Development of Measurement System for Flow and Shape Using Array Ultrasonic Sensors

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1. Introduction

Severe accident at FDNPP occurred after 9.0 magnitude earthquake and a huge tsunami that struck the Tohoku region of Japan. The cold-shutdown condition of the reactors announced by the end of 2011 and the Japanese Government has drawn mid-and-long term roadmap (hereafter referred as the roadmap) towards decommissioning. According to the roadmap, the debris removal from the Unit-2 is scheduled to start within 2021 [1]. However, the fuel debris distribution is still unclear. Submersion method is considering as a basic and possible method for fuel debris retrieval from PCV of FDNPP [2]. Because the fuel debris generates heat that caused by radioactive decay, the submersion method allows to keep cooling the debris. Moreover, the water can be shield from radiation during fuel removal. Due to strong earthquake and tsunami, the PCV had damaged and there is water leakage from PCV’s wall [3]. To retrieve the fuel debris under submersion method, these water leakage and generation of contaminated water must be stopped. However, the leakage may be presented near fuel debris, under turbid water and at narrow places [4]. Due to high radiation environment inside damaged reactor buildings, human access to reactor building is impossible. Therefore, depending on the environment and condition of each units, internal investigation of the PCV for Unit 1 - 3 of FDNPP has performed by remote measurement techniques such as robots that installed camera [5] [6] [7]. Main target of those inspections is to obtain debris and water leakage information. Although the camera is direct observation way to see inside of PCV, the camera visibility reduces and noise caused by high radiation dose [8] [9] [10]. To respond to the situation inside the RPV and the bottom of the PCV where fuel debris is predominantly present, investigating device should necessarily meet specification of radiation resistance, waterproofness, dust resistance and so on [4].

In the present study, ultrasonic measurement is considered as a candidate method to localize contaminated water leakage and debris inside the PCV. Because the water leakage can be predicted by 2D velocity vector measurement based on its direction and magnitude. Moreover, ultrasound can be used to visualize objects under non-transparent medium such as under turbid water in the PCV. An ultrasonic measurement system used to visualize a reactor core that damaged during severe accident of Unit 2 in Three Mile Island (TMI), US [11]. Therefore, present study focuses on the Ultrasonic Velocity Profiler (UVP) and Total Focusing Method (TFM) methods to measure 2D vector flow field and shape of object that representing fuel debris, respectively. The water flow passing objects encompass a variety of fluid mechanics phenomena. The character of the flow field strongly depends on the shape and size of the object. Even the simple shaped objects, like a round, produce rather complex flows [12]. Therefore, simultaneous visualization of the flow and object shape is crucial for internal inspection of PCV where turbid water is circulating. In Section 2 of this paper, basic principle of measurement techniques for 2D velocity vector measurement using the UVP and object shape visualization using the TFM methods will be described. Section 3 will describe design of ultrasonic array sensors and its properties. The performance of sectorial array sensors has tested using smooth and rough objects under with and without flow conditions. The measurement results of these experiments will be described in Sections 4 and 5 respectively. Finally, summary of main findings of present study will be given in Section 6.

2. Principle of Measurement Techniques for Flow and Shape

2.1. Basic Principle of 2D Flow Field Measurement by UVP Method

This study focuses on time averaged 2D velocity field measurement by the UVP method. The UVP method is based on the pulsed echography and it can measure instantaneous velocity profile of fluid along ultrasound beam by analyzing echo signals that reflected from seeding particles [13]. Basic measurement principle of UVP is illustrated using a simple pipe flow in Figure 1. In UVP measurement, particles that nearly equal density of fluid are used as an ultrasound reflectors. A pulsed ultrasound waves are emitted from a sensor with a basic frequency (*f*_{0}) along measurement line with incident angle (*θ*). Then reflected echo signals from particles are detected at same sensor. The pulsed ultrasound has a spatial resolution as illustrated by yellow rectangles in Figure 1. According to Equation (1), the distance between each measurement volume and sensor surface is estimated based on the time interval between emission and reception of the signals. The reflected echo signal contains Doppler shift frequency (*f _{d}*) that containing velocity information of moving particles. Therefore the velocity profile along measurement line is reconstructed by Equation (2).

