COMPOSITE MATERIAL, A WIND TURBINE BLADE, A WIND TURBINE AND A METHOD FOR PRODUCING A COMPOSITE MATERIAL

Abstract

Provided is a composite material for a wind turbine blade, the composite material including a plurality of rigid elements and plurality of flexible elements, wherein each flexible element is arranged between two rigid elements and is connected thereto such that the rigid elements are flexibly connected to each other by the flexible elements. The flexibility of the composite material can be achieved by using the interspaces between the rigid elements. Therefore, when the composite material is placed on a curved surface, hollow spaces between the rigid elements may be reduced or avoided.

Claims

1. A composite material for a wind turbine blade, the composite material comprising a plurality of rigid elements and a plurality of flexible elements, wherein each flexible element is arranged between two of the plurality of rigid elements and is connected thereto such that the rigid elements are flexibly connected to each other by the flexible elements.

2. The composite material according to claim 1, wherein the composite material forms at least one of a flat and adaptable material configured to adapt to a curved surface when being mounted.

3. The composite material according to claim 1, wherein the flexible elements fill gaps between the rigid elements completely such that a surface formed by the rigid elements and the flexible elements is even.

4. The composite material according to claim 1, wherein the rigid elements and the flexible elements are bar-shaped.

5. The composite material according to claim 1, wherein the rigid elements are made of balsa wood or rigid cellular foam.

6. The composite material according to claim 1, wherein each rigid element has a rectangular cross-sectional shape being constant along a longitudinal axis of the rigid element.

7. The composite material according to claim 1, wherein the flexible elements are plastically or elastically deformable.

8. The composite material according to claim 1, wherein the flexible elements are connected to the rigid elements by an adhesive or hot plate welding.

9. The composite material according to claim 1, wherein the rigid elements have a first elasticity module and the flexible elements have a second elasticity module, and wherein the first elasticity module is greater than the second elasticity module.

10. The composite material according to claim 1, wherein between 3 and 20, 4 and 15, or 4 and 10, rigid elements are connected to form a single module which can be handled as one piece.

11. The composite material according to claim 1, wherein the flexible elements comprise plastic material, wherein the plastic material is one of a thermoplastic material, elastomeric material and thermosetting material.

12. The composite material according to claim 1, wherein the flexible elements comprise a highly closed cell material.

13. A wind turbine blade for a wind turbine comprising a composite material according to claim 1.

14. A wind turbine comprising at least one of a composite material according to claim 1 and a wind turbine blade.

15. A method for producing a composite material for a wind turbine blade, the method comprising the steps of: a) providing a plurality of rigid elements, b) providing a plurality of flexible elements, c) arranging each flexible element between two rigid elements, and d) connecting each flexible element to two rigid elements such that the rigid elements are flexibly connected to each other by the flexible elements.

Description

BRIEF DESCRIPTION

[0038] Some of the embodiments will be described in detail, with references to the following Figure, wherein like designations denote like members, wherein:

[0039] FIG. 1 is a perspective view of a wind turbine according to one embodiment;

[0040] FIG. 2 is a perspective view of a wind turbine blade according to one embodiment;

[0041] FIG. 3 shows a perspective view of a composite material according to one embodiment;

[0042] FIG. 4 shows a side view of the composite material according to a further embodiment;

[0043] FIG. 5 shows a side view of the composite material according to a further embodiment;

[0044] FIG. 6 shows a detail view VI from FIG. 5; and

[0045] FIG. 7 shows a block diagram of an embodiment of a method for producing the composite material according to FIG. 3.

DETAILED DESCRIPTION

[0046] FIG. 1 shows a wind turbine 1 according to one embodiment.

[0047] The wind turbine 1 comprises a rotor 2 connected to a generator (not shown) arranged inside a nacelle 3. The nacelle 3 is arranged at the upper end of a tower 4 of the wind turbine 1.

[0048] The rotor 2 comprises three wind turbine blades 5. The wind turbine blades 5 are connected to a hub 6 of the wind turbine 1. Rotors 2 of this kind may have diameters ranging from, for example, 30 to 160 meters or even more. The wind turbine blades 5 are subjected to high wind loads. At the same time, the wind turbine blades 5 need to be lightweight. For these reasons, wind turbine blades 5 in modern wind turbines 1 are manufactured from fiber-reinforced composite materials. Therein, glass fibers are generally preferred over carbon fibers for cost reasons. Oftentimes, glass fibers in the form of unidirectional fiber mats are used.

