WO2022226680A1 - 变桨安装调试系统及其操作方法 - Google Patents

变桨安装调试系统及其操作方法 Download PDF

Info

Publication number
WO2022226680A1
WO2022226680A1 PCT/CN2021/089565 CN2021089565W WO2022226680A1 WO 2022226680 A1 WO2022226680 A1 WO 2022226680A1 CN 2021089565 W CN2021089565 W CN 2021089565W WO 2022226680 A1 WO2022226680 A1 WO 2022226680A1
Authority
WO
WIPO (PCT)
Prior art keywords
blade
signal
pitch
controller
vortex
Prior art date
Application number
PCT/CN2021/089565
Other languages
English (en)
French (fr)
Inventor
王晓宇
钱振华
刘鹏
杨春国
Original Assignee
远景能源有限公司
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 远景能源有限公司 filed Critical 远景能源有限公司
Priority to PCT/CN2021/089565 priority Critical patent/WO2022226680A1/zh
Priority to ES202390124A priority patent/ES2956834R1/es
Priority to MA63060A priority patent/MA63060A1/fr
Priority to CN202180002117.1A priority patent/CN113454336B/zh
Priority to MX2023011700A priority patent/MX2023011700A/es
Publication of WO2022226680A1 publication Critical patent/WO2022226680A1/zh
Priority to ZA2023/09552A priority patent/ZA202309552B/en

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/04—Automatic control; Regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D13/00—Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
    • F03D13/30—Commissioning, e.g. inspection, testing or final adjustment before releasing for production
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D17/00—Monitoring or testing of wind motors, e.g. diagnostics
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Definitions

