FR2516859A3 - Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board - Google Patents
Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board Download PDFInfo
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- FR2516859A3 FR2516859A3 FR8122879A FR8122879A FR2516859A3 FR 2516859 A3 FR2516859 A3 FR 2516859A3 FR 8122879 A FR8122879 A FR 8122879A FR 8122879 A FR8122879 A FR 8122879A FR 2516859 A3 FR2516859 A3 FR 2516859A3
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- Prior art keywords
- mast
- fabric
- mandrel
- point
- maximum stress
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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
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/347—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
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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
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/006—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor the force created by the liberation of the internal stresses being used for compression moulding or for pressing preformed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
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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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- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0809—Fabrics
-
- 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
-
- 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
- B29L2031/00—Other particular articles
- B29L2031/766—Poles, masts, posts
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
L'invention se rapporte à un procédé de fabrication d'un mât en matière plastique armée et au mât obtenu à l'aide de ce procédé. The invention relates to a method of manufacturing a mast made of reinforced plastic and to the mast obtained using this method.
Elle s'applique plus particulièrement mais non exclusivement à la fabrication de mâts classiques mais aussi de poutres et élements semblables qui, à une certaine distance de leurs extrémités, subissent une sollicitation en flexion comme c'est par exemple le cas pour les mâts de planche à voile, à hauteur du "wishbone". It applies more particularly but not exclusively to the manufacture of conventional masts but also of beams and similar elements which, at a certain distance from their ends, undergo a bending stress as is for example the case for board masts sailing, up to the "wishbone".
A ce jour, il est déjà connu de fabriquer un mât de planche à voile en matière plastique armée (brevets frangais A-2.455.980 et A-2.075.042). To date, it is already known to manufacture a windsurf mast made of reinforced plastic (French patents A-2,455,980 and A-2,075,042).
Dans ce procédé connu, il est fait appel à un mandrin au moins légèrement conique, et ce, selon une pente constante tout au long du mât ou progressivement augmentée vers le haut du mât mais quoiqu'il en soit toujours orientée dans le même sens afin de former une face en dépouille permettant lorsque le mât sera terminé le retrait de ce mandrin et son réemploi. In this known method, use is made of an at least slightly conical mandrel, and this, according to a constant slope all along the mast or gradually increased towards the top of the mast but although it is always oriented in the same direction so to form a draft face allowing when the mast is finished the withdrawal of this mandrel and its reuse.
Sur ce mandrin, est alors enroulé un tissu formé à partir des fibres choisies pour réaliser l'armature, telles les fibres de verre. On this mandrel, is then wound a fabric formed from the fibers chosen to make the frame, such as glass fibers.
Avant cet enroulement le tissu, aura été impregné d'un liant constitué de résine thermodurcissable et pourra avoir subi une pré-polymérisation lui donnant une raideur semblable à celle d'un carton. Before this winding, the fabric will have been impregnated with a binder made of thermosetting resin and may have undergone a pre-polymerization giving it a stiffness similar to that of a cardboard.
De même, pour tenir compte de la largeur du tissage, ce tissu aura pu être formé en plusieurs pièces enroulées successivement, et pour tenir compte de la conicité du mandrin et donc de la forme qu'aurait le dit mandrin après son développement, les pièces pourront avoir une configuration trapézoldales dont les grande et petite base formeront respectivement la base et la tête du mât. Similarly, to take into account the width of the weaving, this fabric could have been formed in several pieces wound successively, and to take into account the taper of the mandrel and therefore the shape that the said mandrel would have after its development, the pieces may have a trapezoidal configuration whose large and small base will respectively form the base and the head of the mast.
Après enroulement du tissu imprégné, avant la polymérisation complète de l'ensemble, autour du tissu imprégné est enroulé, avec serrage et en hélice se recouvrant partiellement, un ruban en matière plastique rétractable à chaud et non susceptible de faire corps avec le tissu imprégné après polymérisation. After winding the impregnated fabric, before the complete polymerization of the assembly, around the impregnated fabric is wound, with tightening and in a partially overlapping helix, a ribbon of plastic material which is heat shrinkable and not capable of becoming one with the impregnated fabric after polymerization.
