A wind turbine pitch bearing, and use hereof

Background of the invention

0001The invention relates to a wind turbine according to the preamble of claim 1, and use hereof.

Description of the Related Art

0002A wind turbine known in the art comprises a wind turbine tower and a wind turbine nacelle positioned on top of the tower. A wind turbine rotor with three wind turbine blades is connected to the nacelle through a low speed shaft, which extends out of the nacelle front as illustrated on <figref idref="f0001">figure 1</figref>.

0003Modem wind turbines control the load on the rotor by pitching the blades in and out of the incoming wind. The blades are pitched to optimize the output or to protect the wind turbine from damaging overloads.

0004To perform the pitch each blade is provided with a pitch bearing between the hub and the blade, and some sort of mechanism, most often a hydraulic cylinder, to provide the force for pitching the blade and maintaining it in a given position. This pitching arrangement enables each blade to be turned approximately 90° around their longitudinal axis.

0005The wind load on the blades get bigger as modem wind turbines get bigger, and as both blades and hub get bigger the more relatively soft and flexible they get. These facts make the pitch bearings very crucial components of the rotor, in that they have to be able to transfer the moment produced by the wind load to the hub and at the same time enable that the blades can rotate freely and accurately.

0006To ensure this the obvious solution would be simply to make the pitch bearings bigger, but the bearing balls has already almost reached the limit of what is industrially available, and bigger balls would therefore be economically disadvantageous. Furthermore, the ring size would increase with increased ball size and thereby increase the bearing cost and weight significantly.

0007Another solution would be to provide the blade with more than one bearing spaced apart as shown in e.g. <patcit id="pcit0001" dnum="DE3415428A1"><text>DE 3415428 A1</text></patcit> and <patcit id="pcit0002" dnum="US4668109A"><text>US 4,668,109</text></patcit>. This is advantageous in that it enables relatively small bearings to transfer the moment. But this design is space consuming and requires a high degree of rigidity and thereby increased cost and weight of both the hub and the blades.

0008<patcit id="pcit0003" dnum="SE416990B"><text>SE416990 (B</text></patcit>) describes a journaling yoke for a wind turbine adapted to journal the wind catching blades of the turbine to its hub in a movable manner. <patcit id="pcit0004" dnum="US4668109A"><text>US4668109A</text></patcit> describes a journal with spring loaded bearings for a wind turbine.

0009An object of the invention is therefore to provide a large modem wind turbine pitch bearing without the mentioned disadvantages.

0010Especially it is an object of the invention to provide for a cost and weight efficient wind turbine pitch bearing which can transfer the loads on and from the blades to the hub without reducing the bearings durability or functionality.

The invention

0011The invention provides for a wind turbine comprising at least two pitch controlled wind turbine blades. Each blade comprising one or more pitch bearings including two or more bearing rings, and pitch controlling means for pitching the blades by means of the bearings. The blades being mounted on a hub via the pitch bearings, the one or more pitch bearings comprise separate flexibility enhancing means for controlling loads in the bearings, characterized in that the separate flexibility enhancing means include one or more plates attached to one or more of said bearing rings by means of e.g. screws, bolts, studs, rivets, adhesive means or welding, wherein at least one of said one or more plates is a strengthening plate providing additional circumferential non-uniform rigidity to said bearing ring on which it is attached.

0012It is advantageous to provide the pitch bearings with separate flexibility enhancing means, in that the flexibility enhancing means ensures the durability or functionality of the bearing even though the bearing rings are distorted by the load on and from the blades. Hereby the bearings can transfer a bigger moment or load without the weight or the cost of the bearing being raised much.

0013It should be emphasised that the term "hub" is to be understood as the part of the wind turbine to which the blades are attached. The term "hub" therefore also covers the teetering device to which the blades are attached on teeter wind turbines.

0014In an aspect of the invention, said bearings comprise two rows of rolling elements.

0015The more rows of rolling elements the more sensitive the bearings life and functionality are to a distortion of the bearing rings. It is therefore advantageous to provide a bearing comprising two rows of rolling elements with separate flexibility enhancing means.

