尾水管内气液两相流动测量

doi:10.16183/j.cnki.jsjtu.2023.091

上海交通大学学报 ›› 2024, Vol. 58 ›› Issue (8): 1188-1200.doi: 10.16183/j.cnki.jsjtu.2023.091

尾水管内气液两相流动测量

李金凤¹^,², 陈武光¹, 张正川¹, 徐用良²^,³^,⁴, 李开盈⁵, 尹俊连¹(), 王德忠¹

1.上海交通大学机械与动力工程学院,上海 200240
2.水力发电设备国家重点实验室,哈尔滨 150040
3.哈尔滨电机厂有限责任公司,哈尔滨 150040
4.哈尔滨大电机研究所, 哈尔滨 150040
5.中核核电运行管理有限公司,浙江嘉兴 314300

收稿日期:2023-03-14 修回日期:2023-06-21 接受日期:2023-06-29 出版日期:2024-08-28 发布日期:2024-08-27
通讯作者: 尹俊连,副研究员;E-mail:jlyin@sjtu.edu.cn.
作者简介:李金凤(1999-),硕士生,从事气液两相旋流稳定性研究.
基金资助:
国家自然科学基金(52276158);国家自然科学基金(52206203)

Measurement of Gas-Liquid Two-Phase Flow in Draft Tube

LI Jinfeng¹^,², CHEN Wuguang¹, ZHANG Zhengchuan¹, XU Yongliang²^,³^,⁴, LI Kaiying⁵, YIN Junlian¹(), WANG Dezhong¹

1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
2. State Key Laboratory of Hydropower Equipment, Harbin 150040, China
3. Harbin Electric Machinery Co., Ltd., Harbin 150040, China
4. Harbin Institute of Large Electrical Machinery, Harbin 150040, China
5. China National Nuclear Power Operation Management Co., Ltd., Jiaxing 314300, Zhejiang, China

Received:2023-03-14 Revised:2023-06-21 Accepted:2023-06-29 Online:2024-08-28 Published:2024-08-27

摘要/Abstract

摘要：

当水轮机在部分负荷工况下运行时,尾水管内会形成不稳定的螺旋涡带流动,导致严重的流量不平衡,进而影响系统动态特性.获取尾水管内完整的气液两相流动,是分析涡带生成和发展机理从而对其进行有效控制的基础.为此,本文突破传统测量技术在气液两相流测量中的局限性,结合粒子图像测速和脉冲阴影技术,同步测量液相速度场和两个垂直方向的涡带形态.分析不同涡带形态的演化过程,进一步通过图像处理获取螺旋涡带的直径和空间信息,实现单螺旋涡带的三维重建,得到单螺旋涡带清晰的三维形态和旋转进动过程.最后对尾水管内呈现单螺旋涡带时的液相速度场进行分析,并将液相速度场与涡带的三维形态进行空间关联分析.实验研究表明:尾水管内涡带呈现单螺旋、双螺旋、气芯堆叠3种形态的不稳定循环流动演化,单螺旋涡带局部一分为二时,会转化为双螺旋涡带;单螺旋涡带局部螺旋升角不断减小时,会发生涡带堆叠破裂;尾水管内呈现单螺旋涡带时,涡带整体随液相主流绕中心轴线旋转进动,同时涡带自身局部存在绕某一轴线的旋转,涡带形态的螺旋旋向与整体旋转进动的螺旋旋向相反.流动根据轴向速度分为外围主流区和中心滞止区两部分,主流区和滞止区之间的剪切层卷起形成旋涡,液相旋涡的位置决定了螺旋涡带的空间形态.

关键词: 尾水管涡带, 气液两相流, 粒子图像测速, 脉冲阴影, 涡带三维重建

Abstract:

The limitation of traditional measurement technology in gas-liquid two-phase flow measurement is broken through.The liquid velocity field and vortex rope morphology from two vertical directions were measured synchronically by using particle image velocimetry and pulsed shadowgraphy technique. Experimental measurements show that the vortex rope in the draft tube presents three kinds of unstable circulation flow evolution, single spiral, double spiral, and overstocked rupture. When a single spiral vortex rope is partially split into two, it becomes a double spiral vortex rope. When the local spiral rise angle of a single spiral vortex rope decreases, it becomes an overstocked rupture. When there is a single spiral vortex rope in the draft tube, the vortex rope rotates precession around the central axis along with the liquid main flow, and the flow is divided into two parts, the outer main flow zone and the central stagnation zone, according to the axial velocity. The shear layer between the main flow zone and the stagnation zone rolls up to form several vortices. The position of liquid vortices determines the spatial morphology of the spiral vortex rope.

Key words: vortex rope, gas-liquid two-phase flow, particle image velocimetry, pulsed shadowgraphy, 3D reconstruction

中图分类号:

TK730.1

李金凤, 陈武光, 张正川, 徐用良, 李开盈, 尹俊连, 王德忠. 尾水管内气液两相流动测量[J]. 上海交通大学学报, 2024, 58(8): 1188-1200.

LI Jinfeng, CHEN Wuguang, ZHANG Zhengchuan, XU Yongliang, LI Kaiying, YIN Junlian, WANG Dezhong. Measurement of Gas-Liquid Two-Phase Flow in Draft Tube[J]. Journal of Shanghai Jiao Tong University, 2024, 58(8): 1188-1200.

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参考文献 15

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序号	Q_l×10³/ (m³·s^-1)	Q_g/(m³·s^-1)	Re×10^-5	β/%
1	2.01	3.33×10^-6	0.57	0.17
2	2.01	6.66×10^-6	0.57	0.33
3	2.91	3.33×10^-6	0.82	0.11
4	2.91	6.66×10^-6	0.82	0.23
5	2.91	1.00×10^-5	0.82	0.34
6	2.91	1.33×10^-5	0.82	0.46
7	2.91	1.66×10^-5	0.82	0.57
8	3.52	6.66×10^-6	1.00	0.19
9	3.52	1.00×10^-5	1.00	0.28
10	4.31	6.66×10^-6	1.23	0.15
11	4.31	1.00×10^-5	1.23	0.23
12	4.98	1.00×10^-5	1.41	0.20

尾水管内气液两相流动测量

Measurement of Gas-Liquid Two-Phase Flow in Draft Tube

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