Compound main bearing arrangement for a wind turbine

Abstract

A drive train of a wind turbine is disclosed as having a rotatable hub, a gearbox, a rotatable rotor shaft extending between the rotatable hub and the gearbox, and a main bearing assembly supporting the rotatable rotor shaft, the main bearing assembly having a main bearing housing enclosing one or more compound bearings, each of the one or more compound bearings having at least two axial thrust bearings and a radial bearing.

Claims

1. A drive train of a wind turbine, the drive train comprising: a rotatable hub; a gearbox; a rotatable rotor shaft extending between the rotatable hub and the gearbox; and, a main bearing assembly supporting the rotatable rotor shaft, the main bearing assembly comprising a shaft flange and a main bearing housing enclosing one or more compound bearings, each of the one or more compound bearings comprising at least two axial thrust bearings, a radial bearing, and rotatable raceway components disposed adjacent the at least two axial thrust bearings and the radial bearing and configured as inner radial and axial exterior raceway surfaces, the shaft flange being attached to the rotatable raceway components and comprising a removable retainer flange configured to retain the one or more compound bearings.

2. The drive train of claim 1, wherein the main bearing assembly is coupled to a main bearing pedestal extending from a main frame.

3. The drive train of claim 1, wherein the one or more compound bearings further comprise; a radial bearing pad disposed circumferentially around at least a portion of an inner surface of a fixed raceway annulus, and, at least two axial thrust bearing pads disposed circumferentially around the rotatable rotor shaft on opposing sides of the fixed raceway annulus.

4. The drive train of claim 3, wherein the rotatable rotor shaft is removably coupled to the rotatable hub at the shaft flange.

5. The drive train of claim 4, wherein the at least two axial thrust bearings and the radial bearings comprises at least one of roller bearings, journal bearings, ball bearings or combinations thereof.

6. The drive train of claim 5, wherein the journal bearings comprise at least one of hydrostatic bearings, hydrodynamic bearings, or combinations thereof.

7. The drive train of claim 6, wherein the radial bearing comprises rolling elements and the at least two axial thrust bearings comprises journal bearings.

8. The drivetrain of claim 7, wherein each of the at least two axial thrust bearings comprise at least one tilting pad arranged therewith so as to enable a tilting movement in a least one direction of rotation of the at least two axial thrust bearings.

9. The drive train of claim 8, further comprising a lubricating mechanism, the lubricating mechanism comprising at least one fluid supply groove disposed in the fixed raceway annulus and at least one fluid supply hole configured through the fixed raceway annulus.

10. A wind turbine, comprising: a tower; a nacelle mounted atop the tower; a generator and bearing pedestal coupled to a main frame within the nacelle; a gearbox coupled to the generator via a generator shaft; a rotatable hub; a rotatable rotor shaft extending between the rotatable hub and the gearbox; and, a main bearing assembly coupled with the bearing pedestal and supporting the rotatable rotor shaft, the main bearing assembly comprising a fluted portion and a main bearing housing enclosing one or more compound bearings, each of the one or more compound bearings comprising at least two axial thrust bearings, a radial bearing, and rotatable raceway components disposed adjacent the at least two axial thrust bearings and the radial bearing and configured as inner radial and axial exterior raceway surfaces, the fluted portion being attached to the rotatable raceway components and comprising a removable retainer flange configured to retain the one or more compound bearings.

11. The wind turbine of claim 10, wherein the one or more compound bearings further comprise; a radial bearing pad disposed circumferentially around at least a portion of an inner surface of a fixed raceway annulus, and, at least two axial thrust bearing pads disposed circumferentially around the rotatable rotor shaft on opposing sides of the fixed raceway annulus.

12. The wind turbine of claim 11, wherein the rotatable rotor shaft is removably coupled to the rotatable hub at the shaft flange.

13. The wind turbine of claim 12, wherein the at least two axial thrust bearings and the radial bearing comprise at least one of roller bearings, journal bearings, ball bearings or combinations thereof.

