CN110221232A - Stack formula ultra-magnetic deformation actuator characteristic test system - Google Patents
Stack formula ultra-magnetic deformation actuator characteristic test system Download PDFInfo
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- CN110221232A CN110221232A CN201910584949.3A CN201910584949A CN110221232A CN 110221232 A CN110221232 A CN 110221232A CN 201910584949 A CN201910584949 A CN 201910584949A CN 110221232 A CN110221232 A CN 110221232A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R33/00—Arrangements or instruments for measuring magnetic variables
- G01R33/12—Measuring magnetic properties of articles or specimens of solids or fluids
- G01R33/18—Measuring magnetostrictive properties
Abstract
The invention discloses one kind to stack formula ultra-magnetic deformation actuator characteristic test system, including test with formula ultra-magnetic deformation actuator is stacked, and pressure sensor is installed on the fixing end of ultra-magnetic telescopic module in the actuator；Magnetic field strength transducer includes hall probe and the matched gaussmeter used, and the hall probe is tightly attached to the GMM rod surface of ultra-magnetic telescopic module；Magnetic induction search coil is wound in the outside of the GMM rod；Temperature probe is mounted on the middle part of the ultra-magnetic telescopic module, for measuring the temperature of the ultra-magnetic telescopic module；Strain gauge adhesion is on the GMM rod surface, for incuding the dependent variable of the GMM rod；Laser displacement sensor is oppositely arranged with the test with stacking power output rod in formula ultra-magnetic deformation actuator.The system can obtain stacking the regularity of distribution of each state parameter and the basic output characteristics for stacking formula ultra-magnetic deformation actuator in the work of formula ultra-magnetic deformation actuator, provide reference and foundation for the modeling of subsequent actuator and control.
Description
Technical field
The super mangneto of formula is stacked the present invention relates to ultra-magnetic deformation actuator test device technical field more particularly to one kind to stretch
Contracting actuator characteristics test macro.
Background technique
With the continuous development of material science, novel intelligent material is gradually applied to electrohydraulic servo valve EHSV.As intelligence
Can material family important a member, Giant Magnetostrictive Materials have excellent performance indicator, for example stagnant ring is small, Ying Bian great, defeated
Big, energy density height of power output etc..High performance servo valve ultra-magnetic deformation actuator is developed using these good characteristics of GMM
GMA, for promoting the static and dynamic performance of EHSV, the application field for expanding EHSV is significant.Stack the cause of formula ultra-magnetic telescopic
The structure type that dynamic device SGMA is arranged alternately using permanent magnet and GMM rod, so as to effectively improve the uniformity of bias, simultaneously
The bulky deficiency of tubular permanent magnet quality is overcome, but due to the Distribution of Magnetic Field of the different SGMA of bias applying mode rule
There is larger difference with Traditional GM A, it is therefore desirable to which finding one kind can be to the system that SGMA is tested.
Summary of the invention
Technical problem to be solved by the invention is to provide the distributions that one kind can obtain each state parameter in SGMA work
The basic output characteristics of rule and SGMA stacks the super mangneto of formula for what the modeling of subsequent actuator and control provided reference and foundation
Expansion actuator characteristic test system.
In order to solve the above technical problems, the technical solution used in the present invention is: one kind stacks the actuating of formula ultra-magnetic telescopic
Device characteristic test system, it is characterised in that: including testing with formula ultra-magnetic deformation actuator is stacked, pressure sensor is installed on institute
The fixing end for stating ultra-magnetic telescopic module in actuator, for measuring prestressing force suffered by GMM rod in ultra-magnetic telescopic module；Magnetic
Field intensity sensor includes hall probe and the matched gaussmeter used, and the hall probe is tightly attached to ultra-magnetic telescopic mould
The GMM rod surface of block, for measuring the magnetic field strength near GMM rod surface, the numerical value of measurement sends the gaussmeter to；Magnetic strength
Search coil is answered to be wound into the outside of the GMM rod, for measuring the intensity of magnetization in GMM rod；Temperature probe is mounted on described
The middle part of ultra-magnetic telescopic module, for measuring the temperature of the ultra-magnetic telescopic module；Strain gauge adhesion is in the GMM rod table
Face, for incuding the deformation quantity of the GMM rod；Laser displacement sensor and the test are with stacking formula ultra-magnetic deformation actuator
Middle power output rod is oppositely arranged, for measuring the displacement of the actuator.
