WO2006129351A1 - 旋回輪軸受構造 - Google Patents
旋回輪軸受構造 Download PDFInfo
- Publication number
- WO2006129351A1 WO2006129351A1 PCT/JP2005/009993 JP2005009993W WO2006129351A1 WO 2006129351 A1 WO2006129351 A1 WO 2006129351A1 JP 2005009993 W JP2005009993 W JP 2005009993W WO 2006129351 A1 WO2006129351 A1 WO 2006129351A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rolling element
- outer ring
- ring portion
- slewing
- ring bearing
- Prior art date
Links
- 238000005096 rolling process Methods 0.000 claims abstract description 97
- 230000036316 preload Effects 0.000 claims abstract description 15
- 230000002093 peripheral effect Effects 0.000 claims description 17
- 238000000605 extraction Methods 0.000 claims 1
- 238000009826 distribution Methods 0.000 description 52
- 238000005315 distribution function Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 102220047090 rs6152 Human genes 0.000 description 1
Classifications
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- 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
- F16C19/02—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
- F16C19/14—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load
- F16C19/18—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls
-
- 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
- F03D7/00—Controlling wind motors
- F03D7/02—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor
- F03D7/022—Adjusting aerodynamic properties of the blades
- F03D7/0224—Adjusting blade pitch
-
- 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
- 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
- F16C19/34—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 both radial and axial load
- F16C19/38—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 both radial and axial load with two or more rows 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
- 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
- F16C19/44—Needle bearings
- F16C19/46—Needle bearings with one row or needles
-
- 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
- F16C19/50—Other types of ball or roller bearings
- F16C19/505—Other types of ball or roller bearings with the diameter of the rolling elements of one row differing from the diameter of those of another row
-
- 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
- F16C33/30—Parts of ball or roller bearings
- F16C33/58—Raceways; Race rings
-
- 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
- F16C41/00—Other accessories, e.g. devices integrated in the bearing not relating to the bearing function as such
- F16C41/02—Arrangements for equalising the load on a plurality of bearings or their elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05B2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05B2260/79—Bearing, support or actuation arrangements therefor
-
- 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
- F16C2229/00—Setting preload
-
- 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
-
- 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
Definitions
- the present invention relates to a slewing ring bearing structure, and more particularly, to a slewing ring bearing having a double row.
- a wind turbine generator is a rotating machine that converts wind energy into electric power.
- the wind turbine generator includes a support tower, a wind turbine base 102 that is pivotably supported by the support tower, and an impeller base (rotor head) 103 that is rotatably supported by the wind turbine base 102. It consists of and.
- a plurality of blades (three blades in this example) 104A, 104B, 104C are supported by the rotor head 103 so as to be pivotable (variable in pitch) via the swivel bearings 105A, 105B, 105C, respectively.
- the slewing ring bearing 105B is formed of a non-slewing outer ring 106 on the rotor head side and a slewing inner ring 107 on the blade side.
- An annular rolling element row 108 is interposed between the outer ring 106 and the inner ring 107.
- the rolling element as an element of the rolling element row 108 has a shape of a rolling force S ball or a substantially cylindrical surface or a drum surface rolling roller.
- the rotating ring bearing 105B that supports one of the three blades 104B shown in Fig. 1 has an external force Fxb in the axial direction XB, a rotational moment Mxb around the axial direction XB, and an external force Fyb in the axial direction YB. Then, the rotational moment Myb around the axial direction YB, the external force Fzb in the radiation direction ZB perpendicular to the rotational axis of the rotor head 103, and the rotational moment Mzb around the radial direction ZB act.
- Such two-dimensional three-dimensional forces generate surface pressures on a large number of rolling elements of the outer ring 106, the inner ring 107, and the rolling element row 108.
- Such a surface pressure acts as a deformation force on the outer ring 106, the inner ring 107, and the rolling element row 108.
- Such deformation force is expressed as a distribution function of the circumferential position corresponding to the ball numbers of a large number of rolling elements arranged on the same circumference, and the ball load received by the rolling element or the surface pressure at that position is , Not constant but fluctuating greatly.
- Such deformation force appears as a cause of improper friction generated in the slewing ring bearings 105A, 105B, 105C, and shortens the life of the slewing ring bearing.
