SYSTEM FOR PROTECTION AGAINST LIGHTNING STRIKES FOR A MODULAR BLADE AND METHOD OF FORMING A STACK

Abstract

A lightning protection system for the joint of a modular blade. The joint comprises a number of coated metal elements by Xpacer equipotentially bonded with a number of stacks disposed at the sides of the upper cap and the lower cap and with the lightning down-drop. The preforms of the joint include two stacks at the leading edge and another two stacks at the trailing edge. The stacks are formed by layers of carbon fibre and layers of glass fibre, replaced by copper mesh as from the equipotentiation line. The stack incorporates at the side thereof a metal strip joined to the metal strip that links the tip cap and the root cap, and is coated with a layer of glass fibre.

Claims

1-9. (canceled)

10. A system for protection against lightning strikes for a modular blade, wherein the metal elements of the joint are arranged at the upper cap and the lower cap and together with the webs of the beam and the metal plate that joins them, they constitute a preform that is integrated with the blade beam, the metal joining elements comprising a number of Xpacers that prestress a number of bolts screwed into inserts that are drilled and a combination of carbon layers with glass layers are glued inside the composite material, comprising: a stack of the leading edge and a stack of the trailing edge arranged on the sides of the upper cap and two other stacks arranged on the sides of the lower cap, a metal strip protruding from each stack and joining with: the plate that joins the web, a metal strip that joins the Xpacers, the lightning cable and with the metal strip that joins the tip cap and the root cap, each stack consisting of layers of carbon fibre and layers of glass fibre replaced by a copper mesh from the equipotential bonding line, protruding the meshes of copper from the side wall of the stack, folding on themselves and constituting a surface where the metal strip is attached and each stack is completed with a glass fibre layer that completely covers it.

11. The system for protection against lightning strikes for a modular blade according to claim 10, wherein the layer of the joint is formed by a 20-80 ratio of glass fibre and carbon fibre and from the equipotential bonding point is formed by a copper mesh and carbon fibre in the same proportion.

12. The system for protection against lightning strikes for a modular blade according to claim 10, wherein the configuration of the joint includes a centring pin and the arrangement of the stacks fixed on the sides of the caps a distance equal to the size of the centring pin is delayed and moved away from the joining area and the metal band is lengthened until it covers said distance.

13. The system for protection against lightning strikes for a modular blade according to claim 10, wherein by not using a centring pin, the stack has a length of 200 to 250 mm and a width of 50 to 80 mm, measured from the joint area.

14. The system for protection against lightning strikes for a modular blade according to claim 10, wherein the Xpacers forming the joint of the tip caps and the root caps are joined together with a metal strip that is arranged on the upper part and/or on the lower part of the mentioned Xpacer and also joins with the joining plate of the webs.

15. A method of forming a stack comprising: the existing layers are stacks of carbon fibre and glass fibre and from the equipotential bonding line, the glass fibres are replaced by a copper mesh that extends beyond the end of the stack and with protruding ends, the lower copper mesh being longer than the rest of the meshes, the protruding ends of the copper meshes are folded towards the top of the stack forming a wall on the side of the stack, on said side wall the metal strip is arranged, once the metal strip is arranged, the lower copper mesh is folded, which overlaps the metal strips and ends at the top of the stack, a lower glass fibre layer and an upper glass fibre layer cover the carbon fibre and the copper mesh folds of the stack, and eventually, the assembly is infused.

16. The method of forming a stack according to claim 15, wherein during the folding of the copper meshes it starts with the upper one and continues with the immediately lower one so that the second copper mesh covers up to half of the first.

17. The method of forming a stack according to claim 15, wherein the lower glass fibre layer is longer and protrudes from the side wall of the stack, while the last upper glass fibre layer is the one that overlaps the previous one, covering the carbon fibre and the copper mesh folds of the stack, leaving the whole assembly covered by glass fibre, which favours its subsequent infusion.

18. The method of forming a stack according to claim 15, wherein once it has been infused and the joint has been completed, on the side wall formed by the overlapping of the copper meshes a metal strip is arranged which is ended with a hole that is screwed to the metal strip that joins the stack tip and the stack root, and is screwed to the metal strip of the Xpacers and the lightning down-drop.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] A brief description will be given below for a series of drawings useful for better understanding the invention and that expressly relate to an embodiment of said invention that is presented as a non-limiting example thereof.

[0026] FIG. 1 represents the outline of a modular blade with the two joining preforms overlapping inside it.

