Patent Application
20170234295
The present invention falls within the technical field of wind turbines. More specifically, it disclosed a wind turbine blade having an enhanced bond between the spar and inner surface of the blade.
In general, wind turbine blades have a pressure surface and a suction surface consisting of laminated composite material joined therebetween and which confer the aerodynamic geometry to the blade. The connection of the pressure and suction surfaces is performed joining their ends and by means of spars disposed in the cavity formed by said pressure and suction surfaces. The spars stiffen the pressure and suction surfaces to avoid bending of the laminates that form them. The connection between the spars and pressure and suction surfaces can be executed in various manners, but the most common is bonding by means of adhesive.
In some cases, the blades are formed by a continuous surface, there not existing a bond defined between the pressure and suction surfaces. Also in these cases, the spars stiffen said pressure and suction surfaces and the bond between those and these is usually executed by means of adhesive.
The conventional geometry of the spars is I- or C-shaped, although spars having L- or T-shaped and even X- or K-shaped geometries are also known. The selection of one type of geometry or another depends on the structural requirements in terms of capacity to transmit the shear stress experienced by the blade due to aerodynamic loads and other solicitations arising during wind turbine operation. This shear stress is transmitted from the spars to the pressure and suction surfaces through the bond thereof which, as described previously, is usually an adhesive bond.
The spars comprise:
Usually, the central zone of the spar is disposed substantially transversely or obliquely to the blade pressure and suction surfaces. The spar bonding zones allow adhesive bonding to the blade pressure and suction surfaces and comprise at least one bonding surface substantially parallel to said blade pressure and suction surfaces.
In this manner, each fibre fabric layer of the core forms a shear stress transmission layer such that the spar usually comprises two layers. As the shear stress must be absorbed by the fibre fabric layers, the distribution of shear stress in the adhesive is not even, generating two shear stress tension peaks corresponding to each of the fibre fabric layers.
This makes it necessary, when using spars having a C-shaped geometry, to increase the width of the bond for the purpose of reducing the tension borne by the adhesive. However, this increase in width implies an increased in the use of adhesive material.
The present invention describes a wind turbine blade having at least one spar configured to enhance the adhesive bonding thereof to the inner surface of the longitudinal hollow element of the blade. The spar makes it possible, due to a more homogeneous distribution of shear stress in said bond, to reduce the width of said adhesive bond and enhance the transfer of shear stress between the inner surface of the longitudinal hollow element and the spar itself. This in turn makes it possible to use less adhesive material.
Therefore, the blade of the present invention makes it possible to even out the distribution of shear stress in the adhesive bonding zone between the inner surface of the longitudinal hollow element and the spar, minimising in turn the peak values of said stress.
The proposed blade comprises at least one longitudinal hollow element that defines an aerodynamic outer surface with a pressure zone and a suction zone, and an inner cavity having an inner surface which, in turn, has a zone corresponding to the pressure zone and a zone corresponding to the suction zone. And the blade comprises at least one spar disposed in the inner cavity and joined to the inner surface by at least two bonding surfaces disposed in the spar bonding zones.
In order to achieve the described objectives, the spar of the blade of the present invention comprises, in the spar bonding zones, which are preferably joined to the inner surface by means of an adhesive bond, a larger number of fibre fabric layers than the spars of the state of the art (it comprises at least three layers compared to two layers in the spars of the state of the art), separated therebetween by cores.
The fibre fabric layers which form the spar stress transmission layers that transmit stress to the inner surface of the longitudinal hollow element are disposed parallel therebetween and transversely or obliquely with respect to the inner surfaces in the blade suction and pressure zones.
Although a larger number of fibre fabric layers and cores increases the number of shear tension peaks in the adhesive bond, the maximum values of these peaks are lower than with a smaller number of layers.
In this manner, enhanced transfer of the shear stress between the inner surface and the spars is achieved and the maximum shear stress magnitude in the bond is reduced with respect to the state of the art. The amount of fibre fabric used, which has a higher cost and density than the cores, is also optimised, and the width of the adhesive bond required to adequately transmit the stress is reduced.
