带有蜗壳的离心压气机进口失速先兆位置的确定及其成因分析

推进技术 ›› 2017, Vol. 38 ›› Issue (4): 787-796.

带有蜗壳的离心压气机进口失速先兆位置的确定及其成因分析

杨策¹,王营军¹,佟鼎²,杨长茂¹,李延昭³

北京理工大学机械与车辆学院，北京 100081,北京理工大学机械与车辆学院，北京 100081,中国北方发动机研究所，天津 300405,北京理工大学机械与车辆学院，北京 100081,山东康跃股份有限公司，山东潍坊 262718

发布日期:2021-08-15
作者简介:杨策，博士，教授，研究领域为叶轮机械气动热力学。
基金资助:
国家自然科学基金(51376024)。

Certainty and Interpretation of Inlet Stall Inception Position Caused By Volute Tongue in a Centrifugal Compressor

School of Mechanical Engineering，Beijing Institute of Technology，Beijing 100081，China,School of Mechanical Engineering，Beijing Institute of Technology，Beijing 100081，China,China North Engine Research Institute，Tianjin 300405，China,School of Mechanical Engineering，Beijing Institute of Technology，Beijing 100081，China and Kangyue Technology Co.Ltd，Weifang 262718，China

Published:2021-08-15

摘要/Abstract

摘要： 为了确定离心压气机失速先兆形成的原因，分析蜗舌与失速先兆位置的关系，采用数值计算方法对高速小流量离心压气机失速先兆特征进行了研究。计算结果表明:失速过程中流场结构的变化说明了离心压气机出现的是脉冲波失速先兆，离心压气机失速先兆现象由蜗舌对气流的阻滞作用诱发，蜗壳内部流场在周向55°附近区域出现高静压区域，高静压区域形成的扰动通过前倾后弯的叶轮通道逆向传播至叶轮进口，从而在进口周向115°附近出现失速先兆。

关键词: 离心压气机；叶尖间隙流；蜗舌；静压畸变；失速先兆

Abstract: To determine the formation reason for the stall inception in a centrifugal compressor and analyze the relationship between the volute tongue and the stall inception position，the stall characteristics of a high-speed and small-flow centrifugal compressor was numerically investigated. The results indicate that the spike-type stall in this centrifugal compressor occurs as the flow structure changes during stall process. The stall inception is induced by the volute tongue blocking effect which results in the high pressure area at about 55° circumferential position of the volute. The pressure disturbance-wave adversely propagates to the impeller inlet through the forward inclined and backward swept passage，and the spike-type stall appears at about 115° circumferential position.

Key words: Centrifugal compressor；Tip clearance flow；Volute tongue；Static pressure distortion；Stall inception

杨策,王营军,佟鼎,杨长茂,李延昭. 带有蜗壳的离心压气机进口失速先兆位置的确定及其成因分析[J]. 推进技术, 2017, 38(4): 787-796.

YANG Ce¹,WANG Ying-jun¹,TONG Ding²,YANG Chang-mao¹,LI Yan-zhao³. Certainty and Interpretation of Inlet Stall Inception Position Caused By Volute Tongue in a Centrifugal Compressor[J]. Journal of Propulsion Technology, 2017, 38(4): 787-796.

