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Analytical Formulation of the Jacobian Matrix for Non-linear Calculation of the Forced Response of Turbine Blade Assemblies with Wedge Friction Dampers

机译:带楔形摩擦阻尼器的涡轮叶片总成强迫响应非线性计算的雅可比矩阵的解析表示

摘要

A fundamental issue in turbomachinery design is the dynamical stress assessment of turbine blades. In order to reduce stress peaks in the turbine blades at engine orders corresponding to blade natural frequencies, friction dampers are employed. Blade response calculation requires the solution of a set of non-linear equations originated by the introduction of friction damping. Such a set of non-linear equations is solved using the iterative numerical Newton-Raphson method. However, calculation of the Jacobian matrix of the system using classical numerical finite difference schemes makes frequency domain solver prohibitively expensive for structures with many contact points. Large computation time results from the evaluation of partial derivatives of the non-linear equations with respect to the displacements. In this work a methodology to compute efficiently the Jacobian matrix of a dynamic system having wedge dampers is presented. It is exact and completely analytical. The proposed methods have been successfully applied to a real intermediate pressure turbine (IPT) blade under cyclic symmetry boundary conditions with underplatform wedge dampers. Its implementation showed to be very effective, and allowed to achieve relevant time savings without loss of precision.
机译:涡轮机械设计中的一个基本问题是涡轮叶片的动态应力评估。为了减小对应于叶片固有频率的发动机指令时涡轮叶片中的应力峰值,采用了摩擦阻尼器。叶片响应计算需要解决一组引入摩擦阻尼的非线性方程。使用迭代数值牛顿-拉夫森方法求解此类非线性方程组。然而,使用经典的数值有限差分方案对系统的雅可比矩阵进行计算,使得频域求解器对于具有许多接触点的结构而言过于昂贵。相对于位移,非线性方程的偏导数评估会导致较大的计算时间。在这项工作中,提出了一种有效计算具有楔形阻尼器的动态系统的雅可比矩阵的方法。这是精确且完全分析的。所提出的方法已经成功地应用于具有平台不足的楔形阻尼器的循环对称边界条件下的真实中压涡轮(IPT)叶片。它的实施显示出非常有效的效果,并且可以节省相关时间,而不会降低精度。

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  • 年度 2006
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"english","id":9}
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