WIND TURBINE HAVING A REDUCED RADAR CROSS SECTION

Abstract

A wind turbine including a support structure and one or more turbine blades is presented, that incorporates ways for reducing the radar cross section (RCS), wherein the support structure is notionally divided into an upper section in the shadow of the blade sweep area, and a lower section beneath the upper section, wherein the upper section is adapted to have the ways for reducing the RCS, and the lower section does not have the adaptation. The invention makes use of the realisation that the blade masking the tower as it rotates (or the blade being masked by the tower if facing away from a radar), contributes significantly to interference to radar systems, and so localised application of e.g. RAM can give good RCS reduction at a lower cost than treating the whole structure.

Claims

1-16. (canceled)

17. A wind turbine comprising: a support structure; and one or more turbine blades, each of the one or more turbine blades having a tip at an end thereof, the tip being at a lowest point when the turbine blade reaches its nadir upon aligning with the support structure, wherein the support structure is notionally divided, by the lowest point of the tip of a turbine blade of the one or more turbine blades, into an upper section and a lower section, the upper section including a part of the support structure that overlaps with the turbine blades' sweep area, and the lower section being a remaining part of the support structure below the upper section, wherein a portion spanning from approximately 20 to less than 180 of a circumference of certain cross-sections of the upper section is adapted to have a reduced radar cross section (RCS).

18. The wind turbine as claimed in claim 17, wherein the portion of the upper section is covered with radiation absorbent material (RAM) and substantially none of the length of the lower section has a reduced cross section (RCS).

19. The wind turbine as claimed in claim 18, wherein the RAM is adapted to be absorbent at wavelengths transmitted by an associated radar system.

20. The wind turbine as claimed in claim 17, wherein the portion includes two opposing sections relative to the circumference of the upper section that each span approximately 45.

21. The wind turbine as claimed in claim 17, wherein, given a predetermined location of a radar in relation to the support structure, the portion faces the radar and is covered in RAM.

22. The wind turbine as claimed in claim 21, wherein angular coverage of the portion covered with RAM extends to between approximately 20 to 90 either side of a point on the circumference facing the radar.

23. The wind turbine as claimed in claim 22, wherein the angular coverage is approximately 45 either side of the point facing the radar.

24. The wind turbine as claimed in claim 21, wherein a region on the upper side of the support structure opposite to the side facing the radar also has a RAM coating applied thereto.

25. The wind turbine as claimed in claim 17, wherein the upper section is itself divided into a plurality of sub-sections or sub-regions, wherein a given sub-section or sub-region has a different covering of RAM as compared to another.

26. The wind turbine as claimed in claim 17, wherein substantially of the upper section has a RAM covering.

27. The wind turbine as claimed in claim 17, wherein the RAM comprises a plurality of tiles, each comprising a multi-layered circuit analogue structure.

28. The wind turbine as claimed in claim 27, wherein the tiles have a substrate layer comprising glass fibre.

29. The wind turbine as claimed in claim 17, wherein the upper section of the support structure is shaped so as to avoid reflection of radio frequency electromagnetic (EM) energy in a direction of interest.

30. A wind turbine comprising: a support structure; and one or more turbine blades, each of the one or more turbine blades having a tip at an end thereof, the tip being at a lowest point when the turbine blade reaches its nadir upon aligning with the support structure, wherein the support structure is notionally divided, by the lowest point of the tip of a turbine blade of the one or more turbine blades, into an upper section and a lower section, the upper section including a part of the support structure that goes into shadow of an illuminating radar as a turbine blade sweeps past the support structure, and the lower section being a remaining part of the support structure below the upper section, wherein a portion spanning from approximately 20 to less than 180 of a circumference of certain cross-sections of the upper section is adapted to have a reduced cross radar section (RCS).

31. The wind turbine as claimed in claim 30, wherein substantially none of the length of the lower section has a reduced radar cross section (RCS), and the portion of the upper section is covered with radiation absorbent material (RAM).

32. A method of treating a support structure of a wind turbine, the wind turbine including a blade, the blade having a tip at an end thereof, the tip being at a lowest point when the blade reaches its nadir upon aligning with the support structure, the support structure being notionally divided by the lowest point of the tip into an upper section and a lower section, the method comprising: i) identifying the upper section of the support structure, the upper section being a top part having overlap with a sweep area of the blade of the wind turbine, with a remainder of the support structure below it being the lower section; ii) identifying a region on a side of the support structure facing a region of interest; and iii) adapting at least a portion spanning from approximately 20 to less than 180 of a circumference of certain cross-sections of the upper section of the support structure to reduce its radar cross section (RCS), with the portion including a substantial part of the region defined in (ii).

