Movatterモバイル変換


[0]ホーム

URL:


AU745103B2 - Thin film strain sensors based on interferometric optical measurements - Google Patents

Thin film strain sensors based on interferometric optical measurements
Download PDF

Info

Publication number
AU745103B2
AU745103B2AU56949/99AAU5694999AAU745103B2AU 745103 B2AU745103 B2AU 745103B2AU 56949/99 AAU56949/99 AAU 56949/99AAU 5694999 AAU5694999 AAU 5694999AAU 745103 B2AU745103 B2AU 745103B2
Authority
AU
Australia
Prior art keywords
strain
sensor
thin film
light
passive
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.)
Ceased
Application number
AU56949/99A
Other versions
AU5694999A (en
Inventor
William B. Euler
Otto J. Gregory
Gregg C. Huston
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.)
Rhode Island Board of Education
Original Assignee
Rhode Island Board of Education
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 Rhode Island Board of EducationfiledCriticalRhode Island Board of Education
Publication of AU5694999ApublicationCriticalpatent/AU5694999A/en
Application grantedgrantedCritical
Publication of AU745103B2publicationCriticalpatent/AU745103B2/en
Anticipated expirationlegal-statusCritical
Ceasedlegal-statusCriticalCurrent

Links

Classifications

Landscapes

Description

Title Thin Film Strain Sensors Based on Interferometric Optical Measurements Background of the Invention 1. Field of the Invention The invention relates to polymeric/semiconductor thin film strain gauges 2. Description of the Relevant Art Many civil engineering structures display fatigue, and occasionally failure, after years of exposure to natural forces. In other instances, the failure is a result of a catastrophic event, such as an earthquake, tornado, or hurricane. There is a need for an inexpensive, robust, and sensitive strain gage that is unaffected by seasonal 15 environmental variations. Further, such a sensor should be simple, easily installed, and readily integrated into modern data communication systems.
The sensor system disclosed herein can monitor the integrity of structures for the purpose of public safety and maintenance. Specific applications include building, Sroad, and bridge integrity. The system employs, as the sensing component, multiple S optical strain gages that are inexpensive, inert to natural environments, and physically robust. Combined with an automated data collection and diagnostic analysis programming, such sensors and their optical fiber data links can be placed on the superstructures and footings of bridges, in the support components of buildings, or 25 embedded into the surfaces of roads and pedestrian skywalks. The 'health' of such structures and surfaces can be automatically monitored and assessed with a minimum of human time allocation. Detailed use information would also be valuable in assessing the need for routine maintenance or for the need for repair after a potential catastrophic S loading.
R,4/I sz"1rr la The discussion of the background to the invention herein is included to explain the context of the invention. This is not to be taken as an admission that any of the material referred to was published, known or part of the common general knowledge in Australia as at the priority date of any of the claims.
Summary of the Invention The sensitivity and the passivity behavior of the sensors distinguishes from the prior art. Current resistive strain sensors have gage factors (the measure of sensitivity) of about 2-3. The disclosed sensors have gage factors on the order of 200-800. It is not believed the prior art discloses any passive sensors that have a memory that does *1 a a W:\minul NODELETE\D6949-99.doc WO 00/12960 PCT/US99/19601 2 not rely on a power source.
Thin films of semiconductors or polymers are used to measure strain. The thin films are layered with each layer consisting of materials with different refractive indices. Because each layer has a different refractive index, light that is introduced into the composite structure can either be reflected or pass through at each interface.
This allows interference of the incident light that passes through with light that is reflected resulting in a measurable absorption change. The degree of interference is sensitive to the refractive index and thickness of each layer. The thickness of the each layer changes with application of an external stress. The consequence of this is that the light absorption changes as a function of strain so that the absorption change can be used to measure the strain.
There are two types of interferometric sensors disclosed herein, active and passive. An active sensor responds to the strain reversibly, i.e. as the strain changes the absorption changes in a reversible and predictable fashion. This type of sensor is used to measure the existing strain on a structure.
A passive sensor has a memory of the maximum strain experienced by the structure. For example, if a structure experiences a large deformation a large strain) but then relaxes to a small rest value, the large deformation is not reversible. An active sensor will measure the strain events only if continuously monitored while the passive sensor will measure only the maximum strain experienced. If the active sensor is not being monitored while the maximum strain is occurring, the large strain excursion will not be observed. The passive sensor overcomes this problem.
Broadly the invention comprises both active and passive sensors which preferably are used in the same structure. Both sensors are constructed by layering materials, either semiconductors or polymers having different refractive indices. The sensitivity is increased when the difference in refractive index is maximized and also as the number of layers is increased. The passive sensors are constructed by adding small particulates to one set of layers.
Brief Description of the Drawings Fig. 1 is an illustration of a passive sensor; Figs. 2a and 2b are illustrations of an alternative embodiment of Fig. 1; WO 00/12960 PCTIUS99/19601 3 Fig. 3 is a graph of the optical response of an active sensor; Fig. 4 is a graph of the optical response of an passive sensor; and Fig. 5 is a graph of the optical response of a passive sensor; Description of the Preferred Embodiment(s) Incident light can be measured in reflectance or transmission to determine the strain.
Referring to Fig. 1, reflectance mode, visible light from a spectrometer such as Perkin Elmer Lambda 2, is directed onto a thin film passive sensor shown generally at 12. The sensor 12 comprises a transparent glass substrate 14 and a laminated construction in succession from the substrate 14, of a polyimide layer 18a, a polysiloxane layer 16a filled with alumina particles, a polyimide layer 18b and a polysiloxane layer 16b filled with alumina particles. The incident light beam is normal to the sensor surface. The light is collected along the incidence beam path in a photomultiplier tube detector 20 in the spectrometer 10. The layers can range in thickness from 1-20 microns. The passive sensor is prepared by mixing 50 nm particles of aluminum oxide in with the polysiloxane layer in an amount of 0.5 to 10% by weight based on the total weight of the polysiloxane layer. During preparation, the small particles aggregate to some (currently unknown) degree. Under strain, some of the particles in the aggregate separate and the polymer fills in between the newly separated alumina particles. When the strain is removed, the particles cannot reaggregate because of the intervening polymer. This is detected optically because the size of the aggregates determines the amount of light scattered off of the sample: as the aggregate size changes because of the strain, the amount of light directed toward the detector changes since the detector only samples a small volume of space. The passive sensor requires no power to achieve its memory effect.
