CN103472741A - Control system for fatigue certification experimental test on blades of wind turbine - Google Patents

Control system for fatigue certification experimental test on blades of wind turbine Download PDF

Info

Publication number
CN103472741A
CN103472741A CN2013103842168A CN201310384216A CN103472741A CN 103472741 A CN103472741 A CN 103472741A CN 2013103842168 A CN2013103842168 A CN 2013103842168A CN 201310384216 A CN201310384216 A CN 201310384216A CN 103472741 A CN103472741 A CN 103472741A
Authority
CN
China
Prior art keywords
strain
test
blade
frequency
foil gauge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN2013103842168A
Other languages
Chinese (zh)
Other versions
CN103472741B (en
Inventor
黄永东
黄志华
崔隆宇
赵萍
钟贤和
王�锋
耿向明
羊森林
戚中浩
曾明伍
张慧敏
李�杰
贾森
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dongfang Electric Wind Power Co Ltd
Original Assignee
DEC Dongfang Turbine Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by DEC Dongfang Turbine Co Ltd filed Critical DEC Dongfang Turbine Co Ltd
Priority to CN201310384216.8A priority Critical patent/CN103472741B/en
Publication of CN103472741A publication Critical patent/CN103472741A/en
Application granted granted Critical
Publication of CN103472741B publication Critical patent/CN103472741B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Wind Motors (AREA)

Abstract

The invention discloses a control system for a fatigue certification experimental test on the blades of a wind turbine. The control system comprises a test bed, a load vibration device, a strain gauge, a bridge-type strain processor, a high-speed synchronous data acquisition card, a computer, a storage and a display, wherein the bridge-type strain processor comprises a shunt calibration module capable of recalibrating the sensitivity of the strain gauge, a bridge circuit temperature compensation module capable of compensating an environmental temperature change, and a linear expansion coefficient error between the strain gauge and a tested blade material, and a strain value return-to-zero module capable of returning the initial strain value of the tested blade to zero; an automatic control monitoring module and a test data processing module are installed in the computer, the automatic control monitoring module is used for comparing real-time test strain signal data with a designed value so as to judge whether the test strain value is in the range of the designed value, and deciding whether the output for an invariable-frequency control signal, a variable-frequency control signal or a shut-down control signal of a frequency converter is kept or not according to the judged result, and the test data processing module is used for converting strain voltage signal data to an actual strain measured value.

