Gao Haoqiang, Yan Qun, Liu Xusheng, Zhang Ying, Sun Yongtao, Ding Qian, Wang Liang, Xu Jinxin, Yan Hao
Department of Mechanics and Tianjin Key Laboratory of Nonlinear Dynamics and Control, Tianjin University, Tianjin 300350, China.
Key Laboratory of Aeroacoustics and Dynamics, Aircraft Strength Research Institute, Xi'an 710065, China.
Materials (Basel). 2022 Jan 5;15(1):373. doi: 10.3390/ma15010373.
In order to achieve the dual needs of single-phase vibration reduction and lightweight, a square honeycomb acoustic metamaterials with local resonant Archimedean spirals (SHAMLRAS) is proposed. The independent geometry parameters of SHAMLRAS structures are acquired by changing the spiral control equation. The mechanism of low-frequency bandgap generation and the directional attenuation mechanism of in-plane elastic waves are both explored through mode shapes, dispersion surfaces, and group velocities. Meanwhile, the effect of the spiral arrangement and the adjustment of the equation parameters on the width and position of the low-frequency bandgap are discussed separately. In addition, a rational period design of the SHAMLRAS plate structure is used to analyze the filtering performance with transmission loss experiments and numerical simulations. The results show that the design of acoustic metamaterials with multiple Archimedean spirals has good local resonance properties, and forms multiple low-frequency bandgaps below 500 Hz by reasonable parameter control. The spectrograms calculated from the excitation and response data of acceleration sensors are found to be in good agreement with the band structure. The work provides effective design ideas and a low-cost solution for low-frequency noise and vibration control in the aeronautic and astronautic industries.
为了实现单相减振和轻量化的双重需求,提出了一种具有局部共振阿基米德螺旋的方形蜂窝声学超材料(SHAMLRAS)。通过改变螺旋控制方程获得SHAMLRAS结构的独立几何参数。通过模态形状、色散面和群速度研究了低频带隙产生的机理和面内弹性波的定向衰减机理。同时,分别讨论了螺旋排列和方程参数调整对低频带隙宽度和位置的影响。此外,采用SHAMLRAS板结构的合理周期设计,通过传输损耗实验和数值模拟分析其滤波性能。结果表明,具有多个阿基米德螺旋的声学超材料设计具有良好的局部共振特性,通过合理的参数控制可在500Hz以下形成多个低频带隙。由加速度传感器的激励和响应数据计算得到的频谱图与能带结构吻合良好。该工作为航空航天工业中的低频噪声和振动控制提供了有效的设计思路和低成本解决方案。