轴流风机变负荷泄漏流的实验研究

IF 1.3 Q2 ENGINEERING, AEROSPACE
E. Canepa, A. Cattanei, M. Moradi, A. Nilberto
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引用次数: 0

摘要

本文报道了低速环形风机中运行点对泄漏流影响的2D-PIV(粒子图像测速法)研究。首先,研究了覆盖整个特性曲线的12个操作点的流型。在非常低的负载下,泄漏流沿着转子环流动,并被直接再压缩;然后,附着在环上的分离气泡形成,在接近设计点时,该分离气泡在径向向外流动的流动中发生变化。随着载荷的进一步增加,叶尖区域出现分离的流动区域,该区域最终与泄漏流汇合。在设计一附近的八个操作点进行了进一步、更详细的研究。非常小的负载变化可能会导致泄漏流型的改变,但在过渡期间不存在间歇性,因为任何中间类型的瞬时流型都会连续交替。这些结果为以前的声学测量结果提供了一致的解释。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental Study of the Leakage Flow in an Axial-Flow Fan at Variable Loading
The present paper reports a 2D-PIV (particle image velocimetry) study of the effect of the operating point on the leakage flow in a low-speed ring fan. First, the flow pattern has been studied at 12 operating points covering the whole characteristic curve. At very low loading, the leakage flow streams along the rotor ring and is directly reingested; then, a separation bubble attached to the ring forms that, approaching the design point, modifies in a flow streaming radially outward. As the loading further increases, a separated flow region appears in the blade tip region that finally merges with the leakage flow. A further, more detailed study has been performed at eight operating points in the neighborhood of the design one. Very small loading variations may yield the leakage flow pattern modification, but no intermittence is present during the transition, as instantaneous flow patterns of any intermediate type continuously alternate. These results provide a consistent explanation for the ones of previous acoustic measurements.
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来源期刊
CiteScore
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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