Description

The tired certification test test control system of blade of wind-driven generator
Technical field
The present invention relates to test control system, specifically the tired certification test test control system of a kind of blade of wind-driven generator.
Background technology
Wind wheel blade is one of critical component of aerogenerator, and the Design and manufacture quality of blade directly has influence on operational efficiency, serviceable life and the acting performance of aerogenerator.Introduction and digestion along with the blade of wind-driven generator technology, China also starts autonomous Design and produces the blade of MW class wind turbine, by its commercialization, but, the commercialization of blade of wind-driven generator must obtain corresponding international organization and authenticate, the authentication of the fatigue of blade of wind-driven generator is IEC(International Electrotechnical Commission) one of requisite authentication item in standard, the purpose of its authentication is: find technique irrationality and the manufacturing defect in blade design and manufacture process 1., consistance and the reliability of checking blade design and manufacture, and for improving from now on design, manufacture and subsequent treatment provide reliable basis, 2. guarantee that blade meets or exceeds 20 years serviceable life, 3. in tired certification test, within the strain value of the tired certification test Leaf of General Requirements sensitive spot is controlled at design load ± 5% scope, only in tired certification test process, after guaranteeing that test repeated strain value is within design calculated value institute permissible range, can assert that Design and manufacture has consistance, and can assert reliability, the feasibility of Design and manufacture.
The tired certification test of blade of wind-driven generator mainly comprises following action: independently complete respectively the tired certification test that blade is waved (flapwise) and shimmy (edgewise) direction 1.; 2. at blade, wave and shimmy direction difference installed load exciting device and static counterweight, measure the natural frequency of single blade, according to the repeated strain value recorded and the comparing result of design load, adjust the output frequency of frequency converter, raise or reduce the exciting force in torture test.
Because the test macro that has the tired certification test of blade of wind-driven generator now is the open test system that does not have automatic control monitoring function, mainly there is following problem in it: in tired certification test process, once the repeated strain of blade sensitive spot is not within the zone of reasonableness of design load, be merely able to by the output frequency of artificial adjustment frequency converter, increase or reduce the exciting force of torture test, but, the torture test of an operating mode of blade often needs to continue to carry out the even trimestral time of two weeks, in the process of tired certification test, blade easily is subject to the impact of the factors such as environment temperature and the heating of blade self material, certain variation (for example will occur in its rigidity, when environment temperature is low, the rigidity of blade will increase, otherwise anti-), thereby cause the strain value of blade sensitive spot to change, even surpass or lower than the strain value of blade fatigue design, once the repeated strain tested, be worth improper, need by the output frequency of artificial adjustment frequency converter, control the repeated strain of blade sensitive spot within rational scope, this not only can increase artificial work load greatly, and there is very large subjectivity in artificial the adjustment, accurately and poor reliability, easily make blade in process of the test, the repeated strain value of its sensitive spot surpasses or lower than the fatigue design value, thereby can not meet the requirement of the tired certification test of blade, while particularly when the blade stiffness variation, causing Natural Frequency of Blade to change thereupon, to likely cause tired excited frequency to overlap with Natural Frequency of Blade and produce resonance, now, once artificial treatment not in time, will greatly increase the danger of tired certification test, even can cause the security incident of blade damage.
Summary of the invention
The object of the invention is to: for the deficiency of above-mentioned existing test macro, provide a kind of blade of wind-driven generator simple to operate, that the automatic intelligent degree is high, test data is accurate, safety and reliability is high, practical tired certification test test control system.
The technical solution used in the present invention is, the tired certification test test control system of a kind of blade of wind-driven generator, and described test control system comprises:
-testing table, described testing table is for installing tested blade;
-load exciting device, described load exciting device is for applying dynamic Fatigue Testing Loads to tested blade, and the excited frequency of load exciting device is by Frequency Converter Control;
-foil gauge, described foil gauge is a plurality of, and each foil gauge is self-temperature-compensated strain ga(u)ge, and a plurality of foil gauges are located at respectively on each sensitive spot of tested blade, for detection of the repeated strain value of tested blade each sensitive spot under Fatigue Testing Loads;
-bridge-type strained handling device, the repeated strain signal data that described bridge-type strained handling device arrives for the treatment of all strain measurements; Bridge-type strained handling device comprises shunting calibration module ,Qiao road temperature compensation module and the strain value module that makes zero, and described shunting calibration module for recalibrating the sensitivity of foil gauge, to eliminate the impact of stube cable on foil gauge sensitivity before test; Described bridge road temperature compensation module is for the error of the linear expansion coefficient between compensate for ambient temperature variation and foil gauge and tested blade material, to realize round-the-clock tested blade being carried out to torture test; The module that makes zero described strain value makes zero for the strain initial value by tested blade;