$x=\frac{cT}{2}$ (1)

$V\left(x\right)=\frac{c{f}_{D}}{2{f}_{0}\mathrm{sin}\left(\theta \right)}$ (2)

Main part of the UVP method is to estimate Doppler shift frequency. It is difficult to estimate Doppler shift frequency from an echo signal because it is much smaller than the basic frequency. Therefore, multiple emissions are used to measure velocity profile, at least 2 and typically 128. Figure 2 is demonstrated a block diagram of the signal processing part of the UVP. Doppler shift frequency is estimated by autocorrelation method [14] in this work. According to Figure 2, a pulser and receiver is used to emit and receive the ultrasonic waves through same sensor. The received echo signals contains both carrier and shifted signals. The quadrature detection where echo signals are multiplied by sine and cosine components is applied to separate signals. Then low pass filter is used to eliminate the carrier waves. The complex envelope signal $z\left(t\right)$ after the low pass filter is explained [3] as

$z\left(t\right)=I\left(t\right)+jQ\left(t\right)$ (3)

where,
$I\left(t\right)$ and
$Q\left(t\right)$ are the in-phase signal and the quadrature phase signal with the received signal, respectively. The autocorrelation function *Rf* is expressed as

$Rf=\left({T}_{PRF},t\right)={\displaystyle \int z\left(t\right)\times {z}^{*}\left(t-{T}_{PRF}\right)\text{d}t}={R}_{x}\left({T}_{PRF},t\right)+j{R}_{y}\left({T}_{PRF},t\right)$ (4)

where,
${T}_{PRF}$ is the time interval of the pulse emission,
${z}^{*}$ is the conjugate complex signal of
$z\left(t\right)$.
${R}_{x}$ and
${R}_{y}$ are the real and imaginary part of *Rf*, respectively. The phase shift between consecutive echo signals is expressed as

Figure 1. Simplified illustration of UVP measurement, echo signals and reconstruction of velocity profile by pulse repetition method.

Figure 2. Block diagram of Doppler signal estimation of UVP system.

$\phi \left({T}_{PRF},t\right)={\mathrm{tan}}^{-1}\frac{{R}_{x}\left({T}_{PRF},t\right)}{{R}_{y}\left({T}_{PRF},t\right)}$ (5)

Doppler shift frequency is obtained as follows

${f}_{D}=\frac{1}{2\pi {T}_{PRF}}{\mathrm{tan}}^{-1}\frac{{R}_{x}\left({T}_{PRF},t\right)}{{R}_{y}\left({T}_{PRF},t\right)}$ (6)

Eventually, a velocity profile can be obtained by analyzing the echo signals to derive instantaneous frequencies at each instant.

Originally the UVP method is proposed for one dimensional velocity profile measurement. Main purpose of this work is to introduce a principle of two-dimensional velocity field measurement based on the UVP method. There are several ways to measure 2D velocity field by UVP method. For instance, one transmitting and two/three-receivers configuration of ultrasonic sensors are an option for 2D/3D instantaneous vector measurement [15]. Moreover, phased array is an advanced tool for multi-dimensional flow measurement technique despite precise time delay controlling to steering beam and its measurement angle limitation due to grating lobes. Combining Doppler measurements taken along multiple intersecting ultrasound beams is one of approach to obtaining 2D velocity vector field. It is also referred as cross-beam technique in medical field [16]. In addition, single [17] and multiple ultrasonic sensors [18], such techniques is applied for 2D mapping of liquid metal flow. Based on this approach using a couple of sectorial array sensors, a validation experiment had performed comparing with high-speed camera measurement technique in our previous studies [19] [20]. The ultrasonic sensor composed with two or more single-element is first step in 2D velocity measurement as illustrated in Figure 3.