- an insertion hole is provided in the radial direction of the outer ring or the inner ring, and the rolling elements are inserted. It is described that the preload amount gradually increases as the roller is inserted, but there is no description about the preload amount for each power train.
- a wind turbine blade is disclosed in JP-A-7-310645.
- the blade portion is supported by the rotor head via the slewing ring bearing so that the pitch is variable, and the slewing ring bearing simultaneously supports the radial load and the thrust load.
- This slewing ring bearing is a single row bearing. Disclosure of the invention
- An object of the present invention is to provide a slewing ring bearing that simultaneously realizes double-row slewing ring bearings and surface pressure equalization (ball load equalization).
- Another object of the present invention is to provide a slewing ring bearing that achieves equalizing of the surface pressure by double-slewing the slewing ring bearing and making the proper load distribution equal to the load.
- Still another object of the present invention is to provide a slewing ring bearing that realizes equalization of surface pressure when the slewing ring bearing is double-rowed and the load is not evenly distributed.
- Still another object of the present invention is to provide a wind turbine generator using the above-described slewing ring bearing.
- the slewing ring bearing is provided on the inner side of the outer ring portion, the outer ring portion having first and second circumferential grooves formed on the inner circumferential surface in parallel, and the outer ring portion
- An inner ring portion having first and second circumferential grooves formed on the outer peripheral surface in parallel to correspond to the first and second circumferential grooves, and the first circumferential groove of the outer ring portion and the A first rolling element row provided in the first circumferential groove of the inner ring portion, a second rolling element provided in the second circumferential groove of the outer ring portion and the second circumferential groove of the inner ring portion.
- the inner ring part rotates around the rotation axis in a direction opposite to the outer ring part.
- the first preload on the rolling element of the first rolling element row is applied to the rolling element of the second rolling element row. Greater than the second preload.
- the first preload to the rolling elements of the first rolling element row corresponding to the first outer peripheral part is greater than the second preload to the rolling elements of the second rolling element row corresponding to the second outer peripheral part. Big thing preferable.
- the radial thickness of the first outer peripheral portion of the outer ring portion may be smaller than the radial thickness of the second outer peripheral portion of the outer ring portion.
- the first diameter in the radial direction of the rolling element of the first rolling element may be larger than the second diameter in the radial direction of the rolling element of the second rolling element.
- the width of the outer ring portion in the rotation axis direction may be equal to the width of the inner ring portion in the rotation axis direction, and the width of the outer ring portion in the rotation axis direction may be equal to the rotation axis of the inner ring portion. It may be wider than the width in the direction.
- the outer ring portion When the width of the outer ring portion in the rotation axis direction is wider than the width of the inner ring portion in the rotation axis direction, the outer ring portion is connected to a surface of the outer ring portion orthogonal to the rotation axis direction. Furthermore, you may comprise.
- the inner ring portion may further include a side plate coupled to the surface of the outer ring portion orthogonal to the rotation axis direction.
- interlocking body of the first and second rolling element rows may be a ball or a mouth.
- a wind turbine generator is configured to connect a rotor head connected to a wind power extracting rotary shaft, a plurality of blades, and each of the plurality of blades to the rotor head. And the above-described slewing ring bearing.
- FIG. 1 is a perspective view showing a known slewing ring bearing structure.
- FIG. 2 is a perspective view showing a known slewing ring bearing.
- FIG. 3 is a perspective view showing a slewing ring bearing structure showing an object to which the present invention is applied.
- FIG. 4 is a perspective sectional view of a part of FIG.
- FIG. 5 is a cross-sectional view showing a region division of the slewing ring bearing.
- FIG. 6 is a cross-sectional view showing a realization state of a slewing ring bearing structure for a wind turbine according to the present invention.
- FIG. 7 is a cross-sectional view showing another embodiment of a wind turbine slewing ring bearing structure according to the present invention.
- FIG. 8 is a cross-sectional view showing still another embodiment of the wind turbine slewing ring bearing structure according to the present invention.
- FIG. 9 is a cross-sectional view showing still another embodiment of the wind turbine slewing ring bearing structure according to the present invention.