[0049] FIG. 2 shows a wind turbine blade 5 according to one embodiment.

[0050] The wind turbine blade 5 comprises an aerodynamically designed portion 7, which is shaped for optimum exploitation of the wind energy and a blade root 8 for connecting the rotor blade 5 to the hub 6. Further, a composite material 9 (schematically shown) is provided which reinforces a blade shell 10 of the wind turbine blade 5.

[0051] FIG. 3 shows a perspective view of the composite material 9 according to one embodiment.

[0052] The composite material 9 comprises a plurality of rigid elements 11 and plurality of flexible elements 12, wherein each flexible element 12 is arranged between two rigid elements 11 and is connected thereto such that the rigid elements 12 are flexibly connected to each other by means of the flexible elements 12.

[0053] The rigid elements 11 have an elasticity module E1 (also referred as first elasticity module) and the flexible elements 12 have an elasticity module E2 (also referred as second elasticity module), wherein the elasticity module E1 is greater than the elasticity module E2. The elasticity module E1 is at least 1.5, 2, 3 or 4 times greater than the elasticity module E2. Thus, the rigid elements 11 are significantly stiffer than the flexible elements 12.

[0054] The flexible elements 12 are merely indirectly connected to each other by means of the rigid elements 11. Therefore, the flexible elements 12 are not attached to each other when the composite material 9 is evenly spread out, i.e. is not bended, as shown in FIG. 3. The rigid elements 11 and the flexible element 12 are made of different materials. In particular, all rigid elements 11 are provided identical. For example, also all flexible elements 12 are provided identical. Each flexible element 12 is connected to a side face 13 of one rigid element 11 and to a further side face 14 of a further rigid element 11. The side face 13 and the further side face 14 face each other. A gap G is provided between the side face 13 and side face 14.

[0055] The flexible elements 12 fill all gaps G between the rigid elements 11 completely such that a surface 15 formed by the rigid elements 11 and the flexible elements 12 is even. Completely means up to a complete height H of the rigid elements 11. Therefore, the flexible elements 12 are provided as filling material between the rigid elements 11.

[0056] This has the advantage that after mounting the composite material 9 undesirable hollow spaces in the composite material 9 may be avoided (see also FIG. 4). Thus, additional filling material, in particular blade resin, may be avoided in the gaps G. It is noted that resin in the gaps G can lead to a weak structure since resin, for example, has a lower rigidity than the flexible material 12.

[0057] The rigid elements 12 and the flexible elements 11 are bar-shaped. This means that a length L of the rigid elements 11 is several times, in particular at least 10 times, larger than the height H and/or a width W of the rigid elements 11. Therefore, the composite material 9 is flexible in one bending direction V, i.e. around a longitudinal axis A of the rigid elements 11.

[0058] The rigid elements 11 are made of balsa wood. In particular, the composite material 9in this caseis a flexible wood panel. Alternatively, the rigid elements 11 are made of rigid cellular foam. For example, the rigid cellular foam may comprise or is made of a metal, in particular aluminum, and/or a plastic material.

[0059] Each rigid element 11 has a rectangular cross-sectional shape, in particular being constant along the longitudinal axis A of the rigid elements 11. Thus, the rigid element 11 may be simply produced, in particular by means of cutting and/or sawing. The flexible elements 12 have also a rectangular cross-sectional shape when the composite material 9 is evenly spread out and/or the flexible elements 12 are not deformed.

[0060] In particular, the flexible elements 12 comprise a highly closed cell material. The highly closed cell material comprises a metal or metal foam, in particular an aluminum foam. Additionally, or alternatively, the flexible elements 12 may comprise plastic material, in particular thermoplastic material, elastomeric material and/or thermosetting material.

[0061] The composite material 9 is provided as a module 16. This means that the rigid elements 11 are connected to one module 16 which is separately manageable as one composite component. Thus, modules 16 may be provided which are manageable by hand force of an assembly worker. The module 16 comprises 6 rigid elements 11 and 5 flexible elements 12. However, these numbers can vary depending on the application.

