WO2017199542A1 - 構造物評価システム、構造物評価装置及び構造物評価方法 - Google Patents

構造物評価システム、構造物評価装置及び構造物評価方法 Download PDF

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WO2017199542A1
WO2017199542A1 PCT/JP2017/008818 JP2017008818W WO2017199542A1 WO 2017199542 A1 WO2017199542 A1 WO 2017199542A1 JP 2017008818 W JP2017008818 W JP 2017008818W WO 2017199542 A1 WO2017199542 A1 WO 2017199542A1
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Prior art keywords
elastic wave
evaluation
distribution
region
unit
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English (en)
French (fr)
Japanese (ja)
Inventor
渡部　一雄
英文 高峯
塩谷　智基
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Toshiba Corp
Kyoto University NUC
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Toshiba Corp
Kyoto University NUC
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Priority to JP2017514721A priority Critical patent/JP6366826B2/ja
Priority to CN201780000107.8A priority patent/CN107850579B/zh
Priority to EP17707456.4A priority patent/EP3264076B1/en
Priority to US15/454,101 priority patent/US10330646B2/en
Publication of WO2017199542A1 publication Critical patent/WO2017199542A1/ja
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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/14—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object using acoustic emission techniques
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0008—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of bridges
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0066—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by exciting or detecting vibration or acceleration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04—Analysing solids
    • G01N29/043—Analysing solids in the interior, e.g. by shear waves
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04—Analysing solids
    • G01N29/07—Analysing solids by measuring propagation velocity or propagation time of acoustic waves
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22—Details, e.g. general constructional or apparatus details
    • G01N29/24—Probes
    • G01N29/2437—Piezoelectric probes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/44—Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4409—Processing the detected response signal, e.g. electronic circuits specially adapted therefor by comparison
    • G01N29/4436—Processing the detected response signal, e.g. electronic circuits specially adapted therefor by comparison with a reference signal
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/44—Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4445—Classification of defects
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/44—Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4463—Signal correction, e.g. distance amplitude correction [DAC], distance gain size [DGS], noise filtering
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00—Indexing codes associated with group G01N29/00
    • G01N2291/02—Indexing codes associated with the analysed material
    • G01N2291/023—Solids
    • G01N2291/0232—Glass, ceramics, concrete or stone
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00—Indexing codes associated with group G01N29/00
    • G01N2291/02—Indexing codes associated with the analysed material
    • G01N2291/025—Change of phase or condition
    • G01N2291/0258—Structural degradation, e.g. fatigue of composites, ageing of oils
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00—Indexing codes associated with group G01N29/00
    • G01N2291/02—Indexing codes associated with the analysed material
    • G01N2291/028—Material parameters
    • G01N2291/0289—Internal structure, e.g. defects, grain size, texture

Definitions

  • Embodiments of the present invention relate to a structure evaluation system, a structure evaluation apparatus, and a structure evaluation method.
  • AE Acoustic Emission
  • AE is an elastic wave generated with the progress of fatigue cracks in the material.
  • AE electrostic Emission
  • an elastic wave is detected as an AE signal (voltage signal) by an AE sensor using a piezoelectric element.
  • the AE signal is detected as an indication before material breakage occurs. Therefore, the occurrence frequency and signal intensity of the AE signal are useful as an index representing the soundness of the material. For this reason, research is being conducted on techniques for detecting signs of deterioration of structures by the AE method.
  • the problem to be solved by the present invention is to provide a structure evaluation system, a structure evaluation apparatus, and a structure evaluation method capable of evaluating the soundness of a structure that generates elastic waves.
  • the structure evaluation system of the embodiment includes a plurality of AE sensors, a signal processing unit, a position locating unit, a speed calculation unit, and an evaluation unit.
  • the AE sensor detects elastic waves generated from the structure.
  • the signal processing unit extracts an AE signal including information on the elastic wave by performing signal processing on the elastic wave detected by the AE sensor.
  • the position locating unit derives a transmission source distribution representing the distribution of the elastic wave transmission sources generated in the structure based on the AE signal.
  • the velocity calculation unit derives a propagation velocity of the elastic wave generated in the structure based on the AE signal.
  • An evaluation part evaluates the soundness of the said structure based on the said transmission source distribution and the propagation velocity of the said elastic wave.
