FR2501579A1 - Composite fibre reinforced profiles for sail-board masts - with longitudinal reinforcement of differing lengths for progress stiffness variation overall - Google Patents
Composite fibre reinforced profiles for sail-board masts - with longitudinal reinforcement of differing lengths for progress stiffness variation overall Download PDFInfo
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- FR2501579A1 FR2501579A1 FR8105261A FR8105261A FR2501579A1 FR 2501579 A1 FR2501579 A1 FR 2501579A1 FR 8105261 A FR8105261 A FR 8105261A FR 8105261 A FR8105261 A FR 8105261A FR 2501579 A1 FR2501579 A1 FR 2501579A1
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- Prior art keywords
- tubular structure
- son
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- textile
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Classifications
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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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/805—Applying axial reinforcements
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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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
- B29C53/62—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis
- B29C53/66—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis with axially movable winding feed member, e.g. lathe type winding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B15/00—Superstructures, deckhouses, wheelhouses or the like; Arrangements or adaptations of masts or spars, e.g. bowsprits
- B63B15/0083—Masts for sailing ships or boats
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C1/00—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof
- D04C1/06—Braid or lace serving particular purposes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2023/00—Tubular articles
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2101/00—Inorganic fibres
- D10B2101/02—Inorganic fibres based on oxides or oxide ceramics, e.g. silicates
- D10B2101/06—Glass
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2403/00—Details of fabric structure established in the fabric forming process
- D10B2403/02—Cross-sectional features
- D10B2403/024—Fabric incorporating additional compounds
- D10B2403/0241—Fabric incorporating additional compounds enhancing mechanical properties
- D10B2403/02411—Fabric incorporating additional compounds enhancing mechanical properties with a single array of unbent yarn, e.g. unidirectional reinforcement fabrics
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/02—Reinforcing materials; Prepregs
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
STRUCTURE TUBULAIRE UTII,ISABLE NOTAMMENT POUR LA REALISATION
DE MATS DE VOILIERS DE PLAISANCE.UTII TUBULAR STRUCTURE, ISABLE IN PARTICULAR FOR REALIZATION
OF MATS OF SAILING YACHTS.
La présente invention a trait à un nouveau type de structure tubulaire stratifiée constituée de gaines textiles superposées et imprégnées par une résine appropriée. Elle a trait plus particulièrement à un nouveau type de structure tubulaire présentant une flexibilité variable sur sa longueur et qui, notamment, est particulièrement adaptée pour la réalisation de mâts de voiliers de plaisance. The present invention relates to a new type of laminated tubular structure consisting of superimposed textile sheaths and impregnated with a suitable resin. It relates more particularly to a new type of tubular structure having a variable flexibility over its length and which, in particular, is particularly suitable for the production of masts of sailing yachts.
Dans la suite de la description, l'invention sera décrite plus particulièrement pour cette application mais il est évident que cela n'est pas limitatif et qu'une telle structure pourrait éventuellement être utilisée dans d'autres domaines, par exemple pour réaliser des perches, des poteaux... In the following description, the invention will be described more particularly for this application, but it is obvious that this is not limiting and that such a structure could possibly be used in other fields, for example for making poles. , polls...
Pendant très longtemps, le matériau utilisé pour réaliser des mâts de voiliers a été le bois. Depuis un certain nombre d'années, on réalise des mâts métalliques, notamment en alumi sium et tout récemment il a été proposé de faire appel aux techniques utilisées pour la réalisation de stratifiés c'està-dire de matériaux constitués d'une résine polymérisable renforcée par une structure textile. For a very long time, the material used to make sailboat masts was wood. For a number of years, metal masts have been produced, in particular in alumi sium and quite recently it has been proposed to use the techniques used for the production of laminates, that is to say materials made of a reinforced polymerizable resin. by a textile structure.