  • the invention relates to the technical field of wind turbines, in particular to a pitch-variable installation and debugging system and an operation method thereof.
  • Wind energy is a kind of clean and safe energy, which can be continuously generated in nature and supplemented regularly, so the characteristics of wind energy resources are very obvious, and its development and utilization potential is huge.
  • Variable speed constant frequency technology began to emerge in the 1990s.
  • the speed of the rotor of the variable-speed constant-frequency wind turbine changes with the change of the wind speed, which can make more efficient use of wind energy, and can obtain constant-frequency electric energy through the variable-speed constant-frequency technology.
  • Pitch pitch refers to that the blades installed on the hub of large wind turbines change the pitch angle with the help of control technology and power system to change the aerodynamic characteristics of the blades, so that the blades and The stress condition of the whole machine is greatly improved.
  • Direct-drive wind turbines are pitch-adjustable fans.
  • the blades will rotate around their diameters when the wind speed changes. Rotate to the axis. Therefore, it is possible to have an almost optimal pitch angle and a lower cut-in wind speed over the entire wind speed range, and at high wind speeds, the pitch angle is changed to reduce the power angle, thereby reducing the aerodynamic force on the blade. This ensures that the output power of the impeller does not exceed the rated power of the generator.
  • the pitch mechanism is to adjust the pitch angle at any time according to the change of wind speed and control the absorbed mechanical energy when the wind speed is greater than the rated wind speed.
  • the pitch control can also realize fast and shock-free grid connection.
  • the pitch control system cooperates with the variable speed constant frequency technology, which ultimately improves the power generation efficiency and power quality of the entire wind power generation system.
  • the electric pitch system is that the three blades are respectively equipped with an independent electric pitch system, which mainly includes a slewing support, a reducer device, a servo motor and its driver. It provides the wind turbine with power output and sufficient braking capacity, so as to avoid the damage to the wind turbine caused by overload.
  • an independent electric pitch system which mainly includes a slewing support, a reducer device, a servo motor and its driver. It provides the wind turbine with power output and sufficient braking capacity, so as to avoid the damage to the wind turbine caused by overload.
  • the task of wind turbine installation and commissioning is to organically combine and coordinate the various systems of the unit to ensure the safe, long-term, stable and efficient operation of the unit.
  • the installation and commissioning of the pitch system of the wind turbine includes the hoisting of the blades (blades) on site, and when the transmission line of the power generation equipment and the power grid are disconnected, the temporary power supply or backup power supply is used, and the equipment is carried out according to the provisions of the design and equipment technical documents.
  • the wind farm installation and commissioning should adhere to the principle of safety first and prevention first.
  • the wind farm construction unit shall strictly review the commissioning unit’s commissioning plan, safety measures, organizational measures, etc., and designate the commissioning safety person in charge of the coordination, management and Supervision.
  • the installation and debugging of the pitch system must comply with the safety requirements of each system, especially the safety requirements of the whole machine, otherwise there will be personal safety hazards and safety risks of the wind turbine.
  • the installation and debugging personnel must have a considerable understanding of the functions of the various systems of the fan, and must be carried out by qualified personnel through training, especially on-site installation and debugging. This makes the installation and debugging of the pitch system depend on the training of personnel and the proficiency of the personnel. If the human factor is large, the risk of safety accidents cannot be ruled out. Incorrect operation will result in great loss of life and property.
  • the purpose of the present invention is to provide a pitch pitch installation and debugging system and an operation method thereof, so as to solve the problem that the installation and debugging of the existing pitch pitch system is greatly affected by human factors.
  • the present invention provides a pitch installation and debugging system, including:
  • each position sensor is configured to be mountable at the connection of the pitch system to the blade to detect the position of the blade;
  • each sub-controller is configured to perform the following actions:
  • the master controller is configured to operate the blades according to the enable signal.
  • the position sensor includes:
  • the first position sensor is configured to be able to be installed at the connection between the pitch system and the first blade, wherein the first position sensor is configured to detect whether the pitch angle of the first blade is in a safe position, and if the first blade If the pitch angle of the leaf is in a safe position, a safe position signal is sent to the first sub-controller;
  • the second position sensor is configured to be able to be installed at the connection between the pitch system and the second blade, wherein the second position sensor is configured to detect whether the pitch angle of the second blade is in a safe position, and if the second blade is in a safe position Whether the pitch angle of the leaf is in a safe position, send a safe position signal to the second sub-controller;
  • a third position sensor is configured to be able to be installed at the connection between the pitch system and the third blade, wherein the second position sensor is configured to detect whether the pitch angle of the third blade is in a safe position, and if the third blade is in a safe position Whether the pitch angle of the leaf is in a safe position, a safe position signal is sent to the third sub-controller.
  • the first sub-controller After receiving the safety position signal of the first position sensor, the first sub-controller sends the first safety signal to the main controller;
  • the second sub-controller After receiving the safety position signal of the second position sensor, the second sub-controller sends the second safety signal to the main controller;
  • the third sub-controller After receiving the safety position signal of the third position sensor, the third sub-controller sends a third safety signal to the main controller.
  • the general controller includes a first processor, a second processor and a third processor, wherein:
  • the first processor receives the first security signal, it generates a first enable signal, and sends the first enable signal to the second processor and the third processor respectively;
  • the second processor receives the second security signal, it generates a second enable signal, and sends the second enable signal to the first processor and the third processor respectively;
  • the third processor receives the third security signal, it generates a third enable signal, and sends the third enable signal to the first processor and the second processor respectively.
  • the general controller includes a first controller, a second controller and a third controller, wherein:
  • the first controller can perform the hoisting operation and the power-on operation on the first blade; otherwise, the hoisting operation on the first blade is prohibited and power-on operation;
  • the second controller can perform the hoisting operation and power-on operation on the second blade; otherwise, the hoisting operation on the second blade is prohibited and power-on operation;
  • the third controller can perform the hoisting operation and power-on operation on the third blade; otherwise, the hoisting operation on the third blade is prohibited and power-up operation.
  • an operation prohibition signal is sent to the first processor and the second processor.
  • the first controller prohibits the hoisting operation and the power-on operation of the first blade
  • the second controller prohibits the hoisting operation and the power-on operation of the second blade
  • the third controller prohibits the hoisting operation and the power-on operation of the third blade
  • the prohibition signal has a higher priority than the first enable signal, the second enable signal and the third enable signal.
  • the first controller hoists the first blade, it sends a hoisting end signal to the first processor. After the first processor receives the hoisting end signal, the first controller can power on the first blade. ;
  • the second controller hoists the second blade, it sends a hoisting end signal to the second processor.
  • the second processor receives the hoisting end signal, the second controller can power on the second blade.
  • the third controller hoists the third blade, it sends a hoisting end signal to the third processor. After the third processor receives the hoisting end signal, the third controller can power on the third blade. .
  • the general controller further includes an anti-vortex excitation processor and an anti-vortex excitation controller, wherein:
  • the first controller After the first controller powers on the first blade, it sends a first power-on end signal to the anti-vortex excitation processor;
  • the second controller After the second controller powers on the second blade, it sends a second power-on end signal to the anti-vortex excitation processor;
  • the third controller After the third controller powers on the third blade, it sends a third power-on end signal to the anti-vortex excitation processor;
  • the anti-vortex excitation controller can simultaneously control the first blade, the second blade and the third power-on end signal.
  • the three blades are operated in anti-vortex position simultaneously.
  • the hoisting operation includes: hoisting the first propeller blade, the second propeller blade or the third propeller blade until the position can be docked with the pitch pitch system, and then hoisting the third propeller blade.
  • a blade, a second blade or a third blade is connected to the pitch system;
  • the power-on operation includes: powering on the pitch system, then driving the pitch system to drive the first blade, the second blade or the third blade to rotate, and adjusting the first blade, the second blade or the third blade the pitch angle of the blade;
  • the anti-vortex-induced position operation includes: driving the pitch system to drive the first blade, the second blade and the third blade to rotate, so as to change the pitch angle of the first blade, the second blade and the third blade are adjusted to the anti-vortex-induced position.
  • the position sensor includes:
  • a fourth position sensor configured to be installed at the junction of the pitch system and the first blade to detect whether the pitch angle of the first blade is in an anti-vortex-induced position
  • a fifth position sensor configured to be installed at the connection of the pitch system to the second blade to detect whether the pitch angle of the second blade is in an anti-vortex-induced position
  • a sixth position sensor configured to be installed at the junction of the pitch system with the third blade to detect whether the pitch angle of the third blade is in an anti-vortex-induced position
  • the first sub-controller After receiving the anti-vortex-induced position signal of the fourth position sensor, the first sub-controller sends the first anti-vortex-induced signal to the anti-vortex-induced processor;
  • the second sub-controller After receiving the anti-vortex-induced position signal of the fifth position sensor, the second sub-controller sends a second anti-vortex-induced signal to the anti-vortex-induced processor;
  • the third sub-controller After receiving the anti-vortex-induced position signal of the sixth position sensor, the third sub-controller sends a third anti-vortex-induced signal to the anti-vortex-induced processor.
  • the anti-vortex excitation processor can receive the first anti-vortex excitation signal, the second anti-vortex excitation signal and the third anti-vortex excitation signal at the same time, the anti-vortex The processor generates an installation and debugging end signal.
  • the pitch installation and debugging system further includes an operation panel, wherein the operation panel includes:
  • the first signal display device is configured to display the first display signal when the first processor receives the first safety signal, and the first processor can simultaneously receive the second enable signal and the third enable signal to display the second display signal , the first processor displays the third display signal when the first processor receives the prohibition signal, and the anti-vortex-excitation processor receives the first anti-vortex-excitation signal and displays the fourth display signal;
  • the second signal display device is configured to display the first display signal when the second processor receives the second safety signal, and the second processor can simultaneously receive the first enable signal and the third enable signal to display the second display signal , the second processor displays the third display signal when the second processor receives the prohibition signal, and the anti-vortex-excitation processor receives the second anti-vortex-excitation signal and displays the fourth display signal;
  • the third signal display device is configured to display the first display signal when the third processor receives the third safety signal, and the third processor can simultaneously receive the first enable signal and the second enable signal to display the second display signal , the third processor displays the third display signal when the third processor receives the prohibition signal, and the anti-vortex-excitation processor receives the third anti-vortex-excitation signal and displays the fourth display signal.
  • the operation panel further includes a first gear, a second gear, a third gear, a hoisting button and a power-on button, wherein:
  • the hoisting button is locked under normal circumstances
  • the hoisting button is unlocked so that it can be pressed
  • the pendant button is unlocked so that it can be pressed
  • the pendant button is unlocked so that it can be pressed.
  • the power-on button is locked under normal circumstances
  • the power-on button is unlocked so that it can be pressed
  • the power-on button is unlocked so that it can be pressed
  • the power-on button is unlocked so that it can be pressed.
  • the operation panel further includes an anti-vortex excitation button, wherein:
  • the anti-vortex button is locked under normal conditions
  • the anti-vortex excitation processor receives the first power-on end signal, the second power-on end signal and the third power-on end signal at the same time, the anti-vortex excitation button is unlocked so that it can be pressed;
  • an anti-vortex excitation operation signal is generated, and the anti-vortex excitation controller performs an anti-vortex excitation position operation on the first blade, the second blade and the third blade simultaneously according to the anti-vortex excitation operation signal.
  • the present invention also provides an operation method of the pitch pitch installation and debugging system, comprising:
  • Each position sensor detects the position of its corresponding blade
  • Each position sensor sends the position detection result of its corresponding blade to the sub-controller corresponding to the blade;
  • Each sub-controller in the plurality of sub-controllers judges whether the blade is in the operation enabling position according to the detection result of the position of the corresponding blade;
  • the master controller operates the blades according to the enable signal.
  • the operation method of the pitch pitch installation and debugging system it also includes:
  • One blade is hoisted.
  • the position detection result is obtained through the position sensor to ensure that the pitch angle of the other two blades is in a safe position;
  • the power-on operation is performed on the blade.
  • the position detection result is obtained through the position sensor to ensure that the pitch angle of the other two blades is in a safe position.
  • the operation method of the pitch pitch installation and debugging system it also includes:
  • the pitch angles of the three blades are simultaneously adjusted to the anti-vortex-induced position through the main controller, and the position detection results are obtained through the position sensor to ensure that the pitch angles of the three blades are in the anti-vortex-induced position;
  • each propeller is detected by each position sensor, and each sub-controller judges whether each propeller is in the operation enabling position, and if a certain propeller is in the operating enabling position can position, the main controller operates the blade according to the enabling signal, the present invention realizes the manual judgment in the prior art to operate the blade, and converts it into a complete set of intelligent judgment of sensor, sub-controller and main controller system, more secure and reliable.
  • the invention transforms the disordered, parallel and non-fool-proof state of wind wheel grouping and static adjustment in the industry into a serial, orderly and controllable safe state through the anti-mistake lock.
  • FIG. 1 is a schematic diagram of a pitch pitch installation and debugging system according to an embodiment of the present invention
  • FIG. 2 is a schematic diagram of an operation panel of a pitch pitch installation and debugging system according to an embodiment of the present invention
  • 100 the overall controller; 201 - the first sub-controller; 202 - the second sub-controller; 203 - the third sub-controller; 301 - the first position sensor; 302 - the second position sensor; 303 - third position sensor; 304 - fourth position sensor; 305 - fifth position sensor; 306 - sixth position sensor.
  • the quantifiers "a” and “an” do not exclude the scenario of multiple elements.
  • the core idea of the present invention is to provide a pitch pitch installation and debugging system and an operation method thereof, so as to solve the problem that the installation and debugging of the existing pitch pitch system is greatly affected by human factors.
  • the present invention provides a pitch pitch installation and debugging system and an operation method thereof, comprising: a plurality of position sensors, wherein each position sensor is configured to be installed at the connection between the pitch pitch system and a blade, so as to Detecting the position of the blade, and sending the detection result of the position of the blade to the sub-controller corresponding to the blade; a plurality of sub-controllers, wherein each sub-controller is configured to detect according to the position of the corresponding blade As a result, it is determined whether the blade is in the operation enabling position, and if the blade is in the operation enabling position, an enabling signal is sent to the general controller; the general controller is configured to operate the blade according to the enabling signal .
  • An embodiment of the present invention provides a pitch installation and debugging system, as shown in FIG. 1 , comprising: a plurality of position sensors (301-306), wherein each position sensor is configured to be installed between the pitch system and one blade connection to detect the position of the blade, and send the detection result of the position of the blade to the sub-controllers corresponding to the blade (201-203); a plurality of sub-controllers, wherein each sub-controller is configured according to The position detection result of the corresponding blade determines whether the blade is in the operation enabling position, and if the blade is in the operation enabling position, an enabling signal is sent to the general controller 100; the general controller 100 is Configured to operate the blades based on the enable signal.
  • any non-streamlined object under a certain constant flow rate, will alternately generate vortices detaching from the surface of the structure on both sides of the object, and the vortices constitute the vortex-induced vibration effect.
  • each tower section will produce a relatively strong vortex-induced vibration effect, which will cause the tower section to be displaced or even fall off, and will be installed in the tower.
  • the simulation shows that the life consumed by vortex-induced vibration of a 140m tower in 1 minute is equivalent to the life consumed by normal operation for 4 days, that is, the fatigue failure will occur after accumulating vortex-induced vibration for about 30 hours!
  • the position sensor in the pitch installation and debugging system, includes: a first position sensor 301, which is configured to be installed at the connection between the pitch system and the first blade, so as to Detect whether the pitch angle of the first blade is in a safe position, and if the pitch angle of the first blade is in a safe position, send a safe position signal to the first sub-controller 201;
  • the second position sensor 302 is configured It is installed at the connection between the pitch system and the second blade to detect whether the pitch angle of the second blade is in a safe position, and if the pitch angle of the second blade is in a safe position, send the The controller 202 sends a safe position signal;
  • the third position sensor 303 is configured to be installed at the connection between the pitch system and the third blade to detect whether the pitch angle of the third blade is in a safe position, and if the third Whether the pitch angle of the blade is in a safe position, a safe position signal is sent to the third sub-controller 203 .
  • Three sensors detect whether the three
  • the position sensor includes: after the first sub-controller 201 receives the safe position signal of the first position sensor 301, it sends the signal to the main controller 100 Send the first safety signal; the second sub-controller 202 sends the second safety signal to the master controller 100 after receiving the safety position signal of the second position sensor 302 ; the third sub-controller 203 receives the safety signal of the third position sensor 303 After the safety position signal, a third safety signal is sent to the master controller 100 .
  • the three sub-controllers correspond to the detection of the three blades respectively, which can well distinguish the different states of the three blades, and transmit the safe position signal separately for the functions that the three blades cannot operate at the same time.
  • the overall controller 100 includes a first processor, a second processor and a third processor, wherein: if the first processor receives When the first security signal is reached, the first enable signal is generated, and the first enable signal is sent to the second processor and the third processor respectively; if the second processor receives the second security signal, the second enable signal is generated. and send the second enable signal to the first processor and the third processor respectively; if the third processor receives the third security signal, it will generate a third enable signal and send it to the first processor and the third processor respectively.
  • the second processor sends a third enable signal. That is, when a blade is operated, to ensure that the other two blades are in a safe position, it is necessary to send an enable signal to the other two processors.
  • the overall controller 100 includes a first controller, a second controller and a third controller, wherein: if the first processor can If the second enable signal and the third enable signal are received at the same time, the first controller can perform hoisting and power-on operations on the first blade; otherwise, it is prohibited to perform the hoisting and power-on operations on the first blade; If the second processor can receive the first enable signal and the third enable signal at the same time, the second controller can perform the hoisting operation and power-on operation on the second blade, otherwise the hoisting operation and the power-on operation on the second blade are prohibited.
