• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    wind turbine rotor. the present invention relates to a wind turbine rotor comprising a hub, a plurality of blades and at least one pitch system for rotating a blade substantially along its longitudinal axis, the pitch system comprising a motor, a pinion of drive, a gear arranged to match the drive pinion and a pinion bearing, the pinion bearing comprising an outer bearing ring connected to the hub, an inner bearing ring connected to a blade, and between these two bearing rings. bearing, one or more rows of rotating elements that allow both bearing rings to rotate relative to one another, wherein the inner bearing ring has an inner side, and a reinforcing disc is fixed radially on the inner side of the inner bearing ring.
    公开号:BR112014000600B1
    申请号:R112014000600-8
    申请日:2012-07-12
    公开日:2021-06-22
    发明作者:Pierre Pasquet
    申请人:Ge Renewable Technologies Wind B.V.；
    IPC主号:
    专利说明:

    FIELD OF THE INVENTION
    [001] This application claims the benefit of European Patent Application EP 11382235.7 filed July 13, 2011 and U.S. Provisional Patent Application Serial No. 61/534,028 filed September 13, 2011.
    [002] The present invention relates to wind turbine rotors, and more particularly it relates to wind turbine rotors comprising at least one electromechanical stepping mechanism. The invention further relates to a wind turbine comprising the same and a method of manufacturing a pitch bearing for such wind turbine rotors. BACKGROUND OF THE INVENTION
    [003] Modern wind turbines are commonly used to supply electricity to the grid. Wind turbines generally comprise a rotor with a rotor hub and a plurality of blades. The rotor is set in rotation under the influence of wind on the blades. Rotating the rotor shaft drives the generator rotor either directly ("directly driven") or through the use of a gearbox.
    [004] An important auxiliary system generally provided in wind turbines is the stepping system. Stepping systems are employed to adapt the position of a wind turbine blade to different wind conditions. A pitch system is usually composed of a slewing bearing that comprises an outer ring, an inner ring and, between these two rings, one or more rows of rotating elements, which allow both rings to turn relative to each other.
    [005] In some cases, pitch bearings may further comprise a gear that combines with a drive pinion. When gusts of wind collide with a blade, wind forces can act to substantially bend the blade. Such bending has an effect on the loads transmitted to the bearing. In this way, some of the bearing's rotating elements can support greater loads than others, thus deforming the pitch bearing. The loads acting on the bearing can cause the linear contact and load transmission between the driven gear (crown) and the drive pinion to be displaced from their nominal position and the gear (and bearing) combination of such systems can thus suffer deformations.
    [006] One way to deal with such unevenly distributed loads would be to make the bearing larger in order to increase its rigidity and limit its deformation. However, this would add weight and cost to the project.
    [007] Document US7780417 describes a reinforcement element placed between the rotor blade and the pitch bearing, connected to them through joining means. But this type of solution can be quite complicated and costly.
    [008] Thus, there is still a need to provide a robust electromechanical pitch bearing that reduces its deformations during wind turbine operation and is cost effective. DESCRIPTION OF THE INVENTION
    [009] In a first aspect, a wind turbine rotor is provided, which comprises a hub, a plurality of blades and at least one step system for rotating a blade substantially along its longitudinal axis . The stepping system comprises a motor, a drive pinion, a gear arranged to match the drive pinion, and a step bearing. The pitch bearing comprises an outer bearing ring connected to the hub, an inner bearing ring connected to a blade and, between these two bearing rings, one or more rows of rotating elements which allow both bearing rings to rotate in one direction. in relation to the other, in which the inner bearing ring has an inner side, and in which a reinforcing disc is fixed radially to the inner side of the inner bearing ring.
    [010] According to this aspect, the pitch bearing comprises a reinforcement, which can be fixed radially to the inner side of the inner bearing ring, thus increasing the radial stiffness of the bearing in the bearing ring in which the blade is fixed. At the same time, such a reinforcement increases the rigidity of the link between the blade and the bearing. The rigidity conferred by this reinforcement favors an adequate contact between the rotating elements and paths machined in the bearing rings. The backing disc can thus improve the reliability and durability of an electromechanical pitch bearing.
