CN111366111B - Strain sensor composed of three LGS surface acoustic wave resonators and testing method - Google Patents

Strain sensor composed of three LGS surface acoustic wave resonators and testing method Download PDF

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CN111366111B
CN111366111B CN202010239329.9A CN202010239329A CN111366111B CN 111366111 B CN111366111 B CN 111366111B CN 202010239329 A CN202010239329 A CN 202010239329A CN 111366111 B CN111366111 B CN 111366111B
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lgs
surface acoustic
acoustic wave
strain
temperature
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CN111366111A (en
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彭斌
刘孟轩
李凌
张万里
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University of Electronic Science and Technology of China
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B17/00Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
    • G01B17/04Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations for measuring the deformation in a solid, e.g. by vibrating string
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/16Measuring force or stress, in general using properties of piezoelectric devices
    • G01L1/162Measuring force or stress, in general using properties of piezoelectric devices using piezoelectric resonators
    • G01L1/165Measuring force or stress, in general using properties of piezoelectric devices using piezoelectric resonators with acoustic surface waves
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L25/00Testing or calibrating of apparatus for measuring force, torque, work, mechanical power, or mechanical efficiency

Abstract

The invention belongs to the field of design of surface acoustic wave sensors, and particularly relates to a strain sensor consisting of three LGS surface acoustic wave resonators and a measuring method. Firstly, establishing a relational expression of three resonant frequencies changing along with temperature and strain by using three LGS surface acoustic wave resonators; then according to the characteristics that the surface acoustic wave resonators have the same temperature coefficient and different strain coefficients in the same temperature environment, the changes of the resonant frequency caused by the coupling of the temperature and the temperature changes and the strain changes are eliminated; and finally, obtaining a relational expression between the resonance frequency and the strain change, and obtaining the magnitude delta epsilon of the strain change of the object to be measured through the relational expression. The invention completely eliminates the influence of temperature on the strain test and simultaneously improves the accuracy of the strain test. Can be used in any temperature environment, and is simple and easy to operate.

Description

Strain sensor composed of three LGS surface acoustic wave resonators and testing method
Technical Field
The invention belongs to the field of design of surface acoustic wave sensors, and particularly relates to a strain sensor consisting of three LGS surface acoustic wave resonators and a test method.
Background
The surface acoustic wave device is a device prepared by utilizing the propagation characteristic of surface acoustic waves, and mainly comprises a single substrate material and a surface transducer, wherein the transducer can excite the SAW device on a piezoelectric substrate through an inverse piezoelectric effect, the SAW is transmitted to the transducer in the piezoelectric substrate to be output, and is converted into an electric signal through the piezoelectric effect to be output.
A conventional strain sensor based on a SAW resonator generally comprises two quartz-based SAW resonators, and the relationship between the temperature T and the resonant frequency f of the SAW resonator is linear at a temperature of 20-80 ℃, specifically expressed as:
Figure BDA0002432031990000011
wherein b Δ T represents a first order term of temperature, and c represents a constant term of change in strain. However, when the temperature exceeds 80 ℃, the temperature T is no longer linear with the resonant frequency fIn this case, the strain cannot be accurately measured.
Recent research proposes that two SAW resonators with LGS as a substrate are adopted to form a strain sensor, the SAW resonators can eliminate the influence of temperature change on strain under the condition of small temperature change, such as the change range of-1-1 ℃, and when the temperature changes greatly, the first order coefficient of the strain and the temperature change present a linear function relationship. Therefore, the strain sensor composed of the two SAW resonators with the LGS as the substrate can test the strain in a high-temperature environment, but is limited to an environment with relatively stable temperature, and the strain cannot be accurately tested in an environment with relatively large temperature change.
Disclosure of Invention
In view of this, the invention provides a strain sensor composed of three LGS surface acoustic wave resonators and a test method thereof, which solve the problem in the related art that the strain sensor composed of the surface acoustic wave resonators performs strain test in an environment with large temperature variation.
According to an aspect of the present invention, there is provided a strain sensor composed of three LGS surface acoustic wave resonators, including: a first LGS surface acoustic wave resonator, a second LGS surface acoustic wave resonator, and a third LGS surface acoustic wave resonator; the first LGS surface acoustic wave resonator is arranged on an object to be detected along the same direction of the surface acoustic wave propagation direction and the main strain of the object to be detected, the second LGS surface acoustic wave resonator is arranged on the object to be detected along the vertical direction of the surface acoustic wave propagation direction and the main strain of the object to be detected, and the third LGS surface acoustic wave resonator is arranged on the object to be detected along the direction of the surface acoustic wave propagation direction and the main strain of the object to be detected in any angle direction, wherein any angle refers to an angle except the same direction and the vertical direction; the three LGS acoustic surface wave resonators are arranged at the same horizontal position of an object to be detected; the three LGS surface acoustic wave resonators comprise an LGS piezoelectric substrate, and interdigital fingers and electrodes arranged on the LGS piezoelectric substrate; the piezoelectric substrate materials of the three LGS surface acoustic wave resonators have the same tangential direction.
