Patent Application
20120269644
This application claims priority of European Patent Office Application No. 11162976.2 EP filed Apr. 19, 2011. All of the applications are incorporated by reference herein in their entirety.
A spoiler for a rotor blade of a wind turbine is provided.
A rotor blade of a wind turbine generally does not have a uniformly flat surface, but is formed in the manner of an airfoil with a gradually changing curvature. Furthermore, a transition must be made between an essentially circular root section (for connecting to a circular opening on the hub of the wind turbine) and the comparatively wide and narrow airfoil section. Because of the relatively abrupt shape change in this ‘shoulder’ region, a higher level of turbulence can arise.
The aerodynamic properties of the rotor blade can be improved by modifying the profile of the rotor blade in the critical shoulder region. Such aerodynamic alterations could involve some kind of ‘extension’ to one side of the rotor blade, for example a spoiler extending from a suction side of the blade, i.e. the leeward-facing side of the blade. This can act to reduce the amount of eddies generated as the rotor blade displaces the air through which it moves, and/or to reduce the amount of noise generated by the rotor blade. However, such modifications to the rotor blade during the manufacturing process are not particularly straightforward, since a rotor blade is generally made from fibreglass composite in a vacuum extraction process, which does not lend itself to forming a thin planar extension of a rotor blade surface. However, the addition of such relatively thin and therefore breakable parts makes the transport of the rotor blades, and their mounting onto the hub, more difficult and therefore also more expensive.
The established alternative is to attach the spoilers to the rotor blades after these have been mounted to the hub. Such spoilers often comprise various differently shaped parts that are shaped to suit the various different curved surfaces of the rotor blade in the shoulder region. However, the design of several differently shaped parts is costly, since the parts must exactly fit the rotor blade surface to ensure smooth air travel over the combined rotor blade/spoiler surface. Furthermore, maintenance procedures are generally made more complicated, since specific replacement parts must be provided for the different regions of the rotor blade.
A more simple and economical spoiler for a wind turbine rotor blade is provided as claimed in the claims. Further, rotor blade and a wind turbine with such a spoiler are also provided as claimed in the claims.
A spoiler for a rotor blade of a wind turbine comprises a spoiler body and at least one mounting band arranged along a longitudinal edge of the spoiler body for mounting the spoiler onto a surface of the rotor blade, which mounting band is realised to adapt to a curvature of the rotor blade surface, in particular along an outer longitudinal edge of the rotor blade, wherein the spoiler body and the mounting band are formed as a single entity.
The spoiler is very simple but effective. By realizing the spoiler as a single, essentially flexible entity with mounting bands or attachment bands that can adapt to variations in the curvature of the rotor blade surface, there is no need to design different spoiler parts for different curved surfaces, as is the case for the known spoiler solutions in the prior art. Furthermore, since the spoiler is effectively one entity, comprising only a single part, it is very easy for a service technician to attach it to a rotor blade. Particularly for the case when a spoiler is to be mounted onto a rotor blade already connected to the hub of a wind turbine, the service technician does not have to carry several different small parts such as fittings or fasteners, and does not have to manipulate such items while being suspended from a rope.
A rotor blade for a wind turbine comprises a spoiler mounted onto a surface of the rotor blade, preferably onto the pressure side of the rotor blade.
A wind turbine—comprising a number of rotor blades attached to a hub—comprises at least one rotor blade with a spoiler mounted onto a surface of the rotor blade, preferably onto the pressure side.
The spoiler may very quickly be mounted onto the rotor blade, even along a part of the rotor blade with pronounced differences in curvature, for example in the shoulder or transition region between the root and the airfoil parts of the blade, since the flexible realisation of the spoiler body and its mounting band(s) allows the spoiler to adapt to any changes in the curvature of the rotor blade along the length of the spoiler. Therefore, instead of having to mount several different types of spoiler, each of which is realised to suit a certain rotor blade surface shape, a single spoiler, or at least a single spoiler type, can be used. This saves design costs as well as mounting costs. In particular, the rotor blades of an already operational wind turbine can easily and cheaply be retro-fitted with spoilers, since only a relatively brief down-time is required for a service technician to mount the spoiler(s).
Embodiments and features are given by the dependent claims, as revealed in the following description. Features described in the context of one claim category can apply equally to another claim category. Features of the different claim categories may be combined as appropriate to arrive at further embodiments.
The spoiler may be attached to the rotor blade using a single mounting band, for example a mounting band that is essentially as wide as the spoiler itself. However, a single mounting band may not be able to sufficiently withstand the forces acting on it over time. Furthermore, a single mounting band may not be able to adapt to marked or pronounced variations in the curvature of the rotor blade surface, particularly in the shoulder region of the blade. Therefore, the spoiler comprises a first mounting band arranged along a first longitudinal edge of the spoiler body and a second mounting band arranged along a second longitudinal edge of the spoiler body. Since the spoiler is realized as a single flexible entity, an arrangement of two mounting bands can favourably adapt to essentially any variation in curvature, even over the shoulder region of the rotor blade.
A mounting band can simply comprise an outer band or strip of the spoiler along its longitudinal length, so that the mounting band is initially in the same plane as the spoiler body. That strip can be physically bent, for example manually, to obtain a desired angle for the spoiler body relative to the rotor blade surface when the spoiler is mounted onto the rotor using the mounting band(s). However, depending on the material used, it may be difficult to physically bend a mounting band such that the desired angle is retained, particularly if the material exhibits a degree of elasticity. Furthermore, bending a material such as a plastic can result in cracks or other stress damage. Therefore, a mounting band comprises a pre-formed angled extension of the spoiler body, which angled extension is such that the angle between the mounting band and the spoiler body corresponds essentially to the desired angle or orientation of the spoiler relative to the rotor blade. For example, if the spoiler is to subtend an angle of about 160° between one of its longitudinal edges and the pressure side of the blade, the mounting band along that edge can, during a manufacturing process, be pre-formed or pre-bent relative to the spoiler body by 160° along a pre-bent angle line. Of course, owing to the flexible nature of the spoiler, the mounting band can still adapt to the rotor blade surface as required, without any stress damage along the pre-bent angle line. For example, a pre-bent mounting band at an angle of 160° could easily adapt to surface curvature so that the mounting band subtends an angle of 130°, 170°, 180°, etc. to the spoiler body.
