Wind turbine blades

Abstract

A method of making a wind turbine blade comprises stacking a plurality of strips of fibre-reinforced polymeric material one on top of another to form a stack of strips (40); strapping the stack of strips together by means of at least one strap (41) made from a fibrous material, and thereby forming a strapped stack; infusing the strapped stack with resin; and curing the resin to form an elongate spar structure in which the at least one strap (41) is integrated with the stack of strips.

Claims

1. A method of making a wind turbine blade, the method comprising: stacking a plurality of strips of fibre-reinforced polymeric material one on top of another to form a stack of strips; strapping the stack of strips together by means of at least one strap made from a fibrous material by wrapping the at least one strap around a periphery of the stack of strips, and thereby forming a strapped stack; infusing the strapped stack with resin; and curing the resin to form an elongate spar structure in which the at least one strap is integrated with the stack of strips, wherein wrapping the at least one strap comprises fixing a first end of the at least one strap to the stack, wrapping the remainder of the at least one strap around the stack such that a second end of the at least one strap overlaps the first end, and fixing the overlapping first and second ends together.

2. The method of claim 1, further comprising: arranging the strapped stack in a mould and infusing the strapped stack with resin in the mould.

3. The method of claim 2, comprising stacking and strapping the strips outside the mould and transferring the strapped stack into the mould.

4. The method of claim 3, wherein transferring the strapped stack comprises lifting the strapped stack and lowering the strapped stack into the mould.

5. The method of claim 2 wherein the mould is a blade shell mould, and the method comprises arranging the strapped stack in the blade shell mould together with other structural components of the blade, and infusing the strapped stack and the other structural components with resin in the blade shell mould.

6. The method of claim 2 further comprising transferring the cured elongate spar structure from the mould to a blade shell mould and integrating the cured spar structure with other structural components of the blade in the blade shell mould.

7. The method of claim 1, comprising fixing the first end of the strap to the stack by clamping the first end of the strap to the stack using a removable clamp, and comprising removing the removable clamp from the strap after fixing the overlapping first and second ends together.

8. The method of claim 1, comprising bonding the overlapping first and second ends of the strap together by means of an adhesive layer.

9. The method of claim 8, wherein the adhesive layer is a layer of thermoplastic adhesive material.

10. The method of claim 8, wherein the adhesive layer has a web, mesh or grid structure.

11. The method of claim 1, comprising tensioning the strap around the stack of strips.

12. The method of claim 1, comprising arranging a layer of pre-cured material over the stack and arranging one or more fibrous layers over the pre-cured layer before infusing the components with resin.

13. A wind turbine blade made according to the method of claim 1.

14. An elongate spar structure for a wind turbine blade, the spar structure comprising a stack of strips of fibre-reinforced polymeric material strapped together with at least one strap made of a fibrous material, the at least one strap being wrapped around a periphery of the stack of strips, wherein the at least one strap is integrated with the stack by cured resin, and wherein the at least one strap is wrapped around the stack such that first and second ends of the at least one strap overlap.

15. The elongate spar structure of claim 14, wherein the at least one strap is made from a fibrous material having a density between 50 and 500 grams per square metre.

16. The elongate spar structure of claim 14, wherein the at least one strap is made of a glass fibre material.

17. The elongate spar structure of claim 14, wherein a layer of adhesive material is provided between the overlapping first and second ends of the strap.

18. The elongate spar structure of claim 17, wherein the adhesive material is a thermoplastic adhesive material.

19. The elongate spar structure of claim 17, wherein the layer of adhesive material is formed as a web, mesh or grid structure.

20. The elongate spar structure of claim 14, comprising a plurality of straps.

21. A wind turbine blade comprising one or more elongate spar structures according to claim 14.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIGS. 1a to 1c have already been described above by way of background to the invention. In order that embodiments of the invention might be more readily understood, reference will now be made, by way of example only, to the accompanying drawings, in which:

(2) FIG. 2 is a schematic plan view of apparatus for making a wind turbine blade;

(3) FIG. 3 is a perspective view of a stack of strips for an elongate reinforcing structure for a wind turbine blade, strapped together with a plurality of straps according to an embodiment of the invention;

(4) FIG. 4a is a cross-sectional view along the line A-A of FIG. 2;

(5) FIG. 4b is a perspective exploded view of a joint region forming part of the strap of FIGS. 3 and 4a; and

(6) FIGS. 5 to 20 illustrate stages in a method of making an elongate reinforcing structure for a wind turbine blade, according to an embodiment of the invention.

DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

(7) FIG. 2 illustrates a wind turbine blade mould 20 for moulding a wind turbine blade of the type described above by way of introduction to the present invention. More specifically, the blade mould 20 is used for making wind turbine blades comprising spar caps that extend along a longitudinal axis L, and that comprise a plurality of strips 18 of fibre reinforced polymeric material arranged one on top of another in a stack.

(8) An alignment zone, generally indicated at 60, is defined on the factory floor adjacent the mould 20. Pultruded strips 18 made from carbon-fibre reinforced plastic (CFRP) are fed to the alignment zone 60 from a down-stream strip manufacturing station or strip feed station (not shown) in a feed direction F. At the alignment zone 60, the strips 18 are stacked up to form two stacks 40 that will later form spar caps 15a, 15b, 16a, 16b, (see FIG. 1a) and the stacks are aligned relative to one another as they will be aligned in the mould 20.

(9) As seen in FIGS. 2 and 3, the stacks 40 are strapped together with a plurality of straps 41 that keep the strips 18 aligned during handling of the stacks 40, and during subsequent process stages.

(10) Once the stacks 40 have been strapped together, the stacks 40 are lifted from the alignment zone 60, with their relative positions maintained by a support structure (not shown) and then lowered into the mould 20. Other structural components of the blade are then laid in place around the stacks 40. The structural components are covered with a vacuum bag to form a sealed region, air is evacuated from the sealed region, and the sealed region is infused with resin. The resin infuses between the structural components of the blade, including around the stacks 40 and the straps 41. The resin is then cured, forming a blade shell having integrated spar caps 15a, 15b, 16a, 16b, with each spar cap 15a, 15b, 16a, 16b having a plurality of integrated infusible strap 41.

(11) Referring now to FIG. 3, the straps 41 that hold the stacks 40 together are infusible straps. Each strap 41 is made of a lightweight glass fibre cloth or another suitable fibrous material, having a density of approximately 200 grams per square metre (gsm). The fibrous nature of the straps 41 allows resin to infiltrate into the straps 41 during the resin infusion process, as will be described in more detail later. Each strap has a thickness of approximately 0.05 to 0.4 mm, and a width of approximately 50 mm to 150 mm.

(12) The straps 41 fit tightly around the stack 40 such that the straps 41 are under tension. This prevents the strips 18 moving out of alignment with one another during handling of the stack 40, and once the stack 40 is arranged in the blade mould 20. The straps 41 are pulled tightly around the stack 40.

(13) As best seen in FIG. 4a, end portions 44 of the strap 41 overlap one another at an upper surface of the stack 40 and are bonded to one another by an adhesive layer 45 to form a joint 48.

(14) Referring to FIG. 4b, the adhesive layer 45 is a layer of thermoplastic adhesive material formed into an open web structure. The thermoplastic adhesive material adheres the end portions 44 of the strap 41 together, whilst permitting flexibility of the joint 48, so that the strap 41 can be placed under tension without adversely affecting the joint 48. The open web structure allows infusion resin to infiltrate through the joint 48, so that the joint 48 does not interfere with the later infusion process.

(15) The thermoplastic adhesive material is, for example, a copolyester, an aliphatic polyurethane or any other suitable thermoplastic adhesive material. The material is selected so as not to hinder the later infusion process; in particular, an adhesive is selected that does not react chemically with the infusion resin.

(16) A method of making a wind turbine will now be described, with particular reference to FIGS. 5 to 20.

(17) First, a plurality of strips 18 are stacked one on top of another to form a stack 40, as shown in FIG. 5.

(18) Next, the stack 40 is strapped together by wrapping a strap 41 around the stack 40. To wrap the strap 41 sufficiently tightly, a first end portion 44a of the strap 41 is clamped in place against the stack 40 using a flat, removable clamping piece 46 that extends across the strap 41 and clamps 47 arranged either side of the strap 41, as illustrated in FIG. 6. The adhesive layer 45 is arranged over the first end portion 44a as shown in FIG. 7, and the strap 41 is pulled tightly around the stack 40, until the strap 41 is under the required tension. As shown in FIGS. 8 and 9, a second end portion 44b of the strap 41 is pulled over the first end portion 44a of the strap 41, such that the end portions 44 of the strap 41 overlap with the adhesive layer 45 sandwiched between the overlapping end portions 44. Heat is applied to the end portions by a heating iron, so as to activate the thermoplastic adhesive material and bond the end portions 44 of the strap 41 together. The strap 41 is trimmed if required, and the clamps 47 and removable clamping piece 46 are removed leaving the strap 41 in place around the stack 40, as shown in FIG. 10.