  • FIG. 1 is a diagram illustrating a system configuration of a structure evaluation system 100 according to an embodiment.
  • the structure evaluation system 100 is used for evaluating the soundness of a structure.
  • a bridge is described as an example of a structure, but the structure need not be limited to a bridge.
  • the structure may be any structure as long as an elastic wave is generated due to the occurrence or development of a crack or an external impact (for example, rain, artificial rain, etc.).
  • Bridges are not limited to structures laid on rivers and valleys, but also include various structures (for example, highway viaducts) provided above the ground.
  • the structure evaluation system 100 includes a plurality of AE sensors 10-1 to 10-n (n is an integer of 2 or more), a signal processing unit 11, and a structure evaluation apparatus 20.
  • the signal processing unit 11 and the structure evaluation apparatus 20 are connected to be communicable by wire or wirelessly.
  • the AE sensors 10-1 to 10-n are referred to as AE sensors 10 when not distinguished from each other.
  • the AE sensor 10 is installed in a structure.
  • the AE sensor 10 is installed on a concrete floor slab of a bridge.
  • the AE sensor 10 includes a piezoelectric element, detects an elastic wave (AE wave) generated by a structure, and converts the detected elastic wave into a voltage signal (AE source signal).
  • the AE sensor 10 performs processing such as amplification and frequency limitation on the AE source signal and outputs the signal to the signal processing unit 11.
  • the signal processing unit 11 receives the AE source signal processed by the AE sensor 10 as an input.
  • the signal processing unit 11 extracts an AE feature amount including information on an elastic wave by performing signal processing such as noise removal and parameter extraction required on the input AE source signal.
  • the information on the elastic wave is information such as the amplitude, energy, rise time, duration, frequency, zero cross count number, etc. of the AE source signal.
  • the signal processing unit 11 outputs information based on the extracted AE feature amount to the structure evaluation apparatus 20 as an AE signal.
  • the AE signal output from the signal processing unit 11 includes information such as sensor ID, AE detection time, AE source signal amplitude, energy, rise time, and frequency.
  • the amplitude of the AE source signal is, for example, a maximum amplitude value among elastic waves.
  • the energy is, for example, a value obtained by time integration of the square of the amplitude at each time point.
  • the definition of energy is not limited to the above example, and may be approximated using, for example, a waveform envelope.
  • the rise time is, for example, a time T1 until the elastic wave rises from a zero value exceeding a predetermined value set in advance.
  • the duration is, for example, the time from when the rise of the elastic wave starts until the amplitude becomes smaller than a preset value.
  • the frequency is the frequency of the elastic wave.
  • the zero cross count number is, for example, the number of times the elastic wave crosses a reference line passing through a zero value.
  • the structure evaluation apparatus 20 includes a CPU (Central Processing Unit), a memory, an auxiliary storage device, and the like connected by a bus, and executes an evaluation program. By executing the evaluation program, the structure evaluation device 20 functions as a device including a position locating unit 201, a speed calculation unit 202, an evaluation unit 203, and a display unit 204. Note that all or a part of each function of the structure evaluation apparatus 20 may be realized by using hardware such as ASIC (Application Specific Integrated Circuit), PLD (Programmable Logic Device), and FPGA (Field Programmable Gate Array). .
  • the evaluation program may be recorded on a computer-readable recording medium.
  • the computer-readable recording medium is, for example, a portable medium such as a flexible disk, a magneto-optical disk, a ROM, a CD-ROM, or a storage device such as a hard disk built in the computer system.
  • the evaluation program may be transmitted / received via a telecommunication line.
  • the position locating unit 201 receives the AE signal output from the signal processing unit 11 as an input. In addition, the position locating unit 201 stores in advance information related to the installation position of the AE sensor 10 in the structure (hereinafter referred to as “sensor position information”) in association with the sensor ID.
  • the information regarding the installation position is, for example, latitude and longitude, or distances in the horizontal and vertical directions from a specific position of the structure.
  • the position locating unit 201 locates the AE generation source based on information such as sensor ID and AE detection time included in the input AE signal and sensor position information held in advance.
  • the position location unit 201 derives the AE seismic source density distribution (source distribution) using the position location results for a certain period.
