ROTOR BLADE OF A WIND TURBINE AND WIND TURBINE

Abstract

A rotor blade of a wind turbine include sa first rotor blade segment having a first shell portion, a second rotor blade segment having a second shell portion and a joint connecting the first rotor blade segment with the second rotor blade segment between the first shell portion and the second shell portion, whereby the rotor blade further includes a fairing, the fairing covering the joint and being attached to the first shell portion and the second shell portion by means of an adhesive. Further provided is a wind turbine having this rotor blade.

Claims

1-17. (canceled)

18. A rotor blade of a wind turbine, the rotor blade comprising a first rotor blade segment having a first shell portion, a second rotor blade segment having a second shell portion and a joint connecting the first rotor blade segment with the second rotor blade segment between the first shell portion and the second shell portion, whereby the rotor blade further comprises a fairing, the fairing covering the joint and being attached to the first shell portion and the second shell portion by means of an adhesive.

19. The rotor blade according to claim 18, whereby the adhesive is an elastomeric adhesive.

20. The rotor blade according to claim 18, whereby the adhesive is a rubber-based adhesive.

21. The rotor blade according to claim 18, whereby the adhesive is configured to cure at ambient temperature.

22. The rotor blade according to claim 18, whereby the first shell portion and the second shell portion comprise flange portions at facing ends thereof, whereby the fairing is attached to the flange portions.

23. The rotor blade according to claim 22, whereby the fairing is bonded to bonding surfaces of the flange portions by means of bonding portions of the adhesive.

24. The rotor blade according to claim 22, whereby the fairing is sealed against sealing surfaces of the flange portions by means of sealing portions of the adhesive.

25. The rotor blade according to claim 18, whereby the first rotor blade segment is an inboard blade segment and the second rotor blade segment is an outboard blade section.

26. The rotor blade according to claim 18, whereby the fairing is made from at least two fairing plates.

27. The rotor blade according to claim 26, whereby the fairing plates are sealed against each other by means of an adhesive.

28. The rotor blade according to claim 26, whereby at least one fairing plate of the at least two fairing plates is bonded to the at least other one fairing plate of the at least two fairing plates by means of an adhesive and to a bonding surface thereof.

29. The rotor blade according to claim 26, whereby one fairing plate of the at least two fairing plates is attached to the first shell portion and the second shell portion by means of a weaker adhesive than the at least one other fairing plate of the at least two fairing plates.

30. The rotor blade according to claim 26, whereby a leading edge fairing plate of at least four fairing plates is located at a leading edge of the rotor blade, a trailing edge fairing plate of the at least four fairing plates is located at a trailing edge of the rotor blade, a suction side fairing plate of the at least four fairing plates is located at the suction side of the rotor blade and a pressure side fairing plate of the at least four fairing plates is located at the pressure side of the rotor blade.

31. The rotor blade according to claim 30, whereby the trailing edge fairing plate has a sharp geometry and comprises a trailing edge reinforcement part in between opposite sides of the trailing edge fairing plate.

32. A wind turbine having at least one rotor blade according to claim 18.

33. The rotor blade according to claim 20, wherein the rubber-based adhesive, is a silicon-based adhesive.

34. The rotor blade according to claim 26, wherein the fairing is made from at least four fairing plates.

Description

BRIEF DESCRIPTION

[0026] Some of the embodiments will be described in detail, with reference to the following figures, wherein like designations denote like members, wherein:

[0027] FIG. 1 shows a side view on a wind turbine;

[0028] FIG. 2 shows a side perspective view on a part of an assembly of a rotor blade of FIG. 1;

[0029] FIG. 3 shows a sectional cut through a shell of the assembled rotor blade of FIG. 2 at the location of the fairing;

[0030] FIG. 4 shows a side perspective view on a part of an assembly of the rotor blade of FIG. 2 including a fairing; and

[0031] FIG. 5 shows a side perspective view on the part of the assembled rotor blade of FIG. 2.

DETAILED DESCRIPTION

[0032] FIG. 1 shows a side view on a wind turbine 1. The wind turbine 1 comprises a supporting tower 2 and a nacelle 3, whereby the nacelle 3 is attached to the supporting tower 2. The wind turbine 1 further comprises a generator 4 attached to a rotor 5 of the wind turbine 1.

[0033] Two rotor blades 10, which may alternatively be referred to as wind turbine blades, are attached to the rotor 5. However, the number of rotor blades 10 may alternatively be more than two, such as three, for example.

[0034] Each one of the rotor blades 10 has a first rotor blade segment 11 and a second rotor blade segment 12. The first rotor blade segment 11 is an inboard blade segment, whereas the second blade segment 12 is an outboard blade segment. The two rotor blade segments 11, 12 are joined on site when installing them in the wind turbine 1. A joint 19 as shown in FIG. 2 can be employed for joining the rotor blade segments 11, 12 with each other. After joining the rotor blade segments 11, 12 with each other, a fairing 20 may be provided at the circumference of the shell of the rotor blades 10 to cover the joint 19 and close the gap between the rotor blade segments 11, 12 and their shell portions provided for establishing the joint during assembly.

