EP2705183A1

EP2705183A1 - Reinforcing textile thread for an inflatable sail, and rigging sail comprising such reinforcing textile threads

Info

Publication number: EP2705183A1
Application number: EP12718250.9A
Authority: EP
Inventors: Laurence Pollet; Cécile ROIBET; Sébastien FERAUDET
Original assignee: Porcher Industries SA
Current assignee: Porcher Industries SA
Priority date: 2011-05-05
Filing date: 2012-05-04
Publication date: 2014-03-12
Anticipated expiration: 2032-05-04
Also published as: EP2705183B1; PT2705183T; FR2974819A1; WO2012150334A1; US9234305B2; CN103534395B; CN103534395A; US20140060409A1; FR2974819B1; DK2705183T3

Abstract

The invention relates to a reinforcing textile thread (82) for an inflatable sail, such as a rigging sail or a flight sail, including a plurality of filaments which are agglutinated so as to form an elongate unitary body (820), and a binder (822) which ensures the cohesion among at least some of the filaments (821) of the unitary body (820), and which consists of a coating material. In order to guarantee an effective, directed reinforcement effect within an inflatable sail without limiting the lifespan of said sail, the unitary body has, in the cross-section thereof, an oblong outline, wherein the ratio of the maximum width (e) of said outline, which corresponds to a thickness of the unitary body, to the maximum length (l) of said outline, which corresponds to a width of the unitary body, is less than 0.06, a plurality of filaments (821) being arranged in series over the thickness of the unitary body.

Description

TEXTILE REINFORCING YARN FOR AN INFLATABLE SAIL, AND

SAILING DEVICE COMPRISING SUCH TEXTILE REINFORCING YARNS

The present invention relates to a reinforcing textile yarn for an inflatable sail, such as a rigging sail or a flying sail. It also relates to a rigging sail, in particular a mainsail, comprising at least one such reinforcing textile thread.

On a sailboat, the mainsail is generally the lowest sail of the mainmast and the largest when fully deployed. For a long time, this sail was made by a taffeta made of polyester yarn. Recently, particularly in the field of competition rigging, it has been proposed to replace taffeta with lighter, stronger and more efficient complexes for transmitting wind propulsion efforts. These complexes are typically in the form of a membrane including two plastic films, which are laminated to each other, trapping between them a reinforcing grid. This grid consists of a set of son, arranged in a regular pattern, such as a rhombus or a square, which, by repetition, defines the entire grid. That is to say that the grid is a two-dimensional assembly son, often a weave, which can be associated with a rectilinear main direction and another rectilinear direction, for example perpendicular to the previous, both belonging to the plane of the grid. This structure gives the grid a tear resistance and, more generally, an ability to mechanically strengthen the two contiguous films of the complex, with properties that are not generally identical in all directions of the plane, but which are pre-established relative to to the aforementioned main direction, depending on the pattern of the grid.

Insofar as, within a sail, in particular a mainsail, the service constraints are established along curved stress lines, which generally connect in pairs the vertices and / or the edges of the sail. veil, the aforementioned grid is solicited, within the complex, in directions that change with respect to the main direction of the grid, with local risks of damage to the complex. To reinforce the complex, it is known to add thereto, interposed between the two films, a plurality of individual reinforcing threads, which are respectively oriented, within the complex, along predetermined lines of effort so that, in use, the stresses to which the sail is subjected are essentially, or almost exclusively, supported by these reinforcing threads, which are dimensioned accordingly in order to perpetuate the mechanical strength of the sail, while the other layers constituting the sail, that is, to say both films and the grid, can then be dimensioned, in terms of mechanical strength, minimally: the overall weight of the sail is reduced. In practice, the individual reinforcing threads generally used are aramid, carbon or polyester.