(19) Once the first strap 41 has been fitted as described, further straps 41 are fitted to the stack 40 at regular intervals along the stack 40, as shown in FIG. 11.

(20) The stack 40 is then arranged in the alignment zone 60 defined on the factory floor, with other stacks 40, as shown in FIG. 12. The stacks 40 are aligned relative to one another in the alignment zone 60 in a configuration that matches the eventual configuration of the spar caps 15a, 15b, 16a, 16b in the finished blade 10.

(21) The stacks 40 are then supported in this configuration by a support structure 70, as shown in FIG. 13. Once supported, the stacks 40 are transferred to the mould 20 in the sequence shown in FIGS. 13 to 16. The stacks are lifted upwardly in the direction 100, then moved transversely in the direction 200, and finally lowered in the direction 300 to be laid on the mould surface 21 with a pair of stacks 40 arranged on each side of a foam panel 24. The support structure 70 is then removed leaving the stacks 40 in place in the mould 20, as shown in FIG. 17.

(22) During the transfer process, the straps 41 maintain the alignment of the strips 18 in the stacks 40. In this way, little, if any, subsequent adjustment of the strips 18 is required once the stacks 40 have been arranged in the mould 20. The support structure 70 also maintains the alignment of the stacks 40 during transfer, so that there is no need to rearrange the stacks 40 after the transfer process.

(23) Once the stacks 40 have been arranged in place in the mould, other structural components of the blade are laid on top of the stacks 40, as shown in FIGS. 18 to 20. First, as shown in FIG. 19, a layer of pre-cured mesh material 50 is laid directly on top of the stack 40, such that the straps 41 are sandwiched between the stack 40 and the pre-cured mesh 50. Layers of dry glass fibre fabric 52 are then laid over the pre-cured mesh 50, as shown in FIG. 20. The layer of pre-cured mesh 50 is relatively stiff so that it acts as a wrinkle-preventing layer to prevent the straps 41 from creating wrinkles in the layers of glass fibre fabric 52. The structural components are then covered with a vacuum bag to form a sealed region, air is evacuated from the sealed region using a vacuum pump, and resin is introduced to the sealed region, where it infuses between the components.

(24) As the resin infuses between the structural components of the blade, it infuses around the stacks 40 and into the fibrous material of the straps 41. The fibrous material of the straps 41 is of a low density, thereby ensuring that the strap 41 does not interfere with the infusion process. The open structure of the adhesive layer 45 means that resin can also infuse into and through the adhesive layer 45. The inert nature of the thermoplastic adhesive material means that the layer of adhesive material does not react chemically with the resin. In this way, the strap 41 is infused with resin in the same way as the other components of the blade. When the resin is cured, the strap 41 is therefore integrated with the stack 40, by the cured resin such that the strap 41 forms a structural component of the spar cap 15a, 15b, 16a, 16b.

(25) Accordingly, a particular advantage of the present invention is that it is not necessary to remove the straps 41 once the stacks 40 are in place in the mould 20. This removes a step from the manufacturing process, increasing the speed of the process, and reducing the amount of manual labour required. Furthermore, as the straps 41 remain in place during the infusion process, the straps 41 also serve to maintain the alignment of the strips 18 in the stack 40 as the components are infused with resin, and as the resin is cured.

(26) Although in the embodiment described the straps act primarily to hold the strips of the stack together and in alignment with one another, in other embodiments the straps may also be used to lift the stack into position in the mould.

(27) In some embodiments, a single spar cap may be formed from more than one stack of strips. In this case, the stacks that form the spar cap are arranged side-by-side, and are strapped together by a single strap. This arrangement is useful for creating wider spar caps.

(28) In the embodiment described the joint of the strap 41 is arranged on an upper surface of the stack 40. However, in other embodiments, the joint may be arranged on a side of the stack, particularly if the stack includes a large number of strips and is of a relatively large height. In such embodiments, the joint sits next to the foam panel when the stack is arranged in the mould, and hence the joint is shielded by the foam panel. This further mitigates against the joint causing wrinkles in the glass fibre layers of the wind turbine blade.

(29) The present invention is therefore not limited to the exemplary embodiments described above and many other variations or modifications will be apparent to the skilled person without departing from the scope of the present invention as defined in the following claims.