WO2018026353A1 - Disposition d'articulation de pas au niveau du moyeu d'une éolienne - Google Patents

Disposition d'articulation de pas au niveau du moyeu d'une éolienne Download PDF

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Publication number
WO2018026353A1
WO2018026353A1 PCT/US2016/045083 US2016045083W WO2018026353A1 WO 2018026353 A1 WO2018026353 A1 WO 2018026353A1 US 2016045083 W US2016045083 W US 2016045083W WO 2018026353 A1 WO2018026353 A1 WO 2018026353A1
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WO
WIPO (PCT)
Prior art keywords
bearing
pitch
coupled
rotor blade
pitch bearing
Prior art date
Application number
PCT/US2016/045083
Other languages
English (en)
Inventor
Daniel Jason Erno
Norman Arnold Turnquist
Fulton Jose Lopez
Michael Colan Moscinski
Original Assignee
General Electric Company
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 General Electric Company filed Critical General Electric Company
Priority to PCT/US2016/045083 priority Critical patent/WO2018026353A1/fr
Publication of WO2018026353A1 publication Critical patent/WO2018026353A1/fr

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Classifications

    • 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
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06—Rotors
    • F03D1/065—Rotors characterised by their construction elements
    • F03D1/0691—Rotors characterised by their construction elements of the hub
    • 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
    • F05B2240/00—Components
    • F05B2240/50—Bearings
    • 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 disclosure relates generally to wind turbines and, more particularly, to improved bearing configurations for a wind turbine.
  • a modem wind turbine typically includes a tower, generator, gearbox, nacelle, and one or more rotor blades.
  • the rotor blades capture kinetic energy from wind using known airfoil principles and transmit the kinetic energy through rotational energy to turn a shaft coupling the rotor blades to a gearbox, or if a gearbox is not used, directly to the generator.
  • the generator then converts the mechanical energy to electrical energy that may be deployed to a utility grid.
  • pitch bearing a bearing disposed at the interface between the cantilevered rotor blade and the wind turbine hub.
  • pitch bearings include an inner ring, an outer ring, and two rows of balls, also referred to as rolling elements, concentrically disposed within separate raceways defined between inner and outer bearing races, with each rolling element being configured to contact its corresponding raceway at four separate contact points. This type of bearing is commonly referred to as a four-point bearing.
  • the predominant load applied to the bearing by the cantilevered blade is in the form of a moment that pries the bearing inner ring out of the outer ring.
  • any bearing that is expected to do the job of a pitch bearing should have maximum capacity for moment rather than being designed to handle pure axial or radial load. Inside a bearing, this moment translates into forces on the rolling elements that act mainly parallel to the axis of the blade.
  • normal operation of pitch bearings in wind turbines involves oscillations about a set pitch angle as opposed to continuous rotation at high speed in one direction. Under ideal loading conditions, the loads transmitted through the pitch bearing are distributed evenly over all of the rolling elements.
  • the present disclosure includes a pitch bearing configuration with the bearings of each adjacent blade supporting each other through the bearing housing.
  • the bearing configuration allows for control of rotational displacement of a rotor blade of a wind turbine to enable as much wind energy as possible to be captured.
  • a pitch bearing for a rotor blade of a wind turbine The pitch bearing configuration including a plurality of bearing housings and at least three rotor blade shafts. Each bearing housing having disposed therein at least two pitch bearing assemblies. Each of the at least two pitch bearing assemblies including at least one pitch bearing including an inner beanng race, an outer beanng race and a plurality of rolling elements disposed between the inner bearing race and the outer bearing race. Each of the rotor blade shafts is coupled at an inner end to two of the plurality of bearing housings and at an outer end to a rotor blade of the rotor. The two bearing housings coupled to each shaft of adjacent rotor blades, supports the adjacent rotor blades.
  • the pitch bearing configuration including a first bearing housing (62a), a second bearing housing (62b) and a third bearing housing, a first rotor blade shaft, a second rotor blade shaft and a third rotor blade shaft.
  • Each of the first bearing housing, the second bearing housing and the third bearing housing having disposed therein at least two pitch bearing assemblies.
  • the first rotor blade shaft is coupled at an outer end to a first rotor blade of the rotor and coupled at an inner end to the first bearing housing and the second bearing housing.