In cross-beam technique, two velocity components, *u*_{1} and *u*_{2}, at one spatial point measured by sensor-1(TX-1) and sensor-2(TX-2) are used to form a velocity vector, *V*. Ignoring the influence of ultrasound beam width, only the centerline of ultrasound beam considered in UVP to obtain an intersection points *d*_{1} and *d*_{2} [13]. The *u*_{1} and *u*_{2} are velocity components that measured directly by individual sensors. Let’s assume there are two measurement lines, illustrated in Figure 3, defined as

Measurement line 1:

${x}_{1}={x}_{Tx1}+{d}_{1}\mathrm{cos}{\theta}_{1}$. (7)

${y}_{1}={y}_{Tx1}+{d}_{1}\mathrm{sin}{\theta}_{1}$. (8)

Figure 3. 2D vector reconstruction using single-element and two sensors.

Measurement line 2:

${x}_{2}={x}_{Tx2}+{d}_{2}\mathrm{cos}{\theta}_{2}$. (9)

${y}_{2}={y}_{Tx2}+{d}_{2}\mathrm{sin}{\theta}_{2}$. (10)

where,
${x}_{Tx1},{x}_{Tx2},{y}_{Tx1},{y}_{Tx2}$ are coordinate of sensors.
${\theta}_{1}$ and
${\theta}_{2}$ are incident angle of sensors relative to flow. The *d*_{1} and *d*_{2} are distance from sensor to intersection point of these two lines are expressed as Equation (11) and Equation (12).

${d}_{1}=\frac{\left({x}_{Tx1}-{x}_{Tx2}\right)\cdot \mathrm{sin}{\theta}_{2}-\left({y}_{Tx1}-{y}_{Tx2}\right)\cdot \mathrm{cos}{\theta}_{2}}{\mathrm{sin}\left({\theta}_{1}-{\theta}_{2}\right)}$. (11)

${d}_{2}=\frac{\left({x}_{Tx1}-{x}_{Tx2}\right)\cdot \mathrm{sin}{\theta}_{1}+\left({y}_{Tx1}-{y}_{Tx2}\right)\cdot \mathrm{cos}{\theta}_{1}}{\mathrm{sin}\left({\theta}_{1}-{\theta}_{2}\right)}$. (12)

The distance are divided into the channel width (*w*) to determine what measurement channels (*Ch*) are crossing with each other.

$C{h}_{1}=\frac{{d}_{1}}{{w}_{i,1}}$. (13)

$C{h}_{2}=\frac{{d}_{2}}{{w}_{i,2}}$. (14)

Then, velocity components *u*_{1} and *u*_{2} at *Ch*_{1} and *Ch*_{2} channels that measured by TX-1 and TX-2 are extracted, respectively. Finally, the velocity *V _{x}* and

${V}_{x}=\frac{{u}_{1}+{V}_{y}\mathrm{cos}{\theta}_{1}}{\mathrm{cos}{\theta}_{1}}$. (15)

${V}_{y}=\frac{{u}_{1}\mathrm{cos}{\theta}_{1}+{u}_{2}\mathrm{cos}{\theta}_{1}}{-\mathrm{sin}{\theta}_{1}\mathrm{cos}{\theta}_{2}-\mathrm{sin}{\theta}_{2}\mathrm{cos}{\theta}_{1}}$. (16)

The spatial and temporal resolution of the UVP, in case of one-dimensional velocity profile measurement, are defined by Equation (17) and Equation (18), respectively.

$\Delta x=\frac{n\lambda}{2}$. (17)

where, ∆*x* is spatial resolution, *n* is number of cycle per pulse, *λ* is wavelength.