A further technical solution lies in: the test includes ultra-magnetic telescopic mould with the formula ultra-magnetic deformation actuator of stacking
Block, the ultra-magnetic telescopic module include permanent magnet, GMM rod and driving coil component, and the permanent magnet is arranged there are three more than,
A GMM rod, the stick that the driving coil component is located at the permanent magnet and GMM rod is constituted are provided between every two permanent magnet
The outside of shape structure；The left side of leftmost side permanent magnet is connect by the pressure sensor with left end cap, described in the rightmost side forever
The right side of magnet is connect with the medial end of the power output rod, and the outboard end of the power output rod is stretched from right end cap
Out, the movable end of the laser displacement sensor and the power output rod is oppositely arranged；The right end cap and the rightmost side are forever
It is arranged with reset spring on power output rod between magnet, the one end for connecting sleeve is fixedly connected with the left end cap, connection
The other end of sleeve is fixedly connected with the right end cap, and the connection sleeve is located at the outside of the driving coil component.
A further technical solution lies in: the test further includes clamping device with the formula ultra-magnetic deformation actuator of stacking,
The left end cap is fixedly connected with the clamping device.
A further technical solution lies in: the test macro further includes data collecting card and main control computer, the pressure
The signal output end of force snesor is connect with the signal input part of the data collecting card, for sending the information of acquisition to institute
It states data collecting card to be handled, treated pressure information sends the main control computer to by data collecting card.
A further technical solution lies in: the signal input of the signal output end and the data collecting card of the gaussmeter
End connection, is handled, treated, and magnetic field strength information passes through for sending the information of acquisition to the data collecting card
Data collecting card sends the main control computer to.
A further technical solution lies in: the signal output end of the foil gauge passes through the input of the signal of electric bridge and deformeter
End connection, the signal output end of the deformeter are connect with the signal input part of the data collecting card, the letter for will acquire
Breath sends the data collecting card to and is handled, and treated strain information sends the master control meter to by data collecting card
Calculation machine.
A further technical solution lies in: the signal output end of the temperature probe and the signal input part of temperature transmitter
Connection, the signal output end of the temperature transmitter is connect with the signal input part of the data collecting card, for what will be acquired
Information sends the data collecting card to and is handled, and treated temperature information sends the master control to by data collecting card
Computer.
A further technical solution lies in: the driving signal output end of the data collecting card and the signal of power amplifier
Input terminal connection, the signal output end of the power amplifier connect with the both ends of the driving coil component coil, are used for
Working power is provided for the coil, voltage measurement module and current measurement mould are provided on the conducting wire of power amplifier output
Block, for measuring the output electric current and output voltage of the power amplifier, the voltage measurement module and current measurement module
Signal output end connect with the signal input part of the data collecting card, adopted for sending the information of acquisition to the data
Truck is handled, and treated electric current and information of voltage send the main control computer to by data collecting card.
A further technical solution lies in: the driving coil component includes driving coil and coil rack, the driving
Coil is wound on the coil rack.
A further technical solution lies in: the miniature pressure of DYHW-116 type that the pressure sensor is sensed using Bangbu ocean
Formula sensor；Magnetic field strength transducer uses CH-1600 type magnetic field strength transducer；The foil gauge uses Air China's electrical measurement
BA120-3AA type foil gauge, the STT-FB3 type chip temperature that temperature probe is insulted using match hundred million.
The beneficial effects of adopting the technical scheme are that the test macro is using data collecting card as core,
By configuring multiple sensors, the real time monitoring of achievable a running parameters more to SGMA.On this basis, GMM characteristic is carried out
Experiment and actuator characteristics experiment.By GMM characteristic test, the basic performance indices of material therefor are obtained, determine that actuator is set
The basic parameter of meter；It is tested by actuator characteristics, obtains the regularity of distribution of each state parameter and the base of SGMA in SGMA work
This output characteristics provides reference and foundation for the modeling of subsequent actuator and control.
Detailed description of the invention
The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is the functional block diagram of system described in the embodiment of the present invention；
Fig. 2 is the functional block diagram of software in system described in the embodiment of the present invention；
Fig. 3 is data acquisition module surface chart in system described in the embodiment of the present invention；
Fig. 4 is data readback surface chart in system described in the embodiment of the present invention；
Fig. 5 is data processing module surface chart in system described in the embodiment of the present invention；
Wherein: 1, pressure sensor；2, GMM rod；3, hall probe；4, magnetic induction search coil；5, temperature probe；6, it strains
Piece；7, laser displacement sensor；8, permanent magnet；9, driving coil component；10, left end cap；11, power output rod；12, right end
Lid；13, reset spring；14, sleeve is connected；15, clamping device.
Specific embodiment
With reference to the attached drawing in the embodiment of the present invention, technical solution in the embodiment of the present invention carries out clear, complete
Ground description, it is clear that described embodiment is only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
In the following description, numerous specific details are set forth in order to facilitate a full understanding of the present invention, but the present invention can be with
Implemented using other than the one described here other way, those skilled in the art can be without prejudice to intension of the present invention
In the case of do similar popularization, therefore the present invention is not limited by the specific embodiments disclosed below.