  • the first controller when the first controller performs a hoisting operation and a power-on operation on the first blade, it sends a message to the second processor and the third processor. Operation prohibition signal; when the second controller performs hoisting operation and power-on operation on the second blade, it sends a prohibition signal to the first processor and the third processor; when the third controller hoists the third blade During operation and power-up operations, an operation inhibit signal is sent to the first processor and the second processor.
  • the first controller prohibits the hoisting operation and power-on operation of the first blade
  • the operation prohibition signal is received
  • the second controller prohibits the hoisting operation and power-on operation of the second blade
  • the third processor receives the prohibition signal
  • the third controller prohibits the hoisting operation and power-on operation of the third blade. Power-on operation; the priority of the prohibit operation signal is higher than that of the first enable signal, the second enable signal and the third enable signal.
  • the first controller hoists the first blade, it sends a hoisting end signal to the first processor, and the first processor receives the After the hoisting end signal, the first controller can power on the first blade; after the second controller has hoisted the second blade, it sends a hoisting end signal to the second processor, and the second processor receives it After the hoisting end signal is reached, the second controller can power on the second blade; after the third controller has hoisted the third blade, it sends a hoisting end signal to the third processor, and the third processor After receiving the hoisting end signal, the third controller can power on the third blade.
  • the power-on operation can only be performed after the hoisting operation of one blade is completed.
  • it is necessary to ensure that the other two blades are in a safe position that is, when the first processor receives the hoisting end signal, it also needs to continue to receive After the second enable signal and the third enable signal are reached, and no operation prohibition signal is received, the first blade can be powered on only when the above conditions are satisfied.
  • the power-on operation is also exclusive. When one blade is in progress, the other two blades must remain in their original safe positions.
  • the overall controller 100 further includes an anti-vortex excitation processor and an anti-vortex excitation controller, wherein: the first controller controls the first propeller After the blade is powered on, it sends a first power-on end signal to the anti-vortex excitation processor; after the second controller powers up the second blade, it sends a second power-on end signal to the anti-vortex excitation processor; After the third controller powers on the third blade, it sends a third power-on end signal to the anti-vortex excitation processor; if the anti-vortex excitation processor receives the first power-on end signal and the second power-on end signal at the same time signal and the third power-on end signal, the anti-vortex excitation controller can simultaneously perform the anti-vortex excitation position operation on the first blade, the second blade and the third blade at the same time. After the hoisting operation and power-on operation of the three blades are all completed, the anti-vortex excitation operation can be entered with one
  • the hoisting operation includes: hoisting the first propeller, the second propeller or the third propeller until the position is compatible with the pitch system Docking, and then connect the first propeller, the second propeller or the third propeller with the pitch system;
  • the power-on operation includes: powering on the pitch system, and then driving the pitch system to drive the first propeller , the second paddle or the third paddle rotates, and the pitch angle of the first paddle, the second paddle or the third paddle is adjusted;
  • the anti-vortex-induced position operation includes: driving the pitch system to drive the first paddle , the second blade and the third blade are rotated to adjust the pitch angles of the first blade, the second blade and the third blade to the anti-vortex excitation position.
  • the position sensor in the pitch installation and debugging system, includes: a fourth position sensor 304 configured to be installed at the connection between the pitch system and the first blade, to Detect whether the pitch angle of the first blade is in the anti-vortex excitation position, and if the pitch angle of the first blade is in the anti-vortex excitation position, send the anti-vortex excitation position signal to the first sub-controller 201; fifth The position sensor 305 is configured to be installed at the connection between the pitch system and the second blade to detect whether the pitch angle of the second blade is in the anti-vortex-induced position, and if the pitch angle of the second blade is in the If the anti-vortex excitation position is detected, the anti-vortex excitation position signal is sent to the second sub-controller 202; the sixth position sensor 306 is configured to be installed at the connection between the pitch system and the third blade to detect the position of the third blade.
  • the anti-vortex-induced position signal is sent to the third sub-controller 203 .
  • the above sensors are all detecting whether the pitch angle of the three blades is adjusted to the anti-vortex-induced position to ensure that the adjustment is in place.
  • the first sub-controller 201 after receiving the anti-vortex excitation position signal of the fourth position sensor 304, the first sub-controller 201 sends the first sub-controller 201 to the anti-vortex excitation processor anti-vortex excitation signal; the second sub-controller 202 sends the second anti-vortex-excitation signal to the anti-vortex-excitation processor after receiving the anti-vortex-induced position signal of the fifth position sensor 305; After the anti-vortex-induced position signal of the position sensor 306 is obtained, a third anti-vortex-induced signal is sent to the anti-vortex-induced processor.
  • the anti-vortex excitation processor In the pitch pitch installation and debugging system, if the anti-vortex excitation processor can receive the first anti-vortex excitation signal, the second anti-vortex excitation signal and the third anti-vortex excitation signal at the same time, the anti-vortex excitation processor generates the installation Debug end signal. At this point, the entire installation and commissioning work is over, and the operator can receive the signal at a glance. The entire installation and commissioning process is interlinked. Due to the mutual exclusion of the prohibition signals between the three blades, and the unidirectional sequence of signals such as the hoisting end signal and the power-on end signal, parallel operations cannot be performed, making the process more orderly and reliable. , with the function of foolproof, avoiding the risk of manual misoperation.
  • the pitch pitch installation and debugging system further includes an operation panel, wherein the operation panel includes: a first signal display device 401, which is The first processor is configured to display the first display signal when the first processor receives the first security signal, the first processor can simultaneously receive the second enable signal and the third enable signal to display the second display signal, and the first processor receives the second display signal.
  • the operation panel includes: a first signal display device 401, which is The first processor is configured to display the first display signal when the first processor receives the first security signal, the first processor can simultaneously receive the second enable signal and the third enable signal to display the second display signal, and the first processor receives the second display signal.
  • the second signal display device 401 is configured so that when the second processor receives the second safety signal Display the first display signal, the second processor can simultaneously receive the first enable signal and the third enable signal to display the second display signal, the second processor displays the third display signal when the second processor receives the prohibition signal, anti-vortex excitation
  • the processor receives the second anti-vortex signal and displays the fourth display signal
  • the third signal display device 401 is configured to display the first display signal when the third processor receives the third safety signal, and the third processor can simultaneously receive When the first enable signal and the second enable signal display the second display signal, the third processor displays the third display signal when the operation prohibition signal is received, and the anti-vortex-excitation processor receives the third anti-vortex-excitation signal and displays the fourth display signal.
  • Display signal For example, if three LED lights are set, the first display signal is blue, the second display signal is yellow, the third display signal is red, the fourth display signal is green, and so on. It makes the operator know at a glance whether the operation can be performed and how to operate in the next step.
  • the operation panel further includes a first gear 501, a second gear 501, a third gear 501, a hoisting button and a power-on button, wherein : If the pointer is in the first gear, press the hoisting button or the power-on button to hoist or power on the first blade; if the pointer is in the second gear, press the hoisting button or the power-on button When the hoisting operation or power-on operation is performed on the second blade; if the pointer is in the third gear, when the hoisting button or the power-on button is pressed, the hoisting operation or power-on operation on the third blade is performed.
  • the hoisting button in the pitch pitch installation and debugging system, is locked under normal conditions; if the pointer is in the first gear and the first processor simultaneously receives the second enable signal and With the third enable signal, the hoisting button is unlocked so that it can be pressed; if the pointer is in the second gear and the second processor receives the first and third enable signals simultaneously, the hoisting button is unlocked so that it can be pressed; if the pointer is in the third gear and the third processor receives both the first enable signal and the second enable signal, the pendant button is unlocked so that it can be pressed Down.
  • the power-on button in the pitch pitch installation and debugging system, is locked under normal circumstances; if the pointer is in the first gear and the first processor simultaneously receives the second enable signal and the third enable signal, the power-on button is unlocked so that it can be pressed; if the pointer is in the second gear and the second processor receives the first enable signal and the third enable signal at the same time, then The power-on button is unlocked so that it can be pressed; if the pointer is in the third gear and the third processor receives the first enable signal and the second enable signal at the same time, the power-on button is unlocked so that the It can be pressed.
  • the operation panel further includes an anti-vortex excitation button, wherein: the anti-vortex excitation button is locked under normal conditions; if the anti-vortex excitation processor receives the When the first power-on end signal, the second power-on end signal, and the third power-on end signal are reached, the anti-vortex excitation button is unlocked so that it can be pressed; after the anti-vortex excitation button is pressed, an anti-vortex excitation button is generated.
  • the operation signal, the anti-vortex excitation controller simultaneously performs the anti-vortex excitation position operation on the first blade, the second blade and the third blade according to the anti-vortex operation signal.
  • the present invention also provides an operation method for the pitch installation and debugging system, comprising: installing each position sensor in the plurality of position sensors at the connection between the pitch system and one blade; each position sensor detects its corresponding The position of the blade, and each position sensor sends the detection result of the position of the corresponding blade to the sub-controller corresponding to the blade; each sub-controller in the plurality of sub-controllers Based on the position detection result, it is determined whether the blade is in the operation enabling position; if the blade is in the operation enabling position, an enabling signal is sent to the general controller 100; the general controller 100 operates the blade according to the enabling signal.
  • the method further includes: adjusting the pitch angle corresponding to at least two of the three blades to the Safe position; hoist one blade.
  • the position detection result is obtained through the position sensor to ensure that the pitch angles of the other two blades are in a safe position; after the hoisting operation of one blade is completed, the The blades are powered on.
  • the position detection results are obtained through the position sensor to ensure that the pitch angles of the other two blades are in a safe position.
  • the operation method of the pitch pitch installation and debugging system further includes: sequentially completing the hoisting operation and the power-on operation of the three propeller blades, when one of the propeller blades performs the hoisting operation or the power-on operation During electrical operation, the other two blades are prohibited from any operation; the pitch angle of the three blades is adjusted to the anti-vortex-induced position at the same time through the master controller 100, and the position detection results are obtained through the position sensor to ensure the pitch angle of the three blades. The pitch angles are all in the anti-vortex position; the three blades are de-energized.
  • each propeller In the pitch pitch installation and debugging system and its operation method provided by the present invention, the position of each propeller is detected by each position sensor, and each sub-controller judges whether each propeller is in the operation enabling position, and if a certain propeller is in the operating enabling position can position, then the master controller 100 operates the blade according to the enable signal, the present invention realizes the operation of the blade by manual judgment in the prior art, and converts it into a complete set of sensor, sub-controller and master controller 100 Intelligent judgment system, more secure and reliable.
  • the invention transforms the disordered, parallel and non-fool-proof state of wind wheel grouping and static adjustment in the industry into a serial, orderly and controllable safe state through the anti-mistake lock.
  • the connection relationship between the sub-controller and the pitch system includes: three sets of batteries and shaft control boxes (accommodating the sub-controller), and the servo motor and the reducer are placed at the hub, and each A set of propellers, a main electrical switch box is placed at the connection between the hub and the nacelle, and the communication bus and cables of the entire system are connected to the main controller of the nacelle by slip rings.
  • the master controller communicates with the axle control box in the hub through the field bus, so as to achieve the purpose of controlling three independent pitch devices.
  • the electric pitch system adopts three blades with independent electric drive pitch system, and the mechanical part includes slewing bearing, reducer and transmission.
  • the reducer is fixed on the hub, the inner ring of the slewing bearing is mounted on the blade, and the outer ring of the blade bearing is fixed on the hub.
  • the servo motor drives the output shaft pinion of the reducer to rotate, and the pinion meshes with the inner ring of the slewing bearing, thereby driving the inner ring of the slewing bearing and the blades to rotate together, realizing the change of pitch.
  • the purpose of the distance angle is arranged in the hub, the inner ring of the slewing bearing is mounted on the blade, and the outer ring of the blade bearing is fixed on the hub.
  • the master controller After the whole commissioning process is completed, the master controller sends the command value to the electric pitch system according to the wind speed, generator power and rotation speed, etc., and the electric pitch system feeds back the actual value and operating condition to the master controller.
  • the electric pitch system must meet the requirements of being able to quickly respond to the command of the master controller, having an independent working pitch system, a high-performance synchronizing mechanism, and being safe and reliable.
  • the pitch control system changes the angle of the blades within a certain range (0 to 90 degrees) in order to adjust the output power and avoid the possibility of low power generation in summer and excessive power generation in winter after the fixed-pitch unit determines the angle of attack. question. In the low wind speed section, the power is optimized, and the wind energy can be better converted into electric energy.
  • the operation method of the pitch pitch installation and debugging system of the present invention can also be used to provide manual pitch pitch and other safety maintenance and inspection functions when the wind turbine is in a maintenance state.
  • the backup power supply provides the working voltage of the electrical system, which mainly completes the feathering function.
  • the pitch adjustment mode of the shaft cabinet should be divided into two modes: automatic/manual.
  • the automatic/manual mode setting is realized by a two-position switch, and the forward and reverse adjustment and stop setting of the manual mode are realized by a three-position switch.
  • each blade can be pitched independently, but only one shaft cabinet can be controlled by the corresponding switch to make the pitch motor rotate in the forward and reverse directions. Adjust the pitch angle; the pitch angles of the other two blades must be at 90°, otherwise the manual pitching function will fail.
  • a control switch should be set on the shaft cabinet. When the fan is in maintenance state and personnel need to enter the hub to maintain and repair the pitch system, the control switch should be disconnected, the pitch motor brakes, and the control power supply of the inverter is cut off. , to ensure that the pitch angle stays at a fixed position, and the pitch angle can not be changed until the control switch is closed again. Otherwise, the control switch should always be closed. Compare the pitch angle signals collected by the two ENCODERs configured for each blade.
  • the PLC When the angle deviation is less than 2°, the PLC is allowed to adjust the pitch angle of the blade when needed; otherwise, as long as the blade is If the pitch angle is less than 90, it will be feathered in the direction of 90° at a speed of 7 degrees per second, and the feathering of the remaining blades is controlled by software. All blades are installed with a limit switch at the 91° position, and no limit switch is installed in the 0° direction. Whether the current pitch angle of the blade is less than 0° is determined by the conversion of the measurement results of the two ENCODER sensors. The pitch adjustment mode of the shaft cabinet is in the automatic position.
  • the hardware system of the faulty shaft cabinet shall ensure that the corresponding propellers are feathered in the direction of 90° at a speed of 7° per second, and the unaffected shaft cabinet , the blade feathering is done by software control.
  • the communication bus between the DP slave station and the PLC master station in any axis cabinet is faulty, the fan safety composed of impeller overspeed, vibration switch, TOPBOX emergency stop button, converter cabinet emergency stop button, and yaw limit switch in series
  • the chain and the two impeller lock signals in series with the safety chain are disconnected (24VDC signal), no matter if any one ENCODER fails, or the deviation of the measurement results of the two ENCODERs of the same blade exceeds the specified threshold; any blade pitch angle Less than -2° in the pitch process; the hardware system in the safety chain and release loop is faulty; for the three-phase AC asynchronous pitch motor, the inverter control circuit should provide open-loop frequency control U/F, closed-loop space There are two speed regulation modes of vector control.
  • the default setting is closed-loop space vector control.
  • the inverter control circuit should immediately switch the speed regulation mode to the open-loop frequency control U/F mode, and make the corresponding blades in the U/F mode.
  • the speed of 7 degrees per second is feathered in the direction of 90°, and the remaining blades are controlled by the software; during the pitching process of the fan, the three pitch motors should be started in sequence to prevent the three pitch motors from starting at the same time. , causing the slip ring to be overloaded; the start and stop of all cooling fans in the shaft cabinet should be controlled by software; whether the grid voltage is powered down, the direct judgment method should be selected first, and the judgment method based on the backup power supply voltage should be selected secondly.
  • the axis cabinet should provide a control interface to facilitate the performance test of the backup power supply, mainly referring to the performance test in the case of a power failure of the grid voltage; the axis cabinet should provide a control interface to facilitate the switching of the speed regulation mode of the inverter in the axis cabinet.
  • the position sensor can be a rotary encoder.
  • the incremental rotary encoder converts the timing and phase relationship of its angle code disk through two internal photosensitive receiver tubes, and obtains the increase (positive direction) or decrease (negative direction) of its angle code disk angular displacement. ), after joining digital circuits, especially single-chip microcomputers, incremental rotary encoders are cheaper and more advantageous than absolute rotary encoders in angle measurement and angular velocity measurement.
  • the two encoders configured for each blade should ensure that the measurement accuracy of the blade pitch angle reaches 0.01°, and there should be corresponding modules in the shaft cabinet to display the current pitch angle of the blade, so as to ensure that the pitch angle in the manual pitch mode is guaranteed.
  • the pitch angle will not exceed the position of the 91° limit switch, and the pitch adjustment mode of the shaft cabinet is in the automatic mode. If the pitch angle of the fan exceeds the position of the 91° limit switch during the feathering process, the fan can be switched Switch to the maintenance state, and adjust the pitch angle back to the 90° position through the pitch method in the shaft cabinet.
  • the pitch angle adjustment mode of the shaft cabinet is in the automatic mode. Measures to prevent the pitch angle from exceeding the limit switch, the 91° limit When the limit switch is reached, the pitch motor brakes and the release signal and pitch speed command of the axle cabinet inverter are invalid, which will also make the pitch motor stationary.
  • the above embodiments have described in detail the different configurations of the pitch pitch installation and debugging system and its operation method.
  • the present invention includes but is not limited to the configurations listed in the above embodiments, any configuration provided in the above embodiments.
  • the content that is transformed on the basis of the configuration belongs to the protection scope of the present invention. Those skilled in the art can draw inferences from the contents of the foregoing embodiments.

