WO2014177948A1 - Assembly for collecting wind energy and for transforming same into usable energy - Google Patents

Assembly for collecting wind energy and for transforming same into usable energy Download PDF

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Publication number
WO2014177948A1
WO2014177948A1 PCT/IB2014/060168 IB2014060168W WO2014177948A1 WO 2014177948 A1 WO2014177948 A1 WO 2014177948A1 IB 2014060168 W IB2014060168 W IB 2014060168W WO 2014177948 A1 WO2014177948 A1 WO 2014177948A1
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WO
WIPO (PCT)
Prior art keywords
wing
assembly
wind energy
fixed
support
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Application number
PCT/IB2014/060168
Other languages
French (fr)
Inventor
Samuel GRANGES
Mathias BAVAUD
Hugues De Turckheim
Alain KULCZYKI-WOLCZKO
Original Assignee
Horeos Sàrl
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Publication date
Application filed by Horeos Sàrl filed Critical Horeos Sàrl
Publication of WO2014177948A1 publication Critical patent/WO2014177948A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D5/00Other wind motors
    • F03D5/06Other wind motors the wind-engaging parts swinging to-and-fro and not rotating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy

Definitions

  • the present invention relates to an assembly for capturing wind energy and for converting it into energy that can be used directly or that can be stored for later use, in particular in mechanical energy which can then be converted into electrical or hydraulic energy.
  • the present invention proposes to overcome all of the drawbacks mentioned above by providing an assembly for capturing wind energy and for converting it into usable energy, less cumbersome and less costly both at the time of installation and for maintenance and having a higher performance due to better use of the wind, especially medium or low force winds.
  • the assembly comprises at least one support disposed in a windy sector, on which is mounted at least one elongated wing having a fixed first end secured to said support and a second free end, this wing being animated with a movement oscillating about a fixed axis carried by said support, this fixed axis passing through said first fixed end of the wing, said oscillating movement s' alternating between a first position inclined relative to the vertical and a second position inclined relative to the vertical, angularly offset from said first position, and in that said wing is composed of a plurality of independent superimposed sections arranged between said first fixed end and said second free end.
  • each of said sections of said plurality of sections consists of an assembly of boxes juxtaposed along a central line, and said boxes are articulated with respect to each other in such a way that each of the axes longitudinals said juxtaposed boxes can rotate angularly relative to the longitudinal axes of each juxtaposed boxes.
  • each of said boxes is closed and has an intermediate partition separating it from an adjacent box.
  • Said intermediate partition may advantageously consist of two walls respectively belonging to a first box and a second box adjacent to the first.
  • said walls can belong respectively to a first box and a second box adjacent to the first and are articulated relative to each other.
  • said support is composed of a base comprising a rotating circular platform by means of rollers supported on a fixed plate.
  • the platform preferably carries a pulley comprising two vertical side walls, mounted parallel to each other and a base plate, said frame carrying an oscillating assembly on which is mounted said at least one wing.
  • Said frame can be arranged to house at least one hydraulic pump whose body is mounted on at least one rod and whose piston is coupled indirectly, respectively to at least one yoke integral with the lower surface of the crossbar.
  • FIG. 1A is a perspective view of a first embodiment of the assembly according to the invention , this assembly comprising a single wing mounted on a support
  • Figure 1 B shows an enlarged perspective view of the support base of the wing according to Figure 1A
  • Figure 2A shows a perspective view of a second embodiment. of the assembly according to the invention, this assembly comprising two wings mounted on the same support
  • Figure 2B shows a side elevational view of the two-wing variant as shown in Figure 2A in perspective
  • Figure 3A is a cross-sectional view of a wing corresponding to the embodiment of FIG.
  • Figure 3B is a perspective view of a wing corresponding to the embodiment of Figure 1A
  • Figure 3C is a cross-sectional view similar to Figure 1A, illustrating the mechanical control means and hydraulic positioning of the boxes
  • FIGS. 4A, 4B and 4C illustrate in schematic form the operation of a two-wing assembly operating a hydraulic pump, respectively at full power, medium power and low power.
  • the assembly 10 essentially comprises a support in the form of a fixed base 11 which carries at least one vertical or inclined wing 12 relative to said fixed base 11, this wing being composed a plurality of wing sections 12a, 12b, 12c and 12d superimposed.
  • the wing 12 comprises a driving profile 13 which is common to all the sections 12a, 12b, 12c and 12d.
  • the wing sections are angularly movable relative to each other about an axis located inside the driving profile 13, so that they can shift respectively on the height of the wing depending parameters related to the strength of the wind, the position of the set and the local weather conditions instantaneous.
  • the wing 12 comprises four superimposed sections. This.
  • each wing portion 12a, 12b, 12c and 12d consists of a profiled carcass 15 which is delimited downwards and upwards by a flange 14 substantially planar.
  • the carcass 15 could be made in one piece of a material that gives it rigidity adequate, but it can also be made of several components articulated with respect to each other.
  • the wing 12 is mounted on the base 11 which is shown in the form of an enlarged perspective view in FIG. 1B and in the form of a view which illustrates the structure in transparency, in FIG. 1C.
  • the base 11 comprises a circular platform 16a rotating by means of rollers 16b with respect to a fixed plate 16c.
  • the platform 16a carries a frame 17 comprising two vertical side walls 17a and 17b, mounted parallel to each other and a base plate 17c.
  • This frame 17 carries two side arms 18a and 18b connected by a cross member 18c connecting the two side arms 18a and 18b.
  • the assembly 19 consists of the two lateral arms 18a and 18b and the cross member 18c is rigid and is mounted oscillating on the vertical side walls 17a and 17b about a substantially horizontal axis, materialized by segments of axis 20a and 20b crossing respectively the vertical side wall 17a and the side arm 18a, on the one hand and the vertical side wall 17b and the side arm 18b, on the other hand.
