EP2831409A1 - Elément composite renforcé de fibres pour une pale de rotor, dispositif de fabrication d'un élément composite renforcé de fibres pour une pale de rotor et procédé de fabrication d'un élément composite renforcé de fibres pour une pale de rotor - Google Patents

Elément composite renforcé de fibres pour une pale de rotor, dispositif de fabrication d'un élément composite renforcé de fibres pour une pale de rotor et procédé de fabrication d'un élément composite renforcé de fibres pour une pale de rotor

Info

Publication number
EP2831409A1
EP2831409A1 EP13709758.0A EP13709758A EP2831409A1 EP 2831409 A1 EP2831409 A1 EP 2831409A1 EP 13709758 A EP13709758 A EP 13709758A EP 2831409 A1 EP2831409 A1 EP 2831409A1
Authority
EP
European Patent Office
Prior art keywords
mold
rotor blade
fiber composite
composite component
manufacturing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP13709758.0A
Other languages
German (de)
English (en)
Inventor
Christian Flach
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Senvion GmbH
Original Assignee
Senvion GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Senvion GmbH filed Critical Senvion GmbH
Publication of EP2831409A1 publication Critical patent/EP2831409A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F03D1/0675—Rotors characterised by their construction elements of the blades
    • 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
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/681—Component parts, details or accessories; Auxiliary operations
    • 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
    • B29K2105/25—Solid
    • 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
    • B29K2823/00—Use of polyalkenes or derivatives thereof as mould material
    • B29K2823/04—Polymers of ethylene
    • B29K2823/06—PE, i.e. polyethylene
    • 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
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0018—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular optical properties, e.g. fluorescent or phosphorescent
    • B29K2995/0026—Transparent
    • 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
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2280/00—Materials; Properties thereof
    • F05B2280/60—Properties or characteristics given to material by treatment or manufacturing
    • F05B2280/6003—Composites; e.g. fibre-reinforced
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50—Manufacturing or production processes characterised by the final manufactured product