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Debugging And Monitoring (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

一种变桨安装调试系统，包括：多个位置传感器（301-306），其中每个位置传感器（301-306）被配置为安装在变桨系统与一个桨叶的连接处，以检测该桨叶的位置，以及将该桨叶的位置检测结果发送至该桨叶对应的子控制器（201-203）；多个子控制器（201-203），其中每个子控制器（201-203）被配置为根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操作使能位置，以及若该桨叶处于操作使能位置，则向总控制器（100）发送使能信号；总控制器（100），被配置为根据使能信号对桨叶进行操作。该结构解决了现有技术中变桨系统的安装调试受到人为因素影响较大的问题。另外，还涉及上述变桨调试系统的操作方法。

Description

变桨安装调试系统及其操作方法 技术领域
本发明涉及风力发电机技术领域，特别涉及一种变桨安装调试系统及其操作方法。
背景技术
风能是一种清洁而安全的能源,在自然界中可以不断生成并有规律得到补充,所以风能资源的特点十分明显,其开发利用的潜力巨大。变速恒频技术于20世纪90年代开始兴起。变速恒频风力发电机组风轮转速随着风速的变化而变化，可以更有效地利用风能，并且通过变速恒频技术可得到恒定频率的电能。但变速恒频风力机组仅通过电机自身调节要达到减小风速波动冲击的目的是很困难的，因为自然界中风速瞬息万变，特别是在额定风速以上工况，风力机有可能受到很大的静态或动态冲击。但是变桨风机不会产生此类情况，变桨距是指大型风力发电机安装在轮毂上的桨叶借助控制技术和动力系统改变节距角的大小从而改变桨叶气动特性，使桨叶和整机的受力状况大为改善。近年来，电动变桨距系统越来越多的应用到风力发电机组当中，直驱型风力发电机组为变桨距调节型风机，桨叶在运行期间，它会在风速变化的时候绕其径向轴转动。因此，在整个风速范围内可能具有几乎最佳的节距角和较低的切入风速，在高风速下，改变节距角以减少功角，从而减小了在桨叶上的气动力。这样就保证了叶轮输出功率不超过发电机的额定功率。
变桨距机构就是在风速大于额定风速时，依据风速的变化随时调节节距角,控制吸收的机械能，一方面保证获取最大的能量(与额定功率对应)，同时减少风力对风力机的冲击。在并网过程中，变桨距控制还可实现快速无冲击并网。变桨距控制系统与变速恒频技术相配合，最终提高了整个风力发电系统的发电效率和电能质量。
电动变桨距系统就是三个桨叶分别装有独立的电动变桨距系统，主要包括回转支撑，减速机装置和伺服电动机及其驱动器等。它提供给风力发电机组功率输出和足够的刹车制动能力，这样可以避免过载对风机的破坏。
风力发电机组安装调试的任务是将机组的各系统有机的结合在一起，协调一致，保证机组安全、长期、稳定、高效率的运行。风力发电机组变桨系统安装调试包括现场桨叶(叶片)的吊装，以及在发电设备的输电线路和电网断开的状态下，利用临时电源或备用电源，按设计和设备技术文件规定对设备进行调整、整定和一系列试验工作的过程。风电场安装调试应坚持安全第一、预防为主方针，风电场建设单位应对调试单位的调试方案、安全措施、组织措施等进行严格审查，并指定调试安全负责人负责调试工作的协调、管理和监督。变桨系统的安装调试必须遵守各系统的安全要求，特别是关于整机的安全要求，否则会有人身安全危险及风机的安全风险。安装调试者必须对风机的各系统的功能有相当的了解，必须由通过培训合格的人员进行，尤其是现场安装调试。这就使得变桨系统的安装调试依赖于对人员的培训和人员的熟练程度，人为因素较大会导致不能排除安全事故的风险，若安装调试人员业务不熟练、应急反应能力不足或受到外界因素干扰导致失误操作，会导致极大的生命财产损失。
发明内容
本发明的目的在于提供一种变桨安装调试系统及其操作方法，以解决现有的变桨系统的安装调试受到人为因素影响较大的问题。
为解决上述技术问题，本发明提供一种变桨安装调试系统，包括：
多个位置传感器，其中每个位置传感器被配置为能够安装在变桨系统与桨叶的连接处以检测该桨叶的位置；
多个子控制器，其中每个子控制器被配置为执行下列动作：
根据该子控制器所对应的桨叶的位置，确定该桨叶是否处于操作使能位置；以及
若该桨叶处于操作使能位置，则向总控制器发送使能信号；
总控制器，被配置为根据使能信号对桨叶进行操作。
可选的，在所述的变桨安装调试系统中，所述位置传感器包括：
第一位置传感器，被配置为能够安装在变桨系统与第一桨叶的连接处，其中第一位置传感器被配置为检测第一桨叶的节距角是否处于安全位置，并且若第一桨叶的节距角处于安全位置，则向第一子控制器发送安全位置信号；
第二位置传感器，被配置为能够安装在变桨系统与第二桨叶的连接处，其中第二位置传感器被配置为检测第二桨叶的节距角是否处于安全位置，并且若第二桨叶的节距角是否处于安全位置，则向第二子控制器发送安全位置信号；
第三位置传感器，被配置为能够安装在变桨系统与第三桨叶的连接处，其中第二位置传感器被配置为检测第三桨叶的节距角是否处于安全位置，并且若第三桨叶的节距角是否处于安全位置，则向第三子控制器发送安全位置信号。
可选的，在所述的变桨安装调试系统中，
第一子控制器接收到第一位置传感器的安全位置信号后，向总控制器发送第一安全信号；
第二子控制器接收到第二位置传感器的安全位置信号后，向总控制器发送第二安全信号；
第三子控制器接收到第三位置传感器的安全位置信号后，向总控制器发送第三安全信号。
可选的，在所述的变桨安装调试系统中，所述总控制器包括第一处理器、第二处理器及第三处理器，其中：
若第一处理器接收到第一安全信号，则产生第一使能信号，并分别向第二处理器及第三处理器发送第一使能信号；
若第二处理器接收到第二安全信号，则产生第二使能信号，并分别向第一处理器及第三处理器发送第二使能信号；
若第三处理器接收到第三安全信号，则产生第三使能信号，并分别向第一处理器及第二处理器发送第三使能信号。
可选的，在所述的变桨安装调试系统中，所述总控制器包括第一控制器、第二控制器及第三控制器，其中：
若第一处理器能够同时接收到第二使能信号和第三使能信号，则第一控制器能够对第一桨叶进行吊装操作和上电操作，否则禁止对第一桨叶进行吊装操作和上电操作；
若第二处理器能够同时接收到第一使能信号和第三使能信号，则第二控制器能够对第二桨叶进行吊装操作和上电操作，否则禁止对第二桨叶进行吊装操作和上电操作；
若第三处理器能够同时接收到第一使能信号和第二使能信号，则第三控制器能够对第三桨叶进行吊装操作和上电操作，否则禁止对第三桨叶进行吊装操作和上电操作。
可选的，在所述的变桨安装调试系统中，
当第一控制器对第一桨叶进行吊装操作和上电操作时，向第二处理器和第三处理器发送禁止操作信号；
当第二控制器对第二桨叶进行吊装操作和上电操作时，向第一处理器和第三处理器发送禁止操作信号；
当第三控制器对第三桨叶进行吊装操作和上电操作时，向第一处理器和第二处理器发送禁止操作信号。
可选的，在所述的变桨安装调试系统中，
所述第一处理器接收到禁止操作信号时，第一控制器禁止对第一桨叶进行吊装操作和上电操作；
所述第二处理器接收到禁止操作信号时，第二控制器禁止对第二桨叶进行吊装操作和上电操作；
所述第三处理器接收到禁止操作信号时，第三控制器禁止对第三桨叶进行吊装操作和上电操作；
禁止操作信号的优先级高于第一使能信号、第二使能信号和第三使能信号。
可选的，在所述的变桨安装调试系统中，
第一控制器对第一桨叶进行吊装操作后，向第一处理器发送吊装结束 信号，第一处理器接收到吊装结束信号后，则第一控制器能够对第一桨叶进行上电操作；
第二控制器对第二桨叶进行吊装操作后，向第二处理器发送吊装结束信号，第二处理器接收到吊装结束信号后，则第二控制器能够对第二桨叶进行上电操作；
第三控制器对第三桨叶进行吊装操作后，向第三处理器发送吊装结束信号，第三处理器接收到吊装结束信号后，则第三控制器能够对第三桨叶进行上电操作。
可选的，在所述的变桨安装调试系统中，所述总控制器还包括抗涡激处理器和抗涡激控制器，其中：
第一控制器对第一桨叶进行上电操作后，向抗涡激处理器发送第一上电结束信号；
第二控制器对第二桨叶进行上电操作后，向抗涡激处理器发送第二上电结束信号；
第三控制器对第三桨叶进行上电操作后，向抗涡激处理器发送第三上电结束信号；
若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则抗涡激控制器能够同时对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。
可选的，在所述的变桨安装调试系统中，所述吊装操作包括：将第一桨叶、第二桨叶或第三桨叶吊起直至位置能够与变桨系统对接，然后将第一桨叶、第二桨叶或第三桨叶与变桨系统进行连接；
所述上电操作包括：将变桨系统进行上电，然后驱动变桨系统带动第一桨叶、第二桨叶或第三桨叶转动，调节第一桨叶、第二桨叶或第三桨叶的节距角；
所述抗涡激位置操作包括：驱动变桨系统带动第一桨叶、第二桨叶和第三桨叶转动，以将第一桨叶、第二桨叶和第三桨叶的节距角均调节至抗涡激位置。
可选的，在所述的变桨安装调试系统中，所述位置传感器包括：
第四位置传感器，被配置为安装在变桨系统与第一桨叶的连接处，以检测第一桨叶的节距角是否处于抗涡激位置，以及
若第一桨叶的节距角是否处于抗涡激位置，则向第一子控制器发送抗涡激位置信号；
第五位置传感器，被配置为安装在变桨系统与第二桨叶的连接处，以检测第二桨叶的节距角是否处于抗涡激位置，以及
若第二桨叶的节距角是否处于抗涡激位置，则向第二子控制器发送抗涡激位置信号；
第六位置传感器，被配置为安装在变桨系统与第三桨叶的连接处，以检测第三桨叶的节距角是否处于抗涡激位置，以及
若第三桨叶的节距角是否处于抗涡激位置，则向第三子控制器发送抗涡激位置信号。
可选的，在所述的变桨安装调试系统中，
第一子控制器接收到第四位置传感器的抗涡激位置信号后，向抗涡激处理器发送第一抗涡激信号；
第二子控制器接收到第五位置传感器的抗涡激位置信号后，向抗涡激处理器发送第二抗涡激信号；
第三子控制器接收到第六位置传感器的抗涡激位置信号后，向抗涡激处理器发送第三抗涡激信号。
可选的，在所述的变桨安装调试系统中，若抗涡激处理器能够同时接收到第一抗涡激信号、第二抗涡激信号和第三抗涡激信号，则抗涡激处理器产生安装调试结束信号。
可选的，在所述的变桨安装调试系统中，还包括操作面板，其中操作面板包括：
第一信号显示装置，被配置为第一处理器接收到第一安全信号时显示第一显示信号，第一处理器能够同时接收到第二使能信号和第三使能信号显示第二显示信号，第一处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第一抗涡激信号显示第四显示信号；
第二信号显示装置，被配置为第二处理器接收到第二安全信号时显示 第一显示信号，第二处理器能够同时接收到第一使能信号和第三使能信号显示第二显示信号，第二处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第二抗涡激信号显示第四显示信号；
第三信号显示装置，被配置为第三处理器接收到第三安全信号时显示第一显示信号，第三处理器能够同时接收到第一使能信号和第二使能信号显示第二显示信号，第三处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第三抗涡激信号显示第四显示信号。
可选的，在所述的变桨安装调试系统中，操作面板还包括第一挡位、第二挡位、第三挡位、吊装按钮和上电按钮，其中：
若指针处于第一挡位，则按下吊装按钮或上电按钮时，对第一桨叶进行吊装操作或上电操作；
若指针处于第二挡位，则按下吊装按钮或上电按钮时，对第二桨叶进行吊装操作或上电操作；
若指针处于第三挡位，则按下吊装按钮或上电按钮时，对第三桨叶进行吊装操作或上电操作。
可选的，在所述的变桨安装调试系统中，吊装按钮在常规情况下被锁定；
若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；
若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；
若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则吊装按钮被解锁，以使其能够被按下。
可选的，在所述的变桨安装调试系统中，上电按钮在常规情况下被锁定；
若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；
若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；