  • the second rotor blade shaft is coupled at an outer end to a second rotor blade of the rotor and coupled at an inner end to the first bearing housing and the third bearing housing.
  • the third rotor blade shaft is coupled at an outer end to a third rotor blade of the rotor and coupled at an inner end to the second bearing housing and the third bearing housing.
  • the bearing housings coupled to each shaft of adjacent rotor blades, support the adjacent rotor blade shafts.
  • the wind turbine including a tower, a hub, at least three rotor blades, a pitch bearing configuration rotatably coupling the at least three rotor blades to the hub, a plurality of bearing housings and at least three rotor blade shafts.
  • the at least three rotor blades rotatable in response to wind impinging upon said at least three rotor blades.
  • the pitch bearing configuration including a plurality of bearing housings.
  • Each of the bearing housings has disposed therein at least two pitch bearing assemblies.
  • Each of the rotor blade shafts is coupled to two of the plurality of bearing housings and a rotor blade of the at least three rotor blades.
  • Each of the two bearing housings coupled to each shaft of adjacent rotor blades, support the adjacent rotor blades.
  • FIG. 1 illustrates a perspective view of one embodiment of a wind turbine, in accordance with one or more embodiments shown or described herein;
  • FIG. 2 illustrates a perspective, internal view of the nacelle of the wind turbine shown in FIG. 1, in accordance with one or more embodiments shown or described herein;
  • FIG. 3 illustrates a perspective view of one of the rotor blades of the wind turbine shown in FIG. 1, in accordance with one or more embodiments shown or described herein;
  • FIG. 4 illustrates a partial isometric view of a portion of the wind turbine shown in
  • FIG. 1 and more particularly a plurality of rotor blades coupled to a pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 5 illustrates a partial isometric view of a portion of the wind turbine shown in
  • FIG. 1 and more particularly a pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 6 illustrates a partial cross-sectional view of a portion of the wind turbine shown in FIG. 1, and more particularly the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 7 illustrates a partial cross-sectional view of a portion of the wind turbine shown in FIG. 1, and more particularly the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 8 illustrates a partial cross-sectional view of a portion of the wind turbine shown in FIG. 1, and more particularly the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 9 illustrates a partial cross-sectional view of a portion of the wind turbine shown in FIG. 1, and more particularly the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 10 illustrates a partial isometric view of a portion of the wind turbine shown in
  • FIG. 1 and more particularly a plurality of rotor blades coupled to the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein;
  • FIG. 11 illustrates a partial isometric view of a portion of the wind turbine shown in
  • FIG. 1 and more particularly a plurality of rotor blades coupled to the pitch bearing configuration including mutual adjacent blade support, in accordance with one or more embodiments shown or described herein.
  • the present disclosure is directed to bearing configurations for a wind turbine, and more particularly to a pitch bearing configuration including mutual adj acent blade support. More particularly, the pitch bearing configuration provides for bearings of adjacent blades to support each other through a plurality of bearing housings.
  • the pitch bearing configuration of the wind turbine may include at least two pitch bearing assemblies disposed within each of a plurality of bearing housings. Each pitch bearing including a first raceway and a second raceway defined between inner and outer bearing races of the respective bearing.
  • one or more of the pitch bearing assemblies may be configured as a dual pitch bearing including a first pitch bearing and a second pitch beanng configured such that they are separated axially by a distance LB, thereby removing a significant portion of the bending moment applied to the individual bearings, and transforming substantially the entire load into radial loads.
  • Each of the pitch bearing assemblies is coupled to a rotor blade via a rotor blade shaft, with adjacent rotor blades providing support to one another through the bearing housings and the rotor blade shafts.
  • each blade structure aids in support of the other blades, rather than just itself, resulting in an overall strengthened system.
  • the disclosed bearing configuration(s) including this radial load anangement may allow the large bending and shear forces that result in the unwanted deflections of the bearing races to be minimized and prevent the ball bearings from becoming stuck in the raceways, thereby decreasing the likelihood of component damage/failure.
  • the disclosed pitch bearing configuration(s) have been uniquely configured to handle the dynamic loading of a wind turbine. Specifically, due to enatic moment loading and the fact that each bearing is mounted directly to a relatively flexible rotor blade, the bearings must be equipped to handle axial and radial loads that can vary significantly with time.
  • FIG. 1 illustrates a side view of one embodiment of a wind turbine 10.
