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Analysis of dynamic stresses in Kaplan turbine blades

机译:卡普兰涡轮叶片中的动态应力分析

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Purpose - Some comparison of unsteady flow calculation and the measured stress showed that the dynamic stresses in blades are closely related to hydraulic instability. However, few studies have been conducted for the hydraulic machinery to calculate dynamic stresses caused by the unsteady hydraulic load. The present paper aims to analyse the stresses in blades of a Kaplan turbine. Design/methodology/approach - By employing a partially coupled solution of 3D unsteady flow through its flow passage, the dynamic interaction problem of the blades was analyzed. The unsteady Reynolds-averaged Navier-Stokes equations with the SST κ-ω turbulence model were solved to model the flow within the entire flow path of the Kaplan turbine. The time-dependent hydraulic forces on the blades were used as the boundary condition for the dynamics problem for blades. Findings - The results showed that the dynamic stress in the blade is low under approximately optimum operating conditions and is high under low-output conditions with a small guide vane opening, a small blade angle and a high head.rnResearch limitations/implications - It is assumed that there is no feedback of blade motion on the flow. Self-excited oscillations are beyond the scope of the present paper. Originality/value - The authors developed a code to transfer the pressure on blades as a boundary condition for structure analysis without any interpolation. The study indicates that the prediction of dynamic stress during the design stage is possible. To ensure the safety of the blades it is recommended to check the safety coefficient during the design stage for at least two conditions: the 100 percent output with lower head and the 50 percent output with the highest head.
机译:目的-比较非定常流量和测得的应力表明,叶片中的动应力与水力不稳定密切相关。但是,对于液压机械来计算由不稳定的液压载荷引起的动态应力的研究很少。本文旨在分析Kaplan涡轮机叶片中的应力。设计/方法/方法-通过使用3D非恒定流通过其流动通道的部分耦合解决方案,分析了叶片的动态相互作用问题。解决了具有SSTκ-ω湍流模型的非稳态雷诺平均Navier-Stokes方程,以对Kaplan涡轮整个流动路径内的流动进行建模。叶片上随时间变化的水力被用作叶片动力学问题的边界条件。研究结果-结果表明,叶片的动态应力在最佳运行条件下较低,而在低输出条件下叶片导叶开口小,叶片角度小且扬程高时,动应力较高。研究限制/意义-假设没有叶片运动对流的反馈。自激振荡超出了本文的范围。原创性/价值-作者开发了一个代码,可以将叶片上的压力作为边界条件进行结构分析,而无需任何插值。研究表明,在设计阶段预测动态应力是可能的。为了确保刀片的安全,建议在设计阶段至少检查以下两个条件的安全系数:较低扬程的输出功率为100%,最高扬程的输出功率为50%。

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