Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (2): 130474.doi: 10.7527/S1000-6893.2024.30474
• Fluid Mechanics and Flight Mechanics • Previous Articles
Fei XUE, Yuqi QIN, Wendong LIU, Yangang WANG()
Received:
2024-04-02
Revised:
2024-04-26
Accepted:
2024-05-29
Online:
2024-06-06
Published:
2024-05-30
Contact:
Yangang WANG
E-mail:wyg704@nwpu.edu.cn
Supported by:
CLC Number:
Fei XUE, Yuqi QIN, Wendong LIU, Yangang WANG. Experiments on stall initial disturbance characteristics of contra-rotating compressor with distorted inflow[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(2): 130474.
Table 1
Stall disturbance characteristics of contra-rotating compressor under different inlet conditions
进气条件 | 失速类型 | 传播方向 | 传播速度 | 周向占据范围 |
---|---|---|---|---|
均匀进气 | 先沿周向传播随后固定 | 与前转子转向一致 | %1.25n1,%1.29n1 | 前转子135°,后转子135° |
周向120°畸变 | 先沿周向传播随后固定 | 与前转子转向一致 | %0.94n1,%0.90n1 | 前转子135°,后转子90° |
周向60°畸变 | 先沿周向传播随后固定 | 与前转子转向一致 | %0.94n1,%0.90n1 | 前转子135°,后转子135° |
周向60°畸变十均分 | 先沿周向传播随后固定 | 与前转子转向一致 | %1.04n1,%0.90n1 | 前转子90°,后转子90° |
Table 2
SMV results for different working conditions
参数 | 转速比1.00 (Uniform) | 转速比1.00 (Distortion) | 转速比1.40 (Uniform) | 转速比1.40 (Distortion) | 转速比1.52 (Uniform) | 转速比1.52 (Distortion) |
---|---|---|---|---|---|---|
设计点 | 0.375 6 | 0.375 6 | 0.250 4 | 0.250 4 | 0.250 4 | 0.250 4 |
设计点 | 0.700 5 | 0.733 3 | 0.913 4 | 0.879 6 | 0.803 2 | 0.831 7 |
失速点 | 0.206 6 | 0.195 4 | 0.197 6 | 0.190 9 | 0.189 2 | 0.190 9 |
失速点 | 1.294 4 | 1.287 7 | 1.024 7 | 1.013 0 | 0.962 6 | 0.973 0 |
SMV/% | 1.61 | 8.90 | 5.16 |
1 | STENNING A H, KRIEBEL A R. Stall propagation in a cascade of airfoils[J]. Journal of Fluids Engineering, 1958, 80(4): 777-789. |
2 | EMMONS H W, PEARSON C E, GRANT H P. Compressor surge and stall propagation[J]. Journal of Fluids Engineering, 1955, 77(4): 455-467. |
3 | MOORE F K, GREITZER E M. A theory of post-stall transients in axial compression systems: Part I—development of equations[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(1): 68-76. |
4 | GREITZER E M, MOORE F K. A theory of post-stall transients in axial compression systems: Part II—application[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(2): 231-239. |
5 | MCDOUGALL N M, CUMPSTY N A, HYNES T P. Stall inception in axial compressors[J]. Journal of Turbomachinery, 1990, 112(1): 116-123. |
6 | DAY I J. Stall inception in axial flow compressors[J]. Journal of Turbomachinery, 1993, 115(1): 1-9. |
7 | CAMP T R, DAY I J. A study of spike and modal stall phenomena in a low-speed axial compressor[J]. Journal of Turbomachinery, 1997, 120(3): 393-401. |
8 | DAY I J, BREUER T, ESCURET J, et al. Stall inception and the prospects for active control in four high-speed compressors[J]. Journal of Turbomachinery, 1999, 121(1): 18-27. |
9 | LI J C, DU J, GENG S J, et al. Tip air injection to extend stall margin of multi-stage axial flow compressor with inlet radial distortion[J]. Aerospace Science and Technology, 2020, 96: 105554. |
10 | LI J C, DU J, LIU Y, et al. Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor[J]. Aerospace Science and Technology, 2020, 105: 105886. |
11 | LONGLEY J P, SHIN H W, PLUMLEY R E, et al. Effects of rotating inlet distortion on multisage compressor stability[C]∥Proceedings of ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition, 2015. |
12 | 李佳, 孙大坤, 董旭, 等. 旋转进气畸变下的两级压气机扩稳试验研究[J]. 工程热物理学报, 2020, 41(6): 425-1433. |
LI J, SUN D K, DONG X, et al. Experimental research on stabilization of two-stage compressor under rotating inlet distortion[J]. Journal of Engineering Thermophysics, 2020, 41(6): 1425-1433 (in Chinese). | |
13 | QIU J H, DU J, FAN Z G, et al. Effects of rotating inlet distortion on the stall mechanism of an axial flow compressor[J]. Physics of Fluids, 2023, 35 (11): 114105. |
14 | RAO P S. Development and testing of contra-rotating axial flow fan[D]. Bombay: Indian Institute of Technology, 1988. |
15 | SHARMA P B, JAIN Y P, JHA N K, et al. Stalling behavior of a contra-rotating axial compressor stage[C]∥ International Symposium on Air Breathing Engines. 1985: 734-740. |
16 | SHARMA P B, PUNDIR D S. A study of flow structure in a contra-rotating axial compressor stage[C]∥International Symposium on Air Breathing Engines. 1989: 237-244. |
17 | 高丽敏, 苗芳, 李晓军, 等. 对转压气机转速比对最先失速级的影响[J]. 应用力学学报, 2013, 30(6): 845-848. |
GAO L M, MIAO F, LI X J, et al. Effect of rotating speed ratio of counter-rotating compressor on the first stall stage[J]. Chinese Journal of Applied Mechanics, 2013, 30(6): 845-848 (in Chinese). | |
18 | 高丽敏, 李晓军, 冯旭栋, 等. 对转压气机转速比变化对稳定边界的影响[J]. 推进技术, 2012, 33(6): 881-887. |
GAO L M, LI X J, FENG X D, et al. Effects of rotational speed ratio on stability boundary of contra-rotating compressor[J]. Journal of Propulsion Technology, 2012, 33(6): 881-887 (in Chinese). | |
