Wind Turbine Comprising a Yaw Bearing System

Abstract

The invention relates to a wind turbine comprising a plurality of individual yaw bearing units and a method of replacing a pad of such a yaw bearing unit. The yaw bearing unit comprises a calliper structure divided into an upper portion and a lower portion, wherein the lower portion can be dismounted without also dismounting the upper portion. An upper pad is provided between a flange providing support for a nacelle and a mainframe of the nacelle. A radial pad is arranged on a radial surface of the upper portion and contacts a stop element located at either ends of the upper portion. An adjustable lower pad is arranged in a through hole in the lower portion and can be replaced via a lower opening in the lower portion. The radial pad can be replaced in a sideward direction by removing one of the stop elements or replacing it in an axial direction by removing the lower portion.

Claims

1. A wind turbine (1) comprising a wind turbine tower (2), a nacelle (3) with a mainframe (8), a ring gear (10) and a flange (13) provided at the top of the wind turbine tower (2), the ring gear (10) being configured to engage at least one drive unit (12) for yawing the nacelle (3) relative to the wind turbine tower (2), the flange (13) having an upper surface of flange (39), a lower surface of flange (42), and a radial surface of flange (41), the mainframe (8) having a lower surface of mainframe (40) facing the upper surface of the flange (39), wherein the mainframe (8) is slidable supported on the flange (13) by a plurality of individual yaw bearing units (17) arranged relative to each other, each yaw bearing unit (17) comprising a separate calliper structure (19), the calliper structure having an upper portion (20) with an upper surface of upper portion (23) and a lower portion (21) with an upper surface of lower portion (32); the upper portion (20) having a radial surface of upper portion (25) facing the radial surface of the flange (41) and an upper surface of upper portion (23) facing the lower surface of flange (42), wherein at least one upper pad (18) is arranged between the upper surface of flange (39) and the lower surface of mainframe (40), wherein at least one radial pad (26) is arranged between the radial surface of flange (41) and the radial surface of upper portion (25) of the calliper structure (19), the at least one radial pad (26) has a lower edge contacting the upper surface of lower portion (32) and extends along the entire length of the radial surface of upper portion (25) and wherein the yaw bearing unit (17) further comprises at least one removable stop element (27) configured to be mounted to at least one side surface of the upper portion (20).

2. A wind turbine (1) according to claim 1, wherein the upper portion (20) extends in an axial direction and a removable lower portion (21) extends in a radial direction when mounted, wherein the upper portion (20) is configured to be mounted to the mainframe (8) and the lower portion (21) is configured to be mounted to the upper portion (20).

3. A wind turbine (1) according to claim 1, wherein aid lower portion (21) comprises at least one through hole (35) connected to a first opening in the upper surface of lower portion (32) and a second opening in a lower surface of lower portion (36), wherein at least one lower pad (34) is at least partly positioned inside said at least one through hole (35) and is contacting the lower surface of flange (42), the at least one lower pad (34) being accessible via the second opening.

4. A wind turbine (1) according to claim 3, wherein at least one of the lower pads (34) is connected to an adjusting mechanism configured to adjust a pre-tension force of that least one lower pad (34).

5. A wind turbine (1) according to claim 1, wherein said calliper structure (19) comprises at least two rows of mounting elements (22), e.g. mounting holes, for mounting to the mainframe (8).

6. A wind turbine (1) according to claim 3, wherein said calliper structure (19) has a radial distance, L, measured in the radial direction between a centre axis of a lower pad (34) and a centre axis of a mounting element (22), wherein the radial distance is between 80 millimetres and 100 millimetres.

7. A wind turbine (1) according to claim 1, wherein a number of yaw bearing units (17) are distributed along the circumference of the flange (13), the number being between 15 and 25.

8. A wind turbine (1) according to claim 1, wherein said at least one upper pad (18) is formed by a single pad made of thermoplastic polymer, the single pad having at least: a length of 120 millimetres to 500 millimetres, the length being measured along a central arc line, a width of 100 millimetres to 250 millimetres, the width being measured perpendicular to the central arc line, or a thickness of 15 millimetres to 20 millimetres, the thickness being measured perpendicular to the central arc line and the width.

