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WO2019184181A1 - Wind turbine group, leveling device, and leveling control method, device and system - Google Patents

Wind turbine group, leveling device, and leveling control method, device and system Download PDF

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Publication number
WO2019184181A1
WO2019184181A1 PCT/CN2018/098961 CN2018098961W WO2019184181A1 WO 2019184181 A1 WO2019184181 A1 WO 2019184181A1 CN 2018098961 W CN2018098961 W CN 2018098961W WO 2019184181 A1 WO2019184181 A1 WO 2019184181A1
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WO
WIPO (PCT)
Prior art keywords
leveling
wind
force
wing
nacelle
Prior art date
Application number
PCT/CN2018/098961
Other languages
French (fr)
Chinese (zh)
Inventor
邢波
Original Assignee
新疆金风科技股份有限公司
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 新疆金风科技股份有限公司 filed Critical 新疆金风科技股份有限公司
Publication of WO2019184181A1 publication Critical patent/WO2019184181A1/en

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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
    • F03D15/00Transmission of mechanical power
    • 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
    • F03D17/00Monitoring or testing of wind motors, e.g. diagnostics
    • 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 
    • 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
    • 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
    • F03D7/0204Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for orientation in relation to wind direction
    • 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
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20Wind motors characterised by the driven apparatus
    • F03D9/25Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • 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
    • F05B2270/321Wind directions
    • 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
    • F05B2270/329Azimuth or yaw 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 the field of wind power generation, and more particularly to a wind power generator set and leveling device, a leveling control method, apparatus and system.
  • Wind power is a way of using renewable energy and has the potential for large-scale applications.
  • Wind turbines (especially megawatt wind turbines) are bulky and include at least: a tower, a nacelle disposed on the tower, a hub disposed on the nacelle, and blades disposed on the hub, wherein the tower is To support the nacelle, the nacelle is at the desired height so that the cabin receives the corresponding wind.
  • the center of gravity of the nacelle is on the centerline of the tower.
  • the position of the center of gravity of the nacelle changes, resulting in instability of the wind turbine.
  • a change in the position of the center of gravity of the nacelle may cause an increase in yaw acceleration, which may cause a malfunction; a change in the position of the center of gravity of the nacelle may cause uneven force on the wind turbine, thereby causing a secondary risk.
  • the various aspects of the present invention address at least the above mentioned problems and/or disadvantages and at least provide the following advantages.
  • the present invention may not solve the above mentioned problems and/or disadvantages.
  • a leveling device for a wind power generator set may include a nacelle, and the leveling device may include: a leveling wing disposed on the nacelle for transmitting the received wind power to the nacelle to adjust a center of gravity of the nacelle; driving And a mechanism coupled to the leveling wing for adjusting a posture of the leveling wing to adjust a wind force received by the leveling wing.
  • a leveling control method for a wind power generator set may include the leveling device as described above, wherein the leveling control method may include: receiving the measured force information and wind direction information of the wind power generator set; according to the force information and The wind direction information adjusts the attitude of the leveling wing to adjust the wind force experienced by the leveling wing.
  • a leveling control device for a wind power generator set may include the leveling device as described above, wherein the leveling control device may include: a receiving module, configured to receive the measured force information and wind direction information of the wind power generator set; and the control module And adjusting the attitude of the leveling wing according to the force information and the wind direction information received by the receiving module to adjust the wind force received by the leveling wing.
  • a leveling control system for a wind power generator set is provided.
  • the wind turbine can include a leveling device as described above.
  • the leveling control system may include: a force measuring mechanism for measuring force information of the wind power generator; a wind measuring mechanism for measuring wind direction information; and a leveling control device as described above.
  • a leveling system for a wind power generator which may include a leveling control device as described above and a leveling device as described above.
  • a computer readable storage medium storing instructions that, when executed by a processor, cause a processor to perform a leveling control method as described above.
  • a computer apparatus can store instructions that, when executed by a processor, cause a processor to perform a leveling control method as described above.
  • a wind power generator set which may include a leveling device as described above, or a leveling control device as described above, or a leveling control system as described above, or as described above A leveling system, or a computer readable storage medium as described above, or a computer device as described above.
  • the present invention can adjust the center of gravity of the nacelle by using a leveling wing such that the distance between the center of gravity of the nacelle and the centerline of the tower is within a desired distance, thereby allowing the nacelle and tower to be smooth.
  • a leveling wing such that the distance between the center of gravity of the nacelle and the centerline of the tower is within a desired distance, thereby allowing the nacelle and tower to be smooth.
  • FIG. 1 illustrates a wind power generator set in accordance with an exemplary embodiment of the present invention
  • FIG. 2 illustrates a wind power generator set in accordance with another exemplary embodiment of the present invention
  • FIG. 3 illustrates a wind power generator set in accordance with another exemplary embodiment of the present invention
  • Figure 4 shows a schematic view of a wind power plant provided with a leveling control system in accordance with an exemplary embodiment of the present invention
  • Figure 5 is a plan view of Figure 4.
  • Figure 6 shows a schematic view of a leveling device in accordance with an exemplary embodiment of the present invention
  • FIG. 7 shows a schematic diagram of a leveling control device according to an exemplary embodiment of the present invention.
  • FIG. 8 shows a flowchart of a leveling control method according to an exemplary embodiment of the present invention
  • FIG. 9 illustrates a flow chart for determining a wind force desired to be received, in accordance with an exemplary embodiment of the present invention.
  • Figure 10 is a schematic view showing the correspondence between the posture of the leveling wing, the wind direction, and the force received by the leveling wing;
  • Figure 11 is another schematic diagram showing the correspondence between the attitude of the leveling wing, the wind direction, and the forces experienced by the leveling wing.
  • the wind power generator may include a tower 5, a nacelle 3 disposed on the tower 5, a hub 2 disposed at the head of the nacelle 2, and a wind set at the tail of the nacelle 3.
  • the center of gravity G of the nacelle 3 is located on the center line of the tower 5. That is to say, the point B on the center line of the tower 5 is located on the center line of gravity of the cabin passing through the center of gravity G of the nacelle 3.
  • the angle between the axis of the nacelle 3 and the horizontal line is A, and the wind direction F is horizontal.
  • the position of the center of gravity G changes as the wind direction F changes.
  • the wind received by the blade 1 is transmitted to the nacelle 3 through the hub 2, so that the position of the center of gravity of the nacelle 3 is shifted toward the direction of the hub 2.
  • the force received by the nacelle 3 is transmitted to the tower 5, so that the tower 5 is unevenly loaded, and it is easy to accelerate the loss of the tower 5 and reduce the service life of the tower 5.
  • the wind turbine of the present exemplary embodiment may include a yaw system for yawing the nacelle.
  • the yaw system may include a yaw bearing disposed between the tower and the machine side. In the case shown in Fig. 2, the yaw bearing is unevenly stressed, and it is easy to accelerate the loss of the yaw bearing and reduce the service life of the yaw bearing.
  • the wind received by the blade 1 is transmitted to the nacelle 3 through the hub 2, so that the position of the center of gravity of the nacelle 3 is biased toward the wind measuring mechanism 4. shift.
  • the force received by the nacelle 3 is transmitted to the tower 5, so that the tower 5 is unevenly loaded, and it is easy to accelerate the loss of the tower 5 and reduce the service life of the tower 5.
  • FIG. 4 shows a schematic diagram of a wind power plant provided with a leveling control system in accordance with an exemplary embodiment of the present invention.
  • the wind power generator may include a tower 5, a nacelle 3 disposed on the tower 5, a hub 2 disposed at a head of the nacelle 3, and a blade 1 disposed on the hub 2.
  • the wind power generator set of the present exemplary embodiment may further include a leveling device.
  • the leveling device may comprise: a leveling wing 6 disposed on the nacelle 3 for transmitting the received wind to the nacelle 3 to adjust the position of the center of gravity of the nacelle 3; a drive mechanism coupled to the leveling wing 6, It is used to adjust the attitude of the leveling wing 6 to adjust the wind force received by the leveling wing 6.
  • the drive mechanism can include a driver and a transmission mechanism; the transmission mechanism can include a gear set and a drive shaft, the drive, the gear set, and the drive shaft are sequentially coupled, and the leveling wing is mounted on the drive shaft and rotates with the drive shaft.
  • the leveling control system may include: a force measuring mechanism for measuring force information of the wind power generator; a wind measuring mechanism 4, which may be disposed at the tail of the nacelle 3 for measuring wind direction information; and a leveling control device, And receiving the measured force information and the wind direction information, and adjusting the posture of the leveling wing 6 according to the force information and the wind direction information to adjust the wind force received by the leveling wing 6 .
  • the wind measuring mechanism 4 can measure the wind direction in the plane consisting of the horizontal line and the center line of the tower 5, especially the vertical direction.
  • FIG. 5 is a top view of FIG. 4, in which the wind turbine can include a yaw bearing 7 that can measure the position C at the yaw bearing 7 and/or the external force experienced by the yaw bearing 7 at position D As the force information.
  • the force measuring mechanism includes two resistance strain type force sensors, which are disposed at position C and position D, respectively.
  • the resistance strain type force sensor mainly includes a resistance strain gauge.
  • the strain gauge can be formed from a conductor or a semiconductor material. The conductor or semiconductor material is deformed under the action of an external force, and the resistance value thereof is also changed accordingly. Such a phenomenon is called a resistance strain effect.
  • Two strain gauges are fixed at position C and position D, respectively. When the yaw bearing is unevenly stressed, the deformations caused by position C and position D are different. The correspondence between the change in the resistance value of the strain gauge and the force information can be determined. Thereby, the force information can be determined by the change in the resistance value of the strain gauge provided at these two positions.
  • position C and position D are located at the junction of the yaw bearing and the nacelle 3.
  • FIG. 6 shows a schematic diagram of a leveling device in accordance with an exemplary embodiment of the present invention.
  • the leveling device of the present exemplary embodiment may include a leveling wing 6 and a drive mechanism.
  • the leveling wing 6 can include a blade 10 and a blade 11.
  • the drive mechanism can include a driver 8 and a transmission for powering.
  • the transmission mechanism can include a gear set and a drive shaft 9.
  • the gear set can include gear 14 and gear 15.
  • the driver 8, the gear 14, the gear 15, and the drive shaft 9 are sequentially connected.
  • the blade 10 and the blade 11 are fixedly mounted on the transmission shaft 9 and are rotatable with the transmission shaft 9.
  • the drive shaft 9 is mounted on the nacelle 3 via bearings 12 and bearings 13.
  • the drive 8 can include an electric motor and a frequency converter for controlling the electric motor.
  • the drive 8 can also be powered hydraulically.
  • the driver 8 can sequentially transmit power to the blade 10 and the blade 11 through the gear 14, the gear 15 and the transmission shaft 9 to change the attitude of the blade 10 and the blade 11, that is, change the posture of the leveling wing 6. .
  • the attitude of the leveling wing 6 is changed, the wind force received by the leveling wing 6 can be changed, thereby changing the external force transmitted to the nacelle 3.
  • the external force transmitted to the nacelle 3 is changed, the relative position between the center of gravity of the nacelle 3 and the tower 5 changes.