  • the wind turbine 10 generally includes a tower 12, a nacelle 14 mounted on the tower 12, and a rotor 16 coupled to the nacelle 14.
  • the rotor 16 includes a rotatable hub 18 and at least one rotor blade 20 coupled to and extending outwardly from the hub 18.
  • the rotor 16 includes three rotor blades 20.
  • the rotor 16 may include more than three rotor blades 20.
  • Each rotor blade 20 may be spaced about the hub 18 to facilitate rotating the rotor 16 to enable kinetic energy to be transfened from the wind into usable mechanical energy, and subsequently, electrical energy.
  • the hub 18 may be rotatably coupled to an electric generator 30 (FIG. 2) positioned within the nacelle 14 to permit electrical energy to be produced.
  • FIG. 2 a simplified, internal view of one embodiment of the nacelle
  • the generator 30 may be disposed within the nacelle 14.
  • the generator 30 may be coupled to the rotor 16 of the wind turbine 10 for generating electrical power from the rotational energy generated by the rotor 16.
  • the rotor 16 may include a main rotor shaft 17 coupled to the hub 18 for rotation therewith.
  • the generator 30 may then be coupled to the main rotor shaft 17 such that rotation of the rotor shaft 17 drives the generator 30.
  • the generator 30 includes a generator shaft 32 rotatably coupled to the main rotor shaft 17 through a gearbox 34.
  • the generator shaft 32 may be rotatably coupled directly to the rotor shaft 17.
  • the generator 30 may be directly rotatably coupled to the rotor shaft 17 (often referred to as a "direct-drive wind turbine").
  • the wind turbine 10 may include one or more yaw drive mechanisms 36 mounted to and/or through a bedplate 38 positioned atop the wind turbine tower 12.
  • each yaw drive mechanism 36 may be mounted to and/or through the bedplate 38 so as to engage a yaw bearing 40 coupled between the bedplate 38 and the tower 12 of the wind turbine 10.
  • the yaw bearing 40 may be mounted to the bed plate 38 such that, as the yaw bearing 40 rotates about a yaw axis (not shown) of the wind turbine 10, the bedplate 38 and, thus, the nacelle 14 are similarly rotated about the yaw axis.
  • each yaw drive mechanism 36 may have any suitable configuration and may include any suitable components known in the art that allow such mechanisms 36 to function as described herein.
  • each yaw drive mechanism 36 may include a yaw motor 42 mounted to the bedplate 38.
  • the yaw motor 42 may be coupled to ayaw gear 44 (e.g., a pinion gear) configured to engage the yaw bearing 40.
  • the yaw motor 42 may be coupled to the yaw gear 44 directly (e.g., by an output shaft (not shown) extending through the bedplate 38) or indirectly through a suitable gear assembly coupled between the yaw motor 42 and the yaw gear 44.
  • the torque generated by the yaw motor 42 may be transmitted through the yaw gear 44 and applied to the yaw bearing 40 to permit the nacelle 14 to be rotated about the yaw axis of the wind turbine 10.
  • the illustrated wind turbine 10 is shown as including two yaw drive mechanisms 36, the wind turbine 10 may generally include any suitable number of yaw drive mechanisms 36.
  • the rotor 16 due to an aerodynamic profile on the rotor blades 20. More specifically, in the illustrated embodiment, the rotor 16 turns around a substantially horizontal rotor axis 49, which is substantially parallel to the direction of the incoming wind 48. The rotor 16 drives the generator, such that electrical energy is produced from the kinetic energy of the wind 48.
  • FIG. 3 a partial isometric view of a portion of the wind turbine shown in FIG. 1 , and more particularly a rotor blade 20 for coupling to a pitch bearing configuration, is illustrated in accordance with aspects of the disclosure disclosed herein. It is noted that a single rotor blade/shaft configuration is illustrated in FIG. 3, with the associated bearing housing removed. A body 23 of the rotor blade 20 may extend lengthwise between the blade root 21 and the blade tip 22 and may generally serve as the outer shell of the rotor blade 20.
  • the body 23 may define an aerodynamic profile (e.g., by defining an airfoil shaped cross-section, such as a symmetrical or cambered airfoil-shaped cross-section) to enable the rotor blade 20 to capture kinetic energy from the wind using known aerodynamic principles.