$\Delta t=\frac{{N}_{rep}}{PRF}$. (18)

where, ∆*t* is temporal resolution, *N _{rep}* is number of repetitions per profile and

$\Delta {t}_{2D}=\frac{{N}_{rep}}{PRF}\cdot N\cdot {t}_{switch}$. (19)

where, *N* is number of elements in array sensors, *t _{switch}* is switching time between elements in array sensors.

2.2. Basic Principle of Ultrasonic Imaging by TFM Method

Application of ultrasonic imaging is common in the medical and non-destructive testing because of its instant result, radiation-free and non-intrusive properties. Wide variety of ultrasonic imaging algorithms have developed in these fields. This study focuses on Total Focusing Method (TFM) as a post-processing algorithm to visualize object shape that representing fuel debris. The TFM algorithm provides a best image resolution than any other standard imaging technique [21]. In this method, all possible pairs of transmitting (*N*) and receiving (*N*) time domain signals,
${A}_{ij}\left(t\right)$, collected by the array sensor. This set of data is referred as the Full Matrix Capture. To reconstruct image, the TFM method uses time-domain signals
${S}_{ij}\left(t\right)$ that obtained by the Hilbert’s transform of the raw signals,
${A}_{ij}\left(t\right)$ :

${S}_{ij}\left(t\right)={A}_{ij}\left(t\right)+jh\left[{A}_{ij}\left(t\right)\right]$. (20)

Let’s considering a point $P\left(x,z\right)$ in the imaging plane as illustrated in Figure 5. In the Figure 5, the green arrow is representing emitting wave from array sensor-1 and reflected wave is illustrated by blue arrow which detected by array sensor-2. The intensity $P\left(x,z\right)$ at each imaging point is calculated by Equation (21).

$P\left(x,z\right)={\displaystyle {\sum}_{i=1}^{N}{\displaystyle {\sum}_{j=1}^{N}{D}_{i}{D}_{j}{S}_{ij}}}\left({t}_{ij}={t}_{i}+{t}_{j}\right)$. (21)

By assuming the medium under test is homogeneous and isotropic, the sound velocity is supposed to be constant. Therefore, the distance between transmitter and receiver calculates by Equation (22).

${t}_{ij}=\frac{\sqrt{{\left(x-{x}_{i}\right)}^{2}+{\left(z-{z}_{i}\right)}^{2}}+\sqrt{{\left(x-{x}_{j}\right)}^{2}+{\left(z-{z}_{j}\right)}^{2}}}{c}$. (22)

Figure 4. 2D velocity field measurement using a couple of sectorial and linear array sensors.

Figure 5. Shape measurement by a couple of sectorial array sensors using TFM method.

where, ${x}_{ij},{z}_{ij}$ are coordinates of transmitting and receiving element in the array sensor, respectively. In TFM algorithm as a weighting factor, the directivity function of transmitting and receiving elements in two-dimensional model assumed as following Equations [21].

${D}_{i}=\text{sinc}\left(\frac{\mathrm{sin}{\theta}_{tx}\pi a}{\lambda}\right)$. (23)

${D}_{j}=\text{sinc}\left(\frac{\mathrm{sin}{\theta}_{rx}\pi a}{\lambda}\right)$. (24)

where, *a* is width of element in sectorial array sensor.

3. Design of Sectorial Array Sensors

The specification of sectorial array sensors are showed in Figure 6. There are 256 piezoelectric elements in two sensors and each sectorial array sensor consists with 128 piezoelectric elements. The element width and height of piezoelectric are 0.1 mm and 5 mm, respectively. The angle between two neighboring elements in the array sensor is 0.7 degree. Curvature of array sensor where elements presents is 12.2 mm.