According to another aspect of the present invention, there is provided a method of testing a strain sensor composed of three LGS surface acoustic wave resonators, including the steps of:
step 1: the strain sensor composed of the three LGS surface acoustic wave resonators provided by the invention is firstly bonded on the same horizontal position of an object to be detected by using high-temperature-resistant inorganic glue.
Step 2: and connecting the three LGS surface acoustic wave resonators with a vector network analyzer by using a high-temperature coaxial line with an SMA connector at one end. One end with an SMA joint is connected with a vector network analyzer, the other end of the SMA joint is coaxially stripped and divided into three strands, and the three strands are respectively connected with three LGS surface acoustic wave resonators; under the condition of normal temperature, the initial resonant frequencies of three LGS surface acoustic resonators displayed by a vector network analyzer are respectively recorded: the first LGS SAW resonator is f0-0The second LGS SAW resonator is f0-90The third LGS SAW resonator is f0-x
And step 3: when the temperature rises to T, applying strain to a strain sensor consisting of an object to be measured and the three LGS surface acoustic wave resonators, and respectively recording the resonant frequencies of the three LGS surface acoustic wave resonators displayed by the vector network analyzer: the first LGS SAW resonator is f0-0', the second LGS SAW resonator is f0-90', the third LGS SAW resonator is f0-x′。
And 4, step 4: subtracting the initial resonant frequency corresponding to the step 2 from the resonant frequency recorded in the step 3, and respectively calculating the resonant frequency change value delta f of the first LGS surface acoustic wave resonator0And a resonance frequency variation value Deltaf of a second LGS surface acoustic wave resonator90And a resonance frequency variation value Deltaf of a third LGS surface acoustic wave resonatorx
Step 5, calculating the change result delta f of the resonant frequency according to the step 40、Δf90And Δ fxEstablishing relational expressions (4), (5) and (6) of resonant frequencies of the first, second and third LGS surface acoustic wave resonators with temperature change and strain change, respectively:
first LGS surface acoustic wave resonator:
Figure BDA0002432031990000021
second LGS surface acoustic wave resonator:
Figure BDA0002432031990000022
third LGS surface acoustic wave resonator:
Figure BDA0002432031990000023
wherein: Δ ε represents the change in strain, Δ f0、Δf90And Δ fxRespectively representing the variation values of the resonant frequencies of the first LGS surface acoustic wave resonator, the second LGS surface acoustic wave resonator and the third LGS surface acoustic wave resonator; f. of0-0、f0-90And f0-xRespectively representing initial resonant frequencies of the first, second and third LGS surface acoustic wave resonators; c. C0、c90And cxConstant terms representing strain variations of the first, second, and third LGS surface acoustic wave resonators, respectively; d0,d90,dxConstant terms respectively representing coupling terms of temperature change and strain change of the first LGS surface acoustic wave resonator, the second LGS surface acoustic wave resonator and the third LGS surface acoustic wave resonator; a Δ T2Represents a second order temperature term; b Δ T represents a first order temperature term; Δ T Δ ∈ is expressed as a temperature change and strain change coupling term.
Step 6: eliminating the second order temperature term a delta T of each relation in step 5 by solving the system of equations2And a first order temperature term b Δ T, and then eliminating a temperature change and strain change coupling term Δ T Δ ε to obtain formula (11):
Figure BDA0002432031990000031
the strain change delta epsilon of the object to be measured can be obtained through the formula (11), and therefore the strain magnitude epsilon of the object to be measured can be obtained.
The theoretical analysis of the invention is as follows:
in the prior art, a strain sensor composed of two LGS surface acoustic wave resonators is used for strain testing in an environment with large temperature change, a coupling item can appear between the temperature and the strain, so that a measurement result and a result obtained by reacting a standard strain gauge are greatly different, and therefore the strain sensor composed of the two LGS surface acoustic wave resonators is not suitable for the strain testing in the environment with large temperature change. Based on the result of analyzing the experimental data of the strain sensor consisting of the two LGS surface acoustic wave resonators, the relationship between the change of the resonant frequency along with the temperature and the change of the strain is re-determined, and the formula (1) is obtained:
Figure BDA0002432031990000032
in the formula (1), a.DELTA.T2Representing a second-order temperature term, b Δ T a first-order temperature term, s a strain frequency coefficient of the surface acoustic wave resonator, Δ ε a strain change, f0Representing the resonant frequency of the SAW device at room temperature and deltaf representing the change in resonant frequency. Meanwhile, the strain frequency coefficient of the surface acoustic wave resonator and the change of the temperature present a linear relation, and the relation is specifically shown in formula (2):
s=c+dΔT (2)
in the formula (2), c represents a constant term of a strain change, and d represents a constant term of a coupling term of a temperature change and a strain change.