-high-speed synchronous data acquiring card, described high-speed synchronous data acquiring card becomes digital signal for foil gauge analog signal conversion that bridge-type strained handling device is obtained, and high-speed synchronous collection and keep these signal datas, and these signal datas are flowed to computing machine;
-computing machine, be equipped with automatic control monitoring modular and testing data processing module in described computing machine, real-time testing strain signal data and design load that described automatic control monitoring modular transports the high-speed synchronous data acquiring card are contrasted, within judging with this whether the test strain value is in the scope of design load, if, the exciting force that shows the current output of load exciting device meets the torture test requirement, keep current excited frequency and the eccentric weight quality of load exciting device, if not, the exciting force that shows the current output of load exciting device need to be regulated change, automatically control monitoring modular and send the frequency change control signal that raises or reduce according to comparing result to frequency converter, the frequency of exporting by frequency converter changes the excited frequency of the tested blade of load exciting device exciting, if after the excited frequency that changes the load exciting device, the real-time testing strain signal data that the high-speed synchronous data acquiring card collects have still exceeded the design load scope or have reached setting dangerous values scope, automatically control monitoring modular and export stopping signal to frequency converter, the action of Ending Load exciting device, described testing data processing module, for the treatment of the voltage signal data of foil gauge output, converts the compliance voltage signal data to actual strain measurement value,
-storer, described storer is for storing the measuring-signal data of foil gauge output;
-display, described display is used for showing the measured value of foil gauge output signal after treatment and excited frequency and the fatigue life cycle of current tested blade.
Further, be set with frequency conversion higher limit and frequency conversion lower limit in described frequency converter.
Further, described automatic control monitoring modular is natural frequency that tested blade is tested to the frequency conversion value of frequency converter output 80~95%.
Further, described load exciting device mainly consists of reductor and eccentric weight exciting agency, the load exciting device is fixed on tested blade by fixture, the reductor of load exciting device drives the action of eccentric weight exciting agency, and the exciting force of eccentric weight exciting agency passes to tested blade by fixture.
Further, the temperature self-compensation ambient temperature range of described foil gauge is-20~40 ℃.
Further, described foil gauge is by the room temperature fast-curing glue on the sensitive spot of tested blade, and the exposed surface of foil gauge scribbles the protective finish of waterproof and dustproof.
The invention has the beneficial effects as follows: above-mentioned testing fatigue control system can be applied to the tired certification test test of blade of wind-driven generator that all natural frequencys are greater than 0.9Hz, in the tired certification test process of blade, can meet the data acquisition of test strain signal and the storage work of 16 test channel, simultaneously, it can also meet the static(al) certification test test of blade of wind-driven generator; Above-mentioned test control system mainly can be realized following functions:
1). Natural Frequency of Blade and damping test;
2). automatically realize shunting calibration (shunt calibration), guarantee to test the strain signal data accurately, reliable, the precision that makes to test the strain signal data is not subject to the impact of conductor length;
3). automatically realize ambient temperature compensation, the error that elimination brings because of the factors such as linear expansion coefficient between variation of ambient temperature and foil gauge and tested blade material, further ensure accuracy and the reliability of test strain signal data, to realize round-the-clock tested blade being carried out to tired certification test;
4). automatically realize the work of making zero (Offset Null Compensation) of strain initial testing data, reduced the workload of artificial treatment test data, its principle be utilize digital potentiometer by the output valve of bridge voltage regular be zero;
5). realize the synchronous of multi-point sampler strain signal data and keep function (Simultaneous Sample and Hold), strict guarantee synchronous, the real-time of multi-point sampler strain signal data;
6). automatically realize that test strain signal data and design load are contrasted, and within whether being in the scope of design load according to comparing result judgement test strain signal data, export corresponding maintenance, frequency conversion, shutdown control signal according to judged result, the control of realization to the frequency converter output frequency, thereby the control of the realization of automatic intelligent to whole system, alleviate the hand labor load, the security of safeguards system, tested blade and experimenter's person;
7). according to the shutdown control signal to frequency converter output, synchronously send early warning signal, remind the experimenter to note and check failure and other reasons;
8). the test data to the tired certification test of blade realizes simultaneous display and storage; And the storage of test data can be divided into two parts, wherein part employing FIFO(first in first out) mode is stored (for example strain waveform data in nearest two hours), another part adopts regularly preserving type to store positive peak and the negative peak strain value of each sensitive spot of tired certification test test overall process, data file can all adopt binary format, thereby saves the storage space of computer memory;