    [011] In some embodiments, the outer diameter of the backing disk may be slightly larger than an inner diameter of the inner bearing ring such that the backing disk and inner bearing ring can be shrink-fitted. In this way, once assembled, the reinforcement disc and the inner bearing ring cannot be separated, forming a substantially integral part.
    [012] In such a substantially integral part, the reinforcing disc can absorb internal stresses and can transform them into a homogeneous stress distributed over its entire surface. The reinforcement disc can therefore allow for different gear designs without distorting the loads acting on the bearing, that is, preventing bearing deformation.
    [013] In some embodiments, the reinforcing disc may be made of a different material than that of the inner and outer bearing rings, eg a more economical material. The reinforced bearing can thus be cost-effective.
    [014] In some embodiments, the gear may cover substantially the entire inner or outer side of the bearing inner or outer ring. In other cases, it may span a portion of the inner or outer side of the inner ring or the outer ring of the bearing ring. This can substantially reduce the amount of gear material used.
    [015] In some embodiments, the gear or gear portions can be axially bolted to the reinforcing disc. In this way, if necessary, the gear or gear portions can be easily repaired and/or replaced. Furthermore, such axial bolting can be easily accessible from an inner portion of the hub.
    [016] In some embodiments, the step system may further comprise a lubrication system comprising at least one lubricant feeder and/or at least one lubricant collector disposed on the reinforcing disc. In this way, the components of the lubrication system can be disposed within the blade root or hub, which are substantially closed areas. Thus, there is no need for additional coverage or any other means of protection.
    [017] Another aspect relates to a wind turbine comprising a wind turbine rotor substantially as described hereinbefore.
    [018] Another aspect relates to a method of manufacturing a pitch bearing for a wind turbine rotor substantially as described hereinbefore.
    [019] In some embodiments, the method may comprise: • heating the inner bearing ring, • placing the reinforcement disk on the inner side of the inner bearing ring, and • cooling the inner bearing ring with the reinforcement disk disposed on the your insides.
    [020] In others, it may include: • cryogenically treating the backing disc, and • arranging the backing disc on the inner side of the inner bearing ring.
    [021] Additional objects, advantages and characteristics of embodiments of the invention will become apparent to persons skilled in the art upon examination of the description, or may be learned by practicing the invention. BRIEF DESCRIPTION OF THE DRAWINGS
    [022] Particular embodiments of the present invention will be described below by means of non-limiting examples, with reference to the attached drawings, in which: Figures 1 and 2 show two different perspective views of the same embodiment; Figure 3 shows a bottom view of another embodiment; Figure 4 shows a cross-sectional view along line A-A of Figure 2; Figure 5 shows a partial cross section of the embodiment shown in Figure 3; Figures 6a - 6b show another embodiment; Figures 7a - 7b show still other embodiments; and Figure 8 shows a cross section of another embodiment. DESCRIPTION OF ACHIEVEMENTS OF THE INVENTION
    [023] Figure 1 shows a top perspective view of a bearing according to a first modality. Figure 2 shows a bottom perspective view of the same modality.
    [024] The bearing may comprise an outer bearing ring 21, an inner bearing ring 22 having an inner side (reference 222 of Figure 5) and, between these two bearing rings, one or more rows of rotating elements (see also Figures 4 and 5) which can allow both bearing rings to rotate relative to each other. The bearing may further comprise a gear 223 which may be combined with a drive pinion of a drive motor (none of which are shown). Furthermore, a reinforcement ring 23 can be radially fixed to the inner side of the inner bearing ring 22.
    [025] In an alternative embodiment, the reinforcement ring can be a circular disk. In such cases, the disc may comprise a central opening connecting an inner portion of the blade root with an inner portion of the hub.
    [026] Figure 2 shows an embodiment in which gear 223 can cover the entire inner side of inner bearing ring 22. In this embodiment, gear 223 can be machined on the inner face of inner bearing ring 22.
    [027] Figure 3 shows a bottom view of a bearing, where gear 223 can only cover a portion of the inner face of inner bearing ring 22. As shown in Figure 3, gear 223 can be made from a plurality of annular segments 223a - 223d. These segments 223a - 223d can be axially bolted to the reinforcing ring 23 by fastening means such as screws or bolts 230. These bolts 230 can be placed in the portion of the gear having more material, which may be the portion close to the root of each. gear tooth.
