Movatterモバイル変換


[0]ホーム

URL:


CN109708586A - A kind of packaging method of fiber Bragg grating strain sensor - Google Patents

A kind of packaging method of fiber Bragg grating strain sensor
Download PDF

Info

Publication number
CN109708586A
CN109708586ACN201811653810.1ACN201811653810ACN109708586ACN 109708586 ACN109708586 ACN 109708586ACN 201811653810 ACN201811653810 ACN 201811653810ACN 109708586 ACN109708586 ACN 109708586A
Authority
CN
China
Prior art keywords
strain
grating
sensor
fiber
strain sensor
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.)
Pending
Application number
CN201811653810.1A
Other languages
Chinese (zh)
Inventor
孟凡勇
闫光
朱家林
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.)
Beijing Information Science and Technology University
Original Assignee
Beijing Information Science and Technology University
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 Beijing Information Science and Technology UniversityfiledCriticalBeijing Information Science and Technology University
Priority to CN201811653810.1ApriorityCriticalpatent/CN109708586A/en
Publication of CN109708586ApublicationCriticalpatent/CN109708586A/en
Pendinglegal-statusCriticalCurrent

Links

Landscapes

Abstract

Translated fromChinese

本发明属于光纤传感器测量领域,公开一种光纤布拉格光栅应变传感器的封装方法,其特征在于,包括如下步骤:1)光栅光纤应变传感器封装之前,对所述光栅光纤应变传感器进行力学模拟分析;2)所述光栅光纤应变传感器封装;3)所述光栅光纤应变传感器标定。能够精确测量环境温度,并在实验室环境对应变传感器进行标定,测试传感器拉伸压缩性能。采用基片式封装方法能够有效的传递应变,实现了应变测量。

The invention belongs to the field of optical fiber sensor measurement, and discloses a method for encapsulating a fiber Bragg grating strain sensor, which is characterized by comprising the following steps: 1) before packaging the grating optical fiber strain sensor, perform mechanical simulation analysis on the grating optical fiber strain sensor; 2 ) packaging of the grating fiber optic strain sensor; 3) calibration of the grating fiber optic strain sensor. It can accurately measure the ambient temperature, calibrate the strain sensor in the laboratory environment, and test the tensile and compressive performance of the sensor. The substrate-type packaging method can effectively transmit the strain and realize the strain measurement.