33. The method as claimed in claim 32, further including: arranging the lower part of the support structure such that substantially none of the length thereof is adapted to reduce radar cross section (RCS); and covering the length of the upper section with radiation absorbent material (RAM).

Description

[0025] Embodiments of the invention will now be described, by way of example only, with reference to the following Figures, of which:

[0026] FIG. 1 diagrammatically illustrates a wind turbine upon which embodiments of the current invention may be implemented;

[0027] FIG. 2 diagrammatically illustrates various blade positions of a turbine which lead to the problem addressed by the present invention;

[0028] FIG. 3 diagrammatically illustrates a wind turbine having a minimum separation between its blade and tower that varies along the length of the blade;

[0029] FIGS. 4-9 diagrammatically illustrate various embodiment of the present invention.

[0030] FIG. 1 shows a representation of a wind turbine (1) in profile view, comprising a support tower (2), nacelle (3) and turbine blades (4). The diagram is not shown to scale, and in practice the tower would generally be longer than shown, in relation to the length of the blades. The blades (4) rotate about their rotational axis and hence each blade, at the bottom of its rotation, lines up with the tower (2).

[0031] A radar (5) is shown illuminating the turbine (1) with EM radiation, with that part of its illumination of general interest to the current invention shown (6). The EM radiation (6) hits the tower (2) and blades (4), and reflects back, and is received by the radar (5) and subsequently processed in known manner. For most of the rotational period of the turbine the blades are not obscuring any significant area of the tower. However, when a blade reaches its nadir then it is in line with the tower, and provides maximum obscuration of part of the tower. The lower blade (4) is shown in this position, and it can be seen to be obscuring the upper part of the tower marked by arrow (7) from the radar (5). Thus the section shown by the arrow (7) is the upper section of the tower, while that part of the tower below it is the lower section. It can be seen that the upper section is approximately equal to the length of a single blade (4).

[0032] FIG. 2 shows in more detail the obscuration process as the blade rotates. FIG. 2a shows a blade (4) rotating about a fulcrum (8), and moving in the direction shown by the arrow. It is approaching its lowest point. Tower (2) is partially obscured, mainly in the upper left part, by the leading edge of the blade, but as the blade sweeps round further, the amount of obscuration will increase quickly.

[0033] FIG. 2b shows the blade (4) in its lowest part, and at a point at, or very close to, maximum obscuration of the tower, dependent upon the exact shape of the blade and the angle from which the blade and tower are being observed. The amount of blade movement between FIGS. 2a and 2b is slight, but the additional obscuration of the tower is significant. Thus the obscuration tends to appear, to a radar, as a sudden transition with a discontinuous reflection phase and/or magnitude. In normal operating conditions the transition occurs sufficiently quickly to show as a large Doppler velocity change, which can lead to the radar giving a false measurement or detection.

[0034] FIG. 2c shows the blade moving away from the lowest point, and starting to reveal the previously obscured tower once more, as the blade's trailing edge moves around. The shape of the blade's trailing edge may differ from the leading edge, resulting in a reveal of the tower at a different apparent pace to that of its obscuration. This can compound the problem this causes to the Doppler radar signal processing.

[0035] FIG. 3 shows a type of wind turbine that can create additional RCS peaks due to the relative shaping of the blades and the support tower. Here, wind turbine (30) has a tower (31) that tapers inwards from its base to its top. A blade (32) is shown positioned at its lowest point. It can be seen that the horizontal separation between the blade and the tower varies along the length of the blade. For example, the separation at the blade tip is shown at A, and the separation at the middle of the blade shown at B.

[0036] Thus, as the blade (32) sweeps past the tower as it moves through its nadir, as well as the sudden transition effect described with relation to FIG. 2, there is also a more gradual (but still rapid) apparent change in the average distance of the upper section of the tower as would be perceived by a Doppler radar. This effect can produce the unwelcome RCS peak effects in such radars.

[0037] Prior to this invention, the effects described above were not realised by those working in the field. Therefore, their solution was to cover all, or a significant part of the whole of the tower in some sort or RAM or equivalent, to prevent reflected radiation from interfering with radar systems. The realisation of the cause has enabled a much lower cost option of highly selective RAM placement just where it has the most benefit.