0016It should be emphasised that the term "rolling elements" is to be understood as any form of rolling parts of a bearing such as balls, rollers, needles or other.

0017In an aspect of the invention, said bearings comprise three or more rows of rolling elements.

0018Hereby is achieved an advantageous embodiment of the invention.

0019In an aspect of the invention, said bearings comprise one or more first and one or more second separate flexibility enhancing means.

0020By providing the bearings with both a first and a second separate flexibility enhancing means the bearing becomes more flexible. This is advantageous in that it that it ensures the durability or functionality of the bearing even though the bearing rings are distorted.

0021In an aspect of the invention, said separate flexibility enhancing means are displaced from the load transferring surfaces of said bearing rings.

0022It is advantageous to position the separate flexibility enhancing means away from the surfaces of the bearing rings on which the rolling elements roll in that it enables a more simple design of the separate flexibility enhancing means and it enables the flexibility enhancing means to provide the bearing with more flexibility.

0023In an aspect of the invention, at least one of said one or more bearing rings comprise through holes for blade attachment means such as screws, bolts, studs or rivets.

0024It is advantageous that one or more of the bearing rings comprise through holes in that it enables a simple way of attaching the bearing.

0025In an aspect of the invention, said bearings comprise three bearing rings.

0026Bearings comprising three bearing rings always comprise at least two rows of rolling elements. The more rows of rolling elements the more sensitive the bearings durability and functionality are to a distortion of the bearing rings. It is therefore advantageous to provide a bearing comprising three bearing rings with separate flexibility enhancing means.

0027By providing the bearing rings with one or more plates it is possible to control the bearing rings rigidity and thereby ensure that even though the rings are distorted the bearing still have its full functionality and no part of the bearing are damaged or get excessively strained.

0028By making the plates so that they provide non-uniform rigidity to the bearing ring on which they are attached, the plates can provide the bearings with rigidity and/or flexibility where it is needed, without increasing the bearings weight much.

0029In an aspect of the invention, said additional non-uniform or substantially nonuniform rigidity is provided by means of one or more holes in said strengthening plates.

0030It is advantageous to provide the plates with one or more holes, in that it is a simple and efficient way of controlling the plates rigidity and/or flexibility

0031The invention further provides for use of wind turbine according to any of claims 1 to 26, wherein said wind turbine is a variable speed pitch wind turbine.

Figures

0032The invention will be described in the following with reference to the figures in which <dl id="dl0001"><dt>fig. 1.</dt><dd>illustrates a large modem wind turbine as seen from the front,</dd><dt>fig. 2</dt><dd>illustrates a cross section of a wind turbine hub connected to a hub through a pitch bearing comprising plates,</dd><dt>fig. 3</dt><dd>illustrates the same embodiment of a pitch bearing as illustrated in <figref idref="f0002">fig. 2</figref> as seen from the top,</dd><dt>fig. 4</dt><dd>illustrates a part of a cross section of a pitch bearing comprising three rows of rolling elements,</dd><dt>fig. 5</dt><dd>illustrates a part of a cross section of a pitch bearing comprising six rows of rolling elements,</dd><dt>fig. 6</dt><dd>illustrates a part of a cross section of a pitch bearing comprising angle compensating means,</dd><dt>fig. 7</dt><dd>illustrates the same embodiment of a pitch bearing as illustrated in <figref idref="f0004">fig. 6</figref> as seen from the top,</dd><dt>fig. 8</dt><dd>illustrates an embodiment of a hollow roller as seen from the front and the side,</dd><dt>fig. 9</dt><dd>illustrates an embodiment of a rounded roller as seen from the front and the side,</dd><dt>fig. 10</dt><dd>illustrates a part of a cross section of a pitch bearing comprising rollers,</dd><dt>fig. 11</dt><dd>illustrates a part of a cross section of another pitch bearing comprising rollers,</dd><dt>fig. 12</dt><dd>illustrates an embodiment of rolling element cages and separate compression parts,</dd><dt>fig. 13</dt><dd>illustrates an embodiment of rolling element cages comprising compression zones,</dd><dt>fig. 14</dt><dd>illustrates the same embodiment of rolling element cages as illustrated in <figref idref="f0006">fig. 13</figref> in a compressed state, and</dd><dt>fig. 15</dt><dd>illustrates a part of a cross section of a pitch bearing comprising rolling element cages.</dd></dl>

