Experimental investigation of cavitation instabilities in inducer with different tip clearances

被引:0
|
作者
Le XIANG [1 ]
Yonghua TAN [2 ]
Hui CHEN [1 ]
Kaifu XU [3 ]
机构
[1] Science and Technology on Liquid Rocket Engine Laboratory
[2] Academy of Aerospace Propulsion Technology
[3] Xi'an Aerospace Propulsion Institute
关键词
D O I
暂无
中图分类号
V433.9 [发动机试验];
学科分类号
080703 ; 082502 ;
摘要
To investigate the effect of tip clearance size on cavitation characteristics in a turbopump inducer, a series of experiments have been conducted in a newly developed visualization test facility using room temperature water as working fluid. The pressure fluctuations near the tip region were collected, and the cavity structures under various conditions were documented by a high-speed camera. It is found that large tip clearance distinctly reduces both the non-cavitation and cavitation performance. Three cavitation instabilities, super-synchronous rotating cavitation, synchronous rotating cavitation and cavitation surge have been carefully identified through combination of cross-correlation analysis of pressure signals and visualization results. Large tip clearance displays a remarkable stabilization effect on pressure fluctuation, cavitation surge totally disappears, and the range of occurrence of synchronous rotating cavitation becomes smaller for the large tip clearance,whereas super-synchronous rotating cavitation only occurs in the large tip clearance. The cavitation areas are smaller at large tip clearance, while the flow channels are more seriously choked when cavitation occurs heavily in comparison with those at small tip clearance, which may be responsible for the worse cavitation performance.
引用
收藏
页码:168 / 177
页数:10
相关论文
共 50 条
  • [1] Experimental investigation of cavitation instabilities in inducer with different tip clearances
    Le XIANG
    Yonghua TAN
    Hui CHEN
    Kaifu XU
    Chinese Journal of Aeronautics , 2021, (09) : 168 - 177
  • [2] Experimental investigation of cavitation instabilities in inducer with different tip clearances
    Xiang, Le
    Tan, Yonghua
    Chen, Hui
    Xu, Kaifu
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (09) : 168 - 177
  • [3] Experimental and Numerical Investigation on the Tip Leakage Vortex Cavitation in an Axial Flow Pump with Different Tip Clearances
    Xu, Bin
    Shen, Xi
    Zhang, Desheng
    Zhang, Weibin
    PROCESSES, 2019, 7 (12)
  • [4] An experimental investigation into turbine flutter characteristic at different tip-clearances
    Huang, X. Q.
    He, L.
    Bell, D. L.
    Proceedings of the ASME Turbo Expo 2006, Vol 5, Pts A and B, 2006, : 1071 - 1080
  • [5] Investigation of cavitation and flow characteristics of tip clearance of bidirectional axial flow pump with different clearances
    Wang, Lin
    Tang, Fangping
    Liu, Haiyu
    Zhang, Xiaowen
    Sun, Zhuangzhuang
    Wang, Fei
    OCEAN ENGINEERING, 2023, 288
  • [6] Inducer Design to Avoid Cavitation Instabilities
    Kang, Donghyuk
    Watanabe, Toshifumi
    Yonezawa, Koichi
    Horiguchi, Hironori
    Kawata, Yutaka
    Tsujimotol, Yoshinobu
    10TH ASIAN INTERNATIONAL CONFERENCE ON FLUID MACHINERY, 2010, 1225 : 433 - +
  • [7] Suction performance and cavitation instabilities of turbopumps with three different inducer design
    Morii T.
    Tanaka Y.
    Watanabe S.
    Ohashi S.
    Matsunaga Y.
    International Journal of Fluid Machinery and Systems, 2019, 12 (02) : 128 - 135
  • [8] Experimental characterization of cavitation instabilities in a two-bladed axial inducer
    Cervone, Angelo
    Bramanti, Cristina
    Rapposelli, Emilio
    Torro, Lucio
    d'Agostino, Luca
    JOURNAL OF PROPULSION AND POWER, 2006, 22 (06) : 1389 - 1395
  • [9] Thermodynamic effect on cavitation performances and cavitation instabilities in an inducer
    Kikuta, Kengo
    Yoshida, Yoshiki
    Watanabe, Mitsuo
    Hashimoto, Tomoyuki
    Nagaura, Katsuji
    Ohira, Katsuhide
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2008, 130 (11): : 1113021 - 1113028
  • [10] Cavitation instabilities of an inducer in a cryogenic pump
    Kim, Dae-Jin
    Sung, Hyung Jin
    Choi, Chang-Ho
    Kim, Jin-Sun
    ACTA ASTRONAUTICA, 2017, 132 : 19 - 24