WIND TURBINE TRANSMISSION

Abstract

The invention relates to a wind turbine gearbox (8), in particular a planetary gearbox, having at least one gear (12) mounted on an axle (15), for which purpose a sliding layer (20) is arranged between the gear (12) and the axle (15), said sliding layer (20) being sprayed directly onto the axle (15) or, with intermediate arrangement of at least one further layer (21), onto the further layer (21) by means of a thermal spaying method.

Claims

1: A wind turbine gearbox (8), in particular a planetary gearbox, having at least one gear (12) mounted on an axle (15), for which purpose a sliding layer (20) is arranged between the gear (12) and the axle (15), wherein the sliding layer (20) is sprayed directly onto the axle (15) or, with intermediate arrangement of at least one further layer (21), onto the further layer (21) by means of a thermal spaying method.

2: The wind turbine gearbox (8) according to claim 1, wherein the sliding layer (20) consists of or comprises a material selected from a group comprising consisting of aluminum base alloys, bismuth base alloys, silver base alloys, and copper base alloys.

3: The wind turbine gearbox (8) according to claim 1, wherein a polymer-based running-in layer is arranged on the sliding layer (20).

4: The wind turbine gearbox (8) according to claim 1, wherein two sliding layers (20) arranged at an axial distance from one another are sprayed onto the axle (15) by means of a thermal spaying method.

5: The wind turbine gearbox (8) according to claim 1, wherein hard particles and/or soft phase particles are embedded in the sliding layer.

6: The wind turbine gearbox (8) according to claim 5, wherein the hard particles are selected from a group consisting of metal oxides, metal nitrides, metal carbides, metal borides, and metal silicides and/or wherein the soft phase particles are selected from a group consisting of graphite, hexagonal BN, and metal sulfides.

7: A wind turbine (1) having a rotor (5) and a generator (7), wherein a wind turbine gearbox (8), in particular a planetary gearbox, which is operatively connected to the rotor (5) and the generator (7) is arranged between the rotor (5) and the generator (7), wherein the wind turbine gearbox (8) is designed according to claim 1.

8: A method for producing an axle (15) for a wind turbine gearbox (8), in particular a planetary gearbox, comprising the steps: providing the axle (15), and spraying a sliding layer (20) of a spraying material directly onto the axle (15) or, after application of at least one metallic intermediate layer, onto the intermediate layer by means of a thermal spraying method.

9: The method according to claim 8, wherein a spraying material in which hard particles and/or soft phase particles are contained is used, wherein the hard particles and the soft phase particles are kept in the solid form during spraying on.

10: The method according to claim 8, wherein spraying on the sliding layer (20) and/or the further metal layer (21) is carried out by means of a thermal spaying method selected from a group consisting of flame spraying, plasma spraying, cold spraying, and laser spraying.

Description

[0019] These show in a respectively very simplified schematic representation:

[0020] FIG. 1 a side view of a wind turbine;

[0021] FIG. 2 a sectional side view of a wind turbine gearbox in the form of a planetary gearbox;

[0022] FIG. 3 a cutout from the wind turbine gearbox in a sectional side view;

[0023] FIG. 4 a cutout from an embodiment variant of a wind turbine gearbox in a sectional side view.

[0024] 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.

[0025] FIG. 1 shows a wind turbine 1. This wind turbine 1 in general corresponds to the prior art, meaning that it comprises a tower 2 on whichwith intermediate arrangement of a wind direction follow-up device 3a nacelle 4 is arranged on the front end of which a rotor 5 with rotor blades 6 and on the back end of which a generator 7 are arranged. A wind turbine gearbox 8, which is connected on the one hand to the rotor 5 and on the other hand to the moving member of the generator 7, is arranged between the rotor 5 and the generator 7, i.e. a not further represented moving member of the generator. The wind turbine gearbox 8 serves for increasing the rotational frequency of the moving member as compared to the rotor 5. On the lower part of the tower 2, lastly, there is a network connection 9.

[0026] As these components are in general known from the prior art for wind turbines 1, reference is here made to relevant literature in this regard. However, it should be mentioned that the wind turbine 1 is not obligatorily limited to the type represented in FIG. 1.