若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则上电按钮被解锁，以使其能够被按下。
可选的，在所述的变桨安装调试系统中，操作面板还包括抗涡激按钮，其中：
抗涡激按钮在常规情况下被锁定；
若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则对抗涡激按钮进行解锁，以使其能够被按下；
抗涡激按钮被按下后生成抗涡激操作信号，抗涡激控制器根据抗涡激操作信号对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。
本发明还提供一种变桨安装调试系统的操作方法，包括：
将多个位置传感器中的每个位置传感器安装在变桨系统与一个桨叶的连接处；
每个位置传感器检测其所对应的桨叶的位置，以及
每个位置传感器将其所对应的桨叶的位置检测结果发送至该桨叶对应的子控制器；
多个子控制器中的每个子控制器根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操作使能位置；
若该桨叶处于操作使能位置，则向总控制器发送使能信号；
总控制器根据使能信号对桨叶进行操作。
可选的，在所述的变桨安装调试系统的操作方法中，还包括：
通过总控制器将三个桨叶中的至少两个桨叶对应的节距角调节至安全位置；
对一个桨叶进行吊装操作，在吊装过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置；
完成一个桨叶的吊装操作后，对该桨叶进行上电操作，在上电过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置。
可选的，在所述的变桨安装调试系统的操作方法中，还包括：
依次完成三个桨叶的吊装操作和上电操作，当其中一个桨叶进行吊装 操作或上电操作时，另外两个桨叶禁止任何操作；
通过总控制器将三个桨叶的节距角同时调节至抗涡激位置，通过位置传感器获取位置检测结果，保证三个桨叶的节距角均处于抗涡激位置；
对三个桨叶进行断电。
在本发明提供的变桨安装调试系统及其操作方法中，通过每个位置传感器检测各个桨叶的位置，每个子控制器判断各个桨叶是否处于操作使能位置，若某桨叶处于操作使能位置，则总控制器根据使能信号对该桨叶进行操作，本发明实现了将现有技术中由人工判断来操作桨叶，转换为传感器、子控制器和总控制器一整套智能判断系统，更加安全可靠。
本发明将行业内组风轮，静调工作的无序、可并行、无防呆等状态通过防误锁具转变为串行、有序、可控的安全状态。
附图说明
图1是本发明一实施例变桨安装调试系统示意图；
图2是本发明一实施例变桨安装调试系统的操作面板示意图；
图中所示：100-总控制器；201-第一子控制器；202-第二子控制器；203-第三子控制器；301-第一位置传感器；302-第二位置传感器；303-第三位置传感器；304-第四位置传感器；305-第五位置传感器；306-第六位置传感器。
具体实施方式
下面结合具体实施方式参考附图进一步阐述本发明。应当指出，各附图中的各组件可能为了图解说明而被夸大地示出，而不一定是比例正确的。在各附图中，给相同或功能相同的组件配备了相同的附图标记。
在本发明中，除非特别指出，“布置在…上”、“布置在…上方”以及“布置在…之上”并未排除二者之间存在中间物的情况。此外，
“布置在…上或上方”仅仅表示两个部件之间的相对位置关系，而在一定情况下、如在颠倒产品方向后，也可以转换为“布置在…下或下方”，反之亦然。
在本发明中，各实施例仅仅旨在说明本发明的方案，而不应被理解为限制性的。
在本发明中，除非特别指出，量词“一个”、“一”并未排除多个元素的场景。
在此还应当指出，在本发明的实施例中，为清楚、简单起见，可能示出了仅仅一部分部件或组件，但是本领域的普通技术人员能够理解，在本发明的教导下，可根据具体场景需要添加所需的部件或组件。另外，除非另行说明，本发明的不同实施例中的特征可以相互组合。例如，可以用第二实施例中的某特征替换第一实施例中相对应或功能相同或相似的特征，所得到的实施例同样落入本申请的公开范围或记载范围。
在此还应当指出，在本发明的范围内，“相同”、“相等”、“等于”等措辞并不意味着二者数值绝对相等，而是允许一定的合理误差，也就是说，所述措辞也涵盖了“基本上相同”、“基本上相等”、“基本上等于”。以此类推，在本发明中，表方向的术语“垂直于”、“平行于”等等同样涵盖了“基本上垂直于”、“基本上平行于”的含义。
另外，本发明的各方法的步骤的编号并未限定所述方法步骤的执行顺序。除非特别指出，各方法步骤可以以不同顺序执行。
以下结合附图和具体实施例对本发明提出的变桨安装调试系统及其操作方法作进一步详细说明。根据下面说明和权利要求书，本发明的优点和特征将更清楚。需说明的是，附图均采用非常简化的形式且均使用非精准的比例，仅用以方便、明晰地辅助说明本发明实施例的目的。
另外，除非另行说明，本发明的不同实施例中的特征可以相互组合。例如，可以用第二实施例中的某特征替换第一实施例中相对应或功能相同或相似的特征，所得到的实施例同样落入本申请的公开范围或记载范围。
本发明的核心思想在于提供一种变桨安装调试系统及其操作方法，以解决现有的变桨系统的安装调试受到人为因素影响较大的问题。
为实现上述思想，本发明提供了一种变桨安装调试系统及其操作方法，包括：多个位置传感器，其中每个位置传感器被配置为安装在变桨系统与一个桨叶的连接处，以检测该桨叶的位置，以及将该桨叶的位置检测结果发送至该桨叶对应的子控制器；多个子控制器，其中每个子控制器被配置为根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操作使能位 置，以及若该桨叶处于操作使能位置，则向总控制器发送使能信号；总控制器，被配置为根据使能信号对桨叶进行操作。
本发明的实施例提供一种变桨安装调试系统，如图1所示，包括：多个位置传感器(301～306)，其中每个位置传感器被配置为安装在变桨系统与一个桨叶的连接处，以检测该桨叶的位置，以及将该桨叶的位置检测结果发送至该桨叶对应的子控制器(201～203)；多个子控制器，其中每个子控制器被配置为根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操作使能位置，以及若该桨叶处于操作使能位置，则向总控制器100发送使能信号；总控制器100，被配置为根据使能信号对桨叶进行操作。
从流体的角度来分析，任何非流线型物体，在一定的恒定流速下，都会在物体两侧交替地产生脱离结构物表面的旋涡，所述的漩涡构成了涡激振动效应。在风机塔筒安装过程中，由于风机塔筒外壁呈光滑的柱状，因此各塔筒段均会产生较为强烈的涡激振动效应，使得塔筒段会产生位移、甚至脱落，会在塔筒安装过程中产生较为严重的危险隐患。模拟显示，某140m塔架1分钟涡激振动消耗的寿命相当于4天正常运行消耗的寿命，也就是累积涡激振动约30小时就会发生疲劳破坏！如果实际运行过程中风速达到临界风速范围内，就可能发生危险！在桨叶吊装至变桨系统上，以及连接变桨系统上电调试时，如果不保证桨叶的节距角，可能导致涡激效应，造成事故。尤其是正在吊装的桨叶还没有与变桨系统连接，无法保证节距角的调节，若此时另外两个桨叶也处于较危险的位置，则很容易造成涡激效应，现有的情况下，一般靠人工判断桨叶的节距角来避免事故的发生，但风机桨叶的整个安装调试过程很复杂，流程繁杂，不熟练或注意力不集中的人员很容易多个流程并行或无序，甚至忽视风险。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述位置传感器包括：第一位置传感器301，被配置为安装在变桨系统与第一桨叶的连接处，以检测第一桨叶的节距角是否处于安全位置，以及若第一桨叶的节距角是否处于安全位置，则向第一子控制器201发送安全位置信号；第二位置传感器302，被配置为安装在变桨系统与第二桨叶的连接处，以检测第二桨叶的节距角是否处于安全位置，以及若第二桨叶的节距角是否 处于安全位置，则向第二子控制器202发送安全位置信号；第三位置传感器303，被配置为安装在变桨系统与第三桨叶的连接处，以检测第三桨叶的节距角是否处于安全位置，以及若第三桨叶的节距角是否处于安全位置，则向第三子控制器203发送安全位置信号。三个传感器分别检测三个桨叶是否处于安全位置。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述位置传感器包括：第一子控制器201接收到第一位置传感器301的安全位置信号后，向总控制器100发送第一安全信号；第二子控制器202接收到第二位置传感器302的安全位置信号后，向总控制器100发送第二安全信号；第三子控制器203接收到第三位置传感器303的安全位置信号后，向总控制器100发送第三安全信号。三个子控制器分别对应三个桨叶的检测，可以很好的区分三个桨叶的不同状态，并针对三个桨叶不能同时操作的功能，分别进行安全位置信号的发送。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述总控制器100包括第一处理器、第二处理器及第三处理器，其中：若第一处理器接收到第一安全信号，则产生第一使能信号，并分别向第二处理器及第三处理器发送第一使能信号；若第二处理器接收到第二安全信号，则产生第二使能信号，并分别向第一处理器及第三处理器发送第二使能信号；若第三处理器接收到第三安全信号，则产生第三使能信号，并分别向第一处理器及第二处理器发送第三使能信号。即当对某个桨叶进行操作时，要确保其他两个桨叶处于安全位置，因此需要向其他两个处理器发送使能信号。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述总控制器100包括第一控制器、第二控制器及第三控制器，其中：若第一处理器能够同时接收到第二使能信号和第三使能信号，则第一控制器能够对第一桨叶进行吊装操作和上电操作，否则禁止对第一桨叶进行吊装操作和上电操作；若第二处理器能够同时接收到第一使能信号和第三使能信号，则第二控制器能够对第二桨叶进行吊装操作和上电操作，否则禁止对第二桨叶进行吊装操作和上电操作；若第三处理器能够同时接收到第一使能信号和第二使能信号，则第三控制器能够对第三桨叶进行吊装操作和上电操作， 否则禁止对第三桨叶进行吊装操作和上电操作。即当对某个桨叶进行操作时，要确保其他两个桨叶处于安全位置。
在本发明的一个实施例中，在所述的变桨安装调试系统中，当第一控制器对第一桨叶进行吊装操作和上电操作时，向第二处理器和第三处理器发送禁止操作信号；当第二控制器对第二桨叶进行吊装操作和上电操作时，向第一处理器和第三处理器发送禁止操作信号；当第三控制器对第三桨叶进行吊装操作和上电操作时，向第一处理器和第二处理器发送禁止操作信号。在所述的变桨安装调试系统中，所述第一处理器接收到禁止操作信号时，第一控制器禁止对第一桨叶进行吊装操作和上电操作；所述第二处理器接收到禁止操作信号时，第二控制器禁止对第二桨叶进行吊装操作和上电操作；所述第三处理器接收到禁止操作信号时，第三控制器禁止对第三桨叶进行吊装操作和上电操作；禁止操作信号的优先级高于第一使能信号、第二使能信号和第三使能信号。当对某个桨叶进行操作时，另外两个桨叶不能进行任何操作，否则可能会改变其位于安全位置的状态，导致涡激效应。
在本发明的一个实施例中，在所述的变桨安装调试系统中，第一控制器对第一桨叶进行吊装操作后，向第一处理器发送吊装结束信号，第一处理器接收到吊装结束信号后，则第一控制器能够对第一桨叶进行上电操作；第二控制器对第二桨叶进行吊装操作后，向第二处理器发送吊装结束信号，第二处理器接收到吊装结束信号后，则第二控制器能够对第二桨叶进行上电操作；第三控制器对第三桨叶进行吊装操作后，向第三处理器发送吊装结束信号，第三处理器接收到吊装结束信号后，则第三控制器能够对第三桨叶进行上电操作。即对一个桨叶进行的吊装操作完成后，才能进行上电操作，这里还是要确保另外两个桨叶都位于安全位置，即第一处理器接收到吊装结束信号的同时，还需要持续的接收到第二使能信号和第三使能信号，且没有接收到禁止操作信号，上述条件满足才能对第一桨叶进行上电操作。上电操作也是排他性的，当一个桨叶进行时，另外两个桨叶要保持原来的安全位置不变。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述总控 制器100还包括抗涡激处理器和抗涡激控制器，其中：第一控制器对第一桨叶进行上电操作后，向抗涡激处理器发送第一上电结束信号；第二控制器对第二桨叶进行上电操作后，向抗涡激处理器发送第二上电结束信号；第三控制器对第三桨叶进行上电操作后，向抗涡激处理器发送第三上电结束信号；若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则抗涡激控制器能够同时对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。三个桨叶的吊装操作和上电操作全部完成后，一键进入抗涡激操作，安全简单可靠。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述吊装操作包括：将第一桨叶、第二桨叶或第三桨叶吊起直至位置能够与变桨系统对接，然后将第一桨叶、第二桨叶或第三桨叶与变桨系统进行连接；所述上电操作包括：将变桨系统进行上电，然后驱动变桨系统带动第一桨叶、第二桨叶或第三桨叶转动，调节第一桨叶、第二桨叶或第三桨叶的节距角；所述抗涡激位置操作包括：驱动变桨系统带动第一桨叶、第二桨叶和第三桨叶转动，以将第一桨叶、第二桨叶和第三桨叶的节距角均调节至抗涡激位置。