9. (canceled)

10. A method of replacing a pad of a yaw bearing unit (17) of a wind turbine (1), the wind turbine (1) comprising a wind turbine tower (2), a nacelle (3) with a mainframe (8), a ring gear (10) and a flange (13) provided at the top of the wind turbine tower (2), the ring gear (10) being configured to engage at least one drive unit (12) for yawing the nacelle (3) relative to the wind turbine tower (2), the flange (13) having an upper surface of flange (39), a lower surface of flange (42), and a radial surface of flange (41), the mainframe (8) having a lower surface of mainframe (40) facing the upper surface of flange (39), wherein the mainframe (8) is slidable, supported on the flange (13) by a plurality of individual yaw bearing units (17), arranged relative to each other, each yaw bearing unit (17) comprising a separate calliper structure (19) having an upper portion (20) with an upper surface of upper portion (23) and a lower portion (21) with a upper surface of lower portion (32); the upper portion (20) having a radial surface of upper portion (25) facing the radial surface of flange (41), and an upper surface of upper portion (23) facing the lower surface of flange (42), wherein at least one radial pad (26) is arranged between the radial surface of flange (41) and the radial surface of upper portion (25), wherein the method comprises the steps of: dismounting a stop element (27) positioned adjacent to an old radial pad (26), removing the old radial pad (26) by moving said old radial pad (26) in one tangential direction (30) relative to the radial surface of upper portion (25), the tangential direction (30) being perpendicular to a radial direction in a plane defined by the yaw bearing units (17), moving a new radial pad (26) into position by moving the new radial pad (26) in the opposite tangential direction (30) relative to the radial surface of upper portion (25), and remounting the stop element (27).

Description

DESCRIPTION OF THE DRAWING

[0084] An embodiment of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:

[0085] FIG. 1 shows an exemplary wind turbine comprising a yaw bearing system,

[0086] FIG. 2 shows a conventional yaw bearing system,

[0087] FIG. 3 shows an exemplary embodiment of the yaw bearing system according to the invention,

[0088] FIG. 4 shows the calliper structure of two adjacent yaw bearing units,

[0089] FIG. 5 shows a first embodiment of a method for replacing the radial pad according to the invention,

[0090] FIG. 6 shows a second embodiment of the method for replacing the radial pad,

[0091] FIG. 7 shows a method for replacing the lower pad according to the invention,

[0092] FIG. 8 shows a cross-sectional view of a first embodiment of the yaw bearing unit according to the invention, and

[0093] FIG. 9 shows a cross-sectional view of a second embodiment of the yaw bearing unit according to the invention.

[0094] In the following text, the figures will be described one by one, and the different parts and positions seen in the figures will be numbered with the same numbers in the different figures. Not all parts and positions indicated in a specific figure will necessarily be discussed together with that figure.

POSITIVE NUMBER LIST

[0095] 1. Wind turbine [0096] 2. Tower [0097] 3. Nacelle [0098] 4. Rotor [0099] 5. Hub [0100] 6. Wind turbine blades [0101] 7. Yaw bearing system [0102] 8. Mainframe [0103] 9. Calliper structure [0104] 10. Ring gear [0105] 11. Pinion gear [0106] 12. Drive unit [0107] 13. Flange [0108] 14. Upper pad [0109] 15. Radial pad [0110] 16. Lower pad [0111] 17. Yaw bearing units [0112] 18. Upper pad [0113] 19. Calliper structure [0114] 20. Upper portion [0115] 21. Lower portion [0116] 22. Mounting elements [0117] 23. Upper surface of upper portion [0118] 24. Track [0119] 25. Radial surface of upper portion [0120] 26. Radial pad [0121] 27. Stop elements [0122] 28. Side surface of calliper structure [0123] 29. Rebate [0124] 30. Tangential direction [0125] 31. Projecting element [0126] 32. Upper surface of lower portion [0127] 33. Axial direction [0128] 34. Lower pads [0129] 35. Through holes [0130] 36. Lower surface of lower portion [0131] 37. Adjusting mechanism [0132] 38. Adjustable element [0133] 39. Upper surface of flange [0134] 40. Lower surface of mainframe [0135] 41. Radial surface of flange [0136] 42. Lower surface of flange [0137] 43. Support element [0138] 44. Shaft element [0139] 45. Spring element

DETAILED DESCRIPTION OF THE INVENTION

[0140] FIG. 1 shows an exemplary embodiment of a wind turbine 1, according to the invention, comprising a wind turbine tower 2 arranged on a foundation. The foundation is here shown as an onshore foundation, but also an offshore foundation may be used. A nacelle 3 is arranged on the wind turbine tower 2 via a yaw bearing system (shown in FIGS. 2 and 3). A rotor 4 is rotatably arranged relative to the nacelle 3 and comprises a hub 5 mounted to at least two wind turbine blades 6, e.g. via a pitch bearing system.