9). according to the natural frequency that tested blade is recorded, frequency conversion higher limit and frequency conversion lower limit are set on frequency converter, thereby set the operating frequency range of frequency converter, to frequency converter output frequency change control signal the time, the frequency change control signal that simultaneously can in automatically controlling monitoring modular, set output by the test natural frequency 80~95%, again realize the restriction to the frequency converter frequency working range, and then, more than guaranteeing that tired certification test can not be operated in tested Natural Frequency of Blade point, guarantee the security of system, tested blade and experimenter's person so that dual.
The accompanying drawing explanation
Below in conjunction with accompanying drawing, the present invention is further illustrated.
Fig. 1 is formation of the present invention and uses the status architecture schematic diagram.
Fig. 2 is topology diagram of the present invention.
Fig. 3 is software program structural drawing of the present invention.
Fig. 4 is test flow chart of the present invention.
Fig. 5 is control principle drawing of the present invention.
Embodiment
Formation of the present invention and use status architecture are referring to Fig. 1, bridge-type strained handling device of the present invention, each function of automatically controlling monitoring modular and testing data processing module realize by the software based on the Labview establishment fully, and topological structure of the present invention, software program structure are referring to Fig. 2 and Fig. 3.The present invention includes testing table 1, load exciting device, foil gauge 5, bridge-type strained handling device 6, high-speed synchronous data acquiring card 7, computing machine 12, storer 10 and display 11.
Wherein, testing table 1 is for installing tested blade 2, and tested blade 2 laterally is assemblied on testing table 1.
The load exciting device mainly consists of reductor 4 and eccentric weight exciting agency, the load exciting device is fixed on tested blade 2 by fixture, in case tested blade 2 is caused to damage, the reductor 4 of load exciting device drives the action of eccentric weight exciting agency, the exciting force of eccentric weight exciting agency passes to tested blade 2 by fixture, make tested blade 2 produce upper and lower Fatigue Vibration, the load exciting device is for applying dynamic Fatigue Testing Loads to tested blade 2.Reductor 4 gyro frequencys are controlled by the frequency converter 3 be connected with computing machine 12, according to the natural frequency that tested blade 2 is recorded, are set with frequency conversion higher limit and frequency conversion lower limit in frequency converter 3, thereby set the operating frequency range of frequency converter 3.
Foil gauge 5 is a plurality of; each foil gauge 5 is self-temperature-compensated strain ga(u)ge; their temperature self-compensation ambient temperature range is-20~40 ℃; these foil gauges 5 are by the room temperature fast-curing glue on the sensitive spot of tested blade 2, and each exposed surface of foil gauge 5 scribbles the protective finish of waterproof and dustproof.Tested blade 2 produces upper and lower Fatigue Vibration under the effect of load exciting device, make each sensitive spot of tested blade 2 that corresponding repeated strain occur, these foil gauges 5 are for detection of the repeated strain value of tested blade 2 each sensitive spot distortion under Fatigue Testing Loads.
The repeated strain signal data that bridge-type strained handling device 6 arrives for the treatment of all strain measurements, this bridge-type strained handling device 6 comprises shunting calibration module ,Qiao road temperature compensation module and the strain value module that makes zero.The shunting calibration module, for before experimental test, is recalibrated the sensitivity of foil gauge, to eliminate the impact of stube cable on foil gauge 5 sensitivity.Bridge road temperature compensation module is for the error of the linear expansion coefficient between compensate for ambient temperature variation and foil gauge 5 and tested blade 2 materials, thereby further reduce the affected by environment and test error that brings of foil gauge 5 in the experimental test process, to realize round-the-clock tested blade 2 being carried out to tired certification test.The module that makes zero strain value makes zero for the strain initial value by tested blade 2.
High-speed synchronous data acquiring card 7 becomes digital signal for the foil gauge analog signal conversion that bridge-type strained handling device 6 is obtained, and high-speed synchronous collection and keep these signal datas, and these signal datas are flowed to computing machine 12.
Automatic control monitoring modular 8 and testing data processing module 9 are housed in computing machine 12.Automatically control monitoring modular 8 transports high-speed synchronous data acquiring card 7 real-time testing strain signal data and design load are contrasted, within judging with this whether the test strain value is in the scope of design load, if, show that the excited frequency of the current output of load exciting device is suitable, automatically control monitoring modular 8 lockings, keep the current excited frequency of load exciting device, if not, the excited frequency that shows the current output of load exciting device need to be regulated change, automatically control monitoring modular 8 and send the frequency change control signal that raises or reduce according to comparing result to frequency converter 3, change the exciting force size of the tested blade of load exciting device exciting by the frequency of frequency converter 3 outputs, in order further to guarantee fatigue test system, the safety of tested blade and experimenter's person, automatically controlling in monitoring modular 8 the variable frequency control scope to frequency converter 3 outputs that arranged, 80~95% of test natural frequency that its frequency conversion scope is tested blade 2, again to realize the restriction to frequency converter 3 variable frequency work scopes, and then more than guaranteeing that tired certification test can not be operated in the natural frequency point of tested blade 2, if after the excited frequency that changes the load exciting device, the real-time testing strain signal data that high-speed synchronous data acquiring card 7 collects have still exceeded the design load scope or have reached setting dangerous values scope, automatically control monitoring modular 8 to frequency converter 3 output stopping signals, the work of Ending Load exciting device, meanwhile, automatically control monitoring modular 8 output early warning signal automatically, this early warning signal will exceed the scope of design value and set dangerous values and carry out heterochromatic marking, the early warning result demonstrates by display 11, to remind the experimenter to note and to check failure and other reasons.The compliance voltage signal data that testing data processing module 9 collects for the treatment of high-speed synchronous data acquiring card 7, convert the compliance voltage signal data to actual strain measurement value.