GMM characteristic test demand:
GMM shows complicated constitutive bchavior at work, for the accurate performance indexes for grasping material, actuator is instructed to set
Meter and production, need to analyze the magnetics of material, mechanics, thermodynamic behaviour comprehensively by test experiments.Influence GMM mangneto
The factor of dilatation mainly includes magnetic field strength, prestressing force, temperature and driving magnetic field frequency.It, will be real in GMM characteristic test
It tests and is divided into three, investigate the influence of prestressing force, temperature and driving magnetic field frequency to GMM magnetostrictive strain respectively.
1) under different prestressing force material magnetostrictive strain measurement.Correlative study shows under suitable prestressing force
GMM rod is deformed with maximum magnetostriction.Therefore, the purpose of this experiment is exactly to pass through test and find suitable prestressing force to take
Value, improves the output displacement of GMA.
2) under different temperatures material magnetostrictive strain measurement.Under the conditions of determining suitable prestressed, change GMM
Operating temperature, temperature can be obtained to the influence curve of GMM magnetostrictive strain.By curve, it is defeated to GMA temperature change can be calculated
The influence of precision out, and then suitable temperature control system is designed, improve actuator output accuracy.
3) under different driving frequency material magnetostrictive strain measurement.When GMM works in high-frequency alternating magnetic field, material
Material is internal to generate apparent eddy current effect, increase the energy loss of material internal.So being tested by this item, research material
Magnetostriction deformation under different frequency, facilitates the dynamic output characteristic for predicting GMA, designs its reasonable working band.
In addition to above three factor, magnetic field strength also will affect the magnetostrictive strain of material, with magnetic field strength
Increase, the magnetostriction of GMM deformation is gradually increased, and presence phenomena such as due to dead zone, saturation, and corresponding between them is closed
It is and non-linear.Influence of the magnetic field strength to GMM magnetostrictive strain is studied, for determining the ideal operation section of GMA, is improved
Its output performance has greater significance.Due to having depicted magnetic field strength-magnetostrictive strain in first item and Section 3 experiment
Curve, it is determined that influence of the magnetic field strength to magnetostrictive strain, therefore no longer this is individually studied and discussed.
Actuator characteristics test demand:
The structure type that SGMA uses permanent magnet-GMM rod to be arranged alternately, different with Traditional GM A, such structure facilitates
Actuator obtains more uniform bias magnetic field.But the Distribution of Magnetic Field that special structure also leads to SGMA is different from tradition
GMA, and then lead to the difference of the distribution of the SGMA intensity of magnetization, Strain Distribution and final output characteristic.Special knot based on SGMA
Structure studies the overall permanence of actuator by experiment comprehensively, and content specifically includes that
1) SGMA magnetic field strength, the intensity of magnetization and Strain Distribution research.Magnetic field strength, the intensity of magnetization, strain are SGMA worked
Three important intermediate variables and SGMA are different from the important parameter of Traditional GM A in journey.Pass through these three changes of experiment measurement
Amount, accurately understands its characteristic distributions, can provide foundation for the modeling and optimization of SGMA.
2) SGMA power output and output displacement research.Power output and output displacement are the most direct of measurement GMA output characteristics
With most critical index, the main purpose of this item experiment is by the output performance of the measurement verifying SGMA of this two indexs, simultaneously
Verify the design method and Modeling Theory of actuator.
Actuator controls experiment demand: on the basis of GMM characteristic test and actuator characteristics are tested, by system
Transformation and expansion, it is desirable to be able to complete SGMA control experiment.By different control strategy embedded systems, its control effect is tested, is looked for
To ideal SGMA control method, the high-precision servo control of SGMA is realized.
Other reserved experiment demands: in addition to above-mentioned experiment, designed test macro should be able to be in the SGMA course of work
Each relevant variable parameter carries out overall monitor, convenient for the analysis and research of the part and overall work characteristic SGMA.
Overall, as shown in Figure 1, the embodiment of the invention discloses one kind to stack formula ultra-magnetic deformation actuator characteristic test
System, the system can be divided into four parts: acquisition control system, power-supply system, sensor-based system and actuator system.Acquisition control
System is the maincenter and core of entire test macro, mainly includes main control computer and data collecting card (data
Acquisition card, DAQ), DAQ is connected with computer, the data information that responsible receiving sensor is passed back, and output calculates
The control signal that machine issues.Independently developed experiment test software is run in computer, software is in Labwindows/CVI platform
Lower exploitation can cooperate DAQ to realize real-time acquisition, storage, display and the analysis of experimental data, and monitor whole experiment process.