That being said, the use of these individual reinforcing threads induces practical problems. Indeed, given their considerable thickness compared to the thicknesses of the other constituents of the complex, these threads create significant relief discontinuities: in the long term, these discontinuities are delamination primers of the complex, as well as zones of wear of the complex by friction with the wind. These drawbacks are even more pronounced in the vertices of the sail, where the end parts of a large number of these threads are concentrated and superimposed, if necessary leaving free spaces, not occupied by the films or by glue of the complex. The life of the sail is then limited.

Similar technical considerations are found for rigging sails other than the mainsail, or even for other types of wind-blown sails, such as flight sails which are, among others, kite-surfing sails, paragliding, etc., when seeking to strengthen such inflatable sails by individual son oriented reinforcement.

In order to overcome the disadvantages explained above with regard to the individual reinforcing threads, WO-A-94/1118 proposed to replace these individual threads with strips each consisting of a plurality of parallel monofilaments, which , in a matrix linking them together, are arranged in a single layer whose thickness is equal to the diameter, typically less than 20 μηι, monofilaments. The sail obtained thus includes several of these strips so that the monofilaments of each of them extend in respective directions which are inclined relative to each other: within the complex constituting this sail, the intercrossing density of monofilaments are increased. This solution is attractive on paper, but is particularly difficult to implement because it requires the manufacture, including pultrusion, the strips detailed above, having a thickness of a single monofilament. In addition, this solution requires that each band occupies the entire extent of the complex thus representing a part of the total thickness of the complex whose flexibility is degraded: therefore, it is necessary to provide as many bands as of directions of stress lines to be reinforced, without, moreover, being able to continuously reinforce a line of effort with a curved profile. Furthermore, in a field remote from inflatable sails, EP-A-0 625 417 discloses a reinforcing thread which includes sheath, within which filaments run in a powder. The aerated structure of this powder is used to give great flexibility to the wire. In practice, this reinforcing thread can not be used within a laminated outer film complex.

The purpose of the present invention is to provide individual reinforcing son, which, while ensuring an effective oriented reinforcing effect for an inflatable sail, does not limit the life, especially without inducing premature wear.

For this purpose, the subject of the invention is a reinforcing textile yarn for an inflatable sail, as defined in claim 1.

The invention also relates to a rigging sail, as defined in claim 13.

One of the ideas underlying the invention is not to use individual reinforcing son whose cross section is round or close to a circle, but to use reinforcing son that can be described as flat or flattened. Thus, the reinforcement yarn according to the invention has an oblong cross section, that is to say a longer than wide cross section, whose width, in other words the thickness of the yarn when the latter is considered within an inflatable sail, in particular within the rigging sail according to the invention, is less than 0.06 times its length, that is to say 0.06 times the width of the wire when the latter is considered within the inflatable sail, it being understood that the length of the aforementioned wire corresponds to the dimension of this wire in its longitudinal direction within the inflatable sail. Due to their flat conformation, the individual reinforcing threads according to the invention do not induce significant variation in the total thickness of the inflatable sail, in the sense that the small variation of this thickness, in the zones where at least one of these son is accommodated by the rest of the inflatable sail, in particular by the two plastic films of the rigging sail according to the invention, without risk of delamination between these films. The flat threads also have the advantage of giving the inflatable sail a great flexibility, avoiding stiffening locally. In addition, the external relief of the inflatable sail, resulting from the presence of the flat reinforcing son, is very little pronounced or almost nonexistent, which creates very little or almost no resistance by friction for the wind. In addition, even in the areas of the inflatable sail where two or more flat reinforcing threads are superimposed, for example the tops of the rigging sail according to the invention, the cumulative thickness of the constituents of the inflatable sail remains moderate. : thus, the cohesion between the various reinforcing threads and the grid is maintained without material discontinuity by the two contrecellant films of the rigging sail according to the invention.

In practice, various methods of manufacturing a reinforcing thread according to the invention, as well as various methods of manufacturing the inflatable sail incorporating such reinforcement son are possible by the specialists of the field, without departing from the scope of this invention. It is the same for the materials constituting the various components of the inflatable sail, including the materials constituting his reinforcing son.