Referring to Fig. 2a, the transmission mode, for an active sensor a capillary tube 30, e.g. i.d. 0.5 mm; o.d 0.7 mm, is used as a light conduit. Thin films 32, e.g.
polysiloxane/polyiniide, are deposited onto the outside walls of the capillary tube and then these films are coated with aluminum 34. The aluminum 34 serves as a mirror to keep all the light confined in the tube 30 and to protect the entire structure from the surrounding environment. A fiber optic source 36 inputs light in a WO 00/12960 PCT/US99/19601 4 wavelength range of 500 to 1,000 Angstroms into one end of the capillary tube 30 parallel to the longitudinal axis of the tube and a detector 38 collects the light at the other end.
In the capillary configuration, the tube 30 acts as both a waveguide and a sensor. Under no strain, most of the light passes down the tube without interacting with the walls. With application of a strain the capillary tube 30 bends, Fig. 2b, so that a significant amount of light is introduced into the thin film coatings along the tube walls. Two effects cause a modulation of the output light intensity. First, the path length is changed so any absorption that occurs is increased, depending upon the absorptivity of the wall materials and the number of bounces the light undergoes.
Second, the interference effect observed as light passes through the thin film layers still is operative, also causing intensity modulation by constructive or destructive interference, depending on the refractive index and thickness of each layer and the wavelength of light used.
The film thicknesses 32 are on the order of 1 to 20 microns, thinner being a bit better. The wavelengths of maximum response depends upon the layer thicknesses, but that wavelength can be chosen arbitrarily to match the thin film structure. The aluminum coating has a thickness of between 400 to 800 nm.
The alternating layers must have a different refractive index and the larger the difference, the better the sensor response. Polyimide has n 1.6-1.7 (depending upon the exact polyimide used, the nature of the curing, and the supplier); polysiloxane has n= 1.44. Other commonly available transparent polymers polyethylene, polypropylene, Teflon polyvylidene flouride, polyester, etc. have refractive indices around 1.4 and could substitute for the polysiloxane layer. High refractive index polymers such as polycarbonates have refractive indices approximately the same as polyimide.
A preferred sensor system requires both a passive and an active sensor in close proximity. The passive sensor measures the maximum strain excursion experienced but not a temporal history, i.e. the measured strain may be current or previous. Thus, the role of the active sensor is to measure the existing strain at the time of measurement.
WO 00/12960 PCT/US99/19601 The sensors can be applied to a structure by currently known bonding techniques used for the current generation of strain sensors. Because the sensors are small, they will measure the strain of the substrate material reliably. The optical source and detector need not be embedded with the sensor. With the appropriate fiber optic connections, the optical measurement can be made periodically by connecting a handheld spectrometer to the input and output of the sensor. Thus, for example, after an earthquake the maximum strain experienced by each structural element in a building could be determined well after the event (days or weeks) to establish the safety of the building since the passive sensor retains this information even with (the likely) loss of power. Alternatively, a fiber optic network connected to each sensor in a building that remotely senses the strain automatically. However, during a catastrophic event the fiber network is likely to break and prevent this mode of operation.
The materials used in the sensor are both inexpensive and robust. For example, the polysiloxane is a commercially available gasket sealer. The capillary configuration is especially attractive for long term applications because, if necessary, the entire sensor can be enclosed. Then, for example, if the sensor is to be used in a harsh environment such as a bridge, the entire sensor can be isolated from wind, rain, salt spray, etc. because any coatings applied outside of the aluminum layer have no affect on the sensor performance.
Examples Examples of the sensor response are given in Figures 3, 4 and 5. The light source was a tungsten lamp, and strain was applied by four point bending, see ASTM C-1341-97.
Figure 3 shows the response of two different active strain sensors, one with 12 layers (6 alternating layers of polysiloxane and polyimide) and one with 26 alternating layers. Layer thickness was about 10 microns. The absorbance was monitored at 600 nm as a function of applied strain with the results shown. The gage factor is a function of the number of layers indicating the interferometric nature of the response. Further, the gage factors are large, more than two orders of magnitude larger than found in typical resistance strain gages. Finally, the response is linear and reversible over the entire range up to about 2000 Astrain (this is the typical limit required for structural I ~i 6 applications since most materials exceed their plastic deformation limits at about 2000 pstrain).
Figure 4 shows the response of a passive strain gage having 26 alternating layers. The layer thickness was about 10 microns. As strain is applied, the response is similar to an active gage. The absorbance was monitored at 600 nm. However, when the strain is released the response is no longer reversible, the 0-strain absorbance depends upon the history of the sample. This is demonstrated in Figure 4 for several different strain excursions. The virgin gage has an absorbance value at 600 nm of A 0.73. Application of 300 pstrain changes this to A 0.83. Upon release of the stress back to 0 ustrain the absorbance returns to A 0.78, shown as the short dashed line in Figure 4. Application of any strain less than 300 pstrain follows the dashed line path S: reversibly. However, if the strain exceeds 300 istrain, then the path reverts to the S::I 5 solid line as shown for the 600 jstrain point in Figure 4. Now when the stress is released, a new path is taken, shown as the dotted line, and to a new absorbance at 0 Astrain.
The increments between successive strain excursions decreases with increasing 20 strain the passive response is nonlinear) and this is demonstrated in Figure The 12 layer gage has a small gage factor but a larger, nearly linear response range.
The 26 layer gage has a larger gage factor but becomes clearly nonlinear at significantly smaller maximum strains.
;The foregoing description has been limited to a specific embodiment of the S. 25 invention. It will be apparent, however, that variations and modifications can be made to the invention, with the attainment of some or all of the advantages of the invention.
Therefore, it is the object of the appended claims to cover all such variations and modifications as come within the true spirit and scope of the invention.
Throughout the description and. claims of the specification the word "comprise" and variations of the word, such as "comprising" and "comprises", is not intended to exclude other additives, components, integers or steps.
Having described our invention what we now claim is: 1 dc