The chief component of power-supply system is power amplifier, can amplify the control signal of capture card output, provide not for actuator
With the drive waveforms of form.Sensor-based system mainly includes various sensor and corresponding signal condition equipment, for testing
Each characteristic parameter of SGMA is acquired in journey, and is translated into measurable voltage signal.Actuator system is that the test designed is used
SGMA is the object of test system and test.
Further, described to stack formula ultra-magnetic deformation actuator characteristic test system, including the test super magnetic of the formula that stacks
Expansion actuator is caused, pressure sensor 1 is installed on the fixing end of ultra-magnetic telescopic module in the actuator, for measuring super magnetic
Cause prestressing force suffered by GMM rod 2 in flexible module；Magnetic field strength transducer includes hall probe 3 and the matched height used
This meter, the hall probe 3 is tightly attached to 2 surface of GMM rod of ultra-magnetic telescopic module, for measuring the magnetic near 2 surface of GMM rod
Field intensity, the numerical value of measurement send the gaussmeter to；Magnetic induction search coil 4 is wound into the outside of the GMM rod 2, is used for
Measure the intensity of magnetization in GMM rod 2；Temperature probe 5 is mounted on the middle part of the ultra-magnetic telescopic module, described super for measuring
The temperature of magnetostriction module；Foil gauge 6 is pasted onto 2 surface of GMM rod, for incuding the deformation quantity of the GMM rod 2；Swash
Optical displacement sensor 7 is oppositely arranged with the test with stacking power output rod in formula ultra-magnetic deformation actuator, for measuring
The displacement of the actuator.
Further, the test includes ultra-magnetic telescopic module with the formula ultra-magnetic deformation actuator of stacking, the super magnetic
Causing flexible module includes permanent magnet 8, GMM rod 2 and driving coil component 9；The setting of permanent magnet 8 is there are three more than, every two
A GMM rod 2 is provided between permanent magnet 8, the driving coil component 9 is located at the stick that the permanent magnet 8 is constituted with GMM rod 2
The outside of shape structure；The left side of leftmost side permanent magnet 8 is connect by the pressure sensor 1 with left end cap 10, rightmost side institute
The right side for stating permanent magnet 9 is connect with the medial end of the power output rod 11, the outboard end of the power output rod 11
Portion is stretched out from right end cap 12, and the movable end of the laser displacement sensor 7 and the power output rod 11 is oppositely arranged；The right side
Be arranged with reset spring 13 on power output rod between end cap 12 and the permanent magnet of the rightmost side 8, connect one end of sleeve 14 with
The left end cap 10 is fixedly connected, and the other end of connection sleeve 14 is fixedly connected with the right end cap 12, and the connection sleeve
14 are located at the outside of the driving coil component 9.The driving coil component 9 includes driving coil and coil rack, the drive
Moving winding is wound on the coil rack；The left end cap 10 is fixedly connected with the clamping device 15.
It further, can be using three sections of GMM rods and four sections of set of permanent magnets at magnetostriction module in actuator.By
Test content it is found that need to measure the parameters such as the magnetic field strength of different location, magnetic induction intensity, strain in GMM rod in an experiment,
Therefore GMM rod needs enough length and surface area installation testing element.Four measurement points are chosen in every section of GMM rod, are
The interference of testing element between different measurement points is avoided, the bar that diameter is 16mm is chosen, every segment length is 33mm；Permanent magnet diameter
Equal with GMM rod diameter, every segment length is 6mm.
Further, the signal output end of the pressure sensor 1 is connect with the signal input part of the data collecting card,
It is handled for sending the information of acquisition to the data collecting card, treated, and pressure information is passed by data collecting card
Give the main control computer.Pressure sensor is installed on the fixing end of magnetostriction module, pre- suffered by GMM rod for measuring
Stress.The miniature press type sensor of DYHW-116 type that pressure sensor selects Bangbu ocean to sense, the type sensor have size
Small feature, suitable for size-constrained measurement occasion, range ability is lower than 0.5% up to 1000kg, measurement error.
Magnetic field strength transducer includes hall probe and matched gaussmeter, model CH-1600.Hall probe is tight
It is affixed on GMM rod surface, the magnetic field strength near stick surface can be measured, numerical value is shown by the liquid crystal display panel on gaussmeter, simultaneously
DAQ can also be transferred to by signal wire.
Magnetic induction intensity sensor uses the magnetic induction search coil of voluntarily coiling, and measuring principle can use faraday's electromagnetism
Incude theorem description, indicate are as follows:
In formula,NFor number of inductive coil turns,AFor induction coil cross-sectional area,ε(t) it is the induced electromotive force that coil both ends generate.