The formula (2) is substituted for the formula (1), and the relation formula (3) of the resonant frequency of the surface acoustic wave resonator along with the temperature change and the strain change can be obtained:
Figure BDA0002432031990000033
according to the formula (3), the relations (4), (5) and (6) of the resonant frequencies of the first, second and third LGS surface acoustic wave resonators with the changes of temperature and strain are respectively established:
first LGS surface acoustic wave resonator:
Figure BDA0002432031990000034
second LGS surface acoustic wave resonator:
Figure BDA0002432031990000035
third LGS surface acoustic wave resonator:
Figure BDA0002432031990000036
subtracting the formula (5) from the formula (4), subtracting the formula (5) from the formula (6), and eliminating the second-order temperature term a Δ T2And the first order temperature term b Δ T, yielding formula (7) and formula (8):
Figure BDA0002432031990000037
Figure BDA0002432031990000038
constant term d obtained by dividing temperature change and strain change coupling term by equation (7)0-d90Equation (8) divided by the constant term d of the temperature change and strain change coupling termx-d90To give formulae (9) and (10):
Figure BDA0002432031990000039
Figure BDA0002432031990000041
subtracting the formula (10) from the formula (9), eliminating the coupling term delta T delta epsilon of the temperature change and the strain change, and finally eliminating the influence of the temperature change in the strain test to obtain a relational expression (11) of the resonant frequency and the strain change of the object to be tested:
Figure BDA0002432031990000042
the strain change delta epsilon of the object to be measured can be obtained through the formula (11), and therefore the strain magnitude epsilon of the object to be measured can be obtained.
In the formula (11), the unknown coefficient has Δ f0、Δf90、ΔfxAnd Δ ε;wherein Δ f0、Δf90And Δ fxThe strain change delta epsilon of the object to be tested can be obtained from the vector network analyzer through the test result, and can be obtained only by substituting the test result into the formula (11).
In summary, a strain sensor and a test method using three LGS surface acoustic wave resonators establish a relational expression of three resonant frequencies with temperature change and strain change by using the three LGS surface acoustic wave resonators, and then according to the characteristics that the three LGS surface acoustic wave resonators have the same temperature coefficient and different strain coefficients in the same temperature environment, the influence of temperature and temperature change on strain test is eliminated, and the accuracy of the strain test is improved. Is suitable for any temperature environment, and is simple and easy to operate.
Drawings
FIG. 1 shows placement positions of three LGS-based surface acoustic wave resonators according to an embodiment;
FIG. 2 is a graph showing the change of resonant frequency with strain at different test temperatures according to this embodiment.
Detailed Description
For better understanding of the present invention, the technical solution of the present invention will be described in detail with specific examples, but the present invention is not limited thereto.
The surface acoustic wave resonator comprises an LGS piezoelectric substrate, and an electrode 4 and an interdigital 5 which are arranged on the LGS piezoelectric substrate; the piezoelectric substrate is made of LGS (lanthanum gallium silicate) material with the tangential direction of (0 degrees, 138.5 degrees and 26.6 degrees), the size of the substrate is 6mm multiplied by 6mm, and the thickness of the substrate is 0.5 mm; and growing an Au electrode on the substrate by adopting an electron beam evaporation technology. The specific sensing mode of the surface acoustic wave resonator is the piezoelectric effect.
The three LGS surface acoustic wave resonators are combined into a strain sensor, and the strain sensor comprises: a first LGS surface acoustic wave resonator, a second LGS surface acoustic wave resonator, and a third LGS surface acoustic wave resonator. The three LGS surface acoustic wave resonators are arranged on an object to be detected according to the diagram shown in figure 1, wherein a first LGS surface acoustic wave resonator 1 is arranged on the object to be detected along the surface acoustic wave propagation direction of the first LGS surface acoustic wave resonator and the main strain direction of the object to be detected at an angle of 0 degrees; the second LGS surface acoustic wave resonator 2 is arranged on the object to be detected, and forms an angle of 90 degrees with the main strain vertical direction of the object to be detected along the surface acoustic wave propagation direction; and the third LGS surface acoustic wave resonator 3 is arranged on the object to be detected, and forms an angle of 30 degrees with the main strain direction of the object to be detected along the surface acoustic wave propagation direction of the third LGS surface acoustic wave resonator. The three LGS acoustic surface wave resonators are arranged at the same horizontal position of an object to be detected; the three LGS surface acoustic wave resonators comprise an LGS piezoelectric substrate, and interdigital fingers and electrodes arranged on the LGS piezoelectric substrate; the piezoelectric substrate materials of the three LGS surface acoustic wave resonators have the same tangential direction.