Detailed description

0033<figref idref="f0001">Fig. 1</figref> illustrates a wind turbine 1, comprising a tower 2 and a wind turbine nacelle 3 positioned on top of the tower 2. The wind turbine rotor 4, comprising two wind turbine blades 5, is connected to the nacelle 3 through the low speed shaft which extends out of the nacelle 3 front.

0034<figref idref="f0002">Fig. 2</figref> illustrates a cross section of a wind turbine blade 5 connected to a hub 7 through an embodiment of a pitch bearing 9. In this embodiment the pitch bearing 9 is a triple row 27 ball bearing, but it could also be a double or four rowed 27 bearing.

0035The pitch bearing has to transfer forces mainly from three different sources. The blade 5 (and the bearings 9 themselves off cause) is under constant influence of the force of gravitation. The direction of the gravitational force varies depending on the blades 5 position, inducing different loads on the pitch bearings 9. When the blade is in motion the bearing 9 is also under influence of a centrifugal force, which mainly produces an axial pull in the bearing 9. Finally the bearings 9 are under influence of the wind load on the blades 5. This force is by far the greatest load on the bearings 9 and it produces a massive moment, which the bearings 9 have to stand.

0036Since the pitch mechanism on traditional pitch wind turbine 1 usually can pitch the blade 5 a little over 90°, the load on the pitch bearings 9 is far from uniform under normal operation. The wind load on the blade 5 will make the blade 5 pull in the part of the inner ring 26 of the bearing 9 facing the wind and push on the part of the inner ring 26 facing away from the wind. When the inner ring 26 is pulled forcefully by the blade 5 the balls are pushed outwards and upwards in an angle of approximately 45° as indicated by the arrows. This force will result in an axial pull in the outer ring 24 and a radial push on the outer ring 24. Since the bottom of the outer ring 24 is fixed against the hub 7, the top of the ring 24 will have a tendency to deflect. Likewise will the inner ring 26 have a tendency to deflect at the bottom, since it is fixed against the blade at the top. If this deflection becomes too big, one or more of the rows 27 will be unable to transfer the loads, which could lead to a damaging load on the remaining balls. Because of the direction of the forces this problem is most pronounced at the part of the bearing facing the wind. This deflection could be reduced by making the rings thicker and therefore more rigid, but this would increase the cost and the weight of the bearing significantly.

0037Multi-rowed ball bearings are relatively cheap due to the well proven and relatively simple design, but they have the disadvantage of being relatively high in relation to the width, making them relatively poor regarding the transfer of large moment forces.

0038<figref idref="f0002">Fig. 2</figref> therefore illustrates that the free end of the outer ring 24 is provided with an outer plate 10. The outer plate 10 is fixed to the outer ring 24 and thereby enables the possibility of providing the outer ring 24 with rigidity where it is needed. Likewise, the inner ring 26 is provided with an inner plate 11. To ensure flexibility of the inner plate 11 in the right places, the plate 11 is provided with a hole 8, allowing for the inner ring 26 to deflect a little at the bottom to compensate for a little deflection at the top of the outer ring 24, and thereby ensuring a constant distance between the two rings 24, 26 and a substantially identically load on all the rows 27 of balls 13.

0039<figref idref="f0002">Fig. 3</figref> illustrates the same embodiment of a pitch bearing as illustrated in <figref idref="f0002">fig. 2</figref> as seen from the top. In this embodiment of the invention the outer plate 10 is shaped as an annular semicircular ring with increased width towards the middle of the semicircle. This design ensures most rigidity where the deflection of the outer ring 24 is biggest. In this embodiment of the invention the outer plate 10 covers approximately 180° of the outer ring 24 but in another embodiment the outer plate could cover more or less of the outer ring 24 or it could be formed as a full 360° annular ring. In another embodiment of the invention the outer plate 10 could also be of constant width.

