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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Blade Vibration Stress Determination Method Based on Blade Tip Timing Simulator and Finite Element Method
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Blade Vibration Stress Determination Method Based on Blade Tip Timing Simulator and Finite Element Method

机译:基于叶尖正时模拟器和有限元法的叶片振动应力确定方法

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Blade tip timing (BTT) measurement technology is more widely used to determine the vibrational stress of rotating blades and play an important role for blade service life prediction. The dynamic blade displacements can be measured by tip timing sensors, and then be converted to blade stress by the modal shape information from finite element method (FEM) analysis. However, there are always two uncertainties between the measured displacements by BTT and the modal shape by FEM analysis. First, the effective positions detected by sensors may shift from where they expected due to the deformation of the blade. This deviation may yield calibration factors with deceptions, which will present an inaccurate correlation for the blade stress level and the tip displacement. Second, when vibrating, blade tip would actually oscillate around the equilibrium position both in circumferential and axial direction, while the sensors can only detect the movements along the circumference direction and neglect the other. This causes the measured displacements to be different from the actual displacements. To deal with these two problems, a novel method based on the vibration amplitudes of blade tip along axial direction is proposed to identify the effective detected position. The vibration stress of the whole blade then can be determined by linking the modified displacements to the mode shape information from finite element (FE) predictions. This method is validated by a numerical BTT simulator, which is trying to simulate the actual testing process of BTT measurement. Both synchronous and asynchronous vibrations are discussed to illustrate the applicability of this method. Moreover, sensitivity analysis is performed to identify the uncertainties from the vibration amplitude and mode shape inaccuracies. Results demonstrate the great potential of the method for vibration stress determination.
机译:叶片尖端时间(BTT)测量技术被广泛用于确定旋转叶片的振动应力,并在预测叶片使用寿命方面起着重要作用。可以通过叶尖正时传感器测量动态叶片位移,然后通过来自有限元方法(FEM)分析的模态形状信息将其转换为叶片应力。但是,通过BTT测量的位移与通过FEM分析得到的模态形状之间始终存在两个不确定性。首先,由于叶片的变形,传感器检测到的有效位置可能会偏离预期位置。该偏差可能会产生带有欺骗性的校准因子,这将为叶片应力水平和叶尖位移提供不准确的相关性。其次,当振动时,叶片尖端实际上会在平衡位置上沿圆周方向和轴向方向振动,而传感器只能检测沿圆周方向的运动而忽略其他方向。这导致测得的位移与实际位移不同。针对这两个问题,提出了一种基于叶尖沿轴向振动幅度的新方法来识别有效检测位置。然后可以通过将修改后的位移与来自有限元(FE)预测的模态形状信息相关联,来确定整个叶片的振动应力。该方法已通过数值BTT模拟器验证,该模拟器正在尝试模拟BTT测量的实际测试过程。讨论了同步振动和异步振动,以说明该方法的适用性。此外,执行灵敏度分析以从振动幅度和模态形状误差中识别不确定性。结果证明了该方法在确定振动应力方面的巨大潜力。

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