参考文献

[1] Mcdougal N M, Cumpsty N A, Hynes T P. Stall Inception in Axial Compressors[J]. Journal of Turbomachinery, 1990, 112(1): 116-125.
[2] Carnier V H, Epstein A H, Greitzer E M. Rotating Waves as a Stall Indication in Axial Compressors[J]. Journal of Turbomachinery, 1991, 115(3): 290-302.
[3] Day I J. Stall Inception in Axial Flow Compressor[J]. Journal of Turbomachinery, 1993, 115(1): 1-9.
[4] 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 Turbomachniery, 1999, 121(1): 18-27.
[5] Camp T R, Day I J. A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor[J]. Journal of Turbomachinery, 1998, 120(3): 393-401.
[6] Chen J P, Hathaway M D, Herrick G P. Prestall Behavior of a Transonic Axial Compressor Stage via Time-Accurate Numerical Simulation[J]. Journal of Turbomachniery, 2008, 130(4): 353-368.
[7] Inoue M, Kuroumaru M, Yoshida S, et al. Short and Long Length-Scale Disturbances Leading to Rotating Stall in an Axial Compressor Stage with Different Stator/Rotor Gaps[J]. Journal of Turbomachniery, 2002, 124(3): 376-384.
[8] 耿少娟, 张小玉, 聂超群, 等. 轴流压气机叶顶端区流场周向传播特征及其预测[J]. 机械工程学报, 2012, 48(16): 130-138.
[9] 吴艳辉, 吴俊峰, 稂仿玉, 等. 轴流压气机转子近叶尖流动的试验和数值研究之二:近失速工况流动特征分析[J]. 工程热物理学报, 2014, 35(1): 60-65.
[10] Vo H D, Tan C S, Greitzer E M. Criteria for Spike Initiated Rotating Stall[J]. Journal of Turbomachinery, 2008, 130(1): 155-165.
[11] 程晓斌, 陈静宜. 基于小波变换的离心压气机旋转失速先兆时频分析[J]. 工程热物理学报, 2000, 21(3): 289-293.
[12] 高鹏, 楚武利, 吴艳辉, 等. 带周向槽机匣处理的离心压气机扩稳机理分析[J]. 推进技术, 2007, 28(4): 383-387. (GAO Peng, CHU Wu-li, WU Yan-hui, et al. Mechanism of Stallmargin Improvement in a Centrifugal Compressor with Circumferential Grooves Casing Treatment[J]. Journal of Propulsion Technology, 2007, 28(4): 383-387.)
[13] Spakovszky Z S, Roduner C H. Spikes & Modal Stall Inception in an Advanced Turbocharger Centrifugal Compressor[J]. Journal of Turbomachinery, 2007, 131(3): 1745-1755.
[14] Everitt J N, Spakovszky Z S. An Investigation of Stall Inception in Centrifugal Compressor Vaned Diffuser[J]. Journal of Turbomachinery, 2013, 135(1): 1737-1749.
[15] 韩戈, 卢新根, 赵胜丰, 等. 喉部长度和扩张角对离心压气机管式扩压器影响研究[J]. 推进技术, 2014, 35(12): 1607-1614. (HAN Ge, LU Xin-gen, ZHAO Sheng-feng, et al. Effects of Diffuser Throat Length and Divergence Angle on Performance of Centrifugal Compressor with Pipe Diffuser[J]. Journal of Propulsion Technology, 2014, 35(12): 1607-1614.)
[16] Vagnoli S, Verstraete T. Numerical Investigation of Inlet Distortion on the Stall Inception of a Radial Compressor[R]. ASME GT 2014-25516.
[17] Wang Leilei, Lao Dazhong, Liu Yixiong, et al. Non-Axisymmetric Flow Characteristics in Centrifugal Compressor[J]. Journal of Thermal Science, 2015, 24(4): 313-322.
[18] Chunill Hah, Jorg Bergner, Heinz-Peter Schiffer. Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor-Criteria and Mechanisms[R]. ASME GT 2006-90045.
[19] Hagelstein D, Van den Braembussche R, Keiper R, et al. Experimental Investigation of the Circumferential Static Pressure Distortion in Centrifugal Compressor Stages[R]. ASME GT 1997-050.
[20] Gu F, Engeda A. A Numerical Investigation on the Volute/Impeller Steady-State Interaction Due to Circumferential Distortion[R]. ASME GT 2001-0328.
[21] Yang M, Zheng X, Zhang Y, et al. Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control, Part I: Non-Axisymmetrical Flow in Centrifugal Compressor[J]. Journal of Turbomachinery, 2013, 135(2): 61-69.
[22] Zheng X Q, Huenteler J, Yang M Y, et al. Influence of the Volute on the Flow in a Centrifugal Compressor of a High-Pressure Ratio Turbocharger[J]. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy, 2010, 224(8): 1157-1169.　　　　　　　　　　　　　*　收稿日期:2015-11-11；修订日期:2016-01-05。基金项目:国家自然科学基金(51376024)。作者简介:杨策,博士,教授,研究领域为叶轮机械气动热力学。E-mail: yangce@bit.edu.cn(编辑:张荣莉)