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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >A Method for Parametric Analysis of Stability Boundaries for Nonlinear Periodic Vibrations of Structures With Contact Interfaces
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A Method for Parametric Analysis of Stability Boundaries for Nonlinear Periodic Vibrations of Structures With Contact Interfaces

机译:接触界面结构非线性周期振动稳定边界的参数分析方法

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摘要

A method for parametric analysis of the stability loss boundary has been developed for periodic regimes of nonlinear forced vibrations for a first time. The method allows parametric frequency-domain calculations of the stability loss together with the vibration amplitudes and design parameter values corresponding to the stability boundaries. The tracing algorithm is applied to obtain the trajectories of stability loss points as functions of design parameters. The parametric stability loss is formulated for cases when (i) the design parameters characterize the properties of nonlinear contact interfaces (e.g., gap, contact stiffness, and friction coefficient); (ii) the design parameters describe linear components of the analyzed structure (e.g., parameters of geometric shape, material, natural frequencies, and modal damping); and (iii) these parameters describe the excitation loads (e.g., their level, distribution or frequency). An approach allowing the multiparametric analysis of stability boundaries is proposed. The method uses the multiharmonic representation of the periodic forced response and aimed at the analysis of realistic gasturbine structures comprising thousands and millions degrees-of-freedom (DOF). The method can be used for the effective search of isolated branches of the nonlinear solutions and examples of detection and search of the isolated branches are given: for relatively small and for large-scale finite element (FE) models. The efficiency of the method for calculation of the stability boundaries and for the search of isolated branches is demonstrated on simple systems and on a large-scale model of a turbine blade.
机译:首次针对非线性强迫振动的周期状态,开发了一种稳定性损失边界的参数分析方法。该方法允许对稳定性损失进行参数频域计算,以及对应于稳定性边界的振动幅度和设计参数值。应用跟踪算法获得稳定性损失点的轨迹,作为设计参数的函数。当(i)设计参数表征非线性接触界面的特性(例如,间隙,接触刚度和摩擦系数)时,可计算出参数稳定性损失。 (ii)设计参数描述了分析结构的线性成分(例如,几何形状,材料,固有频率和模态阻尼的参数); (iii)这些参数描述了激励负载(例如,它们的水平,分布或频率)。提出了一种允许对稳定边界进行多参数分析的方法。该方法使用了周期性强制响应的多谐波表示,旨在分析包括数千个和数百万个自由度(DOF)的实际燃气轮机结构。该方法可用于非线性解的孤立分支的有效搜索,并给出检测和搜索孤立分支的示例:适用于相对较小和大规模的有限元(FE)模型。在简单的系统和大型的涡轮叶片模型上证明了计算稳定边界和寻找孤立分支的方法的效率。

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