It should be noted that including integral element in above formula, this process is realized, be generally divided into two steps in an experiment, it is first real
Then the induced voltage that Shi Jilu coil generates completes the solution of integral element using integrator.Obtaining magnetic induction intensity
On the basis of, the intensity of magnetization in GMM rod can be calculated:
In formula,μ 0For space permeability,HFor magnetic field strength corresponding in GMM rod.
The signal output end of the gaussmeter is connect with the signal input part of the data collecting card, the letter for will acquire
Breath sends the data collecting card to and is handled, and magnetic field strength information that treated sends the master to by data collecting card
Control computer.
The signal output end of the foil gauge 6 is connected by the signal input part of electric bridge and deformeter, the deformeter
Signal output end is connect with the signal input part of the data collecting card, is acquired for sending the information of acquisition to the data
Card is handled, and treated strain information sends the main control computer to by data collecting card.Foil gauge selects " Air China
The BA120-3AA type foil gauge of electrical measurement " production, paste position is as in Figure 2-4, and structure size is 6.4mm × 3.5mm, electricity
Resistance value is 120 Ω.Meanwhile have the function of temperature self-compensation, can dynamic strain within 150 DEG C of precise measurement, highest test
Frequency is higher than 1kHz.
The signal output end of the temperature probe 5 and the signal input part of temperature transmitter connect, the temperature transmitter
Signal output end connect with the signal input part of the data collecting card, adopted for sending the information of acquisition to the data
Truck is handled, and treated temperature information sends the main control computer to by data collecting card.Chip temperature installation
Among magnetostriction module, model STT-FB3(production firm be match hundred million insult), can -50 DEG C of precise measurement ~ 200 DEG C it
Between temperature range, precision be 0.1 DEG C.Sensor signal can be changed into voltage signal by cooperation temperature transmitter, facilitate DAQ's
Data acquisition.
In addition, as shown in Figure 1, the driving signal output end of the data collecting card and the signal input part of power amplifier
Connection, the signal output end of the power amplifier are connect with the both ends of the driving coil component coil, for being described
Coil provides working power, is provided with voltage measurement module and current measurement module on the conducting wire of power amplifier output, uses
In the output electric current and output voltage that measure the power amplifier, the signal of the voltage measurement module and current measurement module
Output end is connect with the signal input part of the data collecting card, for by the information of acquisition send to the data collecting card into
Row processing, treated electric current and information of voltage send the main control computer to by data collecting card.
The TA189, output sensitivity 100mV/ of model " Pico electronics " production of current clamp (current measurement module)
A, range are 5mA ~ 30A, and measurement error is lower than 1%.In measurement without cutting, removing or break line, by the input line of SGMA
Across current clamp jaw, driving current value in actuator can be measured.
Displacement sensor selects MicrotrakTM3-LTS-025-02 type laser displacement inductor, the type sensor combine most
New CMOS induction technology, is capable of the change in displacement of precise measurement testee, and measurement sensitivity is 0.25 μm/mV, resolution ratio
It is 0.038 μm, measurement frequency range is 0 ~ 20kHz.
Different from the load cell inside SGMA, piezoelectric force transducer is mounted on the outside of actuator, is contacted with output rod,
For measuring the power output of SGMA.Sensor model number is the DHL050 of " Jiangsu east China test " production, dynamometry range is 0 ~
5000N, sensitivity 3.06pC/N, it is non-linear in measurement process to be lower than 1%.
The effect of power amplifier is so that coil is obtained sufficiently large drive the weak drive signals amplification of capture card output
Streaming current.The model GF-800(production firm that power amplifier is selected is Yangzhou Radio No.2 Factory), peak power output is
800W, maximum are 30A by electric current.
DAQ is the core component of SGMA test macro, and major function includes multi channel signals synchronous acquisition and control letter
Number output.According to design requirement, system needs to complete multinomial experiment, wherein acquiring the most experiment of signal includes No. 10 sensors
Signal.The highest test frequency of SGMA is set as 500Hz, by sampling thheorem it is found that if desired complete recurrence system state, sampling
Frequency should be not less than 20 times of its working frequency, and therefore, the sample rate of DAQ should be higher than that 100kS/s.DAQ selects " American National instrument
The PXIe-6361 of device company (National Instruments, NI) " production, it includes the input of 16 tunnel analog signals and 2 tunnels
Analog signal output, sampling precision are 16, and maximum sampled voltage is ± 10V, and multichannel maximum sample rate is 2MS/s, can
Meet the sample requirement of test macro.
Main control computer selects the Precision work station of Dell, embeds six core E5 processors, and 32G RAM has powerful
Calculated performance, suitable for test macro data storage, analysis and processing.