  • the cross member 18c which is in this case pivoting, serves as support for the wing 12.
  • the interior of the frame 17 houses two hydraulic pumps 21a and 21b, whose bodies are mounted on two through rods 22a and 22b and whose pistons are coupled indirectly to two stirrups 23a and 23b respectively. secured to the lower surface of the cross member 18c.
  • the hydraulic fluid pumped by these hydraulic cylinders circulates in a suitable hydraulic circuit for feeding a hydraulic motor for example.
  • FIGS. 2A and 2B represent, by way of example, a second embodiment of the assembly 10 according to the invention, which in this case comprises two wings 12 mounted side by side on the same support.
  • the support consists, as before, of a base 17 of similar construction to that of FIG. 18, but having larger dimensions so as to accommodate both of them. wings 12.
  • the soc! e 17 is mounted on the platform 16 pivoting, to allow to orient the wings optimally. It is obvious that the invention is not limited to these two embodiments and that it extends to variants with a higher number of wings mounted on the same support, which will of course be dimensioned accordingly, or on juxtaposed supports each carrying one or more similar wings.
  • FIG. 2B shows the two wings 12 in the maximum spacing position and the sections 12a, 12b, 12c which make up these wings in different angular positions so as to offer maximum wind resistance.
  • the relative position of the boxes which constitute said sections is adjusted accordingly.
  • FIGS 3A, 3B and 3C show cross-sectional and perspective views of a wing 12 composed for example, as shown in Figure 1A, wing sections 12a, 12b, 12c and 12d superimposed.
  • Each section consists of several boxes 30a, 30b, 30c which are interconnected by a frame comprising intermediate partitions 31a and 31b. These intermediate partitions consist of two walls respectively belonging to a first box and a second box adjacent to the first. Therefore, each box is independent and closed and they can move relative to each other without the airflow flow surface is interrupted along the profile of the wing.
  • the carcass or body of the boxes 30a, 30b, 30c is made of a suitable material, which may be a molded synthetic material or a sheet of light metal or the like.
  • the boxes are constructed such that they are partially movable relative to each other, in particular articulated so that the respective longitudinal axes of the juxtaposed boxes can tilt relative to each other to vary the profile of each other.
  • the wing and in particular the curvature of each wing section approximately like an airplane wing. This characteristic makes it possible to adapt the profile of the wing, section after section, according to the wind force and its direction.
  • a fin 30d is pivotally mounted at the end of the last box 30c, at the end opposite the attack profile of the wing, which is located at the front, facing the wind of the first box 30a.
  • Figures 3A, 3B and 3C show that the intermediate partition 31a is formed of two walls 32a and 32b which are coupled by a hinge 33 allowing a relative displacement of the wall 32b, movable relative to the wall 32a which is fixed.
  • the intermediate partition 31b is formed of two walls 34a and 34b which are coupled by a hinge 35 which allows a relative displacement of the movable wall 34b with respect to the wall 32a which is fixed.
  • the relative displacement of the different boxes of each wing section is obtained by hydraulic cylinders 36 whose bodies are mounted on said fixed walls 32a and 34a respectively intermediate partitions 31a and 31b and whose pistons are fixed on the movable walls 32b and 34b.
  • the intermediate partition 31a is formed of two walls 32a and 32b which are coupled by a hinge 33 which allows a relative displacement of the movable wall 32b with respect to the wall 32a which is fixed. These means make it possible to move the boxes 30a, 30b and 30c respectively relative to one another by varying the relative angles of their longitudinal axis and consequently to modify the profile of the wing at each of the sections of this section. wing.
  • the first box 30a of each wing section gives the general orientation of the section, the second box 30b being fixed to the first box 30a and the third box 30c being attached to the second box 30b.
  • the rear wing 30d is fixed to the third box 30e.
  • the general orientation of the section is given by a central control mounted in the first box 30a and which comprises a ring gear 37 cooperating with a pinion 38 driven by a positioning motor 39 arranged to angularly position the first box 30a of each section of wing according to meteorological parameters.
  • the second box 30b and the third box 30c are positioned by the cylinders relative to the first box 30a.
  • the views of the three figures 4A, 4B and 4C show an installation 10 with two wings 12, mounted as described above.
  • the displacement of the wings causes the reciprocating movement of a piston 40 of a hydraulic pump 41, this piston being attached by its free end to a pivoting arm 42 actuated by the movement of the wings 12.
  • the mounting of the hydraulic pump is illustrated more in detail in Figure 1 B,
  • the assembly of the assembly according to the invention creates a hydraulic "gearbox" which has, on the one hand, the advantage of being able to offer a continuous adjustment over a very wide range of power and thus solve a specific problem of wind turbines that have a power directly dependent on the wind speed, and secondly to decoupling between the instantaneous angular speed of the wing and the linear speed of the cylinder.
  • the present invention is not limited to the embodiments described, but extends to all obvious variations for those skilled in the art, which arise directly from the elements described. These variants may concern both the wing or wings, their general shape, the derived forms, their number and their relative arrangement as the mechanical part responsible for converting the force of the wind pressure into hydraulic energy that can be used instantly or that can be stored. .

Abstract

The assembly comprises at least one support disposed in a windy location, on which there is mounted at least one elongate wing having a fixed first end rigidly connected to said support and a free second end, this wing being driven in an oscillating movement about a fixed shaft carried by said support, said fixed shaft passing through said fixed first end of the wing, said oscillating movement taking place, alternately, between a first position inclined relative to the vertical and a second position inclined relative to the vertical, angularly offset relative to said first position, and said wing consists of a plurality of separate stacked sections disposed between said fixed first end and said free second end.