Definitions

  • FIBER COMPOSITE COMPONENT FOR A ROTOR BLADE PRODUCTION DEVICE FOR A FIBER COMPOSITE COMPONENT FOR A ROTOR BLADE, AND METHOD FOR PRODUCING A FIBER COMPOSITE COMPONENT FOR A ROTOR BLADE
  • the invention relates to a fiber composite component for a rotor blade of a wind energy plant with a defined predetermined first surface formed on a first side of the fiber composite component.
  • the invention further relates to a production device for producing a fiber composite component for a rotor blade of a wind energy plant using a vacuum infusion process comprising an open manufacturing mold with a molding surface for forming a first surface on a first side of the fiber composite component.
  • the invention also relates to a method for manufacturing a fiber composite component for a rotor blade of a wind energy plant using a vacuum infusion process in an open manufacturing mold, wherein a first surface is formed on a first side of the fiber composite component by means of a mold surface of the manufacturing mold.
  • the invention further relates to a rotor blade for a wind power plant and to a method for manufacturing a rotor blade for a wind turbine.
  • Typical rotor blades consist of at least two rotor blade shells, which specify the outer shape and thus the essential aerodynamic properties of the rotor blade.
  • the rotor blade shells are usually reinforced in the region of the largest profile thickness of the rotor blade by so-called straps and connected to each other in the belt by main webs.
  • the straps and the main webs form the essential supporting structure of the rotor blade.
  • the aerodynamically relevant outer side has a surface with excellent quality, while the inside, on which, for example, the main webs are glued, is relatively rough and uneven.
  • the adhesive joint for example, generously applied adhesive on the inside of the rotor blade shell and pressed a main web with a certain force in the adhesive. The adhesive compensates for unevenness between the components to be joined, so that after curing, there is a surface connection between the components.
  • the object of the present invention is the quality, rigidity and / or life of a single rotor blade and the reproducibility of these properties in a variety of similar rotor blades improve.
  • a fiber composite component for a rotor blade of a wind energy plant with a defined predetermined first surface on a first side of the fiber composite component, which is further developed by the fiber composite component a second defined predetermined shaped surface for connection to another component for the rotor blade Having at least a portion of one of the first side facing away from the second side of the fiber composite component.
  • the second defined predetermined shaped surface is provided, for example, by aftertreating a fiber composite component produced by means of the described vacuum infusion method on the second side.
  • the fit of two components to be joined together is improved for a rotor blade.
  • the invention makes it possible for the second surface of the fiber composite component to be complementary in shape or in sections to form complementary to the further component.
  • the fiber composite component according to the invention is to the fiber composite component according to the invention a mark for a desired position of the further component on or arranged on the second surface.
  • a mark for a desired position of the further component on or arranged on the second surface is ensured to each other when connecting the two components.
  • a control of the relative arrangement of the components to each other after the connection is made possible, so that any production errors can be detected and optionally corrected.
  • the marking is designed as a stop, wherein in particular the further component in the desired position is positively aligned or aligned with the stop. This ensures that the additional component can not slip in the desired position before the final connection with the fiber composite component according to the invention.
  • the fiber composite component is preferably a rotor blade shell or a belt, wherein the further component is in particular a web or a main web.
  • the object on which the invention is based is also achieved by a production device for producing a fiber composite component for a rotor blade of a wind energy plant using a vacuum infusion process comprising an open production mold with a molding surface for forming a first surface on a first side of the fiber composite component, wherein the manufacturing device is further developed in that the production device has a mold insert with a molding surface for forming a second surface for connecting the fiber composite component having a further component for the rotor blade, wherein the mold insert on or in the manufacturing form can be arranged such bar, arranged or arranged that the mold surface of the mold insert of the mold surface of the manufacturing mold is facing.
  • the production device makes it possible to manufacture a fiber composite component according to the invention using a vacuum infusion method.
  • the open manufacturing mold is thereby at least partially covered by the mold insert, so that a cavity for the fiber composite component to be produced is formed between the manufacturing mold and the mold insert.
  • the mold insert preferably covers only a portion of the entire manufacturing form, so that the mold insert is smaller in size than the manufacturing mold. This provides an easy-to-use mold insert of relatively low weight which nevertheless is sufficiently stable for forming a defined and reproducible cavity for the fiber composite component.
  • This cavity is preferably completely filled with resin in the manufacture of the fiber composite component, so that in each case a defined predetermined and reproducible surface is formed on one side of the fiber composite component by the forming surface of the manufacturing mold and on the opposite side of the fiber composite component by the mold surface of the mold insert.
