US20110142630A1 - Wind turbine pitch-angle control device and method thereof - Google Patents

Wind turbine pitch-angle control device and method thereof Download PDF

Info

Publication number
US20110142630A1
US20110142630A1 US12/521,014 US52101408A US2011142630A1 US 20110142630 A1 US20110142630 A1 US 20110142630A1 US 52101408 A US52101408 A US 52101408A US 2011142630 A1 US2011142630 A1 US 2011142630A1
Authority
US
United States
Prior art keywords
wind turbine
pitch
turbine blades
angle control
control device
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
US12/521,014
Inventor
Yoshiyuki Hayashi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Assigned to MITSUBISHI HEAVY INDUSTRIES, LTD. reassignment MITSUBISHI HEAVY INDUSTRIES, LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HAYASHI, YOSHIYUKI
Publication of US20110142630A1 publication Critical patent/US20110142630A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022Adjusting aerodynamic properties of the blades
    • F03D7/0224Adjusting blade pitch
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022Adjusting aerodynamic properties of the blades
    • F03D7/024Adjusting aerodynamic properties of the blades of individual blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/0264Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for stopping; controlling in emergency situations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/0264Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for stopping; controlling in emergency situations
    • F03D7/0268Parking or storm protection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00Control
    • F05B2270/10Purpose of the control system
    • F05B2270/109Purpose of the control system to prolong engine life
    • F05B2270/1095Purpose of the control system to prolong engine life by limiting mechanical stresses
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00Control
    • F05B2270/30Control parameters, e.g. input parameters
    • F05B2270/328Blade pitch angle
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the present invention relates to a wind turbine pitch-angle control device for individually controlling pitch angles of wind turbine blades and to a method thereof.
  • the wind turbine in controlling a wind turbine, the wind turbine is halted when the wind speed exceeds a cutout wind speed at which operation should be halted or when an abnormality, such as acceleration or excessive power output, occurs.
  • the pitch angles of the wind turbine blades are moved from operating state positions to a feathering position (for example, refer to Patent Document 1).
  • the pitch angles of the wind turbine blades do not necessarily match when the wind turbine is halted.
  • the wind turbine blades may be moved from different pitch angles to the feathering position (see FIG. 8 ).
  • the aerodynamic load increases due to an imbalance in the loads on the wind turbine blades.
  • the present invention was conceived to solve the above-described problem, and an object therefor is to provide a pitch-angle control method of wind turbine blades, a device thereof, and a wind turbine that are capable of reducing aerodynamic load when the wind turbine is halted.
  • the present invention employs the following solutions.
  • a first aspect of the present invention is a wind turbine pitch-angle control device configured to carry out individual pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades, wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
  • a representative wind turbine blade when the wind turbine halt command is input, a representative wind turbine blade may be identified on the basis of the pitch angle from among the plurality of wind turbine blades, the pitch angle of the representative wind turbine blade and the pitch angles of the other wind turbine blades may be matched, and then the pitch angles of the wind turbine blades may be moved to the feathering position.
  • the pitch angles of the wind turbine blades can be matched efficiently.
  • the wind turbine blade whose pitch angle may be closest to the feathering position is identified as the representative wind turbine blade.
  • the pitch angles of the wind turbine blades can be moved to the feathering position efficiently.
  • the pitch angles of the wind turbine blades other than the representative wind turbine blade and the pitch angle of the representative wind turbine blade may be matched.
  • the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade while carrying out control for adjusting the pitch angle of the representative wind turbine blade closer to the feathering position. In this way, the time required for moving the pitch angles to the feathering position is reduced compared with when the movement of the pitch angle of the representative wind turbine blade is stopped.
  • the wind turbine blades may be moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
  • pitch angles of the wind turbine blades are moved on the basis of the common pitch-angle command after the pitch angles of the wind turbine blades are matched, control can be simplified, and the aerodynamic load on the wind turbine blades can be reduced.
  • a second aspect of the present invention is a wind turbine including the wind turbine pitch-angle control device described above.
  • a third aspect of the present invention is a wind turbine pitch-angle control method for carrying out independent pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades, wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
  • the present invention is advantageous in that aerodynamic load can be reduced while the wind turbine is halted.
  • FIG. 1 illustrates, in outline, the configuration of a wind turbine according to an embodiment of the present invention.
  • FIG. 2 illustrates the configuration in the periphery of a wind turbine pitch-angle control device according an embodiment of the present invention.
  • FIG. 3 illustrates an operation flow of a wind turbine pitch-angle control device according to an embodiment of the present invention.
  • FIG. 4 illustrates an example of the time-sequential change in pitch angles of wind turbine blades when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 5 illustrates an example of the time-sequential change in pitch angles of wind turbine blades when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 6 illustrates an example of hub load when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 7 illustrates an example of hub load when pitch-angles are controlled individually without matching the pitch angles of the respective wind turbine blades.
  • FIG. 8 illustrates an example of the time-sequential change in the pitch angles of wind turbine blades when the pitch angles of the wind turbine blades are moved to a feathering position by individual control without matching the pitch angles of the wind turbine blades.
  • FIG. 1 is a block diagram illustrating, in outline, the configuration of the wind turbine according to this embodiment.
  • a wind turbine 1 has a tower 2 vertically provided on a base 6 , a nacelle 3 provided at the upper end of the tower 2 , and a rotor head 4 provided on the nacelle 3 in such a manner that it is rotatable around a substantially horizontal axis.
  • Three wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 are attached, in a radial pattern, around the rotational axis of the rotor head 4 .
  • a wind turbine pitch-angle control device 10 (see FIG. 2 ) according to this embodiment is, for example, accommodated inside the nacelle 3 .
  • the pitch-angle control device 10 is equipped with, for example, a central processing unit (CPU), a random access memory (RAM), a read only memory (ROM), and a hard disk drive (HDD).
  • CPU central processing unit
  • RAM random access memory
  • ROM read only memory
  • HDD hard disk drive
  • the pitch-angle control method of the wind turbine blades described below is realized by reading out a control program, which is stored in the HDD or the like, into the RAM or the like and executing it on the CPU.
  • the wind turbine pitch-angle control device 10 acquires actual pitch angles of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 as input information and outputs pitch-angle command values ⁇ com+ ⁇ 1 , ⁇ com+ ⁇ 2 , and ⁇ com+ ⁇ 3 of the wind turbine blades as output information.
  • ⁇ com is a common pitch angle, which is a value common to all wind turbine blades.
  • ⁇ 1 , ⁇ 2 , and ⁇ 3 are adjustment amounts that are set according to the wind turbine blades; for example, they are set to correspond to the loads on the wind turbine blades and the operating environment etc. of the wind turbine, such as wind speed and wind direction.