Description

ENSEMBLE POUR CAPTER L'ENERGIE DU VENT ET POUR LA TRANSFORMER EN ENERGIE UTILISABLE  ASSEMBLY TO CAPTURE WIND ENERGY AND TRANSFORM IT TO USEFUL ENERGY
Domaine technique Technical area
La présente invention concerne un ensemble pour capter l'énergie du vent et pour la transformer en énergie utilisable directement ou pouvant être stockée en vue d'une utilisation ultérieure, notamment en énergie mécanique transformable ensuite en électrique ou en énergie hydraulique. The present invention relates to an assembly for capturing wind energy and for converting it into energy that can be used directly or that can be stored for later use, in particular in mechanical energy which can then be converted into electrical or hydraulic energy.
Technique antérieure Prior art
On connaît déjà des appareils appelés des éoliennes comportant habituellement une colonne de support portant par exemple à son sommet un ensemble de pales montées sur l'arbre d'un aérogénérateur destiné à transformer l'énergie du vent en puissance électrique. Ces appareils sont généralement très imposants, peu esthétiques et extrêmement coûteux à l'acquisition et à l'entretien. De ce fait leur efficacité est souvent contestée et les oppositions contre leur implantation dans des zones touristiques sont nombreuses. L'obligation de rechercher des sources d'énergie alternative a néanmoins permis à ces appareils de s'implanter dans des zones fortement balayées par les vents, notamment en bord de mer ou dans certains secteurs montagneux, même si ia solution apportée par les éoliennes à pales rotatives ne donné pas satisfaction de manière absolue.  Devices known as wind turbines are already known, usually comprising a support column carrying, for example at its top, a set of blades mounted on the shaft of an aerogenerator intended to transform the energy of the wind into electrical power. These devices are generally very impressive, unsightly and extremely expensive to purchase and maintain. As a result, their effectiveness is often disputed and there are many oppositions against their location in tourist areas. The obligation to search for alternative energy sources has nevertheless enabled these devices to set up in areas that are strongly windswept, particularly at the seaside or in certain mountainous areas, even if the solution provided by the wind turbines to Rotating blades do not give absolute satisfaction.
Exposé de l'invention Presentation of the invention
La présente invention se propose de pallier l'ensemble des inconvénients mentionnés ci-dessus en réalisant un ensemble pour capter l'énergie du vent et pour la transformer en énergie utilisable, moins encombrant et moins coûteux à ia fois à l'installation et pour la maintenance et ayant un rendement supérieur en raison d'une meilleur utilisation du vent, notamment des vents de force moyenne ou faible. Ce but est atteint par l'ensemble, selon l'invention tel que défini en préambule et caractérisée en ce qu'il comporte au moins un support disposé dans un secteur venté, sur lequel est montée au moins une aile allongée ayant une première extrémité fixe solidaire dudit support et une seconde extrémité libre, cette aile étant animée d'un mouvement oscillant autour d'un axe fixe porté par ledit support, cet axe fixe passant par ladite première extrémité fixe de l'aile, ledit mouvement d'oscillant s'effectuant alternativement entre une première position inclinée par rapport à la verticale et une deuxième position inclinée par rapport à la verticale, angulairement décalée par rapport à ladite première position, et en ce que ladite aile est composée d'une pluralité de tronçons superposés indépendants disposés entre ladite première extrémité fixe et ladite seconde extrémité libre. The present invention proposes to overcome all of the drawbacks mentioned above by providing an assembly for capturing wind energy and for converting it into usable energy, less cumbersome and less costly both at the time of installation and for maintenance and having a higher performance due to better use of the wind, especially medium or low force winds. This object is achieved by the assembly, according to the invention as defined in the preamble and characterized in that it comprises at least one support disposed in a windy sector, on which is mounted at least one elongated wing having a fixed first end secured to said support and a second free end, this wing being animated with a movement oscillating about a fixed axis carried by said support, this fixed axis passing through said first fixed end of the wing, said oscillating movement s' alternating between a first position inclined relative to the vertical and a second position inclined relative to the vertical, angularly offset from said first position, and in that said wing is composed of a plurality of independent superimposed sections arranged between said first fixed end and said second free end.
Selon une forme de réalisation préférée, chacun desdits tronçons de ladite pluralité de tronçons est constitué d'un assemblage de caissons juxtaposés le long d'une ligne centrale, et lesdits caissons sont articulés les uns par rapport aux autres de telle manière que chacun des axes longitudinaux desdits caissons juxtaposés puissent pivoter angulairement l'un par rapport aux axes longitudinaux de chacun des caissons juxtaposés. De façon avantageuse, chacun desdits caissons est fermé et comporte une cloison intermédiaire le séparant d'un caisson adjacent. According to a preferred embodiment, each of said sections of said plurality of sections consists of an assembly of boxes juxtaposed along a central line, and said boxes are articulated with respect to each other in such a way that each of the axes longitudinals said juxtaposed boxes can rotate angularly relative to the longitudinal axes of each juxtaposed boxes. Advantageously, each of said boxes is closed and has an intermediate partition separating it from an adjacent box.