Additional advantageous features of the reinforcing textile yarn according to the invention and / or the rigging sail according to the invention, taken individually or in any technically possible combination, are specified in claims 2 to 12 and 14 to 16.

The invention also relates to a rig as defined in the claim

17.

The invention will be better understood on reading the description which follows, given solely by way of example and with reference to the drawings in which:

- Figure 1 is a schematic perspective view of a sailboat equipped with a rig according to the invention;

FIG. 2 is a schematic exploded perspective view showing the constituents of the circled sail area II in FIG. 1;

- Figure 3 is a schematic section along the plane III of Figure 2;

- Figure 4 is a schematic view, on a larger scale, of the circled area IV in Figure 3; and

- Figure 5 is a partial schematic section of the sail, in the assembled state, of Figure 2.

In FIG. 1 is shown a sailboat 1 whose rigging 2 comprises, among other things, a mainsail 3 connected to a mast 4 belonging to the rigging 2, typically by ropes not shown in FIG.

As shown very schematically in Figure 2, the mainsail 3 consists of a tissue complex, corresponding to the superposition of several layers joined together. In practice, it will be noted that the mainsail 3 can be made of a single piece of complex or, more frequently, the mainsail consists of several coupons complex, individually shaped flat and assembled to each other to form jointly the mainsail. As can be clearly seen in FIG. 2, the mainsail complex 3 comprises at least four superimposed layers, namely two opposing films 5 and 6 constituting the two faces. opposite of the mainsail, and between these films 5 and 6, a grid 7 and a layer 8 consisting of a plurality of individual son, which are three in number in the example shown in Figure 2, in being respectively referenced 81, 82 and 83. In FIG. 2, Z is the rectilinear direction corresponding to the thickness of the mainsail complex 3: thus, one succeeds in this superimposed direction Z, the film 5, the grid 7, the layer 8 of the son 81, 82 and 83, and the film 6. In the assembled state of the mainsail complex 3, while this complex is laid flat on a flat surface, the different layers components of the complex extend generally in a plane perpendicular to the Z direction.

Of course, in service, that is to say when the mainsail 3 is inflated by the wind for the purpose of propulsion of the boat 1, the complex generally has a three-dimensional geometry, more or less domed shape.

The films 5 and 6 are made of plastic material, being noted that, in practice, the same plastic is used for both films. By way of non-limiting example, the above-mentioned plastics material is polyester, advantageously treated to resist ultraviolet: it may especially be polyethylene terephthalate (PET), optionally mixed with a fluoropolymer of the PVDF type, such as than polyvinylidene fluoride. Also by way of non-limiting example, the thickness of each film 5, 6 is typically of the order of ten micrometers, for example between 5 and 50 μηι.

The gate 7 comprises, or as in the embodiment considered in the figures, consists of an assembly of rectilinear son 71 arranged relative to each other by repeating, regularly in the plane of the grid 7, a predetermined basic pattern. Thus, in the exemplary embodiment considered in FIG. 2, this pattern consists of a rhombus completed with one of its diagonals. In other words, by regular repetition of the aforementioned pattern, in the two directions defined by the plane of the grid 7, the whole of this grid is obtained. Thus, the various wires 71 constituting the grid 7 are positioned relative to one another according to a pre-established geometry, both in relative orientation and in relative spacing in the plane of the grid.

By way of non-limiting example, the son 71 are made of polyester, aramid, carbon, etc. Moreover, within the same grid 7, son 71 made of different respective materials and with different respective titles can be mixed.

According to a preferred embodiment, the threads 71 of the grid 7 are interwoven in the manner of a fabric with some of the threads acting as weft threads, while the other threads act as warp threads. As a variant, the wires 71 do not intersect not, but are superimposed, being divided into at least two superimposed layers. If necessary, the son 71 are, at their intersections or their crossings, glued or welded to each other. As a detailed example, the reader can consult the document EP-A-1 1 1 1 1 14.

