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Performance characteristics of active constrained layer damping versus passive constrained layer damping with active control

机译:主动约束层阻尼与被动约束层阻尼的性能特征

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Abstract: The shear strains in the visco-elastic cores of beams controlled by Active Constrained Layer Damping (ACLD) treatments are determined and compared with those of beams controlled by Active Control (AC) and conventional Passive Constrained Layer Damping (PCLD) treatments. Such comparison is essential in quantifying the individual contribution of the active and passive damping components, to the overall damping characteristics, when each operates separately and when both are combined to interact in unison as in the ACLD treatments. The comparisons are based on distributed-parameter and finite element models which describe the behavior of beams controlled by ACLD as well as beams treated by AC and PCLD treatments. The distributed-parameter models give closed-form expressions for the energy dissipation characteristics of the ACLD treatments in comparison with those of the AC/PCLD treatments. Also, the finite element models are validated experimentally using visco-elastic cores which are photo-elastic in order to study the distribution of the shear strains inside these cores. The results obtained indicate that the ACLD treatments are capable of developing shear deformations, in the visco-elastic cores, higher than those generated by the AC/PCLD treatments when the ratio of the longitudinal rigidity of the constraining layer to that of the base beam is less than 1. With such enhanced shear deformation capabilities, the ACLD treatments can develop high damping and effective attenuation of the vibration of critical systems as the blades of rotorcrafts.!13
机译:摘要:确定了主动约束层阻尼(ACLD)处理的梁的粘弹性芯中的剪切应变,并将其与主动控制(AC)和常规被动约束层阻尼(PCLD)控制的梁的剪切应变进行了比较。这样的比较对于量化有源和无源阻尼组件对整体阻尼特性的贡献是至关重要的,当每个组件单独运行时,以及当两个组件组合在一起共同相互作用时(如ACLD处理)。比较是基于分布参数模型和有限元模型,这些模型描述了ACLD控制的光束以及AC和PCLD处理的光束的行为。与AC / PCLD处理相比,分布参数模型给出了ACLD处理的能量耗散特性的封闭形式。同样,使用光弹性的粘弹性芯通过实验验证了有限元模型,以便研究这些芯内部的剪切应变分布。所得结果表明,当约束层的纵向刚度与基梁的纵向刚度之比为0时,ACLD处理能够在粘弹性芯中产生剪切变形,高于AC / PCLD处理所产生的剪切变形。小于1。通过增强的剪切变形能力,ACLD处理可以对旋翼航空器的叶片产生高阻尼并有效衰减关键系统的振动!13

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