In the blade described, the spar has, in the adhesive bonding zone, at least three fibre fabric layers and a group of cores having at least two cores. The layout of the fibre layers with respect to the cores may depend on the loads of the blade in accordance with the type of wind to be supported, where it is installed, etc. This spar configuration allows a more even distribution of the stress in the adhesive bond between the spar and the inner surface of the longitudinal hollow element of the blade.
Specifically, the at least one spar of the blade described comprises, in the adhesive bonding zone, a number of fibre fabric layers (i.e. shear stress transmission layers) equal to or greater than three. Said at least three layers are separated by at least two cores in the bonding zone of the spar to the blade pressure and suction surfaces.
With respect to another type of spars known in the state of the art, in the bonding zone each of the cores of the present invention is disposed between at least two fibre fabric layers.
As already described, this configuration makes it possible to reduce the maximum shear stress magnitude in the bond between the spars and the blade pressure and suction surfaces. This also results in a reduction in the width of the spar in the bonding zone (the bonding surface of the spar is reduced), making it possible to save a large amount of adhesive and avoid the use of additional bonding and reinforcement elements external to the spar itself.
Therefore, each spar comprises a central core and at least one lateral core. The geometry of the lateral cores is such that, in the bonding zone, all the fibre fabric layers (i.e. all the stress transmission layers) are substantially parallel.
The at least one lateral core comprises an adjacent side, at least one side divergent with respect to, at least, one lateral side of the central core according to an angle of divergence.
The angle of divergence between the lateral surface of the lateral core and the lateral surface of the central core is less than or equal to 60°, preferably less than or equal to 30°. In a preferred embodiment, said angle of divergence remains constant throughout the spar.
The at least one lateral core also comprises a lateral surface parallel to the lateral side of the central core and adjacent to the divergent side of the lateral core that extends between the divergent side and the bonding zone.
In one embodiment, the spar has four layers such as to comprise a central core and two lateral cores on each side of the spar bonding zone. In said bonding zone, each layer is separated from the adjacent layer by at least one core.
In one embodiment, the height of the spars varies from the zone next to the blade root, where they are higher, to the zone nearest the blade tip, where they are lower.
In one embodiment, the height of the lateral surface parallel to the lateral core in the zone opposite the central core is constant throughout the blade.
The height of the lateral cores is less than the height of the central core, in at least one zone of the spar, said zone being disposed near the blade root.
In one embodiment, the thickness of the central core is greater than the thickness of the lateral cores.
The thickness of the central core decreases throughout the length of the spar from the zone near the blade root towards the zone nearest the blade tip, where it is less thick. Likewise, the height of the spars varies from the zone near the blade root, where they are higher, to the zone nearest the blade tip, where they have thinner aerodynamic profiles and, therefore, the spars are lower in height.
Also, the thickness of the lateral cores increases throughout the length of the spar, from the zone near the blade root towards the zone nearest the blade tip.
In addition, according to this embodiment, the thickness of the central core and of the lateral cores is such that the total length of the spar, which is the sum of the thicknesses of the central core and of the lateral cores, is constant throughout the entire length of the spar. This facilitates the blade manufacturing process and increases reliability, as it allows the distance between the adhesive lines of the adhesive bond to be constant throughout the entire length of the blade.
Each fibre fabric layer may be formed by one or more layers of fibre fabric, said fibre fabrics having different surface fibre content densities.
In one embodiment, the spar is composed of a central zone and two bonding zones comprising four layers disposed parallel therebetween and obliquely with respect to the inner blade surface. Each of the layers is separated from the adjacent layer in said bonding zone by at least one core (made of PVC in one embodiment). Specifically, the central layers are separated therebetween by a central core and each layer is separated from the respective outer layers by a lateral core.
According to a particular embodiment wherein the number of layers is four, with two lateral layers and two central layers, the central layers comprise a greater number of fibre fabric layers than the lateral layers. In a preferred embodiment, in turn, the surface density of the fibre content in said fabric layers. According to one embodiment, the central layers comprise three fibre fabric layers of a density 50% greater than the fabric layers of the lateral layers.
In one embodiment, the height of the lateral layers in at least one spar zone is substantially equal to the height of the central core.
In a preferred embodiment, the blade has two spars, a main spar disposed near a zone of the leading edge and a spar disposed near the zone of the trailing edge of the blade and, therefore, generally lower in height than the main spar.
