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Forced vibration of turbine blades

机译:涡轮叶片的强迫振动

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摘要

Many turbines in operation today were designed at a time when little was known about the unsteady loading on blades or about damping. As a result, the blades were designed using a tuning criterion and a steady stress criuterion. More recent approaches to this problem have used the concept of :"stimulus." The stimulus approach assumes that the unsteady loading is proportional to the steady loading on the blade. While this approach is more satisfactory than the steady stress criterion, it is a one mode at a time approach and leaves open the question of vibratory stresses in more than one mode combining to produce a stress greater than the reduced endurance strength. This paper summarizes the deterministic approach described above and extends the analysis, using probabilistic design methods, to include the possibility of stresses in multiple modes combining. The method presented also includes the effect of statistical variations in other design parameters. It is shown that, at the reliability levels of interest, it is necessary to consider multiple mode contributions to the total vibratory stress. The output of this new approach also gives a probability of failure that can be used to make rational decisions when considering different design alternatives.
机译:当今许多运转中的涡轮机是在人们对叶片上的不稳定载荷或阻尼知之甚少的时候设计的。结果,使用调整标准和稳定的应力变形来设计叶片。解决该问题的最新方法使用了“刺激”的概念。激励方法假定非稳定负载与叶片上的稳定负载成比例。尽管此方法比稳态应力准则更令人满意,但它是一次的一种模式,并以一种以上的模式组合产生振动应力的问题,这种振动组合产生的应力大于降低的耐力强度。本文总结了上述确定性方法,并使用概率设计方法扩展了分析范围,以涵盖多种模式组合中出现应力的可能性。提出的方法还包括其他设计参数中统计变化的影响。结果表明,在感兴趣的可靠性级别上,有必要考虑多种模式对总振动应力的影响。这种新方法的输出还给出了失败的可能性,当考虑不同的设计替代方案时,可以用来做出合理的决定。

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