  • the AE hypocenter density distribution represents a distribution in which the source of elastic waves generated in the structure is shown.
  • the position location unit 201 outputs the derived AE seismic source density distribution to the evaluation unit 203.
  • the speed calculation unit 202 receives the AE signal output from the signal processing unit 11 as an input.
  • the speed calculation unit 202 holds the sensor position information in advance in association with the sensor ID.
  • the velocity calculation unit 202 derives the elastic wave propagation velocity distribution of the structure based on information such as sensor ID and AE detection time included in the input AE signal and sensor position information held in advance.
  • the elastic wave propagation velocity distribution represents a distribution in which the propagation velocity of the elastic wave generated in the structure is shown.
  • the velocity calculation unit 202 derives the elastic wave propagation velocity distribution of the structure using the AE tomography analysis method.
  • the velocity calculation unit 202 outputs the derived elastic wave propagation velocity distribution to the evaluation unit 203.
  • the AE tomography analysis method detects the elastic wave generated from the structure with multiple AE sensors, locates the AE source, and measures the theoretical scanning time from the source to each sensor.
  • the propagation speed of the analysis model of the structure is corrected so that the scanning time error converges within an allowable value, and the elastic wave propagation speed distribution in the structure is obtained. Since the speed of AE which advances inside is reduced as the structure is deteriorated, the degree of deterioration inside the structure can be evaluated from the speed distribution of AE by using the AE tomography analysis method.
  • the evaluation unit 203 receives the AE seismic source density distribution output from the position location unit 201 and the elastic wave propagation velocity distribution output from the velocity calculation unit 202 as inputs.
  • the evaluation unit 203 evaluates the soundness of the structure based on the input AE seismic source density distribution and elastic wave propagation velocity distribution.
  • the evaluation unit 203 causes the display unit 204 to display the evaluation result.
  • the display unit 204 is an image display device such as a liquid crystal display or an organic EL (Electro Luminescence) display.
  • the display unit 204 displays the evaluation result according to the control of the evaluation unit 203.
  • the display unit 204 may be an interface for connecting the image display device to the structure evaluation device 20. In this case, the display unit 204 generates a video signal for displaying the evaluation result, and outputs the video signal to an image display device connected to itself.
  • FIG. 2A represents the AE source density distribution
  • FIG. 2B represents the elastic wave propagation velocity distribution.
  • the AE hypocenter density distribution and the elastic wave propagation velocity distribution are distributions obtained based on the same region of the same structure.
  • 2A and 2B show the results of using 15 AE sensors 10 for a floor slab of a certain road structure.
  • the horizontal axis and the vertical axis represent the horizontal length (mm) and the vertical length (mm) from a specific position of the structure to be evaluated.
  • FIG. 2B the horizontal axis and the vertical axis represent the horizontal length (m) and the vertical length (m) from a specific position of the structure to be evaluated.
  • FIG. 2A the richer the source (the denser the source), the darker the color, and the fewer the source (the sparser the source), the thinner.
  • a region 30 in FIG. 2A represents a region where the number of transmission sources is larger than other regions.
  • FIG. 2B the higher the propagation speed is, the darker it is, and the slower the propagation speed is, the thinner it is.
  • the AE source density distribution and elastic wave propagation velocity distribution shown in FIGS. 2A and 2B are input to the evaluation unit 203.
  • the evaluation unit 203 uses the input AE seismic source density distribution based on a reference value related to the density of the transmission source (hereinafter referred to as “density reference value”) and a region where the transmission source is sparse and a region where the transmission source is dense. It is divided into two areas. Specifically, the evaluation unit 203 classifies the region by binarizing the AE hypocenter density distribution based on the density reference value. In this embodiment, the density reference value is set to 0.5.
  • the evaluation unit 203 binarizes an area that is equal to or higher than the density reference value as an area where the transmission source is dense, and an area where the density is lower than the density reference value as an area where the transmission source is sparse. Divide the area.
  • the density reference value is not necessarily limited to the above value, and may be changed as appropriate.