Storer 10 can embeddeding computer 12 in, also can be external outside computing machine 12.Storer 10 is for the measuring-signal data of the foil gauge output of storing machine 12 as calculated and having processed, in order to store comprehensively, reliably data, can consider storer 10 is divided into to two parts, wherein part employing FIFO(first in first out) mode is stored (for example strain waveform data in nearest two hours), another part adopts regularly preserving type to store positive peak and the negative peak strain value of each sensitive spot of tired certification test test overall process, data file can all adopt binary format, thereby saves the storage space of computer memory.
The measured value of display 11 foil gauge output signal after computing machine 12 is processed for demonstration and excited frequency and the fatigue life cycle of current tested blade 2.
In order to check the residual intensity of tested blade after torture test, by set up static(al) test module, long-range apart from detection module, force cell etc. to the present invention, can realize the static(al) test of tested blade residual intensity.
Testing process of the present invention is referring to Fig. 4, and control principle of the present invention is referring to Fig. 5.In the process of the tired certification test of blade, automatically controlling monitoring and adjusting tested blade sensitive spot repeated strain value is one of gordian technique of the present invention, it need to possess two functions, one is: when main sensitive spot strain value surpass the design strain 15% after, automatically stop frequency converter frequency output, the Fatigue Testing Loads that then stops tested blade loads; Its two: when main sensitive spot strain value surpass the design strain 10% the time; automatically controlling monitoring modular is just adjusted excited frequency with predefined frequency converter frequency conversion scope; within Fatigue Testing Loads is adjusted to suitable scope; if still Fatigue Testing Loads can not be adjusted to OK range in given frequency converter setting range within; export stopping signal and stop torture test, so that testing crew is searched reason and solved corresponding fault.For this reason, this is automatically controlled monitoring modular and need to complete following functions:
1). can automatically control the output frequency of frequency converter;
2). when theoretical strain value surpasses 5~10% with the error of testing strain value, automatically adjust the output frequency of frequency converter, its adjustment step-length and frequency adjustment range are optional, to making to test the requirement that the repeated strain value meets torture test, if can not make Theoretical Design repeated strain value when the error of test strain value is in correct scope by the output frequency of adjusting frequency converter, export stopping signal and stop torture test;
3). when the error of any one output test repeated strain value and Theoretical Design repeated strain value reaches 15%, export stopping signal and make torture test stop;
4). the output frequency that frequency converter is set is 0~natural frequency, prevents that the frequency converter hypervelocity from causing unnecessary danger;
5). in automatically controlling monitoring modular, again limit the frequency output area of frequency converter, the scope of its setting is left and right, 0~tested Natural Frequency of Blade ' (90~95%), mainly for preventing the natural frequency of frequency converter output frequency near blade, cause blade produce resonance or produce larger heat and damaged blade in torture test.
Below introduce the course of work of the present invention: at first before test according to the test specification of concrete tested blade, determine the needed load loading position of tested blade and the configuration corresponding sensitive spot the strain testing passage, blades installation, on flapwise or edgewise direction, is then installed to corresponding tired exciting device (being the load exciting device) and static counterweight, after installation, test and determine the natural frequency of tested blade, according to the natural frequency of tested blade, set at frequency converter and automatic control on monitoring modular the reference frequency output that limits frequency converter respectively, then start frequency converter by automatically controlling monitoring modular, and the output frequency of the frequency converter that progressively raises, the repeated strain of each sensitive spot under Real-time Collection and the corresponding exciting force of demonstration, after once the strain of each sensitive spot reaches Theoretical Design repeated strain design load, lock the output frequency of frequency converter, simultaneously, starting the Vibrating Load of automatically controlling in monitoring modular adjusts automatically, report to the police and stopping function, now, tired certification test will carry out according to normal program, once unexpected shutdown the in the torture test process, the experimenter will be according to the repeated strain of the stored waveform of two hours and regularly storage just, negative peak, judge the reason of termination test, in the reason that finds termination test and after doing respective handling, can enough restart tired certification test.