  • the body 23 may generally include a pressure side 24 and a suction side 25 extending between a leading edge 26 and a trailing edge 27.
  • the rotor blade 20 may have a span 28 defining the total length of the body 23 between the blade root 21 and the blade tip 22 and a chord 29 defining the total length of the body 23 between the leading edge 26 and the trailing edge 27.
  • the chord 29 may vary in length with respect to the span 28 as the body 23 extends from the blade root 21 to the blade tip 22.
  • the rotor blade 20 is coupled to a shaft 50 via the pitch bearings, to allow for rotation therewith, as will be described in greater detail below.
  • the shaft 50 is supported by bearing housings (not shown) that are shared by adjacent blades, and thus the rotor blade.
  • FIGSs 4-9 illustrated are various embodiments of a pitch bearing configuration in relation to a wind turbine blade and hub. For the sake of simplicity, only a portion of the wind turbine 10 is shown in FIGs. 4- 9. In addition, it should be noted that identical reference numerals denote the same elements throughout the various views.
  • FIG. 4 a partial, cross-sectional view of a pitch bearing
  • the pitch bearing configuration 60 includes rotor blade support for adjacent rotor blades 20a, 20b, 20c (shown in dotted lined) through a plurality of bearing housings 62.
  • the rotor 16 is comprised of three rotor blades 20a, 20b, and 20c, three rotor blade shafts 50a, 50b, and 50c, and three bearing housings 62a, 62b, and 62c.
  • Alternate embodiments may include additional rotor blades, thus requiring additional rotor blade shafts, and bearing housings.
  • a first rotor blade 20a is coupled to a first shaft 50a via a first bearing housing 62a
  • a second rotor blade 20b is coupled to a second shaft 50b via a third bearing housing 62c.
  • a third rotor blade 20c is coupled to a third shaft 50c via a second bearing housing 62b.
  • the first shaft 50a is further coupled at an innermost end 5 la to the second bearing housing 62b
  • the second shaft 50b is further coupled at an innermost end 5 lb to the first bearing housing 62a
  • the third shaft 50c is further coupled at an innermost end 5 lc to the third bearing housing 62c.
  • the second bearing housing 62b thus providing additional support to the first shaft 50a
  • the first bearing housing 62a providing additional support to the second shaft 50b
  • the third bearing housing 62c providing additional support to the third shaft 50c.
  • each of the bearing housings 62a, 62b and 62c having housed within at least two pitch bearing assemblies (described presently), so as to vastly reducing the moment load carried by any one bearing.
  • the pitch bearing configuration 60 enables the bearings of each adjacent blade to support one other through a respective bearing housing. This support results in an increase in strength in the overall rotor system in that each blade structure (blade and shaft) helps support the other blade structures, rather than just itself.
  • each of the at least two pitch bearing assemblies housed within the bearing housing 62a, 62b, 62c is configured as a two-point (2-P) contact thrust bearing assembly (described below) and may allow each rotor blade 20a, 20b, 20c to be rotated about its pitch axis 46 (e.g., via a pitch adjustment mechanism), thereby allowing the orientation of each blade 20a, 20b, 20c to be adjusted relative to the direction of the wind 48 (FIG. 1).
  • the pitch adjustment mechanism may include a pitch drive motor (e.g., an electric motor).
  • each of the rotor blade shafts 50a, 50b, 50c is coupled at an inner end 84 to two of the plurality of bearing housings 62 and at an outer end 86 to a rotor blade 20 of the rotor 16.
  • the first rotor blade shaft 50a is coupled to the first rotor blade 20a via at least one pitch bearing assembly 64a housed within the first bearing housing 62a and at least one pitch bearing assembly 64b housed within the second bearing housing 62b.
  • the second rotor blade shaft 50b is coupled to the second rotor blade 20b via at least one pitch bearing assembly 66a housed within the first bearing housing 62a and at least one pitch bearing assembly 66b housed within the third bearing housing 62c.
  • the third rotor blade shaft 50c is coupled to the rotor blade 20c via at least one pitch bearing assembly 68a housed within third bearing housing 62c and at least one pitch bearing assembly 68b housed within the second bearing housing 62b.
  • the at least one pitch bearing assembly 64a is configured in a substantially stacked radially orientation relative to the at least one pitch bearing assembly 66a within the first bearing housing 62a.
