The aim of the present invention patent is a wind turbine blade with high-lift devices in the blade's root area, where there are two types of these elements: high-lift devices on the leading edge area and on the trailing edge area, so that said blade is aerodynamically optimized in its whole geometry to increase the wind turbine's energy production.
Traditional wind turbine blades are joined to the hub in a cylindrical area known as the root, with a characteristic length of usually several meters. For most wind turbines, the function of this area is typically structural and does not significantly contribute to the wind turbine's production, as it is not aerodynamically optimized.
In the current state of the art, detachable elements in the root area, are described to improve the blade's performance. However, they are characterized by having a sharp trailing edge and a very large chord length on the joint with the root.
Thus for example, we have document WO 2007/131937 that describes a blade for a wind-power generator with a detachable element on the trailing edge detachable from the blade itself.
To solve the above mentioned problem mentioned, the wind turbine blade with a high-lift device is presented, object of the present patent of invention. Said high-lift devices are of two different types, according to their position and use in the blade:
(i) High-lift device of the wind turbine trailing edge area;
(ii) High-lift device of the wind turbine leading edge area;
The high-lift device of the trailing edge is a fixed part, and not mobile like in other aerodynamic trailing edge devices related in the state of the art. The trailing edge of this element is thicker than known trailing edges, obtaining a bigger lift coefficient, which at the same time allows to make the detachable element with less total length (less chord). In other words, a shorter length or chord is obtained for the same lift, with greater trailing edge relative thickness. The device also allows to make a blade with less torsion, owing to having a greater stall angle in losses at high angles of attack. This high-lift device can be part of a one-piece blade and not only as an additional or detachable element.
The leading edge's high-lift device is selected amongst:
The following technical advantages are obtained with the combined use of the two configurations (trailing edge and leading edge):
The wind turbine produces more energy, on improving the blades' aerodynamic coefficient.
Improved performance is obtained at lower ambient wind speeds, as the wind incidence angle has been improved.
The already installed blades can be used, and their production and transport is also improved and made easier.
A brief description of a series of illustrations is provided below in order to better understand the invention. These illustrations are expressly listed with an embodiment of the present invention and are presented as an illustrative, but not restrictive, example of the same.
As can be observed in the attached figures, the wind turbine blade with high-lift devices comprises, at least, a trailing edge high-lift device (1) with a blunt end and chord (C) length of 5% to 30% less than a conventional profile for the same lift coefficient; and as the joint area radius is related to the blade's (3) root (4) radius, and to the thickness of this trailing edge high-lift device (1).
The first trailing edge high-lift device (1) can be detachable or integrated in a one-piece blade.
The leading edge's high-lift device (2) is selected amongst:
In the design of high-lift devices coupled to the wind turbine blade, both on the leading edge and trailing edge, as well as taking into account optimising the ration between CL lift coefficient and the αSTALL angle of attack, a safety distance between the geometrical limits of the detachments and the machine itself should be taken into account.
Number | Date | Country | Kind |
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P200801632 | May 2008 | ES | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/ES2009/070191 | 5/28/2009 | WO | 00 | 11/23/2010 |