- FIG. 10 is a cross-sectional view showing still another embodiment of the wind turbine slewing ring bearing structure according to the present invention.
- Fig. 11 is a graph showing ball load distribution of a slewing ring bearing structure for a wind turbine according to the present invention.
- FIG. 12 is a drawing showing another ball load distribution of a slewing ring bearing structure for a wind turbine according to the present invention.
- FIG. 13 is a graph showing the surface pressure distribution of the wind turbine slewing ring bearing structure according to the present invention.
- FIG. 14 is a graph showing another surface pressure distribution of the slewing ring bearing structure for wind turbines according to the present invention.
- FIG. 15 is a graph showing still another ball load distribution of the slewing ring bearing structure for wind turbines according to the present invention.
- FIG. 16 is a graph showing still another ball load distribution of the slewing ring bearing structure for wind turbines according to the present invention.
- FIG. 17 is a graph showing still another surface pressure distribution of the slewing ring bearing structure for wind turbines according to the present invention.
- FIG. 18 is a graph showing still another surface pressure distribution of the slewing ring bearing structure for wind turbines according to the present invention.
- FIG. 3 is a perspective view showing the structure of the swirl ring bearing for wind turbines according to the first embodiment of the present invention.
- the impeller body (rotor head) 1 is provided with a wind power take-off rotating shaft 2 and three sets of slewing ring bearings 3.
- Three variable pitch blades (not shown) are supported by three sets of slewing ring bearings 3 respectively.
- Each of the three sets of slewing ring bearings 3 They are arranged at equiangular intervals of 120 degrees on the same plane.
- the slewing ring bearing 3 is formed of an outer ring 4 fixed to the rotor head 1 and an inner ring 5 fixed to the blade.
- a first rolling element row 6 and a second rolling element row 7 are interposed between the inner peripheral surface of the outer ring 4 and the outer peripheral surface of the inner ring 5.
- Each rolling element of the first rolling element row 6 and the second rolling element row 7 has a shape like a ball or a roller.
- the first rolling element row 6 and the second rolling element row 7 are separated by a distance D in the axial direction of the turning axis L.
- the retainers that hold the respective rolling elements of the first rolling element row 6 and the second rolling element row 7 are formed as a single body or as an integrated body with the outer ring 4 or the inner ring 5. Rolling balls and spherical rollers can be used for JIJ as the first rolling element row 6 and the second rolling element row 7.
- Fig. 5 shows that the load fl and the load f2 are distributed in the direction of the swivel axis with the load even or uneven, and the surface pressure in the circumferential direction is equalized (the surface pressure difference distribution is flattened). Indicates the area. Coordinates in the circumferential direction are expressed using ball numbers assigned to balls that are a plurality of rolling elements arranged on the same circumference. Accordingly, the circumferential coordinate is discretized.
- the outer ring 4 formed integrally is virtually divided into a first outer ring portion 8 corresponding to the first rolling element row 6 and a second outer ring portion 9 corresponding to the second rolling element row 7 in the direction of the turning axis. Divided.
- the integrally formed inner ring 5 is virtually divided into a first inner ring portion 11 corresponding to the first rolling element row 6 and a second inner ring portion 12 corresponding to the second rolling element row 7 in the turning axis direction.
- the first outer ring portion 8 and the second outer ring portion 9 are divided in the direction of the turning axis by a virtual center plane S orthogonal to the turning axis L.
- the first inner ring portion 11 and the second inner ring portion 12 are divided by the virtual center plane S in the direction of the turning axis.
- FIG. 6 shows an example of load distribution in the structure of the slewing ring bearing for wind turbine to which the present invention is applied.
- the diameter of the balls of the first rolling element row 6 is the second The diameter is preferably smaller than the diameter of the balls in the rolling element row 7. Since the rigidity of the balls in the second rolling element row 7 is greater than the rigidity of the balls in the first rolling element row 6, the larger the ball diameter, the greater the load carrying capacity of the balls.
- the deformation degree or internal stress distribution of the first outer ring portion 8 and the second outer ring portion 9 can be equalized. Since a part of the load f 2 that is larger than the load fl is distributed to the first rolling element row 6, In this example, the surface pressure distribution is flattened regardless of the uneven load distribution.