Description

A kind of packaging method of optical fibre Bragg optical grating strain sensor
Technical field
The invention belongs to fiber-optic grating sensor fields of measurement, and in particular to a kind of optical fibre Bragg optical grating strain sensorPackaging method.
Background technique
The development of aircraft industry and the increase of aircraft task difficulty, so that the use condition of aircraft and receiving environment are more nextIt is more complicated.The method that " certainty threshold value " based on historical experience covers various random factors and influence is incomplete.It closesThe Aircraft Load parameter testing of reason is lengthened the life etc. and to be had for determining structure design, determining the longevity to ensureing that flight safety is most importantImportant meaning.
In material property and structural mechanical property field, strain measurement is most important test index.The knot of aircraft wingThe problem of detection of structure stress, electrical measuring method have been commonly used, and a large amount of test point is brought as number of cables is more, weightGreatly, it is not easy later maintenance, electromagnetism interference is in addition unable to and the service life is shorter.Therefore, new measurement method is constantly attempted applicationIn Aircraft Load parameter testing.Fiber-optic grating sensor measurement is simple with structure, is easy to networking, electromagnetism interference, high surveyThe advantages that accuracy of measurement, Wavelength-encoding, meets the final requirement of Aircraft Load parameter testing, there is very big application prospect.
Certain substantial progress, but pass non-sensitive for part on Flight Vehicle Structure are achieved to Aircraft Load test at presentThe strain measurement of bond structure does not have effective measurement method.
Summary of the invention
The purpose of the present invention is to solve this problem, providing one kind being capable of precise measurement structural member in a certain rangeThe packaging method of the substrate formula optical fibre Bragg optical grating strain sensor of strain, can precise measurement environment temperature, reach decouplingPurpose, and demarcated in laboratory environment pair of strain sensors, test sensor Compression and Expansion performance.Using novel baseChip package method can effectively transmit strain, realize strain measurement.
For achieving the above object, the technical scheme is that
A kind of packaging method of optical fibre Bragg optical grating strain sensor, which comprises the steps of: 1) gratingBefore fibre optic strain sensor encapsulation, mechanical simulation analysis is carried out to the grating fibers strain transducer;
2) the grating fibers strain transducer encapsulation;
3) the grating fibers strain transducer calibration.
Preferably, mechanical simulation is analyzed, and steps are as follows, and 11, which carry out gridding to sensor with finite element method, drawsPoint;12 simulation extension test loading procedures fix sensor substrate one end, and the other end applies pulling force and stretched, and are simulated with thisWhen adhering to the measured object surface from tensile of sensor, the stress of sensor.
Preferably, in the strain transducer encapsulation process, steps are as follows, and 21, by adjustable optic fibre fixture, apply pre-Clamp force increases two fiber bragg grating center wavelengths, epoxide-resin glue is smeared at sensor substrate A, B, using full coverage typeIt encapsulates at sensor substrate C, for measuring temperature parameters;22 after the completion of dispensing, installs the biography of fiber grating under room temperature state additionalSensor substrate stands setting time, is then socketed fiber optic protection casing and fixation, high-temperature decoupling essence in sensor base two sidesThe encapsulation for spending enhanced sensitivity formula strain fiber-optic grating sensor is completed.
Preferably, the strain transducer calibration, steps are as follows, and 31 build test sensor enhanced sensitivity pilot system, usesMTS cupping machine using KYOWA foil gauge acquisition numerical value as standard strain value, and sets up half-bridge a pair using resistance strain gageOne compensation circuit is compared with the naked mounted packaged fiber grating strain transducer in same level section;32 will answer in high precisionBecome tester and high speed optic fiber grating demodulation module and LabVIEW software is write by host computer, realizes strain transducer inThe long synchronous acquisition storage of cardiac wave;33 in collection process, program-controlled setting cupping machine, under conditions of giving initial tensile forceIt is incremented by pulling force step by step, does two tension and compression circulations by reading foil gauge output numerical value and survey the relationship between pulling force and strain.
Compared with prior art, the beneficial effects of the present invention are:
Improved in the technique of traditional strain transducer, can simultaneously precise measurement environment temperature, reachThe purpose of decoupling, and demarcated in laboratory environment pair of strain sensors, test sensor Compression and Expansion performance.Using novelSubstrate formula packaging method, realize strain measurement.Base material chooses the preferable aerolite 7075-T6 of Compression and ExpansionBase material can effectively transmit strain, achieve the purpose that measure enhanced sensitivity.The temperature decouples enhanced sensitivity formula strain transducer canEffectively reliable accurate means of testing is provided for wing structure Compression and Expansion.
Detailed description of the invention
The drawings herein are incorporated into the specification and forms part of this specification, and shows and meets implementation of the inventionExample, and be used to explain the principle of the present invention together with specification.
Fig. 1 is the sensor base schematic diagram of optical fibre Bragg optical grating strain sensor of the present invention;
Fig. 2 is the encapsulation schematic diagram of optical fibre Bragg optical grating strain sensor of the present invention.
Fig. 3 is the gridding schematic diagram of optical fibre Bragg optical grating strain sensor of the present invention.
The calibration experiment system diagram of Fig. 4 optical fibre Bragg optical grating strain sensor of the present invention.
The pulling force and tension test part strain curve figure of Fig. 5 embodiment of the present invention.
The pulling force and enhanced sensitivity formula strain transducer central wavelength graph of relation of Fig. 6 embodiment of the present invention.
The pulling force and fiber bragg grating center wavelength offset graph of relation of Fig. 7 embodiment of the present invention.
Fig. 8 is the strain transducer repeatability aberration curve figure of the embodiment of the present invention.
Specific embodiment
Below in conjunction with attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.
As shown in Figs 1-4, a kind of optical fibre Bragg optical grating strain sensor includes the following steps: 1) grating fibers strainBefore sensor encapsulation, mechanical simulation analysis is carried out to the grating fibers strain transducer;