On the basis of hardware design, need to design and write SGMA testing system software, realize sensing data acquisition,
Storage, processing and analysis.Labwindows/CVI is a virtual instrument development platform based on ANSI C that NI company releases,
Its programming mode is powerful, convenient, flexible based on C language, in combination with the function library of abundant profession, to be familiar with C language
Developer's exploitation data acquisition of speech, analysis, control software provide an ideal platform.MATLAB is a powerful
Numerical value software for calculation has the characteristics that simple interface, programming are convenient, and includes powerful function and tool box, especially fits
It shares in mathematical computations and analysis.Using modularization programming thought software design, using Labwindows/CVI and
MATLAB hybrid programming writes testing system software, realizes the combination and mutual supplement with each other's advantages of both softwares.
System software overall framework: testing system software needs to realize SGMA characteristic test with hardware system cooperation.Specifically
For, need system can long-time stable acquisition, store and show sensor signal, the online processing for completing signal, such as frequency
Domain is shown, coordinate transforming is shown, simply filtering processing etc..After the completion of data acquisition, the data of acquisition can be played back, and root
According to need to screen data, filter, numerical value calculates and analysis.Fig. 2 is testing system software frame diagram, soft according to function
Part system can be divided into three modules: data acquisition module, data readback module and data processing module.Each module all has solely
Vertical interface, it is interrelated by main program menu between each interface, so that software has preferable operability, it is also beneficial to simultaneously
The update and expansion of software function.In the following, by the function of three modules and implementation method are specifically introduced respectively.
Data acquisition module: data acquisition module is most basic and most important functional module in testing system software, main
It is responsible for the acquisition, storage and display of sensing data, function is similar with the acquisition equipment that oscillograph etc. is traditional, substantially traditional
The virtualization of instrument.Therefore the module is not related to complicated calculating and analysis can individually be opened by Labwindows/CVI platform
Hair.Fig. 3 is data acquisition module interface.
In data acquisition module, the function of communicating submodule is that hardware communications are realized with DAQ, and DAQ is collected
Signal is passed to computer.Due to NI capture card and the good compatibility of Labwindows/CVI, using in Labwindows/CVI
The reliable communication with DAQ can be realized in the simple function set.The workflow of communication submodule can be described as: utilize self-test function
DAQ self-test is completed, checks whether equipment is correctly installed, can be worked normally；Sampling task is established, sampling parameter setting is carried out,
Main includes setting sampling channel, sample rate, triggering mode, range ability etc.；Continuously adopting for data is realized using sampling function
Collection；Remove sampling task, releasing memory.
The function of sub-module stored is by the storage of collected data into computer disk, convenient for subsequent data processing
And analysis.SGMA test sample channel is more, and sample rate is big, and sampling will generate huge data volume for a long time, if dealt with improperly
It will lead to leakage even to overflow.Therefore, how the data that quick storage has acquired become highly important link in system design.
For this purpose, special storage mode --- TDMS file stores data to sub-module stored using a kind of.The number of TDMS format
Have the characteristics that binary data efficient storage according to file, while including the characteristic information for describing data, can not influence to adopt
The quick storage of data is realized under the premise of collecting real-time.
Data of the display sub-module for each channel acquisition of real-time display DAQ, and display setting can be changed according to demand, it is real
Now to the real-time monitoring of acquisition overall process or specific portion feature.Not influence the real-time that data acquire, by display sub-module
An individual threads are put into, in Labwindows/CVI, nonsynchronous timer can be used for generating an independent thread, timing
Precision is up to 1ms.
Data readback module: data readback module mainly includes that reading data and data are shown.The function of reading data is
Some or all of hard disk data will be stored on to re-read in memory, data show be the data that will read as needed
It is screened and is shown.The programming implementation method of the module is similar with real-time display submodule, using Labwindows/CVI
Platform is implemented separately, and Fig. 4 is data readback module interfaces.
Data processing module: in data acquisition, for the real-time for guaranteeing system, usually can not be in detail to data
The analysis of system, devises data processing module thus.Data processing module is analyzed and processed for off-line data, without considering
Real time problems, processing result can provide foundation for the structure optimization of SGMA and control strategy design.In data processing module
In, devise four filtering processing, time-domain analysis, frequency-domain analysis and correlation analysis basic functions.Due to being directed to compare
Complicated numerical value calculates, when writing the module, using ActiveX control, to MATLAB order in Labwindows/CVI
It is called, realizes Labwindows/CVI and MATLAB combined programming.Fig. 5 is data processing module interface.
The test macro is achievable more to SGMA by passing through setting multiple sensors using data collecting card as core
The real time monitoring of a running parameter.On this basis, GMM characteristic test and actuator characteristics experiment are carried out.It is real by GMM characteristic
It tests, obtains the basic performance indices of material therefor, determine the basic parameter of actuator design；It is tested, is obtained by actuator characteristics
The regularity of distribution of each state parameter and the basic output characteristics of SGMA into SGMA work, model and are controlled for subsequent actuator
Reference and foundation are provided.
