SPRING-MOUNTED GEAR MECHANISM HOUSING
20240167459 ยท 2024-05-23
Inventors
Cpc classification
F03D15/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/964
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/913
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D15/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/703
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/80
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/90
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F1/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/14
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
International classification
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A drive arrangement for a wind turbine includes a main shaft, a housing, and a nacelle-mounted support structure. The main shaft of the drive arrangement for the wind turbine is completely supported in the housing. The housing of the drive arrangement for the wind turbine is at least partially resiliently mounted in the support structure.
Claims
1. A drive arrangement for a wind turbine, comprising: a main shaft; a housing; and a nacelle-mounted support structure, wherein the main shaft is completely supported in the housing, and wherein the housing is at least partially resiliently mounted in the support structure.
2. The drive arrangement according to claim 1, wherein the housing is completely resiliently mounted in the support structure.
3. The drive arrangement according to claim 1, wherein the housing is partly resiliently and partly rigidly mounted in the support structure.
4. The drive arrangement according to claim 1 comprising at least two main bearings, wherein the main shaft is supported in the housing by the main bearings, and wherein the main bearings are axially spaced from each other.
5. The drive arrangement according to claim 1 comprising a planet carrier supported by the main shaft.
6. The drive arrangement according to claim 1 comprising one or more elastomers, by which the housing is resiliently mounted in the support structure.
7. The drive arrangement according to claim 1 comprising a first elastomer and a second elastomer of different hardness, wherein the first elastomer is disposed in a radial intermediate space between the housing and the support structure, and wherein the second elastomer is disposed in an axial intermediate space between the housing and the support structure.
8. The drive arrangement according to claim 1 comprising at least one bolt and at least two aligned eyes, wherein the housing and the support structure each have at least one of the eyes, and wherein the bolt engages in the eyes.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0006] Subject matter of the present disclosure will be described in even greater detail below based on the exemplary figures. All features described and/or illustrated herein can be used alone or combined in different combinations. The features and advantages of various embodiments will become apparent by reading the following detailed description with reference to the attached drawings, which illustrate the following:
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DETAILED DESCRIPTION
[0017] In an embodiment, the present invention improves the bearing arrangement of a drivetrain for a wind turbine in a nacelle-mounted support structure.
[0018] The drive arrangement according to an embodiment of the invention includes a main shaft, a housing, and a nacelle-mounted support structure. A main shaft is an input shaft of a gearbox of the wind turbine. In an installed state, it is non-rotatably connected to a wind-driven rotor of the wind turbine.
[0019] The housing is preferably a gearbox housing, i.e. a housing of said gearbox, or a housing comprising at least the gearbox housing.
[0020] The nacelle-mounted support structure is a support structure that is rigidly mounted or configured to be rigidly mounted relative to a nacelle of the wind turbine, i.e. without the possibility of a relative movement. In particular, the nacelle itself can form the support structure.
[0021] The main shaft is fully supported in the housing. This means that the main shaft is supported with each of its bearings in the housing. The main shaft therefore has no bearing, with which it is not supported in the housing.
[0022] Each bearing of the main shaft has two bearing rings. A first of the two bearing rings is fixed to the main shaft or is an integral part of the main shaft. Accordingly, a second of the two bearing rings is fixed to the housing or is an integral part of the housing.
[0023] According to an embodiment of the invention, the housing is at least partially resiliently mounted in the support structure. This means that at least one bearing position, in which the housing is mounted in the support structure is configured to be resilient. A resiliently configured bearing position allows relative movements between the housing. The bearing position has one or more spring elements, the spring forces of which counteract these relative movements.
[0024] An embodiment of the invention makes it possible for not only the housing and part of the main shaft, but also the entire drivetrain of the wind turbine to be resiliently mounted. The drivetrain can be configured as a unit of components connected to each other non-resiliently. If there are no resilient movements between individual components of the drivetrain, the loads acting on the components are reduced and consequently so is the wear and tear.
[0025] In an embodiment, the housing is fully resiliently mounted in the support structure. This means that each bearing position of the housing is configured resiliently and has the one or more spring elements described above. No bearing position is of non-resilient configuration. A non-resilient bearing position has no spring element.
[0026] The fully resilient mounting of the housing allows for the drivetrain of the wind turbine and the support structure to be mechanically decoupled. The transmission of vibrations from the drivetrain into the support structure or in the opposite direction from the support structure into the drivetrain can be almost completely prevented.
[0027] In an embodiment, the housing is partially resiliently mounted and partially rigidly mounted in the support structure. This means that at least one bearing position is resilient and at least one bearing position is non-resilient. Preferably, exactly two bearing positions, such as the gearbox-side bearing position, are non-resilient and exactly two bearing positions, such as the generator-side bearing positions, are resilient.
[0028] Preferably, the drive arrangement is configured with at least two main bearings. A main bearing refers to a bearing of the main shaft. According to this embodiment, the main shaft is mounted in the housing by means of the at least two main bearings. The main bearings are axially spaced from one another, i.e. in the direction of an axis of rotation of the main shaft. There is thus an axial offset between the two bearings. A distance between the two bearings in the axial direction is greater than zero. Due to the axial offset, bending moments acting on the main shaft, i.e. torques acting in axial direction and/or orthogonally to the axis of rotation of the main shaft, can be absorbed.
[0029] In an embodiment, a planet carrier of the gearbox is at least partially supported by the main shaft. The planet carrier is therefore at least partially supported on the main shaft. This means that the main shaft at least partially absorbs a weight force of the planet carrier.