  • the pitch-angle command value ⁇ com+ ⁇ 1 is provided to a driving device 11 - 1 for drive control of the pitch angle of the wind turbine blade 5 - 1 ;
  • the pitch-angle command value ⁇ com+ ⁇ 2 is provided to a driving device 11 - 2 for drive control of the pitch angle of the wind turbine blade 5 - 2 ;
  • the pitch-angle command value ⁇ com+ ⁇ 3 is provided to a driving device 11 - 3 for drive control of the pitch angle of the wind turbine blade 5 - 3 .
  • the pitch angles of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 are controlled by operating the driving devices 11 - 1 , 11 - 2 , and 11 - 3 in response to the input pitch-angle control values.
  • the driving devices 11 - 1 , 11 - 2 , and 11 - 3 are each constructed of an actuator or the like having a fluid-pressure cylinder, etc.
  • a wind turbine halt command is generated at another control device, which is not shown, when the wind speed exceeds the cutout wind speed at which operation should be halted or when an abnormality such as acceleration or excessive power output occurs.
  • the pitch-angle command values for the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 are calculated so as to move the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 to the feathering positions.
  • the feathering position is a position in which the blade surface of a wind turbine blade is substantially parallel to the wind direction. At this position, it is possible to achieve a condition in which the effect of the wind power is minimized.
  • the feathering position can be arbitrarily set within a pitch angle range that achieves the condition in which the effect of the wind power is substantially minimized. In this embodiment, the feathering position is set to, for example, 110°.
  • the position where the blade surface of a wind turbine blade is substantially perpendicular to the wind direction, i.e., a state most affected by wind is defined as a pitch angle of 20°.
  • the pitch-angle control method of the wind turbine blades when a wind turbine halt command is input is described below with reference to FIG. 3 .
  • the pitch-angle control device 10 compares the actual pitch angles of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 and determines whether or not the pitch angles of the wind turbine blades substantially match (Step SA 1 in FIG. 3 ). Specifically, the differences of the pitch angles are calculated by comparing two pitch angles of the wind turbine blades at a time. It is determined whether the maximum value of these differences is smaller than a reference value set in advance.
  • Step SA 2 in FIG. 3 the wind turbine blade whose actual pitch angle is closest to 110° is identified as the representative wind turbine blade.
  • the pitch-angle command values of the wind turbine blades are determined by setting a minimum adjustment amount ⁇ LOW set in advance as the adjustment amount ⁇ 1 corresponding to the wind turbine blade 5 - 1 , which is the representative wind turbine blade, and by setting a maximum adjustment amount ⁇ HIGH set in advance as the adjustment amounts ⁇ 2 and ⁇ 3 corresponding to the other wind turbine blades 5 - 2 and 5 - 3 (Step SA 3 in FIG. 3 ).
  • the adjustment amounts of the wind turbine blades whose pitch angle difference with respect to the representative wind turbine blade is less than a predetermined value are set to the minimum adjustment amount ⁇ LOW .
  • the pitch angle difference, relative to the pitch angle of the representative wind turbine blade, of a wind turbine blade whose pitch angle is within a predetermined range can be prevented from increasing.
  • the ⁇ HIGH is preferable to set to, for example, the capacity limit of each driving device or a value close to the limit. By setting it to such a value, the pitch angles of the wind turbine blades other than the representative wind turbine blade can be efficiently and quickly matched to the pitch angle of the representative wind turbine blade.
  • the minimum adjustment amount ⁇ LOW may be set to a value smaller than the maximum adjustment value, for example, zero. By setting the minimum adjustment amount ⁇ LOW to a value other than zero, the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade while carrying out control for adjusting the pitch angle of the representative wind turbine blade closer to the feathering position, and thus the wind turbine blades can be efficiently moved to the feathering position.
  • the minimum adjustment amount ⁇ LOW is set to 1 (°/s)
  • the maximum adjustment amount ⁇ HIGH is set to 7 (°/s).
  • the pitch-angle command values of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 set in this way are output to the driving devices 11 - 1 , 11 - 2 , and 11 - 3 , respectively (Step SA 4 in FIG. 3 ).
  • control of the pitch angles based on these pitch-angle command values is carried out by the driving devices 11 - 1 , 11 - 2 , and 11 - 3 , and, as a result, the actual pitch angles of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 change.
  • the pitch-angle command values corresponding to the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 are set to a common value by setting the adjustment values ⁇ 1 to ⁇ 3 of the wind turbine blades 5 - 1 , in FIG. 3 ). In this way, after the pitch angles of the wind turbine blades 5 - 1 , 5 - 2 , and 5 - 3 match, the pitch angles of the wind turbine blades can be moved in synchronization to the feathering position.
  • the pitch-angle command values are set to value close to the limit of the driving devices 11 - 1 , 11 - 2 , and 11 - 3 , the pitch angles of the wind turbine blades can be efficiently and quickly moved to the feathering position.
  • the wind turbine blade closest to the feathering position (closest to the fine side) is identified as the representative wind turbine blade.
  • the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade by slowly moving the pitch angle of the representative wind turbine blade and quickly moving the pitch angles of the other wind turbine blades, as shown in FIG. 4 .
  • the three wind turbine blades can be moved in synchronization to the feathering position by controlling the pitch angles of the wind turbine blades on the basis of the common pitch-angle command value, as shown in FIG. 5 .
  • FIG. 6 illustrates the load on a hub when the pitch angles of the wind turbine blades are controlled by the wind turbine pitch-angle control device and the method thereof according to this embodiment, described above.
  • FIG. 7 illustrates the load on the hub when, for example, the pitch angles are individually moved to the feathering position without matching the pitch angles of the wind turbine blades, as shown in FIG. 8 .
  • the horizontal axis represents time
  • the vertical axis represents hub load.
  • the maximum value of the hub load in FIG. 6 is 5458 kNm
  • the maximum value of the hub load in FIG. 7 is 5958 kNm.
  • a load reduction effect of 9% was achieved by employing the wind turbine pitch-angle control device according to this embodiment and the method thereof.
  • the common pitch angle ⁇ com for the wind turbine blades may be set to zero.
  • the wind turbine blades can be controlled by the maximum adjustment amount ⁇ HIGH or minimum adjustment amount ⁇ LOW . In this way, since the moving speed of the representative wind turbine blade can be decreased even more, the pitch angles of the wind turbine blades can be matched even more quickly.
  • the wind turbine blade whose pitch angle is closest to the feathering position is identified as the representative wind turbine blade.
  • another wind turbine blade may be identified as the representative wind turbine blade, and the pitch angles of the other wind turbine blades may be matched to this representative wind turbine blade.
  • the adjustment amount of the representative wind turbine blade is set to the minimum adjustment amount, and the adjustment amounts of the other wind turbine blades are set to the maximum adjustment amount.
  • the adjustment amounts of the other wind turbine blades may be increased, in stages, starting from the one furthest from the feathering position.
  • the pitch angles of the wind turbine blades should be matched before the pitch angles of the wind turbine blades reach the feathering position, and then, after the pitch angles are matched, the pitch angles of the wind turbine blades may be moved in synchronization.
  • the procedure of matching the pitch angles of the wind turbine blades should be selected arbitrarily.