Claims (1)

17. A sensor according to any one of the preceding claims substantially as hereinbefore described with reference to any one of the figures and/or examples. DATED: 24 October 2001 PHILLIPS ORMONDE FITZPATRICK Patent Attorneys for: THE BOARD OF GOVERNORS FOR HIGHER EDUCATION, STATE OF RHODE ISLAND AND PROVIDENCE PLANTATIONS *a °s \n.,lrv\NO DELET E 6949-99 doc
AU56949/99A1998-08-261999-08-25Thin film strain sensors based on interferometric optical measurementsCeasedAU745103B2 (en)

Applications Claiming Priority (3)

Application NumberPriority DateFiling DateTitle
US9798998P1998-08-261998-08-26
US60/0979891998-08-26
PCT/US1999/019601WO2000012960A1 (en)1998-08-261999-08-25Thin film strain sensors based on interferometric optical measurements

Publications (2)

Publication NumberPublication Date
AU5694999A AU5694999A (en)2000-03-21
AU745103B2true AU745103B2 (en)2002-03-14

Family

ID=22266087

Family Applications (1)

Application NumberTitlePriority DateFiling Date
AU56949/99ACeasedAU745103B2 (en)1998-08-261999-08-25Thin film strain sensors based on interferometric optical measurements

Country Status (7)

