EFFICIENCY INCREASE IN CENTRIFUGAL COMPRESSOR WITH OPEN IMPELLER BY USING CURVILINEAR ELEMENT BLADE

被引:0
|
作者
Tsukamoto, Kazuhiro [1 ]
Hiradate, Kiyotaka [1 ]
Sakamoto, Kiyohide [1 ]
Chiba, Haruaki [2 ]
Shinkawa, Yasushi [2 ]
机构
[1] Hitachi Ltd, Hitachi Res Lab, 832-2 Horiguchi, Hitachinaka, Ibaraki, Japan
[2] Hitachi Ltd, Infrastruct Co, Tsuchiura, Ibaraki, Japan
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
The effect of curvilinear element blade on open-type centrifugal impeller is numerically examined in this research. We compared four different open-type centrifugal impellers. Two of them were linear element blade impellers: one has a positive tangential lean to the rotation at the outlet and the other has negative tangential lean. The other two were curvilinear element blade impellers having different tangential lean profiles. Numerical simulation of steady flow was conducted in one-blade path model with inlet, impeller and vane-less diffuser regions. The simulation confirm that impellers with negative tangential lean profiles improve the stage efficiency under the flow rate at the design point and the curvilinear element blade improve the stage efficiency not only at the design point but the lower flow rate regions also. The efficiency increase at the design point is obtained not in the vane-less diffuser region but in the impeller region since the negative lean profile reduce the tip-leakage loss near the impeller outlet region. The negative tangential lean profile changes the pressure distribution in the flow passage between two impeller blades. The pressure difference between the pressure surface and the suction surface of one blade near the tip region decrease because of the pressure distribution change. Hence, the mass flow rate of the tip leakage decreases and reduces the loss generation. In addition, the reason why the stage efficiency increases under the lower flow rate conditions by using curvilinear element blade is the suppression effect of the flow separation in the vane-less diffuser. This result indicates that there is a design criteria both tangential lean angle and the inflection point of the profile from positive to negative to suppress the flow separation at the hub side in the vane-less diffuser.
引用
收藏
页数:9
相关论文
共 50 条
  • [41] Optimization of a centrifugal compressor impeller using CFD: the choice of simulation model parameters
    Neverov, V. V.
    Kozhukhov, Y. V.
    Yablokov, A. M.
    Lebedev, A. A.
    10TH INTERNATIONAL CONFERENCE ON COMPRESSORS AND THEIR SYSTEMS, 2017, 232
  • [42] Radial pressure distribution in lateral clearances of the semi-open axiradial impeller of the centrifugal compressor
    Evgen'Ev S.S.
    Futin V.A.
    Zubrinkin A.V.
    Russian Aeronautics (Iz VUZ), 2012, 55 (3) : 269 - 275
  • [43] AERODYNAMIC OPTIMIZATION OF A TRANSONIC CENTRIFUGAL COMPRESSOR BY USING ARBITRARY BLADE SURFACES
    Hehn, Alexander
    Mosdzien, Moritz
    Grates, Daniel
    Jeschke, Peter
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2C, 2017,
  • [44] Aerodynamic Optimization of a Transonic Centrifugal Compressor by Using Arbitrary Blade Surfaces
    Hehn, Alexander
    Mosdzien, Moritz
    Grates, Daniel
    Jeschke, Peter
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 140 (05):
  • [45] EXPERIMENTAL AND NUMERICAL INVESTIGATION OF VANED HUB AND SHROUD WALL CONTOURED DIFFUSERS DESIGNED TO IMPROVE FLEXIBILITY AND EFFICIENCY OF AN OPEN IMPELLER CENTRIFUGAL COMPRESSOR STAGE
    Hermann, Daniel
    Wirsum, Manfred
    Robinson, Douglas
    Jenny, Philipp
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2D, 2021,
  • [46] Effects of Structural and Technological Factors on the Fatigue Life of the Centrifugal Compressor Impeller Blade-Disk Joint: Experimental Evaluation
    Tsybanyov, G. V.
    Nalimov, Yu. S.
    Kononuchenko, O. V.
    STRENGTH OF MATERIALS, 2024, 56 (06) : 1159 - 1166
  • [47] Study on methods of numerical simulation of transient flow in the semi-open impeller stage of a centrifugal compressor
    Xie, Rong
    Hao, Muting
    Guan, Liang
    Miao, Weidong
    Shi, Yanjun
    Energy Education Science and Technology Part A: Energy Science and Research, 2014, 32 (02): : 1085 - 1092
  • [48] PERFORMANCE IMPROVEMENT OF A CENTRIFUGAL COMPRESSOR STAGE BY INCREASING DEGREE OF REACTION AND OPTIMIZING BLADE LOADING OF A 3D-IMPELLER
    Shibata, Takanori
    Yagi, Manabu
    Nishida, Hideo
    Kobayashi, Hiromi
    Tanaka, Masanori
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 1305 - 1315
  • [49] Performance Improvement of a Centrifugal Compressor Stage by Increasing Degree of Reaction and Optimizing Blade Loading of a 3D Impeller
    Shibata, Takanori
    Yagi, Manabu
    Nishida, Hideo
    Kobayashi, Hiromi
    Tanaka, Masanori
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2011, 133 (02):
  • [50] DESIGN OPTIMIZATION OF A CENTRIFUGAL COMPRESSOR IMPELLER USING RADIAL BASIS NEURAL NETWORK METHOD
    Kim, Jin-Hyuk
    Choi, Jae-Ho
    Kim, Kwang-Yong
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 443 - 451