  • the evaluation unit 203 uses the input elastic wave propagation velocity distribution based on a reference value related to the propagation velocity of the elastic wave (hereinafter referred to as “propagation velocity reference value”), a region having a high propagation velocity, and a propagation velocity. It is divided into two areas of low area. Specifically, the evaluation unit 203 classifies the region by binarizing the elastic wave propagation velocity distribution based on the propagation velocity reference value.
  • the propagation speed reference value is 3800 m / s.
  • the evaluation unit 203 binarizes a region having a propagation velocity higher than the propagation velocity reference value as a region having a higher propagation velocity and a region having a propagation velocity lower than the propagation velocity reference value as a region having a lower propagation velocity. To divide the area.
  • the propagation speed reference value is not necessarily limited to the above value, and may be changed as appropriate.
  • FIG. 3A shows the segmentation result of the AE source density distribution region
  • FIG. 3B shows the segmentation result of the elastic wave propagation velocity distribution region.
  • the diagram shown in FIG. 3A is described as a binarized AE source density distribution
  • the diagram shown in FIG. 3B is described as a binarized elastic wave propagation velocity distribution.
  • the evaluation unit 203 evaluates the soundness of the structure using the binarized AE seismic source density distribution and the binarized elastic wave propagation velocity distribution. Specifically, the evaluation unit 203 superimposes the binarized AE seismic source density distribution and the binarized elastic wave propagation velocity distribution on the soundness of the structure in accordance with the segmented result of the overlapped region. Assess in 4 stages.
  • specific examples of the four-stage evaluation include soundness, intermediate deterioration I, intermediate deterioration II, and limit deterioration. It shows that the deterioration of the structure progresses in the order of soundness, intermediate deterioration I, intermediate deterioration II, and limit deterioration.
  • the evaluation unit 203 evaluates whether each region (each overlapped region) of the structure corresponds to sound, intermediate deterioration I, intermediate deterioration II, or limit deterioration based on the following evaluation conditions.
  • the evaluation unit 203 evaluates the region as a healthy region. In addition, when the overlapping region is a region where the transmission sources are dense and the propagation speed is high, the evaluation unit 203 evaluates the region as a region of intermediate degradation I. Further, when the overlapping region is a region where the transmission sources are dense and the propagation speed is low, the evaluation unit 203 evaluates the region as a region of intermediate degradation II. In addition, when the overlapped area is an area where the transmission source is sparse and the propagation speed is low, the evaluation unit 203 evaluates the area as a marginal deterioration area.
  • the evaluation unit 203 evaluates whether each of the overlapped regions corresponds to sound, intermediate deterioration I, intermediate deterioration II, and limit deterioration, and the evaluation result of each region is indicated.
  • the evaluation result distribution is derived.
  • the evaluation unit 203 represents a healthy region by “1”, an intermediate degradation I region by “2”, an intermediate degradation II region by “3”, and a marginal degradation region. May be represented by “4”.
  • the evaluation unit 203 causes the display unit 204 to display the derived evaluation result distribution.
  • FIG. 4 is a diagram showing an example of the evaluation result distribution. As shown in FIG. 4, by displaying the evaluation result distribution, the worker or the administrator can easily grasp which region of the structure is being deteriorated.
  • FIG. 5 is a diagram showing a verification result of the validity of the evaluation result.
  • FIG. 5 shows the result of collecting and confirming the inside of the floor slab of the structure shown in FIG.
  • a core sample taken from the portion indicated by a circle 31 in the region “4” indicating the limit deterioration is shown in FIG.
  • FIG. 5A the progress of deterioration inside the core sample can be seen to the extent that the core is separated by horizontal cracks.
  • the core sample taken from the portion of the circle 32 in the region “1” representing the sound is FIG. 5B.
  • no cracks are visually confirmed inside the core sample.
  • the effectiveness of the evaluation method by the structure evaluation apparatus 20 was confirmed.
  • FIG. 6 is a sequence diagram illustrating a processing flow of the structure evaluation system 100.
  • each AE sensor 10 and the signal processing unit 11 are sensor units.
  • Each AE sensor 10 detects an elastic wave (AE wave) generated by the structure (step S101).
  • the AE sensor 10 converts the detected elastic wave into a voltage signal (AE source signal), performs processing such as amplification and frequency limitation on the AE source signal, and outputs the signal to the signal processing unit 11.