[0035] FIG. 2 shows a side perspective view on a part of an assembly of one of the rotor blades 10 of the wind turbine 1. The rotor blade segments 11, 12 are shown here only partially. The first rotor blade segment 11 has a first shell portion 13 and the second rotor blade segment 12 has a second shell portion 14. The first rotor blade segment 11 further has a first spar section 15 and the second rotor blade segment 12 has a second spar section 16. These spar sections 15, 16 must be joined with each other so that the rotor blade segments 11, 12 become the structurally integral rotor blade 10.

[0036] For this purpose, in this rotor blade 10, a joint 19 is being formed by multiple bolts 17 and corresponding inserts 18. However, alternatively or additionally to the bolting, the joint 19 may be formed by bonding. To provide the work space at the joint 19 for the joining of the spar sections 15, 16 with each other, the shell portions 13, 14 do not entirely extend over the whole joint 19. Instead, after establishing the joint 19, there is a gap between the shell portions 13, 14. This gap must be closed to avoid aerodynamic disturbances of the rotor blade 10.

[0037] For this purpose, the fairing 20 is provided as shown in the assembly of the rotor blade 10 according to FIG. 2. The fairing 20 closes the gap between the shell portions 13, 14. Thereby, the fairing 20 extends around the joint 19 structurally connecting the spar sections 15, 16.

[0038] In this particular embodiment, the fairing 20 comprises five fairing plates 21, 22, 23, 24, 25. However, the number of fairing plates 21, 22, 23, 24, 25 may alternatively be less or more. These fairing plates 21, 22, 23, 24, 25 consist of a leading edge fairing plate 21 located at a leading edge of the rotor blade 10, a trailing edge fairing plate 22 located at a trailing edge of the rotor blade 10, a suction side fairing plate 24 located at the suction side of the rotor blade 10, a pressure side fairing plate 25 located at the pressure side of the rotor blade 10 and a suction side-trailing edge fairing plate 23 located near the trailing edge and on the suction side of the rotor blade 10.

[0039] Easy access to the joint 19 is possible by simply removing one or more of the fairing plates 21, 22, 23, 24, 25 as required. Further, easy replacement of damaged fairing plates 21, 22, 23, 24, 25 is possible.

[0040] Each one of the fairing plates 21, 22, 23, 24, 25 is attached to both shell portions 13, 14 by means of an adhesive 40 as shown in FIG. 3. FIG. 3 shows a sectional cut through the shell of the assembled rotor blade 10 of FIG. 2 at the location of the fairing 20. The shell is being formed by both shell portions 13, 14 and the fairing 20. Again, the shell portions 13, 14 are only shown partially in this figure.

[0041] From FIG. 3 it can be taken that both shell portions 13, 14 have flange portions 30 facing each other. The flange portions 30 have a step from the outer surface of the shell portions 13, 14. The step is formed into the direction of the joint 19 or inside of the rotor blade 10. Each of these flange portions 30 has a bonding surface 31 and a sealing surface 32. The bonding surface 31 is perpendicular to the sealing surface 32. The fairing 20 is inserted in between the flange portions 30 of the shell portions 13, 14 after the joint 19 has been established.

[0042] In FIG. 3, the cut goes through the shell portions 13, 14 at the location of the suction side fairing plate 24. However, every one of the fairing plates 21, 22, 23, 24, 25 is attached to the shell portions 13, 14 as shown in FIG. 3. That is, adhesive 40 is provided as bonding portions 41 at the bonding surfaces 31 and as sealing portions 42 at the sealing surfaces 32 to provide a low-stiffness bond of the fairing plates 21, 22, 23, 24, 25 to the shell portions 13, 14 and to provide a proper seal in between the fairing plates 21, 22, 23, 24, 25 and the shell portions 13, 14. The adhesive 40 used herein is an elastomeric adhesive and configured to cure at ambient temperature. The bonding portions 41 and the sealing portions 42 may have protuberances to assure a fix thickness of the adhesive 40 for the attachment.

[0043] FIG. 4 shows a side perspective view on a part of an assembly of the rotor blade 10 of FIG. 2 including the fairing 20 with its fairing plates 23 and 22. As can be taken from this perspective particularly well, the trailing edge fairing plate 22 has the sharp trailing edge of the rotor blade 10. In between two opposing sides of this fairing plate 22, a trailing edge reinforcement part 26 in the shape of a wedge is inserted to stabilize the trailing edge of the fairing 20.

[0044] Further, the trailing edge fairing plate 22 has a bonding surface 33 extending towards the adjacent fairing plate 23. In fact, the bonding surface 33 is bonded by means of the adhesive 40 to an underside of the fairing plate 23, whereby the fairing plate 22 is adhered to the fairing plate 23.

[0045] FIG. 5 shows a side perspective view on the part of the assembled rotor blade 10 of FIG. 2. The fairing 20 is attached to both shell portions 13, 14 of the rotor blade segments 11, 12. Indicated are the sealing portions 42 of the adhesive 40 providing a proper seal of the fairing 20 with the shell portions 13, 14 and further a proper seal of the fairing plates 21, 22, 23, 24, 25 with each other.

[0046] Although the present invention has been disclosed in the form of embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.

[0047] For the sake of clarity, it is to be understood that the use of “a” or “an” throughout this application does not exclude a plurality, and “comprising” does not exclude other steps or elements.