[0027] FIG. 2 shows the wind turbine gearbox 8 in the form of a simple planetary gearbox in a sectional side view.

[0028] The wind turbine gearbox 8 comprises a sun gear 10 connected to a shaft 11 so as to be prevented from rotating relative to it, said shaft 11 leading to the generator rotor. The sun gear 10 is surrounded by several gears 12 in the form of planetary gears, for example two, preferably three or four. The sun gear 10 and the gears 12 comprise end toothings 13, 14 that are engaged in meshing arrangement, these end toothings 13, 14 being adumbrated by a cross in FIG. 1. The gears 12 are mounted on an axle 15 (planetary gear bolt). The axles 15 are inserted into bores of an axle carrier 16 (planetary carrier). An internal gear 17 is arranged above the gears 12, said internal gear 17 also at least partially comprising a toothing 18, which is in engaged in meshing arrangement with the end toothing 14 of the gears 12, on an inner surface. The internal gear 17 is connected to a rotor shaft 19 of the rotor 5 of the wind turbine 1 (FIG. 1) so as to be prevented from rotating relative to it. The end toothings 13, 14 and/or the toothing 18 can be designed as spur toothing or helical toothing.

[0029] As such planetary gearboxes are in general also already known from the prior art, further explanations are superfluous here. However, reference is made to the fact that not only single-stage designs of planetary gearboxes are possible but also multi-stage designs, such as two-stage or three-stage designs.

[0030] Reference is made to the fact that below, the singular will be used as regards the gear 12. However, it is clear that the invention is applicable to all gears 12 of such a wind turbine gearbox 8.

[0031] FIG. 3 shows a cutout from the wind turbine gearbox 8 in a sectional side view applied in the region of the bearing of the gear 12 on the axle 15. The gear 12 is mounted on the axle via a sliding bearing. For this purpose, a sliding layer 20 is arranged between the axle 15 and the gear 12. The sliding layer 20 is arranged directly on the axle 15 and connected thereto. For this purpose, the material for the sliding layer 20 is applied onto the axle 15 by means of a thermal spaying method.

[0032] According to a corresponding embodiment variant, if required it can be provided for that prior to the application of the sliding layer 20 onto the axle 15, at least one further layer 21 is applied, as is adumbrated in dashed lines in FIG. 3. Preferably, the further layer 21 is also applied onto the axle 15 by means of a thermal spaying method. The further layer 21 can for example be a diffusion barrier layer and/or a bonding layer and/or a bearing metal layer. The sliding layer 20 is applied directly onto the further layer 21 in this embodiment variant.

[0033] The sliding layer 20 is a metal layer, in particular consisting of or comprising a metal alloy. The material can preferably be selected from a group comprising aluminum base alloys, bismuth base alloys, silver base alloys, copper base alloys. However, other alloys, such as indium-based alloys, lead-based alloys and/or CuPb-based alloys with a high lead content can also be used. However, preferably lead-free alloys are used. Lead-free alloys are alloys which contain lead in a maximum proportion corresponding to the proportion of usual impurities in such alloys.

[0034] The further layer 21 can for example be an aluminum base alloy, a tin base alloy, a copper base alloy, a CuPb base alloy, an AlSn base alloy, an alloy on an AlZn, AlSi, AlSnSi, CuAl, CuSn, CuZn, CuSnZn, CuZnSn, CuBi as well as AlBi base, a pure metal alloy of Al, Ni, Co, Sn, etc., with the proviso that the composition of the further layer 21 is different from that of the sliding layer 20.

[0035] According to another embodiment variant, it can be provided for that a running-in layer 22 is arranged on the sliding layer 20, said running-in layer 22 in this case forming the radially outer layer and being brought into sliding contact with the gear 12. The running-in layer 22 can for example be a pure metal layer, such as tin. However, preferably the running-in layer 22 is a polymer-based running-in layer 22. In particular, a polyimide or a polyamidimide is used as polymer. Moreover, the running-in layer can also contain a proportion of solid lubricant particles, for example MoS.sub.2 and/or graphite. The proportion of the polymer in the running-in layer 22 can amount to between 40 wt. % and 80 wt. %. The balance adding up to 100 wt. % is constituted by the solid lubricant particles.