在本发明的一个实施例中，在所述的变桨安装调试系统中，所述位置传感器包括：第四位置传感器304，被配置为安装在变桨系统与第一桨叶的连接处，以检测第一桨叶的节距角是否处于抗涡激位置，以及若第一桨叶的节距角是否处于抗涡激位置，则向第一子控制器201发送抗涡激位置信号；第五位置传感器305，被配置为安装在变桨系统与第二桨叶的连接处，以检测第二桨叶的节距角是否处于抗涡激位置，以及若第二桨叶的节距角是否处于抗涡激位置，则向第二子控制器202发送抗涡激位置信号；第六位置传感器306，被配置为安装在变桨系统与第三桨叶的连接处，以检测第三桨叶的节距角是否处于抗涡激位置，以及若第三桨叶的节距角是否处于抗涡激位置，则向第三子控制器203发送抗涡激位置信号。上述传感器都是在检测三个桨叶的节距角是否调节至抗涡激位置，以保证调节到位。
在本发明的一个实施例中，在所述的变桨安装调试系统中，第一子控 制器201接收到第四位置传感器304的抗涡激位置信号后，向抗涡激处理器发送第一抗涡激信号；第二子控制器202接收到第五位置传感器305的抗涡激位置信号后，向抗涡激处理器发送第二抗涡激信号；第三子控制器203接收到第六位置传感器306的抗涡激位置信号后，向抗涡激处理器发送第三抗涡激信号。在所述的变桨安装调试系统中，若抗涡激处理器能够同时接收到第一抗涡激信号、第二抗涡激信号和第三抗涡激信号，则抗涡激处理器产生安装调试结束信号。至此整个安装调试工作结束，操作人员可以一目了然的收到信号。整个安装调试过程环环相扣，由于三个桨叶之间的禁止操作信号的互斥，以及吊装结束信号、上电结束信号等信号具有单向顺序，无法并行操作，使得过程更加有序可靠，具有防呆的功能，避免了人工的误操作风险。
为了使得变桨安装调试系统的操作更加简单，在本发明的一个实施例中，在所述的变桨安装调试系统中，还包括操作面板，其中操作面板包括：第一信号显示装置401，被配置为第一处理器接收到第一安全信号时显示第一显示信号，第一处理器能够同时接收到第二使能信号和第三使能信号显示第二显示信号，第一处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第一抗涡激信号显示第四显示信号；第二信号显示装置401，被配置为第二处理器接收到第二安全信号时显示第一显示信号，第二处理器能够同时接收到第一使能信号和第三使能信号显示第二显示信号，第二处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第二抗涡激信号显示第四显示信号；第三信号显示装置401，被配置为第三处理器接收到第三安全信号时显示第一显示信号，第三处理器能够同时接收到第一使能信号和第二使能信号显示第二显示信号，第三处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第三抗涡激信号显示第四显示信号。例如设置三个LED灯，第一显示信号是蓝色，第二显示信号是黄色，第三显示信号是红色，第四显示信号是绿色等。使得操作者对能否操作、以及下一步如何操作一目了然。
在本发明的一个实施例中，在所述的变桨安装调试系统中，操作面板还包括第一挡位501、第二挡位501、第三挡位501、吊装按钮和上电按钮， 其中：若指针处于第一挡位，则按下吊装按钮或上电按钮时，对第一桨叶进行吊装操作或上电操作；若指针处于第二挡位，则按下吊装按钮或上电按钮时，对第二桨叶进行吊装操作或上电操作；若指针处于第三挡位，则按下吊装按钮或上电按钮时，对第三桨叶进行吊装操作或上电操作。
在本发明的一个实施例中，在所述的变桨安装调试系统中，吊装按钮在常规情况下被锁定；若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则吊装按钮被解锁，以使其能够被按下。
在本发明的一个实施例中，在所述的变桨安装调试系统中，上电按钮在常规情况下被锁定；若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则上电按钮被解锁，以使其能够被按下。
在本发明的一个实施例中，在所述的变桨安装调试系统中，操作面板还包括抗涡激按钮，其中：抗涡激按钮在常规情况下被锁定；若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则对抗涡激按钮进行解锁，以使其能够被按下；抗涡激按钮被按下后生成抗涡激操作信号，抗涡激控制器根据抗涡激操作信号对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。
本发明还提供一种变桨安装调试系统的操作方法，包括：将多个位置传感器中的每个位置传感器安装在变桨系统与一个桨叶的连接处；每个位置传感器检测其所对应的桨叶的位置，以及每个位置传感器将其所对应的桨叶的位置检测结果发送至该桨叶对应的子控制器；多个子控制器中的每个子控制器根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操 作使能位置；若该桨叶处于操作使能位置，则向总控制器100发送使能信号；总控制器100根据使能信号对桨叶进行操作。
在本发明的一个实施例中，在所述的变桨安装调试系统的操作方法中，还包括：通过总控制器100将三个桨叶中的至少两个桨叶对应的节距角调节至安全位置；对一个桨叶进行吊装操作，在吊装过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置；完成一个桨叶的吊装操作后，对该桨叶进行上电操作，在上电过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置。
在本发明的一个实施例中，在所述的变桨安装调试系统的操作方法中，还包括：依次完成三个桨叶的吊装操作和上电操作，当其中一个桨叶进行吊装操作或上电操作时，另外两个桨叶禁止任何操作；通过总控制器100将三个桨叶的节距角同时调节至抗涡激位置，通过位置传感器获取位置检测结果，保证三个桨叶的节距角均处于抗涡激位置；对三个桨叶进行断电。
在本发明提供的变桨安装调试系统及其操作方法中，通过每个位置传感器检测各个桨叶的位置，每个子控制器判断各个桨叶是否处于操作使能位置，若某桨叶处于操作使能位置，则总控制器100根据使能信号对该桨叶进行操作，本发明实现了将现有技术中由人工判断来操作桨叶，转换为传感器、子控制器和总控制器100一整套智能判断系统，更加安全可靠。
本发明将行业内组风轮，静调工作的无序、可并行、无防呆等状态通过防误锁具转变为串行、有序、可控的安全状态。
在本发明提供的变桨安装调试系统中，子控制器与变桨系统的连接关系包括：三套蓄电池和轴控制盒(容置子控制器)以及伺服电机和减速机放置于轮毂处，每个桨叶一套，一个总电气开关盒放置在轮毂和机舱连接处，整个系统的通讯总线和电缆靠滑环与机舱的总控制器连接。总控制器与轮毂内的轴控制盒通过现场总线通讯，达到控制三个独立的变桨距装置的目的。电动变桨系统采用三个桨叶分别带有独立的电驱动变桨距系统，机械部分包括回转支承，减速机和传动等。减速机固定在轮毂上，回转支承的内环安装在桨叶上，桨叶轴承的外环固定在轮毂上。当电驱动变桨系统上电后，伺服电动机带动减速机的输出轴小齿轮旋转，而且小齿轮与回 转支承的内环啮合，从而带动回转支承的内环与桨叶一起旋转，实现了改变节距角的目的。
在整个调试过程完成后，总控制器根据风速，发电机功率和转速等，把命令值发送到电动变桨系统，并且电动变桨系统把实际值和运行状况反馈到总控制器。电动变桨系统必须满足能够快速响应总控制器的命令，有独立工作的变桨系统，高性能的同步机制，安全可靠等的要求。变桨控制系统使桨叶的角度在一定范围(0度～90度)变化，以便调节输出功率，避免了定桨距机组在确定攻角后，有可能夏季发电低，而冬季又超发的问题。在低风速段，功率得到优化，能更好的将风能转化电能。
另外，本发明的变桨安装调试系统的操作方法还可以用于风机处于维护状态时，提供手动变桨及其它安全维护及检修的功能。当电网电压掉电时，由备电电源提供电气系统工作电压，主要完成顺桨功能。轴柜变桨调节方式应分为自动/手动两种模式，自动/手动模式设置通过两位置开关实现，手动模式正、反向调节及停止设置通过三位置开关实现。当风机处于维护状态且变桨调节处于手动模式时，可以实现每个桨叶单独变桨，但每次只能有一个轴柜可以通过相应控制开关，使变桨电机在正、反方向旋转来调节节距角；其它两个桨叶节距角必须处于90°位置，否则手动变桨功能失效。
轴柜上应设置一个控制开关，当风机处于维护状态且人员需要进入轮毂对变桨系统进行维护与检修时，该控制开关应断开，变桨电机刹车抱闸，逆变器的控制电源断电，以保证节距角停留在某一固定位置，直到该控制开关重新闭合后，节距角才可以改变。除此之外，该控制开关应一直处于闭合状态。将每个桨叶配置的两个ENCODER采集到的节距角信号进行比较，当角度偏差小于2°时，才允许PLC在需要时，对桨叶节距角进行调节；否则，只要该桨叶节距角小于90，都会以7度每秒的速度朝90°方向顺桨，其余桨叶的顺桨由软件控制完成。所有桨叶在91°位置各安装一个限位开关，在0°方向均不安装限位开关，桨叶当前节距角是否小于0°，由两个ENCODER传感器测量结果经过换算确定。轴柜变桨调节方 式处于自动位置，当下列任何一种情况发生，出故障轴柜的硬件系统应保证相应桨叶以7°每秒的速度朝90°方向顺桨，未受影响的轴柜，其桨叶顺桨由软件控制完成。
任意轴柜内的DP从站与PLC主站之间的通讯总线出现故障，由叶轮过速、振动开关、TOPBOX急停按钮、变流柜急停按钮、偏航限位开关串联组成的风机安全链以及与安全链串联的两个叶轮锁定信号断开(24VDC信号)，无论任何一个ENCODER出现故障，还是同一桨叶的两个ENCODER测量结果偏差超过规定的门限值；任何桨叶节距角在变桨过程中小于-2°；构成安全链、释放回路中的硬件系统出现故障；对于三相交流异步变桨电机，其逆变器控制电路应提供开环频率控制U/F、闭环空间矢量控制两种调速方式，默认设置为闭环空间矢量控制，当速度传感器损坏时，逆变器控制电路应立即将调速方式切换至开环频率控制U/F模式，并使对应桨叶以7度每秒的速度朝90°方向顺桨，其余桨叶则由软件来控制顺桨；在风机变桨过程中，应依次启动三个变桨电机，以防止三个变桨电机同时启动时，造成滑环过载；轴柜内所有冷却风扇的启、停，应受软件控制；电网电压是否掉电，应优先选择直接判断方式，其次选择通过备电电源电压的判断方式。轴柜应提供控制接口，以方便对备电电源性能，主要是指电网电压掉电情况下性能进行测试；轴柜应提供控制接口，以方便对轴柜内逆变器调速模式切换。
位置传感器可以是旋转编码器，增量式旋转编码器通过内部两个光敏接受管转化其角度码盘的时序和相位关系，得到其角度码盘角度位移量增加(正方向)或减少(负方向)，在接合数字电路特别是单片机后，增量式旋转编码器在角度测量和角速度测量较绝对式旋转编码器更具有廉价和优势。
每个桨叶配置的两个编码器，应保证其对桨叶节距角测量精度达到0.01°，轴柜内应有相应模块，用于显示桨叶当前节距角，以保证手动变桨模式下节距角不会超过91°限位开关位置，轴柜变桨调节方式处于自动模式下，若风机在顺桨的过程中节距角超过了91°限位开关的位置，此时可以将风机切换至维护状态，并通过轴柜内的变桨方式，将节距角调回90° 位置，轴柜变桨调节方式处于自动模式下，预防节距角超过限位开关的措施，91°限位开关，到达限位开关时，变桨电机刹车抱闸，轴柜逆变器的释放信号及变桨速度命令无效，同样会使变桨电机静止。
综上，上述实施例对变桨安装调试系统及其操作方法的不同构型进行了详细说明，当然，本发明包括但不局限于上述实施中所列举的构型，任何在上述实施例提供的构型基础上进行变换的内容，均属于本发明所保护的范围。本领域技术人员可以根据上述实施例的内容举一反三。
本说明书中各个实施例采用递进的方式描述，每个实施例重点说明的都是与其他实施例的不同之处，各个实施例之间相同相似部分互相参见即可。对于实施例公开的系统而言，由于与实施例公开的方法相对应，所以描述的比较简单，相关之处参见方法部分说明即可。
上述描述仅是对本发明较佳实施例的描述，并非对本发明范围的任何限定，本发明领域的普通技术人员根据上述揭示内容做的任何变更、修饰，均属于权利要求书的保护范围。

