Patent Application
20100047070
The invention relates to an aerodynamically optimised wind turbine blade and in particular to a wind turbine blade design that reduces the blunt trailing edge noise. The invention also relates to a complementary lightening protection means for the wind turbine blade
The noise from a wind turbine originates from mechanical and aerodynamic sources.
The aerodynamic noise can be split up into different mechanisms that produce the noise:
Thickness noise. Originating from a blade that displaces air by moving through the air. Frequency is discrete and related to blade passing frequency (typical around 1 Hz+harmonics up to around 30 Hz).
Unsteady loading noise. Originating from the pressure fluctuations due to unsteady aerodynamic loading of the blade (from wind shear, rotor misalignment, tower shadow etc.). Frequency is discrete and related to blade passing frequency (typical around 1 Hz+harmonics up to around 30 Hz).
Inflow turbulence noise, also known as leading edge noise. Originating from the leading edge and caused by the atmospheric turbulence, which induces pressure fluctuations when hitting the leading edge. Frequency is broadband and related to the frequency spectrum of the atmospheric turbulence and the tip speed ratio (typical from 0 Hz to around 5000 Hz, most noticeable at low to medium frequencies).
Turbulent boundary layer trailing edge noise. Originating from the fluctuating pressure deficit between the suction side and pressure side when the flows meet at the trailing edge. Frequency is broadband and related to boundary layer parameters (typical from 100 Hz to 10000 Hz, most noticeable at medium frequencies around 1000 Hz).
Tip noise. Originating from the turbulence in the tip vortex. Frequency is broadband and related to the diameter of the tip vortex (typical around 1000 Hz to 8000 Hz).
Stall noise. Originates from the pressure fluctuations in areas with flow separation, often present at high angles of attack. Frequency is broadband and related to the extension of the stall area (typical from 20 Hz to 1000 Hz).
Laminar boundary layer vortex shedding noise. Originates from instabilities in the pressure side boundary layer causing vortex shedding. Frequency is tonal and related to the pressure side boundary layer thickness (typical between 1000 Hz and 4000 Hz).
Blunt trailing edge noise. Originates from the small flow separation zone behind a blunt trailing edge, which causes vortex shedding (well known as von Karman vortex shedding). Frequency is tonal and related to the trailing edge thickness (typical between 1000 Hz and 4000 Hz).
Noise from flow over holes, slits, intrusions. Originating from instable shear flows and vortex shedding. Frequency is tonal and related to the dimension of the flow disturbing element (typical between 1000 and 10000 Hz).
The prior art teaches the use of a serrated trailing edge to reduce the different types of trailing edge noise.
EP 1 314 885 discloses a trailing edge device consisting of a serrated panel to be attached to the trailing edge of the blade.
EP 1 338 793 discloses a one-piece blade made of metal with dentations being formed in the trailing edge part and a two-pieces blade consisting of a main blade body made of metal and a rear member made of a different metal with dentations being formed in the trailing edge part.
None of these proposals produces fully satisfactory results, therefore a continuing need exists for wind turbine blades with a reduced blunt trailing edge noise level.
An object of the present invention is to provide a wind turbine blade that reduces the blunt trailing edge noise.
Another object of the present invention is to provide a wind turbine blade easy to manufacture, handle and transport.
Another object of the present invention is to provide a wind turbine blade having a trailing edge easy to repair when it is damaged.
Another object of the present invention is to provide an improved lightning protection system for the wind turbine blade.
These and other objects of the present invention are met by providing a wind turbine blade comprising a first component having an aerodynamic profile with a leading edge, a blunt trailing edge having a thickness greater than 2 mm, and suction and pressure sides between the leading edge and the trailing edge and a second component having a constant cross section in the spanwise direction of the blade which is rigidly attached to the blunt trailing edge of the first component in at least a part of the wind turbine blade by attachment means that allow its replacement.