CountryLink
EP (1)EP1135667A1 (en)
JP (1)JP2002523764A (en)
KR (1)KR20010072920A (en)
CN (1)CN1314990A (en)
AU (1)AU745103B2 (en)
CA (1)CA2341166A1 (en)
WO (1)WO2000012960A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
MXPA04002266A (en)2001-09-142004-06-29Merck Patent GmbhMoulded bodies consisting of core-shell particles.
DE10204339A1 (en)2002-02-012003-08-07Merck Patent Gmbh Strain and compression sensor
DE10227071A1 (en)2002-06-172003-12-24Merck Patent Gmbh Composite material containing core-shell particles
US7645422B2 (en)*2003-04-112010-01-12Therm-O-Disc, IncorporatedVapor sensor and materials therefor
CN100442007C (en)*2003-08-212008-12-10台达电子工业股份有限公司Method and device for measuring film strain
CN101198851B (en)*2005-05-252010-04-14皇家墨尔本理工大学Polymer Strain Sensor
ITBO20070587A1 (en)*2007-08-132009-02-14Portu Goffredo De METHOD FOR MEASURING VOLTAGES IN A STRUCTURE OR IN A COMPONENT OF A WORKING STRUCTURE
KR102614323B1 (en)2015-04-012023-12-14바야비전 리미티드 Create a 3D map of a scene using passive and active measurements
ITUA20162508A1 (en)*2016-04-122017-10-12Safecertifiedstructure Ingegneria S R L Survey method and device for measuring stresses in an agglomerate structure
US10445928B2 (en)2017-02-112019-10-15Vayavision Ltd.Method and system for generating multidimensional maps of a scene using a plurality of sensors of various types
CN110307921B (en)*2019-07-022021-01-22运城学院Pressure sensor
US11402510B2 (en)2020-07-212022-08-02Leddartech Inc.Systems and methods for wide-angle LiDAR using non-uniform magnification optics
CA3125623C (en)2020-07-212023-06-27Leddartech Inc.Beam-steering device particularly for lidar systems
US11828853B2 (en)2020-07-212023-11-28Leddartech Inc.Beam-steering device particularly for LIDAR systems

Citations (1)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US5120966A (en)*1988-07-121992-06-09Dainippon Screen Mfg. Co., Ltd.Method of and apparatus for measuring film thickness

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US5120966A (en)*1988-07-121992-06-09Dainippon Screen Mfg. Co., Ltd.Method of and apparatus for measuring film thickness

Also Published As

Publication numberPublication date
EP1135667A1 (en)2001-09-26
CA2341166A1 (en)2000-03-09
WO2000012960A1 (en)2000-03-09
KR20010072920A (en)2001-07-31
CN1314990A (en)2001-09-26
AU5694999A (en)2000-03-21
JP2002523764A (en)2002-07-30

Similar Documents

PublicationPublication DateTitle
AU745103B2 (en)Thin film strain sensors based on interferometric optical measurements
US20070116402A1 (en)Humidity sensor and method for monitoring moisture in concrete
Torres et al.Analysis of the strain transfer in a new FBG sensor for structural health monitoring
US20070065071A1 (en)Humidity sensor and method for monitoring moisture in concrete
US20070058898A1 (en)Humidity sensor and method for monitoring moisture in concrete
US6069985A (en)Cross-fiber Bragg grating transducer
US20070280583A1 (en)Fiber Optic Force Sensor for Measuring Shear Force
Costa et al.Fiber optic based monitoring system applied to a centenary metallic arch bridge: Design and installation
Motwani et al.Experimental investigation of strain sensitivity for surface bonded fibre optic sensors
CA2301247A1 (en)Optical nose
CN108844919A (en)The reflection type inclined fiber grating index sensor of covering and production, measurement method
Singh et al.Design of corrosion sensors by using 1D quaternary photonic crystal with defect layer
US5900556A (en)Helical optical fiber strain sensor
Chryssis et al.Increased sensitivity and parametric discrimination using higher order modes of etched-core fiber Bragg grating sensors
JP2003344183A (en) Fiber grating type temperature sensor and temperature measurement system
Mufti et al.Field assessment of fibre-optic Bragg grating strain sensors in the Confederation Bridge
US6850315B1 (en)Intensity-based optical waveguide sensor
WO2005083379A1 (en)Multi-arm fiber optic sensor
Yan et al.Development of flexible pressure sensing polymer foils based on embedded fibre Bragg grating sensors
Caucheteur et al.Use of weakly tilted fiber Bragg gratings for sensing purposes
CN1424560A (en)Temperature stress sensor of composite structure fiber grating and preparation method thereof
AU754096C (en)Active strain gages for earthquake damage assessment
Yan et al.Characterisation of tactile sensors based on fibre Bragg gratings towards temperature independent pressure sensing
Rivera et al.Comparison of recoated fiber Bragg grating sensors under tension on a steel coupon
Okabe et al.Detection of transverse cracks in composites by using embedded FBG sensors

Legal Events

DateCodeTitleDescription
FGALetters patent sealed or granted (standard patent)

[8]ページ先頭

©2009-2025 Movatter.jp