首页> 外文会议>CSPE-JSME-ASME International Conference on Power Engineering Vol.1 Oct 8-11, 2001, Xi'an, China >Evaluation of low cycle fatigue life for fork-type blade root attachments of steam turbine
【24h】

Evaluation of low cycle fatigue life for fork-type blade root attachments of steam turbine

机译:汽轮机前叉式叶片根部附件的低周疲劳寿命评估

获取原文
获取原文并翻译 | 示例

摘要

We have developed a new evaluation method for low-cycle fatigue life for fork-type root attachments of long steam turbine blades. In evaluating low-cycle fatigue strength at the root attachment area, the major difficulty is the contact stress problem. The conventional method, which is based on the local peak stress or strain range and fatigue data for small, plain specimens, has several problems when it is applied at the contact area of pin joints because (a) it does not include the effect of a steep stress or strain distribution along the crack extension direction, and (b) the local peak stress at the contact area depends on the element size of finite element method (FEM) analysis, due to the stress singularity problem. In this study, low-cycle fatigue life was estimated by calculating the micro crack growth life for a range of 0.04 to 1 mm in depth under a steep strain distribution, using the micro fatigue crack growth rate, which is proportional to the effective crack length according to non-linear fracture mechanics. To verify this evaluation method, low-cycle fatigue tests on pin joint models were conducted, in which the crack growth behavior at the inner surface of the pin hole was observed by interrupting the tests. We confirmed that the estimated results for micro crack growth behavior agreed well with the measured results. To obtain the local strain range distribution for fork-type root attachments, we suggest a two-step FEM analysis, including three-dimensional analysis of a whole-blade model and two-dimensional elastic-plastic contact analysis of a single blade-fork model.
机译:我们开发了一种新的评估方法,用于评估长汽轮机叶片的叉形根部附件的低周疲劳寿命。在评估根部附着区域的低周疲劳强度时,主要困难是接触应力问题。传统方法是基于局部峰值应力或应变范围以及小而平整试样的疲劳数据的,当将其应用到销接头的接触区域时会遇到一些问题,因为(a)它不包括a的影响。由于应力奇异性问题,沿裂纹扩展方向的应力或应变分布很陡;(b)接触区域的局部峰值应力取决于有限元方法(FEM)分析的单元尺寸。在这项研究中,通过在陡应变分布下计算深度为0.04至1 mm范围内的微裂纹扩展寿命,并使用与有效裂纹长度成比例的微疲劳裂纹扩展速率,来估算低周疲劳寿命。根据非线性断裂力学。为了验证该评估方法,在销钉接头模型上进行了低周疲劳测试,其中通过中断试验观察到销钉孔内表面的裂纹扩展行为。我们确认微裂纹扩展行为的估计结果与实测结果吻合良好。为了获得叉型根系附件的局部应变范围分布,我们建议进行两步有限元分析,包括对整个叶片模型的三维分析和对单个叶片-叉子模型的二维弹塑性接触分析。 。

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