首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.5; 20070514-17; Montreal(CA) >PREDICTION OF HIGH CYCLE FATIGUE LIFE OF STEAM TURBINE BLADING BASED ON UNSTEADY CFD AND FEM FORCED RESPONSE CALCULATION
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PREDICTION OF HIGH CYCLE FATIGUE LIFE OF STEAM TURBINE BLADING BASED ON UNSTEADY CFD AND FEM FORCED RESPONSE CALCULATION

机译:基于非定常CFD和有限元强迫响应计算的汽轮机叶片高周疲劳寿命预测

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This paper presents the high cycle fatigue life prediction of a shrouded packet blade row for a large high pressure steam turbine. The fatigue life assessment was based on a loosely coupled CFD and FEM calculations supported by the direct cyclic mechanical testing of a full scale model of the blade root attachment. In the first stage, potentially dangerous vibration modes were identified from the linear finite element analyses and verified by testing. Aerodynamic forces acting on rotating blades were obtained from an unsteady sliding mesh CFD calculation based on a viscous unsteady compressible turbulent flow. A forced vibration analysis was then performed for critical resonance frequencies close to nozzle passing frequency considering only the inherent material damping. The calculated alternating stress in the blade root attachment was used to estimate the safety against the high cycle fatigue failure. Fatigue life was evaluated for current and new design of stationary vanes. In the new design the number of vanes was increased and their full 3D shape was optimized. Both changes reduced the excitation forces by more then an order of magnitude. The final evaluation showed that the vibratory stresses for the new design were well below the actual fatigue limit of the blade root attachment.
机译:本文介绍了大型高压蒸汽轮机带罩叶片叶片行的高周疲劳寿命预测。疲劳寿命评估基于松散耦合的CFD和FEM计算,并通过对叶片根部附件的完整模型进行直接循环机械测试得到支持。在第一阶段,从线性有限元分析中识别出潜在危险的振动模式,并通过测试进行验证。作用在旋转叶片上的空气动力是通过基于粘性非稳态可压缩湍流的非稳态滑动网格CFD计算获得的。然后仅考虑固有材料阻尼,对接近喷嘴通过频率的临界共振频率进行强制振动分析。叶片根部附件中计算出的交变应力用于估计高周疲劳失效的安全性。针对固定叶片的最新设计和新设计,评估了疲劳寿命。在新设计中,增加了叶片的数量,并优化了其完整3D形状。两种变化都将激励力降低了一个数量级。最终评估表明,新设计的振动应力远低于叶片根部附件的实际疲劳极限。

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