Claims (10)
1. one kind stacks formula ultra-magnetic deformation actuator characteristic test system, it is characterised in that: including testing the super magnetic of the formula that stacks
Expansion actuator is caused, pressure sensor (1) is installed on the fixing end of ultra-magnetic telescopic module in the actuator, super for measuring
Prestressing force suffered by GMM rod (2) in magnetostriction module；Magnetic field strength transducer includes hall probe (3) and matched makes
Gaussmeter, the hall probe (3) is tightly attached to GMM rod (2) surface of ultra-magnetic telescopic module, for measuring GMM rod (2)
Magnetic field strength near surface, the numerical value of measurement send the gaussmeter to；Magnetic induction search coil (4) is wound into the GMM
The outside of stick (2), for measuring the intensity of magnetization on GMM rod (2)；Temperature probe (5) is mounted on the ultra-magnetic telescopic module
Middle part, for measuring the temperature of the ultra-magnetic telescopic module；Foil gauge (6) is pasted onto the GMM rod (2) surface, is used for
Incude the deformation quantity of the GMM rod (2)；Laser displacement sensor (7) and the test are with stacking formula ultra-magnetic deformation actuator
Middle power output rod is oppositely arranged, for measuring the displacement of the actuator.
2. stacking formula ultra-magnetic deformation actuator characteristic test system as described in claim 1, it is characterised in that: the test
Include ultra-magnetic telescopic module with the formula ultra-magnetic deformation actuator of stacking, the ultra-magnetic telescopic module include permanent magnet (8),
GMM rod (2) and driving coil component (9), there are three more than, every two permanent magnet is arranged between (8) for permanent magnet (8) setting
There is a GMM rod (2), the driving coil component (9) is located at the club shaped structure of the permanent magnet (8) and GMM rod (2) composition
Outside；The left side of the permanent magnet (8) of the leftmost side is connect by the pressure sensor (1) with left end cap (10), the rightmost side
The right side of the permanent magnet (9) is connect with the medial end of the power output rod (11), the power output rod (11)
Outboard end is stretched out from right end cap (12), the movable end phase of the laser displacement sensor (7) and the power output rod (11)
To setting；Reset spring (13) are arranged on power output rod between the right end cap (12) and the permanent magnet (8) of the rightmost side,
One end of connection sleeve (14) is fixedly connected with the left end cap (10), connects the other end and the right end cap of sleeve (14)
(12) it is fixedly connected, and connection sleeve (14) is located at the outside of the driving coil component (9).
3. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 2, it is characterised in that: the test
It further include clamping device (15) with the formula ultra-magnetic deformation actuator of stacking, the left end cap (10) and the clamping device (15) are solid
Fixed connection.
4. stacking formula ultra-magnetic deformation actuator characteristic test system as described in claim 1, it is characterised in that: the test
System further includes data collecting card and main control computer, and the signal output end of the pressure sensor (1) and the data acquire
The signal input part of card connects, and handles for sending the information of acquisition to the data collecting card, pressure that treated
Information sends the main control computer to by data collecting card.
5. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 4, it is characterised in that: the Gauss
The signal output end of meter is connect with the signal input part of the data collecting card, for sending the information of acquisition to the data
Capture card is handled, and magnetic field strength information that treated sends the main control computer to by data collecting card.
6. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 4, it is characterised in that: the strain
The signal output end of piece (6) is connected by the signal input part of electric bridge and deformeter, the signal output end of the deformeter and institute
The signal input part connection for stating data collecting card, handles for sending the information of acquisition to the data collecting card, locates
Strain information after reason sends the main control computer to by data collecting card.
7. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 4, it is characterised in that: the thermometric
Pop one's head in (5) signal output end and temperature transmitter signal input part connect, the signal output end of the temperature transmitter with
The signal input part of the data collecting card connects, and handles for sending the information of acquisition to the data collecting card,
Treated temperature information sends the main control computer to by data collecting card.
8. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 4, it is characterised in that: the data
The driving signal output end of capture card and the signal input part of power amplifier connect, the signal output end of the power amplifier
It is connect with the both ends of the driving coil component coil, for providing working power, power amplifier output for the coil
Be provided with voltage measurement module and current measurement module on the conducting wire at end, for measure the power amplifier output electric current and
The signal output end of output voltage, the voltage measurement module and current measurement module and the signal of the data collecting card input
End connection, is handled for sending the information of acquisition to the data collecting card, and treated electric current and information of voltage are logical
It crosses data collecting card and sends the main control computer to.
9. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 2, it is characterised in that: the driving
Coil block (9) includes driving coil and coil rack, and the driving coil is wound on the coil rack.