  • the tower 5 When the posture of the leveling wing 6 is adjusted in a reasonable manner, the tower 5 can be uniformly and stably stressed, the tower 5 can be prevented from being damaged, the service life of the tower 5 can be prolonged, and the secondary risk can be prevented.
  • the change in the attitude of the leveling wing 6 can be achieved by the leveling control device in the exemplary embodiment of the present invention.
  • the driver 8 may be an electric motor that can calculate the zero position of the motor.
  • the zero position of the motor can be calculated from the value fed back by the motor rotation absolute encoder. Whether it is necessary to correct the zero position by: selecting at least two positions from among the positions that the motor can reach, and calculating at least two zero positions respectively corresponding to the at least two positions; when the at least two zero positions When the deviation between the two is less than the set value, it is judged that it is not necessary to correct the zero position, so that the motor can continue to work, otherwise it is judged that the zero position needs to be corrected and an alarm is issued. This enables an accurate automatic judgment of the zero position for protection such as calibration.
  • FIG. 7 shows a schematic diagram of a leveling control device in accordance with an exemplary embodiment of the present invention.
  • the leveling control apparatus 100 may include: a receiving module 101, configured to receive the measured force information and wind direction information; and a control module 102, configured to adjust according to the force information and the wind direction information Level the wing to adjust the wind that the leveling wing receives.
  • control module 102 can include a center of gravity determination module (not shown) for determining a change in the position of the center of gravity of the nacelle based on the force information; a wind determination module (not shown) for The change in position of the center of gravity determines the desired wind force of the leveling wing; an attitude adjustment module (not shown) for adjusting the attitude of the leveling wing based on the wind direction information and the desired wind force.
  • a center of gravity determination module for determining a change in the position of the center of gravity of the nacelle based on the force information
  • a wind determination module for The change in position of the center of gravity determines the desired wind force of the leveling wing
  • an attitude adjustment module (not shown) for adjusting the attitude of the leveling wing based on the wind direction information and the desired wind force.
  • the force information includes: a magnitude of a first bearing force received by the first position on the wind turbine and a magnitude of a second bearing force received by the second position on the wind turbine, wherein the center of gravity is determined
  • the module calculates a difference in size between the first withstand force and the second withstand force, and determines a change in the position of the center of gravity of the nacelle 3 based on the difference in magnitude. For example, referring to FIGS.
  • the magnitude of the first bearing force received by the position C and the magnitude of the second bearing force received by the position D can be measured, and the line connecting the position C and the position D can be parallel to the center line of the nacelle 3,
  • the distance of the position C from the hub 2 is greater than the distance of the position D from the hub 2.
  • whether the nacelle 3 or the tower 5 is uniformly stressed can be determined by the difference in magnitude between the first withstand force and the second withstand force, and when the difference in magnitude exceeds a predetermined threshold, the nacelle 3 can be determined. Or the tower 5 is unevenly stressed. At this time, it is necessary to change the external force received by the nacelle 3 or the tower 5 to avoid damage to the nacelle 3 or the tower 5.
  • the change in the position of the center of gravity includes a change in direction and a degree of change
  • the wind determination module determines the said center of gravity position is offset toward a head of the nacelle and the degree of change exceeds a predetermined threshold
  • the wind force that is desired to be subjected is a downforce; when the center of gravity position is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold, the wind determination module determines that the wind force desired to be subjected is a rising force.
  • the attitude adjustment module determines whether the leveling wing has obtained the desired wind force according to the wind direction information and the current attitude of the leveling wing; when the leveling wing does not obtain the When the wind is desired to be received, the attitude adjustment module causes the leveling wing to obtain the desired wind force by adjusting an angle at which the leveling wing rotates about a particular axis.
  • the angle of rotation of the motor can be detected by a motor rotary absolute encoder so that the angle of the leveling wing rotation can be calculated from the angle of rotation of the motor.
  • the particular axis is parallel to the horizontal plane and perpendicular to the length of the nacelle.
  • the particular axis is two or more, and at least one blade may be disposed on each axis.
  • the two or more specific axes are in a particular plane, the length direction of the nacelle being perpendicular to the particular plane, each particular axis corresponding to at least one rotation about the particular axis The blades of the flat wing.
  • the attitude adjustment module may determine a desired position of the leveling wing when the leveling wing obtains the desired wind force, and adjust the position of the leveling wing according to the sensing The angle of rotation of the leveling wing is such that the leveling wing is rotated to the desired position.
  • the position of the leveling wing can be sensed by the position sensor.
  • a position sensor can be located adjacent the blade 10 and/or the blade 11 and disposed on the nacelle or leveling device to sense the position of the blade of the leveling wing. Whether the leveling wing reaches a desired position can be determined based on the position of the leveling wing sensed by the position sensor.
  • the leveling wing can also be determined according to the sensed position to reach the maximum rotational position, and when the leveling wing reaches the maximum rotational position, the leveling wing stops rotating or rotates in the opposite direction to avoid leveling the wing damage.
  • FIG. 8 shows a flow chart of a leveling control method according to an exemplary embodiment of the present invention.
  • the leveling control method of the present exemplary embodiment may be used to control the leveling device described in the exemplary embodiment of the present invention, and includes: step 201, receiving the measured wind turbine generator set Force information and wind direction information; Step 202: Adjust the posture of the leveling wing according to the force information and the wind direction information to adjust the wind force received by the leveling wing.
  • the step 202 may include: determining a change in a position of a center of gravity of the nacelle according to the force information; determining a desired wind force of the leveling wing according to the change in the position of the center of gravity; according to the wind direction The information and the desired wind force are adjusted to adjust the attitude of the wing.
  • the force information may include: a magnitude of a first bearing force received by the first position on the wind turbine and a magnitude of a second bearing force received by the second position on the wind turbine,
  • the step of determining the change in the position of the center of gravity of the nacelle by the force information includes: calculating a difference in size between the first withstand force and the second withstand force; determining a change in the position of the center of gravity of the nacelle according to the difference in the size . For example, referring to FIG. 4 and FIG.
  • the magnitude of the first bearing force received by the position C and the magnitude of the second bearing force received by the position D can be measured, and the line connecting the position C and the position D is parallel to the center line of the nacelle 3,
  • the distance of the position C from the hub 2 is greater than the distance of the position D from the hub 2.
  • whether the nacelle 3 or the tower 5 is uniformly stressed can be determined by the difference in magnitude between the first withstand force and the second withstand force, and when the difference in size exceeds a predetermined threshold, the need can be determined.
  • the external force received by the nacelle 3 or the tower 5 is changed to avoid damage to the nacelle 3 or the tower 5.
  • the change in the position of the center of gravity includes a change in direction and a degree of change
  • the step of determining the desired wind force of the leveling wing according to the change in the position of the center of gravity may include: when the position of the center of gravity is toward the nacelle When the head is offset and the degree of change exceeds a predetermined threshold, the wind force that is desired to be subjected is a downward pressure; when the position of the center of gravity is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold, The wind that is expected to be received is a rising force.
  • the step of adjusting the attitude of the leveling wing according to the wind direction information and the wind force desired to be received may include determining the tone according to the wind direction information and a current posture of the leveling wing Whether the flat wing has obtained the desired wind force; when the leveling wing does not obtain the desired wind force, the leveling is adjusted by adjusting the angle at which the leveling wing rotates about a particular axis The wing obtains the desired wind force.
  • the step of adjusting an angle at which the leveling wing rotates about a particular axis may include determining a desired position of the leveling wing when the leveling wing obtains the desired wind force; The sensed position of the leveling wing adjusts the angle of rotation of the leveling wing to rotate the leveling wing to the desired position.
  • the desired wind force described in the exemplary embodiment of the present invention can be calculated by the flow shown in FIG. As shown in FIG. 9, at step 301, the magnitude X of the first withstand force and the magnitude Y of the second withstand force are obtained. At step 302, it is compared whether the absolute value of the difference between X and Y is less than the threshold Z for starting the leveling, and if so, proceeds to step 303, otherwise to step 304. At step 303, it is determined that there is no need to adjust the center of gravity of the nacelle. At step 304, a comparison is made to determine if X is greater than Y, and if so, then proceeds to step 306, otherwise to step 305. At step 306, it is determined that the wind force that is desired to be received is a downforce. At step 305, it is determined that the wind force that is desired to be received is a rising force.
  • step 307 may be performed to determine whether the leveling wing has the ability to obtain the lifting force in the current environment. If yes, proceed to step 310, otherwise proceed to step 309, the current environment including at least the wind direction. At step 310, the attitude of the leveling wing is adjusted to achieve a lifting force for the leveling wing. At step 309, a first alarm is issued, the first alarm indicating that the leveling wing does not have the ability to obtain a lift in the current environment.
  • step 306 the process may proceed to step 308 to determine whether the leveling wing has the ability to obtain the descent force in the current environment. If yes, proceed to step 311, otherwise proceed to step 312. At step 311, the attitude of the leveling wing is adjusted to achieve a lowering force for the leveling wing. At step 312, a second alarm is issued indicating that the leveling wing does not have the ability to obtain a descent force in the current environment.
  • the ability to obtain the lifting force refers to: at least one position of the leveling wing in its range of motion, the component of the wind received in the vertical upward direction or the wind received in the direction perpendicular to the axis of the nacelle and upward
  • the upper component is greater than zero.
  • the ability to obtain a descending force means that the leveling wing is at least one position within its range of motion, and the component of the wind subjected to the vertical downward direction or the received wind force is perpendicular to the cabin axis and downward.
  • the force component in the direction is greater than zero.
  • the first alarm or the second alarm it is possible to detect whether a failure of the measuring component (for example, a wind measuring mechanism, a force measuring mechanism, a position sensor, etc.) occurs.
  • a failure of the measuring component for example, a wind measuring mechanism, a force measuring mechanism, a position sensor, etc.
  • Fig. 10 is a schematic view showing the correspondence relationship between the posture of the leveling wing, the wind direction, and the force received by the leveling wing.
  • the body of the leveling wing is in the shape of a blade, as shown in Fig. 10, the longitudinal direction of the body of the leveling wing is perpendicular to the plane of the paper.
  • the wind direction is F
  • F can be decomposed into a wind direction f1 in the horizontal direction and a wind direction f2 in the vertical direction.
  • the direction in which the leveling wings extend is parallel to the wind direction. In this case, the leveling wing is not able to adjust the position of the center of gravity of the nacelle.
  • the direction of the leveling wing extends at an acute angle to the wind direction F, and the leveling wing can obtain the downforce.
  • the wind direction F is perpendicular to the direction in which the leveling wing extends, and the leveling wing is also able to obtain the downforce.
  • the leveling wing is only capable of obtaining the downforce when the leveling wing is only changeable within the range defined by the first attitude to the third attitude, without obtaining The ability to rise.
  • Fig. 11 is a schematic view showing the correspondence relationship between the posture of the leveling wing, the wind direction, and the force received by the leveling wing.
  • the wind direction is F
  • F can be decomposed into a wind direction f1 in the horizontal direction and a wind direction f2 in the vertical direction.
  • the direction of the leveling wing is parallel to the wind direction. In this case, the leveling wing is not able to adjust the position of the center of gravity of the nacelle.
  • the direction of the leveling wing extends at an acute angle to the wind direction F, and the leveling wing can obtain the lifting force.
