PLAIN BEARING ARRANGEMENT AND NACELLE EQUIPPED WITH A PLAIN BEARING ARRANGEMENT FOR A WIND TURBINE, AND WIND TURBINE
20230228253 ยท 2023-07-20
Assignee
Inventors
- Johannes Sebastian HOELZL (Berg im Attergau, AT)
- Albert WALDL (Laakirchen, AT)
- Patrick LAUBICHLER (Gmunden, AT)
Cpc classification
F05B2260/98
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/57
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/046
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/53
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C23/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F03D1/0691
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A sliding bearing includes an inner ring element; an outer ring element; and at least one sliding bearing element, which is arranged between the inner ring element and the outer ring element, wherein the sliding bearing element includes at least two sliding bearing pads, wherein the individual sliding bearing pads each have a bearing surface, which has the basic shape of a spherical cap.
Claims
1. A sliding bearing (9) comprising: an inner ring element (13); an outer ring element (14); at least one sliding bearing element (15), which is arranged between the inner ring element (13) and the outer ring element (14), wherein the sliding bearing element (15) comprises at least two sliding bearing pads (20), wherein the individual sliding bearing pads (20) each have a bearing surface (23), which has the basic shape of a spherical cap.
2. The sliding bearing (9) according to claim 1, wherein the outer ring element (14) is configured as a bearing block (17) which comprises a bearing block base (18) and a bearing block cover (19).
3. The sliding bearing (9) according to claim 1, characterized in that wherein the bearing surface (23) cooperates with the outer ring element (14), wherein a counterface (24) to the bearing surface (23) is formed in the outer ring element (14).
4. The sliding bearing (9) according to claim 1, wherein the inner ring element (13) has a shaped element (30), in particular in the form of an elevation or an indentation, wherein the sliding bearing pads (20) have a mating shaped element (31) corresponding to the shaped element (30), such that the shaped element (30) serves as an axial securing means for the sliding bearing pads (20).
5. The sliding bearing (9) according to claim 4, wherein the shaped element (30) arranged on the inner ring element (13) is configured in the form of a circumferential bead with a rectangular cross-section, wherein the sliding bearing pads (20) comprise a corresponding groove extending in the circumferential direction.
6. The sliding bearing (9) according to claim 1, wherein at least individual ones of the sliding bearing pads (20) are coupled to one another by means of a connecting element (22).
7. The sliding bearing (9) according to claim 6, wherein the connecting element (22) is arranged on a circumferential side (36) of the sliding bearing pads (20).
8. The sliding bearing (9) according to claim 6, characterized in that wherein the connecting element (22) comprises at least one fastening wedge (39), wherein a fastening groove (38) corresponding to the fastening wedge (39) is formed in the sliding bearing pad (20).
9. The sliding bearing (9) according to claim 6, wherein the connecting element (22) comprises an adjusting means (40), such that the distance to one another of two sliding bearing pads (20) coupled to one another by means of the connecting element (22) may be adjusted.
10. The sliding bearing (9) according to claim 1, wherein at least individual ones of the sliding bearing pads (20) are coupled to the inner ring element (13) by means of a fastening means (35).
11. The sliding bearing (9) according to claim 1, wherein the bearing surface (23) has a spherical cap formed in such a way that the bearing surface (23) has a first diameter (27) in the region of a first end face (26) of the sliding bearing pad (20) and that the bearing surface (23) has a second diameter (29) in the region of a second end face (28) of the sliding bearing pad (20), wherein the first diameter (27) is smaller than the second diameter (29) and wherein the second diameter (29) forms the largest diameter on the bearing surface (23).
12. The sliding bearing (9) according to claim 11, wherein an axial bearing ring (32) is formed which is coupled to the outer ring element (14), wherein an axial sliding surface (33) is formed on the sliding bearing pads (20), wherein an axial counter-sliding surface (34), which corresponds to the axial sliding surface (33), is formed on the axial bearing ring (32).
13. The sliding bearing (9) according to claim 1, wherein the outer ring element (14) comprises a recess (45) and/or a stiffening (46) which serves to change the position of a shear center (43) of the outer ring element (14).
14. The sliding bearing (9) according to claim 1, wherein the counterface (24) of the outer ring element (14) and/or the bearing surfaces (23) of the sliding bearing pads (20) have a shape deviating from an ideal spherical cap by between 0.001 mm and 10 mm, in particular between 0.05 mm and 5 mm, preferably between 0.5 mm and 1 mm, which shape is configured such that load-induced deformations of the inner ring element (13) and/or the outer ring element (14) and/or the sliding bearing pad (20) are compensated and, in the loaded state, the bearing surfaces (23) of the sliding bearing pads (20) lie flat against the counterface (24) of the outer ring element (14).
15. The sliding bearing (9) according to claim 1, wherein the sliding bearing is formed as a hydrodynamic sliding bearing.