Claims (6)

1. the tired certification test test control system of blade of wind-driven generator, is characterized in that, described test control system comprises:
-testing table, described testing table is for installing tested blade;
-load exciting device, described load exciting device is for applying dynamic Fatigue Testing Loads to tested blade, and the excited frequency of load exciting device is by Frequency Converter Control;
-foil gauge, described foil gauge is a plurality of, and each foil gauge is self-temperature-compensated strain ga(u)ge, and a plurality of foil gauges are located at respectively on each sensitive spot of tested blade, for detection of the repeated strain value of tested blade each sensitive spot under Fatigue Testing Loads;
-bridge-type strained handling device, the repeated strain signal data that described bridge-type strained handling device arrives for the treatment of all strain measurements; Bridge-type strained handling device comprises shunting calibration module ,Qiao road temperature compensation module and the strain value module that makes zero, and described shunting calibration module for recalibrating the sensitivity of foil gauge, to eliminate the impact of stube cable on foil gauge sensitivity before test; Described bridge road temperature compensation module is for the error of the linear expansion coefficient between compensate for ambient temperature variation and foil gauge and tested blade material, to realize round-the-clock tested blade being carried out to torture test; The module that makes zero described strain value makes zero for the strain initial value by tested blade;
-high-speed synchronous data acquiring card, described high-speed synchronous data acquiring card becomes digital signal for foil gauge analog signal conversion that bridge-type strained handling device is obtained, and high-speed synchronous collection and keep these signal datas, and these signal datas are flowed to computing machine;
-computing machine, be equipped with automatic control monitoring modular and testing data processing module in described computing machine, real-time testing strain signal data and design load that described automatic control monitoring modular transports the high-speed synchronous data acquiring card are contrasted, within judging with this whether the test strain value is in the scope of design load, if, the exciting force that shows the current output of load exciting device meets the torture test requirement, keep current excited frequency and the eccentric weight quality of load exciting device, if not, the exciting force that shows the current output of load exciting device need to be regulated change, automatically control monitoring modular and send the frequency change control signal that raises or reduce according to comparing result to frequency converter, the frequency of exporting by frequency converter changes the excited frequency of the tested blade of load exciting device exciting, if after the excited frequency that changes the load exciting device, the real-time testing strain signal data that the high-speed synchronous data acquiring card collects have still exceeded the design load scope or have reached setting dangerous values scope, automatically control monitoring modular and export stopping signal to frequency converter, the action of Ending Load exciting device, described testing data processing module, for the treatment of the voltage signal data of foil gauge output, converts the compliance voltage signal data to actual strain measurement value,
-storer, described storer is for storing the measuring-signal data of foil gauge output;
-display, described display is used for showing the measured value of foil gauge output signal after treatment and excited frequency and the fatigue life cycle of current tested blade.
2. the tired certification test test control system of blade of wind-driven generator according to claim 1, is characterized in that, is set with frequency conversion higher limit and frequency conversion lower limit in described frequency converter.
3. the tired certification test test control system of blade of wind-driven generator according to claim 1, is characterized in that, described automatic control monitoring modular is natural frequency that tested blade is tested to the frequency conversion value of frequency converter output 80~95%.
4. the tired certification test test control system of blade of wind-driven generator according to claim 1, it is characterized in that, described load exciting device mainly consists of reductor and eccentric weight exciting agency, the load exciting device is fixed on tested blade by fixture, the reductor of load exciting device drives the action of eccentric weight exciting agency, and the exciting force of eccentric weight exciting agency passes to tested blade by fixture.
5. the tired certification test test control system of blade of wind-driven generator according to claim 1, is characterized in that, the temperature self-compensation ambient temperature range of described foil gauge is-20~40 ℃.
6. according to the tired certification test test control system of the described blade of wind-driven generator of claim 1 or 5; it is characterized in that; described foil gauge is by the room temperature fast-curing glue on the sensitive spot of tested blade, and the exposed surface of foil gauge scribbles the protective finish of waterproof and dustproof.
CN201310384216.8A 2013-08-29 2013-08-29 Blade of wind-driven generator fatigue certification test test control system Active CN103472741B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310384216.8A CN103472741B (en) 2013-08-29 2013-08-29 Blade of wind-driven generator fatigue certification test test control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310384216.8A CN103472741B (en) 2013-08-29 2013-08-29 Blade of wind-driven generator fatigue certification test test control system