  • the wind direction F is perpendicular to the direction in which the leveling wing extends, and the leveling wing can also obtain the lifting force.
  • the leveling wing is only capable of obtaining the lifting force when the leveling wing is only changeable within the range defined by the fourth posture to the sixth posture, and does not have the ability to obtain The ability to stress.
  • the wind force corresponds to the attitude of the leveling wing. Therefore, it is desirable that the wind force received corresponds to the desired posture.
  • the leveling wing needs to be rotated, for example, to bring the leveling wing to the second attitude or
  • the position corresponding to the third posture is such that the leveling wing receives the downforce.
  • the leveling wing needs to be rotated, for example, to bring the leveling wing to the fifth posture or The position corresponding to the sixth posture, in order to obtain the lifting force of the leveling wing.
  • the leveling wings and the hub may be located on either side of the center of gravity of the nacelle along the length of the nacelle to equalize the wind received by the nacelle.
  • a leveling wing can be placed at the rear of the nacelle.
  • the number of blades of the leveling wing is not limited and may be one or more pieces.
  • the position of the leveling wing is not limited to the above embodiment.
  • the leveling wing and hub may be located on the same side of the center of gravity of the nacelle along the length of the nacelle.
  • the attitude of the leveling wing is changed by rotating the leveling wing, and at the same time, the angle between the direction of extension of the leveling wing and the wind direction can be changed to change the wind received by the leveling wing. the size of.
  • a leveling system for a wind power generator set is provided.
  • the leveling system can include a leveling control device and a leveling device as described in the exemplary embodiments of the present invention.
  • a computer readable storage medium storing instructions that, when executed by a processor, cause a processor to perform a leveling control method as described in an exemplary embodiment of the present invention .
  • a computer device stores instructions that, when executed by a processor, cause the processor to perform the leveling control method described in the exemplary embodiments of the present invention.
  • a wind power generator set is provided.
  • the wind turbine may comprise a leveling device as described in an exemplary embodiment of the invention, or a leveling control device as described in an exemplary embodiment of the invention, or in an exemplary embodiment of the invention.
  • the leveling control system, or a leveling system as described in an exemplary embodiment of the invention, or a computer readable storage medium as described in an exemplary embodiment of the invention, or an example of the invention Computer device as described in the embodiments.
  • the present invention employs a leveling wing to adjust the center of gravity of the nacelle to stabilize the nacelle and/or tower.
  • the methods and apparatus provided by the exemplary embodiments of the present invention may be implemented by a stand-alone controller (e.g., a PLC controller) or by a controller of a wind turbine.
  • a stand-alone controller e.g., a PLC controller
  • a controller of a wind turbine e.g., a wind turbine.
  • the computer readable storage medium in the embodiments of the present invention includes program commands, data files, data structures, and the like, or a combination thereof.
  • a program recorded in a computer readable storage medium can be designed or configured to implement the methods of the present invention.
  • Computer readable storage media includes hardware systems for storing and executing programs and/or commands. Examples of hardware systems are magnetic media (such as hard disks, floppy disks, magnetic tapes), optical media (such as CD-ROMs and DVDs), magneto-optical media (such as floppy disks, ROM, RAM, flash memory, etc.).
  • Programs and/or commands include assembly language code or machine code compiled by a compiler and higher level language code interpreted by an interpreter.
  • the hardware system can be implemented with at least one software module to comply with the present invention.
  • One or more general purpose or special purpose computers eg, processors, controllers, digital signal processors, microcomputers, field programmable arrays, programmable logic units, microprocessors, or any other capable of executing software or executing instructions) Apparatus
  • Apparatus to implement at least a portion of the above methods, apparatus, and/or systems.
  • the at least a portion can be implemented in an operating system or in one or more software applications operating under an operating system.

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Abstract

A leveling device for a wind turbine group. The wind turbine group can comprise a nacelle (3). The leveling device can comprise: a leveling wing (6) disposed on the nacelle (3) and used for transferring the received wind to the nacelle (3) so as to adjust the center of gravity position thereof; and a drive mechanism connected to the leveling wing (6) and used for adjusting an altitude of the leveling wing (6) so as to adjust the wind received by the leveling wing. The leveling device can adjust the center of gravity position of the nacelle so as to make the distance between the center of gravity of the nacelle and a center line of a cylindrical tower fall within the expected distance range, thereby stabilizing the nacelle and the cylindrical tower. The present invention also relates to a leveling control method, device and system.

Description

风力发电机组及调平装置、调平控制方法、装置和系统Wind turbine generator and leveling device, leveling control method, device and system 技术领域Technical field
本发明涉及风力发电领域,更具体地,涉及一种风力发电机组及调平装置、调平控制方法、装置和系统。The present invention relates to the field of wind power generation, and more particularly to a wind power generator set and leveling device, a leveling control method, apparatus and system.
背景技术Background technique
当前,世界各国已经对如何针对气候变化来开展国际合作和发展清洁能源达成共识。风力发电是一种可再生能源的利用方式,具有大规模应用的潜力。风力发电机组(特别是兆瓦级风力发电机组)体型庞大,至少包括:塔筒、设置在塔筒上的机舱、设置在机舱上的轮毂、和设置在轮毂上的叶片,其中,塔筒用于支撑机舱,使机舱处于期望的高度,以使机舱获得相应的风力。At present, countries around the world have reached a consensus on how to carry out international cooperation and develop clean energy for climate change. Wind power is a way of using renewable energy and has the potential for large-scale applications. Wind turbines (especially megawatt wind turbines) are bulky and include at least: a tower, a nacelle disposed on the tower, a hub disposed on the nacelle, and blades disposed on the hub, wherein the tower is To support the nacelle, the nacelle is at the desired height so that the cabin receives the corresponding wind.
通常情况下,机舱的重心位于塔筒的中心线上。然而,当机舱受到外力时,机舱的重心位置会发生改变,导致风力发电机组不稳定。例如,机舱的重心位置的改变会引起偏航加速度增大,容易引发故障;机舱的重心位置的改变会使风力发电机组受力不均,从而引发次生风险。Typically, the center of gravity of the nacelle is on the centerline of the tower. However, when the engine room is subjected to an external force, the position of the center of gravity of the nacelle changes, resulting in instability of the wind turbine. For example, a change in the position of the center of gravity of the nacelle may cause an increase in yaw acceleration, which may cause a malfunction; a change in the position of the center of gravity of the nacelle may cause uneven force on the wind turbine, thereby causing a secondary risk.
发明内容Summary of the invention
本发明的各个方面至少可解决以上提到的问题和/或缺点,并且至少提供以下优点。另外,本发明可不解决以上提到的问题和/或缺点。The various aspects of the present invention address at least the above mentioned problems and/or disadvantages and at least provide the following advantages. In addition, the present invention may not solve the above mentioned problems and/or disadvantages.
根据本发明的一方面,提供了一种风力发电机组的调平装置。所述风力发电机组可包括机舱,所述调平装置可包括:调平机翼,设置在所述机舱上,用于将受到的风力传递给所述机舱以调整所述机舱的重心位置;驱动机构,与所述调平机翼连接,用于调整所述调平机翼的姿态以调整所述调平机翼受到的风力。According to an aspect of the present invention, a leveling device for a wind power generator set is provided. The wind power generator may include a nacelle, and the leveling device may include: a leveling wing disposed on the nacelle for transmitting the received wind power to the nacelle to adjust a center of gravity of the nacelle; driving And a mechanism coupled to the leveling wing for adjusting a posture of the leveling wing to adjust a wind force received by the leveling wing.
根据本发明的另一方面,提供了一种风力发电机组的调平控制方法。所述风力发电机组可包括如上所述的调平装置,其中,所述调平控制方法可包括:接收测量得到的所述风力发电机组的受力信息及风向信息;根据所述受 力信息和所述风向信息调整所述调平机翼的姿态以调整所述调平机翼受到的风力。According to another aspect of the present invention, a leveling control method for a wind power generator set is provided. The wind power generator may include the leveling device as described above, wherein the leveling control method may include: receiving the measured force information and wind direction information of the wind power generator set; according to the force information and The wind direction information adjusts the attitude of the leveling wing to adjust the wind force experienced by the leveling wing.
根据本发明的另一方面,提供了一种风力发电机组的调平控制装置。所述风力发电机组可包括如上所述的调平装置,其中,所述调平控制装置可包括:接收模块,用于接收测量得到的所述风力发电机组的受力信息及风向信息;控制模块,用于根据接收模块接收到的受力信息和风向信息调整调平机翼的姿态以调整所述调平机翼受到的风力。According to another aspect of the present invention, a leveling control device for a wind power generator set is provided. The wind turbine generator may include the leveling device as described above, wherein the leveling control device may include: a receiving module, configured to receive the measured force information and wind direction information of the wind power generator set; and the control module And adjusting the attitude of the leveling wing according to the force information and the wind direction information received by the receiving module to adjust the wind force received by the leveling wing.
根据本发明的另一方面,提供了一种风力发电机组的调平控制系统。所述风力发电机组可包括如上所述的调平装置。所述调平控制系统可包括:测力机构,用于测量风力发电机组的受力信息;测风机构,用于测量风向信息;以及如上所述的调平控制装置。According to another aspect of the present invention, a leveling control system for a wind power generator set is provided. The wind turbine can include a leveling device as described above. The leveling control system may include: a force measuring mechanism for measuring force information of the wind power generator; a wind measuring mechanism for measuring wind direction information; and a leveling control device as described above.
根据本发明的另一方面,提供了一种风力发电机组的调平系统,可包括如上所述的调平控制装置及如上所述的调平装置。According to another aspect of the present invention, there is provided a leveling system for a wind power generator, which may include a leveling control device as described above and a leveling device as described above.
根据本发明的另一方面,提供了一种计算机可读存储介质,可存储有当被处理器执行时使得处理器执行如上所述的调平控制方法的指令。According to another aspect of the present invention, there is provided a computer readable storage medium storing instructions that, when executed by a processor, cause a processor to perform a leveling control method as described above.
根据本发明的另一方面,提供了一种计算机设备,可存储有当被处理器执行时使得处理器执行如上所述的调平控制方法的指令。According to another aspect of the present invention, a computer apparatus is provided that can store instructions that, when executed by a processor, cause a processor to perform a leveling control method as described above.
根据本发明的另一方面,提供了一种风力发电机组,可包括如上所述的调平装置,或者如上所述的调平控制装置,或者如上所述的调平控制系统,或者如上所述的调平系统,或者如上所述的计算机可读存储介质,或者如上所述的计算机设备。According to another aspect of the present invention, there is provided a wind power generator set which may include a leveling device as described above, or a leveling control device as described above, or a leveling control system as described above, or as described above A leveling system, or a computer readable storage medium as described above, or a computer device as described above.
本发明可采用调平机翼调整机舱的重心位置,使得机舱的重心与塔筒的中心线之间的距离在期望的距离范围之内,从而可使机舱和塔筒平稳。由此,可避免机舱的偏航加速度增大以及偏航加速度增大引发的故障,可减少塔筒和风力发电机组的至少一部分部件(例如,偏航轴承)的损耗,也可减少次生风险。The present invention can adjust the center of gravity of the nacelle by using a leveling wing such that the distance between the center of gravity of the nacelle and the centerline of the tower is within a desired distance, thereby allowing the nacelle and tower to be smooth. Thereby, the increase of the yaw acceleration of the nacelle and the failure caused by the increase of the yaw acceleration can be avoided, the loss of at least a part of the tower and the wind turbine generator component (for example, the yaw bearing) can be reduced, and the secondary risk can be reduced. .