14. The wind turbine of claim 13, wherein the radial bearing comprises rolling elements and the at least two axial thrust bearings comprises journal bearings.

15. The wind turbine of claim 14, wherein each of the at least two axial thrust bearings comprise at least one tilting pad arranged therewith so as to enable a tilting movement in a least one direction of rotation of the at least two axial thrust bearings.

16. The wind turbine of claim 15, further comprising a lubricating mechanism, the lubricating mechanism comprising at least one fluid supply groove disposed in the fixed raceway annulus and at least one fluid supply hole configured through the fixed raceway annulus.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) A full and enabling disclosure of the present invention, including the best mode thereof, directed to one of ordinary skill in the art, is set forth in the specification, which makes reference to the appended figures, in which:

(2) FIG. 1 illustrates a perspective view of one embodiment of a wind turbine of conventional construction;

(3) FIG. 2 illustrates a perspective, interior view of one embodiment of a nacelle of a wind turbine;

(4) FIG. 3 is a schematic of the components and loading on an exemplary compound main bearing assembly;

(5) FIG. 4 is a perspective of an exemplary compound main bearing assembly;

(6) FIG. 5 is a perspective of an exemplary compound main bearing assembly showing tilt pad axial journal bearings.

(7) Repeat use of reference characters in the present specification and drawings is intended to represent the same or analogous features or elements of the present disclosure.

DETAILED DESCRIPTION OF THE INVENTION

(8) Reference now will be made in detail to embodiments of the invention, one or more examples of which are illustrated in the drawings. Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the scope or spirit of the invention. For instance, features illustrated or described as part of one embodiment can be used with another embodiment to yield a still further embodiment. Thus, it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.

(9) In general, the present subject matter discloses a compound bearing arrangement to handle loads that were previously reacted to the main frame through a pair of axially spaced predominantly radially loaded bearings. When the axial spacing between the pair of bearings is short, the bearings are highly loaded and expensive. When they are spaced apart they are less expensive but require a more expensive longer shaft. If the bearings have a very short axial spacing but are larger diameter the predominant reaction load in the bearings is in the axial direction so the moments can be reacted by axial bearings which, although larger in diameter, can be more compact and hence less expensive. When using larger diameter axial bearings, the radial loads (vertical and lateral) are typically much smaller and can be reacted by a smaller inexpensive radial bearing.

(10) Referring now to the drawings, FIG. 1 illustrates a perspective view of one embodiment of a wind turbine 10 of conventional construction. As shown, the wind turbine 10 includes a tower 12 extending from a support surface 14, a nacelle 16 mounted on the tower 12, and a rotor 18 coupled to the nacelle 16. The rotor 18 includes a rotatable hub 20 and at least one rotor blade 22 coupled to and extending outwardly from the hub 20. For example, in the illustrated embodiment, the rotor 18 includes three rotor blades 22. However, in an alternative embodiment, the rotor 18 may include more or less than three rotor blades 22. Each rotor blade 22 may be spaced about the hub 20 to facilitate rotating the rotor 18 to enable kinetic energy to be transferred from the wind into usable mechanical energy, and subsequently, electrical energy. For instance, the hub 20 may be rotatably coupled to an electric generator 24 (FIG. 2) positioned within the nacelle 16 to permit electrical energy to be produced.

(11) Referring now to FIG. 2, a simplified, internal view of one embodiment of a nacelle 16 of a wind turbine 10 is illustrated. As shown, a generator 24 may be disposed within the nacelle 16. In general, the generator 24 may be coupled to the rotor 18 of the wind turbine 10 for producing electrical power from the rotational energy generated by the rotor 18. For example, as shown in the illustrated embodiment, the rotor 18 may include a rotor shaft 32 coupled to the hub 20 for rotation therewith. The rotor shaft 32 may, in turn, be rotatably coupled to a generator shaft 34, sometimes referred to as the high speed shaft (HSS), of the generator 24 through a gearbox 36 having a gearbox output shaft. As is generally understood, the rotor shaft 32 may provide a low speed, high torque input to the gearbox 36 in response to rotation of the rotor blades 22 and the hub 20. The gearbox 36 may then be configured to convert the low speed, high torque input to a high speed, low torque output to drive the generator shaft 34 (HSS), and thus, the generator 24.