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Wind Motors (AREA)

Abstract

The object is to reduce aerodynamic load when a wind turbine is halted. When a wind turbine halt command is input, pitch angles of wind turbine blades 5-1, 5-2, and 5-3 are matched, and then the pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 are moved to a feathering position.

Description

    RELATED APPLICATIONS
  • The present application is based on, and claims priority from, International Application Number PCT/JP2008/059048 filed May 16, 2008, the disclosure of which is hereby incorporated by reference herein in its entirety.
  • TECHNICAL FIELD
  • The present invention relates to a wind turbine pitch-angle control device for individually controlling pitch angles of wind turbine blades and to a method thereof.
  • BACKGROUND ART
  • Conventionally, in controlling a wind turbine, the wind turbine is halted when the wind speed exceeds a cutout wind speed at which operation should be halted or when an abnormality, such as acceleration or excessive power output, occurs. When the wind turbine is halted, the pitch angles of the wind turbine blades are moved from operating state positions to a feathering position (for example, refer to Patent Document 1).
  • PATENT DOCUMENT 1
    • Japanese Unexamined Patent Application, Publication No. 2006-16984
    DISCLOSURE OF INVENTION
  • When an independent pitch control method for individually controlling the pitch angles of the respective wind turbine blades is employed, the pitch angles of the wind turbine blades do not necessarily match when the wind turbine is halted. Thus, for example, the wind turbine blades may be moved from different pitch angles to the feathering position (see FIG. 8). When wind turbine blades are moved from different pitch angles to the feathering position in this way, there is a problem in that the aerodynamic load increases due to an imbalance in the loads on the wind turbine blades.
  • The present invention was conceived to solve the above-described problem, and an object therefor is to provide a pitch-angle control method of wind turbine blades, a device thereof, and a wind turbine that are capable of reducing aerodynamic load when the wind turbine is halted.
  • To solve the above-described problem, the present invention employs the following solutions.
  • A first aspect of the present invention is a wind turbine pitch-angle control device configured to carry out individual pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades, wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
  • By performing control in this way, when a wind turbine halt command is input, the pitch angles of the wind turbine blades can be moved to the feathering position with the pitch angles being matched. In this way, aerodynamic load generated by an imbalance in the pitch angles can be reduced.
  • In the above-described wind turbine pitch-angle control device, when the wind turbine halt command is input, a representative wind turbine blade may be identified on the basis of the pitch angle from among the plurality of wind turbine blades, the pitch angle of the representative wind turbine blade and the pitch angles of the other wind turbine blades may be matched, and then the pitch angles of the wind turbine blades may be moved to the feathering position.
  • In this way, by identifying the representative wind turbine blade from among a plurality of wind turbine blades and controlling the pitch angles of the other wind turbine blades so as to match the pitch angles to the pitch angle of the representative wind turbine blade, the pitch angles of the wind turbine blades can be matched efficiently.
  • More specifically, for example, the wind turbine blade whose pitch angle may be closest to the feathering position is identified as the representative wind turbine blade.
  • In this way, since the wind turbine blade whose pitch angle is closest to the feathering position is identified as the representative wind turbine blade and the pitch angles of the other wind turbine blades are matched to the pitch angle of the representative wind turbine blade, the pitch angles of the wind turbine blades can be moved to the feathering position efficiently.
  • In the above-described wind turbine pitch-angle control device, by setting the moving speed of the pitch angle of the representative wind turbine blade smaller than the moving speeds of the pitch angles of the wind turbine blades other than the representative wind turbine blade, the pitch angles of the wind turbine blades other than the representative wind turbine blade and the pitch angle of the representative wind turbine blade may be matched.
  • In this way, by setting the moving speed of the pitch angle of the representative wind turbine blade smaller than the moving speeds of the pitch angles of the wind turbine blades other than the representative wind turbine blade, the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade while carrying out control for adjusting the pitch angle of the representative wind turbine blade closer to the feathering position. In this way, the time required for moving the pitch angles to the feathering position is reduced compared with when the movement of the pitch angle of the representative wind turbine blade is stopped.
  • In the above-described wind turbine pitch-angle control device, after the pitch angles of the wind turbine blades are matched, the wind turbine blades may be moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
  • Since the pitch angles of the wind turbine blades are moved on the basis of the common pitch-angle command after the pitch angles of the wind turbine blades are matched, control can be simplified, and the aerodynamic load on the wind turbine blades can be reduced.
  • A second aspect of the present invention is a wind turbine including the wind turbine pitch-angle control device described above.
  • A third aspect of the present invention is a wind turbine pitch-angle control method for carrying out independent pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades, wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
  • The present invention is advantageous in that aerodynamic load can be reduced while the wind turbine is halted.
  • BRIEF DESCRIPTION OF DRAWINGS
  • FIG. 1 illustrates, in outline, the configuration of a wind turbine according to an embodiment of the present invention.
  • FIG. 2 illustrates the configuration in the periphery of a wind turbine pitch-angle control device according an embodiment of the present invention.
  • FIG. 3 illustrates an operation flow of a wind turbine pitch-angle control device according to an embodiment of the present invention.
