• High-degree lightweight design is one of the key techniques for the high speed maglev train with the sandwich panel structure.

    高度轻量化设计是具有三明治复合板结构特征的高速磁浮列车技术关键之一。

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  • With the increasing application of double panel structure in engineering, people pay more and more attention to its sound transmission performance.

    随着双层板结构在工程中的广泛应用,其声透射性能也得到越来越多的关注。

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  • The light panel structure, the high quality PET synthetic fiber filter material is with features of low initial pressure, good fire-proof function.

    轻便的板式结构,优质的聚酯合成纤维过滤材料,初阻力低,防火性好。

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  • Sandwich type panel structure, the middle of flame retardant and heat insulation and noise reduction material, has the fire performance of A0 class.

    三明治夹层式面板结构,中间加阻燃隔热降噪材料,具有A 0级防火性能。

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  • This text gives preliminary study of overall performance and the collapse mode of this new thermal insulation and energy saving Concrete sandwich panel structure.

    本文对这种新型保温节能混凝土夹芯板式结构的整体性能及倒塌模式进行了初步的研究。

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  • The experimental study on the structural and seismic behavior of CS panel structure is presented in the paper.

    本文对这种节能效果很好的CS板式结构的抗震性能进行了初步的试验研究。

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  • Different installments such as horizontal, vertical and diagonally can match to complicated panel structure, and can also realize optical delamination effect between facade panels.

    各种不同的安装方式,即水平、垂直或对角安装,不仅可以配合复杂的嵌板结构,更能轻易实现幕墙嵌板之间视觉分明的分层效果;

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  • In the paper aiming at the problem of low frequency noise transmission through double panel structure, feedback active noise control technique is adopted to control noise transmission.

    本文对于低频噪声在双层板结构中传播的问题,探讨采用反馈的主动噪声控制技术以达到控制噪声传播的目的。

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  • The finite-element simulation models of the discrete rod and the projectile impacting on the aircraft panel structure at high velocity are established according to some experiment projects.

    根据已有实验方案分别建立了离散杆和射弹高速冲击飞机壁板结构的有限元模型,利用显式动力有限元计算程序进行了冲击损伤仿真。

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  • The finite-element simulation models of the discrete rod and the projectile impacting on the aircraft panel structure at high velocity are established according to some experiment projects.

    根据已有实验方案分别建立了离散杆和射弹高速冲击飞机壁板结构的有限元模型,利用显式动力有限元计算程序进行了冲击损伤仿真。

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