A sa mise en place, cet enrobage assure la regularisation de la couche de liant
Ensuite, lors de la polymérisation, par sa rétractation, cet enrobage soumet toute la surface latérale du rouleau de tissu imprégné à un effort de pression améliorant la dûreté et uniformisant l'aspect du mât.When put in place, this coating ensures the regularization of the binder layer
Then, during the polymerization, by its retraction, this coating subjects the entire lateral surface of the roll of impregnated fabric to a pressure force improving the hardness and standardizing the appearance of the mast.
Après cette polymérisation et après que l'enrobage et le mandrin auront été retirés, le mât, constitué essentiellement de matière plastique armée, est terminé et peut alors être usiné et/ou recevoir les accessoires qu'il doit porter. After this polymerization and after the coating and the mandrel have been removed, the mast, consisting essentially of reinforced plastic, is finished and can then be machined and / or receive the accessories which it must carry.
Ainsi réalisé selon la technique connue, le mât se présente sous la forme d'un élément tubulaire qui, dans son ensemble, est légèrement conique avec sa grande base au pied du mât et qui a une paroi d'épaisseur constante au moins entre sa base et le point d'attache du "wishbone". Thus produced according to the known technique, the mast is in the form of a tubular element which, as a whole, is slightly conical with its large base at the foot of the mast and which has a wall of constant thickness at least between its base and the attachment point of the "wishbone".
Pour qu'à ce point d'attache du "wishbone" le mât soit à même de résister aux sollicitations de celui-ci il faut qu'en ce point il offre un moment d'inertie suffisant. So that at this point of attachment of the "wishbone" the mast is able to withstand the stresses of it it is necessary that at this point it offers a sufficient moment of inertia.
Comme, par définition, le moment d'inertie est sensiblement directement proportionnel d'une part à l'épaisseur de la paroi et d'autre part au cube de sa distance à l'axe, dans la technique connue qui conduit à une paroi d'épaisseur constante, à ce point d'attache du "wishbone", le mât doit avoir un diamètre suffisamment important. As, by definition, the moment of inertia is substantially directly proportional on the one hand to the thickness of the wall and on the other hand to the cube of its distance from the axis, in the known technique which leads to a wall d constant thickness, at this point of attachment of the "wishbone", the mast must have a sufficiently large diameter.
En observant le diagramme des sollicitations , au long du mât on remarque que le moment fléchissant qui est maximum au niveau du point d'attache, a une valeur qui décroit progressivement non seulement vers la tête du mât ou grâce à la conicité du mandrin servant à sa fabrication, le mât peut avoir un diamètre très faible mais aussi au pied du mât où malheureusement pour permettre le retrait du mandrin, le diamètre est encore supérieur à celui mesuré au point d'attache du "wishbone". By observing the stress diagram, along the mast we notice that the bending moment which is maximum at the point of attachment, has a value which decreases gradually not only towards the head of the mast or thanks to the taper of the mandrel used to its manufacture, the mast can have a very small diameter but also at the foot of the mast where unfortunately to allow the withdrawal of the mandrel, the diameter is still greater than that measured at the point of attachment of the "wishbone".
Outre qu'il conduit à un mât qui est lourd, ce diamètre confère au pied du mât, un moment d'inertie excessif et parfaitement inutile. In addition to leading to a mast which is heavy, this diameter gives the mast a moment of excessive inertia which is perfectly useless.
