1 IntroductionAcoustic analogies of electrical diodes, which have the exotic property of allowing acoustic waves to transmit through one direction as well as blocking the transmission along the opposite direction, have recently attracted rapidly growing interest in the fields of physics and medicine owing to their great potential applications in many practical scenarios. For example, the elimination of the reflected wave energy may help to improve the quality of medical ultrasound imaging, and enable the design of conceptual devices like unidirectional sound barriers for noise control. The rapid development of sonic crystals and acoustic metamaterials provides various acoustic properties unavailable in nature,[1–7] enabling the design of various acoustic one-way devices.
Recently, many mechanisms have been proposed for designing various acoustic one-way devices by breaking the time reversal symmetry with nonlinear media,[8–10] active methods,[11–13] or gain-loss pair.[14–18] Due to the intrinsic limitations of nonlinear effects, including the inherent signal distortions and transmission efficiency, etc., more attentions have been focused on the asymmetric acoustic transmission (AAT). Several linear acoustic devices have been proposed to realize the AAT, such as acoustic gratings,[19–25] phononic crystals,[26–30] metamaterials,[31–32] and metasurfaces,[33–35] which have advantages of the high transmission efficiency and broad bandwidth of the AAT. However, for most of these AAT structures, the positive transmitted waves are usually two beam,[22] three beam,[19–20] multiple beam,[23,24,26] or distorted waveform in waveguides,[28–30,34,35] and it is difficult to concentrate the transmitted energy into a signal acoustic beam. In this context, the AAT effect with a single transmitted beam has been obtained based on the asymmetric phase modulation.[32–33] But the bandwidth of the AAT is limited owing to the coupling of a gradient-index metasurface and a near-zero-index medium, and it is still a challenge to realize the broadband AAT effect with a single transmitted beam. This restriction apparently becomes an obstacle for the practical application of the AAT.
In this work, we propose a simple acoustic device for realizing the ultra-broadband AAT effect with a single transmitted beam, which consists of a brass plate and a right triangle reflector in water. In the AAT device, the working bandwidth could reach 2000 kHz with the incident angle of 48º, and the positive transmitted wave is only a single acoustic beam. The experimental results agree well with the numerical simulations. Moreover, the AAT effect with different incident angles and plate thicknesses are investigated in detail.
2 Experimental and numerical modelsAs schematically shown in Fig. 1, the AAT device under consideration is a brass plate and a right triangle reflector immersed in water. The abbreviations TI and BI refer to the acoustic waves normally incident from the top and bottom sides of the AAT device, respectively. For TI, the incident wave is firstly reflected by the triangle reflector, and arrives at the brass plate with an incident angle, and the relationship between the incident angle α and the base angle θ is α = 180º − 2θ. However, for BI, the incident wave is incident on the brass plate vertically, and the parameter α is 0º. Throughout this work, the finite element method based on COMSOL Multiphysics software is utilized to numerically calculate the AAT characteristics. The structure parameters are d = 3.0 mm, l = 30.0 mm, and h = 1.0 mm, and the material parameters are adopted as follows: the density ρ = 8400 kg/m3, the longitudinal wave velocity c1 = 4400 m/s, and the transversal wave velocity ct = 2200 m/s for brass; ρw = 998 kg/m3, cw = 1483 m/s for water, at the temperature 296 K. In addition, the width of the incident plane wave is 20 mm.
3 Properties of AAT3.1 Transmission spectraFigures 2(a) – 2(c) show the numerical transmittance spectra for TI and BI. The base angle θ is 58º, 60º, and 62º which correspond to the parameter α: 64º, 60º, and 56º, respectively. The AAT effect exists in the ranges 428 kHz–901 kHz, 547 kHz–1038 kHz, and 720 kHz–1267 kHz for α = 64º, 60º, and 56º, respectively, which are plotted in the black shaded regions. The maximum bandwidth of the AAT reaches about 550 kHz for α = 56º, which is much wider than previous broadband AAT devices.[22,23,28,29] Besides, the peaks of the transmittance spectra for TI locate at 693 kHz, 819 kHz, and 1018 kHz for α = 64º, 60º, and 56º, respectively. It indicates that, with the decrease of α, the working band of the AAT becomes much wider and moves to the high frequency region.