Ladite cloison intermédiaire peut être avantageusement constituée de deux parois appartenant respectivement à un premier caisson et à un deuxième caisson adjacent au premier. Said intermediate partition may advantageously consist of two walls respectively belonging to a first box and a second box adjacent to the first.
Dans ce cas, lesdites parois peuvent appartenir respectivement à un premier caisson et à un deuxième caisson adjacent au premier et sont articulées l'une par rapport à l'autre. In this case, said walls can belong respectively to a first box and a second box adjacent to the first and are articulated relative to each other.
De manière préférentielle, ledit support est composé d'un socle comportant une plateforme circulaire rotative au moyen de galets appuyés sur un plateau fixe. La plateforme porte de préférence un pâti comprenant deux parois latérales verticales., montées parallèlement entre elles et une plaque de base, ledit bâti portant un assemblage oscillant sur lequel est montée ladite au moins une aile. Ledit bâti pet être agencé pour abriter au moins une pompe hydraulique dont le corps est monté sur au moins une tringle traversante et dont le piston est couplé indirectement, respectivement à au moins un étrier solidaire de la surface inférieure de la traverse. Description sommaire des dessins Preferably, said support is composed of a base comprising a rotating circular platform by means of rollers supported on a fixed plate. The platform preferably carries a pulley comprising two vertical side walls, mounted parallel to each other and a base plate, said frame carrying an oscillating assembly on which is mounted said at least one wing. Said frame can be arranged to house at least one hydraulic pump whose body is mounted on at least one rod and whose piston is coupled indirectly, respectively to at least one yoke integral with the lower surface of the crossbar. Brief description of the drawings
La présente invention et ses principaux avantages apparaîtront mieux dans la description de différents modes de réalisation, en référence aux dessins annexés, dans lesquels: la figure 1A représente une vue en perspective d'une première forme de réalisation de l'ensemble selon l'invention, cet ensemble comportant une seule aile montée sur un support, la figure 1 B représente une vue en perspective agrandie du socfe de support de l'aile selon la figure 1A, la figure 2A représente une vue en perspective d'une seconde forme de réalisation de l'ensemble selon l'invention, cet ensemble comportant deux ailes montées sur un même support, la figure 2B représente une vue de côté en élévation de la variante à deux ailes telle que la montre la figure 2A en perspective, la figure 3A est une vue en coupe transversale d'une aile correspondant à la réalisation de la figure 1 A, la figure 3B est une vue en perspective d'une aile correspondant à la réalisation de la figure 1A, la figure 3C est une vue en coupe transversale similaire à la figure 1A, illustrant les moyens de commande mécanique et hydraulique de positionnement des caissons, et les figures 4A, 4B et 4C illustrent sous forme schématique le fonctionnement d'un ensemble à deux ailes actionnant une pompe hydraulique, respectivement à pleine puissance, à moyenne puissance et à faible puissance. The present invention and its main advantages will become more apparent in the description of various embodiments, with reference to the accompanying drawings, in which: FIG. 1A is a perspective view of a first embodiment of the assembly according to the invention , this assembly comprising a single wing mounted on a support, Figure 1 B shows an enlarged perspective view of the support base of the wing according to Figure 1A, Figure 2A shows a perspective view of a second embodiment. of the assembly according to the invention, this assembly comprising two wings mounted on the same support, Figure 2B shows a side elevational view of the two-wing variant as shown in Figure 2A in perspective, Figure 3A is a cross-sectional view of a wing corresponding to the embodiment of FIG. 1A, Figure 3B is a perspective view of a wing corresponding to the embodiment of Figure 1A, Figure 3C is a cross-sectional view similar to Figure 1A, illustrating the mechanical control means and hydraulic positioning of the boxes, and FIGS. 4A, 4B and 4C illustrate in schematic form the operation of a two-wing assembly operating a hydraulic pump, respectively at full power, medium power and low power.
Meilleures manières de réaliser l'invention Best ways to achieve the invention
En référence aux figures et en particulier à la figure 1A, l'ensemble 10 comporte essentiellement un support sous la forme d'un socle fixe 11 qui porte au moins une aile 12 verticale ou inclinée par rapport audit socle fixe 11 , cette aile étant composée d'une pluralité de tronçons d'aile 12a, 12b, 12c et 12d superposés. L'aile 12 comporte un profil d'attaque 13 qui est commun à l'ensemble des tronçons 12a, 12b, 12c et 12d. Les tronçons d'aile sont angulairement mobiles les uns par rapport aux autres autour d'un axe localisé à l'intérieur du profil d'attaque 13, de telle manière qu'ils puissent se décaler respectivement sur la hauteur de l'aile en fonction de paramètres liés à la force du vent, à la position de l'ensemble et aux conditions météorologiques locales instantanées. Dans l'exemple de réalisation représenté, l'aile 12 comporte quatre tronçons superposés. Ce. nombre n'est pas limité et pourrait être augmenté en fonction de la puissance nominale de l'ensemble 10. Les tronçons sont séparés entre eux par des flasques 14 et la base ainsi que le sommet de l'aile 12 sont également équipés d'un flasque 14 de fermeture de l'aile à ses deux extrémités. En d'autre termes, chaque tronçon d'aile 12a, 12b, 12c et 12d est constitué d'une carcasse profilée 15 qui est délimitée vers le bas et vers le haut par un flasque 14 sensiblement plan. La carcasse 15 pourrait être réalisée d'une seule pièce en un matériau qui lui confère une rigidité adéquate, mais elle peut également être réalisée en plusieurs composants articulés les uns par