  • the mold surface of the mold insert preferably has a marking form, for example a protrusion or a depression, for forming a marking for a desired position of the further component on or on the second surface of the fiber composite component.
  • the mold insert is at least partially transparent. This allows the distribution of resin in the mold to be observed and controlled during the vacuum infusion process.
  • a material of the mold insert comprises polyethylene.
  • Such materials are usually self-separating when dealing with epoxy resins, so that after curing of the finished fiber composite component a simple demolding is guaranteed.
  • the molding surface of the mold insert comprises a material with polyethylene or consists of such a material.
  • mold inserts or components for polyethylene mold inserts can be produced simply and inexpensively, for example in a deep-drawing process.
  • a particularly preferred production device is characterized in that a positioning device is included for reproducible positioning of the mold insert on or in the production mold.
  • a positioning device is included for reproducible positioning of the mold insert on or in the production mold.
  • a sealing device for a common contact region of the manufacturing mold and the mold including deposits is, for example, a surface or a line on or along which touch the mold and the mold insert.
  • the object underlying the invention is also achieved by a method for manufacturing a fiber composite component for a rotor blade of a wind energy plant using a vacuum infusion process in an open manufacturing mold, wherein a first surface is formed on a first side of the fiber composite component by means of a molding surface of the manufacturing mold, wherein the method is further developed in that in the manufacture of the fiber composite component, a mold insert is arranged on or in the manufacturing mold, wherein by means of one of the mold surface of the mold facing mold surface of the mold insert a second surface for connecting the fiber composite component with another component for the rotor blade at least a partial region of the first side remote from the second side of the fiber composite component is or is formed.
  • This method is particularly suitable for execution by means of the production device according to the invention described above.
  • a marking for a desired position of the further component is or is formed on or on the second surface of the fiber composite component on or on the second surface. This is done, for example, by subsequent to the introduction of resin into the production mold, which is preferably carried out using the vacuum infusion method, a marking on or on the second surface of the fiber composite component. is brought. For example, the mark is pressed or embossed into the resin before the final cure, or a mark is applied to the at least partially cured resin, for example glued or painted.
  • the marking is or is formed by means of the molding surface of the mold insert, in particular by means of a marking mold of the molding surface.
  • the open mold for the vacuum infusion process is sealed using the mold insert.
  • the areas of the open manufacturing mold, which are not covered by the mold insert, are thereby sealed, for example by means of a vacuum film.
  • the entire manufacturing form including the mold insert is covered and sealed by means of a vacuum film or the mold insert only after sealing the entire manufacturing form by means of a vacuum film or inserted.
  • the object underlying the invention is also achieved by a rotor blade for a wind energy plant with a fiber composite component according to the invention.
  • the object is also achieved by a method for manufacturing such a rotor blade, wherein the fiber composite component is connected to the second surface with a further component for the rotor blade.
  • an alignment of the fiber composite component and the other component is preferably checked each other after the connection based on the mark. It is also advantageous if the fiber composite component and the further component are aligned before joining by means of the marking to each other.
  • Fig. 1 shows schematically a wind turbine
  • FIG. 3 schematically shows the joining together of two rotor blade shells according to the invention and two main webs to form a rotor blade according to the invention
  • FIG. 4 schematically shows a production device according to the invention in a perspective view
  • Fig. 5 shows the manufacturing device of Fig. 4 in a schematic sectional view
  • Fig. 6 shows schematically the joining of two rotor blade shells and two main webs to a rotor blade according to the invention in a further embodiment.
  • a rotor blade 2 consists, for example, of a plurality of components manufactured in fiber composite construction, which are glued together.
  • Fig. 2 shows schematically how a rotor blade 2 of the prior art of two rotor blade shells 3 and two main webs 4 is assembled. Shown is a sectional view along the line A-A on the finished rotor blade in Fig. 1st
  • the rotor blade shells 3 and the main webs 4 are manufactured individually in fiber composite construction using a vacuum infusion process.
  • fiber material is laid out in an open mold, the mold is sealed by means of a vacuum film, the air between the mold and the vacuum film is evacuated, and then resin is passed into the evacuated mold so that the fiber material is impregnated with resin between the mold and the vacuum film becomes.
  • the component produced in this way has a defined upper surface on the side facing the manufacturing mold. surface, which is predetermined by the surface of the manufacturing mold. In the case of the rotor blade shells 3 shown in FIG. 2, this is the outside 11 or the surface 12 of the outside 11.
  • the side that is covered with the vacuum film during production is not able to control the final surface.
  • the side that is covered with the vacuum film during production is not able to control the final surface.
  • forms the flexible vacuum film when evacuating the manufacturing form wrinkles, which later fully run resin.