Fiber Bragg grating strain sensor structure as shown in Figure 1.As shown in figure 3, mechanical simulation is analyzed, steps are as follows, and 11 useFinite element method carries out gridding division to sensor;12 simulation extension test loading procedures keep sensor substrate one end solidFixed, the other end applies pulling force and is stretched, and is simulated with this when adhering to the measured object surface from tensile of sensor, sensorStress.
Load is applied to substrate and carries out finite element analysis.According to stress cloud atlas, it can be concluded that, tensile stress occurs for sensorWhen variation, the special shape of substrate concentrates on substrate deformation between A, B two o'clock, forms stress and concentrates, not will receive biography at CSensor stretches bring any influence, i.e., any deformation does not occur.From the angle of force analysis, it is believed that the sensor baseDesign can reach expected purpose.
2) the grating fibers strain transducer encapsulation;
As shown in Fig. 2, steps are as follows in the strain transducer encapsulation process, 21, by adjustable optic fibre fixture, applyPretightning force makes two fiber bragg grating center wavelengths increase 1nm, and DP420 epoxide-resin glue is smeared at sensor substrate A, B, is adoptedAt full coverage type encapsulation sensor substrate C, for measuring temperature parameters;22 after the completion of dispensing, installs light additional under room temperature stateThe sensor substrate of fine grating stands setting time 24 hours, is then socketed fiber optic protection casing in sensor base two sides and consolidatesFixed, the encapsulation that high-temperature decouples precision enhanced sensitivity formula strain fiber-optic grating sensor is completed;The lesser fiber grating of central wavelength is adoptedIt is encapsulated with full coverage type.
According to theory analysis and purpose of design, sensor is pasted onto testee surface, at affixed points D, E two, then increasesQuick multiple is LDE/LAB.
3) the grating fibers strain transducer calibration.
The strain transducer calibration, steps are as follows, and 31 build test sensor enhanced sensitivity pilot system, is stretched using MTSTesting machine, using KYOWA foil gauge acquisition numerical value as standard strain value, and it is one-to-one compensation using resistance strain gage establishment half-bridgeCircuit is compared with the naked mounted packaged fiber grating strain transducer in same level section;32 by high-precision strain testing instrumentAnd high speed optic fiber grating demodulation module writes LabVIEW software by host computer, realizes strain transducer and central wavelengthSynchronous acquisition storage;33 in collection process, and program-controlled setting cupping machine is incremented by step by step under conditions of giving initial tensile forcePulling force does two tension and compression circulations by reading foil gauge output numerical value and surveys the relationship between pulling force and strain.
In order to test sensor effect of enhanced sensitivity, if Fig. 4 shows, the fiber Bragg grating strain sensor calibration enhanced sensitivity test is builtSystem is to be attached to same level section high-precision KYOWA foil gauge acquisition numerical value with sensor using MTS cupping machineStandard strain value, and the one-to-one compensation circuit of half-bridge is set up using same performance resistance strain gage, it is naked with same level sectionMounted packaged fiber grating strain transducer compares.
During strain transducer and the synchronous acquisition of central wavelength, according to the Young's modulus and cross of tension test partCross-sectional dimension applies the clamping pulling force of 8000N, reaches and need microstrain value.Sigma high-precision strain testing instrument is chosen, mostSmall resolution ratio 1 μ ε, maximum frequency acquisition 500Hz;MTS cupping machine, maximum pull 250000N;Temperature calibration link is sameFlat wideband light source and Ibsen high speed optic fiber grating (FBG) demodulator;No. 45 steel are tensioning member.
In the case of obtaining continuous time, changing rule synchronous with central wavelength is strained, Sigma high-precision is strainedTester and Ibsen high speed (FBG) demodulator write LabVIEW software by host computer, realize strain transducer and central wavelengthSynchronous acquisition storage.
If Fig. 5 shows in collection process, program-controlled setting cupping machine, under conditions of giving initial 2000N pulling force, with1000N, which is stepping, is incremented to 10000N step by step, is drawn-pressure-draws-presses two circulations, real by reading foil gauge output numerical valueSurvey the relationship between pulling force and strain, fitting function formula 1 are as follows:
ε=0.065F-33.635;R2=0.999 (1)
During investigating effect of enhanced sensitivity, the linearity and the repeatability of enhanced sensitivity formula strain transducer, answered with enhanced sensitivity formulaThe same cross-section location for becoming sensor is pasted with the different naked mounted fiber Bragg grating strain sensor of central wavelength, obtains not enhanced sensitivityIn the case of fiber grating survey strain sensitivity coefficient, while using serial temperature compensated optical fiber grating method, exclude temperatureInfluence of the parameter to test result.Ambient temperature effect is excluded by algorithm, value of thrust and enhanced sensitivity formula strain transducer are reflectedCentral wavelength carries out least square fitting, show that its relation curve such as Fig. 6 shows, fitting function and linearity formula 2 be,
λ=9.47 × 10-5F+1537.646;R2=0.999 (2)
Linearity coefficient of determination R2=0.9991, the linearity are good.
Convolution 1, obtain enhanced sensitivity formula strain transducer central wavelength and substrate institute it is strained between relation function formula 3 are as follows:
λ=1.46 × 10-3ε+1537.696 (3)
Effect of enhanced sensitivity and repeatability are to investigate the important indicator of sensor performance, exclude ambient temperature effect by algorithmAfterwards, two different performance strain transducers acquired reflection kernel wavelength data is recycled in Compression and Expansion twice to carry out at algorithmReason, the departure of central wavelength when obtaining stable point fiber grating reflection kernel wavelength and value of thrust 2000N, and carry out respectively mostSmall two multiply fitting, investigate the value of two slope of curve multiples and stepping stable case lower pulling force, and fitting function such as Fig. 7 shows, are fitted letterNumerical expression 4 are as follows:
By analyzing fitting data, enhanced sensitivity formula strain transducer effect of enhanced sensitivity is obvious, reaches 0.095/0.068=1.4 times.
By Fig. 8 to draw a conclusion, enhanced sensitivity formula strain transducer repeats sexual deviation and is no more than ± 5pm, and error is to test resultBring influences to be no more than 3 μ ε, within the allowable range, it is believed that repeatability is good, and the design is feasible.
Embodiments described above is only a part of the embodiment of the present invention, instead of all the embodiments.Based on thisEmbodiment in invention, every other reality obtained by those of ordinary skill in the art without making creative effortsExample is applied, shall fall within the protection scope of the present invention.