In order to complement the description being made and with the aim of helping to better understand the characteristics of the invention, in accordance with a preferred embodiment thereof, said description is accompanied, as an integral part thereof, by a set of drawings where, in an illustrative and non-limiting manner, the following has been represented:
Following is a description, with the help of
The central core (4) of the spar (1) and the two fibre fabric layers (3) comprised by said spar (1) have been represented in said figure. As can be observed in the figure, the fibre fabric layers (3) are disposed covering the two lateral sides of the central core (4) and also compose the bonding zone (2) of the spar (1) that bonds with the inner side of the blade pressure and suction surfaces. As can be observed in the figure, the bonding zones (2) of the spar (1) are formed by a single central core (4) and by the two fibre fabric layers (3). The thickness (E) of the central core (4) and a first width (A), which is the width of the adhesive bond with the inner side of the blade pressure and suction surfaces for a spar (1) of the state of the art, are also indicated.
The present invention describes a wind turbine blade having a spar that ensures a more homogeneous distribution of the shear stress in the adhesive bond between the spar and the inner surface of the longitudinal hollow element.
The blade comprises at least one longitudinal hollow element that defines an outer aerodynamic surface and an inner cavity having an inner surface having a pressure zone and a suction zone; and comprises at least one spar (1). Said spar (1) is disposed in the inner cavity and is joined to the inner surface by at least two bonding surfaces (13) disposed in the spar bonding zones (2).
The key of the present invention is that the spar (1) comprises at least three fibre fabric layers (3) and at least one central core (4) and at least one lateral core (5) disposed between the at least three fibre fabric layers (3), disposed in at least one bonding zone (2).
In one embodiment, the at least three fibre fabric layers (3) are disposed parallel therebetween and transversely or obliquely with respect to the bonding surface (13) in the bonding zone near the bonding surface.
In one embodiment, the at least three fibre fabric layers (3) extend between the spar bonding zones (2).
In one embodiment, each fibre fabric (3) layer is disposed on at least one side of the central core (4) or lateral core (5).
The at least three layers of fibre fabric (3) are separated by at least two cores (4, 5) in the bonding zone (2) of the spar (1).
In one example of embodiment, such as that shown in
Likewise, the at least one central core (4) comprises at least two fibre fabric layers (3) disposed on at least part of one of the lateral sides (6). One of the fibre fabric layers (3) extends up to the bonding surface (13) directly on said lateral side (6) and the other fibre fabric layer (3) is also disposed on the divergent side (7) of the lateral core (5) such that at least two fibre fabric layers (3) are separated therebetween from the corresponding lateral side (6) up to the at least one bonding surface (13).
In one embodiment, the lateral core (5) also comprises a lateral surface (8) parallel to the lateral side (6) of the central core (4) and adjacent to the divergent side (7), which extends between the divergent side (7) and the bonding surface (13). Thus, according to this embodiment, one of the fibre fabric layers (3) extends up to the bonding surface (13) directly on the lateral side (6) of the central core and the other fibre fabric layer (3) is also disposed on the divergent side (7) of the lateral core (5) and on the parallel lateral surface (8), wherein the layer is prolonged up to the bonding surface. In this manner, the layer disposed on the lateral side (6) of the central core (4) and the layer disposed on the parallel lateral surface (8) are disposed parallel therebetween in the bonding zone near said bonding surface (13).
Preferably, the cores (4) are made of foam, PVC or balsa wood. Also preferably, the bond between the spar (1) and the inner surface is executed by means of an adhesive bond.
In the example of embodiment shown in
In one embodiment, at least the lateral surface (8) of the lateral core (5) has a constant height throughout the entire section of the spar (1). In another embodiment, such as that shown in
In one embodiment, the thickness of the central core (4) is greater than the thickness of the lateral cores (5). In another embodiment, the thickness of the central core (4) decreases throughout the length of the spar (1) from the blade root zone to the blade tip zone and/or the thickness of the lateral cores (5) increases throughout the length of the spar (1) from the blade root zone to the blade tip zone.
Preferably, the width of the spar (1), which is the sum of the thicknesses of the central core (4) and of the lateral cores (5), is constant throughout its length.
In one embodiment, as shown in
| Number | Date | Country | Kind |
|---|---|---|---|
| 15382547.6 | Nov 2015 | EP | regional |