  • FIG. 4 illustrates an example of the time-sequential change in pitch angles of wind turbine blades when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 5 illustrates an example of the time-sequential change in pitch angles of wind turbine blades when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 6 illustrates an example of hub load when a pitch-angle control method of a wind turbine according to an embodiment of the present invention is employed.
  • FIG. 7 illustrates an example of hub load when pitch-angles are controlled individually without matching the pitch angles of the respective wind turbine blades.
  • FIG. 8 illustrates an example of the time-sequential change in the pitch angles of wind turbine blades when the pitch angles of the wind turbine blades are moved to a feathering position by individual control without matching the pitch angles of the wind turbine blades.
  • BEST MODE FOR CARRYING OUT THE INVENTION
  • An embodiment of a pitch-angle control method of a wind turbine blade, a device therefor, and a wind turbine according to the present invention will be described below with reference to the drawings.
  • FIG. 1 is a block diagram illustrating, in outline, the configuration of the wind turbine according to this embodiment. As shown in FIG. 1, a wind turbine 1 has a tower 2 vertically provided on a base 6, a nacelle 3 provided at the upper end of the tower 2, and a rotor head 4 provided on the nacelle 3 in such a manner that it is rotatable around a substantially horizontal axis. Three wind turbine blades 5-1, 5-2, and 5-3 are attached, in a radial pattern, around the rotational axis of the rotor head 4. In this way, the force of the wind striking the wind turbine blades 5-1, 5-2, and 5-3 from the direction of the rotational axis of the rotor head 4 is converted to a motive force that rotates the rotor head 4 around the rotational axis. This motive energy is converted to electrical energy by a power generator.
  • A wind turbine pitch-angle control device 10 (see FIG. 2) according to this embodiment is, for example, accommodated inside the nacelle 3. The pitch-angle control device 10 is equipped with, for example, a central processing unit (CPU), a random access memory (RAM), a read only memory (ROM), and a hard disk drive (HDD). The pitch-angle control method of the wind turbine blades described below is realized by reading out a control program, which is stored in the HDD or the like, into the RAM or the like and executing it on the CPU.
  • As shown in FIG. 2, the wind turbine pitch-angle control device 10 acquires actual pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 as input information and outputs pitch-angle command values Δcom+Δθ1, Δcom+Δθ2, and Δcom+Δθ3 of the wind turbine blades as output information.
  • The above-mentioned Δcom is a common pitch angle, which is a value common to all wind turbine blades. Δθ1, Δθ2, and Δθ3 are adjustment amounts that are set according to the wind turbine blades; for example, they are set to correspond to the loads on the wind turbine blades and the operating environment etc. of the wind turbine, such as wind speed and wind direction.
  • The pitch-angle command value Δcom+Δθ1 is provided to a driving device 11-1 for drive control of the pitch angle of the wind turbine blade 5-1; the pitch-angle command value Δcom+Δθ2 is provided to a driving device 11-2 for drive control of the pitch angle of the wind turbine blade 5-2; and the pitch-angle command value Δcom+Δθ3 is provided to a driving device 11-3 for drive control of the pitch angle of the wind turbine blade 5-3. In this way, the pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 are controlled by operating the driving devices 11-1, 11-2, and 11-3 in response to the input pitch-angle control values. The driving devices 11-1, 11-2, and 11-3 are each constructed of an actuator or the like having a fluid-pressure cylinder, etc.
  • In such a wind turbine pitch-angle control device 10, a wind turbine halt command is generated at another control device, which is not shown, when the wind speed exceeds the cutout wind speed at which operation should be halted or when an abnormality such as acceleration or excessive power output occurs.
  • When the wind turbine pitch-angle control device 10 receives such a wind turbine halt command, the pitch-angle command values for the wind turbine blades 5-1, 5-2, and 5-3 are calculated so as to move the wind turbine blades 5-1, 5-2, and 5-3 to the feathering positions. Here, the feathering position is a position in which the blade surface of a wind turbine blade is substantially parallel to the wind direction. At this position, it is possible to achieve a condition in which the effect of the wind power is minimized. Furthermore, the feathering position can be arbitrarily set within a pitch angle range that achieves the condition in which the effect of the wind power is substantially minimized. In this embodiment, the feathering position is set to, for example, 110°. Furthermore, in this embodiment, the position where the blade surface of a wind turbine blade is substantially perpendicular to the wind direction, i.e., a state most affected by wind, is defined as a pitch angle of 20°.
  • The pitch-angle control method of the wind turbine blades when a wind turbine halt command is input is described below with reference to FIG. 3.
  • First, when a wind turbine halt command is input, the pitch-angle control device 10 compares the actual pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 and determines whether or not the pitch angles of the wind turbine blades substantially match (Step SA1 in FIG. 3). Specifically, the differences of the pitch angles are calculated by comparing two pitch angles of the wind turbine blades at a time. It is determined whether the maximum value of these differences is smaller than a reference value set in advance.
  • As a result, when the pitch angles of the wind turbine blades do not substantially match (“NO” in Step SA1 in FIG. 3), subsequently, the wind turbine blade whose actual pitch angle is closest to the feathering position is identified as a representative wind turbine blade (Step SA2 in FIG. 3). In this way, the wind turbine blade whose actual pitch angle is closest to 110° is identified as the representative wind turbine blade.
  • Descriptions will be provided below for when the wind turbine blade 5-1 is identified as the representative wind turbine blade.
  • Subsequently, the pitch-angle command values of the wind turbine blades are determined by setting a minimum adjustment amount ΔθLOW set in advance as the adjustment amount Δθ1 corresponding to the wind turbine blade 5-1, which is the representative wind turbine blade, and by setting a maximum adjustment amount ΔθHIGH set in advance as the adjustment amounts Δθ2 and Δθ3 corresponding to the other wind turbine blades 5-2 and 5-3 (Step SA3 in FIG. 3).