  • the at least one pitch bearing assembly 66b is configured in a substantially stacked radially orientation relative to the at least one pitch bearing assembly 68a within the third bearing housing 62c.
  • the at least one pitch bearing assembly 68b is configured in a substantially stacked radially orientation relative to the at least one pitch bearing assembly 64b within the second bearing housing 62b.
  • Each pitch bearing assembly 64a, 64b, 66a, 66b, 68a and 68b is comprised of a single pitch bearing or a dual pitch bearing, and more particularly a first pitch bearing and a second pitch bearing (described presently).
  • each pitch bearing assembly 64a, 64b, 66a, 66b, 68a and 68b may be comprised of any number of additional pitch bearings.
  • each of the pitch bearing assemblies 64a, 66a, 66b and 68a is comprised of a dual pitch bearing, and more particularly a first pitch bearing, and at least one additional pitch bearing supporting a single shaft .
  • each dual pitch bearing includes the first pitch bearing 70 and a second pitch bearing 72.
  • Alternate configuration may include additional pitch bearings.
  • the first pitch bearing 70 and the second pitch bearing 72, of each pitch bearing assembly 66a and 66b, are configured such that they are separated axially by a distance LB, thereby removing a significant portion of the bending moment applied to the first pitch bearing 70 and the second pitch bearing 72, and transforming substantially the entire load into radial loads.
  • the distance LB is determined by the distance required to reduce the load/moment requirements on the bearings to be within their design capability. In an embodiment, LB is at least 8% of the total blade length, or at least 0.5m. Additional information regarding dual pitch bearings configured as disclosed herein, may be found in, U.S. Patent Application Serial No. 15/148,231, bearing attorney docket no. 287401-1, Adam Daniel Minadeo et al., "Wind Turbine Bearings,” which is incorporated by reference herein in its entirety, and U.S. Patent Application Serial No. 15/166,565, bearing attorney docket no. 310872-1, Michael Colan Moscinski, et al., "Wind Turbine Bearings,” which is incorporated by reference herein in its entirety.
  • each of the first pitch bearing 70 and the second pitch bearing 72 includes an outer bearing race 74, an inner bearing race 76, defining a plurality of raceway grooves (not shown), and a plurality of rolling elements 78 disposed between the outer and inner bearing races 74, 76.
  • the outer bearing race 74 may generally be configured to be mounted to the bearing housing 62 via suitable fastening mechanisms.
  • the inner bearing race 76 may be configured to be mounted to an exterior surface 80 of the shaft 50a, 50b, 50c using any suitable fastening
  • the inner bearing races 76 housed within the bearing housings 62a and 62c may be coupled to the exterior surface 80 of the shaft 50b utilizing known coupling means such as, but not limited to, press fit, wedge, and/or a combination of known coupling means.
  • first pitch bearing 70 and the second pitch bearing 72 housed within each of the bearing housings 62 and associated with a single shaft 50a, 50b, 50c are separated axially by a distance LB, thereby removing a significant portion of the bending moment applied to the bearings 70, 72, and transforming substantially the entire load into one or more radial loads. More particularly, the inclusion of the first pitch bearing 70 and the second pitch bearing 72 enables the reduction of forces and moments at the bearing location, as well as reduction of blade tip deflections.
  • a spacer 82 is disposed between the first pitch bearing 70 and the second pitch bearing 72 of each bearing assembly 64a, 64b (FIG. 5), 66a, 66b, 68a and 68b (FIG. 5) housed within a single bearing housing 62.
  • the spacer 82 may also be referred to herein as a load tube.
  • the spacer 82 is disposed so as to couple the inner bearing races 76 of the first pitch bearing 70 and the second pitch bearing 72 and maintain spacing therebetween.
  • the outer bearing race 74 of each of the first pitch bearing 70 and the second pitch bearing 72 may be configured to be rotated relative to the inner bearing race 76 (via the rolling elements 78) to allow the pitch angle of each rotor blades 20a, 20b, 20c to be adjusted.
  • Such relative rotation of the outer and inner bearing races 74, 76 may be achieved using a pitch adjustment mechanism (not shown), mounted to the shaft(s) or proximate thereto.
  • the pitch adjustment mechanism may include any suitable components and may have any suitable configuration that allows the mechanism to function.
  • the pitch adjustment mechanism may include a pitch drive motor (e.g., an electric motor) (not shown), a pitch drive gearbox (not shown), and a pitch drive pinion (not shown).
