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7.4 Pulse generation

7.4.1 Combination of the responses

7.4.3 Time reversal duration . . . 114 7.4.4 Result of pulse creation . . . 115

7.5 Conclusion . . . 116

This chapter gives experimental results of applications using the time reversal method. Firstly, the excitation pulse position detection is introduced for both single excitation case and multiple excitations case. Then this chapter focuses on the creation of a pulse vibration on a beam. The approche adopted follows instructions presented in previous chapters.

Chapter 7. Experiments

7.1 Introduction

The objective of experiments is to verified previous theoretical modelling of the system. As discussed in Section 4.5, a beam can reduce the two dimensional problem to a one dimensional problem and it is also friendly for simulations in terms of the cost of time and computation resources. Hence, a "narrow" plate has been chosen as the target for our experiments. The experiments will use an aluminum beam of 250 x 16 x 2 mm3with one multilayer piezo- electric actuators of size 10 x 10 x 2 mm3(from NoliacTM) glued on the bottom of the plate. The position of the piezoelectric actuator is at one-fourth of the length of the beam (67.5 mm).

Piezo

67.5 mm

250 mm

16 mm

Figure 7.1 – Bottom view of the beam used for experiments

7.2 Excitation pulse position detection

In order to detect the position of an acoustic emission source, the first step is to create the reversed signal. According to previous studies in acoustic source location, we use a pencil to generate an excitation pulse on the beam [29]. The setup of experiment is illustrated in Fig. 7.2. As the piezoelectric actuator works as a sensor, an oscilloscope (LeCroy LT224) is connected to record the signal.

A P

Piezo

Oscilloscope Excitation

Figure 7.2 – Piezoelectric sensor connected to an oscilloscope for the detection of excitation pulse position

In this expriment, the excitation has been applied at 100 mm (0.4 of the total length) on the top surface of the beam. The signal captured by the piezoelectric actuator is recorded during 2 ms. The result is shown in Fig. 7.3. It is normalised with a maximal amplitude of one and then compared to the theoretical voltage result according to (4.10). The theoretical result takes also 110

7.2. Excitation pulse position detection

into consideration of damping effect which will be discussed later.

Time (ms) N or malised pie zoelectr ic act u ator sign al 0 0.5 1 1.5 2 -1 -0.5 0 0.5 1 Theo value Exp result

Figure 7.3 – Comparison of the signal received by piezoelectric sensor obtained by experiment and by theoretical calculation

In Fig. 7.4, Fourier Transform results of signals obtained by expriments and by theoretical calculation are given. It can be noticed that they have nearly the same spectrum distribution. As (4.10) contains a sin(!nt), their coefficients of Fourier Transform represent the product

of damping depending terms and eigenmode depending terms. Although there is some differences (for example around 14 kHz in Fig. 7.4) between the spectrum, the theoretical analysis can almost predict the results and one can expect the time reversal method will give a right answer for the excitation position.

Frequency (kHz) |Y(f )| 0 5 10 15 20 25 30 0.05 0.1 0.15 0.2 Theo value Exp result

Figure 7.4 – Comparison of FFT coefficients of signals received by piezoelectric sensor

According to the time reversal method, the voltage signal obtained by experiments is then given to a simulation under AnsysTM. The FEM model is made with the real dimension of the beam and piezoelectric actuator. The parameters of piezoelectric actuator are given by [90]. The result is shown in Fig. 7.5. In the simulation, the signal duration used is 1 ms (half of the total duration of recorded signal). It can be found that the maximum peak takes place exactly at 1 ms and at 0.4 of the normalised length.

Chapter 7. Experiments

Figure 7.5 – Simulation with the signal obtained from an experiment where the excitation pulse is applied at 0.4.

Second excitation position

Normalised length on a beam

Amp lit u de m) 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 1 -5 0 5

Figure 7.6 – One excitation at 0.4 and another one at from 0.05 to 0.95

7.3 Multiple excitation pulses position detection

The multiple excitation pulses positions detection is a little bit more complicated. Because of the superposition of associated peaks and measurement errors, it could be difficult to find a best solution. However, for our application to detect parts dropping positions, because they drop from a same height, the impact should be at same level for all the parts. Thus, we are mostly interested the resolution of this method to separate two positions of peaks.

7.4. Pulse generation

This experiment is carried out only by simulation. Supposing we always have a piezoelectric actuator glued at 0.25, two excitation pulses are simultaneously created. One at position 0.4, the other varies its position from 0.05 to 0.95. The result is obtained by FEM simulation as shown in Fig. 7.6. It can be noticed, while the distance between two excitations is less than 0.1, it becomes difficult to distinguish them. This distance is equal to the size of the piezoelectric actuator and thus the length of the created pulse. This property can also be confirmed by the Nyquist-Shannon sampling theorem.

7.4 Pulse generation

7.4.1 Combination of the responses

The input signal is currently generated by our analytical model. As analysed in previous section, the theoretical waveform has nearly the same spectral characteristic as experimental result. Because the cancellation will use the responses at several positions, it is much easier to obtain them by theoretical calculation than by experiments. According to Section 5.3.3, we can use a combination of responses at x1= 0.4, x2= 0.1, x3,+= 0.9+2.59kn = 0.9323 and x3,°= 0.8677

where kn= (25 +12)º = 80.11. The signal generated is plotted in Fig. 7.7.

Time (ms) N or malised amp lit u de 0 1 2 3 -1 -0.5 0 0.5 1

Figure 7.7 – Signal generated for restoring a pulse vibration without associated peaks

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