Disclosure of Invention
The technical problem to be solved by the invention is as follows: aiming at the existing problems, the multipoint displacement testing method based on the fiber bragg grating sensing technology is simple to implement, high in measuring accuracy and capable of realizing on-line monitoring.
The technical scheme adopted by the invention is as follows: a multipoint displacement testing method based on fiber grating sensing technology is characterized in that: the fiber grating optical system comprises a carrier, an inclinometer, a fiber grating string I and a fiber grating string II;
mounting an inclinometer at one end of a carrier to be used as a displacement 0 point;
the fiber grating string I and the fiber grating string II are symmetrically arranged on two sides of the carrier about the central line of the carrier;
measuring the central wavelength lambda of the fiber grating string I and the fiber grating string IIBi0、λ’Bi0As an initial value; obtaining an initial angle θ of an inclinometer0;
When the carrier is deformed synchronously with the measured object, the central wavelength lambda of the fiber grating string I and the fiber grating string II is measuredBi1、λ’Bi1As test values; obtaining a test angle theta of a caster1;
Comparing the test value with the initial value, and calculating the strain variation delta epsilon of each point according to the sensing principle and the temperature compensation principle of the fiber Bragg gratingzi:
In the formula, Pe is the elasto-optic coefficient;
according to the strain variation of each point and the theory of mechanics of materials, the displacement y of each point is obtainediComprises the following steps:
Δθ0=θ1-θ0;
in the formula,. DELTA.xiThe distance between the upper and lower measuring sections along the length direction of the measured object; r is half of the distance between two symmetrical strain measuring points on the section of the measured object.
The fiber grating can not only sense strain, but also transmit signals, and a plurality of fiber grating sensors are connected in series to form a fiber grating string for distributed strain observation. The optical fiber sensing technology has the outstanding advantages of light weight, small diameter, strong electromagnetic interference resistance, corrosion resistance, high temperature resistance, small signal attenuation, integration of information sensing and information transmission and the like, and can realize strain measurement on a measured object.
The invention has the beneficial effects that: the invention installs an inclinometer at one end of the object to be measured, sets two groups of fiber grating strings which are linearly distributed and are symmetrically arranged by taking the central line as the axis, and measures the compressive strain and the tensile strain of each interface in real time, thereby calculating the deflection of the object to be measured, realizing the real-time monitoring of the stability of the object to be measured and ensuring the safety of engineering.
The invention utilizes the fiber grating sensing technology and combines the goniometer to measure the multi-point displacement, overcomes the defect that the traditional displacement measuring method needs to waste a large amount of labor, and has convenient installation, high measuring precision and lower cost.
Detailed Description
The embodiment is a multipoint displacement testing method based on a fiber grating sensing technology, which comprises a carrier, an inclinometer 1, a fiber grating string I3 and a fiber grating string II 4, and comprises the following specific steps:
s01, mounting the inclinometer 1 at one end of the carrier (shown in figure 1) as a displacement 0 point;
s02, symmetrically installing the fiber grating string I3 and the fiber grating string II 4 on two sides of the carrier (see figure 2) relative to the central line of the carrier;
s03, acquiring the initial angle theta of the declination angle gauge 1 in the initial state0(ii) a Measuring the initial central wavelength of the fiber grating string I3 in the initial state as lambdaB10,λB20,λB30,……,λBi0,……,λBm0The initial center wavelength of the fiber grating string II 4 in the initial state is lambda'B10,λ’B20,λ’B30,……,λ’Bi0,……,λ’Bm0;
S04, obtaining the testing angle theta of the caster 1 after the carrier synchronously deforms with the object 2 to be tested1(ii) a Measuring the central wavelengths of the deformed fiber grating strings I3 as lambda respectivelyB11,λB21,λB31,……,λBi1,……,λBm1The center wavelengths of the fiber grating strings II 4 are respectively lambda'B11,λ’B21,λ’B31,……,λ’Bi1,……,λ’Bm1;
S05, comparing the test value with the initial value according to the optical fiberCalculating the strain variation delta epsilon of each point according to the Bragg grating sensing principle and the temperature compensation principlezi:
1. Fiber bragg grating sensing principle
The fiber Bragg grating sensor is one functional fiber sensor with fiber Bragg grating as sensitive element. According to the optical fiber coupling mode theory, when a beam of broadband light passes through the fiber grating, mode coupling is generated, when the Bragg condition is met, the grating plays the role of a reflector and reflects a narrow-band light wave (the rest wavelengths are transmitted continuously through the fiber grating), and the central wavelength of the narrow-band light wave is the Bragg wavelength lambda of the gratingB。
λB=2neffΛ (1)
When the grating is subjected to the action of external temperature, strain and the like, the lambada and the neffThe consequent changes Δ Λ and Δ neffResulting in a shift of the reflection wavelength by Δ λ in accordance with the Bragg conditionB。
ΔλB=2ΔneffΛ+2neffΔΛ (2)
The above formula is the mechanism of grating sensing monitoring, and the displacement delta lambda of the central wavelength of the reflected wave meeting the Bragg condition is monitoredBThe external detected signals such as temperature, strain, stress and the like acting on the fiber bragg grating are detected.
The shift generated by the central wavelength of the fiber grating is as follows:
in the formula ∈ZFor axial strain, PeIs the coefficient of elasticity, alpha∧Is the coefficient of thermal expansion, alpha, of the optical fibernIndicating the thermo-optic coefficient, and Δ T is the amount of change in temperature.
2. Principle of temperature compensation
The multipoint displacement testing device adopts a design of two fiber bragg gratings, the FBGs 1 and the FBG2 are symmetrically arranged on two sides of the same section of the carrier respectively, and the temperature self-compensation of the FBG1 by the FBG2 can be realized. The thermal expansion coefficient and thermo-optic coefficient of FBGs 1 and 2 are the same, and therefore the temperature sensitivity coefficients of both are also the same. It can be seen from the structural design that the shift of the center wavelength is independent of temperature and only changes with the change of strain. The difference of the central wavelength drifts of the two fiber gratings is as follows:
from the above, the amount of change in strain Δ ∈ at each point in the present embodimentziCan be expressed by the following formula:
s06, obtaining the displacement y of each point according to the strain variation of each point and the mechanics theory of materialsiComprises the following steps:
from the theory of material mechanics, it can be known that:
angle of rotation theta of a certain cross section of the object 2 relative to an adjacent cross sectioniStrain difference delta epsilon of two symmetrical points on the sectioniThe relationship of (1) is:
in the formula,. DELTA.xiThe distance between the upper and lower measuring sections along the length direction of the object 2 to be measured; r is half of the distance between two symmetrical strain measuring points on the corresponding section of the object 2 to be measured.
Combining the equations (3) and (7), assuming that the change amount of the inclination angle measured by the inclinometer 1 is Δ θ0And the displacement of the bottom is 0, then the displacement y of a certain section on the measured object 2 is obtainediComprises the following steps:
the displacement yi of each point on the object 2 to be measured in this embodiment is represented by the following formula:
Δθ0=θ1-θ0; (10)
the carrier in this embodiment is a flexible material with a certain rigidity, the deformation modulus of which is slightly smaller than that of soil, and the carrier can be a tubular substance made of PVC material, such as a PVC inclinometer pipe. When the displacement of the deep part is tested, the fiber grating can not be directly arranged on the tested object, the fiber grating is fixedly arranged on the carrier firstly through a carrier, and then the carrier provided with the fiber grating is wrapped with the tested object, so that the tested object and the carrier synchronously deform, the strain on the carrier is the strain of the tested object, and the strain of the carrier is equal to the strain of the tested object in the fiber grating test.