In order to simplify the testing process, three LGS surface acoustic wave resonators are usually connected in parallel by a platinum wire or high-temperature silver paste, and then are respectively connected to the same vector network analyzer, and the resonant frequency changes of the three LGS surface acoustic wave resonators are obtained at the same time. In addition, the three LGS surface acoustic wave resonators may not be connected at all, and in this way, the three LGS surface acoustic wave resonators need to be connected to a vector network analyzer respectively to obtain three surface acoustic wave resonant frequency changes. However, when a strain sensor composed of three LGS surface acoustic wave resonators is used for strain testing, the three LGS surface acoustic wave resonators are required to be in the same temperature environment regardless of the manner used.
In this embodiment, a method for testing a strain sensor including three LGS surface acoustic wave resonators is also provided, and the strain of a rectangular alloy plate is tested by the method, and the specific test steps are as follows:
step 1: the strain sensor composed of three LGS surface acoustic wave resonators provided by the invention is firstly bonded on the same horizontal position of a rectangular alloy plate by using high-temperature-resistant inorganic glue.
Step 2: and connecting the three LGS surface acoustic wave resonators with a vector network analyzer by using a high-temperature coaxial line with an SMA connector at one end. One end with an SMA joint is connected with a vector network analyzer, the other end of the SMA joint is coaxially stripped and divided into three strands, and the three strands are respectively connected with three LGS surface acoustic wave resonators; under the condition of normal temperature, vector is recorded respectivelyInitial resonance frequencies of three LGS surface acoustic resonators as displayed by the quantum network analyzer: initial resonant frequency f of first LGS surface acoustic wave resonator0-0221.286MHz, the initial resonant frequency f of the second LGS SAW resonator0-90227.583MHz, the initial resonant frequency f of the third LGS SAW resonator0-30Is 224.356 MHz.
And step 3: when the temperature rises to 225 ℃, applying strain to a strain sensor consisting of an object to be tested and three LGS surface acoustic wave resonators; the resonant frequencies of the three LGS surface acoustic resonators displayed by the vector network analyzer at this time were recorded separately: first LGS surface acoustic wave resonator f0-0' 221.313MHz, second LGS SAW resonator f0-90' 227.606MHz, third LGS SAW resonator f0-30′=224.382MHz。
And 4, step 4: correspondingly subtracting the initial resonant frequency obtained in the step 2 from the resonant frequency obtained by the three LGS surface acoustic wave resonators in the step 3 to obtain a resonant frequency change value delta f of the first LGS surface acoustic wave resonator0And a resonance frequency variation value Deltaf of a second LGS surface acoustic wave resonator90And a resonance frequency variation value Deltaf of a third LGS surface acoustic wave resonator30
Step 5, changing the resonant frequency change value delta f of the three LGS surface acoustic wave resonators calculated in the step 40、Δf90And Δ f30Formula (11):
Figure BDA0002432031990000051
the calculation was carried out to obtain the magnitude of the strain change Δ ∈ of the rectangular alloy sheet, and finally the magnitude of strain ∈ of the rectangular alloy sheet was 491.459863 μ ∈.
To verify the correctness and feasibility of equation (11), the test of a standard strain gauge was added to the above example and the error between the two was calculated. The standard strain gauge shows that the strain of the rectangular alloy plate is 493 mu epsilon at the temperature T of 225 ℃; comparing the two, the error of the calculation result is only 0.3% by adopting the method provided by the invention. It can be seen that the strain calculated by the theoretical expression of the present invention substantially matches the results shown by the standard strain gauge.
For the present embodiment, the strain sensor is tested at different temperatures, and the results of strain change and frequency change are shown in fig. 2, and when the temperature changes, the relationship between the resonant frequency and the strain is still linear, which indicates that the strain sensor and the testing method provided by the present invention, which are composed of three LGS surface acoustic wave resonators, completely eliminate the influence of temperature change, and the results are more accurate compared with the prior art.