  • the thickness of the component in the production process can thus only be specified within relatively rough inaccuracies.
  • this is the inner side 13 or the surface of the inner side 12.
  • a belt 5 is in each case incorporated in the rotor blade shells 3, wherein two main webs 4 are glued in between the belts 5 or between the rotor blade shells 3 in the region of the belts 5.
  • the main webs 4 have at their edges angled web feet to allow a large-area adhesive bond with the rotor blade shells 3.
  • the second rotor blade shell 3 is likewise provided with adhesive 6 and placed on the first rotor blade shell 3 with the glued-in main webs 4.
  • a certain compressive force F is used in the direction of the arrow shown to press the main webs 4 in the adhesive 6 and to obtain a flat and resilient connection between the main webs 4 and the upper rotor blade shell 3.
  • Due to the curved shape of the rotor blade shell 3 act by the applied compressive force F transverse forces on the upper ends of the main webs 4, which lead to an evasive movement F 'of the main webs 4 relative to the upper rotor blade shell 3 in the direction of the arrows.
  • FIG. 3 schematically illustrates the assembly of a rotor blade 2 according to the invention with rotor blade shells 3 designed according to the invention.
  • a rotor blade shell 3 according to the invention for the rotor blade 2 according to the invention has on the outer side 11 a defined predetermined surface 12 for the desired aerodynamic properties of the rotor blade 2.
  • the rotor blade shell 3 according to the invention also has on the inner side 13 a defined predetermined shaped surface 14, on which the main webs 4 are glued.
  • the defined predetermined shaped surface 14 is formed in particular complementary to the web feet of the main webs 4, so that the main webs 4 are precisely inserted between the two rotor blade shells 3 according to the invention.
  • the markings 17 are designed as stops for the web feet of the main webs 4, so that slipping of the web feet is precluded from the outset.
  • the device comprises a manufacturing mold 20 with a first molding surface 22 for molding the outer surface 12 of the rotor blade shell 3.
  • the device further comprises a mold insert 30 with a second mold surface 32 for a surface 14 on the inside of the rotor blade shell 3.
  • the mold insert 30 is placed on the edges 24 of the mold 20 such that between the mold 20 and the mold insert 30, a cavity 50 forms, as shown in the sectional view in Fig. 5.
  • the cavity 50 is limited by the molding surface 22 of the mold 20 and the mold surface 32 of the mold insert 30th
  • first fiber material and other components for the rotor blade shell 3 are laid out on the forming surface 22 of the production mold 20. Then, the mold insert 30 is placed on the mold 20 and on the edge 24 of the mold 20.
  • the correct positioning of the mold insert 30 on the edge 24 of the manufacturing mold 20 is ensured, for example, by suitable positioning devices 42. These are for example pins attached to the edges 24 of the production mold 20 and complementary holes for the pins on the mold insert 30.
  • the mold insert 30 is at least partially transparent, so that the distribution of the resin in the cavity 50 between the mold insert 30 and the mold 20 is observable. As a result, in particular air pockets can already be detected and corrected during the resin infusion.
  • the mold insert 30 is made of, for example, an extrusion molding process using a material or material with polyethylene.
  • the mold insert 30 is simple and inexpensive to produce and, in particular because the mold insert 30 is substantially smaller than the mold 20, also sufficiently stable.
  • the mold insert 30 or the mold surface 32 of the mold insert 30 has two Marking forms 34 in the form of grooves.
  • the manufacturing mold 20 is sealed by means of a vacuum foil.
  • the mold insert 30 can be used for the seal when between the mold insert 30 and the manufacturing mold 20, a seal 40 is provided.
  • the manufacturing mold 20 shown by way of example in FIGS. 4 and 5 has, at the edges 24, channels for a seal 40, for example a hose seal made of rubber.
  • the fiber material and other materials in the manufacturing mold 20 for the rotor blade shell 3 are impregnated with resin in a vacuum infusion process.
  • the cavity 50 between the mold insert 30 and the manufacturing mold 20 is completely filled with resin, so that by means of the mold surface 32 of the mold insert a surface 14 of the rotor blade shell 3 defined defined or shaped.
  • the grooves of the marking forms 34 are filled with resin, so that after curing of the resin markings 17 are provided for the desired position of the main webs 4 on the rotor blade shell 3.
  • the material for the rotor blade shell 3 is designed in the manufacturing mold 20, sealed the entire manufacturing mold 20 by means of a vacuum film, the mold evacuated under the vacuum film and soaked the material for the rotor blade shell 3 in a vacuum infusion process with resin. Then, before curing of the resin, the mold 30 was placed on the mold and pressed so that the still liquid resin under the vacuum film by means of the mold surface 32 of the mold insert 30 is modeled or molded. This also results in a defined predetermined surface 14 on the inner side 13 of the rotor blade shell third
  • FIG. 6 shows schematically the joining of two rotor blade shells 3 according to the invention and two main webs 4 to form a rotor blade 2 according to the invention in a further embodiment, which is varied with respect to the embodiment from FIG. 3.
  • the main webs 4 have at their ends, for example, a Y-shape, which fit into the markings 17 or fit on the marking 17.
  • the markings 17 are complementary in shape to the ends of the main webs 4 or the main webs 4 are at least partially complementary to the markings 17 at their ends.
  • this measure a very accurate positioning of the main webs 4 when assembling the rotor blade shells 3 according to the invention is possible.