(12) Main bearings 40, sometimes referred to as the rotor bearings, are housed in a main bearing assembly 48 that is supported by a main bearing pedestal 42 attached to the main frame 44 of the wind turbine with a main bearing housing 46 enclosing the main bearings 40. The main bearings 40 can be configured to react to loading as shown in FIG. 3, where the axial loads 50 are imposed on a pair of axial thrust bearings 52, 54 and the radial loads 56 are imposed on a radial bearing 58. This main bearing 40 arrangement is referred to as a compound bearing 60, herein.

(13) One embodiment of the main bearing assembly 48 can have a main bearing housing 46 (not shown) that houses the compound bearing 60 and is further shown in FIGS. 4 and 5 as a three-row structure with the radial bearing pad 62 positioned at right angles (90 degrees) from the axial bearing pads 64. The axial bearing pads 64 can be adjacent a static spacer 80 that is removable to enable access and assembly of the radial bearing 58. The radial bearing pad 62 for the radial bearing 58 can be disposed circumferentially around the inner surface 66 a fixed raceway annulus 70. The fixed raceway annulus 70 can be coupled to the main bearing housing 46. The axial thrust bearing pads (at least two rows) for the axial thrust bearings 52, 54 can be disposed circumferentially around the rotatable rotor shaft 32 on opposing sides of the fixed raceway annulus 70. The axial thrust bearings 52, 54 can extend in the radial direction and be disposed on opposing first and second radial surfaces 67, 68 of the same fixed raceway annulus 70. Rotatable raceway components 72 can be attached to rotor shaft 32 having a removable retainer flange 76 that retains the compound bearing 60 inside the main bearing assembly 48, yet allows removal of the compound bearing 60. The one or more compound bearings 60 can have rotatable raceway components 72 disposed adjacent the at least two axial thrust bearings 52, 54 and the radial bearing 58, with the rotatable raceway components configured as the inner radial raceway surface and axial exterior raceway surface. The rotor shaft 32 can be removably coupled to the rotatable hub 20 via a shaft flange 74 to the opposing end of rotor shaft 32.

(14) It should be appreciated that the axial thrust bearings 52, 54 and the radial bearing 58 can be rolling element, for example roller bearings or ball bearings, and/or journal bearings. All bearings can also be either hydrostatic or hydrodynamic bearings. Using axially loaded thrust bearings instead of conventional vertically loaded radial bearings improves the main bearing arrangement for wind turbines. Journal hydrostatic thrust bearings instead of conventional rolling element bearings is one embodiment that enables the improvement. Another improved embodiment is a combination of rolling element and journal bearings wherein the radial bearing can be a rolling element and the thrust bearings can be journal bearings.

(15) The compound bearing can be specifically configured such that the first and second axial thrust bearings 52, 54 are journal bearings with tilting pads 78 that enable a tilting movement in at least one direction of rotation of the bearing. A white metal or a resin overlay, low in frictional coefficient to the sliding surfaces, can be applied to the tilting pads 78. Elastic support seats can be inserted with tilting pads 78 to correct any unevenness in distribution of loads applied to the tilting pads 78.

(16) Also, a lubricating mechanism for the compound bearing can be at least one fluid supply groove, for example oil, that can be cut in the fixed raceway annulus, and at least one fluid supply hole, communicating with the fluid supply groove(s), which can pass through the inner surface 66, the first axial surface 67, and the second axial surface 68 of the fixed raceway annulus, thus supplying lubricating fluid (oil) to the radial and axial thrust bearing pads.

(17) This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they include structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.