SE1200546A1 - Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly - Google Patents

Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly Download PDF

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Publication number
SE1200546A1
SE1200546A1 SE1200546A SE1200546A SE1200546A1 SE 1200546 A1 SE1200546 A1 SE 1200546A1 SE 1200546 A SE1200546 A SE 1200546A SE 1200546 A SE1200546 A SE 1200546A SE 1200546 A1 SE1200546 A1 SE 1200546A1
Authority
SE
Sweden
Prior art keywords
ring
bearing
shaft
rolling bearing
presents
Prior art date
Application number
SE1200546A
Other languages
English (en)
Inventor
Hans Wendeberg
Haakan Leander
Original Assignee
Skf Ab
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Skf Ab filed Critical Skf Ab
Priority to SE1200546A priority Critical patent/SE1200546A1/sv
Publication of SE1200546A1 publication Critical patent/SE1200546A1/sv
Priority to US14/426,816 priority patent/US20150240874A1/en
Priority to PCT/SE2013/000135 priority patent/WO2014038990A1/en
Priority to JP2015531040A priority patent/JP2015533980A/ja
Priority to CN201380044918.XA priority patent/CN104583623A/zh

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063—Fixing them on the shaft
    • F16C35/0635—Fixing them on the shaft the bore of the inner ring being of special non-cylindrical shape which co-operates with a complementary shape on the shaft, e.g. teeth, polygonal sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B27/00—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for
    • B25B27/02—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for for connecting objects by press fit or detaching same
    • B25B27/06—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for for connecting objects by press fit or detaching same inserting or withdrawing sleeves or bearing races
    • B25B27/064—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for for connecting objects by press fit or detaching same inserting or withdrawing sleeves or bearing races fluid driven
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/70—Bearing or lubricating arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/70—Bearing or lubricating arrangements
    • F03D80/703—Shaft bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/70—Bearing or lubricating arrangements
    • F03D80/705—Lubrication circuits; Lubrication delivery means
    • F03D80/709—Bearing lubrication
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/72—Sealings
    • F16C33/76—Sealings of ball or roller bearings
    • F16C33/80—Labyrinth sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063—Fixing them on the shaft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/078—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing using pressure fluid as mounting aid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C43/00—Assembling bearings
    • F16C43/04—Assembling rolling-contact bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/22—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
    • F16C19/24—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for radial load mainly
    • F16C19/26—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for radial load mainly with a single row of rollers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/10—Force connections, e.g. clamping
    • F16C2226/16—Force connections, e.g. clamping by wedge action, e.g. by tapered or conical parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/06—Ball or roller bearings
    • F16C23/08—Ball or roller bearings self-adjusting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2300/00—Application independent of particular apparatuses
    • F16C2300/10—Application independent of particular apparatuses related to size
    • F16C2300/14—Large applications, e.g. bearings having an inner diameter exceeding 500 mm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/31—Wind motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/08—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key
    • F16D1/09—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with radial clamping due to axial loading of at least one pair of conical surfaces
    • F16D2001/0906—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with radial clamping due to axial loading of at least one pair of conical surfaces using a hydraulic fluid to clamp or disconnect, not provided for in F16D1/091
    • Y—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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • Y—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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49636—Process for making bearing or component thereof
    • Y10T29/49643—Rotary bearing
    • Y10T29/49679—Anti-friction bearing or component thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Rolling Contact Bearings (AREA)
  • Wind Motors (AREA)
  • Mounting Of Bearings Or Others (AREA)