Claims (4)

3. the packaging method of optical fibre Bragg optical grating strain sensor according to claim 1, which is characterized in that second step,In strain transducer encapsulation process, steps are as follows, and 21 by adjustable optic fibre fixture, and applying pretightning force makes two fiber grating centersWavelength increases, and epoxide-resin glue is smeared at sensor substrate A, B, at full coverage type encapsulation sensor substrate C, is used toMeasure temperature parameters;22 after the completion of dispensing, and the sensor substrate for installing fiber grating under room temperature state additional stands setting time, withIt is socketed fiber optic protection casing and fixation in sensor base two sides afterwards, high-temperature decouples precision optical fiber grating enhanced sensitivity formula strain sensingThe encapsulation of device is completed.
4. the packaging method of optical fibre Bragg optical grating strain sensor according to claim 1, which is characterized in that third step,Transducer calibration, 31 build test sensor enhanced sensitivity pilot system, using MTS cupping machine, acquire number with KYOWA foil gaugeValue is standard strain value, and sets up the one-to-one compensation circuit of half-bridge using resistance strain gage, naked mounted with same level sectionPackaged fiber grating strain transducer compares;32 lead to high-precision strain testing instrument and high speed optic fiber grating demodulation moduleIt crosses host computer and writes LabVIEW software, realize the synchronous acquisition storage of strain transducer and central wavelength;33 in collection processIn, program-controlled setting cupping machine is incremented by pulling force step by step under conditions of giving initial tensile force, does two tension and compression circulations, passes throughFoil gauge output numerical value is read, the relationship between pulling force and strain is surveyed.
CN201811653810.1A2018-12-292018-12-29 A kind of packaging method of fiber Bragg grating strain sensorPendingCN109708586A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201811653810.1ACN109708586A (en)2018-12-292018-12-29 A kind of packaging method of fiber Bragg grating strain sensor

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201811653810.1ACN109708586A (en)2018-12-292018-12-29 A kind of packaging method of fiber Bragg grating strain sensor

Publications (1)

Publication NumberPublication Date
CN109708586Atrue CN109708586A (en)2019-05-03

Family

ID=66260673

Family Applications (1)

Application NumberTitlePriority DateFiling Date
CN201811653810.1APendingCN109708586A (en)2018-12-292018-12-29 A kind of packaging method of fiber Bragg grating strain sensor

Country Status (1)

CountryLink
CN (1)CN109708586A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111735714A (en)*2020-06-092020-10-02西北工业大学 A method and device for testing high temperature total stress-strain curve based on optical fiber
CN112043248A (en)*2020-09-032020-12-08山东大学 A flexible pulse-diagnosing hand and a traditional Chinese medicine pulse-diagnosing instrument
CN114608635A (en)*2022-03-072022-06-10广州大学 A reusable microarray self-adhesive optical fiber sensor and preparation method thereof
CN118392063A (en)*2024-05-222024-07-26中国航空工业集团公司北京长城计量测试技术研究所 Auxiliary installation structure of piston type optical fiber strain sensor
CN119043233A (en)*2024-11-012024-11-29浙江雄鹰科菲帝科技股份有限公司CMM automatic coordinate measuring machine and method thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN106482760A (en)*2015-10-142017-03-08北京信息科技大学A kind of system of all-metal packaged fiber grating strain transducer
CN106840018A (en)*2016-11-022017-06-13北京信息科技大学A kind of fiber Bragg grating strain sensor method for packing