  • At this time, the adjustment amounts of the wind turbine blades whose pitch angle difference with respect to the representative wind turbine blade is less than a predetermined value are set to the minimum adjustment amount ΔθLOW. In this way, the pitch angle difference, relative to the pitch angle of the representative wind turbine blade, of a wind turbine blade whose pitch angle is within a predetermined range can be prevented from increasing.
  • It is preferable to set the ΔθHIGH to, for example, the capacity limit of each driving device or a value close to the limit. By setting it to such a value, the pitch angles of the wind turbine blades other than the representative wind turbine blade can be efficiently and quickly matched to the pitch angle of the representative wind turbine blade. Moreover, the minimum adjustment amount ΔθLOW may be set to a value smaller than the maximum adjustment value, for example, zero. By setting the minimum adjustment amount ΔθLOW to a value other than zero, the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade while carrying out control for adjusting the pitch angle of the representative wind turbine blade closer to the feathering position, and thus the wind turbine blades can be efficiently moved to the feathering position.
  • In this embodiment, for example, the minimum adjustment amount ΔθLOW is set to 1 (°/s), and the maximum adjustment amount ΔθHIGH is set to 7 (°/s).
  • Next, the pitch-angle command values of the wind turbine blades 5-1, 5-2, and 5-3 set in this way are output to the driving devices 11-1, 11-2, and 11-3, respectively (Step SA4 in FIG. 3). In this way, control of the pitch angles based on these pitch-angle command values is carried out by the driving devices 11-1, 11-2, and 11-3, and, as a result, the actual pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 change.
  • When the pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 substantially match by repeating the processing described above (“YES” in Step SA1), subsequently, the pitch-angle command values corresponding to the wind turbine blades 5-1, 5-2, and 5-3 are set to a common value by setting the adjustment values Δθ1 to Δθ3 of the wind turbine blades 5-1, in FIG. 3). In this way, after the pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 match, the pitch angles of the wind turbine blades can be moved in synchronization to the feathering position. Moreover, at this time, since the pitch-angle command values are set to value close to the limit of the driving devices 11-1, 11-2, and 11-3, the pitch angles of the wind turbine blades can be efficiently and quickly moved to the feathering position.
  • Then, when the pitch angles of the wind turbine blades 5-1, 5-2, and 5-3 match the feathering position (110°) (“YES” in Step SA6 in FIG. 3), the processing ends.
  • As described above, in the wind turbine pitch-angle control device according to this embodiment and the method thereof, when a wind turbine halt command is input, the wind turbine blade closest to the feathering position (closest to the fine side) is identified as the representative wind turbine blade. By setting the pitch-angle command value of this representative wind turbine blade smaller than the pitch-angle command values of the other wind turbine blades, the pitch angles of the other wind turbine blades can be matched to the pitch angle of the representative wind turbine blade by slowly moving the pitch angle of the representative wind turbine blade and quickly moving the pitch angles of the other wind turbine blades, as shown in FIG. 4. Then, after the pitch angles of the three wind turbine blades are matched, the three wind turbine blades can be moved in synchronization to the feathering position by controlling the pitch angles of the wind turbine blades on the basis of the common pitch-angle command value, as shown in FIG. 5.
  • FIG. 6 illustrates the load on a hub when the pitch angles of the wind turbine blades are controlled by the wind turbine pitch-angle control device and the method thereof according to this embodiment, described above. Furthermore, FIG. 7 illustrates the load on the hub when, for example, the pitch angles are individually moved to the feathering position without matching the pitch angles of the wind turbine blades, as shown in FIG. 8. In FIGS. 6 and 7, the horizontal axis represents time, and the vertical axis represents hub load. In this way, the maximum value of the hub load in FIG. 6 is 5458 kNm, and the maximum value of the hub load in FIG. 7 is 5958 kNm. As a result, a load reduction effect of 9% was achieved by employing the wind turbine pitch-angle control device according to this embodiment and the method thereof.
  • An embodiment of the present invention has been described in detail above with reference to the drawings. However, the detailed structure is not limited to this embodiment, and design modifications, etc. that do not depart from the scope of the present invention are also included.
  • For example, in this embodiment, when a wind turbine halt command is input, the common pitch angle Δcom for the wind turbine blades may be set to zero. By setting the common pitch angle Δcom to zero, the wind turbine blades can be controlled by the maximum adjustment amount ΔθHIGH or minimum adjustment amount ΔθLOW. In this way, since the moving speed of the representative wind turbine blade can be decreased even more, the pitch angles of the wind turbine blades can be matched even more quickly.
  • In this embodiment, the wind turbine blade whose pitch angle is closest to the feathering position is identified as the representative wind turbine blade. Instead, however, another wind turbine blade may be identified as the representative wind turbine blade, and the pitch angles of the other wind turbine blades may be matched to this representative wind turbine blade.
  • In this embodiment, the adjustment amount of the representative wind turbine blade is set to the minimum adjustment amount, and the adjustment amounts of the other wind turbine blades are set to the maximum adjustment amount. However, it is not limited to this example, and the adjustment amounts of the other wind turbine blades may be increased, in stages, starting from the one furthest from the feathering position. In other words, in the present invention, to move the pitch angles of the wind turbine blades to the feathering position, the pitch angles of the wind turbine blades should be matched before the pitch angles of the wind turbine blades reach the feathering position, and then, after the pitch angles are matched, the pitch angles of the wind turbine blades may be moved in synchronization. The procedure of matching the pitch angles of the wind turbine blades should be selected arbitrarily.

