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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistiuning
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Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistiuning

机译:涡轮发动机叶片盘的强制响应和对谐波误响的敏感性

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摘要

The mistimed forced response of turbine engine bladed disks is treated using harmonic perturbations in the properties of a continuous ring. A continuous shear spring is attached to the ring in which the stiffness is allowed to vary along the ring annulus. The modes of such a structure with a single harmonic mistuning pattern are shown to obey the Mathieu equation, which is solved to obtain the natural frequencies and modes of the mistuned system. The forced response of the system is then examined to determine the sensitivity of the system to small mistuning. The model is extended to include multiple harmonics, allowing for the possibility of general mistuning. An expression for the maximum amplitude magnification due to small mistuning is developed by showing that high response is caused by distortion of the structural modes. A method to intentionally mistune systems for maximum forced response is demonstrated, and numerical results demonstrate the accuracy of the analytical prediction. The intentionally mistuned system response is shown to be robust with respect to small random mistuning. Such a result might be useful for designing a test rotor for screening new bladed disk designs or for establishing the root cause of fatigue problems.
机译:使用连续环特性中的谐波扰动来处理涡轮发动机叶片盘的时机错误的强制响应。连续的剪切弹簧连接到环,在其中允许刚度沿着环的环面变化。示出了具有单谐波失谐模式的这种结构的模式服从Mathieu方程,该方程被求解以获得失谐系统的固有频率和模式。然后检查系统的强制响应,以确定系统对小故障的敏感性。该模型被扩展为包括多个谐波,从而允许出现一般的失谐。通过显示出高响应是由结构模式的扭曲引起的,得出了由于小模糊而导致的最大振幅放大率的表达式。演示了有意误调系统以获得最大强制响应的方法,数值结果证明了分析预测的准确性。有意为之误解的系统响应显示出相对于较小的随机性错解是鲁棒的。这样的结果对于设计用于筛选新叶片盘设计的测试转子或确定疲劳问题的根本原因可能是有用的。

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