CN205027513U - Double -bladed model aerogenerator laboratory bench - Google Patents
Double -bladed model aerogenerator laboratory bench Download PDFInfo
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- CN205027513U CN205027513U CN201520531428.9U CN201520531428U CN205027513U CN 205027513 U CN205027513 U CN 205027513U CN 201520531428 U CN201520531428 U CN 201520531428U CN 205027513 U CN205027513 U CN 205027513U
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Abstract
The utility model provides a double -bladed model aerogenerator laboratory bench. This laboratory bench comprises two blade fan platforms and distribution and control system, two blade fan platforms include wheel hub, change oar mechanism, blade, main shaft, moment of torsion detector, moment of torsion loader, lead electrical slip ring and support frame, the blade is connected with wheel hub through becoming oar mechanism, and the blade passes through the main shaft to be connected with the moment of torsion loader, and torsion -testing appearance and axial force tester are gone into to the cluster on the main shaft, and wheel hub is through leading electrical slip ring realization and outside electric contact, the main shaft sets up on the support frame, distribution and control system comprise power distribution loop and the main control unit, and power distribution loop provides the experimental system all part power supplies, and control system contains main control unit, signal acquisition and communication unit, and main control unit connects signal acquisition and communication unit, signal acquisition and communication unit connection moment of torsion detector. The utility model discloses according to the wind speed of difference, can simulate double -bladed wind generating set's operation, include power to the performance of blade, pneumatic performance, mechanical properties studies.
Description
Technical field
The utility model relates to a kind of twayblade model aerogenerator experiment table system, the twayblade model aerogenerator experiment table of particularly Double-vane wind driven generator Blade Properties research and experimental technique.
Background technology
Energy crisis will seriously affect progress and the development of human society.Unremitting effort is all done in the sustainable development for tapping a new source of energy to maintain the earth in the whole world for this reason.Wind energy is the inexhaustible green energy resources of a kind of mankind, and how to effectively utilize and develop wind energy resources is the direction that scientific circles constantly make great efforts always.
Double-vane wind driven generator has that weight is lighter, volume is less, cost is lower, efficiency is higher, be convenient to the features such as maintenance, will become the developing direction of wind generating technology.Twayblade model aerogenerator experiment table is the experiment porch for Blade Properties research, is to one of fan blade aeroperformance and Study on Mechanical Properties important link.
Carry out Blade Properties research, mostly adopt finite element analysis software to analyze blade construction design, the method belongs to theoretical research, can not reflect power and aeroperformance in fan blade rotation process intuitively, and mechanical performance parameter changes.And directly test on the unit of reality, first be wind power generating set more complicated, comprise generator at blower fan system, pitch-variable system, hydraulic system, yaw system, brake system, gear case, control system etc., and influence each other between each system, such complexity and various system bring great inconvenience to the experiment that Blade Properties detects, and considerably increase cycle and the difficulty of experiment.
Summary of the invention
Utility model object: the utility model provides a kind of twayblade model aerogenerator experiment table and experimental technique, its objective is and solve the research of Double-vane wind driven generator group Blade Properties, and theoretical analysis deficiency, the problems such as field experiment difficulty.
technical scheme: the utility model is achieved through the following technical solutions:
A kind of twayblade model aerogenerator experiment table, is characterized in that: this experiment table is made up of two blade fan platforms and distribution and control system; Two blade fan platforms comprise wheel hub, blade pitch device, blade, main shaft, torque tester, torque loader, conducting slip ring and bracing frame; Blade is connected with wheel hub by blade pitch device, and blade is connected with torque loader by main shaft, main shaft seals in torque tester and axial force tester, and wheel hub realizes getting in touch with external electrical by conducting slip ring; Main shaft is arranged on bracing frame;
Distribution and control system are made up of distribution loop and main control unit, distribution loop provides all parts of experimental system to power, control system comprises master controller, signals collecting and communication unit, master controller connection signal gathers and communication unit, and signals collecting and communication unit connect torque tester.
advantage and effect:
The utility model provides a kind of twayblade model aerogenerator experiment table and experimental technique, and it comprises two blade fan platforms, distribution and control system.
This experiment porch is adapted to Blade Properties research, the function realized according to wind power generating set designs, and by pitch-controlled system, propeller pitch angle regulates, the functions such as load torque loading carry out simulation fan operation, carry out the substantially the same of the effect of testing and actual set.