0040<figref idref="f0002">Fig. 3</figref> also illustrates that the inner plate 11 is provided with a plate hole 8 shaped as an ellipse. The hole 8 is also placed near the part of the bearing 9 where the load on the outer ring 24 is biggest. In another embodiment of the invention the hole 8 could have another shape such as circular, polygonal or the flexibility could be provided by means of a number of strategically placed holes 8.

0041<figref idref="f0003">Fig. 4</figref> illustrates a part of a cross section of a pitch bearing 9 comprising three rows 27 of rolling elements 13. In this embodiment of the invention the pitch bearing 9 comprise an outer bearing ring 24 and an inner bearing ring 26. The figure further illustrates that the bearing 9 comprise three rows 27 of balls 13. The three rows of rolling elements 13 have the same diameter as illustrated by d1.

0042<figref idref="f0003">Fig. 5</figref> illustrates a part of a cross section of a pitch bearing 9 comprising two columns of each three rows 27 of rolling elements 13. Between the outer bearing ring 24 and the centre bearing ring 25 is positioned three rows 27 of balls 13 on the same diameter d2. Between the centre bearing ring 25 and the inner bearing ring 26 is positioned three other rows 27 of rolling elements 13 on a common diameter d1, which is different from d2.

0043<figref idref="f0004">Fig. 6</figref> illustrates a part of a cross section of a pitch bearing 9 comprising angle compensating means 14. On an ordinary bearing 9 of this type the top and/or the bottom row 27 of rollers 13 would press against the middle section during normal operation. To ensure long life of the rollers 13 and the bearing 9, the transferred load has to be distributed evenly over the entire roller surface. This could be ensured if the rings were made very strong and rigid, but this would also mean a significant increase in cost and weight.

0044<figref idref="f0004">Fig. 6</figref> therefore illustrates that the bearing 9 is provided with angle compensating means 10 in form of two separate rings provided with a plan surface 16 facing the rollers 13 and a semicircular surface 15 facing the middle section 29. In another embodiment the plane surface 16 could be provided with a groove, in which the rollers 13 would roll and/or the semicircular surface 15 could be formed as a plane surface with more or less rounded corners.

0045The angle compensating means 10 could be made of hardened steel, but it would still be so flexible, that it can twist a little to compensate for any angle differences between the roller surface and the opposing surface on the middle section 29.

0046<figref idref="f0004">Fig. 7</figref> illustrates the same embodiment of a pitch bearing as illustrated in <figref idref="f0004">fig. 6</figref> as seen from the top. The angle compensating mean 10 is illustrated in dotted lines as one full 360° ring. In another embodiment the angle compensating mean 10 could be made of several individual or joined ring parts e.g. to lower the production costs.

0047<figref idref="f0005">Fig. 8</figref> illustrates an embodiment of a hollow roller 12 as seen from the front and the side. The rollers 13 in roller bearings 9 as the ones illustrated in <figref idref="f0003">fig. 4</figref>, <figref idref="f0005">8 and 9</figref> are all very sensitive to angle differences between the different rings 24, 25, 26. If one of the rings 24, 25, 26 is under the influence of a heavy load, the design of the bearings 9 could result in such an angle difference, if the rings 24, 25, 26 are not strong and rigid enough. To ensure that the rollers 13 are not damaged by such an angle difference the rollers 13 could be provided with a hole 22 in the middle, providing it with that much flexibility that the roller 12 is not damaged even though the load on it is not evenly distributed.

0048In this embodiment the hole 22 is bigger near the ends of the roller 12, to ensure most flexibility where it is most needed, but in another embodiment of the invention the hole could be straight or the flexibility could be provided by a blind hole in one or each end of the roller 12.