Publications (2)

Publication Number Publication Date
CN103472741A true CN103472741A (en) 2013-12-25
CN103472741B CN103472741B (en) 2016-09-14

Family

ID=49797632

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310384216.8A Active CN103472741B (en) 2013-08-29 2013-08-29 Blade of wind-driven generator fatigue certification test test control system

Country Status (1)

Country Link
CN (1) CN103472741B (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104019968A (en) * 2014-05-20 2014-09-03 北京航空航天大学 Testing system for testing fatigue performance of propeller blades
CN104330317A (en) * 2014-10-31 2015-02-04 西安交通大学 High-temperature and high-cycle compound fatigue test platform for turbine blade
CN104374651A (en) * 2014-10-31 2015-02-25 国家电网公司 Device and method for detecting transformer substation post insulator strength
CN105784274A (en) * 2014-12-16 2016-07-20 中材科技风电叶片股份有限公司 Large-sized vane static test system
CN107061160A (en) * 2017-04-26 2017-08-18 浙江运达风电股份有限公司 It is a kind of that operation safety control method and system are carried based on the wind generator set blade ice that blade loading is detected
CN107941636A (en) * 2017-11-08 2018-04-20 武汉航空仪表有限责任公司 A kind of fatigue life test system and method for helicopter blade electric heating assembly
CN110608138A (en) * 2019-10-21 2019-12-24 南京工业大学 Wind turbine blade real-scale simulation wind power distributed loading test system and operation method
CN111470065A (en) * 2020-04-30 2020-07-31 中国飞机强度研究所 Safety alarm device and method for airplane structural strength test
CN112378998A (en) * 2020-10-26 2021-02-19 北京中科泛华测控技术有限公司 Engine blade natural frequency testing method
CN113532261A (en) * 2021-08-16 2021-10-22 河北工业大学 Strain monitoring system and method
CN113532260A (en) * 2021-07-23 2021-10-22 中国航发贵阳发动机设计研究所 Process for sticking strain gauge by using P-A adhesive
CN114151290A (en) * 2021-11-09 2022-03-08 明阳智慧能源集团股份公司 Wind generating set transmission chain torque testing system and implementation method thereof
CN114279676A (en) * 2021-11-23 2022-04-05 国核电力规划设计研究院有限公司 Sea condition threshold judgment method for strain damage of submarine suspended cable
CN115031948A (en) * 2022-08-10 2022-09-09 常州市宏发纵横新材料科技股份有限公司 Modularized blade fatigue life prediction method and device, control device and storage medium

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040139809A1 (en) * 2003-01-22 2004-07-22 Mitsubishi Heavy Industries, Ltd. Turbine blade fatigue life evaluating method, turbine blade creep elongation strain measuring apparatus, and turbine blade
CN1517691A (en) * 2003-01-22 2004-08-04 三菱重工业株式会社 Estimating method for fatigue life of turbine blade, turbine blade creep elongation strain measurement device and turbine blade
CN1554935A (en) * 2003-12-29 2004-12-15 阎晓军 High frequency preheating treatment technology for high temperature alloy creep/fatique test
CN101949770A (en) * 2010-08-14 2011-01-19 东方电气集团东方汽轮机有限公司 Identifying and testing system of static force of blades of wind driven generator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040139809A1 (en) * 2003-01-22 2004-07-22 Mitsubishi Heavy Industries, Ltd. Turbine blade fatigue life evaluating method, turbine blade creep elongation strain measuring apparatus, and turbine blade
CN1517691A (en) * 2003-01-22 2004-08-04 三菱重工业株式会社 Estimating method for fatigue life of turbine blade, turbine blade creep elongation strain measurement device and turbine blade
CN1554935A (en) * 2003-12-29 2004-12-15 阎晓军 High frequency preheating treatment technology for high temperature alloy creep/fatique test
CN101949770A (en) * 2010-08-14 2011-01-19 东方电气集团东方汽轮机有限公司 Identifying and testing system of static force of blades of wind driven generator

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
尹育聪等: "发动机叶片多功能测控试验系统的实现方法", 《工业控制计算机》, vol. 19, no. 11, 31 December 2006 (2006-12-31), pages 75 - 76 *
李海波等: "风力机叶片动力特性实验台设计", 《热能动力工程》, vol. 27, no. 1, 31 January 2012 (2012-01-31) *