The thickness of the grid 7 is equal to the thickness of the wires 71 for the most part of this grid, except in the quasi-point areas where at least two of the wires 71 intersect or intersect, overlapping in the direction Z, areas in which the thickness of the grid 7 is locally increased at most as many times as the number of son 71 overlapping. By way of non-limiting example, the thickness of the wires 71, and thus the thickness of the grid 7, except for the overlap areas of several wires 71, may be of the order of a hundred or a few hundred micrometers. , or even more, depending in particular on the title of the threads.

Within the complex of the mainsail 3, the function of the grid 7 is to mechanically strengthen the contiguous films 5 and 6, typically by increasing the resistance of the complex to tearing. More generally, as explained in the introductory part of this document, the intercrossing of the wires 71 give the grid 7 mechanical strength properties, which are different in the direction in the plane of the grid, depending on the geometry of the pattern elementary of this interlacing.

Unlike the wires 71 of the grid 7, the wires 81, 82 and 83 of the layer 8 are individual wires, in the sense that, before assembly of the mainsail complex 3, these wires 81, 82 and 83 are mechanically independent of each other. Within the complex of mainsail 3, the son 81, 82 and 83 have the function of reinforcing this complex, being oriented along predetermined lines of effort and, in particular, curved stress lines: thus, each of the son 81, 82 and 83 extends in length, in the plane of the mainsail complex 3, in a proper longitudinal direction X81, X82, X83, possibly curved, as shown in FIG. in a manner known per se, each of these wires 81, 82, 83 thus follows, along its longitudinal direction X81, X82, X83, a prefixed path, along which it has been predetermined, in particular by ad hoc prior calculations, that Significant constraints will apply to the mainsail complex 3 when this mainsail is in service, especially at a given pace. Thus, as explained in the introductory part of this document, the stresses applied to the mainsail complex 3 are then supported, essentially or almost entirely, by one or more of the wires 81, 82 and 83. which are sized accordingly. The advantage is then that the other constituents of the complex, that are the films 5 and 6 and the grid 7, can be dimensioned, in terms of mechanical strength, minimally, which, between other, reduces the overall weight of the mainsail 3. As a non-limiting example, at least some of the aforementioned lines of effort connect the vertices of the mainsail 2 in pairs in a curved manner in the plane of the mainsail. complex of this mainsail.

Subsequently, we will describe in more detail, especially with reference to FIGS. 3 to 5, the wire 82, it being understood that the following considerations apply to the other wires 81 and 83 of the layer 8. Of course, understands that, in practice, the total number of reinforcing threads, similar to threads 81, 82 and 83, within the mainsail complex 3 is generally much larger than three.

Thus, the wire 82 comprises, or, as in the example considered here, consists of an assembly body 820 which extends in length in the direction X82, being substantially centered on an axis geometrically materializing the direction X82.

As can be clearly seen in FIG. 3, the wire 82 does not have, in cross-section along its longitudinal direction X82, a circular profile or even close to a circle, as might be expected for a traditionally used textile reinforcement yarn in the field concerned here. In contrast, the cross-section of the assembly body 820 of the wire 82, i.e. its section in a geometric plane perpendicular to its longitudinal direction X82, has an oblong shape, i.e. a shape significantly longer than wide. Considering the wire 82 according to its overall volume, this amounts to saying that the body 820 has a width significantly greater than its thickness, it being agreed that the thickness of the wire is its dimension considered in the Z direction while its width is its dimension which, in the plane of the mainsail complex 3, is perpendicular to the longitudinal direction X82. Thus, in FIG. 3, the length of the elongated section of the overall body 820 of the wire 82 is noted, while e is the width of this oblong section, respectively with reference to the width and the thickness of the wire 82. Of course, by definition, the width / wire 82 is significantly smaller than the corresponding dimension of the films 5 and 6, so that, in the assembled state of the complex constituting the mainsail 3, the wire does not cover the entire area with respect to each of the films 5 and 6, but, on the contrary, covers only a limited fraction, which ensures a good flexibility to the complex.