0049<figref idref="f0005">Fig. 9</figref> illustrates an embodiment of a rounded roller 28 as seen from the front and the side. As explained above angle differences between the bearing rings 24, 25, 26 can damage the rollers 13 or reduce their life. To provide the bearings 9 with the flexibility enabling it to handle distortion of the bearing rings 24, 25, 26 the rollers 13 could also be provided with a curved roller surface either by making it bulge or by rounding 17 the two edges.

0050<figref idref="f0005">Fig. 10 and fig. 11</figref> illustrates parts of cross sections of two different embodiments of pitch bearings 9. In these bearings 9 no angle compensating means are provided, so if the bearing rings 24, 25, 26 are distorted by the loads on and/or from the blades 5, the rollers or their respective opposing contact surfaces could be damaged. In these types of bearings flexibility enhancing means such as angle compensating means 14, inner and/or outer plates 10, 11, hollow rollers 12, rounded rollers 28 or any combination thereof would enable the bearings 9 to transfer a much greater load than otherwise possible without significantly increasing the cost or the weight of the bearings.

0051<figref idref="f0006">Fig. 12</figref> illustrates an embodiment of rolling element cages 19. To ensure that the rolling elements 13 of the pitch bearing 9 are separated and stay in place, the rolling elements 13 are provided with rolling element cages 19. This could be a single 360° cage ensuring a constant distance between all the rolling elements 13, but if one or more bearing rings 24, 25, 26 are distorted, a force could arise forcing one or more rolling elements 13 apart. If the rolling elements 13 mutual distance is fixed, this force could potentially damage the rolling elements 13 or their corresponding contact surfaces on the bearing rings 24, 25, 26. As illustrated in <figref idref="f0006">fig. 12</figref> the rolling element cages 19 could be divided into a number of separate cages 19 kept apart by compression parts 6. The compression parts 6 can be compressed and thereby absorbing some or the separating forces. The compression parts 6 could e.g. be rubber blocks, metal springs or other elastical devices or materials.

0052In this embodiment each cage 19 contains 4 balls but in another embodiment of the invention the cage 19 could contain two, three, five, six or more balls or rollers 13.

0053<figref idref="f0006">Fig. 13</figref> illustrates another embodiment of rolling element cages 19. In this embodiment each cage 19 comprise a compression zone 20, in form of a transverse slit 21 formed integrally in the cage 19. The cages 19 could be made from some sort of steel plate which then could be flame or laser cut into the desired shape.

0054<figref idref="f0006">Fig. 14</figref> illustrates the same embodiment of rolling element cages 19 as illustrated in <figref idref="f0006">fig. 13</figref> in a compressed state.

0055<figref idref="f0007">Fig. 15</figref> illustrates a part of a cross section of an embodiment of a pitch bearing 9 comprising rolling element cages 19.

0056The invention has been exemplified above with reference to specific examples of separate flexibility enhancing means in pitch bearings 9 for a wind turbine 1. However, it should be understood that the invention is not limited to the particular examples described above but may be designed and altered in a multitude of varieties within the scope of the invention as specified in the claims.

List

0057<ul id="ul0001" list-style="none" compact="compact"><li>1. Wind turbine</li><li>2. Tower</li><li>3. Nacelle</li><li>4. Rotor</li><li>5. Blade</li><li>6. Compression part</li><li>7. Hub</li><li>8. Plate hole</li><li>9. Pitch bearing</li><li>10. Outer plate</li><li>11. Inner plate</li><li>12. Hollow roller</li><li>13. Rolling elements</li><li>14. Angle compensating mean</li><li>15. Semicircular contact surface</li><li>16. Plane roller surface</li><li>17. Rounding</li><li>18. Through hole</li><li>19. Rolling element cage</li><li>20. Compression zone</li><li>21. Transverse slit</li><li>22. Roller hole</li><li>23. Rolling element bed</li><li>24. Outer ring</li><li>25. Centre ring</li><li>26. Inner ring</li><li>27. Rolling element row</li><li>28. Rounded roller</li><li>29. Middle section</li><li>d1. Common diameter of rows of rolling elements</li><li>d2. Common diameter of other rows of rolling elements</li></ul>