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A Study on the Fundamental Cause of Stall Stagnation Phenomena in Surges in Compressor Systems

机译:压缩机系统喘振失速停滞现象的根本原因研究

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Although the stall stagnation phenomena have often been experienced in site and also analytically in numerical experiments in surges in systems of compressors and flow paths, the fundamental causes have not been identified yet. In order to clarify the situations, behaviours of infinitesimal disturbance waves superposed on a main flow were studied in a simplified one-dimensional flow model. A ratio of the amplifying rate of the system instability to the characteristic slope of the compressor element was surveyed as the instability enhancement factor. Numerical calculations have shown the following tendency of the factor. In the situation where both the sectional area ratio and the length ratio of the delivery flow-path to the suction duct are sufficiently large, the enhancement factors are greater in magnitude, which means occurrence of ordinary deep surges. However, in the situation where the area ratio and/or the length ratio is relatively smaller, the enhancement factor tends to lessen significantly, which situation tends to suppress deep surges for the same value of the characteristic slope. It could result in the stall stagnation condition. In the domain of area ratio vs. length ratio of the delivery duct to the suction duct, contour-lines of the enhancement factor behave qualitatively similar to those of the stall stagnation boundaries of a fan analytically obtained, suggesting that a certain range of the enhancement factor values could specify the stagnation occurrence. The significant decreases in the factors are observed to accompany appearances of phase lags and travelling waves in the wave motions, which macroscopically suggests breaking down of the complete surge actions of filling and emptying of the air in the delivery duct. The strength of the action is deeply related with acoustic interferences and is evaluated in terms of the volume-modified reduced resonance frequency proposed by the author. These observations have shown the fundamental cause and the sequence of the stall stagnation in principle.
机译:尽管失速停滞现象经常在现场以及压缩机和流路系统喘振中的数值实验中进行分析,但根本原因尚未确定。为了弄清情况,在简化的一维流模型中研究了叠加在主流上的无穷小扰动波的行为。作为不稳定性增强因素,调查了系统不稳定性的放大率与压缩机元件的特性斜率的比。数值计算表明该因子具有以下趋势。在输送流路到吸引管的截面积比和长度比都足够大的情况下,增强因子的大小较大,这意味着发生普通的深波动。然而,在面积比和/或长度比相对较小的情况下,增强因子趋于显着减小,对于相同的特征斜率值,这种情况趋于抑制深度波动。这可能导致失速停滞状态。在输送管与吸入管的面积比与长度比的范围内,增强因子的轮廓线在质量上的行为类似于通过分析获得的风扇的失速停滞边界的轮廓线,这表明增强的特定范围因子值可以指定停滞发生。观察到这些因素的显着降低是伴随着相位滞后和行波运动中行波的出现,这从宏观上暗示了输送管道中空气填充和排空的完全浪涌作用的破坏。该作用的强度与声干扰密切相关,并根据作者提出的体积修正降低的共振频率进行评估。这些观察从原理上显示了失速停滞的根本原因和顺序。

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