To quantify the AAT performance, we introduce the contrast ratio (δ) as δ = |TT − TB| / (TT + TB), where TT and TB are the transmittances for TI and BI, respectively. Figures 2(d) – 2(f) present the contrast ratio with different α which correspond to Figs. 2(a) – 2(c), respectively. In the black shaded regions, most values of δ are close to 1.0 in the working bands of the AAT, indicating that the AAT devices have good performance.
Figure 3 shows the spatial distributions of the intensity field through the AAT devices. The incident frequencies are 693 kHz for α = 64º [Figs. 3(a) and 3(b)], 819 kHz for α = 60º [Figs. 3(c) and 3(d)], and 1018 kHz for α = 56º [Figs. 3(e) and 3(f)], respectively. In the case of TI [Figs. 3(a), 3(c), and 3(e)], the incident wave is firstly reflected by the triangle reflector, and reaches the brass plate with an incident angle α, and finally transmits through the brass plate, forming only a single acoustic beam. However, in the case of BI [Figs. 3(b), 3(d), and 3(f)], the incident angle α is 0º, and the acoustic wave is almost completely reflected without any transmission.
3.2 Physical mechanism of AATFigures 3(g) – 3(i) present the zoom of the deformation of the displacement field in the brass plate in Figs. 3(a), 3(c), and 3(e), respectively. Note that the asymmetric zero-order Lamb wave (A0 mode) is excited for TI. In general, if the phase velocity of the Lamb wave in the brass plate is larger than the bulk velocity in water, the Lamb wave could couple energy into water, creating a leaky bulk wave at a critical angle. The leakage angle (θ) is defined as θ = sin-1 (cw / cp), where cw is the bulk velocity of the water, and cp is the phase velocity of the Lamb wave.[36,37]
Figure 4 shows the leaky angle distribution of the A0 mode, in which the frequencies at points A, B, and C are 693 kHz, 819 kHz, and 1018 kHz, corresponding to the leaky angles of the A0 mode 64º, 60º, and 56º, respectively. These frequencies and angles are the same as those in Figs. 3(a), 3(c), and 3(e). Besides, the A0 mode in the brass plate could be excited when the incident angle of the external bulk wave is the same as or close to the leaky angle at a certain frequency.[38] Therefore, the acoustic wave can pass through the brass plate, which is shown in Figs. 3(a), 3(c), and 3(e). However, in Figs. 3(b), 3(d), and 3(f), the incident angle has great difference with the leaky angle, so little energy could transmit through the brass plate. Furthermore, as shown in Fig. 4, the gradient of the leaky angle curve of the A0 mode at point C is smaller than that at points A and B, which explains that the working band of the AAT becomes much wider with the decrease of α It is deduced that the AAT effect is attributed to the asymmetric excitation of the A0 mode in the brass plate induced by the incident angle of the external bulk wave, and the band of the AAT is determined by the incident angle and its corresponding gradient of the leaky angle curve.
3.3 Experimental verificationsIn order to experimentally verify the AAT effect, we have measured acoustic transmittances by the well-known ultrasonic transmission technique.[39] In the AAT models, the right triangle reflector is used to adjust the incident direction of acoustic waves for TI, and is replaced by a rotating ultrasonic transducer in the experiment. Figure 5 shows the schematic diagram of the experimental setup. The brass plate with the thickness of 1.0 mm is placed between two broadband ultrasonic transducers, one as generator and the other as detector, which is immersed in a water tank. Owing to the bandwidth limitation, two pairs of ultrasonic transducers (diameters of 20 mm) are used to fully cover the working range of the AAT from 300 kHz to 1500 kHz. One pair works at 500-kHz central frequency and 250 kHz–1100 kHz bandwidth, and the other pair at 1000-kHz central frequency and 700 kHz–1600 kHz bandwidth. The generation and detection transducers are obliquely towards the center of the brass plate with the same distance of 10 cm, and the incident angle of the generation transducer are set as 64º, 60º, and 56º which correspond to the incident angle α for TI in Figs. 2(a) – 2(c), respectively. Besides, the incident angle of 0º is also measured, corresponding to that for BI.
