Journal of Shanghai Jiaotong University >
Numerical Simulation of Compressor Stall Recovery Control
Received date: 2020-08-14
Online published: 2021-12-03
In order to explore the influencing factors of the effectiveness and stability for stall recovery and its flow mechanism when the antisurge valve is opened quickly, the dynamic stall recovery processes are simulated and the recovery processes at different discharging speeds are emphatically compared. Two numerical simulation methods, i.e., the distributed speed-changeable MG (Moore-Greitzer) model and the RANS (Reynolds Averaged Navier-Stokes) equation are used. The performance curves predicated by the two models agree well. The results of RANS show that the flow field changes are essentially the same when the valve is opened at different speeds. The disturbance, affected by the high-speed air flow generated at the inlet, moves downstream and finally reaches the leading edge of the rotor, whose scale will be further reduced with the impact of axial high-speed flow until completely dissipated. A comparison of different valve opening speeds indicates that the faster the valve is opened, the stronger the high-speed air flow generated at the inlet, shortening the stall recovery time. The greater the disturbance weakening degree, the faster the circumferential propagation speed of the disturbance, and the closer to the rotor speed. In the process of valve opening, the air flow fluctuation is more intense, and more energy is lost.
GAO Yuan, WU Yadong, OUYANG Hua . Numerical Simulation of Compressor Stall Recovery Control[J]. Journal of Shanghai Jiaotong University, 2021 , 55(11) : 1343 -1351 . DOI: 10.16183/j.cnki.jsjtu.2020.261
[1] | 桂幸民, 滕金芳, 刘宝杰. 航空压气机气动热力学理论与应用[M]. 上海: 上海交通大学出版社, 2014. |
[1] | GUI Xingmin, TENG Jinfang, LIU Baojie. Compressor aerothermodynamics and its applications in aircraft engines[M]. Shanghai: Shanghai Jiao Tong University Press, 2014. |
[2] | 吴艳辉. 轴流压缩系统过失速性能及失速可恢复性的研究[D]. 西安: 西北工业大学, 2001. |
[2] | WU Yanhui. A study on post-stall behavior recoverability in axial-flow compression system[D]. Xi’an: Northwestern Polytechnical University, 2001. |
[3] | 马彩东, 李应红, 吴云, 等. 转子叶尖端壁失速特性试验研究[J]. 推进技术, 2015, 36(5):722-728. |
[3] | MA Caidong, LI Yinghong, WU Yun, et al. Experimental investigation on stall characteristics on rotor tip end-wall[J]. Journal of Propulsion Technology, 2015, 36(5):722-728. |
[4] | HICKMAN, ADAM R. The transition from rotating stall to surge in an axial compressor[D]. Notre Dame: University of Notre Dame, 2017. |
[5] | 李志平, 张鹏, 李秋实. 低速轴流压气机旋转失速边界的模型描述[J]. 航空动力学报, 2017, 32(3):519-527. |
[5] | LI Zhiping, ZHANG Peng, LI Qiushi. Model description of rotating stall boundary in low-speed axial compressor[J]. Journal of Aerospace Power, 2017, 32(3):519-527. |
[6] | 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. |
[7] | MANSOUX C A, GYDLING D L, SETIAWAN J D, et al. Distributed nonlinear modeling and stability analysis of axial compressor stall and surge[C]// American Control Conference. Baltimore, MD, USA: IEEE, 1994: 2305-2316. |
[8] | GRAVDAHL J T, EGELAND O. A Moore-Greitzer axial compressor model with spool dynamics[C]// Proceedings of the 36th IEEE Conference on Decision and Control. San Diego, CA, USA: IEEE, 1998: 4714-4719. |
[9] | SARI G, AKHRIF O, SAYDY L. Qualitative analysis of an axial compressor model with non-constant speed[C]// ASME 2011 Power Conference collocated with JSME ICOPE 2011. Denver, Colorado, USA: ASME, 2011: 515-524. |
[10] | 苏三买, 孙占恒, 吕烨, 等. 压气机失速与喘振动态模型与仿真[J]. 推进技术, 2016, 37(5):960-965. |
[10] | SU Sanmai, SUN Zhanheng, LÜ Ye, et al. Dynamic model and simulation of compressor rotating stall and surge[J]. Journal of Propulsion Technology, 2016, 37(5):960-965. |
[11] | 陈亚新, 苏三买. 可变转速工况的压气机分布式动态模型与仿真[J]. 推进技术, 2020, 41(3):675-684. |
[11] | CHEN Yaxin, SU Sanmai. Compressor distributed dynamic model and simulation under non-constant speed[J]. Journal of Propulsion Technology, 2020, 41(3):675-684. |
[12] | LIN P, WANG C, WANG Y. A high-order model of rotating stall in axial compressors with inlet distortion[J]. Chinese Journal of Aeronautics, 2017, 30(3):898-906. |
[13] | HOS C. Bifurcation analysis of surge and rotating stall in the Moore-Greitzer compression system[J]. IMA Journal of Applied Mathematics, 2003, 68(2):205-228. |
[14] | 王聪, 文彬鹤, 司文杰, 等. 轴流压气机旋转失速建模与检测: I——基于确定学习理论与高阶Moore-Greitzer 模型的研究[J]. 自动化学报, 2014, 40(7):1265-1277. |
[14] | WANG Cong, WEN Binhe, SI Wenjie, et al. Modeling and detection of rotating stall in axial flow compressors: Part I. Investigation on high-order M-G models via deterministic learning[J]. Acta Automatica Sinica, 2014, 40(7):1265-1277. |
[15] | 王聪, 司文杰, 文彬鹤, 等. 轴流压气机旋转失速建模与检测Ⅱ: 基于北航低速压气机试验台的实验研究[J]. 控制理论与应用, 2014, 31(10):1414-1422. |
[15] | WANG Cong, SI Wenjie, WEN Binhe, et al. Modeling and detection of rotating stall in axial flow compressors, Ⅱ: Experimental study for a low-speed compressor in Beihang University[J]. Control Theory & Applications, 2014, 31(10):1414-1422. |
/
〈 |
|
〉 |