INFLUENCE OF DESIGN PARAMETERS ON THE GLOBAL PERFORMANCES OF LOW-SPEED COUNTER -ROTATING AXIAL-FLOW FANS

被引:0
|
作者
Wang, Juan [1 ]
Ravelet, Florent [1 ]
Bakir, Farid [1 ]
机构
[1] Arts & Metiers ParisTech, Dynfluid Lab, Paris, France
关键词
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 present work aims at experimentally investigating the effects of some parameters on the performances of a counter rotating stage, and on the instationary flow between the rotors. Three counter-rotating fans, which have the same design point, have been designed. These systems differ by the distribution of the loading and of the ratio of angular velocity between the front rotor and the rear rotor. All the configurations have been tested in a normalized test rig, where the ratio of angular velocities and the axial distance between the two rotors can be varied. The influence of these parameters are then addressed by analysing the experimental results of the static pressure rise and static efficiency, as well as of the wall pressure fluctuations registered by a microphone at the wall. The three systems achieve the design point with a high efficiency. The counter-rotating systems lead to at least a 10 percentage points gain in static efficiency at the design flow rate, compared to the typical peak efficiency of a traditional rotor-stator stage. Meanwhile, counter-rotating systems display good working stabilities at very low volume flow rates. In addition, at the design speed ratio, the overall performance decreases almost monotonically with the axial distance. Nevertheless, an optimum in axial distance can be found for higher speed ratios. Finally, the investigations of the wall pressure fluctuations show that the amplitudes of power spectral density corresponding to the blade passing frequency of the rear rotor are significantly higher than that of the front rotor. The interaction peaks are also stronger for an equal distribution of the work on the two rotors.
引用
收藏
页数:9
相关论文
共 50 条
  • [41] Investigations of rotating instability and fluctuating tip clearance flow in a low-speed axial compressor
    Wang, Hao
    Wu, Yadong
    Ouyang, Hua
    Tian, Jie
    Du, Zhaohui
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (06) : 981 - 994
  • [42] OPTIMUM DESIGN OF AXIAL-FLOW FANS WITH CAMBERED BLADES OF CONSTANT THICKNESS
    BLAHO, M
    PERIODICA POLYTECHNICA-MECHANICAL ENGINEERING, 1975, 19 (02): : 79 - 89
  • [43] DESIGN AND APPLICATION OF HIGH-PRESSURE COEFFICIENT AXIAL-FLOW FANS
    SAWYER, JG
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1945, 12 (03): : 281 - 284
  • [44] NUMERICAL AND EXPERIMENTAL ANALYSES FOR THE AERODYNAMIC DESIGN OF HIGH PERFORMANCE COUNTER-ROTATING AXIAL FLOW FANS
    Cho, Leesang
    Choi, Hyunmin
    Lee, Seawook
    Cho, Jinsoo
    FEDSM2009, VOL 2, 2009, : 231 - 244
  • [45] Beamforming based extension of semi-empirical noise modelling for low-speed axial flow fans
    Benedek, Tamas
    Vad, Janos
    APPLIED ACOUSTICS, 2021, 178
  • [46] ACTIVE CONTROL OF ROTATING STALL IN A LOW-SPEED AXIAL COMPRESSOR
    PADUANO, JD
    EPSTEIN, AH
    VALAVANI, L
    LONGLEY, JP
    GREITZER, EM
    GUENETTE, GR
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (01): : 48 - 56
  • [47] Effect of Circumferential Casing Treatment on Low-Speed Contra-Rotating Fans
    Heinrich, M.
    Khaleghi, H.
    Friebe, C.
    JOURNAL OF APPLIED FLUID MECHANICS, 2020, 13 (06) : 1719 - 1726
  • [48] A turbomachinery design tool for teaching design concepts for axial-flow fans, compressors, and turbines
    Turner, Mark G.
    Merchant, Ali
    Bruna, Dario
    PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 1, 2006, : 937 - 952
  • [49] Influence of deterministic stresses on flow prediction of a low-speed axial flow compressor rear stage
    Li, YG
    Tourlidakis, A
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2001, 215 (A5) : 571 - 583
  • [50] Pressure oscillations in a single stage axial-flow low-speed compressor during pre-stall and stall
    Levy, Y.
    Pismenny, J.
    Deppe, A.
    Saathoff, H.
    Schrapp, H.
    Stark, U.
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2007, 24 (01) : 29 - 50