    [028] In addition, segments 223a - 223d can be concentric. In some embodiments, segments 223a - 223d may have different arc widths; in others they may be symmetrical.
    [029] In the example of Figure 3, the maximum travel angle for the mechanical mesh between the gear (formed by segments 223a - 223d) and the drive pinion (not shown) can be substantially 110°, which can generally be sufficient for all step effects. On most wind turbines, there is an angle of approximately 90° between the maximum and minimum pitch positions.
    [030] Thus, a gear design as shown in Figure 3 entails economic cost reductions in the amount of gear material used and in terms of repairing or replacing a portion of damaged teeth. The reinforcement ring can guarantee the proper working conditions of the different gear designs, as this allows for a homogeneous distribution of loads, thus avoiding bearing deformation.
    [031] In general, the backing ring 23 can be made of a different material than the inner bearing rings 22 and outer bearing 21. A typical material for the inner and outer bearing ring may be a high-grade steel, for example , 42 CrMo4. The reinforcement ring can be made from a more economical material, such as a high strength low alloy, eg S355 structural steel. The backing ring can be added during the manufacturing process of the inner bearing ring. So this extra part can belong to the bearing as an area of its final geometry.
    [032] Figure 4 shows a cross-sectional view of Figure 2, where the gear 223 can be machined into the inner bearing ring 22. Two rows of rotating elements 23a, 23b can be arranged between the inner bearing rings 22 and external 21 and can allow both bearing rings to rotate relative to each other.
    [033] Figure 5 shows a partial cross-section of Figure 3. This Figure shows a mode in which the gear 223 can be fixed axially to the reinforcement ring 23 by means of fastening means such as screws or bolts 230.
    [034] In general, gear 223 may have a height h in an axial direction that may be less than a height H of the inner bearing ring 22, such that a non-geared portion 224 can be defined on the inner side 222 of the inner bearing ring 22. In this way, the reinforcing ring 23 can be radially fixed to said gearless portion 224.
    [035] Another aspect relates to a method of manufacturing a pitch bearing for a wind turbine rotor substantially as described hereinbefore. The method can be based on shrink fit techniques. In order to carry out said method, an outer diameter of the reinforcing disc can be made slightly larger than an inner diameter of the inner bearing ring. The inner bearing ring can be heated to a temperature at which the inner bearing ring expands. This temperature may vary depending on the material or alloy used for the bearing rings. Then the backing ring can be arranged on the inner side of the inner bearing ring, for example using a press. The contact area at the union between the heated inner bearing ring and the reinforcement ring which is at a lower temperature can reduce the temperature of the inner bearing ring, thus reducing its expanded diameter. The rigidity of the inner bearing ring - joining reinforcement ring may increase as both parts reach the same temperature. Such a union can prevent any relative movement between them. In this way, the final inner bearing ring can have two different materials that are completely interdependent, as if the bearing ring were made from the same blank.
    [036] In alternative embodiments, the reinforcement ring can be cryogenically treated. Since the backing ring is cryogenically treated, the backing ring can be arranged on the inner side of the inner bearing ring which can be preheated or not. Thus, the contact area at the union between the cooled backing ring and the inner side of the inner bearing ring which is at a higher temperature can heat up the backing ring until both parts reach the same temperature. As mentioned earlier, the rigidity of the inner bearing ring - joining reinforcement ring can increase as both parts reach the same temperature. And the final inner bearing ring can feature two different materials that are completely interdependent substantially as explained above.
    [037] In some modalities, such cryogenic treatment of the reinforcement ring can be carried out by means of a nitrogen blanket disposed around the reinforcement ring. Disposition of the cooled backing ring on the inner side of the inner bearing ring can be accomplished using a press.
    [038] Once the backing ring - fitted inner bearing ring has been fabricated, there may be different possibilities for completing the bearing fabrication depending on the gear type.