Ainsi, on a proposé de réaliser des mâts par bobinage d'un tissu mixte, fibre de verre/carbone, renforcé longitudinalement de fibres de carbone unidirectionnelles, l'ensemble étant imprégné de résine polymérisable. Ce type de mât permet d'obtenir une certaine souplesse dans le sens longitudinal, ce qui améliore le rendement de la voilure et autorise l'utilisation d'une voile à deux plis qui ceinture le mât et est maintenu en place par un "Wishbone". Thus, it has been proposed to produce masts by winding a mixed fabric, glass fiber / carbon, reinforced longitudinally with unidirectional carbon fibers, the assembly being impregnated with polymerizable resin. This type of mast makes it possible to obtain a certain flexibility in the longitudinal direction, which improves the performance of the wing and allows the use of a two-ply sail which surrounds the mast and is held in place by a "Wishbone" .
Par ailleurs, dans sa demande de brevet français no 79/12 533, la Demanderesse a proposé une structure tubulaire composite à couches multiples qui peut être utilisée pour réaliser des mâts de planche à voile. Cependant, le matériau faisant l'objet de cette demande n'est pas adapté à la fabrication de mâts pour voiliers conventionnels étant donné que pour une telle application, le mât doit être pratiquement rigide jusqu'au tiers de sa hauteur alors qu'il doit présenter une flexibilité progressif jusqu'à son sommet. Par opposition, un mât de planche à voile doit pouvoir fléchir pratiquement depuis sa base jusqu'à son extrémité et ne comporte pas de partie rigide. Furthermore, in its French patent application No. 79/12 533, the Applicant has proposed a composite multilayer tubular structure which can be used to make windsurf masts. However, the material which is the subject of this request is not suitable for the manufacture of masts for conventional sailboats since, for such an application, the mast must be practically rigid up to a third of its height whereas it must present progressive flexibility to the top. In contrast, a windsurf mast should be able to flex practically from its base to its end and has no rigid part.
Or on a trouvé, et c'est ce qui fait l'objet de la présente invention un nouveau type de stucture tubulaire qui, non seulement est simple et économique à réaliser mais qui, par ailleurs, permet d'obtenir des mâts de toutes dimensions, ces mâts présentant en outre une flexibilité progressive de leur base à leur sommet, une première partie du mât s'étendant depuis la base sur une longueur relativement importante, en général égale au 1/3 de la longueur totale du mât, étant pratiquement rigide alors que la partie restante dudit mât présente une flexibilité variable sur sa longueur. Now we have found, and this is what is the subject of the present invention, a new type of tubular structure which not only is simple and economical to produce but which, moreover, makes it possible to obtain masts of all dimensions. , these masts also having progressive flexibility from their base to their top, a first part of the mast extending from the base over a relatively large length, generally equal to 1/3 of the total length of the mast, being practically rigid while the remaining part of said mast has variable flexibility along its length.
D'une manière générale, l'invention concerne donc une structure tubulaire du type comportant une pluralité de couches textiles superposées, au moins la couche interne et la couche externe étant constituées par des gaines tressées bidirectionnelles, s'étendant sur toute la longueur du matériau et cette structure étant caractérisée par le fait qu'entre les deux couches extrêmes sont disposées une pluralité de gai intermédiaires, constituées au moins pour partie majoritaire de fils longitudinaux, s'étendant depuis une extrémité de la structure sur des longueurs de plus en plus courtes lorsque l'on va de la couche interne à la couche externe. In general, the invention therefore relates to a tubular structure of the type comprising a plurality of superposed textile layers, at least the internal layer and the external layer being constituted by bidirectional braided sheaths, extending over the entire length of the material. and this structure being characterized by the fact that between the two extreme layers are arranged a plurality of intermediate cheeks, constituted at least in the majority of longitudinal wires, extending from one end of the structure over increasingly short lengths when we go from the inner layer to the outer layer.
Ces différentes couches textiles sont, de manière conventionnelle, imprégnées avec une résine polymérisable. These different textile layers are conventionally impregnated with a polymerizable resin.
Comme matière textile pouvant entrer dans la constitution tant des gaines tressées bidirectionnelles que des couches intermédiaires à base de fils longitudinaux, on peut utiliser des fils de verre, des fils à module d'élasticité élevée tels que ceux à base de bore, de carbone, d'aramide... As textile material which can enter into the constitution both of bidirectional braided sheaths and of intermediate layers based on longitudinal threads, it is possible to use glass threads, threads with a high modulus of elasticity such as those based on boron, carbon, aramid ...
