ES2568501T3 - Un procedimiento de fabricación de una pala de turbina eólica que comprende un larguero a partir de elementos que tienen porciones de extremo que se extienden transversalmente con respecto a una porción intermedia y la pala de turbina eólica relacionada - Google Patents
Un procedimiento de fabricación de una pala de turbina eólica que comprende un larguero a partir de elementos que tienen porciones de extremo que se extienden transversalmente con respecto a una porción intermedia y la pala de turbina eólica relacionada Download PDFInfo
- Publication number
- ES2568501T3 ES2568501T3 ES09765921.3T ES09765921T ES2568501T3 ES 2568501 T3 ES2568501 T3 ES 2568501T3 ES 09765921 T ES09765921 T ES 09765921T ES 2568501 T3 ES2568501 T3 ES 2568501T3
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- Spain
- Prior art keywords
- intermediate portion
- end portions
- wind turbine
- turbine blade
- covers
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- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 abstract 1
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- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
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
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/02—Assembly jigs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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- B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/112—Single lapped joints
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- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
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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
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/05—Particular design of joint configurations
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- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
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- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
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- B29C66/543—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles joining more than two hollow-preforms to form said hollow articles
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
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- B29D23/00—Producing tubular articles
- B29D23/001—Pipes; Pipe joints
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
- F03D80/30—Lightning protection
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/00—General aspects of processes or apparatus for joining preformed parts
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- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
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- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
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- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7394—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
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Abstract
Un procedimiento de fabricación de una pala de turbina eólica (19) que comprende un larguero (1), comprendiendo el procedimiento las etapas de: - proporcionar al menos dos tapas (2), formando cada tapa (2) una porción intermedia (4) entre dos porciones de extremo (5) y que está configurada para su fijación a una carcasa de pala (20, 21), de modo que la porción intermedia (4) de una de las tapas (2) está orientada hacia una carcasa de pala o forma parte de una superficie aerodinámicamente activa de la pala y la porción intermedia (4) de la otra de las tapas (2) está orientada hacia otra carcasa de pala o forma parte de la superficie aerodinámicamente activa de la pala, donde cada una de las porciones de extremo (5) forma una porción de superficie de unión de tapa (6) a lo largo de un borde que se extiende longitudinal de la porción de extremo (5) y la porción intermedia (4) forma una porción de superficie exterior (7) del larguero, - proporcionar al menos dos bandas (3), estando provista cada banda (3) de porciones de superficie de unión de banda (8) a lo largo de bordes opuestos y que se extienden longitudinalmente y - conectar las porciones de superficie de unión (6) de las tapas con las porciones de superficie de unión (8) de las bandas para formar una configuración tubular del larguero (1), en el que las tapas (2) se proporcionan de manera que las porciones de extremo (5) se extienden transversalmente a la porción intermedia (4) y en el que las tapas (2) están dispuestas entre sí de manera que las porciones de extremo (5) de una tapa (2) se extienden desde la porción intermedia (4) hacia las porciones de extremo (5) de otra tapa (2).
Description
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La figura 2a ilustra partes de una realización de un larguero 1 en el que las bandas 3a, 3b comprenden una pluralidad de elementos de banda 10a 10b. Para evitar una unión a tope entre los elementos de banda 10a, 10b, cada uno de los elementos de banda 10a, 10b comprende una superficie de unión 11a, 11b que termina en un ángulo agudo. Esto aumenta el área de las superficies de unión 11a, 11b y facilita la unión de los elementos de banda 10a 10b.
Las figuras 2b y 2c ilustran una realización alternativa de un larguero 1 en la que las bandas 3a, 3b comprenden una pluralidad de elementos de banda 10a, 10b, 10c. En lugar de la unión de solapamiento que se ilustra en la figura 2a, los elementos de banda 10a, 10b se unen en sus secciones de extremo formando, en esta realización, un recorte elíptico que deja un orificio 36 en las bandas 3a, 3b. En el área recortada 36, las cargas de corte son tomadas por las tapas 2a, 2b.
