Volume 40 Issue 5
May  2025
Turn off MathJax
Article Contents
YANG Fan, WU Yanhui, QIAN Kun, et al. Experiment on intermittent rotating instability based on wavelet transform analysis[J]. Journal of Aerospace Power, 2025, 40(5):20230576 doi: 10.13224/j.cnki.jasp.20230576
Citation: YANG Fan, WU Yanhui, QIAN Kun, et al. Experiment on intermittent rotating instability based on wavelet transform analysis[J]. Journal of Aerospace Power, 2025, 40(5):20230576 doi: 10.13224/j.cnki.jasp.20230576

Experiment on intermittent rotating instability based on wavelet transform analysis

doi: 10.13224/j.cnki.jasp.20230576
  • Received Date: 2023-09-08
    Available Online: 2024-06-29
  • A subsonic axial compressor isolated rotor test rig was taken as the research object to explore the time-frequency characteristics and physical nature of rotational instability (RI) through measurement of unsteady pressure at the blade tip region. Using the power spectrum estimation, the spatial distribution and frequency characteristics of RI were studied, indicating that the frequency characteristics and spatial distribution of RI did not change with the blade tip clearance size, rotating speed and mass flow rate. Using wavelet transform to study the time-frequency characteristics of RI, it was found that RI was not continuous in time. The increase of blade tip clearance would increase the occurrence frequency of RI. The time-frequency characteristics of RI were simulated by artificial signals, and the hypothesis that RI would only appear on specific blades was verified. The pressure field on the tip of the blade showed that the physical nature of RI was represented by a two-channel flow structure with alternating high and low loading formed by the tip leakage vortex breakdown.

     

  • loading
  • [1]
    VO H D. Role of tip clearance flow in rotating instabilities and nonsynchronous vibrations[J]. Journal of Propulsion and Power,2012,26(3): 556-561.
    [2]
    KAMEIER F,NEISE W. Rotating blade flow instability as a source of noise in axial turbomachines[J]. Journal of Sound and Vibration,1997,203(5): 833-853. doi: 10.1006/jsvi.1997.0902
    [3]
    VO H D,TAN C S,GREITZER E M. Criteria for spike initiated rotating stall[J]. Journal of Turbomachinery,2008,130(1): 011023.
    [4]
    MAILACH R,LEHMANN I,VOGELER K. Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex[J]. Journal of Turbomachinery,2001,123(3): 453-460. doi: 10.1115/1.1370160
    [5]
    MÄRZ J,HAH C,NEISE W. An experimental and numerical investigation into the mechanisms of rotating instability[J]. Journal of Turbomachinery,2002,124(3): 367-374. doi: 10.1115/1.1460915
    [6]
    CHEN Zhiyang,WU Yanhui,AN Guangyang. Tip leakage flow,tip aerodynamic loading and rotating instability in a subsonic high-speed axial flow compressor rotor[J]. Aerospace Science and Technology,2021,110:106486.
    [7]
    MAILACH R,SAUER H,VOGELER K. The periodical interaction of the tip clearance flow in the blade rows of axial compressors[R]. New Orleans,Louisiana,US: ASME Turbo Expo 2001 American Society of Mechanical Engineers,2001.
    [8]
    付磊,袁巍,宋西镇,等. 跨声速压气机转子叶尖流场旋转不稳定现象的数值研究[J]. 航空动力学报,2014,29(5): 1145-1153. FU Lei,YUAN Wei,SONG Xizhen,et al. Numerical investigation on rotating instability phenomenon in tip flow field of transonic compressor rotor[J]. Journal of Aerospace Power,2014,29(5): 1145-1153. (in Chinese

    FU Lei, YUAN Wei, SONG Xizhen, et al. Numerical investigation on rotating instability phenomenon in tip flow field of transonic compressor rotor[J]. Journal of Aerospace Power, 2014, 29(5): 1145-1153. (in Chinese)
    [9]
    付磊,宋西镇,袁巍,等. 跨声速压气机转子叶尖非定常流场数值研究[J]. 航空动力学报,2013,28(12): 2821-2828. FU Lei,SONG Xizhen,YUAN Wei,et al. Numerical investigations on unsteady flow field at tip region in transonic compressor rotor[J]. Journal of Aerospace Power,2013,28(12): 2821-2828. (in Chinese

    FU Lei, SONG Xizhen, YUAN Wei, et al. Numerical investigations on unsteady flow field at tip region in transonic compressor rotor[J]. Journal of Aerospace Power, 2013, 28(12): 2821-2828. (in Chinese)
    [10]
    王昊,吴亚东,欧阳华. 低速轴流压气机中气动旋转不稳定性和叶顶泄漏流脉动特性[J]. 航空动力学报,2016,31(9): 2239-2250. WANG Hao,WU Yadong,OUYANG Hua. Aerodynamic rotating instability and fluctuated characteristics of tip clearance flow in low speed axial flow compressor[J]. Journal of Aerospace Power,2016,31(9): 2239-2250. (in Chinese