Claims (21)

  1. 一种变桨安装调试系统，其特征在于，包括：
    多个位置传感器，其中每个位置传感器被配置为能够安装在变桨系统与桨叶的连接处以检测该桨叶的位置；
    多个子控制器，其中每个子控制器被配置为执行下列动作：
    根据该子控制器所对应的桨叶的位置，确定该桨叶是否处于操作使能位置；以及
    若该桨叶处于操作使能位置，则向总控制器发送使能信号；
    总控制器，被配置为根据使能信号对桨叶进行操作。
  2. 如权利要求1所述的变桨安装调试系统，其特征在于，所述位置传感器包括：
    第一位置传感器，被配置为能够安装在变桨系统与第一桨叶的连接处，其中第一位置传感器被配置为检测第一桨叶的节距角是否处于安全位置，并且若第一桨叶的节距角处于安全位置，则向第一子控制器发送安全位置信号；
    第二位置传感器，被配置为能够安装在变桨系统与第二桨叶的连接处，其中第二位置传感器被配置为检测第二桨叶的节距角是否处于安全位置，并且若第二桨叶的节距角是否处于安全位置，则向第二子控制器发送安全位置信号；
    第三位置传感器，被配置为能够安装在变桨系统与第三桨叶的连接处，其中第二位置传感器被配置为检测第三桨叶的节距角是否处于安全位置，并且若第三桨叶的节距角是否处于安全位置，则向第三子控制器发送安全位置信号。
  3. 如权利要求2所述的变桨安装调试系统，其特征在于，
    第一子控制器在接收到第一位置传感器的安全位置信号后，向总控制器发送第一安全信号；和/或
    第二子控制器在接收到第二位置传感器的安全位置信号后，向总控制器发送第二安全信号；和/或
    第三子控制器在接收到第三位置传感器的安全位置信号后，向总控制 器发送第三安全信号。
  4. 如权利要求3所述的变桨安装调试系统，其特征在于，所述总控制器包括第一处理器、第二处理器及第三处理器，其中：
    若第一处理器接收到第一安全信号，则产生第一使能信号，并分别向第二处理器及第三处理器发送第一使能信号；
    若第二处理器接收到第二安全信号，则产生第二使能信号，并分别向第一处理器及第三处理器发送第二使能信号；以及
    若第三处理器接收到第三安全信号，则产生第三使能信号，并分别向第一处理器及第二处理器发送第三使能信号。
  5. 如权利要求4所述的变桨安装调试系统，其特征在于，所述总控制器包括第一控制器、第二控制器及第三控制器，其中：
    若第一处理器能够同时接收到第二使能信号和第三使能信号，则第一控制器能够对第一桨叶进行吊装操作和上电操作，否则禁止对第一桨叶进行吊装操作和上电操作；
    若第二处理器能够同时接收到第一使能信号和第三使能信号，则第二控制器能够对第二桨叶进行吊装操作和上电操作，否则禁止对第二桨叶进行吊装操作和上电操作；以及
    若第三处理器能够同时接收到第一使能信号和第二使能信号，则第三控制器能够对第三桨叶进行吊装操作和上电操作，否则禁止对第三桨叶进行吊装操作和上电操作。
  6. 如权利要求5所述的变桨安装调试系统，其特征在于，
    当第一控制器对第一桨叶进行吊装操作和上电操作时，向第二处理器和第三处理器发送禁止操作信号；
    当第二控制器对第二桨叶进行吊装操作和上电操作时，向第一处理器和第三处理器发送禁止操作信号；以及
    当第三控制器对第三桨叶进行吊装操作和上电操作时，向第一处理器和第二处理器发送禁止操作信号。
  7. 如权利要求6所述的变桨安装调试系统，其特征在于，
    所述第一处理器接收到禁止操作信号时，第一控制器禁止对第一桨叶 进行吊装操作和上电操作；
    所述第二处理器接收到禁止操作信号时，第二控制器禁止对第二桨叶进行吊装操作和上电操作；
    所述第三处理器接收到禁止操作信号时，第三控制器禁止对第三桨叶进行吊装操作和上电操作；以及
    禁止操作信号的优先级高于第一使能信号、第二使能信号和第三使能信号。
  8. 如权利要求7所述的变桨安装调试系统，其特征在于，
    第一控制器对第一桨叶进行吊装操作后，向第一处理器发送吊装结束信号，第一处理器接收到吊装结束信号后，则第一控制器能够对第一桨叶进行上电操作；
    第二控制器对第二桨叶进行吊装操作后，向第二处理器发送吊装结束信号，第二处理器接收到吊装结束信号后，则第二控制器能够对第二桨叶进行上电操作；以及
    第三控制器对第三桨叶进行吊装操作后，向第三处理器发送吊装结束信号，第三处理器接收到吊装结束信号后，则第三控制器能够对第三桨叶进行上电操作。
  9. 如权利要求8所述的变桨安装调试系统，其特征在于，所述总控制器还包括抗涡激处理器和抗涡激控制器，其中：
    第一控制器对第一桨叶进行上电操作后，向抗涡激处理器发送第一上电结束信号；
    第二控制器对第二桨叶进行上电操作后，向抗涡激处理器发送第二上电结束信号；
    第三控制器对第三桨叶进行上电操作后，向抗涡激处理器发送第三上电结束信号；以及
    若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则抗涡激控制器能够同时对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。
  10. 如权利要求9所述的变桨安装调试系统，其特征在于，所述吊装 操作包括：将第一桨叶、第二桨叶或第三桨叶吊起直至位置能够与变桨系统对接，然后将第一桨叶、第二桨叶或第三桨叶与变桨系统进行连接；
    所述上电操作包括：将变桨系统进行上电，然后驱动变桨系统带动第一桨叶、第二桨叶或第三桨叶转动，调节第一桨叶、第二桨叶或第三桨叶的节距角；以及
    所述抗涡激位置操作包括：驱动变桨系统带动第一桨叶、第二桨叶和第三桨叶转动，以将第一桨叶、第二桨叶和第三桨叶的节距角均调节至抗涡激位置。
  11. 如权利要求10所述的变桨安装调试系统，其特征在于，所述位置传感器包括：
    第四位置传感器，被配置为安装在变桨系统与第一桨叶的连接处，以检测第一桨叶的节距角是否处于抗涡激位置，以及
    若第一桨叶的节距角是否处于抗涡激位置，则向第一子控制器发送抗涡激位置信号；
    第五位置传感器，被配置为安装在变桨系统与第二桨叶的连接处，以检测第二桨叶的节距角是否处于抗涡激位置，以及
    若第二桨叶的节距角是否处于抗涡激位置，则向第二子控制器发送抗涡激位置信号；
    第六位置传感器，被配置为安装在变桨系统与第三桨叶的连接处，以检测第三桨叶的节距角是否处于抗涡激位置，以及
    若第三桨叶的节距角是否处于抗涡激位置，则向第三子控制器发送抗涡激位置信号。
  12. 如权利要求11所述的变桨安装调试系统，其特征在于，
    第一子控制器接收到第四位置传感器的抗涡激位置信号后，向抗涡激处理器发送第一抗涡激信号；
    第二子控制器接收到第五位置传感器的抗涡激位置信号后，向抗涡激处理器发送第二抗涡激信号；
    第三子控制器接收到第六位置传感器的抗涡激位置信号后，向抗涡激处理器发送第三抗涡激信号。
  13. 如权利要求12所述的变桨安装调试系统，其特征在于，若抗涡激处理器能够同时接收到第一抗涡激信号、第二抗涡激信号和第三抗涡激信号，则抗涡激处理器产生安装调试结束信号。
  14. 如权利要求13所述的变桨安装调试系统，其特征在于，还包括操作面板，其中操作面板包括：
    第一信号显示装置，被配置为第一处理器接收到第一安全信号时显示第一显示信号，第一处理器能够同时接收到第二使能信号和第三使能信号显示第二显示信号，第一处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第一抗涡激信号显示第四显示信号；
    第二信号显示装置，被配置为第二处理器接收到第二安全信号时显示第一显示信号，第二处理器能够同时接收到第一使能信号和第三使能信号显示第二显示信号，第二处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第二抗涡激信号显示第四显示信号；
    第三信号显示装置，被配置为第三处理器接收到第三安全信号时显示第一显示信号，第三处理器能够同时接收到第一使能信号和第二使能信号显示第二显示信号，第三处理器接收到禁止操作信号时显示第三显示信号，抗涡激处理器接收到第三抗涡激信号显示第四显示信号。
  15. 如权利要求12所述的变桨安装调试系统，其特征在于，操作面板还包括第一挡位、第二挡位、第三挡位、吊装按钮和上电按钮，其中：
    若指针处于第一挡位，则按下吊装按钮或上电按钮时，对第一桨叶进行吊装操作或上电操作；
    若指针处于第二挡位，则按下吊装按钮或上电按钮时，对第二桨叶进行吊装操作或上电操作；以及
    若指针处于第三挡位，则按下吊装按钮或上电按钮时，对第三桨叶进行吊装操作或上电操作。
  16. 如权利要求15所述的变桨安装调试系统，其特征在于，吊装按钮在常规情况下被锁定；
    若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；
    若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则吊装按钮被解锁，以使其能够被按下；以及
    若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则吊装按钮被解锁，以使其能够被按下。
  17. 如权利要求15所述的变桨安装调试系统，其特征在于，上电按钮在常规情况下被锁定；
    若指针处于第一挡位且第一处理器同时接收到第二使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；
    若指针处于第二挡位且第二处理器同时接收到第一使能信号和第三使能信号，则上电按钮被解锁，以使其能够被按下；以及
    若指针处于第三挡位且第三处理器同时接收到第一使能信号和第二使能信号，则上电按钮被解锁，以使其能够被按下。
  18. 如权利要求12所述的变桨安装调试系统，其特征在于，操作面板还包括抗涡激按钮，其中：
    抗涡激按钮在常规情况下被锁定；
    若抗涡激处理器同时接收到第一上电结束信号、第二上电结束信号和第三上电结束信号，则对抗涡激按钮进行解锁，以使其能够被按下；
    抗涡激按钮被按下后生成抗涡激操作信号，抗涡激控制器根据抗涡激操作信号对第一桨叶、第二桨叶和第三桨叶同时进行抗涡激位置操作。
  19. 一种变桨安装调试系统的操作方法，其特征在于，包括：
    将多个位置传感器中的每个位置传感器安装在变桨系统与一个桨叶的连接处；
    每个位置传感器检测其所对应的桨叶的位置，以及
    每个位置传感器将其所对应的桨叶的位置检测结果发送至该桨叶对应的子控制器；
    多个子控制器中的每个子控制器根据其所对应的桨叶的位置检测结果，判断该桨叶是否处于操作使能位置；
    若该桨叶处于操作使能位置，则向总控制器发送使能信号；以及
    总控制器根据使能信号对桨叶进行操作。
  20. 如权利要求19所述的变桨安装调试系统的操作方法，其特征在于，还包括：
    通过总控制器将三个桨叶中的至少两个桨叶对应的节距角调节至安全位置；
    对一个桨叶进行吊装操作，在吊装过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置；以及
    完成一个桨叶的吊装操作后，对该桨叶进行上电操作，在上电过程中，通过位置传感器获取位置检测结果，保证另外两个桨叶的节距角处于安全位置。
  21. 如权利要求20所述的变桨安装调试系统的操作方法，其特征在于，还包括：
    依次完成三个桨叶的吊装操作和上电操作，当其中一个桨叶进行吊装操作或上电操作时，另外两个桨叶禁止任何操作；
    通过总控制器将三个桨叶的节距角同时调节至抗涡激位置，通过位置传感器获取位置检测结果，保证三个桨叶的节距角均处于抗涡激位置；以及
    对三个桨叶进行断电。
PCT/CN2021/089565 2021-04-25 2021-04-25 变桨安装调试系统及其操作方法 WO2022226680A1 (zh)