Aux problèmes identiques se posant dans le domaine des mâts en duralumin, une solution satisfaisante ayant été donnée par l'adoption d'un mât biconique, les constructeurs de mâts en matière plastique armée, ont alors tenté d'adopter la même solution et pour résoudre le problème du retrait du mandrin de fabrication, ils ont réalisé séparément les parties du mât situé d'un côté et de l'autre du point d'attache, lesquelles parties, seulement après démandrinnage, sont alors assemblées par un manchon s'insérant dans la grande base de chacune d'elles
Si ces deux parties forment bien un mât biconique et résolvent le problème du démandrinnage tout en permettant de donner au mât un diamètre plus important au point d'attache du "wishbone" qu'aussi bien à la tête qu'au pied du mât, malheureusement, il s'avère qu'est très compliqué et coûteux un manchonnage suffisamment résistant pour être effectué à l'endroit même où le moment fléchissant est maximum.To the identical problems arising in the field of duralumin masts, a satisfactory solution having been given by the adoption of a biconical mast, the manufacturers of masts in reinforced plastic material, then attempted to adopt the same solution and to resolve the problem of the withdrawal of the manufacturing mandrel, they produced separately the parts of the mast located on one side and the other of the attachment point, which parts, only after retraining, are then assembled by a sleeve fitting into the great basis of each of them
If these two parts do form a biconical mast and solve the problem of tilting while allowing to give the mast a larger diameter at the point of attachment of the "wishbone" as well as at the head than at the foot of the mast, unfortunately , it turns out that it is very complicated and expensive a sleeving sufficiently resistant to be carried out at the same place where the bending moment is maximum.
Un résultat que l'invention vise à obtenir est un procédé de fabrication d'un mât en matière plastique qui soit en une seule pièce, léger et qui tout en ayant une forme intérieure légèrement conique dans un sens constant pour permettre le retrait de son mandrin, offre au droit du point d'attache du "wishbone" un moment d'inertie nettement plus important non seulement qu'à la tête mais aussi qu'au pied du mât. A result which the invention aims to obtain is a method of manufacturing a plastic mast which is in one piece, light and which while having an interior shape slightly conical in a constant direction to allow the withdrawal of its mandrel , offers to the right of the attachment point of the "wishbone" a moment of inertia markedly greater not only than at the head but also at the foot of the mast.
A cet effet, l'invention a pour objet un procédé de fabrication d'un mât en matière plastique armée du type cité plus haut, notamment caractérisé en ce qu'au droit du point de sollicitation maximale du mât, on enroule une largeur totale de tissu, qui est plus importante que celle du tissu qui indépendamment des renforts éventuels est enroulé au pied et à la tête du mât, et en ce qu'entre chacune de ces extrémités du mât et le point de sollicitation maximale, cette largeur varie progressivement. To this end, the subject of the invention is a method of manufacturing a mast made of reinforced plastic of the type mentioned above, in particular characterized in that, at the point of the point of maximum stress on the mast, a total width of fabric, which is more important than that of the fabric which, independently of any reinforcements, is wound at the foot and at the head of the mast, and in that between each of these ends of the mast and the point of maximum stress, this width varies gradually.
Elle a également pour objet le mât obtenu à l'aide de ce procédé. It also relates to the mast obtained using this process.
L'invention sera bien comprise à l'aide de la description ci-après faite à titre d'exemple non limitatif, en regard du dessin qui représente, schématiquement, et sans que les proportions entre longueur et diamètre et pente soient respectées
- figure 1 : vue en cours de sa fabrication , une
perspective du mât,
- figure 2 : une demi-coupe d'un mât terminé,
- figure 3 : vu de profil le mandrin,
- figure 4 : vues en plan, les pièces de tissu impré
gné qui seront enroulées sur le mandrin,
- figure 5 : le diagramme des moments fléchissant au
long du mât.The invention will be better understood with the aid of the description below given by way of nonlimiting example, with regard to the drawing which represents, schematically, and without the proportions between length and diameter and slope being respected
- Figure 1: view during its manufacture, a
mast perspective,
- Figure 2: a half-section of a completed mast,
- Figure 3: seen in profile the mandrel,
- Figure 4: plan views, the pieces of impregnated fabric
which will be wound on the mandrel,
- Figure 5: the diagram of the bending moments at
along the mast.