将在接下来的描述中部分阐述本发明总体构思另外的方面和/或优点,还有一部分通过描述将是清楚的,或者可以经过本发明总体构思的实施而得知。Additional aspects and/or advantages of the present general inventive concept will be set forth in part in the description.
附图说明DRAWINGS
现将详细参照本发明的实施例,所述实施例的示例在附图中示出,其中, 相同的标号始终指的是相同的部件。以下将通过参照附图来说明所述实施例,以便解释本发明。The embodiments of the present invention will now be described in detail with reference to the accompanying drawings. The embodiments are described below in order to explain the present invention by referring to the figures.
图1示出了根据本发明的示例性实施例的风力发电机组;FIG. 1 illustrates a wind power generator set in accordance with an exemplary embodiment of the present invention;
图2示出了根据本发明的另一示例性实施例的风力发电机组;FIG. 2 illustrates a wind power generator set in accordance with another exemplary embodiment of the present invention;
图3示出了根据本发明的另一示例性实施例的风力发电机组;FIG. 3 illustrates a wind power generator set in accordance with another exemplary embodiment of the present invention;
图4示出了设置有根据本发明的示例性实施例的调平控制系统的风力发电机组的示意图;Figure 4 shows a schematic view of a wind power plant provided with a leveling control system in accordance with an exemplary embodiment of the present invention;
图5是图4的俯视图;Figure 5 is a plan view of Figure 4;
图6示出了根据本发明的示例性实施例的调平装置的示意图;Figure 6 shows a schematic view of a leveling device in accordance with an exemplary embodiment of the present invention;
图7示出了根据本发明的示例性实施例的调平控制装置的示意图;FIG. 7 shows a schematic diagram of a leveling control device according to an exemplary embodiment of the present invention; FIG.
图8示出了根据本发明的示例性实施例的调平控制方法的流程图;FIG. 8 shows a flowchart of a leveling control method according to an exemplary embodiment of the present invention;
图9示出了根据本发明的示例性实施例的确定期望受到的风力的流程图;FIG. 9 illustrates a flow chart for determining a wind force desired to be received, in accordance with an exemplary embodiment of the present invention; FIG.
图10是示出了调平机翼的姿态、风向以及调平机翼的受到的力之间的对应关系的示意图;Figure 10 is a schematic view showing the correspondence between the posture of the leveling wing, the wind direction, and the force received by the leveling wing;
图11是示出了调平机翼的姿态、风向以及调平机翼的受到的力之间的对应关系的另一示意图。Figure 11 is another schematic diagram showing the correspondence between the attitude of the leveling wing, the wind direction, and the forces experienced by the leveling wing.
具体实施方式detailed description
以下,将参照附图更加详细地描述发明构思的示例性实施例。Hereinafter, exemplary embodiments of the inventive concept will be described in more detail with reference to the accompanying drawings.
图1至图3示出了根据本发明的示例性实施例的风力发电机组。如图1至图3中所示,风力发电机组可包括:塔筒5、设置在塔筒5上的机舱3、设置在机舱3的头部的轮毂2、设置在机舱3的尾部的测风机构4、以及设置在轮毂2上的叶片1,其中,塔筒5是主要的承重部件,如果塔筒5出现受力不均等问题,则影响风力发电机组的安全。1 to 3 illustrate a wind power generator set according to an exemplary embodiment of the present invention. As shown in FIGS. 1 to 3, the wind power generator may include a tower 5, a nacelle 3 disposed on the tower 5, a hub 2 disposed at the head of the nacelle 2, and a wind set at the tail of the nacelle 3. The mechanism 4, and the blade 1 disposed on the hub 2, wherein the tower 5 is the main load-bearing component, affects the safety of the wind turbine if the tower 5 has problems such as uneven force.
通常情况下,如图1中所示,机舱3的重心G位于塔筒5的中心线上。也就是说,塔筒5的中心线上的点B位于通过机舱3的重心G的机舱重心线上。在这种情况下,机舱3的轴线与水平线之间的夹角是A,风向F为水平方向。Normally, as shown in FIG. 1, the center of gravity G of the nacelle 3 is located on the center line of the tower 5. That is to say, the point B on the center line of the tower 5 is located on the center line of gravity of the cabin passing through the center of gravity G of the nacelle 3. In this case, the angle between the axis of the nacelle 3 and the horizontal line is A, and the wind direction F is horizontal.
重心G的位置会随着风向F的改变而改变。当风向F由水平方向向竖直向下方向转变的过程中,如图2中所示,叶片1受到的风力通过轮毂2传递给机舱3,使机舱3的重心位置向轮毂2的方向偏移。在这种情况下,机舱3 受到的力会被传递给塔筒5,使得塔筒5受力不均,容易加快塔筒5的损耗,降低塔筒5的使用寿命。The position of the center of gravity G changes as the wind direction F changes. During the transition of the wind direction F from the horizontal direction to the vertical downward direction, as shown in FIG. 2, the wind received by the blade 1 is transmitted to the nacelle 3 through the hub 2, so that the position of the center of gravity of the nacelle 3 is shifted toward the direction of the hub 2. . In this case, the force received by the nacelle 3 is transmitted to the tower 5, so that the tower 5 is unevenly loaded, and it is easy to accelerate the loss of the tower 5 and reduce the service life of the tower 5.
本示例性实施例的风力发电机组可包括偏航系统,用于使机舱偏航。偏航系统可包括偏航轴承,设置在塔筒和机侧之间。在图2所示的情况下,偏航轴承受力不均,容易加快偏航轴承的损耗,降低偏航轴承的使用寿命。The wind turbine of the present exemplary embodiment may include a yaw system for yawing the nacelle. The yaw system may include a yaw bearing disposed between the tower and the machine side. In the case shown in Fig. 2, the yaw bearing is unevenly stressed, and it is easy to accelerate the loss of the yaw bearing and reduce the service life of the yaw bearing.
当风向F由水平方向向竖直向上方向转变的过程中,如图3中所示,叶片1受到的风力通过轮毂2传递给机舱3,使机舱3的重心位置向测风机构4的方向偏移。在这种情况下,机舱3受到的力会被传递给塔筒5,使得塔筒5受力不均,容易加快塔筒5的损耗,降低塔筒5的使用寿命。In the process of the wind direction F transitioning from the horizontal direction to the vertical upward direction, as shown in FIG. 3, the wind received by the blade 1 is transmitted to the nacelle 3 through the hub 2, so that the position of the center of gravity of the nacelle 3 is biased toward the wind measuring mechanism 4. shift. In this case, the force received by the nacelle 3 is transmitted to the tower 5, so that the tower 5 is unevenly loaded, and it is easy to accelerate the loss of the tower 5 and reduce the service life of the tower 5.
在图2和图3所示的情况下,还可能由于机舱3的重心位置的改变而使偏航加速度增大,造成倒塔等次生风险。In the case shown in Figs. 2 and 3, it is also possible that the yaw acceleration is increased due to the change in the position of the center of gravity of the nacelle 3, causing secondary risks such as inverted towers.
图4示出设置有根据本发明的示例性实施例的调平控制系统的风力发电机组的示意图。4 shows a schematic diagram of a wind power plant provided with a leveling control system in accordance with an exemplary embodiment of the present invention.
如图4中所示,风力发电机组可包括:塔筒5、设置在塔筒5上的机舱3、设置在机舱3的头部的轮毂2、以及设置在轮毂2上的叶片1。本示例性实施例的风力发电机组还可包括调平装置。As shown in FIG. 4, the wind power generator may include a tower 5, a nacelle 3 disposed on the tower 5, a hub 2 disposed at a head of the nacelle 3, and a blade 1 disposed on the hub 2. The wind power generator set of the present exemplary embodiment may further include a leveling device.
作为示例,调平装置可包括:调平机翼6,设置在机舱3上,用于将受到的风力传递给机舱3以调整机舱3的重心位置;驱动机构,与调平机翼6连接,用于调整调平机翼6的姿态以调整调平机翼6受到的风力。作为示例,驱动机构可包括驱动器和传动机构;传动机构可包括齿轮组和传动轴,驱动器、齿轮组及传动轴依次连接,调平机翼安装在传动轴上并且随传动轴转动。在下文中,参照图6对调平装置进行了详细描述。As an example, the leveling device may comprise: a leveling wing 6 disposed on the nacelle 3 for transmitting the received wind to the nacelle 3 to adjust the position of the center of gravity of the nacelle 3; a drive mechanism coupled to the leveling wing 6, It is used to adjust the attitude of the leveling wing 6 to adjust the wind force received by the leveling wing 6. As an example, the drive mechanism can include a driver and a transmission mechanism; the transmission mechanism can include a gear set and a drive shaft, the drive, the gear set, and the drive shaft are sequentially coupled, and the leveling wing is mounted on the drive shaft and rotates with the drive shaft. Hereinafter, the leveling device will be described in detail with reference to FIG.
作为示例,调平控制系统可包括:测力机构,用于测量风力发电机组的受力信息;测风机构4,可设置在机舱3的尾部,用于测量风向信息;以及调平控制装置,用于接收测量得到的受力信息及风向信息,并且根据所述受力信息和所述风向信息调整调平机翼6的姿态以调整调平机翼6受到的风力。As an example, the leveling control system may include: a force measuring mechanism for measuring force information of the wind power generator; a wind measuring mechanism 4, which may be disposed at the tail of the nacelle 3 for measuring wind direction information; and a leveling control device, And receiving the measured force information and the wind direction information, and adjusting the posture of the leveling wing 6 according to the force information and the wind direction information to adjust the wind force received by the leveling wing 6 .
在一个优选的实施例中,测风机构4可测量由水平线和塔筒5的中心线组成的平面内的风向,尤其是竖直方向的风向。In a preferred embodiment, the wind measuring mechanism 4 can measure the wind direction in the plane consisting of the horizontal line and the center line of the tower 5, especially the vertical direction.
图5是图4的俯视图,在图5中,风力发电机组可包括偏航轴承7,测力机构可测量在偏航轴承7上的位置C和/或位置D处偏航轴承7受到的外力作为受力信息。5 is a top view of FIG. 4, in which the wind turbine can include a yaw bearing 7 that can measure the position C at the yaw bearing 7 and/or the external force experienced by the yaw bearing 7 at position D As the force information.