  • the signal processing unit 11 performs signal processing such as necessary noise removal and parameter extraction on the input AE source signal (step S102).
  • the signal processing unit 11 outputs information based on the AE feature amount extracted by performing signal processing to the structure evaluation apparatus 20 as an AE signal (step S103). Steps S101 to S103 are executed for a predetermined period.
  • the position location unit 201 locates the AE generation source based on the AE signal output from the signal processing unit 11 and sensor position information held in advance (step S104). The position location unit 201 performs the process of step S104 for a predetermined period. And the position location part 201 derives
  • the velocity calculation unit 202 derives the elastic wave propagation velocity distribution of the structure based on the AE signal output from the signal processing unit 11 (step S106). For example, the velocity calculation unit 202 may derive an elastic wave propagation velocity distribution using an AE signal for a predetermined period, or an elastic wave propagation velocity distribution using an AE signal for a period shorter than the predetermined period. May be derived. The velocity calculation unit 202 outputs the derived elastic wave propagation velocity distribution to the evaluation unit 203. Note that step S105 and step S106 are in no particular order.
  • the evaluation unit 203 binarizes the AE source density distribution output from the position location unit 201 and the elastic wave propagation velocity distribution output from the velocity calculation unit 202, thereby binarizing the AE source density distribution. And a binarized elastic wave propagation velocity distribution are derived (step S107).
  • the evaluation unit 203 derives the evaluation result distribution by evaluating each region of the structure based on the evaluation condition using the derived binarized AE seismic source density distribution and the binarized elastic wave propagation velocity distribution. (Step S108).
  • the evaluation unit 203 causes the display unit 204 to display the derived evaluation result distribution.
  • the display unit 204 displays the evaluation result distribution according to the control of the evaluation unit 203 (step S109).
  • FIG. 7 is a diagram showing a basic concept of soundness evaluation by the structure evaluation apparatus 20 in the present embodiment.
  • the level of elastic wave propagation speed and the density of AE seismic source density are each divided into four quadrants using a two-dimensional evaluation axis.
  • the structure evaluation apparatus 20 classify
  • the conventional evaluation method and the evaluation method in this embodiment are compared.
  • Fig. 8A shows the evaluation based only on the AE hypocenter location
  • Fig. 8B shows the evaluation based only on the propagation velocity.
  • the evaluation based only on the AE seismic source location indicates that the possibility that the structure is deteriorated is higher as the AE seismic source is sparser and denser.
  • the evaluation based only on the propagation speed indicates that the possibility that the structure is deteriorated is higher as the propagation speed is lower.
  • FIG. 9 is a diagram illustrating an example of an evaluation result when it is assumed that the conventional two evaluation methods illustrated in FIGS. 8A and 8B are combined.
  • the region where the elastic wave propagation velocity is higher than a certain standard and the AE source density distribution is sparse becomes healthy.
  • the elastic wave propagation velocity is lower than a certain standard and the AE seismic source density distribution is denser (the source is denser)
  • the deterioration of the structure progresses and becomes a linear change that leads to marginal deterioration.
  • the structure evaluation apparatus 20 evaluates the soundness of the structure based on the evaluation conditions using the AE hypocenter density distribution obtained from the elastic waves detected by each of the plurality of AE sensors 10 and the elastic wave propagation velocity distribution. To do. As described above, the structure evaluation apparatus 20 in this embodiment can evaluate the deterioration level of the structure for each region by combining the AE seismic source density distribution and the elastic wave propagation velocity distribution. Therefore, it is possible to evaluate the soundness of a structure that generates elastic waves. Moreover, the structure evaluation apparatus 20 can perform more accurate evaluation by using a plurality of pieces of information instead of one piece of information obtained from elastic waves.
  • the structure evaluation apparatus 20 may include only the evaluation unit 203, and the position location unit 201, the speed calculation unit 202, and the display unit 204 may be provided in another casing.
  • the evaluation part 203 acquires AE seismic source density distribution and elastic wave propagation velocity distribution from another housing, and uses the acquired AE seismic source density distribution and elastic wave propagation velocity distribution for a structure. Assess the health of And the evaluation part 203 outputs an evaluation result to the display part 204 with which another housing is provided.