Thus, the wire 82 may be described as flat or flattened wire, which for the purposes of this document consists in providing that the ratio e // between its thickness and its width, ie the ratio between the maximum width and the length of the oblong section of its overall body 820 is less than 0.06, or preferably less than 0.05.

In practice, the flat or flattened shape of the overall body 820 of the wire 82 is related to the constitution of this overall body. Indeed, as shown schematically in FIG. 4, the body 820 is not a single piece, but results from the agglutination of a large number of elementary filaments 821: each of these filaments 821 can be individually dissociated from the others and, in this sense, can so be called monofilament. Individually, it can be considered that each of these filaments 821 has, in cross section along the axis X82, a substantially circular section, with a diameter of the order of ten micrometers, in particular between 3 and 30 μηι. When considering these filaments 821 in the agglutinated state within the assembly body 820, these filaments 821 are arranged relative to each other to give this overall body 820 the oblong section described above, being noted that several hundreds or even one or a few thousand filaments, in other words at least two hundred, or even at least one thousand filaments, are thus agglutinated to form the overall body 820. As a result, the thickness e of the overall body 820 is greater than 50 μηι, being in particular of the order of one-tenth of a millimeter, which is to say that, in the direction Z, several filaments 821, in particular one or even several tens of filaments 821 succeed each other over the thickness 820. More precise quantitative examples will be given at the very end of this description.

According to preferred embodiments, the filaments 821 are made either of an organic material, in particular aramid, polyamide, polyester, especially aromatic polyester, such as VECTRAN (registered trademark), or polyethylene, especially polyethylene high density (HDPE) or polyethylene naphthalate (PEN), such as PENTEX (registered trademark), or a mineral material, especially carbon or glass.

According to the embodiment shown in Figures 3 and 4, the overall body 820 of the wire 82 is glued, heart and, advantageously, externally. More specifically, as shown schematically in Figure 4, glue or, more generally, a coating material is provided interposed between the filaments 821, thereby forming a bonding binder 822 between these filaments. In addition, a coating material is advantageously provided wrapping around the filaments 821 located at the periphery of the overall body 820, so as to form a coating sheath 823 of this body 820. Although, as a variant not shown, only the binder 822is actually present, this binder 822 and the sheath 823 are advantageously associated, being, in practice, constituted by the same constitutive adhesive, in particular applied by sizing, more generally by coating.

The binder 822 and the sheath 823 help to hold the filaments 821 in place within the overall body 820. In addition, the binder 822 is specifically designed to function of limiting or even preventing water infiltration by capillarity in the overall body 820. As for the sheath 823, it specifically has the additional function of facilitating the use of the wire 82, in particular by allowing its winding and / or by improving its physico-chemical integration within the mainsail complex 3, as mentioned below.

The coating material or materials used to form the binder 822 and the sheath 823 are advantageously based on a polymer, in particular based on acrylic, polyurethane or polyethylene. Specific references of usable glues are given at the very end of the description.

Because of the presence of the binder 822 and, advantageously, the sheath 823, the overall body 820 has a part of its mass of the coating material constituting this binder and, if appropriate, this sheath. It is thus possible to define a coating ratio of the overall body 820, which is defined as a hundred times the ratio between, on the one hand, the difference between the title of the coated wire and the title of the uncoated wire, and, d on the other hand, the title of the uncoated wire. In practice, this coating rate is between 5 and 100%. It is preferably less than 50%, for reasons related in particular to the final weight of the mainsail complex 3.

