首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >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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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 characterise the properties of nonlinear contact interfaces (e.g. gap, contact stiffness, friction coefficient, etc.) and (ⅱ) the design parameters describe linear components of the analysed structure (e.g. parameters of geometric shape, material, natural frequencies, modal damping etc.) 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 gas-turbine structures comprising thousands and millions degrees of freedom. 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 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,开发了一种用于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。针对以下情况制定参数稳定性损失:(ⅰ)设计参数表征了非线性接触界面的特性(例如,间隙,接触刚度,摩擦系数等),并且(ⅱ)设计参数描述了所分析结构的线性成分(例如,几何形状,材料,固有频率,模态阻尼等参数)和(ⅲ)这些参数描述了励磁负载(例如其水平,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。该方法使用周期性强迫响应的多谐波表示,旨在分析包含数千个和数百万个自由度的真实燃气轮机结构。该方法可用于非线性解的孤立分支的有效搜索,并给出孤立分支的检测和搜索示例:针对相对较小和大规模的有限元模型。在简单的系统和大型的涡轮叶片模型上证明了计算稳定性边界和寻找孤立分支的方法的效率。

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