This experiment table, according to the air dynamic behaviour of actual blower fan, not possessing the laboratory under actual wind field environment and also can simulate the actual condition of blower fan, brings great convenience to the experiment of Double-vane wind driven generator group; Experiment table blade is connected with wheel hub by blade pitch device, and blade pitch device realizes blade 0-90 degree and rotates, and to reach the needs of different operating characteristic, provides great convenience to experimenter.The utility model, can the operation of simulated dual blade wind power generation unit according to different wind speed and directions, and comprise power to the performance of blade, aeroperformance, mechanical property is studied.
accompanying drawing illustrates:
Fig. 1 is fan platform structural representation;
Fig. 2 is system control interface figure;
Fig. 3 is parameter revision surface chart;
Fig. 4 is that unit parameter arranges figure;
Fig. 5 is MANUAL CONTROL mode figure.
embodiment:below in conjunction with accompanying drawing, the utility model is further described:
As shown in Figure 1, the utility model provides a kind of twayblade model aerogenerator experiment table, and this experiment table is made up of two blade fan platforms and distribution and control system; Two blade fan platforms comprise wheel hub 1, blade pitch device 2, blade 3, main shaft 4, torque tester 5, torque loader 6, conducting slip ring 7 and bracing frame 8; Blade is connected with wheel hub by blade pitch device, and blade is connected with torque loader by main shaft, main shaft seals in torque tester and axial force tester, and wheel hub realizes getting in touch with external electrical by conducting slip ring; Main shaft 4 is arranged on bracing frame 8;
Distribution and control system are made up of distribution loop and main control unit, distribution loop provides all parts of experimental system to power, control system comprises master controller, signals collecting and communication unit, master controller connection signal gathers and communication unit, and signals collecting and communication unit connect torque tester 5.
Experiment platform control system researches the performance of blade according to the following steps:
First, experiment table powers on and carries out self-inspection, blade is connected with wheel hub by blade pitch device, make blade pitch device realize blade 0-90 degree to rotate, the wind energy that blade is absorbed passes to torque loader by main shaft, regulate the loading moment of main shaft loader to realize load to regulate, utilize torque tester and axial force tester load that final drive shaft seals in the rotary torque suffered by final drive shaft and axial force detection;
Wheel hub is realized and external electrical is got in touch with by conducting slip ring, under automatic operational mode, experimental system runs control automatically according to the control flow of setting, regulate comprising automatic propeller pitch angle, load torque loads automatically, on the basis of automatic mode torque-power data, manual adjustments becomes propeller angle, the set-point of loading moment regulates;
Observed data can gather display system by man-machine interface, the relevant data of experiment table can be obtained; In whole experimentation, the protection system of experiment table plays device security and experimenter's safety that protection monitors whole parts of experiment table.
The utility model carries out driftage by pitch-controlled system and becomes oar, and the aeroperformance realizing blade detects, and can adjust performance, the generating of low wind, the adjustment of strong wind power and stall performance to the power of blade and analyzes and researches.
Utilize blade absorb wind energy and pass to torque loader by main shaft, regulate the loading moment of main shaft loader to realize load and regulate; Loading moment size can control setting by master control system, realizes at the actual fan operation of situation Imitating without motor.To moment of torsion in experiment table runs, thrust, rotating speed carries out detecting and data being sent to master control system, measures the wheel hub anglec of rotation.
The signal gathered shows with the form of real-time curve by the utility model, and carries out real-time analysis, and record is preserved provides great convenience to Blade Properties analysis and research.
Two blade fan platforms:
(1) pitch-controlled system: by electric signal, control pitch motor action, pitch motor realizes blade 0-90 degree position synchronization control with constant speed.
(2) moment of torsion loads: moment of torsion is loaded and realized by moment of torsion load apparatus, and loading moment size is given by master control system.
(3) moment of torsion detects: detect the torque suffered by main shaft by torque tester, and pass the signal to master control system.
(4) thrust measurement: thrust signal is sent to master control system by sensor.
(5) driftage function: bottom tower cylinder, manual rotation regulates and realizes driftage function.
(6) Rotating speed measring: detect the speed of mainshaft by speed probe, passes the signal to master control system
(7) wheel hub rotation angle measurement
Distribution and control system:
Distribution and control system are made up of distribution loop and main control unit, and distribution loop provides all parts of experimental system to power, and comprises 220V busbar electric distribution system and 24V circuit distribution system etc.Control system comprises master controller, signals collecting and communication unit, logic control and defencive function.Implementation method:
(1) automatic operational mode
Under automatic operational mode, experimental system runs control automatically according to the control flow of setting, regulates comprising automatic propeller pitch angle, and load torque such as to load automatically at the function.