Description

10 According to a first aspect, the objects are achieved by a method to mount a rolling bearing onto a wind turbine rotor shaft, wherein the bearing presents an outer ring, an inner ring and rolling elements interposed in-between the rings, and wherein the inner ring presents an inner circumferential surface, which surface presents a frusto-conical profile. The rolling bearing is meant to be mounted on a corresponding conical seat on the rotor shaft by the frusto-conical inner circumferential surface. The method comprises the following steps: - pressing a liquid in-between the inner circumferential surface of the inner ring and the conical seat to thereby facilitate the driving up of the rolling bearing on the conical seat, - driving up the rolling bearing on the conical seat by an axial force acting on the rolling bearing, - wherein the liquid is pressed in-between the two surfaces at an axial end portion of the inner circumferential surface.
This method has the advantage that there is no need to drill a bore in the rotor shaft of the wind turbine. This will lead to that the shaft will have an improved strength compared to shafts with drilled bores. To have a rigid and robust design of the wind turbine rotor assembly is of high importance to thereby avoid unnecessary maintenance and repair work. The rotor assembly is mounted into a nacelle of the wind turbine, which is located high up above the ground level.
Therefore, repair work and maintenance can be costly and also difficult to perform. ln an embodiment of the method, the liquid is any of oil, synthetic oil or other non- corrosive fluid. ln an embodiment of the method, a ring is mounted on the shaft and is located adjacent to and in contact with the axial end portion of the inner ring, wherein the liquid is pressed in-between the two surfaces via a conduit in the ring, which conduit ends proximate the axial end portion of the inner circumferential surface.
According to the second aspect of the invention, the objects are achieved by a wind turbine bearing assembly, which comprises: - a rotor shaft, - a rolling bearing, wherein the rolling bearing presents an outer ring, an inner ring and rolling elements interposed in-between the rings, and wherein the inner ring presents an inner circumferential surface, which surface presents a frusto- conical profile, and wherein the rolling bearing is mounted on a corresponding conical seat on the rotor shaft by the frusto-conical inner circumferential surface.
The bearing assembly further comprises a first ring mounted on the shaft and contacting at least the inner ring at an axial end portion of the rolling bearing, and wherein the first ring further presents a conduit, wherein the conduit ends proximate the axial end portion of the inner circumferential surface.
This design has the advantage that there is no need to drill a bore in the rotor shaft of the wind turbine. instead there is a conduit in the labyrinth ring where a liquid, such as oil, will be pressed in between the inner ring and the shaft. This will lead to that the shaft will have an improved strength compared to shafts with drilled bores. To have a rigid and robust design of the wind turbine rotor assembly is of high importance to thereby avoid unnecessary maintenance and repair work. The rotor assembly is mounted into a nacelle of the wind turbine, which is located high up above the ground level. Therefore, repair work and maintenance can be costly and also difficult to perform.
All embodiments of the first aspect are applicable to all embodiments of the second aspect and vice versa. ln an embodiment of the invention, the first ring is a labyrinth ring, wherein the labyrinth ring contacts at least the inner ring and the outer ring at an axial end portion of the rolling bearing, and wherein the labyrinth ring seals off a space between the outer and inner ring. ln another embodiment, the first ring is any of a ring-shaped part of a bearing housing, a seal or a bearing inner ring locating arrangement or any other suitable ring. ln an embodiment, the rolling bearing is any of a toroidal roller bearing, a spherical roller bearing, a tapered roller bearing, a cylindrical roller bearing, or any other suitable rolling bearing for a wind turbine bearing assembly. ln an embodiment of the bearing assembly, the assembly further presents a second labyrinth ring mounted on the shaft and contacting the inner ring and the outer ring on the other axial end portion of the rolling bearing, wherein the second labyrinth ring seals off a second space between the outer and inner ring. ln an embodiment of the bearing assembly, the assembly comprises a third ring mounted on the shaft and being adjacent the first labyrinth ring, wherein the first labyrinth ring, the third ring and the shaft are configured to create a circumferential cavity in a circumferential extension around the shaft. ln an embodiment of the bearing assembly, the cavity is meant to act as a pressure chamber for mounting the bearing on the shaft by axially driving up the bearing on the conical seat on the shaft. ln an embodiment of the bearing assembly, the shaft presents a circumferential groove, and wherein the third ring is meant to be axially fixed on the shaft between the first labyrinth ring and a metal wire in the groove.
BRIEF DESCRIPTION OF DRAWINGS Below, a more detailed description of a number of preferred embodiments will be described. lt should be noted that the accompanying drawings are not drawn to scale, and in some cases specific details may have been exaggerated in order to better explain the invention. Furthermore, the invention as claimed is not limited to the embodiments described and shown, but modifications are possible for a skilled person within the scope of the claims.
Figure 1 shows an embodiment of an axial cross section of a wind turbine bearing assemby according to the invention.
Figure 2 shows a flow chart of the method according to the invention.
DETAILED DESCRIPTION Figure 1 shows an embodiment of an axial cross section of a wind turbine i bearing assemby according to the invention. The assembly comprises: - a rotor shaft 2, - a rolling bearing 1, wherein the rolling bearing presents an outer ring 12, an inner ring 13 and rolling elements 14 interposed in-between the rings, and wherein the inner ring 13 presents an inner circumferential surface 15, which surface presents a frusto-conical profile, and wherein the rolling bearing 1 is mounted on a corresponding conical seat 21 on the rotor shaft by the frusto- conical inner circumferential surface (15). The bearing assembly further comprises a first labyrinth ring 3 mounted on the shaft 2 and contacting the inner ring 13 and the outer ring 14 at an axial end portion of the rolling bearing 1, wherein the first labyrinth ring 3 seals off a space between the outer and inner ring 12, 13, and wherein the first labyrinth ring 3 further presents a conduit 31, wherein the conduit 31 ends proximate the axial end portion 16 of the inner circumferential surface 15.
Figure 2 shows a flowchart of the method according to the invention. The method comprises the steps of: - (100) pressing a liquid in-between the inner circumferential surface 15) of the inner ring 13 and the conical seat 21 to thereby facilitate the driving up of the rolling bearing 1 on the conical seat 21, - (200) driving up the rolling bearing 1) on the conical seat 21 by an axial force acting on the rolling bearing 1, - wherein the liquid is pressed in-between the two surfaces 15, 21 at an axial end portion 16 of the inner circumferential surface.

Claims (1)

10 15 20 25 30 CLAlMS 3. Method to mount a rolling bearing (1) onto a wind turbine rotor shaft (2), wherein the bearing (1) presents an outer ring (12), an inner ring (13) and rolling elements (14) interposed in-between the rings, and wherein the inner ring (13) presents an inner circumferential surface (15), which surface presents a frusto-conical profile, and wherein the rolling bearing (1) is meant to be mounted on a corresponding conical seat (21) on the rotor shaft (2) by the frusto-conical inner circumferential surface (15), the method comprising: - (100) pressing a liquid in-between the inner circumferential surface (15) of the inner ring (13) and the conical seat (21) to thereby facilitate the driving up of the rolling bearing (1) on the conical seat (21), - (200) driving up the rolling bearing (1) on the conical seat (21) by an axial force acting on the rolling bearing (1), - wherein the liquid is pressed in-between the two surfaces (15, 21) at an axial end portion (16) of the inner circumferential surface. The method according to claim 1, wherein the liquid is any of oil, synthetic oil or other non-corrosive fluid. The method according to any of the preceding claims, wherein a ring (3) is mounted on the shaft and being located adjacent to and in contact with the axial end portion of the inner ring, wherein the liquid is pressed in-between the two surfaces via a conduit (31) in the ring (3), which conduit ends proximate the axial end portion (16) of the inner circumferential surface. Wind turbine bearing assembly, comprising, - a rotor shaft (2), 10 15 20 25 30 - a rolling bearing (1), wherein the rolling bearing presents an outer ring (12), an inner ring (13) and rolling elements (14) interposed in-between the rings, and wherein the inner ring (13) presents an inner circumferential surface (15), which surface presents a frusto-conical profile, and wherein the rolling bearing (1) is mounted on a corresponding conical seat (21) on the rotor shaft by the frusto-conical inner circumferential surface (15), - wherein the bearing assembly further comprises a first ring (3) mounted on the shaft (2) and contacting at least the inner ring (13) at an axial end portion of the rolling bearing (1), and wherein the first ring (3) further presents a conduit (31), wherein the conduit (31) ends proximate the axial end portion (16) of the inner circumferential surface (15). Wind turbine bearing assembly according to claim 4, - wherein the first ring (3) is any of: - a labyrinth ring (3), wherein the labyrinth ring is contacting at least the inner ring (13) and the outer ring (14), and wherein the labyrinth ring (3) seals off a space between the outer and inner ring (12, 13), - a ring-shaped part of a bearing housing, - a seal, or - a bearing inner ring locating arrangement. Wind turbine bearing assembly according to claim 4 or 5, - wherein the assembly further presents a second labyrinth ring (4) mounted on the shaft (2) and contacting the inner ring (13) and the outer ring (14) on the other axial end portion of the rolling bearing (1), wherein the second labyrinth (4) ring seals off a second space between the outer and inner ring. Wind turbine bearing assembly according to any of claim 4 to 6, 10 further comprising a third ring (5) mounted on the shaft (2) and being adjacent the first ring (3), wherein the first ring (3), the third ring (5) and the shaft (2) are configured to create a circumferential cavity (7) in a circumferential extension around the shaft. Wind turbine bearing assembly according to claim 7, - wherein the cavity (7) is meant to act as a pressure chamber for mounting the bearing (1) on the shaft (2) by axially driving up the bearing (1) on the conical seat (21) on the shaft (1). Wind turbine bearing assembly according to any of claim 7 and 8, - wherein the shaft (2) presents a circumferential groove (8), and wherein the third ring (5) is meant to be axially fixed on the shaft between the first ring (3) and a metal wire (6) in the groove.
SE1200546A 2012-09-07 2012-09-07 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly SE1200546A1 (sv)

Priority Applications (5)

Application Number Priority Date Filing Date Title
SE1200546A SE1200546A1 (sv) 2012-09-07 2012-09-07 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly
US14/426,816 US20150240874A1 (en) 2012-09-07 2013-09-02 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly
PCT/SE2013/000135 WO2014038990A1 (en) 2012-09-07 2013-09-02 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly
JP2015531040A JP2015533980A (ja) 2012-09-07 2013-09-02 風力タービンシャフトに転がり軸受を取り付けるための方法及び風力タービン軸受組立体
CN201380044918.XA CN104583623A (zh) 2012-09-07 2013-09-02 一种在风力涡轮机的轴和风力涡轮机轴承组件上安装滚动轴承的方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE1200546A SE1200546A1 (sv) 2012-09-07 2012-09-07 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly

Publications (1)

Publication Number Publication Date
SE1200546A1 true SE1200546A1 (sv) 2012-11-07

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SE1200546A SE1200546A1 (sv) 2012-09-07 2012-09-07 Method to mount a rolling bearing on a wind turbine shaft and a wind turbine bearing assembly

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US (1) US20150240874A1 (sv)
JP (1) JP2015533980A (sv)
CN (1) CN104583623A (sv)
SE (1) SE1200546A1 (sv)
WO (1) WO2014038990A1 (sv)

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Publication number Priority date Publication date Assignee Title
DE102015218625A1 (de) * 2015-09-28 2017-03-30 Aktiebolaget Skf Dichtung für eine Radlageranordnung
DE102019106276A1 (de) * 2019-03-12 2020-09-17 Schaeffler Technologies AG & Co. KG Rotorlagerung einer Windkraftanlage Technisches Gebiet

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