rapport aux autres. With reference to the figures and in particular to FIG. 1A, the assembly 10 essentially comprises a support in the form of a fixed base 11 which carries at least one vertical or inclined wing 12 relative to said fixed base 11, this wing being composed a plurality of wing sections 12a, 12b, 12c and 12d superimposed. The wing 12 comprises a driving profile 13 which is common to all the sections 12a, 12b, 12c and 12d. The wing sections are angularly movable relative to each other about an axis located inside the driving profile 13, so that they can shift respectively on the height of the wing depending parameters related to the strength of the wind, the position of the set and the local weather conditions instantaneous. In the exemplary embodiment shown, the wing 12 comprises four superimposed sections. This. number is not limited and could be increased depending on the nominal power of the assembly 10. The sections are separated from each other by flanges 14 and the base and the top of the wing 12 are also equipped with a flange 14 closing the wing at both ends. In other words, each wing portion 12a, 12b, 12c and 12d consists of a profiled carcass 15 which is delimited downwards and upwards by a flange 14 substantially planar. The carcass 15 could be made in one piece of a material that gives it rigidity adequate, but it can also be made of several components articulated with respect to each other.
L'aile 12 est montée sur le socle 11 qui est représenté sous forme de vue en perspective agrandie par la figure 1B et sous forme d'une vue qui illustre la structure en transparence, par la figure 1C. Le socle 11 comporte une plateforme circulaire 16a rotative au moyen de galets 16b par rapport à un plateau fixe 16c. La plateforme 16a porte un bâti 17 comprenant deux parois latérales verticales 17a et 17b, montées parallèlement entre elles et une plaque de base 17c. Ce bâti 17 porte deux bras latéraux 18a et 18b reliés par une traverse 18c reliant les deux bras latéraux 18a et 18b. L'assembiage 19 constitué des deux bras latéraux 18a et 18b et la traverse 18c est rigide et il est monté oscillant sur les parois latérales verticales 17a et 17b autour d'un axe sensiblement horizontal, matérialisé par des segments d'axe 20a et 20b traversant respectivement la paroi latérale verticale 17a et le bras latéral 18a, d'une part et la paroi latérale verticale 17b et le bras latéral 18 b, d'autre part. La traverse 18c, qui est en l'occurrence pivotante, sert d'appui à l'aile 12. The wing 12 is mounted on the base 11 which is shown in the form of an enlarged perspective view in FIG. 1B and in the form of a view which illustrates the structure in transparency, in FIG. 1C. The base 11 comprises a circular platform 16a rotating by means of rollers 16b with respect to a fixed plate 16c. The platform 16a carries a frame 17 comprising two vertical side walls 17a and 17b, mounted parallel to each other and a base plate 17c. This frame 17 carries two side arms 18a and 18b connected by a cross member 18c connecting the two side arms 18a and 18b. The assembly 19 consists of the two lateral arms 18a and 18b and the cross member 18c is rigid and is mounted oscillating on the vertical side walls 17a and 17b about a substantially horizontal axis, materialized by segments of axis 20a and 20b crossing respectively the vertical side wall 17a and the side arm 18a, on the one hand and the vertical side wall 17b and the side arm 18b, on the other hand. The cross member 18c, which is in this case pivoting, serves as support for the wing 12.
Comme le montre la figure 1 B, l'intérieur du bâti 17 abrite deux pompes hydrauliques 21 a et 21b, dont les corps sont montés sur deux tringles traversantes 22a et 22b et dont les pistons sont couplés indirectement, respectivement à deux étriers 23a et 23b solidaires de la surface inférieure de la traverse 18c. Le fluide hydraulique pompé par ces vérins hydrauliques circule dans un circuit hydraulique approprié en vue d'alimenter un moteur hydraulique par exemple. As shown in Figure 1B, the interior of the frame 17 houses two hydraulic pumps 21a and 21b, whose bodies are mounted on two through rods 22a and 22b and whose pistons are coupled indirectly to two stirrups 23a and 23b respectively. secured to the lower surface of the cross member 18c. The hydraulic fluid pumped by these hydraulic cylinders circulates in a suitable hydraulic circuit for feeding a hydraulic motor for example.
Les figures 2A et 2B représentent à titre d'exemple, une deuxième forme de réalisation de l'ensemble 10 selon l'invention qui comporte dans ce cas deux ailes 12 montées côte à côte sur un même support. On notera que les axes des deux ailes forment entre eux un angle aigu prédéterminé, leur position par rapport au support commun étant définie par construction. Le support, est constitué, comme précédemment d'un socle 17 de construction similaire à celui de la figure 18, mais ayant des dimensions plus importantes de manière à pouvoir accueillir les deux ailes 12. Comme précédemment, le soc!e 17 est monté sur la plateforme 16 pivotante, pour permettre d'orienter les ailes de façon optimale. Il est évident que l'invention ne se limite pas à ces deux formes de réalisations et qu'elle s'étend à des variantes comportant un nombre plus élevé d'ailes montées soit sur un même support, qui sera bien entendu dimensionné en conséquence, soit sur des supports juxtaposés portant chacun une ou plusieurs ailes similaires. FIGS. 2A and 2B represent, by way of example, a second embodiment of the assembly 10 according to the invention, which in this case comprises two wings 12 mounted side by side on the same support. It will be noted that the axes of the two wings form between them a predetermined acute angle, their position relative to the common support being defined by construction. The support consists, as before, of a base 17 of similar construction to that of FIG. 18, but having larger dimensions so as to accommodate both of them. wings 12. As before, the soc! e 17 is mounted on the platform 16 pivoting, to allow to orient the wings optimally. It is obvious that the invention is not limited to these two embodiments and that it extends to variants with a higher number of wings mounted on the same support, which will of course be dimensioned accordingly, or on juxtaposed supports each carrying one or more similar wings.