In a preferred embodiment the second component includes a conductive layer connected to the wind turbine blade lightning system. Hereby a improved lightning protection system for the wind turbine blade is achieved.
Other features and advantages of the present invention will be understood from the following detailed description in relation with the enclosed drawings.
a to 8d are schematic sectional views of different embodiments of a splitter plate according to the present invention incorporating means for protecting the blade against lightning.
Depending on the bluntness and the shape of the trailing edge 13 and the Reynolds number, vortex shedding 23 can occur resulting in a von Karman type vortex street. The alternating vortices in the near wake produce higher surface pressure fluctuations close to the trailing edge 13. If the bluntness parameter T/δ, where T is the trailing edge 13 thickness and δ the boundary layer 25 displacement thickness, is large enough, fluctuation forces will occur resulting in dipole noise of tonal character.
The wind turbine blade first component 7 according to the present invention, shown in
In the embodiment shown in
The noise produced by the blunt trailing edge noise mechanism (a completely different physical mechanism than the turbulent boundary layer trailing edge noise) is proportional to the trailing edge thickness T.
The noise produced by the turbulent boundary layer mechanism is proportional to cosq3, where q is the flow angle between the flow direction over the trailing edge and a line perpendicular to the trailing edge. For a normal wind turbine blade without significant spanwise flow this angle is usually small (around 0° to 10°), and the cosine term is approximately 1. In the case of a serrated trailing edge, such as those of the prior art proposal above-mentioned, this angle is much higher (depending on the angle of the serrations), maybe around 70° to 85°, and the cosine term is close to 0. This will dramatically reduce the noise in theory but in practice the results are not always as good as expected.
The trailing edge strip 9 has a sharp profile with upper and lower surfaces shaped as extensions of the suction and pressure sides of said first component 7 ending in a sharp edge.
By using a trailing edge strip 9, which is more or less sharp, the resulting trailing edge thickness is close to 0, and thereby the blunt trailing edge noise mechanism is eliminated.
The trailing edge strip 9 has a constant cross section in spanwise direction while the serrated trailing edge of the above-mentioned prior art proposals has a non-constant cross section in spanwise direction.
The upper and lower surfaces of the trailing edge strip 9 could have a flat geometry or a slightly curved geometry.
The attachment of the trailing edge strip 9 to the first component 7 can be made in any suitable manner.
In a preferred embodiment the trailing edge strip 9 includes a plate 10 which extends in between the shells of the first component 7 and it is glued together.
In another preferred embodiment the trailing edge strip 9 is attached to the first component 7 by means of a ‘click-on device’ (not shown).
In the embodiment shown in
In a preferred embodiment the thickness T2 of the splitter plate 12 is lesser than 1 mm.
In another preferred embodiment the width W2 of the splitter plate 12 extending from the blunt trailing edge 13 is greater than two times the thickness T of the blunt trailing edge 13.
The splitter plate 12 prevents the otherwise periodical alternating vortex shedding from the upper and lower corners of the blunt trailing edge 13, which produce tonal noise. The splitter plate 12 dramatically reduces the periodical vortex shedding and could almost eliminate the tonal part of the trailing edge bluntness noise. There will still be some periodical vortex shedding from the end of the splitter plate 12, but if the thickness T2 of this splitter plate is small, the amplitude of the tonal noise will also be small (possibly drowned by other noise sources) and the frequency will be high (possibly outside the audible frequency range of the human hearing). If the blunt trailing edge 13 gets damaged, it would be easy to repair it just by replacing a piece of the splitter plate 12.
The splitter plate 12 is fastened between the shells by gluing, a click-on device or by other means. The precise placement of the splitter plate 12 is not critical because it is effective in different angles with respect to the blunt trailing edge 13 and in different extension lengths from the blunt trailing edge
In a preferred embodiment, the splitter plate 12 includes one or several perpendicular walls 14 having a length L1 lesser than the thickness T of the blunt trailing edge 13.