  • the pitch drive motor may be coupled to the pitch drive gearbox so that the motor imparts mechanical force to the gearbox.
  • the gearbox may be coupled to the pitch drive pinion for rotation therewith.
  • the pinion may, in turn, be in rotational engagement with the inner bearing races 76 to result in rotation of the inner bearing races 76 relative to the outer bearing race 74 and, thus, rotation of the rotor blades 20a, 20b, 20c relative to the hub 18 (FIG. 1).
  • each shaft is supported by a pitch bearing assembly disposed in a first bearing housing and a pitch bearing assembly disposed in a second bearing housing. More particularly, in this particular embodiment each shaft is supported by a single pitch bearing disposed in a first bearing housing and a dual pitch bearing disposed in the second bearing housing.
  • the bearing housing 62a has disposed therein the bearing assembly 66a, comprised of a single pitch bearing 73 and the bearing housing 62c has disposed therein the bearing assembly 66b comprised of a dual pitch bearing, and more particularly, a first pitch bearing 70, and at least one additional pitch bearing 72.
  • the outermost bearing housing associated with a shaft (closest to the blade), and more particularly the bearing housing 62a, has housed therein the single pitch bearing 73, with the innermost bearing housing associated with a shaft, and more particularly the bearing housing 62c, having housed therein the dual pitch bearing, and more particularly, the first pitch bearing 70, and the second pitch bearing 72.
  • each of the first pitch bearings 70 and the at least one additional, or second, pitch bearing 72 includes an outer bearing race 74, an inner bearing race 76, defining a plurality of raceway grooves (not shown), and a plurality of rolling elements 78 disposed between the outer and inner bearing races 74, 76.
  • the outer bearing race 74 may generally be configured to be mounted to the bearing housing 62 via suitable fastening mechanisms.
  • the inner bearing race 76 may be configured to be mounted to an exterior surface 80 of the shaft 50a, 50b, 50c using any suitable fastening mechanisms.
  • the outer bearing race 74 may be configured to be rotated relative to the inner bearing race 76 (via the rolling elements 78) to allow the pitch angle of each rotor blades 20a, 20b, 20c to be adjusted.
  • Such relative rotation of the outer and inner bearing races 74, 76 may be achieved using a pitch adjustment mechanism (not shown), mounted to the shaft(s) or proximate thereto.
  • each shaft is supported by a pitch bearing assembly disposed in a first bearing housing and a pitch bearing assembly disposed in a second bearing housing. More particularly, in this particular embodiment each shaft is supported by a dual pitch bearing disposed in a first bearing housing and a single pitch bearing disposed in the second bearing housing.
  • the bearing housing 62a has disposed therein the bearing assembly 66a, comprised of a dual pitch bearing, and more particularly, a first pitch bearing 70, and at least one additional pitch bearing 72 and the bearing housing 62c has disposed therein the bearing assembly 66b comprised of a single pitch bearing 73.
  • the outermost bearing housing associated with a shaft (closest to the blade), and more particularly the bearing housing 62a, has housed therein the dual pitch bearing, and more particularly, the first pitch bearing 70, and the second pitch bearing 72, with the innermost bearing housing associated with a shaft, and more particularly the bearing housing 62c, having housed therein the single pitch bearing 73.
  • each of the pitch bearings 70 and the at least one additional, or second, pitch bearing 72 includes an outer bearing race 74, an inner bearing race 76, defining a plurality of raceway grooves (not shown), and a plurality of rolling elements 78 disposed between the outer and inner bearing races 74, 76.
  • the outer bearing race 74 may generally be configured to be mounted to the bearing housing 62 via suitable fastening mechanisms.
  • the inner bearing race 76 may be configured to be mounted to an exterior surface 80 of the shaft 50a, 50b, 50c using any suitable fastening mechanisms.
  • the outer bearing race 74 may be configured to be rotated relative to the inner bearing race 76 (via the rolling elements 78) to allow the pitch angle of each rotor blades 20a, 20b, 20c to be adjusted.
  • Such relative rotation of the outer and inner bearing races 74, 76 may be achieved using a pitch adjustment mechanism (not shown), mounted to the shaft(s) or proximate thereto.