La vue de côté en élévation de la figure 2B montre les deux ailes 12 en position d'écartement maximal et tes tronçons 12a, 12b, 12c qui composent ces ailes dans des positions angulaires différentes de manière à offrir le maximum de résistance au vent. La position relative des caissons qui constituent iesdits tronçons est ajustée en conséquence. The side elevational view of FIG. 2B shows the two wings 12 in the maximum spacing position and the sections 12a, 12b, 12c which make up these wings in different angular positions so as to offer maximum wind resistance. The relative position of the boxes which constitute said sections is adjusted accordingly.
Les figures 3A, 3B et 3C représentent des vues en coupe transversale et en perspective d'une aile 12 composée par exemple, comme le montre la figure 1A, de tronçons d'aile 12a, 12b, 12c et 12d superposés. Chaque tronçon est constitué de plusieurs caissons 30a, 30b, 30c qui sont reliés entre eux par une ossature comprenant des cloisons intermédiaires 31a et 31b. Ces cloisons intermédiaires sont constituées de deux parois appartenant respectivement à un premier caisson et à un deuxième caisson adjacent au premier. De ce fait, chaque caisson est indépendant et fermé et ils peuvent bouger les uns par rapport aux autres sans que la surface d'écoulement du flux d'air ne soit interrompu le long du profil de l'aile. La carcasse ou carrosserie des caissons 30a, 30b, 30c est réalisée en un matériau adéquat, qui peut être un matériau synthétique moulé ou une tôle en métal léger ou similaire. Les caissons sont construits de telle manière qu'ils soient partiellement mobiles les uns par rapport aux autres, en particulier articulés de telle manière que les axes longitudinaux respectifs des caissons juxtaposés puissent s'incliner les uns par rapport aux autres pour faire varier le profil de l'aile et notamment la courbure de chaque tronçon d'aile, approximativement comme une aile d'avion. Cette caractéristique permet d'adapter le profil de l'aile, tronçon après tronçon, en fonction de la force du vent et de sa direction. Un aileron 30d est monté pivotant à l'extrémité du dernier caisson 30c, â l'extrémité opposée au profil d'attaque de l'aile, qui est situé à l'avant, face au vent du premier caisson 30a. Figures 3A, 3B and 3C show cross-sectional and perspective views of a wing 12 composed for example, as shown in Figure 1A, wing sections 12a, 12b, 12c and 12d superimposed. Each section consists of several boxes 30a, 30b, 30c which are interconnected by a frame comprising intermediate partitions 31a and 31b. These intermediate partitions consist of two walls respectively belonging to a first box and a second box adjacent to the first. Therefore, each box is independent and closed and they can move relative to each other without the airflow flow surface is interrupted along the profile of the wing. The carcass or body of the boxes 30a, 30b, 30c is made of a suitable material, which may be a molded synthetic material or a sheet of light metal or the like. The boxes are constructed such that they are partially movable relative to each other, in particular articulated so that the respective longitudinal axes of the juxtaposed boxes can tilt relative to each other to vary the profile of each other. the wing and in particular the curvature of each wing section, approximately like an airplane wing. This characteristic makes it possible to adapt the profile of the wing, section after section, according to the wind force and its direction. A fin 30d is pivotally mounted at the end of the last box 30c, at the end opposite the attack profile of the wing, which is located at the front, facing the wind of the first box 30a.
Les figures 3A, 3B et 3C montrent que ia cloison intermédiaire 31a est formée de deux parois 32a et 32b qui sont couplées par une articulation 33 permettant un déplacement relatif de la paroi 32b, mobile par rapport à la paroi 32a qui est fixe. De façon similaire, la cloison intermédiaire 31b est formée de deux parois 34a et 34b qui sont couplées par une articulation 35 qui permet un déplacement relatif dela paroi 34b mobile par rapport à la paroi 32a qui est fixe. Le déplacement relatif des différents caissons de chaque tronçon d'aile est obtenu par des vérins hydrauliques 36 dont les corps sont montés sur lesdites parois fixes 32a et 34a respectivement des cloisons intermédiaires 31a et 31b et dont les pistons sont fixés sur les parois mobiles 32b et 34b. La cloison intermédiaire 31a est formée de deux parois 32a et 32b qui sont couplées par une articulation 33 qui permet un déplacement relatif de la paroi 32b mobile par rapport à ia paroi 32a qui est fixe. Ges moyens permettent de déplacer les caissons 30a, 30b et 30c, respectivement les uns par rapport aux autres en faisant varier les angles relatifs de leur axe longitudinal et en conséquence, de modifier le profil de l'aile au niveau de chacun des tronçons de cette aile. Figures 3A, 3B and 3C show that the intermediate partition 31a is formed of two walls 32a and 32b which are coupled by a hinge 33 allowing a relative displacement of the wall 32b, movable relative to the wall 32a which is fixed. Similarly, the intermediate partition 31b is formed of two walls 34a and 34b which are coupled by a hinge 35 which allows a relative displacement of the movable wall 34b with respect to the wall 32a which is fixed. The relative displacement of the different boxes of each wing section is obtained by hydraulic cylinders 36 whose bodies are mounted on said fixed walls 32a and 34a respectively intermediate partitions 31a and 31b and whose pistons are fixed on the movable walls 32b and 34b. The intermediate partition 31a is formed of two walls 32a and 32b which are coupled by a hinge 33 which allows a relative displacement of the movable wall 32b with respect to the wall 32a which is fixed. These means make it possible to move the boxes 30a, 30b and 30c respectively relative to one another by varying the relative angles of their longitudinal axis and consequently to modify the profile of the wing at each of the sections of this section. wing.