Claims (18)

1. A wind turbine pitch-angle control device configured to carry out individual pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades,
wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
2. The wind turbine pitch-angle control device according to claim 1, wherein, when the wind turbine halt command is input, a representative wind turbine blade is identified on the basis of the pitch angle from among the plurality of wind turbine blades, the pitch angle of the representative wind turbine blade and the pitch angles of the other wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to the feathering position.
3. The wind turbine pitch-angle control device according to claim 2, wherein the wind turbine blade whose pitch angle is closest to the feathering position is identified as the representative wind turbine blade.
4. The wind turbine pitch-angle control device according to claim 3, wherein, by setting the moving speed of the pitch angle of the representative wind turbine blade smaller than the moving speeds of the pitch angles of the wind turbine blades other than the representative wind turbine blade, the pitch angles of the wind turbine blades other than the representative wind turbine blade and the pitch angle of the representative wind turbine blade are matched.
5. The wind turbine pitch-angle control device according to claim 1, wherein, after the pitch angles of the wind turbine blades are matched, the wind turbine blades are moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
6. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 1.
7. A wind turbine pitch-angle control method for carrying out independent pitch-angle control for individually controlling pitch angles of a plurality of wind turbine blades,
wherein, when a wind turbine halt command is input, the pitch angles of the wind turbine blades are matched, and then the pitch angles of the wind turbine blades are moved to a feathering position.
8. The wind turbine pitch-angle control device according to claim 2, wherein, after the pitch angles of the wind turbine blades are matched, the wind turbine blades are moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
9. The wind turbine pitch-angle control device according to claim 3, wherein, after the pitch angles of the wind turbine blades are matched, the wind turbine blades are moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
10. The wind turbine pitch-angle control device according to claim 4, wherein, after the pitch angles of the wind turbine blades are matched, the wind turbine blades are moved to the feathering position by controlling the wind turbine blades using a common pitch-angle control command.
11. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 1.
12. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 2.
13. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 3.
14. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 4.
15. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 5.
16. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 8.
17. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 9.
18. A wind turbine comprising:
the wind turbine pitch-angle control device according to claim 10.
US12/521,014 2008-05-16 2008-05-16 Wind turbine pitch-angle control device and method thereof Abandoned US20110142630A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2008/059048 WO2009139066A1 (en) 2008-05-16 2008-05-16 Windmill pitch angle controller and method for controlling windmill pitch angle