To assess performance of sectorial array sensors, sound pressure distribution is carried out by needle hydrophone under water. Figure 7 shows experimental the set-up for the sound pressure distribution. It consists with automatic 3D stage which is installed on top of the water tank, a stage controller (Sigma Kiko Co., Ltd.), a pulser & receiver (600C, P/R, Japan Probe Co.Ltd.) and a PC. The 3D stage is controlled by LabVIEW software in the PC. The sectorial array sensor is connected to the Multiplexer (MUX) and Pulser/Receiver (P/R, 600C, Japan Probe Co.Ltd.) which generates a pulse. The experiment were performed

(a)(b)

Figure 6. Specification of sectorial array sensors (a) Photo of sectorial arrays, (b) Detailed specification.

Figure 7. Measurement system for sound pressure distribution.

under stagnant water and water temperature was 17˚C. The needle hydrophone was traversed by the 3D stage to measure the ultrasonic signals according to preditermined grid. The resolution of the grid was 2 mm × 2 mm along both lateral and axial directions The peak-to-peak between the maximum and minimum of the received signal was considered as the ultrasound pressure at the each measurement points. The measured values were used to calculated sound pressure level (*SPL*) according to Equation (25).

$SPL=20{\mathrm{log}}_{10}\left(\frac{P}{{P}_{0}}\right)$. (25)

where, *SPL*—sound pressure level in decibel [dB], *P*—sound pressure at spatial point, *P*_{0}—reference sound pressure.

The sound pressure distribution of element No.64 in array sensor-1 is illustrated in Figure 8. In the Figure 8, x- and y-axis are representing axial and lateral directions, respectively. The legend is showing SPL at each spatial location of measurement. The *SPL* decreases (see Figure 9(a)) with increasing axial distance and variation of *SPL* was measured within –20 dB until 195 mm. To assess beam width along lateral direction, Full Width at Half Maximum (FWHM) is calculated at center along axial positions. An example of the FWHM calculation at axial direction of 50 mm is showed in Figure 9(b) and Figure 9(c) shows the FWHM versus different axial positions.

4. Shape Measurement by Sectorial Array Sensor (without Flow)

4.1. Test on Smooth Surface

To demonstrate imaging accuracy of the sectorial array sensors, different size of metal rectangle objects had measured in big acrylic tank that is used for sound pressure distribution experiment. The measurements were performed in stagnant water. The size of rectangle objects were 1 mm, 3 mm, 5 mm, 15 mm, 25 mm and 50 mm. The experimental set-up is illustrated in Figure 10. In this experiment, distance between the sectorial array and rectangles objects were *d* = 50 mm and *d* = 100 mm. The measurement condition is listed in Table 1.

Figure 8. An example of sound pressure distribution of element No.64 in sensor-1.

(a)(b)(c)

Figure 9. (a) Sound pressure level at the centerline (lateral direction = 0 mm) along axial direction, (b) An example of FWHM calculation (axial distance = 50 mm) and (c) FWHM versus axial distance.

Figure 10. Experimental set-up for accuracy measurement.

Table 1. Measurement parameters.

In data acquisition for shape visualization, totally, 128 × 128 time domain signals have collected and it used to reconstruct image of object by TFM method. Post processing is performed by MATLAB algorithm. An example of measurement results of 50 × 50 mm rectangle at different axial distances are showed in Figure 11. According to measurement result in Figure 11, the top surface of rectangle objects and bottom wall of tank are visualized while there are some parabolic hyperbola artifacts are comes out at the edge of rectangle objects. The reason of hyperbola artefact is that emitted ultrasound beam from sensor has a finite beam width, the object illuminated for a finite length of the scanning axis. The artifact was strong when distance between sensor and object is close (see Figure 11) while the parabolic hyperbola artifact was decreasing when the axial distance increases. Figure 12 shows measurement results of six different size of rectangle objects. The bigger size rectangles such as 25 mm and 50 mm are accurately measured and the measurement error was less than 10%. On the other hand, smaller size of rectangles such as 1 mm, 3 mm and 5 mm have larger error but less than 30%.