Le premier caisson 30a de chaque tronçon d'aile donne .l'orientation générale du tronçon, le deuxième caisson 30b étant fixé au premier caisson 30a et le troisième caisson 30c étant rattaché au deuxième caisson 30b. L'aileron arrière 30d est fixé au troisième caisson 30e. L'orientation générale du tronçon est donnée par une commande centrale montée dans le premier caisson 30a et qui comprend une couronne dentée 37 coopérant avec un pignon 38 entraîné par un moteur de positionnement 39 agencé pour positionner angulairement le premier caisson 30a de chaque tronçon d'aile en fonction de paramètres météorologiques. Le deuxième caisson 30b et le troisième caisson 30c sont positionnés par les vérins par rapport au premier caisson 30a. Les vues des trois figures 4A, 4B et 4C montrent une installation 10 à deux ailes 12, montées comme décrit précédemment. Le déplacement des ailes engendre le mouvement alternatif d'un piston 40 d'une pompe hydraulique 41 , ce piston étant attaché par son extrémité libre à un bras 42 pivotant actionné par te mouvement des ailes 12, Le montage de la pompe hydraulique est illustré plus en détail par la figure 1 B, Le montage de l'ensemble selon l'invention crée une « boîte de vitesse » hydraulique qui présente en outre, d'une part l'avantage de pouvoir offrir un réglage en continu sur une très grande plage de puissance et solutionner ainsi un problème spécifique des éoliennes qui ont une puissance directement dépendante de la vitesse du vent, et d'autre part d'effectuer un découplage entre la vitesse angulaire instantanée de l'aile et la vitesse linéaire du vérin. Ceci permet à l'aile de procéder librement à la phase d'accélération de son cycle et de pomper le fluide hydraulique pendant la phase de décélération du cycle. La présente invention n'est pas limitée aux formes de réalisations décrites, mais s'étend à toutes les variantes évidentes pour un homme de l'art, qui découlent directement des éléments décrits. Ces variantes peuvent concerner aussi bien la ou les ailes, leur forme générale, les formes dérivées, leur nombre et leur disposition relative que la partie mécanique chargée de convertir la force de la poussée du vent en énergie hydraulique utilisable instantanément ou susceptible d'être stockée. Un des avantages de l'ensemble décrit par rapport aux éoliennes rotatives, considérées aujourd'hui comme classiques, est leur relativement faible encombrement, leur facilité d'installation, la possibilité d'adapter leurs dimensions aux besoins beaux, par exemple privés, le faible coût de leur construction et de leur installation, le niveau modeste des frais de gestion, de sorte que cette installation est en mesure d'apporter au problème de la génération d'énergie alternative une solution économique et conviviale lui permettant de sortir du cercle fermé des très grosses structures et de s'ouvrir à des utilisateurs particuliers. The first box 30a of each wing section gives the general orientation of the section, the second box 30b being fixed to the first box 30a and the third box 30c being attached to the second box 30b. The rear wing 30d is fixed to the third box 30e. The general orientation of the section is given by a central control mounted in the first box 30a and which comprises a ring gear 37 cooperating with a pinion 38 driven by a positioning motor 39 arranged to angularly position the first box 30a of each section of wing according to meteorological parameters. The second box 30b and the third box 30c are positioned by the cylinders relative to the first box 30a. The views of the three figures 4A, 4B and 4C show an installation 10 with two wings 12, mounted as described above. The displacement of the wings causes the reciprocating movement of a piston 40 of a hydraulic pump 41, this piston being attached by its free end to a pivoting arm 42 actuated by the movement of the wings 12. The mounting of the hydraulic pump is illustrated more in detail in Figure 1 B, The assembly of the assembly according to the invention creates a hydraulic "gearbox" which has, on the one hand, the advantage of being able to offer a continuous adjustment over a very wide range of power and thus solve a specific problem of wind turbines that have a power directly dependent on the wind speed, and secondly to decoupling between the instantaneous angular speed of the wing and the linear speed of the cylinder. This allows the wing to proceed freely to the acceleration phase of its cycle and to pump the hydraulic fluid during the deceleration phase of the cycle. The present invention is not limited to the embodiments described, but extends to all obvious variations for those skilled in the art, which arise directly from the elements described. These variants may concern both the wing or wings, their general shape, the derived forms, their number and their relative arrangement as the mechanical part responsible for converting the force of the wind pressure into hydraulic energy that can be used instantly or that can be stored. . One of the advantages of the assembly described with respect to rotary wind turbines, considered today as conventional, is their relatively small size, their ease of installation, the possibility of adapting their dimensions to the beautiful needs, for example private, the weak cost of their construction and installation, the modest level of management fees, so that this facility is able to bring to the problem of alternative energy generation an economical and user-friendly solution allowing it to leave the closed circle of very big structures and open to particular users.