[0027] FIG. 2a represents a part of the lower cap of the preform of FIG. 1, with the arrangement of the equipotentially bonding of the stack.

[0028] FIG. 2b shows a second embodiment where the stacking arrangement is behind blocks used by centring pins.

[0029] FIG. 3 shows a detail of the joint of a modular blade.

[0030] FIG. 4 shows a detail of FIG. 2b with all the electrical connections of the lightning protection system.

[0031] FIG. 5a is a profile section of the blade showing the upper and lower cap.

[0032] FIG. 5b shows the connection of the metal joint with the web from the trailing edge.

[0033] FIG. 5c shows the connection of the metal joint with the web through the leading edge.

[0034] FIG. 6 shows a detail of the cap with the holes where the joining elements and the centring pins are inserted.

[0035] FIG. 7a shows a step of the method for equipotentially bond a stack of composite material.

[0036] FIG. 7b shows a step of the method for equipotentially bond a stack of composite material.

[0037] FIG. 7c shows a step of the method for equipotentially bond a stack of composite material.

[0038] FIG. 7d shows a step of the method for equipotentially bond a stack of composite material.

[0039] FIG. 7e shows a step of the method for equipotentially bond a stack of composite material.

DETAILED DESCRIPTION

[0040] The blade of a wind turbine has a tip and a root. If, in addition, the blade is modular, like the one shown in FIG. 1, two parts are configured from the joint area (1), the tip area (2) from the joint to the tip and the root area (3) from the joint to the root. The blade has an internal structure consisting of two caps and two webs consisting of composite material that form an internal beam on which the upper and lower shells are arranged. The metal elements conforming the joint of this modular blade are arranged in the upper cap (4) and in the lower cap (5). Said caps (4 and 5) and their corresponding webs, together with the joining area (1), constitute two preforms, one upper and one lower, which overlap on the original beam structure of the blade. So that, as they move away from the junction point (1), the cap narrows and thins its thickness so that the overlap with the rest of the interior of the blade is more effective.

[0041] The material used in the cap is glass fibre and carbon fibre in a ratio of 20% to 80%.

[0042] FIG. 2a shows the joining area (1) of the lower cap (5) with its tip side (2) and its root side (3). Said metal joint rests on the lower shell of the blade and due to its aerodynamic configuration, the preform of the joint is closer to the leading edge (7) and further from the trailing edge (8). On both sides of the lower cap (5) is where the stack (9) is arranged, equipotentially bonding the composite material that houses the metal elements of the joint. The lightning protection system of the lower cap (5) shown in FIGS. 2a and 2b, has two stacks (9) on the leading edge (7) and another two stacks (9) on the trailing edge (8).

[0043] In a second practical embodiment shown in FIG. 2b, the sides of the lower cap (5) house some centring pins (10) that help to complete the in-situ assembly of the modular blade and that are subsequently removed. In the event that the joint (1) has these pins (10), the stack (9) moves towards the interior of the tip zone (2) and the root zone (3) respectively, but maintains its dimensions in both cases.

[0044] The stack (9) is approximately 150 mm or 250 mm long and 50 mm or 80 mm wide.

[0045] Measured from the joint area (1) and more specifically from the last metal element that makes up the joint.

[0046] FIG. 3 shows a section of the modular blade object of the invention. It includes the tip area (2), the root area (3), the leading edge (7), the trailing edge (8) and the joint area (1) covered by the metal elements that constitute the joint itself: The set of Xpacers® that cover and prestress the union bolts, which in turn are threaded in their corresponding inserts, which are glued to the laminated combination of carbon fibre and glass fibre that must be equipotentially bonded. The Xpacers are the metal elements visible when the joint is completed. The shells that cover the blade have holes (11) in the joint area (1) to allow access during assembly. Subsequently, these holes (11) will be covered with a hull.

[0047] As shown in the practical embodiment of FIG. 4, the stacks (9) fitted with the trailing edge (8) comprise a metal strip (12) that protrudes from its interior. Said strip (12) has a hole for its connection with other elements. The stack (9) of the tip (2) and the stack (9) of the root (3) corresponding to the lower cap (5) are joined together with another metal strip (13) screwed through the corresponding connection holes of the metal strip (12) mentioned above. This union is complemented by the metal strip (14) that covers all of the Xpacers (15). Said metal strip (14) is screwed to each and every one of the Xpacers (15) contained in the joining area (1). Finally, the union (16) that joins the metal strips (12) of the stacks (9) corresponding to the tip zone (2) and the root zone (3) together with the metal strip (14) of the Xpacer (15) also serves as a link with the lightning down-drop (17), where the entire assembly is equipotentially bonded. This joint (16), together with the rest of the joints, is preferably a screwed joint.

