according to the The invention can be implemented with deformable bands in which the two unidirectional plies make angles of opposite signs, the absolute values of which may be different from 45 ° and possibly different from each other.
• these angles Preferably, however, in order to maintain a sufficient capacity for deformation of the elementary meshes, these angles have an absolute value of between 30 ° and 60 ° and preferably also, these angles have the same absolute value in order to maintain a character of symmetry to the strip. deformable.
• the flat helical winding of the fibrous strip as obtained at the outlet of the lapping installation of FIG. 1.
• the fibrous strip obtained at the outlet of the coating installation is divided into several deformable strips having or not the same width, by cutting parallel to the longitudinal direction.

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• Engineering & Computer Science (AREA)
• Textile Engineering (AREA)
• Mechanical Engineering (AREA)
• Chemical & Material Sciences (AREA)
• General Engineering & Computer Science (AREA)
• Inorganic Chemistry (AREA)
• Composite Materials (AREA)
• Nonwoven Fabrics (AREA)
• Treatment Of Fiber Materials (AREA)
• Ceramic Products (AREA)
• Braking Arrangements (AREA)
• Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
• Woven Fabrics (AREA)
• Wire Processing (AREA)

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Cited By (6)

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• 1997
  • 1997-03-28 FR FR9703833A patent/FR2761379B1/fr not_active Expired - Fee Related
• 1998
  • 1998-03-25 JP JP54122398A patent/JP4083815B2/ja not_active Expired - Fee Related
  • 1998-03-25 UA UA99105812A patent/UA54502C2/uk unknown
  • 1998-03-25 EP EP98917227A patent/EP0970271B1/fr not_active Expired - Lifetime
  • 1998-03-25 US US09/381,943 patent/US6319348B1/en not_active Expired - Lifetime
  • 1998-03-25 ES ES98917227T patent/ES2167888T3/es not_active Expired - Lifetime
  • 1998-03-25 RU RU99122690/12A patent/RU2176296C2/ru active
  • 1998-03-25 DE DE69802508T patent/DE69802508T2/de not_active Expired - Lifetime
  • 1998-03-25 CA CA002285375A patent/CA2285375C/en not_active Expired - Fee Related
  • 1998-03-25 WO PCT/FR1998/000598 patent/WO1998044182A1/fr not_active Ceased
  • 1998-03-25 KR KR10-1999-7008866A patent/KR100501632B1/ko not_active Expired - Fee Related

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