Dans la suite de la description, l'invention sera décrite pour un matériau entièrement à base de fils de verre mais, bien entendu, cela n'est pas limitatif et l'on pourrait, comme dans tout stratifié, utiliser des combinaisons diverses de matières par exemple réaliser les couches internes et externes en verre et les couches intermédiaires en carbone ou autres ou avoir dans une même couche une alternance de fils différents par exemple une alternance de fils de verre et de fils de carbone. In the following description, the invention will be described for a material entirely based on glass strands but, of course, this is not limiting and one could, as in any laminate, use various combinations of materials for example making the internal and external layers of glass and the intermediate layers of carbon or other or having in the same layer an alternation of different threads, for example an alternation of glass threads and carbon threads.
Par ailleurs, au sens de la présente invention, par "gaines tressées bidirectionnelles", on désigne une ti-esse constituée de deux séries ou groupes de fils de pi-éférence identiques, entrecroisé et disposés suivant un angle déterminé par rapport aux génératrices de ladite gaine, l'inclinaison des fils étant en général, avant mise en place du matériau, voisine de 45o. De telles tresses présentent comme caractéristiques de pouvoir se déformer aussi bien dans le sens longitudinal que dans le sens latéral et par suite de pouvoir prendre une forme autre que cylindrique, tronconique par exemple. Furthermore, within the meaning of the present invention, by "bidirectional braided sheaths" means a ti-esse consisting of two series or groups of son of identical pi-éference, crisscrossed and arranged at a determined angle relative to the generatrices of said sheath, the inclination of the wires being generally, before placing the material, close to 45 °. Such braids have the characteristic of being able to deform both in the longitudinal direction and in the lateral direction and as a result of being able to take a shape other than cylindrical, frustoconical for example.
Par ailleurs, si les gaines textiles intermédiaires peuvent être constituées uniquement de fils longitudinaux, parallèles entre eux, ne comportant aucun élément de liaison, dans une forme préférentielle de l'invention les fils longitudinaux seront maintenus entre eux par des fils de liage tressés, ces fils de liage étant relativement fins par rapport aux fils longitudinaux et ne constituant qu'une partie minoritaire de l'ensemble. Furthermore, if the intermediate textile sheaths can consist only of longitudinal threads, parallel to each other, comprising no connecting element, in a preferred form of the invention the longitudinal threads will be held together by braided binding threads, these tying threads being relatively fine compared to the longitudinal threads and constituting only a minority part of the whole.
En outre, si dans chaque couche intermédiaire les fils longitudinaux peuvent avoir des longueurs identiques, dans certains cas il peut être envisagé d'avoir des fils de longueurs différentes. Ainsi, dans chaque couche intermédiaire, on peut envisager d'avoir des fils alternativement plus longs et plus courts. C'est un mode de réalisation qui favorise l'ob tention d'une structure tubulaire de forme tronconique présentant une pente relativement importante. Si en général, la couche interne et la couche externe desdites structures tubulaires sont constituées par une seule gaine tressée bidirectionnelle il peut être envisagé, pour certaines applications, d'avoir par exemple une couche externe constituée de deux gaines tressées bidirectionnelles superposées. In addition, if in each intermediate layer the longitudinal wires can have identical lengths, in some cases it can be envisaged to have wires of different lengths. Thus, in each intermediate layer, it is possible to envisage having alternately longer and shorter wires. It is an embodiment which favors the obtaining of a tubular structure of frustoconical shape having a relatively large slope. If in general, the inner layer and the outer layer of said tubular structures are constituted by a single bidirectional braided sheath, it may be envisaged, for certain applications, to have, for example, an external layer constituted by two superimposed bidirectional braided sheaths.
L'invention et les avantages qu'elle apporte seront cependant mieux compris grâce à l'exemple de réalisation donné ci-après à titre indicatif mais non limitatif et qui est illus- tré par les schémas annexés dans lesquels
- la figure 1 illustre en perspective, de manière schématique, une structure tubulaire réalisée conformement à l'invention,
- les figures 2, 3 et4 sont également des vues en perspective schématiques montrant plus en détail les différents types de matériaux pouvant entrer ds la réalisation d'une telle structure tubulaire.The invention and the advantages which it brings will however be better understood thanks to the example of embodiment given below by way of indication but not limitation and which is illustrated by the attached diagrams in which
FIG. 1 illustrates in perspective, schematically, a tubular structure produced in accordance with the invention,
- Figures 2, 3 and 4 are also schematic perspective views showing in more detail the different types of materials that can enter the realization of such a tubular structure.