- FIG. 7 shows another example of load distribution in a wind turbine slewing ring bearing structure to which the present invention is applied.
- the diameters of the balls of the first rolling element row 6 and the second rolling element row 7 are the same.
- the load f2 acting on the outer peripheral surface of the second outer ring portion 9 is greater than the load fl acting on the outer peripheral surface of the first outer ring portion 8
- the rigidity of the second outer ring portion 9 is greater than that of the first outer ring portion 8.
- the thickness in the radial direction of the first outer ring portion 8 is set to be greater than the thickness in the radial direction of the second outer ring portion 9 so as to be greater than the rigidity.
- FIG. 8 shows still another example of the load distribution of the wind turbine slewing ring bearing structure to which the present invention is applied.
- This example is the same as the embodiment of FIG. 7 in that the shapes of the outer ring 4 and the inner ring 5 are adjusted.
- the magnitude relation of the width of the outer ring 4 and the inner ring 5 in the direction of the turning axis is determined.
- the magnitude relation of the width in the turning axis direction of the first outer ring part 8 and the second outer ring part 9, or the turning axis direction of the first inner ring part 11 and the second inner ring part 12 The size relationship of the width of is defined.
- load equalization is realized.
- FIG. 9 shows still another example of the load distribution of the wind turbine slewing ring bearing to which the present invention is applied. Based on the magnitude relationship between fl and f 2, a slight difference AR is given to the ball diameter R1 of the first rolling element row 6 and the ball diameter R2 of the second rolling element row 7.
- a first rolling element row 6 and a second rolling element row 7 are provided between the outer ring 4 and the inner ring 5, and the first rolling element row 6 and the second rolling element row 7 are strongly clamped between the outer ring 4 and the inner ring 5.
- the load fl acting on the outer peripheral surface of the first outer ring portion 8 is larger than the load f 2 acting on the outer peripheral surface of the second outer ring portion 9, and in this case, the ball 7 having a slightly larger ball diameter is used. Since the preload of the ball is large, the rigidity of the ball 7 is increased. As a result, a larger load is applied to the larger rigidity, and the load is evenly distributed between the first rolling element row 6 and the second rolling element row 7.
- the bearing surface pressure can be equalized and the surface pressure difference distribution can be flattened.
- the preload adjustment concept of this example although not shown, there is a slight difference between the diameter R1 ′ of the annular row of the first rolling element row 6 and the diameter R2 ′ of the annular row of the second rolling element row 7.
- the bearing surface pressure distribution can be equalized (flattened) between both rows.
- FIG. 10 shows still another example of load equalization.
- An annular plate (side plate) 13 having a thickness determined based on the magnitude relationship between fl and f2 is attached to the side peripheral surface of the first outer ring portion 8, and an annular plate having a thickness determined based on the magnitude relationship between fl and f2.
- (Side plate) 13 ′ is attached to the side peripheral surface of the second outer ring portion 9.
- the thickness 13 ′ is determined based on the size relationship between fl and f2
- the thickness 13 ′ is determined based on the size relationship between fl and f 2.
- the ring plate 13 ′ is attached to the side peripheral surface of the second inner ring portion 12.
- the thickness of the ring plate 13 attached to the first outer ring portion 8 and the thickness of the ring plate 13 ′ attached to the first inner ring portion 11 may be adjusted based on the magnitude relationship between fl and f2.
- the thickness of the ring plate 13 attached to the second outer ring portion 9 and the thickness of the ring plate 13 ′ attached to the second inner ring portion 12 may be adjusted based on the magnitude relationship between fl and f2.
- the load distribution can be realized by adjusting the rigidity.
- the ring plate may be provided only in the outer ring portion 4 or only in the inner ring portion 5. Further, the ring plate may extend to the vicinity of the rotation shaft so as not to interfere with the rotation shaft coupled to the inner ring portion 5.
- FIGS. 11 to 14 show the FEM analysis results of the load distributed by the load distribution described above.
- the horizontal axis is the angular coordinate for one round of the inner and outer rings, and is discretized by the ball number.
- Fig. 11 shows the ball load distribution on the rotor head side when FEM analysis is performed with different fl and f 2 distribution ratios.
