航天器宽频带流体减振支柱设计及特性仿真
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国家自然科学基金资助项目(12072075)


Design and Characteristics Simulation of a Broadband Fluid Damping Strut for Spacecraft Vibration Reduction
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    摘要:

    为了提高现有三参数隔振器的隔振性能,设计了一种宽频带波纹管流体减振支柱产品原型,该减振支柱通过设计若干只频率阀,用于调节其在低频段的阻尼特性,通过设计带有间隙元件的机加工弹簧作为二级刚度.建立了基于该流体减振支柱的航天器控制力矩陀螺隔振系统的动力学数学模型与仿真模型,仿真结果表明:相对于现有三参数阻尼器,所设计的流体减振支柱获得了低频段高阻尼、高频段小阻尼的自适应外特性,其对低频振动尤其是对共振峰具有明显的抑制作用,在中、高频段的统计隔振效果也更好,即在较宽的频带范围内取得了良好的隔振性能.

    Abstract:

    To enhance the isolation performance of the current three-parameter isolators, a prototype of broadband fluid damping strut has been designed. The damping strut features several frequency selective valves to adjust its damping characteristics at the low-frequency range, and a machined spring with a clearance element to act as a secondary stiffness. A dynamic mathematical model and a simulation model of a vibration isolation system using the designed fluid damping strut for a spacecraft control moment gyroscope have been established, followed simulation results indicate that compared to current three-parameter dampers the designed damping strut has achieved adaptive outer characteristics of high damping in the low-frequency range and low damping in the high-frequency range, it has obtained a significant suppressive effect on low-frequency vibrations, especially those near the resonance peak, its statistical vibration isolation effect is also better than that of the current dampers in the mid and high frequency bands, thus, the designed fluid damping strut has obtained excellent vibration isolation characteristics in a broad frequency band.

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王文林,陈汝星,丁洋,刘永.航天器宽频带流体减振支柱设计及特性仿真[J].动力学与控制学报,2025,23(2):1~9; Wang Wenlin, Chen Ruxing, Ding Yang, Liu Yong. Design and Characteristics Simulation of a Broadband Fluid Damping Strut for Spacecraft Vibration Reduction[J]. Journal of Dynamics and Control,2025,23(2):1-9.

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历史
  • 收稿日期:2024-06-15
  • 最后修改日期:2024-09-19
  • 在线发布日期: 2025-03-13
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