Conformément à l'invention, on réalise une structure tubulaire tronconique ayant une longueur totale de 9,50 m, un diamètre intérieur D de 106 mm à la base et d de 50 mm au sommet. In accordance with the invention, a frustoconical tubular structure is produced having a total length of 9.50 m, an internal diameter D of 106 mm at the base and d of 50 mm at the top.
Pour réaliser une telle pièce, on utilise un mandrin tronconique 1 en acier (ou tout autre matériau) ayant les dimensions précitées et qui est monté à port#e-à-faux pour permettre la mise en place des différentes couches textiles. Sur ce mandrin, préalablement revêtu d'une couche d'un agent démoulant conventionnel, on enfile une première gaine tressée bidirectionnelle, s'étendant sur toute la longueur ayant une structure telle que celle illustrée à la figure 4. Cette gaine est constituée de deux séries ou groupes de fils entrecroisés 3-4 qui forment entre eux un angle d'envircn 400. Compte-tenu des possibilités de déformation d'une telle structure, il est possible d'adapter parfaitement la gaine autour du mandrin 1. To make such a part, a frusto-conical mandrel 1 made of steel (or any other material) having the aforementioned dimensions is used and which is mounted in port # e-à-faux to allow the establishment of the various textile layers. On this mandrel, previously coated with a layer of a conventional release agent, a first bidirectional braided sheath, threaded over the entire length, having a structure such as that illustrated in FIG. 4, is threaded. series or groups of crisscrossed wires 3-4 which form an angle of approx. 400 between them. Given the possibilities of deformation of such a structure, it is possible to perfectly adapt the sheath around the mandrel 1.
Dans le cas présent, cette gaine tressée bidirectionnelle a, avant mise en place, un diamètre nominal de 110 mm et est constituée de deux groupes de fils de verre entrecroisés, chaque groupe comportant 48 fils de verre ayant chacun un titre global de 52 000 Tex.In this case, this bidirectional braided sheath has, before installation, a nominal diameter of 110 mm and is made up of two groups of interlaced glass strands, each group comprising 48 glass strands each having an overall titer of 52,000 Tex .
Compte-tenu des possibilités de déformation d'une telle structure textile, cette gaine épouse parfaitement la surface du mandrin. Cette gaine étant mise en place, on en fixe les extrémités sur le mandrin par exemple au moyen d'un ruban autocollant,
Cette opération étant faite, on superpose à cette première couche quatre gaines textiles unidirectionnelles 5, 6, 7, 8 constituées pour partie majoritaire de fils longitudinaux.Given the possibilities of deformation of such a textile structure, this sheath perfectly matches the surface of the mandrel. This sheath being put in place, the ends of it are fixed on the mandrel for example by means of an adhesive tape,
Once this operation has been carried out, four unidirectional textile sheaths 5, 6, 7, 8 are superimposed on this first layer, consisting mainly of longitudinal threads.
Ces gaines s'étendent depuis la base du mandrin de diamètre D sur des longueurs de plus en plus courtes lorsque l'on va de la couche interne 2 à la couche externe. Dans le cas présent, ces quatre gaines ont respectivement les longueurs suivantes
- gaine 5 : 9,50 m
- gaine 6 : 8,55 m
- gaine 7 : 6,50 m
- gaine 8 : 3,50 m
Ces gaines sont constituées, ainsi que cela est illustré à la figure 2, de fils parallèles 9 liés entre eux par des fils de liage tressés lâches 10. Dans le cas présent, les fils 9 ont un titre global de 187 000 Tex et les fils de liage 10, également en verre, ont un titre global de 13 000 Tex.These sheaths extend from the base of the mandrel of diameter D over increasingly shorter lengths when one goes from the inner layer 2 to the outer layer. In the present case, these four sheaths respectively have the following lengths
- duct 5: 9.50 m
- duct 6: 8.55 m
- duct 7: 6.50 m
- duct 8: 3.50 m
These sheaths are made up, as illustrated in FIG. 2, of parallel threads 9 linked together by loose braided binding threads 10. In the present case, the threads 9 have an overall titer of 187,000 Tex and the threads binding 10, also in glass, have an overall titer of 13,000 Tex.