Figure 6 shows the measured transmittance spectra of different incident angles, in which the corresponding numerical results are plotted for comparison. The measured transmittance spectra agree with the numerical results. Moreover, as shown in the black shaded regions, the characteristics of the transmittance spectra agree well with those in the band of the AAT in Figs. 2(a) – 2(c), which verifies the feasibility of the AAT device.
3.4 Ultra-broadband AATAccording to this mechanism of the AAT, we could realize the ultra-broadband AAT effect with the single transmitted beam by the excitation of the external bulk waves with the incident angle α of 48º. Figures 7(a) and 7(b) show the numerical transmittance spectra and contrast ratio, respectively, in which the base angle θ is 66º. Note that the working band of the AAT is in the range 1320 kHz–3320 kHz (black shaded region) and is up to 2000 kHz with the incident angle of 48º. Besides, the maximum transmittance for TI is about 0.65 at 2320 kHz, whereas the transmittance for TI is close to zero. Furthermore, as shown in Fig. 7(b), most values of δ are close to 1.0 in the black shaded region, indicating that the device has good performance in this ultra-broad band of the AAT.
As shown in Fig. 4, the frequency and the leaky angle at point D are 2320 kHz and 48°. The leaky angle, the A0 mode and the frequency at point D are the same as the incident angle and the frequency of the maximum transmittance for TI in Fig. 7(a). Therefore, the ultra-broadband AAT effect arises from the excitation of the A0 mode. Besides, the gradient of the leaky angle curve of the A0 mode at point D is much smaller than that at points A, B, and C. Therefore, the working band of the AAT can reach 2000 kHz, which is much wider than previous broadband AAT devices.
3.5 Different plate thicknessFigures 8(a) and 8(b) show the numerical transmittance spectra with the plate thickness (h) of 0.8 mm and 1.2 mm. In the simulations, the parameters are the same as those in Fig. 2(c), and incident angle α for TI is 56°. It is shown from Figs. 8(a) and 8(b) that the working bands of the AAT are 895 kHz–1600 kHz and 585 kHz–1068 kHz, respectively. Note that, with the increase of h, the band of the AAT becomes narrower and moves to the low frequency region.
Figure 9 displays the leaky angle curve of the A0 mode in the brass plate with the thickness of 0.8 mm and 1.2 mm, in which the leaky angle of both points E and F is 56°. With the increase of h, the leaky angle curve of the A0 mode shifts to the low frequency region, and thus the frequencies at points E and F are 800 kHz and 1200 kHz, respectively. Besides, the AAT effect exists only when the incident angle of the external bulk wave is the same as or close to the leaky angle of the A0 mode. Therefore, the bands of the AAT are 895 kHz–1600 kHz and 585 kHz–1068 kHz for h = 0.8 mm and 1.2 mm, respectively. Furthermore, the gradient of the leaky angle curves of the A0 mode at point F is smaller than that at point E, and this explains that the band of the AAT becomes narrower with the increase of h. In addition to the incident angle, the band of the AAT is also closely related to the plate thickness.
3.6 Two positive transmitted wavesWe also find that the transmitted waves could be divided into two beams by using an isosceles triangle reflector, which is schematically shown in Fig. 10. The structure parameters are θ = 62°, d = 3.0 mm, l = 30.0 mm, and h = 1.0 mm. Figure 11 shows the spatial distributions of the intensity field through the device with the incident frequency of 1018 kHz. For TI [Fig. 11(a)], the incident wave is divided into two beams by the isosceles triangle reflector, and reaches the brass plate with an incident angle (α) of 56°, and transmits through the brass plate with two beams. However, in the case of BI [Fig. 11(b)], the acoustic energy is also completely reflected.