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Tube Compliance Effects on Fluidic Flexible Matrix Composite Devices for Rotorcraft Vibration Control

机译:管柔顺性对用于旋翼飞机振动控制的流体柔性基复合材料装置的影响

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Fluidic Flexible Matrix Composite (F~2MC) tubes are a new class of lightweight and compact actuators with potential applications in rotorcraft vibration control. These tubes' high volume change in response to axial strain can be harnessed in new fluidic damper and absorber concepts. In this paper, a model for an F~2MC-integrated tailboom is used to determine the optimal F~2MC tube construction for a damped fluidic absorber on a small-scale tailboom. Benchtop experiments are performed to characterize model parameters related to the compliance and volume change of an individual F~2MC tube. Simulation results indicate that thin, soft tube bladders maximize vibration reduction. A 17.2 dB (86%) reduction in response is predicted in the first vertical tailboom bending mode for an F~2MC tube design using a stainless steel mesh and 1/32" thick rubber bladder configuration.
机译:流体柔性基体复合材料(F〜2MC)管是一类新型的轻巧紧凑的执行器,在旋翼飞机振动控制中具有潜在的应用前景。这些管响应于轴向应变而发生的大体积变化可以在新的流体阻尼器和吸收器概念中加以利用。本文采用F〜2MC一体式尾杆的模型来确定小型尾杆上阻尼流体吸收器的最佳F〜2MC管结构。进行台式实验以表征与单个F〜2MC管的柔度和体积变化有关的模型参数。仿真结果表明,细而柔软的管形气囊可最大程度地减少振动。对于使用不锈钢网和1/32英寸厚的橡胶气囊结构的F〜2MC管设计,在第一种垂直尾杆弯曲模式下,预计响应降低17.2 dB(86%)。

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