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN106482760A (en)*2015-10-142017-03-08北京信息科技大学A kind of system of all-metal packaged fiber grating strain transducer
CN106840018A (en)*2016-11-022017-06-13北京信息科技大学A kind of fiber Bragg grating strain sensor method for packing

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
张开宇 等: "温度解耦增敏式光纤光栅应变传感器", 《光学精密工程》*

Cited By (8)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111735714A (en)*2020-06-092020-10-02西北工业大学 A method and device for testing high temperature total stress-strain curve based on optical fiber
CN112043248A (en)*2020-09-032020-12-08山东大学 A flexible pulse-diagnosing hand and a traditional Chinese medicine pulse-diagnosing instrument
CN112043248B (en)*2020-09-032021-07-20山东大学 A flexible pulse-diagnosing hand and a traditional Chinese medicine pulse-diagnosing instrument
CN114608635A (en)*2022-03-072022-06-10广州大学 A reusable microarray self-adhesive optical fiber sensor and preparation method thereof
CN114608635B (en)*2022-03-072023-11-21广州大学 A reusable microarray self-adhesive optical fiber sensor and its preparation method
CN118392063A (en)*2024-05-222024-07-26中国航空工业集团公司北京长城计量测试技术研究所 Auxiliary installation structure of piston type optical fiber strain sensor
CN119043233A (en)*2024-11-012024-11-29浙江雄鹰科菲帝科技股份有限公司CMM automatic coordinate measuring machine and method thereof
CN119043233B (en)*2024-11-012025-02-11浙江雄鹰科菲帝科技股份有限公司CMM automatic coordinate measuring machine and method thereof

Similar Documents

PublicationPublication DateTitle
CN109708586A (en) A kind of packaging method of fiber Bragg grating strain sensor
CN108895978B (en) A Sensitivity Calibration Method for Optical Fiber Strain Sensor Based on Bare Optical Fiber
CN108195555B (en)Optical fibre balance aerodynamics force measurement system and measurement method
CN108519175B (en)Variable-range soil pressure measuring method based on Bragg fiber grating
CN105116168B (en)Optical fibre grating three-dimensional acceleration sensor based on flexible hinge
Peng et al.Design and investigation of a sensitivity-enhanced fiber Bragg grating sensor for micro-strain measurement
CN103335603B (en)A kind of distributive fiber optic strain factor calibration device and scaling method
CN105115438B (en)A kind of optical fiber sensing system temperature compensation
CN107036543A (en)A kind of fiber Bragg grating strain sensor demarcation and fatigue detecting system
US11215447B2 (en)Mechanical strain amplifying transducer
CN111735714B (en)High-temperature full-stress-strain curve testing method and device based on optical fiber
CN203658011U (en)Optical fiber balance for wind tunnel test measurement
Li et al.Design of an enhanced sensitivity FBG strain sensor and application in highway bridge engineering
CN108871638B (en)Optical fiber measuring device and monitoring method for residual stress of material
CN108760109A (en)The soil pressure measuring device and method of changeable fluid based on bragg grating
CN104697682A (en)Fiber Bragg grating strain-measuring method and fiber Bragg grating strain sensor
CN103278279B (en)A kind of cable force measurement method and apparatus
Dalla Vedova et al.Design and development of innovative FBG-based fiber optic sensors for aerospace applications
Ma et al.Strain transfer characteristics of surface-attached FBGs in aircraft wing distributed deformation measurement
CN103940577B (en)A kind of appraisal procedure of wind tunnel test balance based on acceleration signal energy
CN106871810A (en)Calibration method, device and system of fiber grating strain sensor
CN210862557U (en)Optical fiber grating sensor device
Mitra et al.Development and Validation of Experimental Setup for Flexural Formula of Cantilever Beam Using NI-LabVIEW
CN109612401A (en) Fabrication of a temperature-decoupled long-range strain sensor
Heaney et al.Distributed sensing of a cantilever beam and plate using a fiber optic sensing system

Legal Events

DateCodeTitleDescription
PB01Publication
PB01Publication
SE01Entry into force of request for substantive examination
SE01Entry into force of request for substantive examination
WD01Invention patent application deemed withdrawn after publication
WD01Invention patent application deemed withdrawn after publication

Application publication date:20190503


[8]ページ先頭

©2009-2025 Movatter.jp