[0036] It is further possible that hard particles and/or soft phase particles are embedded in the sliding layer 20. The hard particles can be selected from a group comprising metal oxides such as MgO, TiO.sub.2, ZrO.sub.2, Al.sub.2O.sub.3, metal nitrides, metal carbides such as SiC, WC, B.sub.4C, metal borides, metal silicides. The soft phase particles can be selected from a group comprising graphite, hexagonal BN, metal sulphides.

[0037] It should be mentioned that the hard particles have a higher hardness than the matrix of the sliding layer 20 in which they are embedded. The soft phase particles, in contrast, have a lower hardness than the matrix of the sliding layer 20 in which they are embedded.

[0038] The proportion of the hard particles and/or soft phase particles in the sliding layer 20 can be selected from a range between 3 wt. % to 25 wt. %, in particular of 5 wt. % to 20 wt. %.

[0039] According to another embodiment variant, the mean particle size of the soft phase particles and/or hard phase particles can amount to between 1 m and 100 m, preferably between 5 m and 20 m.

[0040] FIG. 4 shows a cutout of another embodiment variant of the wind turbine gearbox 8 in longitudinal section. As opposed to the above embodiment variant of the wind turbine gearbox 8, in this embodiment variant two sliding layers 20 arranged at an axial distance from one another are sprayed onto the axle 15 by means of a thermal spaying method. Due to the axial distance of the two sliding layers 20, an intermediate space 23 is formed between these. Said space can be used for feeding a lubricant. In this respect, the lubricant feed can be carried out (solely) via the axle 15 as is adumbrated in dashed lines.

[0041] For better distribution of the lubricant across at least approximately the entire running surfaces, the intermediate space 7 can be connected to the ambient atmosphere via at least one connecting line. Preferably, the connecting line extends within the axle 15.

[0042] It should be mentioned that instead of two sliding layers 20, more than two sliding layers 20 could be sprayed onto the axle 15.

[0043] As was already mentioned, the sliding layer 20 is sprayed onto the axle 15 by means of a thermal spaying method. Preferably, a spraying method selected from a group of flame spraying, for example wire flame spraying or high velocity flame spraying, e.g. HVOF (high velocity oxygen fuel) or HVAF (high velocity air fuel), plasma spraying, cold spraying, laser spraying is used.

[0044] According to an embodiment variant in this regard, it can be provided for that a spraying material in which hard particles and/or soft phase particles are contained is used, wherein the hard particles and the soft phase particles are kept in the solid form during spraying on. For this purpose, a metal alloy having a low melting point is selected as the hard particles and/or soft phase particles.

[0045] Prior to spraying the sliding layer 20 or the further layer 21 onto the axle 15, which is in particular constituted of a steel, the axle is preferably pretreated. This pretreatment preferably comprises roughening of the surface of the axle 15 at least in the region in which the sliding layer 20 or the further layer 21 is applied. In particular, the axle 15 is blasted in this region.

[0046] Then, the axle 15 is preferably cleaned.

[0047] The spraying material can be used in a wire or powder form.

[0048] Spraying on the sliding layer 20 and/or the further layer 21 can also be carried out in a vacuum or a protective gas atmosphere.

[0049] After spraying on, the sliding layer 20 and/or the further layer 21 can be subjected to after-treatment.

[0050] The exemplary embodiments show possible embodiment variants, while it should be noted at this point that combinations of the individual embodiment variants are also possible.

[0051] Finally, as a matter of form, it should be noted that for ease of understanding of the wind turbine gearbox 8 and/or the wind turbine 1, these are not obligatorily depicted to scale.

LIST OF REFERENCE NUMBERS

[0052] 1 wind turbine [0053] 2 tower [0054] 3 wind direction follow-up device [0055] 4 nacelle [0056] 5 rotor [0057] 6 rotor blades [0058] 7 generator [0059] 8 wind turbine gearbox [0060] 9 network connection [0061] 10 sun gear [0062] 11 shaft [0063] 12 gear [0064] 13 end toothing [0065] 14 end toothing [0066] 15 axle [0067] 16 planetary carrier [0068] 17 internal gear [0069] 18 toothing [0070] 19 rotor shaft [0071] 20 sliding layer [0072] 21 layer [0073] 22 running-in layer [0074] 23 intermediate space