En se reportant au dessin (figure 3), on voit que le mandrin 1 est un corps présentant une conicité de sens constant mais de pente pouvant être croissante, par exemple la partie 2 s'étendant sur environ les trois quarts de sa longueur à partir de sa base 3 aura une conicité de cinq pour dix mille, le dixième de longueur suivant sera scindé en quatre parties 4, 5, 6, 7 qui auront respectivement des conicités de cinquante six pour dix mille, cent sept pour dix mille, cent cinquante neuf pour dix mille et deux cent dix pour dix mille. Enfin, le reste 8 formant environ les quinze pour cent de sa longueur et s'étendant donc jusqu'à la tête 9 du mandrin aura une conicité de deux cent quatre vingt dix pour dix mille. Referring to the drawing (FIG. 3), it can be seen that the mandrel 1 is a body having a conicity of constant direction but of slope which can be increasing, for example the part 2 extending over approximately three quarters of its length from from its base 3 will have a taper of five per ten thousand, the next tenth of length will be split into four parts 4, 5, 6, 7 which will have conicities of fifty six for ten thousand, one hundred and seven for ten thousand, one hundred and fifty respectively nine for ten thousand and two hundred and ten for ten thousand. Finally, the remainder 8 forming approximately fifteen percent of its length and therefore extending to the head 9 of the mandrel will have a taper of two hundred ninety per ten thousand.
Autour de ce mandrin 1 est enroulé un tissu 10 formé de plus de chaîne 11 que de trame 12 et par exemple de quatre vingt cinq à quatre vingt dix pour cent de chaîne 11 et de dix pour cent à quinze pour cent de trame 12 de fibres ou faisceaux de fibres du matériau choisi tel la fibre de verre, lequel tissu a au préalable été imprégné de résine thermodurcissable. Around this mandrel 1 is wound a fabric 10 formed of more warp 11 than weft 12 and for example from eighty five to ninety percent warp 11 and from ten percent to fifteen percent weft 12 of fibers or bundles of fibers of the chosen material such as fiberglass, which fabric has previously been impregnated with thermosetting resin.
Compte tenu de la largeur dans laquelle il peut être fabriqué, le tissu imprégné 10 est généralement formé de plusieurs pièces principales 14, 15 enroulées suc cesivement. Given the width in which it can be manufactured, the impregnated fabric 10 is generally formed from several main parts 14, 15 wound successively.
Cet enroulement s'opère en plaçant la chaîne 11 parallèlement à l'axe longitudinal 13 du mandrin 1. This winding takes place by placing the chain 11 parallel to the longitudinal axis 13 of the mandrel 1.
Evidemment, indépendamment de ces pièces principales, peuvent être prévues localement des petites pièces de renfort 16, 17 qui, quant à elles peuvent être orientées avec leur chaîne perpendiculaire à l'axe du mandrin. Obviously, independently of these main parts, small reinforcing parts 16, 17 can be provided locally which, for their part, can be oriented with their chain perpendicular to the axis of the mandrel.
En se reportant figure 5, on voit que le diagramme 18 des moments fléchissants a sensiblement la forme d'un triangle dont la base correspond à l'axe 13 du mât et dont le sommet 19 est situé sur la droite 20 qui, perpendiculairement à cet axe, passe par le point 21 d'attache du "wishbone". Referring to Figure 5, we see that the diagram 18 of the bending moments has substantially the shape of a triangle whose base corresponds to the axis 13 of the mast and whose top 19 is located on the line 20 which, perpendicular to this axis, goes through the attachment point 21 of the "wishbone".
Selon une caractéristique essentielle de l'invention, la largeur totale L1 de tissu enroulé dans la zone d'attache du "wishbone" est beaucoup plus importante que celle L2, L3 du tissu qui, indépendamment des éventuels renforts, est enroulé tant au pied qu'à la tête du mât et entre chacune desquelles extrémités et la zone d'attache, cette longueur varie progressivement. According to an essential characteristic of the invention, the total width L1 of fabric wound in the attachment area of the "wishbone" is much greater than that L2, L3 of the fabric which, independently of any reinforcements, is wound both at the foot and 'at the head of the mast and between each of which ends and the attachment zone, this length varies gradually.
