主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
M型皱褶芯材夹层板隔声性能研究
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南京航空航天大学 航空学院

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V214.8

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Research on the soundproof of the M-type folded core sandwich panel
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College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics

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    摘要:

    作为先进复合材料夹层结构,皱褶芯材构型多样,先前研究大多围绕V 型皱褶芯材展开,现有对其他构型的隔声性能研究。建立垂直入射声压激励下的四边简支M 型皱褶芯材夹层板数值模型,基于有限元软件对其隔声性能进行数值仿真,并将理论预测的蜂窝夹层板隔声曲线与仿真结果进行对比;基于仿真模型,系统地研究M 型皱褶芯材夹层板结构的隔声性能,讨论皱褶芯材胞元几何参数对隔声性能的定性影响规律;提出并研究双层芯材的M 型皱褶芯材夹层板上下两层芯材的相对铺设错位、铺设角度对隔声性能的影响。结果表明:上下两层芯材在胞元Z 形线步长方向错位叠放时隔声效果提高,且优于同面密度的单层皱褶芯材夹层板;在上下两层芯材相对铺设角度变化时,上下层芯材轴线垂直铺设时计权隔声量最大。

    Abstract:

    As an advanced composite sandwich structure, folded core sandwich panels are expected to be applied as sound insulation structures in transportation vehicles such as aircraft and high-speed trains. However, the configuration of folded core is diverse, and previous research has mostly focused on the V-shaped folded core, while there is still relatively little research on the sound insulation performance of other configurations. Therefore, this article establishes a numerical model of a four sided simply supported M-shaped folded core sandwich panel under vertical incident sound pressure excitation, and conducts numerical simulation of its sound insulation performance based on finite element software. The theoretical predicted sound transmission loss curve of the honeycomb sandwich panel is compared with the simulation results to verify the effectiveness of the numerical method proposed in this article. Based on simulation models, the sound insulation performance of M-type folded core sandwich panel structure was systematically studied, and the qualitative influence of geometric parameters of folded core cell on sound insulation performance was discussed. Subsequently, the influence of relative misalignment and laying angle of the upper and lower layers of M-type folded core sandwich panel with double-layer core on sound insulation performance was proposed and studied, the results show that the sound insulation performance is improved when the upper and lower layers of core are staggered and stacked in the Z-shaped line step direction of the cell, and it is better than single-layer folded core sandwich panel with the same surface density; when the relative laying angle of the upper and lower layers of core changes, the maximum weighted sound insulation is achieved when the axis of the upper and lower layers of core is vertically laid, and the trend prediction curve of the mean transmission loss with the change of the laying angle of the core is obtained, providing a reference for the optimization design of sound insulation in sandwich panels with folded core sandwich structures.

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叶语睿,王志瑾. M型皱褶芯材夹层板隔声性能研究[J].航空工程进展,2024,15(5):135-147

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历史
  • 收稿日期:2024-05-21
  • 最后修改日期:2024-07-04
  • 录用日期:2024-07-05
  • 在线发布日期: 2024-09-13
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