作为示例,测力机构包括两个电阻应变式力传感器,分别设置在位置C和位置D。电阻应变式力传感器主要包括电阻应变片。电阻应变片可由导体或半导体材料形成。导体或半导体材料在外力作用下发生形变,其电阻值也会随之发生相应的改变,这样的现象被称为电阻应变效应。两个电阻应变片分别固定在位置C和位置D上。当偏航轴承受力不均时,位置C和位置D产生的形变不同。可确定电阻应变片的电阻值的变化与受力信息之间的对应关系。由此,可通过这两个位置上设置的电阻应变片的电阻值的变化来确定受力信息。在一个优选的实施例中,位置C和位置D位于偏航轴承与机舱3的连接处。As an example, the force measuring mechanism includes two resistance strain type force sensors, which are disposed at position C and position D, respectively. The resistance strain type force sensor mainly includes a resistance strain gauge. The strain gauge can be formed from a conductor or a semiconductor material. The conductor or semiconductor material is deformed under the action of an external force, and the resistance value thereof is also changed accordingly. Such a phenomenon is called a resistance strain effect. Two strain gauges are fixed at position C and position D, respectively. When the yaw bearing is unevenly stressed, the deformations caused by position C and position D are different. The correspondence between the change in the resistance value of the strain gauge and the force information can be determined. Thereby, the force information can be determined by the change in the resistance value of the strain gauge provided at these two positions. In a preferred embodiment, position C and position D are located at the junction of the yaw bearing and the nacelle 3.
图6示出根据本发明的示例性实施例的调平装置的示意图。FIG. 6 shows a schematic diagram of a leveling device in accordance with an exemplary embodiment of the present invention.
如图6中所示,本示例性实施例的调平装置可包括:调平机翼6和驱动机构。调平机翼6可包括叶片10和叶片11。驱动机构可包括用于提供动力的驱动器8和传动机构。传动机构可包括齿轮组和传动轴9。齿轮组可包括齿轮14和齿轮15。驱动器8、齿轮14、齿轮15及传动轴9依次连接。叶片10和叶片11固定安装在传动轴9上并且能够随传动轴9转动。传动轴9通过轴承12和轴承13安装在机舱3上。驱动器8可包括电动机和用于控制电动机的变频器。驱动器8也可采用液压的方式提供动力。As shown in FIG. 6, the leveling device of the present exemplary embodiment may include a leveling wing 6 and a drive mechanism. The leveling wing 6 can include a blade 10 and a blade 11. The drive mechanism can include a driver 8 and a transmission for powering. The transmission mechanism can include a gear set and a drive shaft 9. The gear set can include gear 14 and gear 15. The driver 8, the gear 14, the gear 15, and the drive shaft 9 are sequentially connected. The blade 10 and the blade 11 are fixedly mounted on the transmission shaft 9 and are rotatable with the transmission shaft 9. The drive shaft 9 is mounted on the nacelle 3 via bearings 12 and bearings 13. The drive 8 can include an electric motor and a frequency converter for controlling the electric motor. The drive 8 can also be powered hydraulically.
在本实施例中,驱动器8可依次通过齿轮14、齿轮15及传动轴9将动力传递给叶片10和叶片11,以改变叶片10和叶片11的姿态,即:改变调平机翼6的姿态。当改变调平机翼6的姿态后,可改变调平机翼6受到的的风力,从而改变传递给机舱3的外力。当改变传递给机舱3的外力时,机舱3的重心与塔筒5之间的相对位置改变。当按照合理的方式调整调平机翼6的姿态时,可使塔筒5受力均匀、稳定,防止塔筒5损坏,延长塔筒5的使用寿命,防止次生风险。可通过本发明的示例性实施例中的调平控制装置来实现调平机翼6的姿态的改变。In the present embodiment, the driver 8 can sequentially transmit power to the blade 10 and the blade 11 through the gear 14, the gear 15 and the transmission shaft 9 to change the attitude of the blade 10 and the blade 11, that is, change the posture of the leveling wing 6. . When the attitude of the leveling wing 6 is changed, the wind force received by the leveling wing 6 can be changed, thereby changing the external force transmitted to the nacelle 3. When the external force transmitted to the nacelle 3 is changed, the relative position between the center of gravity of the nacelle 3 and the tower 5 changes. When the posture of the leveling wing 6 is adjusted in a reasonable manner, the tower 5 can be uniformly and stably stressed, the tower 5 can be prevented from being damaged, the service life of the tower 5 can be prolonged, and the secondary risk can be prevented. The change in the attitude of the leveling wing 6 can be achieved by the leveling control device in the exemplary embodiment of the present invention.
在本发明的示例性实施例中,驱动器8可以是电动机,可计算电动机的零位。例如,可通过电机旋转绝对值编码器反馈的数值计算电动机的零位。可通过如下操作判断是否需要校正零位:从电动机能够到达的位置中选择至少两个位置,并计算与所述至少两个位置分别对应的至少两个零位;当所述至少两个零位之间的偏差小于设定值时,判断出不需要校正零位,可使电动机继续工作,否则判断出需要校正零位并发出报警。由此实现零位是否准确 的自动判断,以便进行校准等保护工作。In an exemplary embodiment of the invention, the driver 8 may be an electric motor that can calculate the zero position of the motor. For example, the zero position of the motor can be calculated from the value fed back by the motor rotation absolute encoder. Whether it is necessary to correct the zero position by: selecting at least two positions from among the positions that the motor can reach, and calculating at least two zero positions respectively corresponding to the at least two positions; when the at least two zero positions When the deviation between the two is less than the set value, it is judged that it is not necessary to correct the zero position, so that the motor can continue to work, otherwise it is judged that the zero position needs to be corrected and an alarm is issued. This enables an accurate automatic judgment of the zero position for protection such as calibration.
图7示出根据本发明的示例性实施例的调平控制装置的示意图。如图7中所示,调平控制装置100可包括:接收模块101,用于接收测量得到的受力信息及风向信息;控制模块102,用于根据所述受力信息和所述风向信息调整调平机翼的姿态以调整调平机翼受到的风力。FIG. 7 shows a schematic diagram of a leveling control device in accordance with an exemplary embodiment of the present invention. As shown in FIG. 7, the leveling control apparatus 100 may include: a receiving module 101, configured to receive the measured force information and wind direction information; and a control module 102, configured to adjust according to the force information and the wind direction information Level the wing to adjust the wind that the leveling wing receives.
作为示例,控制模块102可包括:重心确定模块(未示出),用于根据所述受力信息确定所述机舱的重心位置的改变;风力确定模块(未示出),用于根据所述重心位置的改变确定所述调平机翼的期望受到的风力;姿态调整模块(未示出),用于根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态。As an example, the control module 102 can include a center of gravity determination module (not shown) for determining a change in the position of the center of gravity of the nacelle based on the force information; a wind determination module (not shown) for The change in position of the center of gravity determines the desired wind force of the leveling wing; an attitude adjustment module (not shown) for adjusting the attitude of the leveling wing based on the wind direction information and the desired wind force.
作为示例,受力信息包括:风力发电机组上的第一位置受到的第一承受力的大小和所述风力发电机组上的第二位置受到的第二承受力的大小,其中,所述重心确定模块计算所述第一承受力和所述第二承受力之间的大小差异,并根据所述大小差异确定机舱3的重心位置的改变。例如,参照图4和图5,可测量位置C受到的第一承受力的大小和位置D受到的第二承受力的大小,位置C和位置D的连线可与机舱3的中心线平行,位置C距离轮毂2的距离大于位置D距离轮毂2的距离。在这种情况下,可通过第一承受力和第二承受力之间的大小差异来确定机舱3或塔筒5是否受力均匀,当所述大小差异超过预定阈值时,可确定出机舱3或塔筒5受力不均,此时,需要改变机舱3或塔筒5受到的外力,以避免机舱3或塔筒5损坏。As an example, the force information includes: a magnitude of a first bearing force received by the first position on the wind turbine and a magnitude of a second bearing force received by the second position on the wind turbine, wherein the center of gravity is determined The module calculates a difference in size between the first withstand force and the second withstand force, and determines a change in the position of the center of gravity of the nacelle 3 based on the difference in magnitude. For example, referring to FIGS. 4 and 5, the magnitude of the first bearing force received by the position C and the magnitude of the second bearing force received by the position D can be measured, and the line connecting the position C and the position D can be parallel to the center line of the nacelle 3, The distance of the position C from the hub 2 is greater than the distance of the position D from the hub 2. In this case, whether the nacelle 3 or the tower 5 is uniformly stressed can be determined by the difference in magnitude between the first withstand force and the second withstand force, and when the difference in magnitude exceeds a predetermined threshold, the nacelle 3 can be determined. Or the tower 5 is unevenly stressed. At this time, it is necessary to change the external force received by the nacelle 3 or the tower 5 to avoid damage to the nacelle 3 or the tower 5.
作为示例,所述重心位置的改变包括改变方向和改变程度,其中,当所述重心位置朝向所述机舱的头部偏移并且所述改变程度超过预定阈值时,所述风力确定模块确定所述期望受到的风力为下压力;当所述重心位置朝向所述机舱的尾部偏移并且所述改变程度超过所述预定阈值时,所述风力确定模块确定所述期望受到的风力为上升力。As an example, the change in the position of the center of gravity includes a change in direction and a degree of change, wherein the wind determination module determines the said center of gravity position is offset toward a head of the nacelle and the degree of change exceeds a predetermined threshold The wind force that is desired to be subjected is a downforce; when the center of gravity position is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold, the wind determination module determines that the wind force desired to be subjected is a rising force.
作为示例,所述姿态调整模块根据所述风向信息和所述调平机翼的当前姿态确定所述调平机翼是否已经获得所述期望受到的风力;当所述调平机翼未获得所述期望受到的风力时,所述姿态调整模块通过调整所述调平机翼围绕特定轴线旋转的角度来使所述调平机翼获得所述期望受到的风力。As an example, the attitude adjustment module determines whether the leveling wing has obtained the desired wind force according to the wind direction information and the current attitude of the leveling wing; when the leveling wing does not obtain the When the wind is desired to be received, the attitude adjustment module causes the leveling wing to obtain the desired wind force by adjusting an angle at which the leveling wing rotates about a particular axis.
作为示例,可通过电机旋转绝对值编码器检测电机旋转的角度,从而可根据电机旋转的角度计算调平机翼旋转的角度。As an example, the angle of rotation of the motor can be detected by a motor rotary absolute encoder so that the angle of the leveling wing rotation can be calculated from the angle of rotation of the motor.
在一个优选的实施例中,所述特定轴线平行于水平面,并且垂直于机舱的长度方向。在另一个实施例中,所述特定轴线为两个或更多个,每个轴线上可设置至少一个叶片。在另一个优选的实施例中,所述两个或更多个特定轴线在特定平面内,机舱的长度方向垂直于所述特定平面,每个特定轴线对应于至少一个绕该特定轴线旋转的调平机翼的叶片。In a preferred embodiment, the particular axis is parallel to the horizontal plane and perpendicular to the length of the nacelle. In another embodiment, the particular axis is two or more, and at least one blade may be disposed on each axis. In another preferred embodiment, the two or more specific axes are in a particular plane, the length direction of the nacelle being perpendicular to the particular plane, each particular axis corresponding to at least one rotation about the particular axis The blades of the flat wing.
作为示例,所述姿态调整模块可确定当所述调平机翼获得所述期望受到的风力时所述调平机翼的期望位置,并根据感测得到的所述调平机翼的位置调整所述调平机翼的旋转角度,以使所述调平机翼旋转到所述期望位置。As an example, the attitude adjustment module may determine a desired position of the leveling wing when the leveling wing obtains the desired wind force, and adjust the position of the leveling wing according to the sensing The angle of rotation of the leveling wing is such that the leveling wing is rotated to the desired position.