- the ball load on the rotor head side is larger than the ball load on the wing side.
- the ball load distribution when a normal load with a distribution rate of 50% is applied is larger than the ball load distribution when a normal load with a distribution rate of 59% or a distribution rate of 61% is applied. Is kept small.
- FIG. 13 shows the surface pressure distribution on the rotor head side corresponding to the ball load distribution shown in FIG.
- the surface pressure distribution when a normal load with a distribution rate of 50% is applied is compared to the surface pressure distribution when a normal load with a distribution rate of 59% or a distribution rate of 61% is applied. Is kept small. In this way, these values are kept small on the side where the ball load distribution and surface pressure distribution are large, and they increase on the small side. Both distributions are flattened. Figures 12 and 14 show that the ball load difference distribution and the surface pressure difference fabric in both rows are flattened, and that the equal distribution is the proper distribution.
- FIGS. 15 to 18 show the FEM analysis results of the load when the ring plates (one top plate) 13 and 13 ′ shown in FIG. 10 are added.
- the distribution ratio is 48%, which is close to 50%, the ball load and the surface pressure are large.
- the ball load difference distribution and the surface pressure difference distribution are generally further flattened on the rotor head side. Show! /
- the load capacity of the bearing is increased, and some load unevenness can be absorbed.
- the integration of the cage of the first rolling element row 6 and the cage of the second rolling element row 7 is effective for equalizing (flattening) the surface pressure. It is effective to equalize the ball load on one circle.
- both the rolling surface of the outer ring 4 and the rolling surface of the inner ring 5 are formed in a non-circular shape, or one of the outer ring 4 and the inner ring 5 is formed in a non-circular shape, and By adjusting the preload applied, the bearing surface pressure distribution can be equalized (flattened).
- the surface pressure difference distribution is flattened by flattening the load difference distribution, and the double-row slewing ring bearing and the surface pressure equalization are realized simultaneously. be able to. Thereby, it is possible to evenly distribute the load shared by the outer ring and the inner ring corresponding to the double row rolling element rows.
- Load equalization is realized when the double row slewing ring bearing has high rigidity or the total rigidity (bearing rigidity + support rigidity) corresponding to each rolling element row is equal.
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- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Rolling Contact Bearings (AREA)
- Wind Motors (AREA)
Abstract
Description
Claims
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020107005952A KR101022104B1 (ko) | 2005-05-31 | 2005-05-31 | 풍력 터빈용 선회 베어링 구조체 및 풍력 발전 장치 |
KR1020077028035A KR100967640B1 (ko) | 2005-05-31 | 2005-05-31 | 풍력 터빈용 선회 베어링 구조체 및 풍력 발전 장치 |
MX2007015178A MX2007015178A (es) | 2005-05-31 | 2005-05-31 | Estructura de cojinete de giro. |
EP05745857A EP1887237A4 (en) | 2005-05-31 | 2005-05-31 | ROLLING ANNULAR BEARING |
CN200580049970XA CN101194110B (zh) | 2005-05-31 | 2005-05-31 | 旋转环轴承结构 |
CA 2610407 CA2610407C (en) | 2005-05-31 | 2005-05-31 | Slewing bearing structure |
AU2005332456A AU2005332456B2 (en) | 2005-05-31 | 2005-05-31 | Structure of slewing ring bearing |
US11/916,106 US7927019B2 (en) | 2005-05-31 | 2005-05-31 | Slewing bearing structure |
PCT/JP2005/009993 WO2006129351A1 (ja) | 2005-05-31 | 2005-05-31 | 旋回輪軸受構造 |