Claims (2)

1. A test method for performing strain test by using three LGS surface acoustic wave resonators is characterized in that: the method comprises the following steps:
step 1: firstly, adhering a strain sensor consisting of three LGS surface acoustic wave resonators on the same horizontal position of an object to be detected by using high-temperature-resistant inorganic glue;
step 2: connecting three LGS surface acoustic wave resonators and a vector network analyzer by using a high-temperature coaxial line with an SMA joint at one end; one end with an SMA joint is connected with a vector network analyzer, the other end of the SMA joint is coaxially stripped and divided into three strands, and the three strands are respectively connected with three LGS surface acoustic wave resonators; under the condition of normal temperature, the initial resonant frequencies of three LGS surface acoustic resonators displayed by a vector network analyzer are respectively recorded: the first LGS SAW resonator is f0-0The second LGS SAW resonator is f0-90The third LGS SAW resonator is f0-x
And step 3: when the temperature rises to T, applying strain to a strain sensor consisting of an object to be measured and the three LGS surface acoustic wave resonators, and respectively recording the resonant frequencies of the three LGS surface acoustic wave resonators displayed by the vector network analyzer: the first LGS SAW resonator is f0-0', the second LGS SAW resonator is f0-90', the third LGS SAW resonator is f0-x′;
And 4, step 4: subtracting the initial resonant frequency corresponding to the step 2 from the resonant frequency recorded in the step 3, and respectively calculating the resonant frequency of the first LGS surface acoustic wave resonatorRate change value Δ f0And a resonance frequency variation value Deltaf of a second LGS surface acoustic wave resonator90And a resonance frequency variation value Deltaf of a third LGS surface acoustic wave resonatorx
Step 5, calculating the change result delta f of the resonant frequency according to the step 40、Δf90And Δ fxEstablishing relational expressions (4), (5) and (6) of resonant frequencies of the first, second and third LGS surface acoustic wave resonators with temperature change and strain change, respectively:
first LGS surface acoustic wave resonator:
Figure FDA0003310019810000011
second LGS surface acoustic wave resonator:
Figure FDA0003310019810000012
third LGS surface acoustic wave resonator:
Figure FDA0003310019810000013
wherein: Δ ε represents the change in strain, Δ f0、Δf90And Δ fxRespectively representing the variation values of the resonant frequencies of the first LGS surface acoustic wave resonator, the second LGS surface acoustic wave resonator and the third LGS surface acoustic wave resonator; f. of0-0、f0-90And f0-xRespectively representing initial resonant frequencies of the first, second and third LGS surface acoustic wave resonators; c. C0、c90And cxConstant terms representing strain variations of the first, second, and third LGS surface acoustic wave resonators, respectively; d0,d90,dxConstant terms respectively representing coupling terms of temperature change and strain change of the first LGS surface acoustic wave resonator, the second LGS surface acoustic wave resonator and the third LGS surface acoustic wave resonator; a Δ T2Represents a second order temperature term; b Δ T represents a first order temperature term; Δ T Δ ∈ is expressed as a temperature change and strain change coupling term;
step 6: eliminating the second order temperature term a delta T of each relation in step 5 by solving the system of equations2And a first order temperature term b Δ T, then decoupling the temperature change from the strain changeThe term Δ T Δ ∈, yielding formula (11):
Figure FDA0003310019810000021
the strain change delta epsilon of the object to be measured can be obtained through the formula (11), and therefore the strain magnitude epsilon of the object to be measured can be obtained.
2. A strain sensor composed of three LGS surface acoustic wave resonators, for use in the test method for performing strain test according to claim 1, characterized in that: the strain sensor includes: a first LGS surface acoustic wave resonator, a second LGS surface acoustic wave resonator, and a third LGS surface acoustic wave resonator; the first LGS surface acoustic wave resonator is arranged on an object to be detected along the same direction of the surface acoustic wave propagation direction and the main strain of the object to be detected, the second LGS surface acoustic wave resonator is arranged on the object to be detected along the vertical direction of the surface acoustic wave propagation direction and the main strain of the object to be detected, and the third LGS surface acoustic wave resonator is arranged on the object to be detected along the direction of the surface acoustic wave propagation direction and the main strain of the object to be detected in any angle direction, wherein any angle refers to an angle except the same direction and the vertical direction; the three LGS acoustic surface wave resonators are arranged at the same horizontal position of an object to be detected; the three LGS surface acoustic wave resonators comprise an LGS piezoelectric substrate, and interdigital fingers and electrodes arranged on the LGS piezoelectric substrate; the piezoelectric substrate materials of the three LGS surface acoustic wave resonators have the same tangential direction.
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