[0141] The wind turbine blades 6 are here shown as full-span wind turbine blades, but also partial-pitchable wind turbine blades may be used. The partial-pitchable wind turbine blade comprises an inner blade section and an outer blade section, wherein the pitch bearing system is arranged between the two blade sections.

[0142] FIG. 2 shows a conventional yaw bearing system 7 arranged between the wind turbine tower 2 and the nacelle 3. Here, only a part of a mainframe 8 of the nacelle 3 is shown for illustrative purposes. The mainframe 8 is connected to a U-shaped calliper structure 9 which forms two radial extending legs facing the wind turbine tower 2. The calliper structure 9 is here shown as part of the mainframe 8, however, the calliper structure 9 may be a separate structure mounted to the lower surface of the mainframe 8.

[0143] The wind turbine tower 2 is mounted to a ring gear 10 having a plurality of teeth configured to engage a plurality of complementary teeth of a pinion gear 11 which is rotatably connected to a drive unit 12, e.g. a yaw motor. Here, two sets of drive units 12 and pinion gears 11 are shown. The ring gear 10 further comprises a flange 13 extending in a radial direction. The flange 13 is situated between the radial extending legs of the calliper structure 9. An upper pad 14, a radial pad 15, and a lower pad 16 are arranged on the calliper structure 9 and are facing the flange 13 as shown in FIG. 2. The calliper structure 9 is able to slide along the outer surfaces of the flange via the respective pads 14, 15, 16.

[0144] FIG. 3 shows an exemplary embodiment of the yaw bearing system, according to the invention, comprising a plurality of individual yaw bearing units 17 distributed along the circumference of the flange 13. Here, the engaging teeth are arranged on the outer side of the ring gear 10 while the flange is extending inwards towards a centre axis of the wind turbine tower 2.

[0145] Each yaw bearing unit 17 is configured as a separate unit which is spaced apart from an adjacent yaw bearing unit 17. Each yaw bearing unit 17 comprises an upper pad 18 arranged relative to the flange 13.

[0146] A predetermined number of yaw bearing units 17 are distributed along the circumference of the flange 13. Here, twenty yaw bearing units 17 are shown, however, this number may be increased or reduced depending on the desired application. This reduces the tilting moment and the axial force acting on each yaw bearing unit, and reduces the weight and costs of each yaw bearing unit.

[0147] FIG. 4 shows the calliper structure 19 of two adjacent yaw bearing units 17 wherein each calliper structure 19 has an L-shaped structure. The calliper structure 19 is divided into an upper portion 20 extending in an axial direction and a lower portion 21 extending in a radial direction. The lower and upper portions 20, 21 comprise a first set of mounting elements 22, here four is shown, in the form of mounting holes for receiving separate fastener elements, such as bolts, (shown in FIGS. 8 and 9). The mounting elements 22 extend from an upper surface 23 of the upper portion 20 to a lower surface of the lower surface of the lower portion 21. The upper portion 20 further comprises a second set of mounting elements 22 for receiving another set of fastener elements.

[0148] At least one track 24 is optionally arranged on the upper surface 23, wherein this track 24 extends along the length of the respective yaw bearing unit 17. The mainframe 8 optionally comprises at least one complementary recess for receiving the track 24 as shown in FIGS. 8 and 9. The track 24 and complementary recess are used to position the individual yaw bearing units 17 correctly relative to the flange 13, and they also prevent the yaw bearing units 17 from moving in a radial direction.

[0149] The calliper structure 19, e.g. the upper portion 20, has a radial surface 25 facing the flange 13 as shown in FIGS. 8 and 9. A rebate and a projecting elongated element are formed in the radial surface 25 as shown in FIGS. 5 and 6. A radial pad 26 is arranged in the rebate as shown in FIG. 4. A pair of stop elements 27 is arranged on opposite sides of the radial pad 26. The stop elements 27 are removable stop elements mounted to a side surface 28 of the calliper structure 19, e.g. the upper portion. This prevents the radial pad 26 from moving in a circumference direction during yawing.

[0150] FIG. 5 shows a first embodiment of a method for replacing the radial pad 26, wherein the radial pad 26 is accessed from a sideward or tangential direction. In event that replacement is required, e.g. due to wear or other conditions, one of the stop elements 27 is demounted and removed. The old radial pad 26 is then pulled out of the rebate 29 in the tangential direction (indicated by arrow 30). A new radial pad 26 is pushed into the rebate 29 in the opposite direction until it reaches contact with the other stop element 27. The stop element 27 is then repositioned and remounted to the calliper structure 19. This allows for a simple and quick replacement of the radial pad without having to remove the calliper structure first.