  • the manufacturing cost of the structure evaluation apparatus 20 can be suppressed by using an existing apparatus for deriving the AE seismic source density distribution and the elastic wave propagation velocity distribution.
  • the signal processing unit 11 may be provided in the structure evaluation apparatus 20. When configured in this manner, the signal processing unit 11 acquires the AE source signal that has been processed by the AE sensor 10 directly from the AE sensor 10 or via a relay device (not shown). In FIG. 1, one signal processing unit 11 is connected to a plurality of AE sensors 10-1 to 10-n. However, the structure evaluation system 100 includes a plurality of signal processing units 11, and each AE sensor 10 The signal processing unit 11 may be connected to each of the plurality of sensor units, and a plurality of sensor units may be provided.
  • the velocity calculation unit 202 may be configured to derive a velocity in a region having a density equal to or higher than a predetermined threshold in the AE source density distribution illustrated in FIG. 2A or a velocity in a region having a density lower than the predetermined threshold.
  • the evaluation part 203 evaluates the soundness of a structure using the AE hypocenter density distribution derived
  • the evaluation unit 203 may operate as an output control unit.
  • the output control unit controls the output unit and outputs an evaluation result.
  • the output unit includes a display unit 204, a communication unit, and a printing unit.
  • the output control unit controls the communication unit and transmits the evaluation result to another device.
  • the output unit is a printing unit
  • the output control unit controls the printing unit to print the evaluation result.
  • the structure evaluation apparatus 20 may include the display unit 204, the communication unit, and a part or all of the printing unit as an output unit, and execute the above operation.
  • the position locating unit 201 may derive the AE seismic source density distribution using only the information on the AE generated from the transmission source in which the amplitude of the first arrival wave of the AE is equal to or greater than a predetermined threshold.
  • the position location unit 201 may derive the AE seismic source density distribution using only information on the AE generated from a transmission source having an amplitude of the first arrival wave of AE of 60 dB or more. This will be specifically described with reference to FIGS. 10A and 10B.
  • FIG. 10A is an AE source density distribution derived using AE information generated from a source with an AE first arrival wave having an amplitude of 53 dB or more
  • FIG. 10A is an AE source density distribution derived using AE information generated from a source with an AE first arrival wave having an amplitude of 53 dB or more
  • FIG. 10A is an AE source density distribution derived using AE information generated from a source with an AE first arrival wave having an amplitude of 53 dB or
  • the 10B is an AE first arrival wave having an amplitude of 60 dB or more. This is the AE seismic source density distribution derived using information on AE generated from the source. In view of the validity verification result of FIG. 5, it becomes possible to perform more accurate evaluation by using only information on AE generated from a transmission source having a certain amplitude or more as shown in FIG. 10B. Therefore, with this configuration, it is possible to contribute to effective deterioration diagnosis.
  • the first arrival wave means an elastic wave that first reaches the AE sensor when a plurality of AE sensors detect an elastic wave generation event (event) that has occurred in the structure.
  • FIG. 11 is a diagram showing another example of the basic concept shown in FIG.
  • an “initial” phase corresponding to an initial stage immediately after construction and repair of a structure is added.
  • This represents a situation where a large amount of transmission sources are observed when a load is applied for the first time in the initial state after construction and manufacture of the structure. This does not immediately indicate the progress of deterioration of the structure, but shows the response of the structure to the first load experienced by the structure. Thereafter, the occurrence of AE is reduced with respect to the existing load. Therefore, it is positioned as a pre-stage of the healthy phase in FIG. 7, and after the initial phase, represents a transition to the healthy phase as the number of transmission sources decreases.
  • the example shown in FIG. 11 is a phase that should be taken into consideration when the soundness is evaluated immediately after the construction and repair of the structure.
  • a plurality of AE sensors 10 for detecting elastic waves generated from a structure, and signal processing on the elastic waves detected by the AE sensor 10 to perform processing on the elastic waves.
  • a signal processing unit 11 for extracting an AE signal including information; a position locating unit 201 for deriving a source distribution based on the AE signal; a speed calculating unit 202 for deriving a propagation speed based on the AE signal; and a source distribution
  • the evaluation unit 203 that evaluates the soundness of the structure based on the propagation speed, the soundness of the structure that generates elastic waves can be evaluated.

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