作为示例,可通过位置传感器感测调平机翼的位置。位置传感器可位于叶片10和/或叶片11附近并设置在机舱或调平装置上,以感测调平机翼的叶片的位置。可基于位置传感器感测到的调平机翼的位置确定调平机翼是否达到期望位置。还可根据感测到的位置确定调平机翼是否达到最大旋转位置,并在调平机翼达到最大旋转位置时,使调平机翼停止转动或向相反方向转动,以便避免调平机翼损坏。As an example, the position of the leveling wing can be sensed by the position sensor. A position sensor can be located adjacent the blade 10 and/or the blade 11 and disposed on the nacelle or leveling device to sense the position of the blade of the leveling wing. Whether the leveling wing reaches a desired position can be determined based on the position of the leveling wing sensed by the position sensor. The leveling wing can also be determined according to the sensed position to reach the maximum rotational position, and when the leveling wing reaches the maximum rotational position, the leveling wing stops rotating or rotates in the opposite direction to avoid leveling the wing damage.
图8示出根据本发明的示例性实施例的调平控制方法的流程图。FIG. 8 shows a flow chart of a leveling control method according to an exemplary embodiment of the present invention.
如图8中所示,本示例性实施例的调平控制方法可用于控制本发明的示例性实施例中描述的调平装置,且包括:步骤201,接收测量得到的所述风力发电机组的受力信息及风向信息;步骤202:根据所述受力信息和所述风向信息调整所述调平机翼的姿态以调整所述调平机翼受到的风力。As shown in FIG. 8, the leveling control method of the present exemplary embodiment may be used to control the leveling device described in the exemplary embodiment of the present invention, and includes: step 201, receiving the measured wind turbine generator set Force information and wind direction information; Step 202: Adjust the posture of the leveling wing according to the force information and the wind direction information to adjust the wind force received by the leveling wing.
作为示例,所述步骤202可包括:根据所述受力信息确定所述机舱的重心位置的改变;根据所述重心位置的改变确定所述调平机翼的期望受到的风力;根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态。As an example, the step 202 may include: determining a change in a position of a center of gravity of the nacelle according to the force information; determining a desired wind force of the leveling wing according to the change in the position of the center of gravity; according to the wind direction The information and the desired wind force are adjusted to adjust the attitude of the wing.
作为示例,受力信息可包括:风力发电机组上的第一位置受到的第一承受力的大小和所述风力发电机组上的第二位置受到的第二承受力的大小,所述根据所述受力信息确定所述机舱的重心位置的改变的步骤包括:计算所述第一承受力和所述第二承受力之间的大小差异;根据所述大小差异确定所述机舱的重心位置的改变。例如,参照图4和图5,可测量位置C收到的第一承受力的大小和位置D受到的第二承受力的大小,位置C和位置D的连线与机舱3的中心线平行,位置C距离轮毂2的距离大于位置D距离轮毂2的距离。在这种情况下,可通过述第一承受力和第二承受力之间的大小差异来确定机舱3或塔筒5是否受力均匀,当所述大小差异超过预定阈值时,可确定 出需要改变机舱3或塔筒5受到的外力,以避免机舱3或塔筒5损坏。As an example, the force information may include: a magnitude of a first bearing force received by the first position on the wind turbine and a magnitude of a second bearing force received by the second position on the wind turbine, The step of determining the change in the position of the center of gravity of the nacelle by the force information includes: calculating a difference in size between the first withstand force and the second withstand force; determining a change in the position of the center of gravity of the nacelle according to the difference in the size . For example, referring to FIG. 4 and FIG. 5, the magnitude of the first bearing force received by the position C and the magnitude of the second bearing force received by the position D can be measured, and the line connecting the position C and the position D is parallel to the center line of the nacelle 3, The distance of the position C from the hub 2 is greater than the distance of the position D from the hub 2. In this case, whether the nacelle 3 or the tower 5 is uniformly stressed can be determined by the difference in magnitude between the first withstand force and the second withstand force, and when the difference in size exceeds a predetermined threshold, the need can be determined. The external force received by the nacelle 3 or the tower 5 is changed to avoid damage to the nacelle 3 or the tower 5.
作为示例,重心位置的改变包括改变方向和改变程度,所述根据所述重心位置的改变确定所述调平机翼的期望受到的风力的步骤可包括:当所述重心位置朝向所述机舱的头部偏移并且所述改变程度超过预定阈值时,所述期望受到的风力为下压力;当所述重心位置朝向所述机舱的尾部偏移并且所述改变程度超过所述预定阈值时,所述期望受到的风力为上升力。As an example, the change in the position of the center of gravity includes a change in direction and a degree of change, the step of determining the desired wind force of the leveling wing according to the change in the position of the center of gravity may include: when the position of the center of gravity is toward the nacelle When the head is offset and the degree of change exceeds a predetermined threshold, the wind force that is desired to be subjected is a downward pressure; when the position of the center of gravity is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold, The wind that is expected to be received is a rising force.
作为示例,所述根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态的步骤可包括:根据所述风向信息和所述调平机翼的当前姿态确定所述调平机翼是否已经获得所述期望受到的风力;当所述调平机翼未获得所述期望受到的风力时,通过调整所述调平机翼围绕特定轴线旋转的角度来使所述调平机翼获得所述期望受到的风力。As an example, the step of adjusting the attitude of the leveling wing according to the wind direction information and the wind force desired to be received may include determining the tone according to the wind direction information and a current posture of the leveling wing Whether the flat wing has obtained the desired wind force; when the leveling wing does not obtain the desired wind force, the leveling is adjusted by adjusting the angle at which the leveling wing rotates about a particular axis The wing obtains the desired wind force.
作为示例,所述调整所述调平机翼围绕特定轴线旋转的角度的步骤可包括:确定当所述调平机翼获得所述期望受到的风力时所述调平机翼的期望位置;根据感测得到的所述调平机翼的位置调整所述调平机翼的旋转角度,以使所述调平机翼旋转到所述期望位置。As an example, the step of adjusting an angle at which the leveling wing rotates about a particular axis may include determining a desired position of the leveling wing when the leveling wing obtains the desired wind force; The sensed position of the leveling wing adjusts the angle of rotation of the leveling wing to rotate the leveling wing to the desired position.
可通过图9所示流程来计算本发明的示例性实施例中描述的期望受到的风力。如图9中所示,在步骤301,获得第一承受力的大小X和第二承受力的大小Y。在步骤302,比较X和Y的差值的绝对值是否小于用于开始调平的阈值Z,如果是则进入步骤303,否则进入步骤304。在步骤303,确定不需要调整机舱的重心位置。在步骤304,比较判断X是否大于Y,如果是,则进入步骤306,否则进入步骤305。在步骤306,确定期望受到的风力为下压力。在步骤305,确定期望受到的风力为上升力。The desired wind force described in the exemplary embodiment of the present invention can be calculated by the flow shown in FIG. As shown in FIG. 9, at step 301, the magnitude X of the first withstand force and the magnitude Y of the second withstand force are obtained. At step 302, it is compared whether the absolute value of the difference between X and Y is less than the threshold Z for starting the leveling, and if so, proceeds to step 303, otherwise to step 304. At step 303, it is determined that there is no need to adjust the center of gravity of the nacelle. At step 304, a comparison is made to determine if X is greater than Y, and if so, then proceeds to step 306, otherwise to step 305. At step 306, it is determined that the wind force that is desired to be received is a downforce. At step 305, it is determined that the wind force that is desired to be received is a rising force.
在步骤305之后,可进入步骤307,判断调平机翼在当前环境下是否具备获得上升力的能力,如果是,则进入步骤310,否则进入步骤309,所述当前环境至少包括风向。在步骤310,调整调平机翼的姿态,以使调平机翼获得上升力。在步骤309,发出第一报警,第一报警指示调平机翼在当前环境下不具备获得上升力的能力。After step 305, step 307 may be performed to determine whether the leveling wing has the ability to obtain the lifting force in the current environment. If yes, proceed to step 310, otherwise proceed to step 309, the current environment including at least the wind direction. At step 310, the attitude of the leveling wing is adjusted to achieve a lifting force for the leveling wing. At step 309, a first alarm is issued, the first alarm indicating that the leveling wing does not have the ability to obtain a lift in the current environment.
在步骤306之后,可进入步骤308,判断调平机翼在当前环境下是否具备获得下降力的能力,如果是,则进入步骤311,否则进入步骤312。在步骤311,调整调平机翼的姿态,以使调平机翼获得下降力。在步骤312,发出第二报警,第二报警指示调平机翼在当前环境下不具备获得下降力的能力。After step 306, the process may proceed to step 308 to determine whether the leveling wing has the ability to obtain the descent force in the current environment. If yes, proceed to step 311, otherwise proceed to step 312. At step 311, the attitude of the leveling wing is adjusted to achieve a lowering force for the leveling wing. At step 312, a second alarm is issued indicating that the leveling wing does not have the ability to obtain a descent force in the current environment.
所述具备获得上升力的能力是指:调平机翼在其运动范围内的至少一个位置处,受到的风力在竖直向上方向的分力或受到的风力在垂直于机舱轴线且向上的方向上的分力大于零。所述具备获得下降力的能力是指:调平机翼在其运动范围内的至少一个位置处,受到的风力在竖直向下方向的分力或受到的风力在垂直于机舱轴线且向下的方向上的分力大于零。The ability to obtain the lifting force refers to: at least one position of the leveling wing in its range of motion, the component of the wind received in the vertical upward direction or the wind received in the direction perpendicular to the axis of the nacelle and upward The upper component is greater than zero. The ability to obtain a descending force means that the leveling wing is at least one position within its range of motion, and the component of the wind subjected to the vertical downward direction or the received wind force is perpendicular to the cabin axis and downward. The force component in the direction is greater than zero.
当发出第一报警或第二报警时,可检测是否出现测量部件(例如,测风机构、测力机构、位置传感器等)故障。When the first alarm or the second alarm is issued, it is possible to detect whether a failure of the measuring component (for example, a wind measuring mechanism, a force measuring mechanism, a position sensor, etc.) occurs.
图10是示出调平机翼的姿态、风向以及调平机翼的受到的力之间的对应关系的示意图。Fig. 10 is a schematic view showing the correspondence relationship between the posture of the leveling wing, the wind direction, and the force received by the leveling wing.
在本示例性实施例中,调平机翼的主体呈叶片状,如图10中所示,调平机翼的主体的长度方向垂直于纸面。在图10中,风向为F,F可被分解为水平方向的风向f1和竖直方向的风向f2。在第一姿态下,调平机翼的延伸方向平行于风向。在这种情况下,调平机翼不能够对机舱的重心位置进行调节。在第二姿态下,调平机翼的延伸方向与风向F成锐角,调平机翼能够获得下压力。在第三姿态下,风向F垂直于调平机翼的延伸方向,调平机翼也能够获得下压力。In the present exemplary embodiment, the body of the leveling wing is in the shape of a blade, as shown in Fig. 10, the longitudinal direction of the body of the leveling wing is perpendicular to the plane of the paper. In Fig. 10, the wind direction is F, and F can be decomposed into a wind direction f1 in the horizontal direction and a wind direction f2 in the vertical direction. In the first attitude, the direction in which the leveling wings extend is parallel to the wind direction. In this case, the leveling wing is not able to adjust the position of the center of gravity of the nacelle. In the second attitude, the direction of the leveling wing extends at an acute angle to the wind direction F, and the leveling wing can obtain the downforce. In the third attitude, the wind direction F is perpendicular to the direction in which the leveling wing extends, and the leveling wing is also able to obtain the downforce.