EP20120182556 EP2532904A3 (en) | 2005-05-31 | 2005-05-31 | Structure of slewing ring bearing |
Applications Claiming Priority (1)
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PCT/JP2005/009993 WO2006129351A1 (ja) | 2005-05-31 | 2005-05-31 | 旋回輪軸受構造 |
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WO2006129351A1 true WO2006129351A1 (ja) | 2006-12-07 |
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PCT/JP2005/009993 WO2006129351A1 (ja) | 2005-05-31 | 2005-05-31 | 旋回輪軸受構造 |
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US (1) | US7927019B2 (ja) |
EP (2) | EP2532904A3 (ja) |
KR (2) | KR100967640B1 (ja) |
CN (1) | CN101194110B (ja) |
AU (1) | AU2005332456B2 (ja) |
CA (1) | CA2610407C (ja) |
MX (1) | MX2007015178A (ja) |
WO (1) | WO2006129351A1 (ja) |
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WO2009147865A1 (ja) * | 2008-06-06 | 2009-12-10 | Ntn株式会社 | 旋回軸受およびその軌道溝加工方法 |
JP4484964B2 (ja) * | 2007-09-28 | 2010-06-16 | Thk株式会社 | 旋回リング |
EP2045464A3 (en) * | 2007-10-01 | 2012-05-16 | Siemens Aktiengesellschaft | Pitch bearing for wind turbine rotor blades |
EP2985458A1 (en) | 2014-08-12 | 2016-02-17 | Mitsubishi Heavy Industries, Ltd. | Slewing bearing device for a wind turbine |
US10429316B2 (en) | 2016-01-11 | 2019-10-01 | Teknologisk Institut | Method and device for scanning of objects using a combination of spectral ranges within vision, near infrared light and X-rays |
JP2021528598A (ja) * | 2018-05-18 | 2021-10-21 | ムハマッド、イブラヒム | 風力発電施設のロータブレード用の回転結合構造 |
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- 2005-05-31 EP EP20120182556 patent/EP2532904A3/en not_active Withdrawn
- 2005-05-31 US US11/916,106 patent/US7927019B2/en active Active
- 2005-05-31 KR KR1020077028035A patent/KR100967640B1/ko not_active IP Right Cessation
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- 2005-05-31 KR KR1020107005952A patent/KR101022104B1/ko not_active IP Right Cessation
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Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
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JPWO2009041311A1 (ja) * | 2007-09-28 | 2011-01-27 | Thk株式会社 | 旋回リング |
JP4484964B2 (ja) * | 2007-09-28 | 2010-06-16 | Thk株式会社 | 旋回リング |
US7967511B2 (en) | 2007-09-28 | 2011-06-28 | Thk Co., Ltd. | Rotation ring |
US8322928B2 (en) | 2007-10-01 | 2012-12-04 | Siemens Aktiengesellschaft | Pitch bearing for wind turbine rotor blades |
EP2045464A3 (en) * | 2007-10-01 | 2012-05-16 | Siemens Aktiengesellschaft | Pitch bearing for wind turbine rotor blades |
EP2045464B2 (en) † | 2007-10-01 | 2016-08-24 | Siemens Aktiengesellschaft | Pitch bearing for wind turbine rotor blades |
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EP3085957A1 (en) | 2014-08-12 | 2016-10-26 | Mitsubishi Heavy Industries, Ltd. | Slewing bearing device for a wind turbine |
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JP2021528598A (ja) * | 2018-05-18 | 2021-10-21 | ムハマッド、イブラヒム | 風力発電施設のロータブレード用の回転結合構造 |
JP7032607B2 (ja) | 2018-05-18 | 2022-03-08 | ムハマッド、イブラヒム | 風力発電施設のロータブレード用の回転結合構造 |
Also Published As
Publication number | Publication date |
---|---|
US7927019B2 (en) | 2011-04-19 |
US20090016665A1 (en) | 2009-01-15 |
AU2005332456B2 (en) | 2010-02-25 |
CN101194110A (zh) | 2008-06-04 |
AU2005332456A1 (en) | 2006-12-07 |
CA2610407A1 (en) | 2006-12-07 |
EP2532904A3 (en) | 2012-12-19 |
EP2532904A2 (en) | 2012-12-12 |
CA2610407C (en) | 2013-01-08 |
KR20100035186A (ko) | 2010-04-02 |
EP1887237A1 (en) | 2008-02-13 |
KR101022104B1 (ko) | 2011-03-17 |
KR100967640B1 (ko) | 2010-07-07 |
CN101194110B (zh) | 2011-04-20 |
KR20080009738A (ko) | 2008-01-29 |
MX2007015178A (es) | 2008-02-19 |
EP1887237A4 (en) | 2011-11-02 |
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