16. The sliding bearing (9) according to claim 15, wherein the bearing block base (18) and the bearing block cover (19) are divided such that a separation gap between the bearing block base (18) and the bearing block cover (19) is arranged at a distance from a load transfer zone (42).
17. The sliding bearing (9) according to claim 1, wherein at least one driving recess (47) for conveying lubricating oil (51) is formed on the bearing surface (23) of at least one of the sliding bearing pads (20).
18. The sliding bearing (9) according to claim 1, wherein a first labyrinth seal (49) is formed in the axial bearing ring (32) and/or that wherein a second labyrinth seal (50) is formed in a sealing ring (48).
19. A nacelle (2) for a wind turbine (1), the nacelle (2) comprising: a nacelle housing (4); a rotor shaft (16); a rotor hub (6) which is arranged on the rotor shaft (16); a rotor bearing (8) for bearing the rotor shaft (16) on the nacelle housing (4), characterized in that wherein the rotor bearing (8) comprises the sliding bearing (9) according to claim 1.
20. The nacelle (2) according to claim 19, wherein the rotor shaft (16) forms the inner ring element (13).
21. The nacelle (2) according to claim 19, wherein the bearing surface (23) is configured in the form of a spherical cap in such a way that the bearing surface (23) has a first diameter (27) in the region of a first end face (26) of the sliding bearing pad (20) and that the bearing surface (23) has a second diameter (29) in the region of a second end face (28) of the sliding bearing pad (20), wherein the first diameter (27) is smaller than the second diameter (29) and wherein the second diameter (29) forms the largest diameter on the bearing surface (23), wherein the second end face (28) faces a rotor hub (6).
22. A wind turbine (1) having a nacelle (2), the nacelle (2) comprising: a nacelle housing (4); a rotor hub (6) with rotor blades arranged thereon; a rotor bearing (8) for bearing the rotor hub (6) on the nacelle housing (4), characterized in that wherein the rotor bearing (8) comprises the sliding bearing (9) according to claim 1.
23. The wind turbine (1) according to claim 22, wherein the outer ring element (14) has a shear center (43) and that wherein the sliding bearing pad (20) acts on the outer ring element (14) in a main direction of force (44), wherein the main direction of force (44) acts closer to the second end face (28) of the sliding bearing pad (20) than where the shear center (43) is formed.
Description
[0046] For the purpose of better understanding of the invention, it will be elucidated in more detail by means of the figures below.
[0047] These show in a respectively very simplified schematic representation:
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[0055]
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[0059]
[0060] First of all, it is to be noted that in the different embodiments described, equal parts are provided with equal reference numbers and/or equal component designations, where the disclosures contained in the entire description may be analogously transferred to equal parts with equal reference numbers and/or equal component designations. Moreover, the specifications of location, such as at the top, at the bottom, at the side, chosen in the description refer to the directly described and depicted figure and in case of a change of position, these specifications of location are to be analogously transferred to the new position.
[0061]
[0062] Moreover, a rotor 5 is formed, which has a rotor hub 6 with rotor blades 7 arranged thereon. The rotor hub 6 is considered part of the nacelle 2. The rotor hub 6 is received so as to be rotatable on the nacelle housing 4 by means of a rotor bearing 8. In particular, it is provided that a sliding bearing 9 according to the invention and described in more detail below is used as a rotor bearing 8.
[0063] The rotor bearing 8, which serves for bearing the rotor hub 6 on the nacelle housing 4 of the nacelle 2, is configured for absorbing a radial force 10 and an axial force 11. The axial force 11 is caused by the force of the wind. The radial force 10 is caused by the weight force of the rotor 5 and is effective at the center of gravity of the rotor 5. As the center of gravity of the rotor 5 is outside the rotor bearing 8, a tilting torque 12 is generated in the rotor bearing 8 by the radial force 10. The tilting torque 12 may also be caused by an uneven load of the rotor blades 7. This tilting torque 12 can be absorbed by means of a second sliding bearing, which is arranged at a distance from the sliding bearing 9 according to the invention.
[0064] The rotor bearing 8 according to the invention can have a diameter of 0.5 m to 5 m, for example. Of course, it is also conceivable that the rotor bearing 8 is smaller or larger.
[0065]
[0066]
[0067] Below, the sliding bearing 9 will be described by means of a combination of
[0068] As can be seen from
[0069] In the exemplary embodiment shown in
[0070] Furthermore, it may be provided that the outer ring element 14 is configured as a bearing block 17 which comprises a bearing block base 18 and a bearing block cover 19. In particular, it may be provided that the bearing block base 18 is coupled to the nacelle housing 4. In this exemplary embodiment, it may thus be provided that the outer ring element 14 is rigidly coupled to the nacelle housing 4 and that the inner ring element 13 is rotatable about a rotor axis 21 relative to the outer ring element 14 by means of the sliding bearing element 15.