[0062] The module 16 comprises between 3 and 20, 4 and 15, or 4 and 10, in particular 6 rigid elements 11. The module 16 is produced by means of cutting through two flexible elements 12. The rigid elements 11 and the flexible elements 11 alternate in a direction B which runs perpendicular to axis A.

[0063] FIG. 4 shows a side view of the composite material 9 according to a further embodiment.

[0064] The composite material 9 forms a flat and adaptable material which rests on and is adapted in shape to a curved surface 17 of the blade shell 10. In this state the composite material 9 reinforces the blade shell 10. As shown in FIG. 4 the flexible elements 12 are deformed such that the rigid elements can be adapted to the curved surface 17. The rigid elements 11 are not deformed. Thus, the composite material 9 can be adapted to the curved surface 15 without breaking. The composite material 9 may be in surface contact with surface 17 across its entire surface 15 (or surface 23 in another embodiment, not shown). For example, the composite material 9 may be bonded to the surface 17 using an adhesive.

[0065] The flexible elements 12 are plastically or elastically deformable. In particular, the flexible elements 12 have a greater ductility than the rigid element 11. The ductility of the flexible elements is chosen such that, for example, contourability is induced to the composite material merely by gravity or by forcing it manually into the geometry of the curved surface 17 such that the composite material 9 stays in this shape due to plastic deformation.

[0066] As shown in FIG. 4, the composite material 9 is bended around the direction V. The advantage of such flexible elements 12 is that hollow spaces between the rigid elements 11 are avoided. This is in particular relevant when thick (i.e. height H is increased) rigid elements 11 are used.

[0067] FIG. 5 shows a side view of the composite material 9 before being provided as a mountable module 16, as shown in FIG. 3.

[0068] The composite material 9 is provided as semi-finished block 18. By contrast to module 16, the block 18 has the height H1 which is several times, in particular at least 3, 5, 7 or 10 times, larger than the height H. Each rigid element 21 and/or flexible element 22 has the height H1.

[0069] By cutting the block 18 into portions having the height H, several modules 16 can be produced. The block 18 is produced by means of cutting through two flexible elements 22.

[0070] FIG. 6 shows a detail view VI from FIG. 5.

[0071] The flexible elements 22, for example, are connected to the rigid elements 21 by means of an adhesive, in particular an adhesive layer 19, arranged between the face 13 and the flexible element 22 and an adhesive, in particular adhesive layer 20, arranged between the face 14 and the flexible element 22.

[0072] Alternatively, the rigid elements 21 may be connected to the flexible element 22 by means of hot plate welding. In this case the layers 19, 20 may be provided as melted and then solidified zones.

[0073] Thus, sufficient strength of the composite material 9 may be achieved. Therefore, detaching of the rigid elements 11 from the flexible element 12 may be avoided.

[0074] FIG. 7 shows a block diagram of an embodiment of a method for producing the composite material 9 according to FIG. 3 or the wind turbine blade 5 according to FIG. 2.

[0075] In a first step S1 a plurality of rigid elements 21 each having the height H1, the width W and the length L are provided. The rigid elements 21 may be provided from balsa wood, in particular by sawing. Alternatively, the rigid elements 21 are provided from rigid cellular foam.

[0076] Further, in a step S2 a plurality of flexible elements 22 having the height H1 and the length L are provided.

[0077] In a step S3 each flexible element 22 is arranged between two rigid elements 21.

[0078] In a step S4 each flexible element 22 is connected to two rigid elements 21 such that the rigid elements 21 are flexibly connected to each other by means of the flexible elements 22. This connection step S4 can be done by means of gluing or hot plate welding. In particular, the steps S3 and S4 are executed as one step. At this stage the composite material 9 is created.

[0079] In a step S5 the composite material 9 can be cut such that a block 18 having the width W1 (see FIG. 6) is provided. Alternatively, steps S3, S4 are executed such that the block 18 having the width W1 is created immediately after the steps S3 and S4. In a step S6 the block 18 is cut into modules 16 having the height H. In a step S7 the module 16 is connected to the surface 17 of the blade shell 10 for producing the wind turbine blade 5.

[0080] Although the present invention has been disclosed in the form of preferred embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention

[0081] For the sake of clarity, it is to be understood that the use of a or an throughout this application does not exclude a plurality, and comprising does not exclude other steps or elements.