A cet effet, dans un mode préféré de l'invention, au moins une partie du tissu imprégné 10, et par exemple la pièce 15, est découpée selon une forme sensiblement triangulaire dont la base 22 est parallèle à la chaîne 11 et dont, après enroulement, le sommet 23 se situera à hauteur du point 21 d'attache du "wishbone" de manière telle qu'en ce point l'enroulement du tissu ait une épaisseur (el) plus importante que l'épaisseur (e2) mesurée au pied 24 du mât et que celle (e3) mesurée à la tête 25 du dit mât 26. To this end, in a preferred embodiment of the invention, at least part of the impregnated fabric 10, and for example the part 15, is cut into a substantially triangular shape, the base 22 of which is parallel to the chain 11 and of which, after winding, the top 23 will be located at the point 21 of attachment of the "wishbone" so that at this point the fabric winding has a thickness (el) greater than the thickness (e2) measured at the foot 24 of the mast and that that (e3) measured at the head 25 of said mast 26.
Cette différence d'épaisseur sera d'autant plus sensible que la hauteur du triangle sera grande et que son enroulement se fera donc sur plusieurs, par exemple, quatre tours. This difference in thickness will be all the more significant as the height of the triangle will be large and that its winding will therefore be done over several, for example, four turns.
Cette différence peut aller jusqu'à donner au mât, dans la zone d'attache, un diamètre supérieur à celui qu'il présente au pied, lequel mât acquerra ainsi une forme externe sensiblement biconique. This difference can go so far as to give the mast, in the attachment zone, a diameter greater than that which it presents at the foot, which mast will thus acquire a substantially biconical external shape.
Pour tenir compte de la variation possible de hauteur du point d'attache, le sommet du triangle peut être tronqué, le mât présentera alors dans la zone du point d'attache, une partie cylindrique séparant les deux zones de conicité inverse. To take into account the possible variation in height of the attachment point, the top of the triangle can be truncated, the mast will then present in the area of the attachment point, a cylindrical part separating the two zones of reverse taper.
Après cette phase caractéristique de découpe et d'enroulement du tissu imprégné, le procédé de fabrication se poursuit selon la technique traditionnelle par enrobage sous film rétractable à chaud puis par polymérisation et enfin par pelage du film rétractable et retrait du mandrin. After this characteristic phase of cutting and winding of the impregnated fabric, the manufacturing process continues according to the traditional technique by coating with hot shrink film then by polymerization and finally by peeling of the shrink film and removal of the mandrel.
Le mât 26 ainsi obtenu qui a extérieurement une forme sensiblement biconique, offre, à hauteur du point 21 d'attache du "wishbone", un moment d'inertie nettement plus important qu'à sa tête 25 et qu'à son pied 24, tout en ayant été formé en une seule pièce sur un mandrin dont la conicité à un sens constant et dont le retrait reste de ce fait possible. The mast 26 thus obtained which has an outwardly substantially biconical shape, offers, at the point of attachment 21 of the "wishbone", a moment of inertia markedly greater than at its head 25 and at its foot 24, while having been formed in one piece on a mandrel whose conicity in a constant direction and whose withdrawal remains therefore possible.
Il a également l'avantage d'être plus résistant tout en étant plus léger et au moins aussi rigide que les mâts connus à ce jour. It also has the advantage of being more resistant while being lighter and at least as rigid as the masts known to date.
Dans une variante de réalisation, la variation de la largeur de tissu enroulé est obtenu en enroulant successivement, en les superposant, des pièces pouvant être par exemple rectangulaires, trapezoldales ou autres, mais de dimensions de plus en plus faibles dans le sens longitudinal, chacune d'elles étant plus ou moins centrées par rapport à la précédente et par rapport à la zone d'attache du "wishbone", afin que l'épaisseur (el) de matière y soit supérieure à celle (e2) et (e3) au pied et en tête de mât et afin qu'entre la zone d'attache du "wishbone" et, tant le pied que la tête du mât, la dite épaisseur varie assez progressivement. In an alternative embodiment, the variation in the width of wound fabric is obtained by successively winding, by superimposing them, pieces which may be, for example rectangular, trapezoidal or other, but of increasingly smaller dimensions in the longitudinal direction, each of them being more or less centered with respect to the previous one and with respect to the attachment zone of the "wishbone", so that the thickness (el) of material there is greater than that (e2) and (e3) at foot and at the top of the mast and so that between the attachment zone of the "wishbone" and, both the foot and the head of the mast, the said thickness varies fairly gradually.