[0151] As clearly shown in FIGS. 5 and 6, the rebate 29 extends along the entire length of the radial surface 25. The rebate 29 further extends from the projecting element 31 to the lowermost edge of the upper portion 20 in the axial direction. The radial pad 26 contacts the projecting element 31, the stop elements 27, and the upper surface 32 of the lower portion 21 as clearly indicated in FIG. 4. This increases the total surface area of radial pad 26, which, in turn, reduces the edge pressure applied to the stop elements 27.

[0152] FIG. 6 shows a second embodiment of the method for replacing the radial pad 26, wherein the radial pad 26 is accessed from the axial direction. In the event that replacement is required, e.g. due to wear or other conditions, the lower portion 21 of the calliper structure 19 is demounted and removed. The old radial pad 26 is then pulled out of the rebate 29 in the axial direction (indicated by arrow 33). A new radial pad 26 is pushed into the rebate 29 in the opposite direction until it reaches contact with the projecting element 31. The lower portion 21 is repositioned and remounted to the upper portion 20 of the calliper structure 19. This also allows for a simple and quick replacement of the radial pad as only part of the calliper structure has to be removed first.

[0153] FIG. 7 shows a method for replacing the lower pad 34, wherein the lower pad 34 is accessed via an opening in a lower surface of the lower portion. The lower portion 21 comprises a number of through holes 35 in which the individual lower pads 34 are at least partly arranged. The through holes 35 extend from the upper surface 32 to the lower surface 36 of the lower portion 21. The lower pad 34 is connected to an adjusting mechanism 37 configured to adjust the pre-tension force of the lower pad 34 as indicated in FIGS. 8 and 9. The adjusting mechanism 37 comprises an adjustable element 38 in the form of a bolt head. The adjusting mechanism 37 is arranged in the through hole 35 and can be engaged by an external tool from the bottom side of the calliper structure 19.

[0154] In the event that replacement is required, e.g. due to wear or other conditions, the adjustable element 38 is demounted and removed. The remaining parts of the adjusting mechanism 37 and the old lower pad 34 are then removed via the opening (shown in FIGS. 8 and 9) in the lower surface 36. The old lower pad 34 is removed from a support element (shown in FIGS. 8 and 9) of the adjusting mechanism 37 and a new lower pad 34 is placed on the support element, e.g. using an adhesive. The new lower pad 34 and the above-mentioned remaining part are then repositioned inside the through hole 35 via the opening in the lower surface 36. Finally, the adjustable element 38 is repositioned and remounted to the lower portion 21. This enables the lower pad 34 to be replaced without having to remove the calliper structure first.

[0155] FIGS. 8 and 9 show a cross-sectional view of a first and a second embodiment of the yaw bearing unit 17, wherein the upper pad 18 is arranged in a recess (not shown) in the upper surface 39 of the flange 13. Further, the upper pad 18 is in slidable contact with a lower surface 40 of the mainframe 8. The radial pad 26 is in slidable contact with a radial surface 41 of the flange 13. The lower pad 34 is in slidable contact with a lower surface 42 of the flange 13.

[0156] The upper pad 18 is formed as a single continuous pad made of thermoplastic polymer having an optimal length, width, and thickness. Test results have shown that an optimal balance between the edge pressure of the upper pad 18 and the shape of the upper pad 18 is achieved when the upper pad 18 has a length of 120 millimetres to 500 millimetres, a width of 100 millimetres to 250 millimetres, and a thickness of 15 millimetres to 20 millimetres.

[0157] The adjusting mechanism 37 has a support element 43 on which the lower pad 34 is situated. The support element 43 is further connected to a shaft element 44 configured to contact the adjustable element 38 and thus limit the downwards axial movement of the lower pad 34. A spring element 45 is arranged between the support element 43 and the adjustable element 38 and is configured to bias the downwards axial movement of the lower pad 34.

[0158] The mounting elements 22 in the calliper structure 19 may be arranged in one row as shown in FIGS. 4 and 8. The yaw bearing unit 17 has a distance, L, measured in the radial direction between a centre axis of one lower pad 34 and a centre axis of one mounting element 22. This distance L defines a moment arm (indicated by arrow F in FIG. 9) for transferring tilting moments from the nacelle 3 to the wind turbine tower 2 via the flange 13.

[0159] The mounting elements 22 may advantageously be arranged in two rows as shown in FIGS. 3 and 9. The distance L to an adjacent mounting element 22 is then reduced to a range of 80 millimetres to 100 millimetres. This configuration enables the eccentricity and the individual bolt forces to be reduced which, in turn, enable the width of the yaw bearing unit 17 and the width of the flange 13 to be reduced.