Dans le cas présent, les gaines 5 et 6 ont, avant mise en place, un diamètre de 105 mm et comportent 156 fils longitudinaux 9. Les gaines 7 et 8 ont un diamètre interne de 110 mm et sont constituées chacune de 156 fils longitudinaux 9. In the present case, the sheaths 5 and 6 have, before installation, a diameter of 105 mm and have 156 longitudinal wires 9. The sheaths 7 and 8 have an internal diameter of 110 mm and are each made up of 156 longitudinal wires 9 .
Pour certaines applications, il pourrait être envisagé ainsi que cela est illustré à la figure 3, d'utiliser des gaines intermédiaires dans lesquelles les fils longitudinaux 9 auraient deux longueurs différentes. Cette solution peut être envisagée lorsque la conicité de la structure tubulaire que l'on envisage de réaliser est importante, ce qui permettrait d'obtenir une meilleure progressivité et une répartition plus homogène des filaments. For certain applications, it could be envisaged, as illustrated in FIG. 3, to use intermediate sheaths in which the longitudinal wires 9 would have two different lengths. This solution can be envisaged when the taper of the tubular structure which it is envisaged to produce is large, which would make it possible to obtain better progressiveness and a more homogeneous distribution of the filaments.
Dans le présent exemple, seules des gaines intermédiaires du type illustré par la figure 2 sont utilisées. In the present example, only intermediate sheaths of the type illustrated in FIG. 2 are used.
Après mise en place de chacune de ces gaines, on recouvre l'ensemble au moyen de deux gaines tressées bidirectionnelles 10-11 s'étendant sur toute la longueur de la structure. After each of these sheaths has been put in place, the assembly is covered by means of two bidirectional braided sheaths 10-11 extending over the entire length of the structure.
(Figure 1). Une partie seulement de la longueur des gaines a été représentée pour permettre de figurer les gaines textiles complémentaires internes. Ces gaines tressées 10-11 ont la même constitution que la gaine interne 2 et, compte-tenu de leurs possibilités de déformation, viennent s'appliquer par faitement autour des couches précédemment mises en place et emprisonnent les gaines intermédiaires 5, 6, 7 et 8.(Figure 1). Only part of the length of the sheaths has been shown to allow the internal complementary textile sheaths to be shown. These braided sheaths 10-11 have the same constitution as the internal sheath 2 and, taking into account their deformation possibilities, come to be applied by fact around the layers previously put in place and trap the intermediate sheaths 5, 6, 7 and 8.
Sur cette structure textile complexe ainsi réalisée, on dépose ensuite, d'une manière conventionnelle, une résine polymérisable à chaud ou à froid (du type polyester, vinylester ou epoxy). Après polymérisation, le mandrin est alors enlevé. On this complex textile structure thus produced, a hot or cold polymerizable resin (of the polyester, vinylester or epoxy type) is then deposited in a conventional manner. After polymerization, the mandrel is then removed.
Ces opérations étant classiques ne seront pas décrites en détail par mesure de simplification. These operations being conventional will not be described in detail for the sake of simplification.
Une telle structure tabulaire peut être utilisée comme mât de voiliers de plaisance et l'on a constaté qu'elle présentait, par rapport aux mâts antérieurs, l'avantage de possèder une flexibilité ajustable depuis la base dudit mât jusqu'à son sommet. Ainsi, par exemple, on peut réaliser un mât dont la partie inférieure présente, sur une longueur relativement importante, par exemple sur les 1/3 de la hauteur totale du mât, une bonne rigidité alors que la partie restante présente une flexibilité variable jusqu'au sommet. Such a tabular structure can be used as a mast for pleasure yachts and it has been found that it has, compared to previous masts, the advantage of having adjustable flexibility from the base of said mast to its top. Thus, for example, we can make a mast whose lower part has, over a relatively large length, for example on 1/3 of the total height of the mast, good rigidity while the remaining part has a variable flexibility up to at the top.