4.2. Test on Rough Surface

To evaluate performance of sectorial array sensor on irregular shaped object that representing fuel debris have tested. The dimension of debris was the length of 80 mm (Y direction), width of 70 mm (X direction) and height of 50 mm (Z direction). Photo of object is showed in Figure 14. Since the object is irregular, the

(a)(b)

Figure 11. Measurement result of rectangle object (a) at 50 mm and (b) at 100 mm. (a) Measurement result. d = 50 mm. (b) Measurement result. d = 100 mm.

Figure 12. Measurement results of six different size of rectangles at different axial distances.

sectorial array sensor is moved along x-direction with 3 mm steps by 3D stage to obtain whole image. Measurement performed at 24 positions along x-axis. Total scanned area is 72 mm (24 × 3 mm). The measurement parameters were same as data illustrated in Table 1. The distance between bottom wall of tank and sensor surface was around 100 mm and a simulated debris was placed under sensor. The measurement results that integrated all 24 positions are depicted in Figure 13. Strong reflections were observed from the bottom wall of tank and surface of debris near sensor according to measurement result that showed in Figure 13. The spatial resolution along y, z direction was 0.2 mm and 0.2 mm, respectively, in the Figure 13. Measurement data at all measurement positions were integrated and 2D results along ZY, XZ and YX are qualitatively compared with image of the simulated fuel debris in Figure 14. According to measurement data, the dimension of debris are approximately estimated as 80 mm, 69 mm and 50 mm, along Y, X and Z directions, respectively. Due to diffuse reflection on the rough surface, the parabolic hyperbola artifact was less than smooth surfaces on the measurement results. However, the artifact is observed from bottom wall of tank because of smooth and flat surface where highest reflection is occurred (see Figure 14).

5. Shape and Flow Measurement by Sectorial Array Sensors

To measure flow field and shape simultaneously, an A/D converter (National Instruments, USB-5133) is integrated with measurement system that used to shape measurement. A LabVIEW software is used to control ultrasonic system. A measurement system that reconstructed for flow and shape is showed in Figure 15. It consists with a couple of sectorial array sensors, a pulser and receiver (600C, P/R, Japan Probe), a multiplexer (MUX-128, Japan Probe), an A/D converter (National Instruments, USB-5133) and a laptop. The function of the multiplexer is to select desired channel or element of sensors as a transmitter and receiver.

Figure 13. Measurement result of simulated fuel debris (3D views).

(a)(b)(c)

Figure 14. Measurement result of simulated fuel debris comparing with real photo of debris. (a) z-y view, (b) z-x view and (c) y-x view.

Figure 15. Measurement system for flow and shape measurement.

A flow chart of measurement procedures to obtaining velocity and shape is illustrated in Figure 16. A mock-up experiment using developed system has performed in acrylic water tank with dimension of 1280 × 450 × 450 mm. In this experiment, simultaneous measurement have carried out by UVP and Particle Image Velocimetry (PIV) techniques to compare measurement results of 2D flow field. The experimental set-up is illustrated in Figure 17. There is a drain (20 mm in diameter) that representing leakage point at the bottom of the tank wall. The water leakage was placed between two simulated fuel debris which has smooth and rough surfaces, respectively. Water circulated by pump (MD-100RM, Iwaki magnet pump, Iwaki Co., Ltd.) and flow rate is monitored by a flow meter (NW-10 NTN, Aichi Tokei Denki, Co., Ltd.). The flow rate in this experiment was 10 ± 1 l/min. The sectorial array sensors were located 115 mm above the bottom of the water tank and distance between two sensors were 90 mm. Nylon

Figure 16. Flow chart of 2D flow and shape measurement.

