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Cracking Mechanism And Retrofit Design Of Governing Stage Blades For A Steam Turbine

机译:汽轮机调节级叶片的开裂机理及改造设计

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Cracking of blade dovetails occurred in a governing stage of a 50MW steam turbines twice within 5 months. To find out the failure mechanism and measures to avoid the failure accident, one of the cracked blades has been inspected by the metallography and a scanning electronic microscope. The inspection results show that the cracking of the blade is caused by the high cycle fatigue. When governing stage blades are in operation, the vibration of blades can extend to platform or even to dovetail parts over radial supporting surfaces depending on temperature, centrifugal force and assembly tolerance. The calculated results by FEM show that not only natural frequencies of blades in operating are smaller than that in stationary but also the modal order shifts when the blade runs from stationary to operation states. The effect of mode shift on the failure was investigated. According to the conclusion, the blades have been retrofitted by increasing neck of dovetail to avoid dangerous resonance, and the blades have been operating in healthy condition for two years after the modification. Contrarily, if the phenomenon of mode shift were ignored, it would be difficult to find out the right reason of resonance and ways to retrofit the damaged blades.
机译:50兆瓦汽轮机的调节阶段在5个月内两次出现叶片燕尾裂纹。为了找出失效机理和避免失效事故的措施,已经通过金相学和扫描电子显微镜检查了破裂的叶片之一。检查结果表明,叶片的裂纹是由高循环疲劳引起的。当调节级叶片在运行时,叶片的振动会根据温度,离心力和装配公差而扩展到平台,甚至会延伸到径向支撑面上的燕尾部件。有限元法的计算结果表明,不仅叶片在运行中的固有频率比静止时要小,而且叶片从静止状态运行到运行状态时的模态阶数也发生了变化。研究了模式转换对故障的影响。根据结论,叶片已通过增加燕尾榫的颈部进行了改装,以避免发生危险的共振,并且叶片在改造后已在健康状态下运行了两年。相反,如果忽略模式偏移现象,将很难找到正确的共振原因和改造受损叶片的方法。

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