Par#ai11eurs, la surface périphérique de cette struc ture étant parfaitement lisse, ce mât peut être utilisé en association avec une voile à deux plis maintenue en place par un wishbone. By # ai11eurs, the peripheral surface of this structure being perfectly smooth, this mast can be used in combination with a two-ply sail held in place by a wishbone.
Bien entendu, l'invention n'est pas limitée au mode de réalisation cité-précédemment, mais elle en couvre toutes les variantes réalisées dans le même esprit. Ainsi, en fonction des performances recherchées, il pourrait être envisagé de réaliser une structure comportant un nombre plus ou moins important de couches intermédiaires constituées pour partie majoritaire de fils longitudinaux. De même, si dans l'exemple donné, deux couches externes 10-11 sont prévues, il pourrait être envisagé de n'en avoir qu'une seule. Of course, the invention is not limited to the embodiment cited above, but it covers all the variants produced in the same spirit. Thus, depending on the desired performance, it could be envisaged to produce a structure comprising a more or less large number of intermediate layers made up mainly of longitudinal wires. Similarly, if in the example given, two external layers 10-11 are provided, it could be envisaged to have only one.
Par rapport aux mâts antérieurs, une telle structure tubulaire présente comme avantage de pouvoir être réalisée très facilement et d'une manière économique, sur des longueurs importantes, et surtout de présenter une flexibilité variable sur sa longueur. De plus, cette flexibilité peut facilement être adaptée en modifiant le nombre de couches intermédiaires et/ou la longueur de ces différentes couches les unes tant aux autres. Compared to previous masts, such a tubular structure has the advantage of being able to be produced very easily and economically, over significant lengths, and above all to have variable flexibility over its length. In addition, this flexibility can easily be adapted by modifying the number of intermediate layers and / or the length of these different layers together.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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FR8105261A FR2501579A1 (en) | 1981-03-13 | 1981-03-13 | Composite fibre reinforced profiles for sail-board masts - with longitudinal reinforcement of differing lengths for progress stiffness variation overall |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR8105261A FR2501579A1 (en) | 1981-03-13 | 1981-03-13 | Composite fibre reinforced profiles for sail-board masts - with longitudinal reinforcement of differing lengths for progress stiffness variation overall |
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FR2501579A1 true FR2501579A1 (en) | 1982-09-17 |
FR2501579B1 FR2501579B1 (en) | 1984-02-24 |
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FR8105261A Granted FR2501579A1 (en) | 1981-03-13 | 1981-03-13 | Composite fibre reinforced profiles for sail-board masts - with longitudinal reinforcement of differing lengths for progress stiffness variation overall |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2537171A1 (en) * | 1982-12-02 | 1984-06-08 | Verre Tisse Sa | Plaited textile material for the production of tubular laminated articles |
EP0113196A1 (en) * | 1982-12-01 | 1984-07-11 | Cambridge Consultants Limited | Woven tubular structure |
FR2546473A1 (en) * | 1983-05-24 | 1984-11-30 | Verre Tisse Sa | TUBULAR MATERIAL BASED ON A RESIN REINFORCED BY A TEXTILE MATERIAL AND BICYCLE FRAME OR SIMILAR VEHICLE MADE FROM SUCH A MATERIAL |
EP0301995A2 (en) * | 1987-07-30 | 1989-02-01 | United Technologies Corporation | Composite helicopter rotor hub |
EP0487549A1 (en) * | 1989-06-15 | 1992-06-03 | Fiberspar Inc | Composite structural member with high bending strength and method of manufacture. |
EP0662391A2 (en) * | 1994-01-07 | 1995-07-12 | Composite Development Corporation | Composite shaft structure and manufacture |