The mounting bands may be oriented to lie under the spoiler body. However, such an arrangement might make it more difficult to perform the mounting step when the spoiler is to be attached to the rotor blade. Therefore, a mounting band is pre-bent to extend outwardly away from the spoiler. For example, a mounting band is arranged for mounting onto a pressure side of the rotor blade, along an edge of the pressure side along the trailing edge of the rotor blade, in other words along an intersection between the pressure side of the blade and its trailing edge. In another embodiment, a mounting band is arranged for mounting onto a blunt or flat trailing edge of the rotor blade.
The spoiler may be mounted onto the rotor blade in any suitable manner, for example using the traditional types of fasteners such as bolts or screws. However, bolt or screw heads can protrude above the mounting band, and might have a detrimental effect on the aerodynamic properties of the rotor blade. Therefore, a rotor blade comprises an adhesive layer between a mounting band and the rotor blade surface for an adhesive connection to the rotor blade surface. An adhesive can provide robust adherence for a favourably long time. However, heat and cold could compromise the lifetime of the adhesive. Therefore, to protect the adhesive layer, an additional grout seal could be applied along the outer edges of the mounting bands. Of course, the use of an adhesive as a primary attachment means does not exclude the use of a number of fasteners such as screws, bolts, or rivets for an additional threaded and/or riveted connection to the rotor blade surface in regions that do not affect the airflow over the spoiler and rotor blade surface.
The spoiler can effectively comprise a single element, which can be imagined as a single plane bent into a spoiler shape. Such a spoiler is preferably manufactured using any of the techniques of extrusion, casting, injection moulding. Of course, the spoiler can have a more complex form. For example, the spoiler body comprises an aerodynamic element, and a reinforcing element arranged to project outward from the aerodynamic element. The aerodynamic element can simply be a gently curved foil arranged to smoothly extend beyond the rotor blade surface, while a reinforcing element can comprise rigid ‘struts’ that are arranged in an upright manner, for example at right angles, between the aerodynamic element and the rotor blade surface. In such an embodiment, a first mounting band is preferably formed to extend from the aerodynamic element, and a second mounting band is preferably formed to extend from the reinforcing element. The second mounting band, since it is ‘hidden’ from the airflow by the aerodynamic element, can be attached to the rotor blade using fasteners such as a bolts or screws, while the first mounting band is preferably attached to the rotor blade surface by means of adhesive so that an favourably smooth transition between rotor blade surface and spoiler surface can be obtained.
A spoiler could equally well comprise a closed spoiler body, i.e. the spoiler could be hollow, or might comprise a solid body. In such a realization, mounting bands might be formed to extend outward from the spoiler body. Alternatively, the spoiler can comprise a first mounting band and a second mounting band arranged on a common spoiler body surface, which spoiler body surface is disposed toward a rotor blade surface, for example the pressure side of the rotor blade. In such a realization, a cavity may be formed between the rotor blade surface, the sides of the mounting bands, and the underside of the spoiler (i.e. the surface of the spoiler disposed toward the rotor blade surface). However, water, snow or ice crystals may collect in such a cavity, and may cause damage (for example if collected water should freeze and expand) or may detract from the performance of the rotor blade (as a result of the added weight). Therefore, the closed spoiler preferably comprises a number of drainage holes for allowing a fluid to drain from a cavity formed by the spoiler body, the mounting bands, and the rotor blade surface. A drainage hole can simply be an opening at one end of the spoiler, for example at an outer end, so that any collected water can be expelled by the centrifugal force acting on it as the blade rotates. Alternatively, a drainage hole can comprise a gap intentionally formed along a mounting band.
For optimal aerodynamic properties, a rotor blade surface should be as smooth as possible. Therefore, mounting bands that are attached to the surface of the rotor blade are preferably thin, and an adhesive layer is also preferably thin. However, such a thin mounting band might not be particularly robust. Therefore, a rotor blade comprises a recess at least along a length of the rotor blade surface upon which a spoiler is to be mounted, which recess is realised to at least partially accommodate a mounting band. For example, a recess can comprise a flat groove, perhaps a few millimetres deep, so that an adhesive layer can be spread over the ‘floor’ of the recess and so that a mounting band can be pressed into the recess. Preferably, a mounting band is contained in the recess such that an outer surface of the mounting band is flush with the rotor blade surface. To this end, the depth of the recess is chosen to accommodate a certain adhesive layer thickness and a certain mounting band thickness.
Other objects and features will become apparent from the following detailed descriptions considered in conjunction with the accompanying drawings. It is to be understood, however, that the drawings are designed solely for the purposes of illustration and not as a definition of the limits of the invention.
In the drawings, like reference numbers refer to like objects throughout. Objects in the diagrams are not necessarily drawn to scale.
It will be understood that numerous additional modifications and variations may be made to the spoiler, rotor blade and wind turbine without departing from the scope of the disclosed spoiler, rotor blade and wind turbine.
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.
| Number | Date | Country | Kind |
|---|---|---|---|
| EP11162976 | Apr 2011 | EP | regional |