    [039] If the initial inner bearing ring already comprises a gear machined on its inner side, a final machining of the adjusted inner bearing ring - backing ring can be performed. This final machining can be carried out on the complete inner bearing ring, the gear, the paths and the upper surface of the inner bearing ring with the reinforcement ring, in order to guarantee the leveling of said upper surface. In this way, said upper surface can be used as a mounting surface for a blade root.
    [040] If the initial inner bearing ring does not comprise a gear yet, but the bearing design is such that the gear is provided over the inner bearing ring, then the gear or gear portions can be axially bolted to the bearing ring. reinforcement using fastening means such as pegs (as shown in Figure 5).
    [041] The last step is to assemble the outer bearing ring.
    [042] In these embodiments with a gear provided on the outer bearing ring, the gear can be first mounted or machined on the outer bearing ring and then mounted with a fitted backing ring - inner bearing ring substantially as described above.
    [043] A further aspect of an internal reinforcement disc substantially as described hereinbefore is that it may lead to the possibility of disposing other systems or components, such as lubrication components or step retention system components thereon.
    [044] Figures 6a - 7b show examples of components of a lubrication system arranged on the reinforcement disc.
    [045] Figure 6a shows a wind turbine rotor that may comprise a hub 10 to which a plurality of blades (not shown) may be rotatably connected. A stepping mechanism can be provided to rotate each blade along its longitudinal axis. The pitch mechanism may comprise a pitch bearing 20. The pitch bearing 20 may comprise an outer bearing ring 21 connected to the hub 10 and an inner bearing ring 22 connected to a blade (not shown). Hub 10 may comprise a flange 11 for mounting a drive pinion of a drive motor (not shown). In some embodiments, the flange can form an integral part with the hub. In others it may be a separate piece fixed to the hub by welding or by fastening means such as screws, bolts or the like. In addition, a backing ring 23 can be radially attached to an inner side (reference 222 of Figure 5) of the inner bearing ring 22.
    [046] The reinforcement ring 23 can be provided with through holes 231 arranged axially. The lubricant injectors 32 can be fixed to the reinforcing ring 23, for example, using screws, bolts, clamps or any other suitable fastening means, in combination with said direct hole 231.
    [047] Furthermore, a support device 30 for supporting the lubricating components can be fixed to the reinforcing ring 23 in such a way that the support arrangement 30 traverses a pitch bearing rotation axis 24. The support arrangement 30 may comprise two substantially parallel beams 31. Each beam 31 may be secured to the reinforcing ring 23 by screws, bolts 311 or the like, for example a bolt at each end. In alternative embodiments, the support arrangement may comprise a beam diametrically attached to the reinforcing ring. In still other embodiments, the support arrangement can be attached directly to the inner side of the inner bearing ring.
    [048] Such a support arrangement 30 can support a lubrication pump 40. In some cases, the pump 40 can be mounted on a platform 41 provided on the beams 31. The pump 40 can be arranged such that its center line 42 can run along the axis of rotation of bearing 24, from pump 40 to a front frame 12 on which hub 10 can be rotatably mounted. And from said front structure, the center line can continue towards a general electrical system housed inside the nacelle (not shown). This way, it cannot be affected by a blade pitch movement, ie the centerline will not wrap around other components. Pump 40 can be used, for example, to pump lubricant through lubricant injectors 32 to a supply line, through inlets (not shown) arranged on an inner side (reference 222 of Figure 5) of the inner bearing ring 22 .
    [049] In the embodiment shown in Figure 6a, a lubricant reservoir 43 may still be arranged on the support arrangement 30. In some cases, the lubricant reservoir 43 may be mounted on a platform 44 provided on the beams 31. lubricant 43 can be used, for example, to store old lubricant recovered from inside the bearing. Such lubricant recovery may require a recovery circuit and lubricant extractors (reference 33a in Figure 6b). In alternative embodiments, the lubricant reservoir can form part of the pump set.
    [050] Figure 6b shows a rear view of Figure 6a, in which the hub and flange for mounting the drive pinion have been excluded. In Figure 6b, lubricant injectors 32 and lubricant extractors 33a can be attached to backing ring 23.