[0071] As the rotor shaft 16, which is coupled to the rotor hub 6 and thus to the rotor 5, is received in the inner ring element 13, the rotor shaft 16 is therefore rotatably received in the nacelle housing 4 by means of the sliding bearing 9.
[0072] As can further be seen in
[0073] As can be seen in particular from
[0074] As can further be seen from
[0075]
[0076] As can be seen from
[0077] In particular, it may be provided that the connecting elements 22 are configured in the form of screws. As can further be seen from
[0078] In the operating state of the sliding bearing 9, the individual sliding bearing pads 20 are thus fixedly connected to the inner ring element 13 due to the structure described and thus, rotate along with it relative to the outer ring element 14. In order to enable the rotational movement between the inner ring element 13 and the outer ring element 14, on each of the individual sliding bearing pads 20 one bearing surface 23 is formed which abuts on a counterface 24 of the outer ring element 14 in the operational state of the sliding bearing 9. The counterface 24 is arranged on the inside 25 of the outer ring element 14.
[0079] The bearing surface 23 of the sliding bearing pad 20 and the counterface 24 of the outer ring element 14 are designed as sliding surfaces, which slide on one another during operation of the sliding bearing 9. In particular, it may be provided that the counterface 24 of the outer ring element 14 is designed as a hard, wear-resistant surface, which may be formed, for example, by a hardened steel. The bearing surface 23 of the sliding bearing pad 20 may be formed of a sliding bearing material which is soft in comparison to the counterface 24. Of course, it is also conceivable that the bearing surface 23 has an anti-friction coating.
[0080] As can be seen particularly well in
[0081] Moreover, due to the design of the bearing surface 23 and/or the counterface 24 in the shape of a spherical cap, axial bearing forces can also be transferred in addition to the transfer of radial bearing forces.
[0082] As can further be seen in
[0083] As can further be seen from
[0084] As can further be seen from
[0085]
[0086] As can be seen from
[0087] As can further be seen from
[0088]
[0089] As can be seen from
[0090] As can further be seen from
[0091] In a first exemplary embodiment, it may be provided that the connecting element 22 is configured in the form of a rectangular rod which is introduced into a fastening groove 38 arranged in the circumferential sides 36. As can be seen from
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[0095] As can further be seen from
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[0099] As can be seen from
[0100] As can be seen from
[0101] Therefore, it is conceivable that, as shown in
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[0103] In a preferred embodiment variant, the shear center 43 is influenced such by means of the recess 45 and/or the stiffening 46 that the main direction of force 44 is arranged so as to be positioned precisely in the shear center 43.
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[0105] As can be seen from
[0106] The exemplary embodiments show possible embodiment variants, and it should be noted in this respect that the invention is not restricted to these particular illustrated embodiment variants of it, but that rather also various combinations of the individual embodiment variants are possible and that this possibility of variation owing to the technical teaching provided by the present invention lies within the ability of the person skilled in the art in this technical field.
[0107] The scope of protection is determined by the claims. Nevertheless, the description and drawings are to be used for construing the claims. Individual features or feature combinations from the different exemplary embodiments shown and described may represent independent inventive solutions. The object underlying the independent inventive solutions may be gathered from the description.
[0108] All indications regarding ranges of values in the present description are to be understood such that these also comprise random and all partial ranges from it, for example, the indication 1 to 10 is to be understood such that it comprises all partial ranges based on the lower limit 1 and the upper limit 10, i.e. all partial ranges start with a lower limit of 1 or larger and end with an upper limit of 10 or less, for example 1 through 1.7, or 3.2 through 8.1, or 5.5 through 10.
[0109] Finally, as a matter of form, it should be noted that for ease of understanding of the structure, elements are partially not depicted to scale and/or are enlarged and/or are reduced in size.
TABLE-US-00001 List of reference numbers 1 Wind turbine 2 Nacelle 3 Tower 4 Nacelle housing 5 Rotor 6 Rotor hub 7 Rotor blade 8 Rotor bearing 9 Sliding bearing 10 Radial force 11 Axial force 12 Tilting torque 13 Inner ring element 14 Outer ring element 15 Sliding bearing element 16 Rotor shaft 17 Bearing block 18 Bearing block base 19 Bearing block cover 20 Sliding bearing pad 21 Rotor axis 22 Connecting element 23 Bearing surface 24 Counterface 25 Inside 26 First end face 27 First diameter 28 Second end face 29 Second diameter 30 Shaped element 31 Mating shaped element 32 Axial bearing ring 33 Axial sliding surface 34 Axial counter-sliding surface 35 Fastening means 36 Circumferential sides 37 Gap 38 Fastening groove 39 Fastening wedge 40 Adjusting means 41 Fastening means 42 Load transfer zone 43 Shear center 44 Main direction of force 45 Recess 46 Stiffening 47 Driving recess 48 Sealing ring 49 First labyrinth seal 50 Second labyrinth seal 51 Lubricating oil