然而,在图10所示示例性实施例中,调平机翼仅能够在第一姿态至第三姿态限定的范围内变化时,调平机翼仅具备获得下压力的能力,而不具备获得上升力的能力。However, in the exemplary embodiment shown in FIG. 10, the leveling wing is only capable of obtaining the downforce when the leveling wing is only changeable within the range defined by the first attitude to the third attitude, without obtaining The ability to rise.
图11是示出调平机翼的姿态、风向以及调平机翼的受到的力之间的对应关系的示意图。Fig. 11 is a schematic view showing the correspondence relationship between the posture of the leveling wing, the wind direction, and the force received by the leveling wing.
如图11中所示,风向为F,F可被分解为水平方向的风向f1和竖直方向的风向f2。在第四姿态下,调平机翼的延伸方向平行于风向。在这种情况下,调平机翼不能够对机舱的重心位置进行调节。在第五姿态下,调平机翼的延伸方向与风向F成锐角,调平机翼能够获得上升力。在第六姿态下,风向F垂直于调平机翼的延伸方向,调平机翼也能够获得上升力。As shown in FIG. 11, the wind direction is F, and F can be decomposed into a wind direction f1 in the horizontal direction and a wind direction f2 in the vertical direction. In the fourth attitude, the direction of the leveling wing is parallel to the wind direction. In this case, the leveling wing is not able to adjust the position of the center of gravity of the nacelle. In the fifth attitude, the direction of the leveling wing extends at an acute angle to the wind direction F, and the leveling wing can obtain the lifting force. In the sixth attitude, the wind direction F is perpendicular to the direction in which the leveling wing extends, and the leveling wing can also obtain the lifting force.
然而,在图11所示示例性实施例中,调平机翼仅能够在第四姿态至第六姿态限定的范围内变化时,调平机翼具备获得上升力的能力,而不具备获得下压力的能力。However, in the exemplary embodiment shown in FIG. 11, the leveling wing is only capable of obtaining the lifting force when the leveling wing is only changeable within the range defined by the fourth posture to the sixth posture, and does not have the ability to obtain The ability to stress.
如图10和图11所示,风力对应于调平机翼的姿态。因此,期望受到的风力对应于期望的姿态。As shown in Figures 10 and 11, the wind force corresponds to the attitude of the leveling wing. Therefore, it is desirable that the wind force received corresponds to the desired posture.
在图10中,如果期望受到的风力是下压力,则当调平机翼的当前姿态是第一姿态时,需要使调平机翼旋转,例如,使调平机翼到达与第二姿态或第三姿态对应的位置,以便使调平机翼获得下压力。In FIG. 10, if the wind force desired to be received is the downforce, when the current attitude of the leveling wing is the first attitude, the leveling wing needs to be rotated, for example, to bring the leveling wing to the second attitude or The position corresponding to the third posture is such that the leveling wing receives the downforce.
在图11中,如果期望受到的风力是上升力,则当调平机翼的当前姿态是第四姿态时,需要使调平机翼旋转,例如,使调平机翼到达与第五姿态或第六姿态对应的位置,以便使调平机翼获得上升力。In FIG. 11, if the wind force desired to be received is a rising force, when the current attitude of the leveling wing is the fourth attitude, the leveling wing needs to be rotated, for example, to bring the leveling wing to the fifth posture or The position corresponding to the sixth posture, in order to obtain the lifting force of the leveling wing.
在本发明的示例性实施例中,调平机翼与轮毂可沿机舱的长度方向分别位于机舱的重心的两侧,从而可使机舱受到的风力均衡。例如,调平机翼可设置在机舱的后部。调平机翼的叶片数量不受限制,可以是一片或更多片。In an exemplary embodiment of the invention, the leveling wings and the hub may be located on either side of the center of gravity of the nacelle along the length of the nacelle to equalize the wind received by the nacelle. For example, a leveling wing can be placed at the rear of the nacelle. The number of blades of the leveling wing is not limited and may be one or more pieces.
上述实施例仅仅是示例,调平机翼的位置不限于上述实施例。例如,调平机翼与轮毂可沿机舱的长度方向位于机舱的重心的同一侧。The above embodiment is merely an example, and the position of the leveling wing is not limited to the above embodiment. For example, the leveling wing and hub may be located on the same side of the center of gravity of the nacelle along the length of the nacelle.
在本发明的实施例中,通过旋转调平机翼来改变调平机翼的姿态,同时,可改变调平机翼的延伸方向与风向之间的夹角以改变调平机翼受到的风力的大小。In an embodiment of the invention, the attitude of the leveling wing is changed by rotating the leveling wing, and at the same time, the angle between the direction of extension of the leveling wing and the wind direction can be changed to change the wind received by the leveling wing. the size of.
根据本发明的另一示例性实施例,提供了一种风力发电机组的调平系统。所述调平系统可包括本发明的示例性实施例中所述的调平控制装置及调平装置。According to another exemplary embodiment of the present invention, a leveling system for a wind power generator set is provided. The leveling system can include a leveling control device and a leveling device as described in the exemplary embodiments of the present invention.
根据本发明的另一示例性实施例,提供了一种计算机可读存储介质,存储有当被处理器执行时使得处理器执行本发明的示例性实施例中所述的调平控制方法的指令。According to another exemplary embodiment of the present invention, there is provided a computer readable storage medium storing instructions that, when executed by a processor, cause a processor to perform a leveling control method as described in an exemplary embodiment of the present invention .
根据本发明的另一示例性实施例,提供了一种计算机设备。所述计算机设备存储有当被处理器执行时使得处理器执行本发明的示例性实施例中所述的调平控制方法的指令。According to another exemplary embodiment of the present invention, a computer device is provided. The computer device stores instructions that, when executed by a processor, cause the processor to perform the leveling control method described in the exemplary embodiments of the present invention.
根据本发明的另一示例性实施例,提供了一种风力发电机组。所述风力发电机组可包括本发明的示例性实施例中所述的调平装置,或者包括本发明的示例性实施例中所述的调平控制装置,或者包括本发明的示例性实施例中所述的调平控制系统,或者包括本发明的示例性实施例中所述的调平系统,或者包括本发明的示例性实施例中所述的计算机可读存储介质,或者包括本发明的示例性实施例中所述的计算机设备。According to another exemplary embodiment of the present invention, a wind power generator set is provided. The wind turbine may comprise a leveling device as described in an exemplary embodiment of the invention, or a leveling control device as described in an exemplary embodiment of the invention, or in an exemplary embodiment of the invention The leveling control system, or a leveling system as described in an exemplary embodiment of the invention, or a computer readable storage medium as described in an exemplary embodiment of the invention, or an example of the invention Computer device as described in the embodiments.
本发明采用调平机翼调整机舱的重心位置,使得机舱和/或塔筒稳定。由此,可避免机舱的偏航加速度改变以及偏航加速度改变引发的故障,减少塔 筒和风力发电机组的一部分部件(例如,偏航轴承)的损耗,减少次生风险。The present invention employs a leveling wing to adjust the center of gravity of the nacelle to stabilize the nacelle and/or tower. As a result, changes in the yaw acceleration of the nacelle and failures caused by changes in yaw acceleration can be avoided, reducing losses in the tower and some components of the wind turbine (eg, yaw bearings), reducing the secondary risk.
本发明的示例性实施例提供的方法和装置可由独立的控制器(例如,PLC控制器)实现或者由风力发电机组的控制器实现。The methods and apparatus provided by the exemplary embodiments of the present invention may be implemented by a stand-alone controller (e.g., a PLC controller) or by a controller of a wind turbine.
本发明实施例中的计算机可读存储介质包含程序命令、数据文件、数据结构等、或它们的组合。被记录在计算机可读存储介质中的程序可被设计或被配置以实现本发明的方法。计算机可读存储介质包括用于存储并执行程序和/或命令的硬件系统。硬件系统的示例有磁介质(诸如硬盘、软盘、磁带)、光介质(诸如CD-ROM和DVD)、磁光介质(诸如软光盘、ROM、RAM、闪存等)。程序和/或命令包括由编译器编译的汇编语言代码或机器代码和由解释器解释的更高级语言代码。硬件系统可利用至少一个软件模块来实施以符合本发明。The computer readable storage medium in the embodiments of the present invention includes program commands, data files, data structures, and the like, or a combination thereof. A program recorded in a computer readable storage medium can be designed or configured to implement the methods of the present invention. Computer readable storage media includes hardware systems for storing and executing programs and/or commands. Examples of hardware systems are magnetic media (such as hard disks, floppy disks, magnetic tapes), optical media (such as CD-ROMs and DVDs), magneto-optical media (such as floppy disks, ROM, RAM, flash memory, etc.). Programs and/or commands include assembly language code or machine code compiled by a compiler and higher level language code interpreted by an interpreter. The hardware system can be implemented with at least one software module to comply with the present invention.
可使用一个或多个通用或专用计算机(例如,处理器、控制器、数字信号处理器、微型计算机、现场可编程阵列、可编程逻辑单元、微处理器或能够运行软件或执行指令的任何其它装置)来实施上述方法、装置和/或系统的至少一部分。所述至少一部分可在操作系统中实现,也可在操作系统下操作的一个或多个软件应用中实现。One or more general purpose or special purpose computers (eg, processors, controllers, digital signal processors, microcomputers, field programmable arrays, programmable logic units, microprocessors, or any other capable of executing software or executing instructions) Apparatus) to implement at least a portion of the above methods, apparatus, and/or systems. The at least a portion can be implemented in an operating system or in one or more software applications operating under an operating system.
为了示意和描述的目的,给出了对本发明的描述,该描述的意图不在于以所公开的形式来穷尽或限制本发明。对于本领域普通技术人员来说,在不脱离本发明构思的情况下,可对实施例进行各种修改和改变。The description of the present invention has been presented for purposes of illustration and description. Various modifications and changes may be made to the embodiments without departing from the spirit and scope of the invention.

Claims (19)

  1. 一种风力发电机组的调平装置,其特征在于,所述风力发电机组包括机舱,所述调平装置包括:A leveling device for a wind power generator, characterized in that the wind power generator comprises a nacelle, and the leveling device comprises:
    调平机翼,设置在所述机舱上,用于将受到的风力传递给所述机舱以调整所述机舱的重心位置;a leveling wing disposed on the nacelle for transmitting the received wind power to the nacelle to adjust a center of gravity of the nacelle;
    驱动机构,与所述调平机翼连接,用于调整所述调平机翼的姿态以调整所述调平机翼受到的风力。a driving mechanism coupled to the leveling wing for adjusting a posture of the leveling wing to adjust a wind force received by the leveling wing.
  2. 如权利要求1所述的调平装置,其特征在于,所述驱动机构包括驱动器和传动机构;The leveling device of claim 1 wherein said drive mechanism comprises a driver and a transmission;
    所述传动机构包括齿轮组和传动轴,所述驱动器、所述齿轮组及所述传动轴依次连接,所述调平机翼安装在所述传动轴上并且随所述传动轴转动。The transmission mechanism includes a gear set and a transmission shaft, the drive, the gear set and the transmission shaft are sequentially connected, and the leveling wing is mounted on the transmission shaft and rotates with the transmission shaft.