La figura 2b también ilustra que las uniones de banda, es decir las uniones entre dos elementos de banda adyacentes 10a, 10b y 10b, 10c, están escalonadas a lo largo de la longitud del larguero 1 montado para evitar que las uniones de banda en lados opuestos del larguero 1 estén colocadas vis-à-vis entre sí. Esta manera de escalonar las uniones de banda es también aplicable para las uniones de banda de la figura 2a.
La figura 2b ilustra una alternativa adicional de una realización de un larguero 1 en el que las bandas 3a, 3b comprenden una pluralidad de elementos de banda 10a 10b, 10c. Como se ilustra, dos elementos de banda adyacentes 10a, 10b -10b, 10c tienen interfaces 100 que no están conectadas entre sí.
Esto significa, que estos elementos de banda adyacentes 10a, 10b -10b, 10c no están conectados directamente entre sí sino solo conectados entre sí a través de las tapas 2a, 2b a las que están ambos unidos. En consecuencia, los elementos de banda adyacentes 10a, 10b -10b, 10c no están unidos, pegados, atornillados o fijados de manera similar entre sí.
Cuando no se conectan los elementos de banda 10a, 10b -10b, 10c, solamente la unión de las tapas 2a, 2b y las bandas 3a, 3b es necesaria y se puede omitir unión adicional para los elementos de banda. Esto puede disminuir la cantidad de adhesivo necesaria para el montaje del larguero 1 y el tiempo implicado en el montaje del larguero y por lo tanto reducir los costes asociados con el mismo. Los orificios 36 se pueden utilizar para el acceso de Inspección y están conformados de manera que reducen al mínimo las concentraciones de tensión en el extremo de los elementos de banda.
La figura 3A ilustra una realización de un molde de tapa 12 con una tapa 2a y la figura 3b ilustra una realización de un molde de banda 13 con una banda 3a.
El molde de tapa 12 comprende un molde inferior 14 y dos extensiones de molde superiores 15. La superficie interior de las extensiones de molde superior 15 está provista de un material que no se adhiere a la resina de la tapa 2a y que además es capaz de definir geométricamente las porciones de unión de superficie de la tapa 6 mediante el contacto con la misma. Un ejemplo de un material tal es una capa de tela.
La porción de superficie exterior 7 de la porción intermedia 4 se define también por el contacto con la superficie interior del molde de tapa 12.
La superficie interna del molde de tapa 12 comprende dos puntos de referencia 16 en forma de pequeños salientes, un pequeño cono. Cada uno de los puntos de referencia 16 forma una hendidura 17 en la tapa 2a durante su moldeo. Estas hendiduras 17 se utilizan para colocar la tapa 2a con relación a las bandas 3a, 3b (no mostradas) antes de conectarlas. El posicionamiento se puede hacer mediante el uso de una herramienta de montaje.
Como se ilustra en la figura 3b, la superficie interior 18 y las porciones de superficie de unión de banda 8 de la banda 3a se definen por contacto con el molde de banda 13, permitiendo así una geometría bien definida de las porciones de superficie de unión de banda 8 que se van a unir con las porciones de superficie de tapa 5. Es decir, las porciones de superficie de unión 6, 8 coincidentes están moldeadas para facilitar una unión más precisa entre las tapas 2a, 2b y las bandas 3a, 3b.
Las figuras 4a y 4b ilustran dos formas diferentes de fijar el larguero 1 a las carcasas de una pala de turbina eólica
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En la figura 4a el larguero 1 se coloca entre dos carcasas de pala 20a, 20b de la pala de turbina eólica 19a. Las porciones de superficie exteriores 7 forman una cara de contacto para su montaje con las carcasas de pala 20a, 20b. El larguero 1 se une a las carcasas de pala 20a, 20b mediante la adición de un adhesivo (no mostrado) a la porción de superficie exterior 7 de cada una de las tapas 2a, 2b.
