NUMERICAL STUDY OF THE EFFECT OF HONEYCOMB TIP ON TIP LEAKAGE FLOW IN TURBINE CASCADE

被引:0
作者
Fu, Yunfeng [1 ]
Chen, Fu [1 ]
Chen, Cong [1 ]
Song, Yanping [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2B | 2016年
关键词
SQUEALER TIP; GEOMETRIES;
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
A novel leakage flow control strategy with honeycomb seal applied on the tip of the rotor blades in a highly-loaded turbine cascade is proposed. The numerical method is used to study the tip leakage flow in a highly-loaded turbine cascades with flat tip and with honeycomb seal structure, the mechanism of honeycomb tip on inhibiting leakage flow is analyzed, the influence of various relative gap heights is also been investigated The discussions of the action of the honeycomb-tip structure in reducing leakage flow and improving the turbine efficiency provide the according for control methods of tip leakage flow. Through the comparative study among three different tip structures of honeycomb tip, honeycomb casing and flat tip, the results show. that both honeycomb tip and honeycomb casing inhibit the leakage flow effectively, but honeycomb tip has positive effect on reducing the flow loss in cascade. For the cascade with honeycomb tip, on one hand, the vortices rolled up in the regular hexagon honeycomb cavities dissipate the energy of the tip leakage flow, and the range of influence of the vortices is nearly one third of the tip clearance height. On the other hand, the radial jets caused by the honeycomb obstruct the tip leakage flow like a "pneumatic fence", resulting in weaker leakage flow and less leakage flow rate. Besides, the honeycomb tip reduces the scale of the leakage vortex, thus the leakage loss also decreases. Compared with the flat tip cascade at the clearance height of 1%H, the honeycomb tip cascade with the same clearance height obtains decrease of the leakage flow rate and leakage flow speed in circumference by 10.16% and 20%. As a result, the leakage vortex in honeycomb tip cascade is undermined, the loss is reduced by nearly 4.43%. Considering the abradable property of the honeycomb seal that can protect the blade tips from damage, the cascade with honeycomb tip structure can obtain a smaller clearance height and achieve better sealing effect. Compared to cascade with the flat tip at the clearance height of 2%H, the amount of leakage flow using inlet flow in the honeycomb tip cascades decreases by 17.33%, 36.63% and 54.79% at the clearance heights of 2%H, 1.5%H and 1%H, the losses related to the leakage flow is reduced by nearly 5.71%, 14.33% and 25.24%, respectively.
引用
收藏
页数:10
相关论文
共 50 条
  • [41] Effect of multiple cavities and tip injection on the aerothermal characteristics of the squealer tip in turbine stage
    Bi, Shuai
    Mao, Junkui
    Chen, Pingting
    Han, Feng
    Wang, Lei
    APPLIED THERMAL ENGINEERING, 2023, 220
  • [42] Effect of in-service burnout on the transonic tip leakage flows over flat tip model
    Saleh, Zainab
    Avital, Eldad J.
    Korakianitis, Theodosios
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2020, 234 (05) : 655 - 669
  • [43] Numerical Investigations on the Steady and Unsteady Leakage Flow and Heat Transfer Characteristics of Rotor Blade Squealer Tip
    Li, Jun
    Sun, Hao
    Wang, Jinshan
    Feng, Zhenping
    JOURNAL OF THERMAL SCIENCE, 2011, 20 (04) : 304 - 311
  • [44] Numerical investigations on the steady and unsteady leakage flow and heat transfer characteristics of rotor blade squealer tip
    Jun Li
    Hao Sun
    Jinshan Wang
    Zhenping Feng
    Journal of Thermal Science, 2011, 20 : 304 - 311
  • [46] AN EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF GROOVED TIP GEOMETRY ON THE FLOW FIELD IN A TURBINE CASCADE PASSAGE USING STEREOSCOPIC PIV
    Tian, Yangtao
    Ma, Hongwei
    Wang, Lixiang
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2A, 2017,
  • [47] Effects of inclined squealer rims on tip leakage vortex and loss in a transonic axial turbine
    Wang, Yufan
    Zhang, Weihao
    Mu, Yumo
    Jiang, Shoumin
    Chen, Yun
    Ma, Guangjian
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2023, 237 (02) : 236 - 250
  • [48] EFFECT OF COOLANT FLOWRATE ON HIGH-PRESSURE TURBINE TIP FLOW STRUCTURES AND THERMAL LOADING
    Christensen, Louis
    Celestina, Richard
    Sperling, Spencer
    Mathison, Randall
    Aksoy, Hakan
    Liu, Jong
    Nickol, Jeremy
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 7A, 2023,
  • [49] Numerical investigation of blade tip grooving effect on performance and dynamics of an axial flow fan
    Ye, Xuemin
    Li, Pengmin
    Li, Chunxi
    Ding, Xueliang
    ENERGY, 2015, 82 : 556 - 569
  • [50] Film cooling effects on the tip flow characteristics of a gas turbine blade
    Wang, Jin
    Sunden, Bengt
    Zeng, Min
    Wang, Qiuwang
    PROPULSION AND POWER RESEARCH, 2015, 4 (01) : 9 - 22