The thickness T of the blunt trailing edge 13 is greater than 2 mm, which is the minimum thickness of standard wind turbine blades in serial production using standard manufacturing procedures.
In another preferred embodiment the thickness T of the blunt trailing edge 13 is greater than 5 mm.
In another preferred embodiment the thickness T of the blunt trailing edge 13 is greater than 10 mm.
Blades with thicker trailing edges than current standard blades made with trailing edge thickness T in the range of 2-3 mm could be easier in production and finish and more robust for transportation.
In a preferred embodiment the trailing edge strip 9 or the splitter plate 12 could cover the outermost part of the blade, in a length from 2% to 35% of the blade radius. At the midspan and the inboard part of the blade, it is normally not so interesting to have the second component, because the noise produced from these parts of the blade is minor compared to the outer part. Furthermore, there are other factors making it desirable to have a thicker blunt trailing edge at the inboard part of the blade.
The trailing edge strip 9 or the splitter plate 12 can be made in plastic or any other material that is cheap and easy to shape in the desired geometry in predetermined lengths L of e.g. 1 m for facilitating the attachment to the first component 7.
In preferred embodiments a porous material (or a solid material having holes) or a flexible material are used to decrease the surface acoustic impedance and consequently reducing the noise caused by other noise sources.
The trailing edge strip 9 or the splitter plate 12 according to the present invention can be attached to blades preferably made in GFRP although can also be attached to blades made of other materials such as wood, metal, CFRP or other fiber materials.
In addition to its function as a device for reducing the blunt trailing edge noise, the splitter plate 12 may also be used as a complementary means for protecting the blade against lightning or other electrical discharges.
As shown in
To accomplish said complementary lightning protection the splitter plate 12 comprises a base plate 31 made in a non-conductive material and a layer 33 of a conductive material connected to the lightning protecting system covering at least a section of one of the surfaces of the base plate 31.
In a preferred embodiment, the fixture of the layer 33 to the base plate 31 will be done in a similar manner to the conductive layer on an electronic printed circuit board (PCB).
Taking into account that the edgewise loads typically makes the trailing edge 13 to one of the highest stress areas of the blade where the extreme strains can reach up to 10.000 μstrain, the layer 33 can not be a “straight” but a “flexible” conductor element able to withstand said strains.
Consequently, the layer 33 is not expected to have a good conductibility for a normal constant current, but for a sphere of ionized air with high electric potential. The layer 33 shall be seen as an “attractive conductor” capable to guide the energy towards the more heavy lightning down conductor 41 designed to transmit the high frequency current with high current altitude and hence potential heat generation towards a stable ground potential.
Hence the layer 33 must with interval be connected to the lightning down connector 41 and this connection must be made in a way which enable good guidance of this extreme energy transmission with no or limited “flash over” with possible damage outside the lightning protection system. The physical interval between said connections could be in the range from 0,5 m to 5 m.
Said connections may be made by means of flexible conductors 45 inside the blade and/or conducting tapes 47 mounted at the blade surface between the layer 33 and the lightning receptors 43.
The typical lightning impact area on a wind turbine blade is in the outer part 5 of the blade. Due to this, the splitter plate 12 preferably comprises conductive layers 33 in the outer part 5 of the blade along a length in the range of 2% to 35% the blade radius.
In preferred embodiments, shown in
In the embodiment shown in
In the embodiment shown in
In the embodiments shown in
The embodiments shown in
The main advantage of having complementary means for protecting the blade against lightning or other electrical discharges in the splitter plate 12 is that the damages caused by lightening in the own blade are reduced. On the other hand, the damages caused in the splitter plate 12 are easy to repair.
Although the present invention has been fully described in connection with preferred embodiments, it is evident that modifications may be introduced within the scope thereof, not considering this as limited by these embodiments, but by the contents of the following claims.
| Number | Date | Country | Kind |
|---|---|---|---|
| P200602347 | Sep 2006 | ES | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/ES07/70160 | 9/14/2007 | WO | 00 | 8/18/2009 |