USRE35081E (en) * | 1989-06-15 | 1995-11-07 | Fiberspar, Inc. | Composite structural member with high bending strength |
US5556677A (en) * | 1994-01-07 | 1996-09-17 | Composite Development Corporation | Composite shaft structure and manufacture |
US5580626A (en) * | 1992-07-14 | 1996-12-03 | Composite Development Corporation | High strength, high stiffness, curved composite member |
EP0844072A1 (en) * | 1996-05-16 | 1998-05-27 | Toray Industries, Inc. | Large-sized columnar body of fiber-reinforced plastic |
US5888601A (en) * | 1994-01-07 | 1999-03-30 | Composite Development Corporation | Composite tubular member having consistent strength |
US6148865A (en) * | 1996-12-02 | 2000-11-21 | A & P Technology, Inc. | Braided sleeve, tubular article and method of manufacturing the tubular article |
US6250193B1 (en) | 1996-12-02 | 2001-06-26 | A & P Technology, Inc. | Braided structure with elastic bias strands |
EP1588935A1 (en) * | 2004-04-23 | 2005-10-26 | TRIANA s.r.l. | Improved mast, in particular for sailboards |
ES2259567A1 (en) * | 2005-06-23 | 2006-11-01 | Fuore Design S.L. | Candle boat, has pillars embedded in cover in individual embedding points, where individual embedding points are located in proximity of flanks of helmet, and space defined between bridge and cover |
EP2678263B1 (en) | 2011-02-23 | 2015-04-08 | Cifa S.P.A. | Method to make arms in a composite material for the distribution of concrete and arm thus obtained |
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FR1116181A (en) * | 1954-11-15 | 1956-05-04 | Comp Generale Electricite | Conical or frustoconical objects of great length and of low taper, such as ship masts, antenna masts, electricity poles, etc. |
GB928348A (en) * | 1960-12-01 | 1963-06-12 | A C Ford Ltd | Improvements relating to columns for supporting lamps for street lighting purposes |
US4172175A (en) * | 1978-02-17 | 1979-10-23 | Tillotson-Pearson, Inc. | Pole construction |
FR2455980A1 (en) * | 1979-05-11 | 1980-12-05 | Tech Verre Tisse | Laminated surfboard mast mfr. - from superposed plaited hoses alternate ones having unidirectional reinforcements |
FR2462266A1 (en) * | 1979-07-26 | 1981-02-13 | Tech Verre Tisse | Laminated racquet shaft reinforced with parallel and crossed filaments - laid up in separate layers to maintain alignment |
-
1981
- 1981-03-13 FR FR8105261A patent/FR2501579A1/en active Granted
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FR1116181A (en) * | 1954-11-15 | 1956-05-04 | Comp Generale Electricite | Conical or frustoconical objects of great length and of low taper, such as ship masts, antenna masts, electricity poles, etc. |
GB928348A (en) * | 1960-12-01 | 1963-06-12 | A C Ford Ltd | Improvements relating to columns for supporting lamps for street lighting purposes |
US4172175A (en) * | 1978-02-17 | 1979-10-23 | Tillotson-Pearson, Inc. | Pole construction |
FR2455980A1 (en) * | 1979-05-11 | 1980-12-05 | Tech Verre Tisse | Laminated surfboard mast mfr. - from superposed plaited hoses alternate ones having unidirectional reinforcements |
FR2462266A1 (en) * | 1979-07-26 | 1981-02-13 | Tech Verre Tisse | Laminated racquet shaft reinforced with parallel and crossed filaments - laid up in separate layers to maintain alignment |
Cited By (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0113196A1 (en) * | 1982-12-01 | 1984-07-11 | Cambridge Consultants Limited | Woven tubular structure |
FR2537171A1 (en) * | 1982-12-02 | 1984-06-08 | Verre Tisse Sa | Plaited textile material for the production of tubular laminated articles |
FR2546473A1 (en) * | 1983-05-24 | 1984-11-30 | Verre Tisse Sa | TUBULAR MATERIAL BASED ON A RESIN REINFORCED BY A TEXTILE MATERIAL AND BICYCLE FRAME OR SIMILAR VEHICLE MADE FROM SUCH A MATERIAL |
EP0127553A2 (en) * | 1983-05-24 | 1984-12-05 | T.V.T. Composites | Tubular material based on a resin reinforced with textile material and a frame for a bicycle or similar vehicle made from this material |