Priority Applications (6)

Application Number Priority Date Filing Date Title
PCT/CN2021/089565 WO2022226680A1 (zh) 2021-04-25 2021-04-25 变桨安装调试系统及其操作方法
ES202390124A ES2956834R1 (es) 2021-04-25 2021-04-25 Sistema de instalacion y depuracion de paso variable y metodo de funcionamiento del mismo
MA63060A MA63060A1 (fr) 2021-04-25 2021-04-25 Système d'installation et de débogage à pas variable et procédé de fonctionnement de celui-ci
CN202180002117.1A CN113454336B (zh) 2021-04-25 2021-04-25 变桨安装调试系统及其操作方法
MX2023011700A MX2023011700A (es) 2021-04-25 2021-04-25 Sistema de instalacion y depuracion de paso variable y metodo de funcionamiento del mismo.
ZA2023/09552A ZA202309552B (en) 2021-04-25 2023-10-12 Variable-pitch installation and debugging system and operation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2021/089565 WO2022226680A1 (zh) 2021-04-25 2021-04-25 变桨安装调试系统及其操作方法

Publications (1)

Publication Number Publication Date
WO2022226680A1 true WO2022226680A1 (zh) 2022-11-03

Family

ID=77819419

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2021/089565 WO2022226680A1 (zh) 2021-04-25 2021-04-25 变桨安装调试系统及其操作方法

Country Status (6)

Country Link
CN (1) CN113454336B (zh)
ES (1) ES2956834R1 (zh)
MA (1) MA63060A1 (zh)
MX (1) MX2023011700A (zh)
WO (1) WO2022226680A1 (zh)
ZA (1) ZA202309552B (zh)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109989881A (zh) * 2019-05-21 2019-07-09 国电联合动力技术有限公司 用于风电机组单叶片吊装的控制装置及其控制方法和机组
CN118517370B (zh) * 2024-07-23 2024-10-08 东方电气风电股份有限公司 一种风电机组自动抗涡激方法、系统及存储介质

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101646867A (zh) * 2007-02-13 2010-02-10 罗伯特.博世有限公司 用于驱动多个轴的驱动装置
CN202718807U (zh) * 2011-02-15 2013-02-06 Ssb风系统两合公司 风力涡轮机
EP2980401A1 (en) * 2014-07-29 2016-02-03 ALSTOM Renewable Technologies Pitch drive system with lubrication arrangement
WO2017193358A1 (zh) * 2016-05-13 2017-11-16 周方 风力发电机的多段式转子叶片
CN108180109A (zh) * 2017-12-30 2018-06-19 北京金风科创风电设备有限公司 变桨系统及叶片零度位置校准方法
WO2019028375A1 (en) * 2017-08-03 2019-02-07 Barnhart Crane and Rigging Co. DEVICE AND METHOD FOR REMOVING AND INSTALLING WIND TURBINE BEARING

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203257603U (zh) * 2012-12-14 2013-10-30 天津瑞能电气有限公司 一种新型风力发电机组变桨距系统调试装置
DE102014215969A1 (de) * 2014-08-12 2016-02-18 Wobben Properties Gmbh Verfahren zum Installieren eines Rotorblattes an einer Windenergieanlage
CN205484581U (zh) * 2015-12-31 2016-08-17 新疆金风科技股份有限公司 变桨直流驱动器检测平台及检测柜
CN107246357A (zh) * 2017-07-13 2017-10-13 固安华电天仁控制设备有限公司 一种桨叶位置自检风力发电变桨系统
US10953938B2 (en) * 2018-03-15 2021-03-23 The Boeing Company Apparatus and methods for maintenance of wind turbine blades
CN208996866U (zh) * 2018-08-02 2019-06-18 固安华电天仁控制设备有限公司 一种海洋能发电机组的变桨控制装置
CN112855444A (zh) * 2021-03-18 2021-05-28 华润风电(龙岩)有限公司 一种变桨控制系统及风力发电机组

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101646867A (zh) * 2007-02-13 2010-02-10 罗伯特.博世有限公司 用于驱动多个轴的驱动装置
CN202718807U (zh) * 2011-02-15 2013-02-06 Ssb风系统两合公司 风力涡轮机
EP2980401A1 (en) * 2014-07-29 2016-02-03 ALSTOM Renewable Technologies Pitch drive system with lubrication arrangement
WO2017193358A1 (zh) * 2016-05-13 2017-11-16 周方 风力发电机的多段式转子叶片
WO2019028375A1 (en) * 2017-08-03 2019-02-07 Barnhart Crane and Rigging Co. DEVICE AND METHOD FOR REMOVING AND INSTALLING WIND TURBINE BEARING
CN108180109A (zh) * 2017-12-30 2018-06-19 北京金风科创风电设备有限公司 变桨系统及叶片零度位置校准方法

Also Published As

Publication number Publication date
CN113454336A (zh) 2021-09-28
ES2956834A2 (es) 2023-12-28
ES2956834R1 (es) 2024-10-14
MX2023011700A (es) 2023-10-19
ZA202309552B (en) 2024-06-26
MA63060A1 (fr) 2024-01-31
CN113454336B (zh) 2022-08-26

Similar Documents

Publication Publication Date Title
EP1664527B1 (en) Redundant blade pitch control system for a wind turbine
EP1990539B1 (en) Wind power generation system, and control method therefor
US8154141B2 (en) Wind power installation and method of modifying the blade pitch in a wind power installation
US8240990B2 (en) Apparatus and method for reducing asymmetric rotor loads in wind turbines during shutdown
CN101555871B (zh) 一种变桨距变速风力发电机组
CN201474863U (zh) 一种变桨距变速风力发电机组
WO2022226680A1 (zh) 变桨安装调试系统及其操作方法
US20130088009A1 (en) Method to Prevent Over Torque of Yaw Drive Components in a Wind Turbine
CN203161440U (zh) 一种风力发电机组变桨系统的应急顺桨冗余控制装置
CN107407259A (zh) 设置成控制支持臂定向的用于具有多个转子的风力涡轮机的控制系统
CN111561421B (zh) 用于保护风力涡轮免于在高风速期间颤振的系统和方法
CN208900281U (zh) 一种风力发电机组变桨双电机驱动控制系统
CN105257474B (zh) 一种手动变桨控制系统
CN208040621U (zh) 变桨系统和风力发电机组
CN103883469A (zh) 机械耦合式磁悬浮风机偏航系统
KR101350511B1 (ko) 피치 시스템 및 이를 포함하는 풍력발전기
KR20140009631A (ko) 풍력, 태양광 및 디젤엔진을 이용한 하이브리드선박 복합발전장치
CN207620967U (zh) 风力发电机组的变桨控制系统
CN110067703B (zh) 蜗杆式同步变桨风电机组及控制方法
EP2963286A1 (en) Windturbine and method for stopping the same
CN106150900A (zh) 双馈‑异步风力发电系统及其运行方法
CN105048496A (zh) 一种双电机风力发电机组的并网控制方法
CN101004167A (zh) 花瓣状风叶垂直轴高效风力发电机
WO2016086443A1 (zh) 风力发电机
CN108979945A (zh) 一种双向发电的潮流能发电机组及其系统

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 21938173

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: P202390124

Country of ref document: ES

WWE Wipo information: entry into national phase

Ref document number: MX/A/2023/011700

Country of ref document: MX

WWE Wipo information: entry into national phase

Ref document number: 202317076514

Country of ref document: IN

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 523450862

Country of ref document: SA

122 Ep: pct application non-entry in european phase

Ref document number: 21938173

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 523450862

Country of ref document: SA