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104019968B (en) * 2014-05-20 2016-06-15 北京航空航天大学 A kind of pilot system testing screw blade fatigue property
CN104019968A (en) * 2014-05-20 2014-09-03 北京航空航天大学 Testing system for testing fatigue performance of propeller blades
CN104330317A (en) * 2014-10-31 2015-02-04 西安交通大学 High-temperature and high-cycle compound fatigue test platform for turbine blade
CN104374651A (en) * 2014-10-31 2015-02-25 国家电网公司 Device and method for detecting transformer substation post insulator strength
CN105784274A (en) * 2014-12-16 2016-07-20 中材科技风电叶片股份有限公司 Large-sized vane static test system
CN107061160A (en) * 2017-04-26 2017-08-18 浙江运达风电股份有限公司 It is a kind of that operation safety control method and system are carried based on the wind generator set blade ice that blade loading is detected
CN107941636A (en) * 2017-11-08 2018-04-20 武汉航空仪表有限责任公司 A kind of fatigue life test system and method for helicopter blade electric heating assembly
CN110608138B (en) * 2019-10-21 2024-02-27 南京工业大学 Wind turbine blade real-scale simulation wind power distributed loading test system and operation method
CN110608138A (en) * 2019-10-21 2019-12-24 南京工业大学 Wind turbine blade real-scale simulation wind power distributed loading test system and operation method
CN111470065A (en) * 2020-04-30 2020-07-31 中国飞机强度研究所 Safety alarm device and method for airplane structural strength test
CN112378998A (en) * 2020-10-26 2021-02-19 北京中科泛华测控技术有限公司 Engine blade natural frequency testing method
CN113532260A (en) * 2021-07-23 2021-10-22 中国航发贵阳发动机设计研究所 Process for sticking strain gauge by using P-A adhesive
CN113532261A (en) * 2021-08-16 2021-10-22 河北工业大学 Strain monitoring system and method
CN114151290A (en) * 2021-11-09 2022-03-08 明阳智慧能源集团股份公司 Wind generating set transmission chain torque testing system and implementation method thereof
CN114151290B (en) * 2021-11-09 2024-01-26 明阳智慧能源集团股份公司 Torque testing system for driving chain of wind generating set and implementation method thereof
CN114279676A (en) * 2021-11-23 2022-04-05 国核电力规划设计研究院有限公司 Sea condition threshold judgment method for strain damage of submarine suspended cable
CN114279676B (en) * 2021-11-23 2024-06-07 国核电力规划设计研究院有限公司 Sea state threshold value judging method for strain damage of submarine suspended cable
CN115031948A (en) * 2022-08-10 2022-09-09 常州市宏发纵横新材料科技股份有限公司 Modularized blade fatigue life prediction method and device, control device and storage medium

Also Published As

Publication number Publication date
CN103472741B (en) 2016-09-14

Similar Documents

Publication Publication Date Title
CN103472741A (en) Control system for fatigue certification experimental test on blades of wind turbine
CN107223206B (en) Fatigue test
US10371123B2 (en) Methods and systems for detecting wind turbine rotor blade damage
CN101839216B (en) Intelligent blade of wind power generator with strain sensors
CN102607831A (en) Evaluation method for fatigue damage and service life of horizontal axis wind turbine blade
US20150354402A1 (en) Detecting blade structure abnormalities
CN203365124U (en) Full-dimension test system and platform for megawatt-level blower fan blade
EP2390501A3 (en) Method and system for validating wind turbine
CN101949770B (en) Identifying and testing system of static force of blades of wind driven generator
US20160161538A1 (en) Method for testing dynamic model parameters of wind power plant
CN108333446A (en) Super capacitor detection method based on variable propeller pitch control
ES2902395T3 (en) A method for handling subsynchronous resonances
CN103455028B (en) A kind of control system of wind turbines PID link static test and method of calibration
CN105717450B (en) The appraisal procedure of pitch drive ability during a kind of low voltage crossing
US11732696B2 (en) Load sensors in wind turbines
CN112796957B (en) Method, device and equipment for detecting fan blade
CN103217282A (en) Fatigue test method of blade scaling model of horizontal axis wind turbine based on equal-service-life principle
CN106338384B (en) A kind of wind generator set blade Quan Zhanxiang load measurement method
CN116613896B (en) Data acquisition monitoring method based on micro-grid
CN109798226A (en) A kind of Wind turbines tower loading prediction method and system
CN105759159B (en) Wind power plant SVG response time testing system adopting partial pressure adjusting device
CN102831317B (en) A kind of method and apparatus obtaining wind power generating set load data
CN103353576B (en) Based on the photovoltaic module energy output method of measurement of volt-ampere characteristic
CN201852702U (en) Wind generating set load test system meeting IEC61400-13 standard
CN204462695U (en) A kind of control system of wind power equipment securing member vision-based detection

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C41 Transfer of patent application or patent right or utility model
TA01 Transfer of patent application right

Effective date of registration: 20160419

Address after: 618000 Sichuan Province, Deyang city Huashan road two No. 2

Applicant after: DONGFANG ELECTRIC WIND POWER CO., LTD.

Address before: 618000 Jiangxi hi tech Industrial Park, Sichuan, Jinsha Road, No. 666, No.

Applicant before: Dongfang Turbine Co., Ltd., Dongfang Electric Group

C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 618000 2 Huashan South Road, Deyang, Sichuan, 2

Patentee after: Dongfang Electric Wind Power Co.,Ltd.

Address before: 618000 2 Huashan South Road, Deyang, Sichuan, 2

Patentee before: DONGFANG ELECTRIC WIND POWER Co.,Ltd.