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Explicit analysis using time-dependent damping simulation of one-sided laser shock peening on martensitic steel turbine blades

机译:用时间依赖性阻尼仿真在马氏体钢涡轮叶片上采用一侧激光冲击的时间依赖性阻尼模拟

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摘要

Down-times from the in-service failure of power plant components, such as turbine blades, portend dire impacts and consequences in the form of huge financial losses. The susceptibility of steam turbine blades to failure is now being reduced by a novel technique, laser shock peening (LSP), which induces compressive layers through the surface of the blades. Current simulation studies of LSP employing conventional methods are indeed computationally expensive and time-consuming. Hence, this paper explores an alternative numerical modeling technique to investigate the economic parameters of residual stresses induced in martensitic steel turbine blades when subjected to LSP treatment. An explicit simulation method of analysis, using commercial finite-element software, which employs time-dependent damping, is presented. The study shows that this technique is time-efficient compared with the conventional explicit-implicit methods commonly used for such simulations. It is interesting to note that the results indicate that up to 500 MPa of induced compressive stress of layers reaching 1 mm in depth can be obtained. Encouragingly, these results correlate well with previous experimental studies, lending credence to the method’s validity. The technique employed hence offers solutions for timely, non-destructive, methodical maintenance and improvement of the mechanical properties of turbine blades, in the quest to reduce the risks of their in-service failure, as well as lengthening of their service life.
机译:从发电厂组件的换行失败,如涡轮叶片,以巨大的财务损失的形式开展可怕的影响和后果的逆时。现在通过一种新颖的技术,激光冲击喷丸(LSP)来降低蒸汽轮机叶片对故障的敏感性,其引起压缩层穿过叶片的表面。使用常规方法的LSP的电流模拟研究确实是计算昂贵且耗时的。因此,本文探讨了替代的数值建模技术,以研究在进行LSP处理时探讨马氏体钢涡轮机叶片中诱导的残余应力的经济参数。采用采用时间依赖性阻尼的商业有限元软件,提出了一种显式仿真方法。该研究表明,与通常用于这种模拟的传统显式隐式方法相比,该技术与这种技术相比是较效率的。值得注意的是,结果表明,可以获得高达500MPa的诱导的层的诱导压缩应力达到1mm深度的深度。鼓励,这些结果与先前的实验研究相关,贷款信任对该方法的有效性很好。因此,该技术因此提供了用于及时,无损,有条理的维护和改进涡轮叶片的机械性能的解决方案,以减少其在役失败的风险,以及它们的使用寿命的延长。

著录项

  • 来源
    《Simulation》 |2020年第12期|927-938|共12页
  • 作者

    Festus Fameso; Dawood Desai;

  • 作者单位

    Department of Mechanical and Mechatronics Engineering Tshwane University of Technology;

    Department of Mechanical and Mechatronics Engineering Tshwane University of Technology;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Laser peening; martensitic steel; modeling; residual stresses; simulation;

    机译:激光喷丸;马氏体钢;建模;残余应力;模拟;

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