  3. 一种风力发电机组的调平控制方法,其特征在于,所述风力发电机组包括如权利要求1或2所述的调平装置,其中,所述调平控制方法包括:A leveling control method for a wind power generator, characterized in that the wind power generator set includes the leveling device according to claim 1 or 2, wherein the leveling control method comprises:
    接收测量得到的所述风力发电机组的受力信息及风向信息;Receiving the measured force information and wind direction information of the wind power generator set;
    根据所述受力信息和所述风向信息调整所述调平机翼的姿态以调整所述调平机翼受到的风力。Adjusting the attitude of the leveling wing according to the force information and the wind direction information to adjust the wind force received by the leveling wing.
  4. 如权利要求3所述的调平控制方法,其特征在于,所述根据所述受力信息和所述风向信息调整所述调平机翼的姿态以调整所述调平机翼受到的风力的步骤包括:The leveling control method according to claim 3, wherein said adjusting said attitude of said leveling wing based on said force information and said wind direction information to adjust a wind force received by said leveling wing The steps include:
    根据所述受力信息确定所述机舱的重心位置的改变;Determining a change in a position of a center of gravity of the nacelle according to the force information;
    根据所述重心位置的改变确定所述调平机翼的期望受到的风力;Determining a desired wind force of the leveling wing according to a change in the position of the center of gravity;
    根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态。The attitude of the leveling wing is adjusted based on the wind direction information and the desired wind force.
  5. 如权利要求4所述的调平控制方法,其特征在于,所述受力信息包括:所述风力发电机组上的第一位置受到的第一承受力的大小和所述风力发电机组上的第二位置受到的第二承受力的大小,The leveling control method according to claim 4, wherein the force information includes: a magnitude of a first bearing force received by the first position on the wind power generator set and a number on the wind power generating set The magnitude of the second bearing force received by the two positions,
    所述根据所述受力信息确定所述机舱的重心位置的改变的步骤包括:The step of determining a change in the position of the center of gravity of the nacelle according to the force information includes:
    计算所述第一承受力和所述第二承受力之间的大小差异;Calculating a difference in size between the first withstand force and the second withstand force;
    根据所述大小差异确定所述机舱的重心位置的改变。A change in the position of the center of gravity of the nacelle is determined based on the difference in size.
  6. 如权利要求4所述的调平控制方法,其特征在于,所述重心位置的改变包括改变方向和改变程度,所述根据所述重心位置的改变确定所述调平机 翼的期望受到的风力的步骤包括:The leveling control method according to claim 4, wherein the change in the position of the center of gravity includes changing a direction and a degree of change, and determining a desired wind force of the leveling wing according to a change in the position of the center of gravity The steps include:
    当所述重心位置朝向所述机舱的头部偏移并且所述改变程度超过预定阈值时,所述期望受到的风力为下压力;When the position of the center of gravity is offset toward the head of the nacelle and the degree of change exceeds a predetermined threshold, the desired wind force is a downforce;
    当所述重心位置朝向所述机舱的尾部偏移并且所述改变程度超过所述预定阈值时,所述期望受到的风力为上升力。The desired wind force is a rising force when the center of gravity position is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold.
  7. 如权利要求4所述的调平控制方法,其特征在于,所述根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态的步骤包括:The leveling control method according to claim 4, wherein the step of adjusting the posture of the leveling wing according to the wind direction information and the wind force desired to be received comprises:
    根据所述风向信息和所述调平机翼的当前姿态确定所述调平机翼是否已经获得所述期望受到的风力;Determining, according to the wind direction information and a current attitude of the leveling wing, whether the leveling wing has obtained the desired wind force;
    当所述调平机翼未获得所述期望受到的风力时,通过调整所述调平机翼围绕特定轴线旋转的角度来使所述调平机翼获得所述期望受到的风力。The leveling wing obtains the desired wind force by adjusting an angle at which the leveling wing rotates about a particular axis when the leveling wing does not achieve the desired wind force.
  8. 如权利要求7所述的调平控制方法,其特征在于,所述调整所述调平机翼围绕所述特定轴线旋转的角度的步骤包括:The leveling control method according to claim 7, wherein said step of adjusting an angle at which said leveling wing rotates about said specific axis comprises:
    确定当所述调平机翼获得所述期望受到的风力时所述调平机翼的期望位置;Determining a desired position of the leveling wing when the leveling wing obtains the desired wind force;
    根据感测得到的所述调平机翼的位置调整所述调平机翼的旋转角度,以使所述调平机翼旋转到所述期望位置。Adjusting a rotation angle of the leveling wing based on the sensed position of the leveling wing to rotate the leveling wing to the desired position.
  9. 一种风力发电机组的调平控制装置,其特征在于,所述风力发电机组包括如权利要求1或2所述的调平装置,其中,所述调平控制装置包括:A leveling control device for a wind power generator, characterized in that the wind power generator set includes the leveling device according to claim 1 or 2, wherein the leveling control device comprises:
    接收模块,用于接收测量得到的所述风力发电机组的受力信息及风向信息;a receiving module, configured to receive the measured force information and wind direction information of the wind power generator set;
    控制模块,用于根据接收模块接收到的受力信息和风向信息调整所述调平机翼的姿态以调整所述调平机翼受到的风力。And a control module, configured to adjust a posture of the leveling wing according to the force information and the wind direction information received by the receiving module to adjust a wind force received by the leveling wing.
  10. 如权利要求9所述的调平控制装置,其特征在于,所述控制模块包括:The leveling control apparatus according to claim 9, wherein said control module comprises:
    重心确定模块,用于根据所述受力信息确定所述机舱的重心位置的改变;a center of gravity determining module, configured to determine a change in a position of a center of gravity of the nacelle according to the force information;
    风力确定模块,用于根据所述重心位置的改变确定所述调平机翼的期望受到的风力;a wind determining module, configured to determine a desired wind force of the leveling wing according to the change in the position of the center of gravity;
    姿态调整模块,用于根据所述风向信息和所述期望受到的风力调整所述调平机翼的姿态。And an attitude adjustment module, configured to adjust a posture of the leveling wing according to the wind direction information and the desired wind force.
  11. 如权利要求10所述的调平控制装置,其特征在于,所述受力信息包 括:所述风力发电机组上的第一位置受到的第一承受力的大小和所述风力发电机组上的第二位置受到的第二承受力的大小,The leveling control apparatus according to claim 10, wherein said force information comprises: a magnitude of a first bearing force received by said first position on said wind power generator set and a number on said wind power generating set The magnitude of the second bearing force received by the two positions,
    其中,所述重心确定模块计算所述第一承受力和所述第二承受力之间的大小差异,并根据所述大小差异确定所述机舱的重心位置的改变。The center of gravity determination module calculates a difference in size between the first withstand force and the second withstand force, and determines a change in a position of a center of gravity of the nacelle according to the difference in size.
  12. 如权利要求10所述的调平控制装置,其特征在于,所述重心位置的改变包括改变方向和改变程度,The leveling control device according to claim 10, wherein the change in the position of the center of gravity includes a change in direction and a degree of change,
    其中,当所述重心位置朝向所述机舱的头部偏移并且所述改变程度超过预定阈值时,所述风力确定模块确定所述期望受到的风力为下压力;Wherein, when the position of the center of gravity is offset toward the head of the nacelle and the degree of change exceeds a predetermined threshold, the wind determination module determines that the wind force desired to be received is a downward pressure;
    当所述重心位置朝向所述机舱的尾部偏移并且所述改变程度超过所述预定阈值时,所述风力确定模块确定所述期望受到的风力为上升力。The wind determination module determines that the desired wind force is a rising force when the center of gravity position is offset toward the tail of the nacelle and the degree of change exceeds the predetermined threshold.
  13. 如权利要求10所述的调平控制装置,其特征在于,所述姿态调整模块根据所述风向信息和所述调平机翼的当前姿态确定所述调平机翼是否已经获得所述期望受到的风力;The leveling control apparatus according to claim 10, wherein said attitude adjustment module determines whether said leveling wing has obtained said expectation based on said wind direction information and said current attitude of said leveling wing Wind power
    当所述调平机翼未获得所述期望受到的风力时,所述姿态调整模块通过调整所述调平机翼围绕特定轴线旋转的角度来使所述调平机翼获得所述期望受到的风力。The attitude adjustment module obtains the desired level of the leveling wing by adjusting an angle at which the leveling wing rotates about a particular axis when the leveling wing does not obtain the desired wind force Wind power.
  14. 如权利要求13所述的调平控制装置,其特征在于,所述姿态调整模块确定当所述调平机翼获得所述期望受到的风力时所述调平机翼的期望位置,并根据感测得到的所述调平机翼的位置调整所述调平机翼的旋转角度,以使所述调平机翼旋转到所述期望位置。A leveling control apparatus according to claim 13 wherein said attitude adjustment module determines a desired position of said leveling wing when said leveling wing obtains said desired wind force, and The measured position of the leveling wing adjusts the angle of rotation of the leveling wing to rotate the leveling wing to the desired position.
  15. 一种风力发电机组的调平控制系统,其特征在于,所述风力发电机组包括如权利要求1或2所述的调平装置,其中,所述调平控制系统包括:A leveling control system for a wind power generator, characterized in that the wind power generator set includes the leveling device according to claim 1 or 2, wherein the leveling control system comprises:
    测力机构,用于测量风力发电机组的受力信息;a force measuring mechanism for measuring the force information of the wind turbine;
    测风机构,用于测量风向信息;以及a wind measuring mechanism for measuring wind direction information;
    如权利要求9-14中的任意一项所述的调平控制装置。A leveling control device according to any one of claims 9-14.
  16. 一种风力发电机组的调平系统,其特征在于,包括如权利要求9-14中的任意一项所述的调平控制装置及如权利要求1或2所述的调平装置。A leveling system for a wind power generator, comprising the leveling control device according to any one of claims 9-14 and the leveling device according to claim 1 or 2.
  17. 一种计算机可读存储介质,存储有当被处理器执行时使得处理器执行如权利要求3-8中任意一项所述的调平控制方法的指令。A computer readable storage medium storing instructions that, when executed by a processor, cause a processor to perform the leveling control method of any of claims 3-8.
  18. 一种计算机设备,存储有当被处理器执行时使得处理器执行如权利要求3-8中任意一项所述的调平控制方法的指令。A computer device storing instructions for causing a processor to perform the leveling control method of any one of claims 3-8 when executed by a processor.
  19. 一种风力发电机组,其特征在于,包括如权利要求1或2所述的调平装置,或者如权利要求9-14中的任意一项所述的调平控制装置,或者如权利要求15所述的调平控制系统,或者如权利要求16所述的调平系统,或者如权利要求17所述的计算机可读存储介质,或者如权利要求18所述的计算机设备。A wind power generator comprising the leveling device according to claim 1 or 2, or the leveling control device according to any one of claims 9-14, or as claimed in claim 15. A leveling control system, or a leveling system according to claim 16, or a computer readable storage medium according to claim 17, or a computer device according to claim 18.
PCT/CN2018/098961 2018-03-30 2018-08-06 Wind turbine group, leveling device, and leveling control method, device and system WO2019184181A1 (en)

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