Figure 17. Measurement set-up and configuration.

particles with 80 μ in mean diameter mixed with water and it used as ultrasound reflector and illumination particles for PIV. The PIV system consists with a High Speed Camera (Photron FASTCAM Mini AX50) and a laser source (Ray Power 450, DANTEC DYNAMICS, Max output <0.5 W at 532 nm). The laser head is located top of the water tank and laser enters to test section between sensors. A series of images with 1024 × 1024 pixel at 500 frames per second were captured by High Speed Camera (HSC) and recorded data were proceeded further by PIVlab software in MATLAB [22]. However, in PIV data processing, only area of 410 × 860 pixel where main flow recorded were processed. In ultrasonic measurement, totally, 128 × 128 time-domain signals were stored to reconstruct object shape by TFM method. The measurement lines of all elements are illustrated in Figure 18. In the Figure 18, the black and blue lines are representing measurement pathways and angles. To obtain leakage point by UVP, 20 elements from both sensors, totally 40 measurement lines, were used to measure velocity profiles. These measurement lines are created a mesh with 259 intersection points where 2D velocity vectors reconstructed. The measurement parameters and conditions of the UVP and PIV are listed in Table 2.

The simulated fuel debris were visualized by sectorial array sensors as showed in Figure 19. However, the measurement result of shape deteriorated due to high flow effect where leakage point was existing between simulated debris. Moreover, the parabolic hyperbola artifacts that caused by smooth surfaces of triangle and bottom wall of tank is appeared on measurement result.

Table 2. Measurement parameters for flow and shape.

Figure 18. Illustration of measurement lines for shape and intersection points between measurement lines where 2D velocity vectors are constructed.

Figure 19. Measurement result of simulated fuel debris.

Measurement results of 2D velocity field by UVP and PIV are showed in Figure 20. In Figure 20(a) shows the sensors position, measurement pathways while detailed image of measurement result of UVP is showed in Figure 20(c) where bottom wall of the acrylic tank and simulated leakages are indicated by a solid lines (black) and empty space between lines, respectively. Figure 20(b) shows the measurement result of the PIV. 2D velocity vectors at closest coordinate are extracted from the PIV result for a qualitative comparison with UVP data and the extracted data is showed in Figure 20(d). According to qualitative comparison between UVP and PIV, highest velocity field is detected near simulated leakage point in the both results. Statistical characteristics of the UVP and PIV velocity measurements are listed in Table 3 and such statistical data interpretation were used for low flow of rivers in [23].

To demonstrate agreement between the UVP and PIV on 2D flow measurement, the Bland-Altman plot is drawn and it is showed in Figure 21(a) and

(a) (b) (c) (d)

Figure 20. Measurement results of 2D vector field by UVP ((a) & (c)) and PIV ((b) & (d)).

Table 3. Descriptive statistics of the UVP and PIV measurements.

Figure 23(a). The Bland-Altman plot is formed by plotting the differences on vertical axis versus the averages on the horizontal axis. A red horizontal lines are representing the bias. Additional horizontal lines, known as limits of agreement (LOA), are added to the plot at ±1.96 SD. According to Bland-Altman plots, most of velocity values along vertical (Figure 21(a)) and axial directions (Figure 23(a)) are existing ±1.96 SD of the mean differences. To show outliers, in addition, distribution plots of difference between two measurement techniques are illustrated along lateral and axial direction, respectively, in the Figure 21(a) and Figure 23(a). In these histograms, for each bin, we counted the number of velocity values that fall in interval of 0.002 m/s and 0.005 m/s along vertical and horizontal axis, respectively. The vertical axis shows the relative frequency which is defined by ratio between absolute frequency of velocity values at each intervals and total number of data. In Figure 21(b) and Figure 23(b), outliers that existing outside of ±1.96 SD in the histograms are indicated by red (outliers higher than ±1.96 SD) and blue (outliers lower than ±1.96 SD) dots in the measurement grid of UVP. The most of the outliers are estimated as reverse vectors at near leakage and simulated fuel debris where high and complex flow presents. In Figure 22 and Figure 24, time averaged velocity profiles that obtained by measurement lines No.14 and No.6 of Sensor-1 and measurement lines No.5 and No.13 of Sensor-2 are illustrated because most of outliers are existing along these measurement lines. These measurement lines are indicated in the Figure 21(b) and Figure 23(b) as a black and red lines. The outliers were estimated at distance of over than 70 mm from sensors surface where the velocity profiles were significantly fluctuating and deteriorates as showed in Figure 22 and Figure 24. If we take a look at the SPL measurement result (Figure 8 and Figure 9), the SPL and FWHM were less than −13 dB and over than 13, respectively, after 70 mm from sensor surface. Eventually, an integrated measurement results of simulated fuel debris shape and 2D vector field by developed ultrasonic system is illustrated in Figure 25.