    [051] In this way, the components of the lubrication circuit can be arranged inside the blade root, which ensures adequate protection against corrosion. Furthermore, in the case of wind turbines equipped with a temperature and humidity control inside the hub, for example, for cold climates or desert climates, all components housed inside the blade root can still be protected from moisture and of extreme temperatures. These provisions may also be suitable for offshore wind farms as no high salt content or moisture in the air can come into contact with these components disposed within the blade root.
    [052] Figure 7a shows another modality. The main difference from the modality shown in Figures 6a - 6b is that the lubricant extractors and the lubricant reservoir have been replaced by lubricant collectors 33b, such as bottles. Using collectors or bottles is more economical than using extractors, but the manual operation of emptying the bottles can be tricky as each bottle has to be emptied separately.
    [053] Figure 7b shows a rear view of Figure 7a, in which the hub and flange for mounting the drive pinion have been excluded. Backing ring 23 can be provided with a first set of axial through holes (reference 231 of Figure 6a) and a second set of axial through holes 232. Lubricant injectors 32 can be bolted to backing ring 23 via the first set of through holes (reference 231 of Figure 6a) and lubricant or bottle manifolds 33b can be attached to backing ring 23 by the second set of through holes 232. A tube 233 can connect each outlet (not shown) with a manifold. lubricant or bottle (reference 33b of Figure 7a).
    [054] Figure 8 shows the components of a pitch restraint system mounted on the backing ring 23. The pitch restraint system may comprise a cam profile 51 and a cam follower 52. The cam follower 52 may comprise a pressure member 521 and a contact member 524. The pressure member 521 may be arranged to push the contact element 524 towards the cam profile 51 and the cam profile 51 may comprise a local depression (not shown ). Cam follower 52 and cam profile 51 can be arranged in such a way that when the blade is in a pitch position at or below nominal wind speed, contact member 524 can be retained in said local depression. In such cases, the cam profile 51 can be mounted on the backing ring 23 fixed to the inner bearing ring 22. The cam profile can be bolted, glued or welded to the backing ring. In some embodiments, the cam profile can be attached to the bearing ring, for example, by means of an adapter comprising a plurality of holes in order to facilitate its attachment with pins or the like.
    [055] The provision of such a pitch holding system can be beneficial in reducing the wear of the teeth of an electromechanical pitch system by providing a holding torque in the pitch position that is assumed to be equal to or less than the nominal wind speed.
    [056] Although only a number of particular embodiments and examples of the invention have been described herein, it is to be understood by those skilled in the art that other alternative embodiments and/or uses of the invention and obvious and equivalent modifications thereof are possible. Furthermore, the present invention encompasses all possible combinations of the particular embodiments described. Thus, the scope of the present invention is not to be limited by particular embodiments, but is to be determined only by a fair reading of the claims that follow.
    权利要求:
    Claims (15)
    [0001]
    1. WIND TURBINE ROTOR, comprising a hub (10), a plurality of blades and at least one pitch system for rotating a blade along its longitudinal axis, the pitch system comprising a motor, a drive pinion, a gear (223) arranged to match the drive pinion and a pinion bearing, the pinion bearing comprising an outer bearing ring (21) connected to the hub (10), an inner bearing ring (22) connected to a blade and, between the two bearing rings (21, 22), one or more rows of rotating elements (23a; 23b) which allow both bearing rings (21, 22) to rotate with respect to each other, in that the inner bearing ring (22) has an inner side (222); characterized in that a reinforcing disk (23) is fixed radially on the inner side (222) of the inner bearing ring (22).
    [0002]
    2. WIND TURBINE ROTOR according to claim 1, characterized in that an outer diameter of the reinforcing disk (23) is greater than an inner diameter of the inner bearing ring (22) such that the gusset (23) and inner bearing ring (22) can be shrink-fitted.
    [0003]
    3. WIND TURBINE ROTOR according to any one of claims 1 to 2, characterized in that the reinforcement disc (23) is made of a material different from the inner and outer bearing rings (22,21).
    [0004]
    4. WIND TURBINE ROTOR according to any one of claims 1 to 3, characterized in that the reinforcement disc (23) is an annular disc.
    [0005]
    5. WIND TURBINE ROTOR according to any one of claims 1 to 4, characterized in that the gear (223) covers the entire inner side (222) of the inner bearing ring (22) or the entire outer side of the bearing ring external (21).