[0030] Preferably, the planet carrier is fully supported by the main shaft. In this case, the main shaft fully absorbs the weight of the planet carrier. This eliminates the need for a separate bearing arrangement for the planet carrier. The reduced number of bearing positions simplifies the configuration of the drivetrain.
[0031] Preferably, the drive arrangement is further configured with one or more elastomers. An elastomer is a spring element consisting of a viscoelastic polymer. By means of the one or more elastomers, the housing is resiliently mounted in the support structure. The housing thereby supports itself via the one or more elastomers in the support structure. The resilience of the elastomers allows for relative movements between the housing and the support structure. The use of elastomers in accordance with this further embodiment is advantageous because elastomers have a simple structure and are therefore inexpensive and fail-safe.
[0032] In an embodiment, elastomers of different stiffness are provided. According to this embodiment, a first elastomer and a second elastomer, as described above, serve to mount the housing in the support structure. The first elastomer and the second elastomer are characterized in that they have a different stiffness. The stiffness of the elastomers is influenced by their designed configuration and material hardness.
[0033] According to an embodiment, the first elastomer is arranged in a radial intermediate space between the housing and the support structure. The radial intermediate space extends in the radial direction, i.e. orthogonally to the axis of rotation of the main shaft. As a result, spring forces applied by the first elastomer counteract relative movements between the housing and the support structure in the radial direction.
[0034] The second elastomer is arranged in an axial intermediate space between the housing and the support structure. The axial intermediate space extends in the axial direction, i.e. parallel to the axis of rotation of the main shaft. Spring forces applied by the first elastomer correspondingly counteract relative movements between the housing and the support structure in the axial direction.
[0035] Due to the different hardnesses of the first elastomer and the second elastomer according to the embodiment, the drive arrangement can be adapted particularly well to vibration modes that differ in the axial and radial directions.
[0036] Preferably, the drive arrangement is configured with at least one bolt and at least two eyes that are aligned with each other. Eyes designate through-holes or blind holes that serve to receive a bolt. Presently, the housing and the support structure each have at least one of the eyes. The bolt engages in the eyes. Thus, a portion of the bolt is located in each of the at least two eyes. The eyes, together with a bolt engaging therein, form one of the bearing positions described above.
[0037] Preferred embodiments of the invention are shown in the figures. Matching reference numerals indicate thereby identical or functionally identical features.
[0038] The drive arrangement 101 shown in
[0039] The entire drivetrain shown, comprising the main shaft 105, the gearbox 107 and the generator 109, is housed in a single housing structure 115. Accordingly, the main shaft 105 is supported in the housing structure 115 by means of two main bearings 117. The two main bearings 117, each of which may be constructed from one or more bearing units, form the only bearing positions of the main shaft 105.
[0040] The planet carrier 113 does not have its own bearings. Instead, it is supported by the main shaft 105. For this purpose it is screwed to the main shaft 105.
[0041] The housing structure 115 consists of several parts that are rigidly screwed together. The housing structure 115 is resiliently mounted in the machine carrier 111 by means of elastomers 119.
[0042] Each elastomer 119 is part of a bearing position 201 shown in
[0043] The drive arrangement 101 has exactly four bearing positions 201. Exemplary embodiments for the configuration of the bearing positions 201 are shown in
[0044] According to
[0045] Two of the four bearing points 201 furthermore each have two disk-shaped elastomers 309. These are each located in an axial intermediate space between the eye 303 of the housing structure 111 and an eye 301 of the machine carrier 111. Accordingly, the elastomers 309 serve to absorb forces in the axial direction.
[0046] In the exemplary embodiments shown in
[0047] A corresponding exploded view is shown in
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[0049] In accordance with
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[0051] In accordance with
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[0053] While subject matter of the present disclosure has been illustrated and described in detail in the drawings and foregoing description, such illustration and description are to be considered illustrative or exemplary and not restrictive. Any statement made herein characterizing the invention is also to be considered illustrative or exemplary and not restrictive as the invention is defined by the claims. It will be understood that changes and modifications may be made, by those of ordinary skill in the art, within the scope of the following claims, which may include any combination of features from different embodiments described above.
[0054] The terms used in the claims should be construed to have the broadest reasonable interpretation consistent with the foregoing description. For example, the use of the article a or the in introducing an element should not be interpreted as being exclusive of a plurality of elements. Likewise, the recitation of or should be interpreted as being inclusive, such that the recitation of A or B is not exclusive of A and B, unless it is clear from the context or the foregoing description that only one of A and B is intended. Further, the recitation of at least one of A, B and C should be interpreted as one or more of a group of elements consisting of A, B and C, and should not be interpreted as requiring at least one of each of the listed elements A, B and C, regardless of whether A, B and C are related as categories or otherwise. Moreover, the recitation of A, B and/or C or at least one of A, B or C should be interpreted as including any singular entity from the listed elements, e.g., A, any subset from the listed elements, e.g., A and B, or the entire list of elements A, B and C.
LIST OF REFERENCE NUMERALS
[0055] 101 drive arrangement [0056] 103 rotor [0057] 105 main shaft [0058] 107 gearbox [0059] 109 generator [0060] 111 machine carrier [0061] 113 planet carrier [0062] 115 housing structure [0063] 117 main bearing [0064] 119 elastomer [0065] 201 bearing position [0066] 203 rotation axis [0067] 301 eye [0068] 303 eye [0069] 305 bolt [0070] 307 elastomer [0071] 309 elastomer [0072] 401 elastomer [0073] 403 basic body [0074] 405 bridge [0075] 501 elastomer [0076] 600 retaining ring [0077] 601 end plates [0078] 603 screw [0079] 701 screw [0080] 703 nut [0081] 901 shoulder