EP0127553A3 (en) * | 1983-05-24 | 1985-10-23 | Technique Du Verre Tisse S.A. | Tubular material based on a resin reinforced with textile material and a frame for a bicycle or similar vehicle made from this material |
US4657795A (en) * | 1983-05-24 | 1987-04-14 | Technique Du Verre Tisse S.A. | Tubular material based on a fabric-reinforced resin, and a bicycle or similar vehicle frame constructed with such a material |
EP0301995A2 (en) * | 1987-07-30 | 1989-02-01 | United Technologies Corporation | Composite helicopter rotor hub |
EP0301995A3 (en) * | 1987-07-30 | 1990-02-28 | United Technologies Corporation | Composite helicopter rotor hub |
EP0733469A3 (en) * | 1989-06-14 | 1996-11-06 | Fiberspar, Inc. | Composite structural member with high bending strength and method of manufacture |
EP0733469A2 (en) * | 1989-06-14 | 1996-09-25 | Fiberspar, Inc. | Composite structural member with high bending strength and method of manufacture |
EP0487549A1 (en) * | 1989-06-15 | 1992-06-03 | Fiberspar Inc | Composite structural member with high bending strength and method of manufacture. |
EP0487549A4 (en) * | 1989-06-15 | 1993-04-07 | Fiberspar, Inc. | Composite structural member with high bending strength and method of manufacture |
USRE35081E (en) * | 1989-06-15 | 1995-11-07 | Fiberspar, Inc. | Composite structural member with high bending strength |
US5580626A (en) * | 1992-07-14 | 1996-12-03 | Composite Development Corporation | High strength, high stiffness, curved composite member |
US5556677A (en) * | 1994-01-07 | 1996-09-17 | Composite Development Corporation | Composite shaft structure and manufacture |
US6129962A (en) * | 1994-01-07 | 2000-10-10 | Exel Oyj | Sports implement and shaft having consistent strength |
EP0662391A3 (en) * | 1994-01-07 | 1995-11-15 | Composite Dev Corp | Composite shaft structure and manufacture. |
EP0662391A2 (en) * | 1994-01-07 | 1995-07-12 | Composite Development Corporation | Composite shaft structure and manufacture |
US5688571A (en) * | 1994-01-07 | 1997-11-18 | Composite Development Corporation | Composite tubular member with internal reinforcement and method |
US5549947A (en) * | 1994-01-07 | 1996-08-27 | Composite Development Corporation | Composite shaft structure and manufacture |
US5888601A (en) * | 1994-01-07 | 1999-03-30 | Composite Development Corporation | Composite tubular member having consistent strength |
EP0844072A1 (en) * | 1996-05-16 | 1998-05-27 | Toray Industries, Inc. | Large-sized columnar body of fiber-reinforced plastic |
EP0844072A4 (en) * | 1996-05-16 | 2001-04-04 | Toray Industries | Large-sized columnar body of fiber-reinforced plastic |
US6148865A (en) * | 1996-12-02 | 2000-11-21 | A & P Technology, Inc. | Braided sleeve, tubular article and method of manufacturing the tubular article |
US6250193B1 (en) | 1996-12-02 | 2001-06-26 | A & P Technology, Inc. | Braided structure with elastic bias strands |
EP1588935A1 (en) * | 2004-04-23 | 2005-10-26 | TRIANA s.r.l. | Improved mast, in particular for sailboards |
ES2259567A1 (en) * | 2005-06-23 | 2006-11-01 | Fuore Design S.L. | Candle boat, has pillars embedded in cover in individual embedding points, where individual embedding points are located in proximity of flanks of helmet, and space defined between bridge and cover |
EP2678263B1 (en) | 2011-02-23 | 2015-04-08 | Cifa S.P.A. | Method to make arms in a composite material for the distribution of concrete and arm thus obtained |
US10399282B2 (en) | 2011-02-23 | 2019-09-03 | Cifa Spa | Method to make arms in a composite material for the distribution of concrete and arm thus obtained |
EP2678263B2 (en) † | 2011-02-23 | 2020-01-01 | Cifa S.P.A. | Method to make arms in a composite material for the distribution of concrete and arm thus obtained |
Also Published As
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