Publications (1)

Publication Number Publication Date
US20110142630A1 true US20110142630A1 (en) 2011-06-16

Family

ID=41318448

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/521,014 Abandoned US20110142630A1 (en) 2008-05-16 2008-05-16 Wind turbine pitch-angle control device and method thereof

Country Status (11)

Country Link
US (1) US20110142630A1 (en)
EP (1) EP2290232B1 (en)
JP (1) JP4875750B2 (en)
KR (1) KR101115278B1 (en)
CN (1) CN101715515A (en)
AU (1) AU2008334195C1 (en)
CA (1) CA2670279C (en)
DK (1) DK2290232T3 (en)
PT (1) PT2290232E (en)
TW (1) TW200949069A (en)
WO (1) WO2009139066A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140064961A1 (en) * 2012-09-06 2014-03-06 Delta Electronics, Inc. Method for backing up and recovering blade zero point of pitch drive system for wind turbine and pitch drive system for wind turbine
US20150086360A1 (en) * 2012-04-23 2015-03-26 Vestas Wind Systems A/S Method for controlling a wind turbine during shutdown
US20150110596A1 (en) * 2012-05-02 2015-04-23 General Electric Company System and method for stopping the operation of wind turbine
US9976539B2 (en) 2014-06-11 2018-05-22 General Electric Company Control method and system for wind turbine
DE102018007997A1 (en) * 2018-10-10 2020-04-16 Senvion Gmbh Method and system for operating a wind turbine
US10823144B2 (en) 2013-07-08 2020-11-03 Vestas Wind Systems A/S Method for controlling a wind turbine during safety operation
DE102019117934A1 (en) * 2019-07-03 2021-01-07 aerodyn product + license GmbH Method for the aerodynamic power control of a wind energy installation having a plurality of rotor blades

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2010201706A1 (en) 2010-02-08 2011-08-25 Mitsubishi Heavy Industries, Ltd. Wind turbine generator and blade pitch angle control method thereof
US10030630B2 (en) 2013-04-22 2018-07-24 Vestas Wind Systems A/S Method for controlling a wind turbine during shutdown
KR101475274B1 (en) * 2013-07-19 2014-12-22 삼성중공업 주식회사 Pitch control system and method of wind generator
ES2668502T3 (en) * 2014-03-05 2018-05-18 Nordex Energy Gmbh Procedure for the operation of a wind power plant
EP2937559A1 (en) 2014-04-25 2015-10-28 Moog Unna GmbH Method for an emergency feathering drive
CN105836085B (en) * 2016-03-28 2017-09-19 武汉船用机械有限责任公司 The control method and device of a kind of adjustable pitch propeller
CN106224161A (en) * 2016-07-19 2016-12-14 沈阳华创风能有限公司 Independent pitch system and change oar method with controller strategy
CN108443065A (en) * 2018-03-06 2018-08-24 浙江运达风电股份有限公司 A kind of Large-scale Wind Turbines independent feathering control optimization method
CN114829767A (en) 2019-11-21 2022-07-29 维斯塔斯风力系统集团公司 Stopping a wind turbine rotor based on a stored pitch angle signal
CN110844030A (en) * 2019-11-22 2020-02-28 中国船舶重工集团公司第七0四研究所 Pitch feedback signal acquisition and processing method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4462753A (en) * 1982-06-22 1984-07-31 United Technologies Corporation Blade feathering system for wind turbines
US6783326B2 (en) * 2001-08-20 2004-08-31 General Electric Company Means for adjusting the rotor blade of a wind power plant rotor
WO2006007838A1 (en) * 2004-07-23 2006-01-26 Vestas Wind Systems A/S Method of controlling the pitch velocity of a wind turbine blade and control system therefore
US20090047129A1 (en) * 2005-05-31 2009-02-19 Shigeo Yoshida Horizontal axis wind turbine
US20090148286A1 (en) * 2007-12-06 2009-06-11 General Electric Company Apparatus and method for reducing asymmetric rotor loads in wind turbines during shutdown