  • each shaft is supported by a pitch bearing assembly disposed in a first bearing housing and a pitch bearing assembly disposed in a second bearing housing. More particularly, in this particular embodiment a single pitch bearing is disposed in each bearing housing supporting a shaft. As best illustrated with regard to shaft 50b, the bearing housing 62a has disposed therein a single pitch bearing 73 and the bearing housing 62c has disposed therein a single pitch bearing 73. In this particular embodiment, both bearing housings associated with a single shaft have housed therein the single pitch bearing 73.
  • each of the pitch bearings 73 includes an outer bearing race 74, an inner bearing race 76, defining a plurality of raceway grooves (not shown), and a plurality of rolling elements 78 disposed between the outer and inner bearing races 74, 76.
  • the inner and outer bearing races 74, 76 may be mounted to the bearing housings and shafts as previously described with the outer bearing race 74 configured to be rotated relative to the inner bearing race 76 (via the rolling elements 78) to allow the pitch angle of each rotor blades 20a, 20b, 20c to be adjusted.
  • FIGs. 10 and 11 illustrated are two bearing configurations, each having a plurality of blades 20 attached thereto, illustrating the blades 20 in a first operable stage 100 and in a second operable stage 150, whereby a blade pitch angle has been changed to address an oncoming change in the wind 48.
  • pitch bearing configuration incorporating thrust bearing technology and an adjacent blade support configuration that solves many issues in current bearing designs
  • the pitch bearing configuration disclosed herein offers several advantages over existing pitch bearing designs, including, but not limited to: i) the reduction of forces and moments at the bearing location, as well as reduction of blade tip deflections; ii) minimization of the potato chip effect on the race bearing helping prevent ball bearings from becoming stuck in the race; iii) ability to handle larger diameter rotors; iv) higher reliability (v) increase strength in the overall rotor/bearing configuration by allowing the hub to hold the maximum length of shaft to reduce reaction forces in the bearings, while making a stiffer system due to the mutual support the blades give each other; and v) cost saving.

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  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
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  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

L'invention concerne une configuration de l'articulation de pas pour le rotor d'une éolienne. La configuration de l'articulation de pas comprend une pluralité de boites à roulement, chacun comportant au moins deux ensembles d'articulation de pas. La configuration comprend en outre au moins trois arbres de pales de rotor, chacun étant couplé à deux de la pluralité des boites de roulement et à une pale du rotor. Les deux boites à roulement couplés à chaque arbre des pales de rotor adjacentes, supportent les arbres de pales de rotor adjacents. La configuration d'articulation de pas réduit au minimum la charge de moment sur les articulations de pas à l'intérieur de chaque boite de roulement. L'invention concerne également une éolienne comprenant cette configuration d'articulation de pas.
PCT/US2016/045083 2016-08-02 2016-08-02 Disposition d'articulation de pas au niveau du moyeu d'une éolienne WO2018026353A1 (fr)

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PCT/US2016/045083 WO2018026353A1 (fr) 2016-08-02 2016-08-02 Disposition d'articulation de pas au niveau du moyeu d'une éolienne

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PCT/US2016/045083 WO2018026353A1 (fr) 2016-08-02 2016-08-02 Disposition d'articulation de pas au niveau du moyeu d'une éolienne

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WO2018026353A1 true WO2018026353A1 (fr) 2018-02-08

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100086409A1 (en) * 2008-10-08 2010-04-08 David Anthony Whiley Wind turbine rotor
US20100143136A1 (en) * 2009-08-31 2010-06-10 Jeffrey Michael Daniels Systems and methods for assembling a pitch assembly for use in a wind turbine
US7939961B1 (en) * 2010-04-28 2011-05-10 General Electric Company Wind turbine with integrated design and controlling method
EP3023634A1 (fr) * 2014-11-24 2016-05-25 Blade Dynamics Limited Moyeu pour une éolienne

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100086409A1 (en) * 2008-10-08 2010-04-08 David Anthony Whiley Wind turbine rotor
US20100143136A1 (en) * 2009-08-31 2010-06-10 Jeffrey Michael Daniels Systems and methods for assembling a pitch assembly for use in a wind turbine
US7939961B1 (en) * 2010-04-28 2011-05-10 General Electric Company Wind turbine with integrated design and controlling method
EP3023634A1 (fr) * 2014-11-24 2016-05-25 Blade Dynamics Limited Moyeu pour une éolienne

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