19 | GAO L M, LI R Y, MIAO F, et al. Unsteady investigation on tip flow field and rotating stall in counter-rotating axial compressor[J]. Journal of Engineering for Gas Turbines and Power, 2015, 137(7): 072603. |
20 | 王昊, 薛飞, 岳少原, 等. 对转压气机变转速比失速特性试验研究[J]. 西北工业大学学报, 2021, 39(6): 1340-1348. |
WANG H, XUE F, YUE S Y, et al. Experimental investigation on stall characteristics of contra-rotating compressor with variable speed ratios[J]. Journal of Northwestern Polytechnical University, 2021, 39(6): 1340-1348 (in Chinese). | |
21 | 王昊, 薛飞, 岳少原, 等. 对转压气机变转速比失速类型试验[J]. 航空学报, 2022, 43(7): 125596. |
WANG H, XUE F, YUE S Y, et al. Test on stall types of contra-rotating compressor with variable speed ratios[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(7): 125596 (in Chinese). | |
22 | MANAS M P, PRADEEP A M. Stall inception mechanisms in a contra-rotating fan operating at different speed combinations[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2020, 234(8): 1041-1052. |
23 | MADASSERI P M, PRADEEP A M. Pre-stall waves: precursors to stall inception in a contra-rotating axial fan[C]∥Proceedings of ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. 2021. |
24 | SHARMA P B, JAIN Y P, PUNDHIR D S. A study of some factors affecting the performance of a contra-rotating axial compressor stage[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Power and Process Engineering, 1988, 202(1): 15-21. |
25 | MANAS M P, PRADEEP A M. Influence of distorted inflows on the performance of a contra-rotating fan[J]. The Aeronautical Journal, 2021, 125(1286): 702-719. |
26 | MANAS M P, PRADEEP A M. Stall inception in a contra-rotating fan under radially distorted inflows[J]. Aerospace Science and Technology, 2020, 105: 105909. |
27 | MILESHIN V, BRAILKO I, STEPANOV A, et al. Numerical and experimental investigations of steady and unsteady characteristics of a counter rotating fan model with thickened blades of working wheel[C]∥Proceedings of ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 2013: 491-500. |
28 | YUE S Y, WANG Y G, WEI L G, et al. Experimental investigation on the development process of large-scale low-speed stall disturbance in contra-rotating compressor[J]. Journal of Thermal Science, 2020, 29(5): 1282-1291. |
29 | HUANG S, HAN G, YANG C W. Experimental research on flow instability mechanism of a highly loaded axial compressor[J]. Journal of Engineering for Gas Turbines and Power, 2023, 145(9): 091006. |
30 | CHEN W X, WANG Y G, WANG H. Investigation of the unsteady disturbance in tip region of a contra-rotating compressor near stall[J]. Journal of Thermal Science, 2019, 28(5): 962-974. |
31 | DU J, LU Y, LL J C, et al. Adaptive feedback control of stability in an axial compressor with circumferential inlet distortion[J]. Chinese Joumal of Aeronautics, 2023, 36(5): 187-201. |
32 | SUN D K, XU R Z, DONG X, et al. Aeroengine stall warning by multicorrelation analysis[J]. Journal of Propulsion and Power, 2023, 40(1): 138-151. |
33 | HEWKIN-SMITH M, PULLAN G, GRIMSHAW S D, et al. The role of tip leakage flow in spike-type rotating stall inception[J]. Journal of Turbomachinery, 2019, 141(6): 061010. |
34 | YUE S Y, WANG Y G, WEI L G, et al. The joint empirical mode decomposition-local mean decomposition method and its application to time series of compressor stall process[J]. Aerospace Science and Technology, 2020, 105: 1059. |
[1] | Junyang YU, Wenguang FU, Peng SUN, Tao ZHANG, Chunxue WANG, Wei ZHAO. Design and stabilization mechanism of non-axisymmetric fans under inlet distortion conditions [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(16): 129725-129725. |
[2] | WANG Hao, XUE Fei, YUE Shaoyuan, WANG Yangang. Test on stall types of contra-rotating compressor with variable speed ratios [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 125596-125596. |
[3] | LI Zhiping, WANG Mengqi. Airworthiness certification method for aeroengine on stall and surge with inlet distortion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 2947-2957. |
[4] | AN Yuge, LIU Huoxing. Numerical Simulation of Compressor with Inlet Distortion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(9): 1624-1632. |
[5] | Zheng Qing-xiong;Lian Xiao-chun;Chen fu-qun;Shen Shao-ying. INFLUENCE OF INLET DISTORTION ON THE PERFORMANCE OF TWIN-SPOOL TURBOJET ENGINES [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(10): 529-531. |
[6] | Lin Qi-xun;Chen Fu-qun;Zhang Dong;Fang Xin;Gao Zhong-bo;Xian Ning-fang. THE EXPERIMENTAL INVESTIGATION OF THE INLET DISTORTION SIMULATION EQUIPMENT [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(2): 89-93. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341