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4076123B2 (en) * 2002-01-07 2008-04-16 富士重工業株式会社 Windmill pitch alignment adjustment method
JP4468751B2 (en) 2004-06-30 2010-05-26 富士重工業株式会社 Horizontal axis wind turbine and its standby method
JP4690829B2 (en) * 2005-08-30 2011-06-01 富士重工業株式会社 Horizontal axis windmill
DE102005034899A1 (en) * 2005-07-26 2007-02-01 Repower Systems Ag Wind energy plant with single pitch devices
US7488155B2 (en) * 2005-11-18 2009-02-10 General Electric Company Method and apparatus for wind turbine braking

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4462753A (en) * 1982-06-22 1984-07-31 United Technologies Corporation Blade feathering system for wind turbines
US6783326B2 (en) * 2001-08-20 2004-08-31 General Electric Company Means for adjusting the rotor blade of a wind power plant rotor
WO2006007838A1 (en) * 2004-07-23 2006-01-26 Vestas Wind Systems A/S Method of controlling the pitch velocity of a wind turbine blade and control system therefore
US20090047129A1 (en) * 2005-05-31 2009-02-19 Shigeo Yoshida Horizontal axis wind turbine
US20090148286A1 (en) * 2007-12-06 2009-06-11 General Electric Company Apparatus and method for reducing asymmetric rotor loads in wind turbines during shutdown

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150086360A1 (en) * 2012-04-23 2015-03-26 Vestas Wind Systems A/S Method for controlling a wind turbine during shutdown
US9709033B2 (en) * 2012-04-23 2017-07-18 Vestas Wind Systems A/S Method for controlling a wind turbine during shutdown
US20150110596A1 (en) * 2012-05-02 2015-04-23 General Electric Company System and method for stopping the operation of wind turbine
US9726147B2 (en) * 2012-05-02 2017-08-08 General Electric Company System and method for stopping the operation of wind turbine
US20140064961A1 (en) * 2012-09-06 2014-03-06 Delta Electronics, Inc. Method for backing up and recovering blade zero point of pitch drive system for wind turbine and pitch drive system for wind turbine
US9453498B2 (en) * 2012-09-06 2016-09-27 Delta Electronics, Inc. Method for backing up and recovering blade zero point of pitch drive system for wind turbine and pitch drive system for wind turbine
US10823144B2 (en) 2013-07-08 2020-11-03 Vestas Wind Systems A/S Method for controlling a wind turbine during safety operation
US9976539B2 (en) 2014-06-11 2018-05-22 General Electric Company Control method and system for wind turbine
DE102018007997A1 (en) * 2018-10-10 2020-04-16 Senvion Gmbh Method and system for operating a wind turbine
DE102019117934A1 (en) * 2019-07-03 2021-01-07 aerodyn product + license GmbH Method for the aerodynamic power control of a wind energy installation having a plurality of rotor blades

Also Published As

Publication number Publication date
JPWO2009139066A1 (en) 2011-09-15
EP2290232A4 (en) 2013-11-27
EP2290232A1 (en) 2011-03-02
KR101115278B1 (en) 2012-03-09
PT2290232E (en) 2015-11-12
EP2290232B1 (en) 2015-08-05
WO2009139066A1 (en) 2009-11-19
CA2670279A1 (en) 2009-11-16
DK2290232T3 (en) 2015-10-26
AU2008334195B2 (en) 2011-11-10
CN101715515A (en) 2010-05-26
AU2008334195C1 (en) 2012-11-29
JP4875750B2 (en) 2012-02-15
CA2670279C (en) 2013-06-25
TW200949069A (en) 2009-12-01
TWI347402B (en) 2011-08-21
KR20100007852A (en) 2010-01-22
AU2008334195A1 (en) 2009-12-03

Similar Documents

Publication Publication Date Title
US20110142630A1 (en) Wind turbine pitch-angle control device and method thereof
EP2306003B1 (en) System and methods for controlling a wind turbine
EP2712403B1 (en) Power management system for yaw controlled wind turbines
CN109891091B (en) Dynamically controlled wind turbine shutdown
US20140030090A1 (en) Systems and methods for controlling tower clearance in a wind turbine
JP6230967B2 (en) Wind power generator and blade pitch angle adjusting method thereof
US20200291920A1 (en) High Yaw Error and Gust Ride Through
CN101688519A (en) A method of operating a wind turbine with pitch control, a wind turbine and a cluster of wind turbines
US10294920B2 (en) Wind turbine and method for operating a wind turbine
CN107407258A (en) Power ramp of the turbine from low-power mode
EP3966449B1 (en) Wind turbine control using predicted steady-state deflection
KR20140113510A (en) Actuation of distributed load management devices on aerodynamic blades
KR101363516B1 (en) Method for controlling a generator of wind turbine generator
EP3351789A1 (en) Wind power generation system or method of operating wind power generation system
DK2607688T3 (en) Method for controlling a wind turbine
KR20150019461A (en) Wind-Electric Power Generation System and Driving Stop Method Thereof
CN115667705A (en) Method for operating a wind turbine in response to a grid disturbance
US20220397091A1 (en) Pivot angle control of blades of a wind turbine with hinged blades
EP4172497B1 (en) Wind turbine operation in extreme wind conditions
Sirigu et al. Innovative blade design for wind generator application
CN115667700A (en) Controlling yaw to reduce motor speed

Legal Events

Date Code Title Description
AS Assignment

Owner name: MITSUBISHI HEAVY INDUSTRIES, LTD., JAPAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HAYASHI, YOSHIYUKI;REEL/FRAME:022866/0051

Effective date: 20090617

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION