Wind turbine rotor blade with vortex generators
A wind turbine rotor blade with an airfoil having a suction side and a pressure side is provided. The airfoil comprises an inner airfoil portion and an outer airfoil portion, where the inner airfoil portion is comparatively thicker than the outer airfoil portion and provided with vortex generators. The thickness of the inner airfoil portion is between 30% and 80% of the inner airfoil portion's chord length, and the vortex generators are located at the suction side of the inner airfoil portion between 8% and 12% of the chord length, as measured from the leading edge of the airfoil portion.
This application claims priority of European Patent Office application No. 07000617.6 EP filed Jan. 12, 2007, which is incorporated by reference herein in its entirety.
FIELD OF INVENTIONThe present invention relates to a wind turbine rotor blade with vortex generators and to a wind turbine with at least one of such rotor blades.
BACKGROUND OF INVENTIONA state of the art rotor blade for a wind turbine is, e.g. described in EP 1 314 885 A1. Such a blade comprises a root portion having a cylindrically shaped cross-section by which the rotor blade is fixed a hub of the rotor and an airfoil portion with an aerodynamically shaped cross-section.
It is usual to subdivide the airfoil portion notionally into a relatively thick inner airfoil portion and a relatively thin outer airfoil portion where the inner airfoil portion is located between the root portion and the outer airfoil portion.
The wind turbine rotor blade disclosed in EP 1 314 885 A1 is provided with vortex generators located at the suction side of the inner airfoil portion.
Vortex generators which are located on a wind turbine rotor blade close to the hub portion are also known from WO 02/08600 A1. In addition, the use of vortex generators is described in WO 00/15961 as well as in EP 0 947 693 A2.
In Van Rooij, R. P. J. O. M.; Timmer, W. A.: “Roughness sensitivity considerations for thick rotor blade airfoils”, Journal of Solar Energy Engineering, vol. 125, no. 4, November 2003 (2003-11), pages 468-478, XP00807970 New York, N.Y., US and in Peter Fuglsang, Christian Bak: “Development of the Riso Wind Turbine Airfoils” A Sampling of the 2003 EWEC in Madrid, vol. 7, no. 2, 24 May 2004 (2004-05-24), pages 145-162, XP002436915 John Wiley & Sons Ltd., different wind turbine rotor blades having a thickness between 25% and 40.1% as compared to the chord length are described. The rotor blades are equipped with vortex generators, which are located at the airfoil's suction side at 20% or 30% of the chord length, as measured from the leading edge of the airfoil.
In the mentioned state of the art, the use of vortex generators for improving the aerodynamical properties of the wind turbine rotor blades is described. However, an optimum position of the vortex generators depends on many parameters. Therefore, a good position of vortex generators at the outer airfoil portion of a rotor blade cannot necessarily be expected to be also a good position of the vortex generators at the inner airfoil portion of the rotor blade. However, in particular the inner airfoil portion of the rotor blade has a reduced aerodynamic performance as compared to the outer airfoil portion. The reason is that the inner part of the wind turbine rotor blade needs to carry the load from the entire blade. This means a number of design constrains in order to achieve sufficient stiffness of the rotor blade. The reduced aerodynamic performance of the inner airfoil portion compared to the outer airfoil portion reduces the overall efficiency of a wind turbine. It is therefore desired to improve the aerodynamic performance of the inner airfoil portion.
SUMMARY OF INVENTIONIn view of the aforementioned it is an objective of the present invention to provide an improved wind turbine rotor blade with vortex generators located such that a sufficient aerodynamic performance and, at the same time, a high load bearing can be achieved.
It is a further objective of the present invention to provide an improved wind turbine.
The first objective is solved by a wind turbine rotor blade according to a independent claim and the second objective is solved by a wind turbine according to a further independent claim. The depending claims define further developments of the present invention.
An inventive wind turbine rotor blade comprises an airfoil having a suction side and a pressure side. The airfoil further comprises an inner airfoil portion and an outer airfoil portion where the inner airfoil portion is comparatively thicker than the outer airfoil portion. In addition, the inner airfoil portion is provided with vortex generators. In the inventive wind turbine rotor blade the thickness of the inner airfoil portion is between 30% and 80% of the inner airfoil portions chord length. The vortex generators are located at the suction side of the inner airfoil portion between 8% and 12% of the chord length, as measured from the leading edge of the airfoil portion.
The inventive wind turbine rotor blade provides an improved stiffness as compared to the state of the art rotor blades with comparable aerodynamic performance of the inner airfoil portion. The high stiffness is achieved by the extreme thickness of the inner airfoil portion which lies between 40% and 80% chord length. However, usually, thicker blades are related to lower are aerodynamic performance. In the present invention the lower aerodynamic performance of an extreme thick airfoil portion is overcome by positioning vortex generators on the suction side of the thick inner airfoil portion. Therefore, the combination of the extreme thickness of the inner airfoil portion and the suitably located vortex generators allows for wind turbine rotor blades having a high stiffness in the inner airfoil portion and, at the same time, a satisfactory aerodynamic performance. Up to now, the use of vortex generators for extreme thick blades was unknown. Even in WO 02/08600 A1, where vortex generators are located close to the root, the airfoil portion carrying the vortex generators is not a thick airfoil portion.
A sufficient strength of the wind turbine rotor blades inner airfoil portion can also be achieved with a thickness between 40% and 65% chord length.
To achieve the maximum effect of the vortex generators it is advantageous when vortex generators are present along the whole span of the inner airfoil portion. All vortex generators may be located at the same chord length.
It should be noted, that the use of vortex generators in the outer, thinner airfoil portion shall not be excluded by the invention.
An inventive wind turbine rotor comprises at least one rotor blade according to the invention. In particular all rotor blades of the wind turbine, e.g. all three rotor blades of a three-bladed wind turbine rotor, are rotor blades according to the invention.
Further features, properties and advantages of the present invention will become clear from the following description of embodiments of the invention in conjunction with the accompanying drawings.
In the drawings:
The rotor blade 1 shown in
The airfoil 5 extends along the so called span (dash dotted line in
A chord-wise cross-section through the rotor blades thin airfoil portion 6 along the line I-I is shown in
A chord-wise cross-section through the rotor blades thick airfoil portion 7 along the line II-II in
The main difference between the cross-section of the thick airfoil portion shown in
Also shown in the thick airfoil portion's cross-section according to the first embodiment is a vortex generator 21 which is located at the suction side 13 between 25 and 30% chord length, as measured from the leading edge 9.
Alternative locations of the vortex generators 21′, 21″ on the suction side 13 of the thick airfoil portion are shown in
It should be noted that the optimum position of the vortex generator may vary depending on the thickness to chord length ratio of the profile as well as on the overall shape of the cross-section. However, it is advantageous if the vortex generator lies in the range between 5% and 30% of the chord length for thick airfoil portions with a ratio of thickness to chord length in the range between 30% and 80% and in particular for ratios in the range between 40% and 65%.
The influence of the vortex generators 21, 21′, 21″′ at the locations shown in
The line denoted by A is the result of a lift coefficient measurement for a wind turbine blade without any vortex generators. The lines designated by B, C and D show the results of turbine blades having vortex generators at the suction side of the thick airfoil portion at the locations shown in
It can be easily seen from
As a general trend it can be noted that the maximum lift coefficient of the blade moves towards higher angles of attack as the location of the vortex generators moves towards the leading edge of the profile. Moreover, the maximum value of the lift coefficient cl increases accordingly.
Based on the differences in the lift coefficients cl and the drag coefficient cd for the different vortex generator configurations shown in
Although the main advantage of the vortex generators is an improved energy production, other advantages are achievable, too. The drop of lift, as represented by the drop of the lift coefficient cl in
Claims
1.-5. (canceled)
6. A wind turbine rotor blade, comprising:
- an airfoil having a suction side and a pressure side, the airfoil comprising an inner airfoil portion and an outer airfoil portion, where the inner airfoil portion is comparatively thicker than the outer airfoil portion, the thickness of the inner airfoil portion being between 30% and 80% of a inner airfoil portion's chord length; and
- vortex generators at the suction side of the inner airfoil portion between 8% and 12% of the chord length, as measured from the leading edge of the airfoil portion.
7. The wind turbine rotor blade as claimed in claim 6, wherein the thickness of the inner airfoil portion is between 40% and 65% of the chord length.
8. The wind turbine rotor blade as claimed in claim 6, wherein all vortex generators are located at the same chord length.
9. The wind turbine rotor blade as claimed in claim 7, wherein all vortex generators are located at the same chord length.
10. The wind turbine rotor blade as claimed in claim 6, wherein vortex generators are present along the whole span of the inner airfoil portion.
11. The wind turbine rotor blade as claimed in claim 7, wherein vortex generators are present along the whole span of the inner airfoil portion.
12. The wind turbine rotor blade as claimed in claim 8, wherein vortex generators are present along the whole span of the inner airfoil portion.
13. The wind turbine rotor blade as claimed in claim 9, wherein vortex generators are present along the whole span of the inner airfoil portion.
14. A wind turbine, comprising:
- a rotor blade having an airfoil having a suction side and a pressure side, the airfoil comprising an inner airfoil portion and an outer airfoil portion, where the inner airfoil portion is comparatively thicker than the outer airfoil portion, the thickness of the inner airfoil portion being between 30% and 80% of a inner airfoil portion's chord length, and vortex generators at the suction side of the inner airfoil portion between 8% and 12% of the chord length, as measured from the leading edge of the airfoil portion.
15. The wind turbine as claimed in claim 14, wherein the thickness of the inner airfoil portion is between 40% and 65% of the chord length.
16. The wind turbine as claimed in claim 15, wherein all vortex generators are located at the same chord length.
17. The wind turbine as claimed in claim 16, wherein vortex generators are present along the whole span of the inner airfoil portion.
Type: Application
Filed: Jan 11, 2008
Publication Date: Dec 25, 2008
Inventors: Peder Bay Enevoldsen (Vejle), Soeren Hjort (Brande)
Application Number: 12/008,690
International Classification: F01D 5/14 (20060101);