[0048] As shown in FIGS. 5a, 5b and 5c, the cap is responsible for housing the elements of the metal joint. The Xpacers (15) have an upper and a lower surface. In these surfaces is where the corresponding metal strips (14) are screwed, both on its upper part and on its lower part.

[0049] The upper cap (4) is fitted with a metal plate that joins the webs (18) of the trailing edge (8) through a tape that is screwed to the metal strip (14) of the Xpacer (15). The lower cap (5) is fitted with the metal sheet that joins the webs (18) of the leading edge (7) through its connection with another tape that is screwed to its corresponding metal strip (14) of the Xpacers (15). Arranging the metal strips (14) at the top and/or at the bottom of the Xpacers (15) and connecting them with the plate that joins the webs (18) of the leading edge (7) or the trailing edge (8) are design solutions based on the length of the blade and the number of Xpacers (15) that make up the joint.

[0050] FIG. 6 represents the configuration of a cap and shows how its different layers are. The line (19) marks where the layer changes from the front part (19′) to the back part (19″). The front part (19′) are layers of constant thickness and are made up of carbon fibre and glass fibre in a ratio of approximately 80-20. This is the place where the cavities are drilled where the inserts are subsequently inserted and glued. The joint is completed by screwing the bolts inside the inserts and facing the assembly to the counterpart cap. By unscrewing the bolts of the first cap they are inserted into the counterpart. Finally, they are covered with the Xpacers and prestressed. The back part (19″) are layers that narrow and lose thickness to facilitate the overlap of the preform with the rest of the blade cap.

[0051] Two practical embodiments with a centring pin (10) and without a centring pin (10) have been described in FIGS. 2a and 2b. In the present FIG. 6, a hole (20) for the centring pin is shown on both sides of the cap. This forces the equipotential stacking (9) to be delayed and the metal strip (12) to extend from the stacking (9) to the apex of the joining zone (1). Said metal strip (12) may be shorter in the event that there is no centring pin (10).

[0052] FIGS. 7a, 7b, 7c, 7d and 7e describe the method of forming the stack (9) of equipotentially bonded layers. For reference purposes, the hole closest to the stack (9) is represented, for this practical embodiment it is the cavity of an insert, which is longer than the cavity of the centring pin. The existing layers from the hole are stacks of carbon fibre (21) and glass fibre (22) and this combination is repeated until achieving an equipotentially bonded line (23). From said line, the glass fibres (22) are replaced by a copper mesh (24) that extends beyond the end of the stack (9) leaving its protruding ends. The lower copper mesh (25) is longer than the rest of the meshes (24).

[0053] As shown in FIG. 7b, the copper meshes (24) are folded towards the top of the stack (9), starting at the top and continuing at the bottom. The protruding ends of the copper meshes (24) overlap a smaller portion than the stack formed by a set of carbon fibres (21) with its corresponding glass fibre (22). The second copper mesh covers up to half of the first.

[0054] By overlapping the copper meshes (24) a wall is formed on the side of the stack (9). On said surface, the metal strip (12) is arranged, ending in a hole (26) to be able to be screwed to the metal strip (13) that joins the stack (9) of the tip (2) and the stack (9) of the root (3) indicated in FIG. 4, where the equipotential bonding line (23) is also shown. Once the metal strip (12) is arranged, the lower copper mesh (25) is folded which, thanks to its greater length, overlaps the metal strip (12) and ends at the top of the stack (9), as can be seen in FIGS. 6c and 6d.

[0055] The stack (9) depicted in all FIGS. 7a, 7b, 7c, 7d and 7e has a longer lower glass fibre layer (27), protruding from the side wall of the stack (9). Once the lower glass fibre (27) is folded, its final end is covered with the last upper glass fibre layer (28) that covers the carbon fibre (21) and the copper mesh folds (24) of the stack (9). This completes the final overlap of the two glass fibre layers (27 and 28), which favours the infusion of the whole. This cover can also be made up of a single layer.

[0056] Once the stacks (9) have been infused and the union of the modular blade has been completed, we proceed with the equipotential bonding, by screwing the metal strips (12, 13 and 14) together and with the line of the lightning down-drop (17).