Claims

Revendications claims
1. Ensemble (10) pour capter l'énergie du vent et pour la transformer en énergie utilisable directement ou pouvant être stockée en vue d'une utilisation ultérieure, notamment en énergie mécanique transformable ensuite en énergie électrique ou en énergie hydraulique, caractérisé en ce qu'il comporte au moins un support disposé dans un secteur venté, sur lequel est montée au moins une aile (12) allongée ayant une première extrémité fixe solidaire dudit support et une seconde extrémité libre, cette aile (12) étant animée d'un mouvement oscillant autour d'un axe fixe porté par ledit support, cet axe fixe passant par ladite première extrémité fixe de l'aile, ledit mouvement d'oscillant s'ëffectuant alternativement entre une première position inclinée par rapport à là verticale et une deuxième position inclinée par rapport à la verticale, angulairement décalée par rapport à ladite première position, et en ce que ladite aile est composée d'une pluralité de tronçons (12a, 12b, 12c et 12d) superposés indépendants disposés entre ladite première extrémité fixe et ladite seconde extrémité libre. 1. A set (10) for capturing wind energy and for converting it into energy that can be used directly or that can be stored for later use, in particular mechanical energy which can then be converted into electrical energy or hydraulic energy, characterized in that it comprises at least one support disposed in a windy sector, on which is mounted at least one elongated wing (12) having a fixed first end secured to said support and a second free end, this wing (12) being driven by a oscillating movement about a fixed axis carried by said support, this fixed axis passing through said fixed first end of the wing, said oscillating movement alternately occurring between a first position inclined relative to there vertical and a second position inclined relative to the vertical, angularly offset from said first position, and in that said wing is composed of a plurality sections (12a, 12b, 12c and 12d) independent bunk disposed between said first fixed end and said second free end.
2. Ensemble pour capter l'énergie du vent selon la revendication 1 , caractérisé en ce que chacun desdits tronçons de ladite pluralité de tronçons (12a, 12b, 12c et 12d} est constitué d'un assemblage de caissons (30a, 30b, 30c) juxtaposés ie long d'une ligne centrale, et en ce que Iesdits caissons (30a, 30b, 30c) sont articulés les uns par rapport aux autres de telle manière que chacun des axes longitudinaux: desdits caissons juxtaposés puisse pivoter angulairement l'un par rapport aux axes longitudinaux de chacun des caissons juxtaposés. 2. A set for capturing wind energy according to claim 1, characterized in that each of said sections of said plurality of sections (12a, 12b, 12c and 12d) consists of an assembly of boxes (30a, 30b, 30c ) juxtaposed along a central line, and in that said boxes (30a, 30b, 30c) are articulated with respect to each other so that each of the longitudinal axes: said juxtaposed boxes can rotate angularly one by relative to the longitudinal axes of each of the juxtaposed caissons.
3. Ensemble pour capter l'énergie du vent selon la revendication 1 , caractérisé en ce que chacun desdits caissons (30a, 30b, 30c) est fermé et comporte une cloison intermédiaire (31a et 31b) le séparant d'un caisson adjacent. 3. The assembly for capturing wind energy according to claim 1, characterized in that each of said boxes (30a, 30b, 30c) is closed and has an intermediate partition (31a and 31b) separating it from an adjacent box.
4. Ensemble pour capter l'énergie du vent selon la revendication 3, caractérisé en ce que ladite cloison intermédiaire (31a et 31b) est constituée de deux parois (32a et 32b ; 34a, 34b) appartenant respectivement à un premier caisson et à un deuxième caisson adjacent au premier. 4. An assembly for capturing wind energy according to claim 3, characterized in that said intermediate partition (31a and 31b) consists of two walls (32a and 32b; 34a, 34b) respectively belonging to a first box and a second box adjacent to the first.
5. Ensemble pour capter l'énergie du vent selon la revendication 4, caractérisé en ce que lesdites parois (32a et 32b ; 34a, 34b) appartenant respectivement à un premier caisson et à un deuxième caisson adjacent au premier sont articulées l'une par rapport à l'autre. 5. An assembly for capturing wind energy according to claim 4, characterized in that said walls (32a and 32b, 34a, 34b) respectively belonging to a first caisson and a second caisson adjacent to the first are articulated one by report to the other.
6. Ensemble pour capter l'énergie du vent selon la revendication 1 , caractérisé en ce que ledit support est composé d'un socle (11) comportant une plateforme circulaire (16a) rotative au moyen de galets (16b) appuyés sur un plateau fixe (16c). 6. A set for capturing wind energy according to claim 1, characterized in that said support is composed of a base (11) having a circular platform (16a) rotatable by means of rollers (16b) supported on a fixed plate (16c).
7. Ensemble pour capter l'énergie du vent selon la revendication 6. caractérisé en ce que la plateforme (16a) porte un bâti (17) comprenant deux parois latérales verticales (17a et 17b); montées paraHèlement entre elles et une plaque de base (17c), ledit bâti portant un assemblage oscillant sur lequel est montée ladite au moins une aile (12). 7. A set for capturing wind energy according to claim 6. characterized in that the platform (16a) carries a frame (17) comprising two vertical side walls (17a and 17b); mounted parallel to each other and a base plate (17c), said frame carrying an oscillating assembly on which is mounted said at least one wing (12).
8. Ensemble pour capter l'énergie du vent selon l'une quelconque des revendications précédentes, caractérisée en ce que ledit bâti (17) abrite au moins une pompe hydraulique (21a ou 21b), dont le corps est monté sur au moins une tringle traversante (22a ou 22b) et dont le piston est couplé indirectement, respectivement à au moins un étrier (23a ou 23b) solidaire de la surface inférieure de la traverse (18c). 8. assembly for capturing wind energy according to any one of the preceding claims, characterized in that said frame (17) houses at least one hydraulic pump (21a or 21b), whose body is mounted on at least one rod through (22a or 22b) and whose piston is coupled indirectly, respectively to at least one yoke (23a or 23b) integral with the lower surface of the cross member (18c).
PCT/IB2014/060168 2013-04-30 2014-03-26 Assembly for collecting wind energy and for transforming same into usable energy WO2014177948A1 (en)

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CH8932013A CH707974A2 (en) 2013-04-30 2013-04-30 Set to capture the energy of the wind and turn it into usable energy.

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Publication number Priority date Publication date Assignee Title
FR3037621B1 (en) * 2015-06-19 2020-02-14 Manuel Villeneuve SENSOR DEVICE, ADVANTABLY OF THE WIND OR HYDROLIAN TYPE, FOR CAPTURING THE KINETIC ENERGY OF A FLUID FLOW
CH714054A1 (en) * 2017-08-11 2019-02-15 Horeos Sarl C/O Emmanuel Vuille A device with an oscillating rectilinear wing for the transformation of the kinetic energy from the wind or an aquatic current into a mechanical energy and method for such a transformation.

Citations (4)

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Publication number Priority date Publication date Assignee Title
US4024409A (en) * 1975-01-07 1977-05-17 Payne Peter R Aeolian windmill
US20070297903A1 (en) * 2005-02-25 2007-12-27 Wind Innovations Llc Oscillating fluid power generator
WO2009041819A2 (en) * 2007-09-28 2009-04-02 Tenca Device for generating power from wind flow or water flow
US20090224553A1 (en) * 2008-03-04 2009-09-10 Johnnie Williams Oscillating Windmill

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4024409A (en) * 1975-01-07 1977-05-17 Payne Peter R Aeolian windmill
US20070297903A1 (en) * 2005-02-25 2007-12-27 Wind Innovations Llc Oscillating fluid power generator
WO2009041819A2 (en) * 2007-09-28 2009-04-02 Tenca Device for generating power from wind flow or water flow
US20090224553A1 (en) * 2008-03-04 2009-09-10 Johnnie Williams Oscillating Windmill

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