En la figura 4b se ilustra una realización alternativa. Las porciones de superficie exteriores 7 están adaptadas para formar parte de la superficie aerodinámicamente activa de la pala de turbina eólica 19b. Por lo tanto, el larguero 1 no está encapsulado completamente dentro de las carcasas de pala 21a, 21b, 21c.
La figura 5 ilustra un larguero 1 que comprende dos tapas 2a, 2b y dos bandas 3a, 3b. Las tapas 2a, 2b comprenden
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Claims (1)
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PCT/EP2009/057683 WO2009153342A2 (en) | 2008-06-20 | 2009-06-19 | A method of manufacturing a spar for a wind turbine from elements having end portions extending transversely to an intermediate portion |
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EP2295235B1 (en) * | 2009-08-20 | 2013-07-03 | Siemens Aktiengesellschaft | Fiber reinforced plastic-structure and a method to produce the fiber reinforced plastic-structure |
CN102022254B (zh) * | 2009-09-23 | 2014-12-17 | 固瑞特模具(太仓)有限公司 | 风轮机叶片及其生产方法 |
IT1401996B1 (it) * | 2010-09-30 | 2013-08-28 | Wilic Sarl | Metodo per realizzare un longherone tubolare di una pala di una turbina eolica |
US8186964B2 (en) * | 2010-12-10 | 2012-05-29 | General Electric Company | Spar assembly for a wind turbine rotor blade |
ES2399259B1 (es) * | 2011-05-24 | 2014-02-28 | Gamesa Innovation & Technology, S.L. | Un método de unión para una pala de aerogenerador multi-panel. |
EP2570254A1 (en) * | 2011-09-15 | 2013-03-20 | Siemens Aktiengesellschaft | Method for manufacturing a wind turbine rotor blade with a shear web |
FR2981880B1 (fr) * | 2011-10-28 | 2014-09-19 | Daher Aerospace | Procede pour etancher un reservoir de carburant |
US20130216388A1 (en) * | 2012-02-20 | 2013-08-22 | General Electric Company | Box-shaped shear web for wind turbine blades and method of making |
DE102012107932C5 (de) * | 2012-08-28 | 2024-01-11 | Siemens Gamesa Renewable Energy Service Gmbh | Verfahren zur Fertigung eines Rotorblattes und ein Rotorblatt einer Windenergieanlage |
FR3005280B1 (fr) * | 2013-05-06 | 2015-05-15 | Safran | Outillage pour la fixation d'un renfort metallique sur le bord d'attaque d'une aube de turbomachine et procede utilisant un tel outillage |
GB2524489B (en) * | 2014-03-24 | 2016-02-24 | Marine Current Turbines Ltd | Turbine blade and method of manufacture |
EP2927481B1 (en) * | 2014-03-31 | 2021-09-22 | Siemens Gamesa Renewable Energy A/S | Rotor blade for a wind turbine |
US10293930B2 (en) * | 2015-01-14 | 2019-05-21 | Sikorsky Aircraft Corporation | Spar end cap with drain hole provisions |
US10830207B2 (en) * | 2018-08-28 | 2020-11-10 | General Electric Company | Spar configuration for jointed wind turbine rotor blades |
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2009
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- 2009-06-19 WO PCT/EP2009/057683 patent/WO2009153342A2/en active Application Filing
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- 2009-06-19 DK DK09765921.3T patent/DK2310185T3/en active
- 2009-06-19 EP EP09765921.3A patent/EP2310185B1/en active Active
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CN102123849A (zh) | 2011-07-13 |
EP2310185A2 (en) | 2011-04-20 |
EP2310185B1 (en) | 2016-01-27 |
CN102123849B (zh) | 2015-03-11 |
WO2009153342A3 (en) | 2010-03-18 |
DK2310185T3 (en) | 2016-04-18 |
US8899936B2 (en) | 2014-12-02 |
WO2009153342A2 (en) | 2009-12-23 |
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