(a)(b)

Figure 21. Agreement between the UVP and PIV velocity measurement results. (a) Bland-Altman plot of the UVP and PIV measurement results on lateral direction. (b) Outliers indicated at measurement grid of the UVP.

Figure 22. Time averaged velocity profiles measured by element No. 14 (black) and Element No.5 (red) of Sensor-1 and Sensor-2, respectively.

(a)(b)

Figure 23. Agreement between the UVP and PIV velocity measurement results. (a) Bland-Altman plot of UVP and PIV measurement results on axial direction. (b) Outliers indicated at measurement grid of the UVP.

Figure 24. Time averaged velocity profiles measured by element No.6 (black) and Element No. 13 (red) of Sensor-1 and Sensor-2, respectively.

(a)(b)

Figure 25. Integrated measurement results of simulated fuel debris and leakage point.

6. Conclusions

In the present study, ultrasonic measurement technique has considered as a candidate method that can obtain simultaneous information of fuel debris and contaminated water leakage from PCV of FDNPP. Therefore, a measurement system using a couple of sectorial shaped ultrasonic array sensors have developed because sectorial array sensors have some advantages, such as inspection area is larger than linear array sensor and it does not required to precise controlling of time delay for beam steering like phased array sensors. The aim of present study was to demonstrate applicability of ultrasonic measurement system for simultaneous measurement of objects and flow around it using TFM and UVP methods, respectively. The performance of the system on shape and velocity measurement have evaluated individually. After that a simultaneous measurement of shape and velocity have conducted in laboratory scaled tank where simulated debris and leakage are presented. In order to compare and validate velocity measurement results of the ultrasonic system, a simultaneous measurement by PIV technique have conducted. Main findings of present study are summarized as below.

1) Different size of simple rectangle objects were measured to assess performance of system with sectorial array sensor. Surface of the rectangle objects are successfully visualized although parabolic hyperbola artifacts appeared on the measurement results. The measurement result was showing that strong and multiple artifacts when distance between sensor and objects are short. The rectangle objects with size of 25 mm and 50 mm are measured at high accuracy with less than 10% while the smaller size of objects (1 mm, 3 mm and 5 mm) can be measured with around 30% of error.

2) An irregular rock sample was measured after simple rectangle objects. The dimension of the sample was length of 80 mm (Y), width of 70 mm (X) and height of 50 mm (Z). A qualitative comparison between the ultrasonic measurement and photo images of object were showed a good agreement. Dimension of the object that measured by ultrasonic revealed as length of 80 mm (Y), width of 69 mm (X) and height of 50 mm (Z).

3) A mock-up experiment have carried out in the laboratory scaled tank where simulated fuel debris and leakage are placed. Although visualization result of simulated debris by ultrasonic method was deteriorated where high flow detected, the measurement results revealed that the UVP and the TFM methods using sectorial array sensors can be visualize the shape of simulated debris and localize the water leakage point, simultaneously. To conclude, it is clarified that the measurement system with sectorial array sensors is an effective way to obtain object shape and flow around it.

Acknowledgements

The authors are grateful for the support of Ministry of Education, Culture, Sports, Science and Technology (MEXT).

Nomenclature

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