In practice, various geometries are possible for the cross section of the overall body 820, provided that these geometries have an oblong contour. Thus, in the embodiment illustrated schematically in FIG. 3, the contour of the cross section of the assembly body 820 has two substantially flat opposed segments 820A and 820B, between which the width of its contour is defined, that is, The thickness e of the overall body 820. This amounts to saying that the segments 820A and 820B extend substantially perpendicularly to the direction Z, being separated from the distance e. The respective ends of these flat segments 820A and 820B are connected in pairs by two opposed segments 820C and 820D of the transverse contour of the assembly body 820, these segments 820C and 820D being convex, in particular by continuously connecting the flat segments 820A and 820B. . Of course, the segments 820A and 820B are not strictly flat, in the sense that they are defined by a succession of filaments 821 located at the periphery of the overall body 820, where appropriate covered by a portion of the sheath. 823. This embodiment has the advantage that the thickness e of the overall body 820 has a substantially constant value over most of the width of this body, especially without having, in the direction of the width of the body 820 , a local maximum value. This amounts to saying that the flat or flattened shape according to the invention is thus optimized. That being said, as a variant not shown, the oblong contour of the cross section of the assembly body 820 can correspond substantially to an ellipse or, more generally, to a substantially elliptical contour, which is centered on an axis that geometrically embodies the direction X82 and whose minor axis extends in the direction Z. In this case, the ratio between the maximum width and the maximum length of this contour corresponds to the ratio between the small radius and the large radius of the elliptical shape.

More generally, other geometries than those mentioned above are conceivable for the transverse oblong contour of the overall body 820.

According to an advantageous aspect, in the case where the filaments 821 are aramid, the ratio between the title of the wire 82 and the width / of its overall body 820 is provided less than a predetermined value. This amounts, for a given yarn, to provide a thickness e of the overall body 820 sufficiently small so that the filaments 821 of this body are distributed over a large width. Thus, the aforementioned ratio is advantageously less than 1000 (thousand), by expressing the title of the overall body 820 uncoated in dTex and expressing its width /, that is to say the length of its oblong contour in millimeters.

As mentioned above, various methods can be envisaged to manufacture the wire 82.

By way of example, one of these processes consists of starting from a pre-existing wire with a substantially circular cross-section, and then subjecting it to one or more flattening operations, accompanied, where appropriate, by coating operations, in particular sizing, in order to result in the structure of the wire 82 presented in detail above. With regard to sizing, the reader may, by way of a detailed example, refer to document US-A-2010/0089017. Alternatively, the wire 82 may be manufactured directly from the filaments 821, including arranging them relative to each other to obtain the structure described above. In all cases, a flattened or flat wire is advantageously capable of being wound and stored for later use, in particular for manufacturing the mainsail complex 3.

Similarly, the manufacture of the mainsail complex 3, that is to say the assembly of the films 5 and 6, the grid 7 and the son 81, 82 and 83, can be achieved by various methods. By way of example, from the film 5, the grid 7, coming for example from a coil, is deposited on it successively, and the wires 81, 82 and 83, the latter being obtained in particular by cutting from a coil of wire as the one mentioned in the previous paragraph, then the film 6 is reported on the semi-complex thus formed, in order to obtain the complete complex. As an alternative, the grid 7 and the son 81, 82 and 83 are initially prepositioned between the films 5 and 6, before constraining the joining of these films, in particular by creating a depression between them. The films 5 and 6 are held together by any appropriate means, especially by gluing, the glue can be made externally or be integrated with one and / or the other of the films. Advantageously, this glue effectively binds to sheath 823.

In any case, at the end of the manufacturing process, the complex of the mainsail 3 has the schematic configuration of FIG. 5, with, among other things, the wires 71 of the grid 7 and the wire 82 trapped between them. 5 and 6. This schematic representation of FIG. 5 illustrates that the presence of the wire 82 does not induce significant relief discontinuity for the complex, particularly compared to the wires 71 of the grid 7. In particular, even though method of manufacturing the grid 7 and / or the method of manufacturing the complex would tend to ovalize the cross section of the son 71, slightly crushing the latter in the Z direction, the oblong contour of the cross section of the wire 82 is clearly distinguishable from the cross section of the son 71, in the sense that, for respective titles substantially identical for the son 71 and the son 82, the thickness e of the assembly body 820 of the wire 82 is advantageously au ns twice smaller than that of the wires 71 of the grid 7 in the direction Z.

