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Analytical and experimental studies of composite isogrid structures with integral passive damping

机译:具有整体被动阻尼的复合等斜结构的分析和实验研究

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Composite isogrid structure are currently in use in a number of aerospace applications where the control of structural vibration response is an important design consideration. In this paper. a recent investigation of the modal vibration characteristics of composite isogrid structures with embedded viscoelastic damping layers will be summarized. Analysis was done by means of the finite-element-based modal strain energy method. while experiments were done by using an impulse-frequency response technique. Composite isogrid test panels were fabricated by a fast and inexpensive thermoplastic stamping process using co-mingled glass/polypropylene. The viscoelastic layer damping materials were embedded at the interface between the ribs and the skin where the shear deformations are greatest in order to significantly improve the damping properties of the structures. Good agreement between measured and predicted modal frequencies and damping factors was found in the cases where degradation of the damping layer during the thermoplastic stamping process was avoided by using a secondary bonding process. It was also found that the required amount of damping material could be reduced significantly if it is optimally placed.
机译:目前,在许多航空航天应用中都使用复合等距结构,其中结构振动响应的控制是重要的设计考虑因素。在本文中。总结了对埋有粘弹性阻尼层的复合等斜结构的模态振动特性的最新研究。分析是通过基于有限元的模态应变能方法进行的。同时使用脉冲频率响应技术进行了实验。使用共混的玻璃/聚丙烯,通过快速且廉价的热塑性冲压工艺制造了复合等速测试板。粘弹性层阻尼材料嵌入在剪切变形最大的肋骨和皮肤之间的界面处,以显着改善结构的阻尼特性。在通过使用二次粘结工艺避免了热塑性冲压过程中阻尼层退化的情况下,在实测模态频率和预测模态频率与阻尼因子之间找到了很好的一致性。还发现,如果阻尼材料放置在最佳位置,则可以大大减少所需的阻尼材料量。

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