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Monitoring low cycle fatigue damage in turbine blade using vibration characteristics

机译:利用振动特性监测涡轮叶片的低周疲劳损伤

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摘要

A finite element based approach is used to simulate the evolution of low cycle fatigue damage in a turbine blade. The turbine blade is modelled as a rotating Timoshenko beam with taper and twist. A damage growth model for low cycle fatigue damage developed using a continuum mechanics approach is integrated with the finite element model. Numerical results are obtained to study the effect of damage growth on the rotating frequencies. It is found that low cycle fatigue causes sufficient degradation in blade stiffness for changes in rotating frequency to be used as an indicator to track damage growth. Continuum damage mechanics models in conjunction with finite element analysis are used to develop thresholds for damage indicators. By placing suitable threshold on the frequency change, it is possible to detect the onset of the final stage of damage in the structure before failure occurs.
机译:基于有限元的方法用于模拟涡轮叶片中低周疲劳损伤的演变。涡轮叶片建模为带有锥度和扭曲度的旋转Timoshenko梁。使用连续体力学方法开发的低周疲劳损伤的损伤增长模型与有限元模型集成在一起。获得数值结果以研究损伤增长对旋转频率的影响。已经发现,低循环疲劳会导致叶片刚度充分下降,从而导致旋转频率的变化用作跟踪损伤增长的指标。结合有限元分析的连续损伤力学模型可用于确定损伤指标的阈值。通过在频率变化上设置适当的阈值,可以检测出发生故障之前结构中最终损坏阶段的开始。

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