Note that, given the flattened or flat shape that son 81, 82 or 83 before assembly to the rest of the mainsail complex 3, their maximum thickness e, in other words the maximum width of their transverse contour oblong, is not modified during the manufacture of the complex, except in marginal proportions, not significant vis-à-vis the dimensions of the overall body 820, especially vis-à-vis the ratio e / /. In addition, as mentioned above, several of the son 81, 82 and 83 can partially be superimposed in the direction Z: such a superposition results from the drawing of the lines of effort respectively along which run these son. This is typically the case at the tops of the mainsail 3.

Before presenting specific examples of embodiments below, it will be noted that various arrangements and variants to the complex of the mainsail 3, in particular to the reinforcing threads 81, 82, 83, are conceivable:

For example, the complex of the mainsail 3 can include at least one additional layer, in the form of a taffeta, corresponding to a polyester fabric, for example from 40 to 90 g / m ² ; in practice, this additional layer of taffeta is either interposed between the films 5 and 6, in a position of indifferent interposition vis-à-vis the grid 7 and the layer of reinforcing son 8, or be reported in overlay to Mon and / or the other of films 5 and 6; in all cases, this or these additional layers of taffeta weigh down the complex of the mainsail 3, but give it a more traditional aesthetic, that is to say, an aesthetic reminiscent of the mainsails constituted exclusively of such polyester fabric;

- At the tops of the mainsail 3, additional pieces of fabric can reported in a manner superimposed on the complex, for local reinforcement purposes;

- Of course, other rigging sails that mainsail 3, such as a spinnaker or a gennaker, can be made in a complex as described so far; and or

The individual reinforcing threads described heretofore described, such as the threads 81, 82 and

83, can be integrated with other inflatable sails that rigging sails, in the sense that such inflatable sails allow, under the action of wind or a gas, to produce a traction effect or levitation vis- a body connected to the inflatable sail; in particular, flight sails, such as paragliding, kite-surfing, hang gliding, kite flying, parachute, aerostat balloon, etc., are advantageously affected.

EXAMPLES EXAMPLE 1 Reinforcing yarn 81, 82, 83, which includes 2,000 filaments made of aramid, more precisely KEVLAR®, which has a titer of 3,300 dTex, which is coated at 30% by weight. an acrylic adhesive, such as the adhesive marketed under the reference "UCECOAT DW 3134" from CYTEC, and which has a width / equal to 4 mm and a maximum thickness e equal to 0.1 mm.

With the aid of a TABER stiffness meter, it is measured that this thread has a stiffness of 8.8 TABER stiffness units, ie 0.8 TSU (for "Taber Stiffness Units", corresponding to reference units). being carried out on test pieces of three wires 3 cm long and with a deflection angle of 15%. This measurement reflects a great flexibility for the yarn of Example 1, in particular by comparison with a yarn having the same constituents but substantially round section, whose stiffness was measured at 56.6 TABER stiffness units, or 5 TSU.

Example 2: reinforcing thread 81, 82, 83, which includes 1000 filaments of aramid, which has a title of 1 680 dTex, which is coated with 30% of a polyester-polyurethane type glue, such as glue marketed under the reference "PRIMAL NW- 1845K "of the company ROHM-AND-HAAS, and which has a width / equal to 2.7 mm and a maximum thickness e equal to 0.1 mm.

Example 3: reinforcing thread 81, 82, 83, which comprises polyester filaments, more specifically VECTRAN (registered trademark), which has a title of 2530 dTex, which is coated with 21% of an acrylic glue, such as the adhesive sold under the reference "PRIMAL E 941 P" of the company ROHM-AND-HAAS and which has a width / equal to 2.7 mm and a thickness e equal to 0.16 mm.

