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Fatigue life prediction of regulating valves on the intermediate-pressure section of a 400 MW steam turbine

机译:400 MW汽轮机中压段调节阀的疲劳寿命预测。

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Fatigue life prediction of regulating valves on the intermediate-pressure (IP) section of steam turbine is presented in this paper. The transient temperature fields and stress fields of the valve body are calculated using finite element method, and the operating records of a 400 MW steam turbine located in Hubei Province of China, is used as input, and all practical operating processes including cold-startup, hot-startup, extreme-hot-startup, shutdown and emergence shutdown are considered in the FEM computations. The load patterns for the valve are determined using rain-flow counting method and the local stress-strain approach, furthermore, the cyclic stress-strain loop of the key point enduring maximum stress range is plotted. Prediction of fatigue crack-initiation life for the turbine valve is given, and the life and crack prediction are agreed with the data from practical industry inspection. It is found in the computation that the maximum stress range appears near the stiffening rib in the valve body during turbine service. This result indicates that the circumferential thermal stress concentration region is near the stiffening rib, and also implied that crack may emerge in this location. Some cracks are actually witnessed near the rib when we did inspection on the turbine valves since 2000. The fatigue life prediction is also roughly accord with our investigative data. It is concluded that the damage during turbine emergence shutdown contributes the main part to the damage fatigue capability which is defined as the number of cycles to crack-initiation in the valve due to cyclic operating conditions. The method for comprehensive study on transient temperature and stress fields and life estimation of the turbine valve is also proposed in this paper.
机译:提出了汽轮机中压(IP)段调节阀的疲劳寿命预测。阀体的瞬态温度场和应力场采用有限元法计算,并以位于中国湖北省的400 MW汽轮机的运行记录作为输入,并包括冷启动, FEM计算中考虑了热启动,极端热启动,关机和紧急关机。通过雨流计数法和局部应力应变法确定了阀门的载荷模式,并绘制了承受最大应力范围的关键点的循环应力应变循环。给出了涡轮阀疲劳裂纹萌生寿命的预测,其寿命和裂纹预测与实际的工业检验数据相吻合。在计算中发现,在涡轮机维修期间,最大应力范围出现在阀体内的加强肋附近。该结果表明,周向热应力集中区域在加强肋附近,并且还暗示在该位置可能出现裂纹。自2000年以来,当我们对涡轮机气门进行检查时,实际上在肋骨附近发现了一些裂纹。疲劳寿命的预测也大致与我们的研究数据相符。结论是,涡轮机紧急停机期间的损坏是损坏疲劳能力的主要部分,疲劳疲劳能力的定义是由于循环工况而导致阀中裂纹产生的循环次数。本文还提出了对瞬态温度和应力场进行综合研究以及对涡轮阀寿命进行估算的方法。

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