Automatic control flow chart is as follows:
(2) manual mode of operation
System, under manual mode of operation, completes following functions: on the basis of automatic mode torque-power data, and manual adjustments becomes propeller angle, the set-point of loading moment regulates.
Be connected with wheel hub by blade pitch device with reference to Fig. 1 blade, blade pitch device realizes blade 0-90 degree and rotates, the wind energy that blade absorbs passes to torque loader by main shaft, regulate the loading moment of main shaft loader to realize load to regulate, final drive shaft seals in torque tester and axial force tester, and load detects the rotary torque suffered by final drive shaft and axial force.Wheel hub and external electrical are got in touch with and being realized by conducting slip ring.
Simatic WINCC configuration software is adopted with reference to figure 2 monitoring of toolss and function software.By man-machine interface, carry out unit parameter setting and comprise startup propeller pitch angle, start maximum (top) speed, rated speed, maximum (top) speed, become oar setting parameter, rotational speed and torque setting dispatch control system operational mode.By man-machine interface and data acquisition display unit Real-time Collection wind speed, rotating speed, torque, blade angle, the data such as thrust, position angle, adjustment rotating speed or torque, curve display wind speed, rotating speed, torque, blade angle, the change of the data such as thrust, position angle and trend.Real time record and the analysis of historical data are derived.
Revising function with reference to figure 3 unit parameter is carry out initialization check and correction to unit various kinds of sensors numerical value.Comprise and become the correction of oar zero angle, crab angle angle value sets, and sensor parameters corrects, position angle trigger angle setting etc.
Be used to reference to figure 4 unit parameter table some special parameters setting unit, comprise start-up parameter setting, operating parameter setting, become oar setting parameter, rotary speed-torque setting etc.
With reference to figure 5 in a manual mode, can to unit propeller pitch angle, manual adjustments is carried out in torque.
The utility model realizes pitch-controlled system by the action controlling pitch motor, simulates wind wheel characteristic.Utilize moment of torsion load apparatus to realize moment of torsion to load, also the actual working characteristics of wind power generating set can be simulated in the laboratory not possessing actual wind field environment, utilize the real time signal aquisition of man-machine interface, real-time curve shows, and achieves the performance study to twayblade fan blade, and especially the aeroperformance of blade detects, can to the power adjustment performance of blade, low wind generating, strong wind power adjusts, and stall performance is analyzed and researched.
Claims (1)
1. a twayblade model aerogenerator experiment table, is characterized in that: this experiment table is made up of two blade fan platforms and distribution and control system; Two blade fan platforms comprise wheel hub (1), blade pitch device (2), blade (3), main shaft (4), torque tester (5), torque loader (6), conducting slip ring (7) and bracing frame (8); Blade is connected with wheel hub by blade pitch device, and blade is connected with torque loader by main shaft, main shaft seals in torque tester and axial force tester, and wheel hub realizes getting in touch with external electrical by conducting slip ring; Main shaft (4) is arranged on bracing frame (8);
Distribution and control system are made up of distribution loop and main control unit, distribution loop provides all parts of experimental system to power, control system comprises master controller, signals collecting and communication unit, master controller connection signal gathers and communication unit, and signals collecting and communication unit connect torque tester (5).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520531428.9U CN205027513U (en) | 2015-07-21 | 2015-07-21 | Double -bladed model aerogenerator laboratory bench |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520531428.9U CN205027513U (en) | 2015-07-21 | 2015-07-21 | Double -bladed model aerogenerator laboratory bench |
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| CN205027513U true CN205027513U (en) | 2016-02-10 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105181307A (en) * | 2015-07-21 | 2015-12-23 | 沈阳华人风电科技有限公司 | Double-blade model wind driven generator experimental table and experimental method |
| CN106441903A (en) * | 2016-09-28 | 2017-02-22 | 内蒙古工业大学 | Experiment research device for dynamic characteristics of horizontal axis composite wind turbine blade |
-
2015
- 2015-07-21 CN CN201520531428.9U patent/CN205027513U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105181307A (en) * | 2015-07-21 | 2015-12-23 | 沈阳华人风电科技有限公司 | Double-blade model wind driven generator experimental table and experimental method |
| CN106441903A (en) * | 2016-09-28 | 2017-02-22 | 内蒙古工业大学 | Experiment research device for dynamic characteristics of horizontal axis composite wind turbine blade |
| CN106441903B (en) * | 2016-09-28 | 2018-06-12 | 内蒙古工业大学 | A kind of trunnion axis wind machine's laminae made from composite material study dynamic properties device |
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