基于库仑摩擦的隔震残余位移理论分析与研究
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1.基准方中建筑设计股份有限公司;2.昆明有色冶金设计研究院股份公司;3.云南震研减震科技有限公司;4.昆明学院

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Theoretical investigation of Coulomb-Friction-Based residual displacement in seismic isolation systems
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1.JZFZ Architectural Design Co., Ltd.;2.Kunming Engineering & Research Institute of Nonferrous Metallurgy Co., Ltd.;3.Yunnan Zhenyan Damping Technology CO., LTD.;4.Kunming University

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    摘要:

    残余位移的大小反映了隔震层复位能力的强弱,是衡量主体结构建筑功能在震后能否正常使用的重要指标之一。震害调查发现,隔震支座震后存在残余位移,导致隔震层未完全复位。为揭示隔震层残余位移产生的机理,基于库仑摩擦单自由度体系(SDOF),根据隔震层双线性滞回特性建立了隔震层的自由衰减动力模型,提出了最大残余位移的简化计算公式,并进行了数值模拟验证,为合理评估隔震层的复位能力提供了理论支撑。研究表明:隔震层的残余位移分布具有高度离散性,但其最大值是确定的;其影响因素包括名义屈服强度Qd、初始刚度 k0、屈服后刚度k及阻尼比ξ。该残余位移简化计算公式在工程设计中具有一定的指导意义。

    Abstract:

    The residual displacement magnitude is a vital indicator reflecting the self-centering ability of the seismic isolation layer and a key criterion for evaluating the post-earthquake normal functionality of main structural buildings.Earthquake damage surveys have shown that isolation bearings commonly experience residual displacement after seismic activities,leading to incomplete self-centering of the isolation layer.To elucidate the mechanism of residual displacement generation in the isolation layer,a free vibration decay dynamic model was established based on the Coulomb friction single-degree-of-freedom (SDOF) system and the bilinear hysteresis characteristics of the isolation layer.A simplified formula for calculating the maximum residual displacement was proposed and validated through rigorous numerical simulations, providing theoretical support for rationally assessing the self-centering capacity of the isolation layer. Results indicate that the distribution of residual displacement in the isolation layer is highly scattered, yet its maximum value can be ascertained.The influencing factors involve the nominal yield strength Qd, initial stiffness k0, post-yield stiffness k, and damping ratio ξ. The proposed simplified formula offers practical guidance for engineering design.

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  • 收稿日期:2024-07-29
  • 最后修改日期:2025-04-27
  • 录用日期:2025-08-14
  • 在线发布日期: 2025-12-24
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