Claims (9)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8122879A FR2516859A3 (en) | 1981-11-26 | 1981-11-26 | Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8122879A FR2516859A3 (en) | 1981-11-26 | 1981-11-26 | Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2516859A3 true FR2516859A3 (en) | 1983-05-27 |
| FR2516859B3 FR2516859B3 (en) | 1983-10-21 |
Family
ID=9264757
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8122879A Granted FR2516859A3 (en) | 1981-11-26 | 1981-11-26 | Double-tapered fibre reinforced plastics mast - thickest at point of greatest stress, used for wind surf board |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2516859A3 (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| US5549947A (en) * | 1994-01-07 | 1996-08-27 | Composite Development Corporation | Composite shaft structure and manufacture |
| 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 |
| US5888601A (en) * | 1994-01-07 | 1999-03-30 | Composite Development Corporation | Composite tubular member having consistent strength |
| EP0947308A3 (en) * | 1998-03-28 | 2000-07-26 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for producing energy absorbing structural members |
| FR2802141A1 (en) * | 1999-12-14 | 2001-06-15 | Laurent Barlesi | METHOD FOR MANUFACTURING A HOLLOW COMPOSITE STRUCTURE AND STRUCTURE OBTAINED ACCORDING TO SAID METHOD |
| CN117103653A (en) * | 2023-10-24 | 2023-11-24 | 北京玻钢院复合材料有限公司 | Mould for preparing variable-diameter large-cone-bottom composite mast and mast preparation method |
-
1981
- 1981-11-26 FR FR8122879A patent/FR2516859A3/en active Granted
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USRE35081E (en) * | 1989-06-15 | 1995-11-07 | Fiberspar, Inc. | Composite structural member with high bending strength |
| EP0487549A4 (en) * | 1989-06-15 | 1993-04-07 | Fiberspar, Inc. | Composite structural member with high bending strength and method of manufacture |
| US5580626A (en) * | 1992-07-14 | 1996-12-03 | Composite Development Corporation | High strength, high stiffness, curved composite member |
| US5888601A (en) * | 1994-01-07 | 1999-03-30 | Composite Development Corporation | Composite tubular member having consistent strength |
| US5556677A (en) * | 1994-01-07 | 1996-09-17 | 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 |
| US6129962A (en) * | 1994-01-07 | 2000-10-10 | Exel Oyj | Sports implement and shaft having consistent strength |
| EP0947308A3 (en) * | 1998-03-28 | 2000-07-26 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for producing energy absorbing structural members |
| US7238250B2 (en) | 1998-03-28 | 2007-07-03 | Duetsches Zentrum Fuer Luft-Und Raumfahrt E.V. | Energy absorbing systems and processes, and processes for the production of energy absorbing structural elements |
| FR2802141A1 (en) * | 1999-12-14 | 2001-06-15 | Laurent Barlesi | METHOD FOR MANUFACTURING A HOLLOW COMPOSITE STRUCTURE AND STRUCTURE OBTAINED ACCORDING TO SAID METHOD |
| WO2001043937A3 (en) * | 1999-12-14 | 2001-12-13 | Laurent Barlesi | Method for producing a hollow composite structure and structure obtained according to this method |
| CN117103653A (en) * | 2023-10-24 | 2023-11-24 | 北京玻钢院复合材料有限公司 | Mould for preparing variable-diameter large-cone-bottom composite mast and mast preparation method |
| CN117103653B (en) * | 2023-10-24 | 2024-03-08 | 北京玻钢院复合材料有限公司 | Mould for preparing variable-diameter large-cone-bottom composite mast and mast preparation method |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2516859B3 (en) | 1983-10-21 |
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