    WANG Hao, WU Yadong, OUYANG Hua. Aerodynamic rotating instability and fluctuated characteristics of tip clearance flow in low speed axial flow compressor[J]. Journal of Aerospace Power, 2016, 31(9): 2239-2250. (in Chinese)
    [11]
    姚丹,田杰,欧阳华,等. 压气机旋转不稳定性的周向模态特性及其分解方法[J]. 航空动力学报,2018,33(2): 431-439. YAO Dan,TIAN Jie,OUYANG Hua,et al. Circumferential mode characteristic of rotating instability and its decomposition method of compressor[J]. Journal of Aerospace Power,2018,33(2): 431-439. (in Chinese

    YAO Dan, TIAN Jie, OUYANG Hua, et al. Circumferential mode characteristic of rotating instability and its decomposition method of compressor[J]. Journal of Aerospace Power, 2018, 33(2): 431-439. (in Chinese)
    [12]
    吴亚东,李涛,赖生智. POD和DMD方法分析不同间隙压气机旋转不稳定性特性[J]. 航空动力学报,2019,34(9): 2018-2026. WU Yadong,LI Tao,LAI Shengzhi. Analysis of rotating instability characteristics in compressor with different tipclearances by POD and DMD methods[J]. Journal of Aerospace Power,2019,34(9): 2018-2026. (in Chinese

    WU Yadong, LI Tao, LAI Shengzhi. Analysis of rotating instability characteristics in compressor with different tipclearances by POD and DMD methods[J]. Journal of Aerospace Power, 2019, 34(9): 2018-2026. (in Chinese)
    [13]
    YANG Zeyuan,WU Yadong,OUYANG Hua. Investigation on mode characteristics of rotating instability and rotating stall in an axial compressor[J]. Journal of Turbomachinery,2022,144(6): 061010. doi: 10.1115/1.4053238
    [14]
    YAMADA K,FUNAZAKI K,SASAKI H. Numerical investigation of relation between unsteady behavior of tip leakage vortex and rotating disturbance in a transonic axial compressor rotor[R]. ASME Paper GT2008-50779,2008.
    [15]
    WU Y,AN G,WANG B. Numerical investigation into the underlying mechanism connecting the vortex breakdown to the flow unsteadiness in a transonic compressor rotor[J]. Aerospace Science and Technology,2019,86: 106-118. doi: 10.1016/j.ast.2018.12.040
    [16]
    BRANDSTETTER C,SCHIFFER H P. PIV measurements of the transient flow structure in the tip region of a transonic compressor near stability limit[J]. Journal of the Global Power and Propulsion Society,2017,2(1): 303-316.
    [17]
    BIELA C,MÜLLER M,SCHIFFER H,et al. Unsteady pressure measurement in a single stage axial transonic compressor near the stability limit[R]. ASME Paper GT2008-50245,2008.
    [18]
    SCHRAPP H,STARK U,SAATHOFF H. Unsteady behaviour of the tip clearance vortex in a rotor equivalent compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy,2009,223(6):635-643.
    [19]
    SCHRAPP H,STARK U,SAATHOFF H. Unsteady behaviour of the tip clearance vortex in a rotor equivalent compressor cascade[J]. Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy,2009,223(6): 635-643. doi: 10.1243/09576509JPE816
    [20]
    WANG Bozhe,WU Yanhui,YANG Fan,et al. Intermittent breakdown of the tip leakage vortex and the resultant flow unsteadiness in the tip-region of a subsonic compressor cascade[J]. Aerospace Science and Technology,2021,113: 106679. doi: 10.1016/j.ast.2021.106679
    [21]
    SARPKAYA T. On stationary and travelling vortex breakdowns[J]. Journal of Fluid Mechanics,1971,45: 545-559. doi: 10.1017/S0022112071000181
    [22]
    SARPKAYA T. Vortex breakdown in swirling conical flows[J]. AIAA Journal,1971,9:1792-1799.
    [23]
    CASSIDY J J,FALVEY H T. Observations of un-steady flow arising after vortex breakdown[J]. Journal of Fluid Mechanics,1970,41: 727-736. doi: 10.1017/S0022112070000873
    [24]
    YANG F,WU Yanhui,ZHANG Z,et al. Periodic unsteadiness of tip clearance vortex in an axial compressor rotor[R]. ASME Paper GT2020-15167, 2020.
    [25]
    YANG Fan,WU Yanhui. The tip leakage vortex break-down and its possible relationship with rotating in-stability in a subsonic compressor rotor[R]. ASME Paper GT2021-58492,2021.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (422) PDF downloads(35) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return