Abstract

L'invention concerne un élément composite renforcé de fibres (3, 4, 5) pour une pale de rotor (2) d'une installation d'énergie éolienne (1), présentant une première surface (12, 14) façonnée de manière définie sur une première face (11, 13) de l'élément composite renforcé de fibres (3, 4, 5). L'élément composite renforcé de fibres (3, 4, 5) selon l'invention est perfectionné en ce que l'élément composite renforcé de fibres (3, 4, 5) présente une deuxième surface (14, 12) façonnée de manière définie, destinée au raccordement à un autre élément (3, 4, 5) pour la pale de rotor (2) sur au moins une zone partielle d'une deuxième face (13, 11) opposée à la première face (11, 13) de l'élément composite renforcé de fibres (3, 4, 5). L'invention concerne en outre un dispositif pour la fabrication d'un élément composite renforcé de fibres (3, 4, 5) pour une pale de rotor (2) d'une installation d'énergie éolienne (1) utilisant un dispositif d'infusion sous vide, et un procédé pour la fabrication d'un élément composite renforcé de fibres (3, 4, 5) pour une pale de rotor (2) d'une installation d'énergie éolienne (1) utilisant un procédé d'infusion sous vide. L'invention concerne en outre une pale de rotor (2) pour une installation d'énergie éolienne (1), et un procédé de fabrication d'une pale de rotor (2).
EP13709758.0A 2012-03-27 2013-02-28 Elément composite renforcé de fibres pour une pale de rotor, dispositif de fabrication d'un élément composite renforcé de fibres pour une pale de rotor et procédé de fabrication d'un élément composite renforcé de fibres pour une pale de rotor Withdrawn EP2831409A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012204858A DE102012204858A1 (de) 2012-03-27 2012-03-27 Fertigung eines Faserverbundbauteils für ein Rotorblatt
PCT/EP2013/000587 WO2013143641A1 (fr) 2012-03-27 2013-02-28 Elément composite renforcé de fibres pour une pale de rotor, dispositif de fabrication d'un élément composite renforcé de fibres pour une pale de rotor et procédé de fabrication d'un élément composite renforcé de fibres pour une pale de rotor

Publications (1)

Publication Number Publication Date
EP2831409A1 true EP2831409A1 (fr) 2015-02-04

Family

ID=47891577

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13709758.0A Withdrawn EP2831409A1 (fr) 2012-03-27 2013-02-28 Elément composite renforcé de fibres pour une pale de rotor, dispositif de fabrication d'un élément composite renforcé de fibres pour une pale de rotor et procédé de fabrication d'un élément composite renforcé de fibres pour une pale de rotor

Country Status (5)

Country Link
US (1) US20140369849A1 (fr)
EP (1) EP2831409A1 (fr)
CA (1) CA2868654C (fr)
DE (1) DE102012204858A1 (fr)
WO (1) WO2013143641A1 (fr)

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DE202014000999U1 (de) 2014-01-31 2014-04-09 Windnovation Engineering Solutions Gmbh Vorrichtung zur Herstellung von Rotorblattschalen
BR112016024391B1 (pt) * 2014-04-24 2021-07-06 Lm Wp Patent Holding A/S sistema e método para fabricação de pá de turbina eólica
GB2527587A (en) * 2014-06-27 2015-12-30 Vestas Wind Sys As Improvements relating to wind turbine blade manufacture
GB2529186A (en) * 2014-08-12 2016-02-17 Vestas Wind Sys As Improvements relating to wind turbine blade manufacture
DE102014221965A1 (de) * 2014-10-28 2016-04-28 Senvion Gmbh Rotorblatt für eine Windkraftanlage und Verfahren zum Herstellen eines Rotorblatts
CN105269837B (zh) * 2015-10-28 2017-08-29 北京金风科创风电设备有限公司 大梁预制件及其制造方法、叶片及其制造方法
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CN108495999B (zh) 2015-11-26 2020-08-07 维斯塔斯风力系统有限公司 关于风轮机叶片制造的改进
ES2908135T3 (es) 2017-04-05 2022-04-27 Vestas Wind Sys As Mejoras con relación a la fabricación de una pala de aerogenerador
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CA2868654C (fr) 2018-07-31
US20140369849A1 (en) 2014-12-18
WO2013143641A1 (fr) 2013-10-03
CA2868654A1 (fr) 2013-10-03

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