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
  • [1] ROTATING STALL CELLS IN A LOW-SPEED AXIAL-FLOW COMPRESSOR
    BREUGELMANS, FAE
    MATHIOUDAKIS, K
    CASALINI, F
    JOURNAL OF AIRCRAFT, 1985, 22 (03): : 175 - 181
  • [2] Analysis of Tonal Noise Generating Mechanisms in Low-Speed Axial-Flow Fans
    Canepa, Edward
    Cattanei, Andrea
    Zecchin, Fabio Mazzocut
    JOURNAL OF THERMAL SCIENCE, 2016, 25 (04) : 302 - 311
  • [3] Analysis of Tonal Noise Generating Mechanisms in Low-Speed Axial-Flow Fans
    Edward Canepa
    Andrea Cattanei
    Fabio Mazzocut Zecchin
    Journal of Thermal Science, 2016, 25 (04) : 302 - 311
  • [4] Analysis of tonal noise generating mechanisms in low-speed axial-flow fans
    Edward Canepa
    Andrea Cattanei
    Fabio Mazzocut Zecchin
    Journal of Thermal Science, 2016, 25 : 302 - 311
  • [5] Design and Experimental Validation of a Ducted Counter-Rotating Axial-Flow Fans System
    Nouri, H.
    Ravelet, F.
    Bakir, F.
    Sarraf, C.
    Rey, R.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2012, 134 (10):
  • [6] UNSTEADY LOSS IN A LOW-SPEED AXIAL-FLOW COMPRESSOR DURING ROTATING STALL
    BREUGELMANS, FAE
    HUANG, L
    LAROSILIERE, L
    ANDREW, P
    NINTH INTERNATIONAL SYMPOSIUM ON AIR BREATHING ENGINES, VOLS 1 AND 2: SYMPOSIUM PAPERS, 1989, : 262 - 270
  • [7] Instantaneous PIV data related to the leakage flow of a low-speed axial-flow fan with rotating shroud
    Canepa, Edward
    Cattanei, Andrea
    Zecchin, Fabio Mazzocut
    Parodi, Davide
    DATA IN BRIEF, 2019, 24
  • [8] DESIGN AND OPERATION OF AXIAL-FLOW FANS
    OLESEN, P
    COMBUSTION, 1977, 49 (01): : 26 - 28
  • [9] VORTEX SHEDDING NOISE OF LOW TIP SPEED, AXIAL-FLOW FANS
    LONGHOUSE, RE
    JOURNAL OF SOUND AND VIBRATION, 1977, 53 (01) : 25 - 46
  • [10] NOISE MECHANISM SEPARATION AND DESIGN CONSIDERATIONS FOR LOW TIP-SPEED, AXIAL-FLOW FANS
    LONGHOUSE, RE
    JOURNAL OF SOUND AND VIBRATION, 1976, 48 (04) : 461 - 474