Example 4: reinforcing thread 81, 82, 83, which comprises carbon filaments, which has a title of 8 200dTex, which is coated with 25% of a polyether-polyurethane glue, such as the glue marketed under the reference " IMPRANIL LP RSC 4002 "from Bayer, which has a width / equal to 5 mm and a thickness e equal to 0.18 mm.

Claims

1. Reinforcement textile yarn (81, 82, 83) for an inflatable sail, such as a rigging sail (3) or a flying sail,

comprising a plurality of filaments (821), which are agglutinated to form an elongated body assembly (820), and a binder (822) for cohesion between at least some of the filaments (821) of the assembly body (820), which consists of a coating material, characterized in that, in cross section, the overall body (820) has an oblong contour whose ratio between its maximum width (e), which corresponds to a thickness of the body overall and its maximum length (ή, which corresponds to a width of the overall body, is less than 0.06, several filaments (821) succeeding one another over the thickness of the overall body.

2. - Thread according to claim 1, characterized in that the thickness of the overall body (820) is greater than 50 μηι.

3. - Thread according to one of claims 1 or 2, characterized in that a dozen filaments (821) succeed each other over the thickness of the overall body (820).

4. Wire according to one of claims 1 or 2, characterized in that several tens of filaments (821) succeed each other over the thickness of the overall body (820).

5. - Thread according to any one of the preceding claims, characterized in that it further comprises a sheath (823) for coating the assembly body (820).

6. - Thread according to claim 5, characterized in that the sheath (823) consists of a coating material which is identical to that constituting the binder (822).

7. - Thread according to one of claims 5 or 6, characterized in that the coating material constituting the binder (822) and / or a coating material constituting the sheath

(823) are each based on a polymer, in particular based on acrylic, polyurethane or polyethylene.

8. - Thread according to any one of the preceding claims, characterized in that the oblong contour of the assembly body (820) has two opposite segments.

(820A, 820B) substantially flat, between which is defined the width (e) of the contour.

9. - Thread according to any one of the preceding claims, characterized in that the filaments (821) are made of an organic material, in particular aramid, polyamide, polyester or polyethylene, or a mineral material, especially in carbon or glass.

10. Thread according to any one of the preceding claims, characterized in that the coating rate of the overall body (820) is between 5 and 100%.

1 1. Yarn according to claim 10, characterized in that the coating rate of the overall body (820) is between 5 and 50%.

12. - Thread according to claim 1 1, characterized in that, in the case where the filaments (821) are made of aramid, the body assembly (820) has a ratio between, on the one hand, its expressed title in dTex, and, on the other hand, the maximum length (ή of its oblong contour, expressed in millimeters, whose value is less than 1000.

13. - Rigging sail (3),

comprising two plastic films (5, 6), which are laminated to one another and between which are interposed, in a superposition direction (Z) defined by the thickness of the films, both a grid of reinforcement (7), which has a predetermined pattern of repetition, and at least one individual reinforcing textile thread (81, 82, 83), which is oriented along a predetermined line of effort,

characterized in that the or each reinforcing textile yarn (81, 82, 83) is in accordance with any one of the preceding claims and is arranged so that, in cross-section, the width (e) of the oblong contour of its body assembly (820) extends in the direction of superposition (Z).

14. - Sail according to claim 13, characterized in that the or each reinforcing wire (81, 82, 83) covers only a limited fraction of the surface facing each of the two films (5, 6).

15. - Sail according to claim 13 or claim 14, characterized by a plurality of reinforcing textile threads (81, 82, 83), at least two of which are partially superimposed in the direction of superposition (Z).

16.- Sail according to any one of claims 13 to 15, characterized in that, in the case where the reinforcing grid (7) consists essentially of son (71) whose title is substantially identical to that of the body d together (820) of the or each reinforcing textile yarn (81, 82, 83), the width (e) of the oblong contour of the assembly body (820) is at least two times smaller than the corresponding dimension of the yarns (71) of the reinforcing grid (7) in the superposition direction (Z).

17. Rigging, characterized in that it comprises a mainsail (3) according to any one of claims 13 to 16.