首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >A LCF LIFE ASSESSMENT METHOD FOR STEAM TURBINE LONG BLADE BASED ON ELASTOPLASTIC ANALYSIS AND LOCAL STRAIN APPROACH
【24h】

A LCF LIFE ASSESSMENT METHOD FOR STEAM TURBINE LONG BLADE BASED ON ELASTOPLASTIC ANALYSIS AND LOCAL STRAIN APPROACH

机译:基于弹塑性分析和局部应变方法的汽轮机长叶片LCF寿命评估方法

获取原文

摘要

Cyclic loads applied to a structure can develop local cyclic plasticity deformation, lead to fatigue damage and fracture at the high-stress regions, which can be assessed through a local strain approach. Each cycle of start-operation-stop steam turbine, making the low cycle fatigue (LCF) load of long blade, results in damage to the long blade, and the fatigue fracture occurs when the damage accumulated to its critical value. To evaluate the fatigue life, the experimental data illustrating the cyclic behavior of a material under simple loading condition must be gathered, and also a suitable local stress-strain range calculation approach needs to be chosen to represent the accurate material behavior under loadings. With the consideration of the difference between the specimen and actual blade, the influential factors, such as mean stress, geometry effect, blade surface quality, and water erosion, on the fatigue life should be investigated when using the cyclic fatigue data of specimen to predict fatigue life of actual blade. In this study, a new local stress-strain range approach is introduced based on elastoplastic finite element analysis and Neuber rule. And also a modified strain-life fatigue model is used by considering leading causes of fatigue and also the cumulative damage rule is set up to predict the LCF life of the steam turbine long blade. It is found that the assessment method proposed in this study is capable of predicting the LCF life of steam turbine long blade.
机译:施加到结构上的循环载荷会产生局部的循环塑性变形,从而导致疲劳破坏和高应力区域的断裂,这可以通过局部应变方法进行评估。启停汽轮机的每个循环都会导致长叶片的低循环疲劳(LCF)负载,从而导致长叶片损坏,并且当损伤累积到其临界值时,就会发生疲劳断裂。为了评估疲劳寿命,必须收集说明材料在简单载荷条件下的循环行为的实验数据,并且还需要选择合适的局部应力-应变范围计算方法来表示材料在载荷下的精确行为。考虑到试样与实际叶片之间的差异,在使用试样的循环疲劳数据进行预测时,应研究平均应力,几何效应,叶片表面质量和水蚀等对疲劳寿命的影响因素。实际叶片的疲劳寿命。在这项研究中,基于弹塑性有限元分析和Neuber规则,引入了一种新的局部应力-应变范围方法。并考虑了疲劳的主要原因,使用了改进的应变寿命疲劳模型,并建立了累积损坏规则来预测汽轮机长叶片的LCF寿命。发现本研究提出的评估方法能够预测汽轮机长叶片的LCF寿命。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号