[0038] FIGS. 4 to 8 show various embodiments of the invention wherein a selected part of the upper section of the support structure is treated to reduce reflections back to an associated radar system. In all figures the upper section is that part lying above the dotted line (43).

[0039] With regards to FIG. 4a, a part of a wind turbine (40) is shown, including the uppermost part of the tower (41) and nacelle and blades (42). Located on the tower is a patch of RAM (44) that stretches from the bottom of the upper section to almost the top of the tower. The RAM (44) covers a 90 sector of the tower's circumference, as indicated at (44) in the cross section view at FIG. 4b. The RAM (44) is chosen to be absorbent to radiation emitted by an associated radar system. The location of the radar system is generally known, particularly if it is a fixed, ground based radar. In such circumstances, the RAM is positioned on the tower so that the horizontal centre of the RAM faces the radar's location. This gives RAM coverage up to 45 each side of boresight direction, to cover instances where the nacelle is not pointing straight at the radar location.

[0040] FIG. 5 shows another embodiment of the invention having different treatments to reduce the RCS of the upper section. FIG. 5a shows a similar wind turbine (50) and its support structure (51), having a partial RAM coating (52) on the front (i.e. the region facing towards a known radar position), as in FIG. 4. However, as is evident from the cross-sectional view at FIG. 5b, as well as the front RAM coating (52), there is also a rear coating (53) of similar size, and on an opposing side of the tower (51). This rear coating is present to attenuate radar returns when the turbine nacelle (42) is facing away from the radar, and hence when there exists a significant possibility for multipath reflections from the blades 54 and the rear of the tower (51).

[0041] FIG. 6a shows an embodiment wherein, within the upper region of a wind turbine support structure (60), the support structure has two differing RAM covering regimes. A first length of the support structure (60), denoted x has a 90 RAM covering (61) on the front of the tower, as is shown by reference to the cross section of that first length at FIG. 6b. A second length of the support structure (60), denoted y, has a 45 RAM covering (62), as shown in the cross-section view of the second length at FIG. 6c. Thus the amount of RAM coating (or indeed any other technique used to reduce reflections back to the radar) can be tailored according to the measured or predicted effects of particular parts of the support structure. Here, the design reflects the result of such predictions or measurements that a lower Doppler return will emanate from the second length, and hence a smaller, and hence cheaper, region of the tower needs to be treated with the RAM coating.

[0042] FIG. 7 shows an embodiment of the invention similar to that of FIG. 6, but having a different RAM coverage pattern. FIG. 7a shows the front view of the turbine unit (70). A first length (x) has a RAM coating (71) covering a 180 span, whereas a second length (y) has a 90 angular coverage of RAM coating (72). FIG. 7b shows in cross section the coverage for the first length (x) with RAM coating (71) attached to a front facing part of the tower structure, while FIG. 7c shows in cross section the coverage for the second length (y).

[0043] FIG. 8 shows an embodiment of the invention having both a front and rear coating of RAM, with differing coverage along the length on the front face. FIG. 8a shows the front view of a wind turbine (80). On the front face of the turbine (80) a first length (x) has a RAM coating (81) covering a 90 span, whereas a second length (y) has a 45 angular coverage of RAM (82) coating the side of the tower. On the rear face of the turbine (80) is a strip of RAM (83) of a width that provides a 45 coating running the length of the upper section. FIGS. 8b and 8c show cross sectional views of the tower for the first length (x) and a second length (y) respectively, with the sectorial RAM coverage of the lengths indicated.

[0044] FIG. 9a shows an embodiment of the invention wherein a turbine (90) has a RAM coating (91) covering substantially all of the upper section of its support structure, on both the front and back. This provides maximum attenuation of radiation that impinges upon the upper section, but also has the largest coverage area (and hence cost) and weight. FIG. 9b shows a cross-sectional view of the upper section, where it can be seen that the RAM coating (91) covers the whole circumference.

[0045] The invention has been described primarily with relation to the commonplace HAWT version of the wind turbine. The normally skilled person will appreciate that various modifications and alterations may be applied to the embodiments described without deviating from the spirit and scope of the invention, including adapting the patterning and area coverage of any anti-reflection coatings (including RAM), shaping to reduce reflections in any given direction, and use of the invention on VAWT systems.