INFLUENCE OF TIP CLEARANCE ON THE PERFORMANCE AND MATCHING OF MULTISTAGE AXIAL COMPRESSORS

被引:0
|
作者
Zheng, Xinqian [1 ]
Yang, Heli [1 ]
机构
[1] Tsinghua Univ, Turbomachinery Lab, State Key Lab Automot Safety & Energy, Beijing 100084, Peoples R China
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2A | 2016年
关键词
FLOW;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Tip clearance has great influence on the performance of multistage axial compressors including efficiency, pressure rise, mass flow, as well as matching. This paper reports a study into the influence of tip clearance on the performance and matching of a 5-stage axial compressor by a numerical method. Different tip clearances from 0% to 5.0% span which represents the typical range of tip clearance in modern multistage axial compressors were simulated and analyzed. The results show that as tip clearance increases from 0% to 5.0% span, the choked mass flow decreases by about 21.8%, the peak pressure ratio decreases by about 43.1% and the peak efficiency decreases about 14.3 percents. As tip clearance increases, the efficiency of the whole compressor decreases in a parabolic manner not linearly as previous suggested, which is partially attributable to the cantilevered stators considered in this paper and primarily due to the mismatching of different stages. It is of great importance to control the tip clearance. When tip clearance increases, the front stage tends to work near surge condition and the rear stage tends to work near choke condition, which leads to lower efficiency than in the middle stages. A weight was defined to evaluate each stage's contribution to the whole compressor's efficiency deficit caused by the increase of tip clearance. Front and rear stages contribute more to the efficiency deficit than the middle stages, which indicates that more attention should be paid on front and rear stages to improve the performance of multistage axial compressors. In order to evaluate the matching of multistage axial compressors with a quantified method, a new parameter named "Peak Efficiency Deviation (PED)" was defined based on the difference between each stage's operating efficiency and its peak efficiency. The mass flow of multistage axial compressors should be well considered to make the PED parameter to be close to zero as possible. In the most commonly used range of tip clearance from 0.5% to 3.0% span, the PED varies little within 0.4 percent, which is only about 8.4% of the peak efficiency deficit at 1.5% span tip clearance. So, the PED could be small within a wide range of tip clearances if the matching of the compressor is perfect at design tip clearance.
引用
收藏
页数:12
相关论文
共 50 条
  • [21] The impact of forward swept rotors on tip clearance flows in subsonic axial compressors
    McNulty, GS
    Decker, JJ
    Beacher, BF
    Khalid, SA
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (04): : 445 - 454
  • [22] Interaction of tip clearance flow and three-dimensional separations in axial compressors
    Gbadebo, Semiu A.
    Cumpsty, Nicholas A.
    Hynes, Tom P.
    Proceedings of the ASME Turbo Expo 2006, Vol 6, Pts A and B, 2006, : 71 - 78
  • [23] IMPACT OF TIP CLEARANCE VARIATION OF HIGHLY LOADED TANDEM BLADES IN AXIAL COMPRESSORS
    Konrath, Liesbeth
    Peitsch, Dieter
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13A, 2023,
  • [24] Influence of tip clearance inclination on the performance of axial flow impeller in storage mode
    Zhu, Di
    Jin, Faye
    Hu, Zilong
    Luo, Yongyao
    Tao, Ran
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2023, 237 (04) : 831 - 842
  • [25] REVERSE FLOW IN MULTISTAGE AXIAL COMPRESSORS
    GAMACHE, RN
    GREITZER, EM
    JOURNAL OF PROPULSION AND POWER, 1990, 6 (04) : 461 - 473
  • [26] QUANTIFICATION OF THE NUMERICAL SOLUTION SENSITIVITY TO TIP CLEARANCE DIMENSIONS IN AN AXIAL MULTISTAGE COMPRESSOR
    Mouret, Gaelle
    Gourdain, Nicolas
    10TH EUROPEAN CONFERENCE ON TURBOMACHINERY: FLUID DYNAMICS AND THERMODYNAMICS, 2013,
  • [27] Dynamic Simulations of Post-stall Performance in Multistage Axial Compressors
    Olivier Léonard
    Journal of Thermal Science, 2012, 21 (04) : 311 - 321
  • [28] Dynamic simulations of post-stall performance in multistage axial compressors
    Wenhai Du
    JunQiang Zhu
    Olivier Léonard
    Journal of Thermal Science, 2012, 21 : 311 - 321
  • [29] Dynamic Simulations of Post-stall Performance in Multistage Axial Compressors
    Du Wenhai
    Zhu JunQiang
    Leonard, Olivier
    JOURNAL OF THERMAL SCIENCE, 2012, 21 (04) : 311 - 321
  • [30] MODELING FOR TIP CLEARANCE EFFECTS ON STALL-ONSET CONDITION IN TRANSONIC AXIAL COMPRESSORS
    Ye, Shubo
    Zhao, Qingjun
    Xiang, Xiaorong
    Xi, Guang
    Xu, Jianzhong
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2A, 2016,