10. stacking formula ultra-magnetic deformation actuator characteristic test system as claimed in claim 4, it is characterised in that: the pressure
The miniature press type sensor of DYHW-116 type that force snesor (1) uses Bangbu ocean to sense；Magnetic field strength transducer uses CH-
1600 type magnetic field strength transducers；The foil gauge (6) uses the BA120-3AA type foil gauge of Air China's electrical measurement, temperature probe (5)
The STT-FB3 type chip temperature insulted using match hundred million.
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| CN201910584949.3A CN110221232A (en) | 2019-07-01 | 2019-07-01 | Stack formula ultra-magnetic deformation actuator characteristic test system |
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| CN201910584949.3A CN110221232A (en) | 2019-07-01 | 2019-07-01 | Stack formula ultra-magnetic deformation actuator characteristic test system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114236438A (en) * | 2021-12-20 | 2022-03-25 | 中国石油大学(华东) | Measuring device and measuring method for magnetic parameters of giant magnetostrictive material |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101301930A (en) * | 2007-03-23 | 2008-11-12 | 古德里奇驱动系统有限公司 | Improved load detection on a flight control actuator |
| CN101995730A (en) * | 2009-08-18 | 2011-03-30 | 松下电器产业株式会社 | Optical element driving device and imaging device |
| CN102255555A (en) * | 2011-07-11 | 2011-11-23 | 南京航空航天大学 | Permanent magnet dual-coil-driven giant magnetostrictive actuator and working method thereof |
| CN202165685U (en) * | 2011-08-01 | 2012-03-14 | 艾默生过程管理(天津)阀门有限公司 | Connector for valve assembly and valve assembly with same |
| CN104280243A (en) * | 2013-07-08 | 2015-01-14 | Smc株式会社 | Fault detection system for actuator |
| CN205271597U (en) * | 2015-12-23 | 2016-06-01 | 王晶怡 | Low -power consumption precision on -line monitoring system in precision finishing |
| CN107218884A (en) * | 2017-07-14 | 2017-09-29 | 武汉地震科学仪器研究院有限公司 | A kind of drilling strain gauge overall performance test device and method of testing |
| WO2017208674A1 (en) * | 2016-06-02 | 2017-12-07 | 株式会社コガネイ | Position detecting device and actuator |
| CN108981756A (en) * | 2017-05-30 | 2018-12-11 | 梅斯法国公司 | The temperature-compensating of field sensing unit and the field sensing unit for using temperature-compensating |
-
2019
- 2019-07-01 CN CN201910584949.3A patent/CN110221232A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101301930A (en) * | 2007-03-23 | 2008-11-12 | 古德里奇驱动系统有限公司 | Improved load detection on a flight control actuator |
| CN101995730A (en) * | 2009-08-18 | 2011-03-30 | 松下电器产业株式会社 | Optical element driving device and imaging device |
| CN102255555A (en) * | 2011-07-11 | 2011-11-23 | 南京航空航天大学 | Permanent magnet dual-coil-driven giant magnetostrictive actuator and working method thereof |
| CN202165685U (en) * | 2011-08-01 | 2012-03-14 | 艾默生过程管理(天津)阀门有限公司 | Connector for valve assembly and valve assembly with same |
| CN104280243A (en) * | 2013-07-08 | 2015-01-14 | Smc株式会社 | Fault detection system for actuator |
| CN205271597U (en) * | 2015-12-23 | 2016-06-01 | 王晶怡 | Low -power consumption precision on -line monitoring system in precision finishing |
| WO2017208674A1 (en) * | 2016-06-02 | 2017-12-07 | 株式会社コガネイ | Position detecting device and actuator |
| CN108981756A (en) * | 2017-05-30 | 2018-12-11 | 梅斯法国公司 | The temperature-compensating of field sensing unit and the field sensing unit for using temperature-compensating |
| CN107218884A (en) * | 2017-07-14 | 2017-09-29 | 武汉地震科学仪器研究院有限公司 | A kind of drilling strain gauge overall performance test device and method of testing |
Non-Patent Citations (2)
| Title |
|---|
| 何忠波: """叠堆式超磁致伸缩致动器的模型预测滑模控制"", 《光学精密工程》 * |
| 崔旭: ""超磁致伸缩致动器优化设计与特性测试"", 《机械设计及制造》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114236438A (en) * | 2021-12-20 | 2022-03-25 | 中国石油大学(华东) | Measuring device and measuring method for magnetic parameters of giant magnetostrictive material |
| WO2023115671A1 (en) * | 2021-12-20 | 2023-06-29 | 中国石油大学(华东) | Device and method for measuring magnetic parameter of giant magnetostrictive material |
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Application publication date: 20190910 |