    [0006]
    6. WIND TURBINE ROTOR according to any one of claims 1 to 4, characterized in that the gear (223) covers a portion of the inner side (222) of the inner bearing ring (22) or a portion of the outer side of the ring outer bearing (21).
    [0007]
    7. WIND TURBINE ROTOR according to any one of claims 5 to 6, characterized in that the gear (223) is made from a plurality of arc segments (223a, 223b).
    [0008]
    8. WIND TURBINE ROTOR according to any one of claims 1 to 7, characterized in that the gear (223) is provided on the inner bearing ring (22) and a height (h) of the gear in an axial direction is less than that a height (H) of the inner bearing ring (22) such that a non-geared portion (224) is defined on the inner side (222) of the inner bearing ring (22) and the reinforcing disc (23) is radially attached to the non-gear portion (224).
    [0009]
    9. WIND TURBINE ROTOR, according to claim 8, characterized in that the gear (223) is axially screwed (230) to the reinforcement disc (23).
    [0010]
    10. WIND TURBINE ROTOR according to any one of claims 1 to 9, characterized in that the step system further comprises a lubrication system comprising at least one lubricant feeder (32) and/or at least one lubricant collector ( 33b) arranged on the reinforcement disc (23).
    [0011]
    11. WIND TURBINE, characterized in that it comprises a wind turbine rotor as defined in any one of claims 1 to 10.
    [0012]
    12. METHOD FOR MANUFACTURING A PITCH BEARING (20) FOR A WIND TURBINE ROTOR, as defined in any one of claims 1 to 10, the method being characterized by comprising: heating the inner bearing ring (22); disposing the backing ring (23) on the inner side of the inner bearing ring (22); and cooling the inner bearing ring (22) with the backing ring (23) disposed within it.
    [0013]
    13. METHOD FOR MANUFACTURING A PITCH BEARING FOR A WIND TURBINE ROTOR, as defined in any one of claims 1 to 10, the method being characterized by comprising: cryogenically treating the reinforcing ring (23); and disposing the backing ring (23) on the inner side of the inner bearing ring (22).
    [0014]
    14. METHOD, according to any one of claims 12 to 13, characterized in that it further comprises the step of final machining or fixing the gear (223) on the reinforcement ring (23) and assembly of the outer bearing ring (21) .
    [0015]
    15. METHOD according to any one of claims 12 to 13, characterized in that it further comprises the step of machining or fixing the gear (223) on the outer bearing ring (21) or mounting the outer bearing ring (21) to the inner bearing ring (22) and backing ring (23).
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    同族专利:
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    US8628301B2|2014-01-14|
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    CN109736973A|2019-01-30|2019-05-10|北京星际荣耀空间科技有限公司|Tank transition rings and propellant tank|
    法律状态:
    2018-03-27| B15K| Others concerning applications: alteration of classification|Ipc: F03D 7/02 (2006.01), B23P 11/00 (2006.01), F03D 1/ |
    2018-05-22| B25D| Requested change of name of applicant approved|Owner name: GENERAL ELECTRIC RENOVABLES ESPANA, S.L. (ES) |
    2018-06-12| B25A| Requested transfer of rights approved|Owner name: GE RENEWABLE TECHNOLOGIES (FR) |
    2018-07-03| B25A| Requested transfer of rights approved|Owner name: GE RENEWABLE TECHNOLOGIES WIND B.V. (NL) |
    2018-12-11| B06F| Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]|
    2020-01-14| B06U| Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]|
    2021-05-18| B09A| Decision: intention to grant [chapter 9.1 patent gazette]|
    2021-06-22| B16A| Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 12/07/2012, OBSERVADAS AS CONDICOES LEGAIS. |
    优先权:
    申请号 | 申请日 | 专利标题
    EP11382235.7A|EP2546512B1|2011-07-13|2011-07-13|Wind turbine rotor|
    EP11382235.7|2011-07-13|
    US201161534028P| true| 2011-09-13|2011-09-13|
    US61/534,028|2011-09-13|
    PCT/EP2012/063653|WO2013007775A1|2011-07-13|2012-07-12|Wind turbine rotor|
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