Position rule of turboshaft engine surge based on bench test

Siqi YAN; Benwei LI; Yonghua WANG; Yun ZHANG; Pengyu ZHOU

doi:10.13224/j.cnki.jasp.20210085

Chinese

您当前的位置：

首页 >

文章列表页 >

Position rule of turboshaft engine surge based on bench test

Structure,Strength and Vibration | 更新时间：2025-04-07

- Position rule of turboshaft engine surge based on bench test
- Journal of Aerospace Power Vol. 37, Issue 2, Pages: 263-273(2022)
- 作者机构：
  
  1.海军航空大学航空基础学院，山东烟台 264001
  2.中国人民解放军 92326部队，广东湛江 524005
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210085
  CLC：
- 稿件说明：
移动端阅览
Siqi YAN, Benwei LI, Yonghua WANG, et al. Position rule of turboshaft engine surge based on bench test[J]. Journal of Aerospace Power, 2022, 37(2): 263-273.
DOI：

Siqi YAN, Benwei LI, Yonghua WANG, et al. Position rule of turboshaft engine surge based on bench test[J]. Journal of Aerospace Power, 2022, 37(2): 263-273. DOI： 10.13224/j.cnki.jasp.20210085.

摘要

为了探究某型涡轴发动机喘振发生位置规律，采集并分析了台架喘振试验时进气道、轴流压气机叶尖、轴流压气机出口和离心压气机出口的压力信号。采用连续小波时频变换对压力信号进行特征提取，以小波系数作为喘振信号特征，阈值为小波系数最大值的10%，结果表明：某型涡轴发动机的轴流压气机总是比离心压气机先发生喘振，喘振在轴向上由进气道向离心压气机传递的同时，在周向上也沿着压气机转子叶片旋转方向传递。对某型号发动机进行实时喘振监测时，监测轴流压气机能比监测离心压气机更早发现喘振，在后续某型涡轴发动机改型设计时，可增加轴流压气机的喘振裕度来提升整机防喘能力。

Abstract

In order to investigate the surge position of turboshaft engine，the pressure signals of air inlet，axial compressor tip，axial compressor outlet and centrifugal compressor outlet were collected and analyzed during the bench surge test.Continuous wavelet time⁃frequency transform was used to extract the characteristics of the pressure signal.The wavelet coefficients were used as the characteristics of the surge signal，and the threshold value was 10% of the maximum value of the wavelet coefficients.The results showed that the axial flow compressor of a turboshaft engine surged earlier than the centrifugal compressor，and the surge was transmitted from the inlet to the centrifugal compressor in the axial direction，and also along the rotor blade rotation in the circumferential direction.When the real⁃time surge monitoring was carried out for a certain type of engine，the surge can be detected earlier by monitoring the axial compressor than by monitoring the centrifugal compressor.In the subsequent modification design of a certain type of turboshaft engine，the surge margin of the axial compressor can be increased to improve the anti⁃surge ability of the whole engine.

关键词

Keywords

references

潘天宇 , 孙太璐 , 李志平 , 等 . 局部喘振的发生机理 [J]. 航空动力学报 , 2016 , 31 （ 4 ）: 877 ⁃ 885 .

PAN Tianyu , SUN Tailu , LI Zhiping , et al . Occurrence mechanism of partial surge [J]. Journal of Aerospace Power ， 2016 , 31 （ 4 ）: 877 ⁃ 885 . （in Chinese）

代坷 , 郭峰 , 失剑锋 , 等 . 基于DMD方法的超声速进气道喘振特性分析 [J]. 航空动力学报 , 2019 , 34 （ 5 ）: 1076 ⁃ 1084 .

DAI Ke , GUO Feng , SHI Jianfeng , et al . Characteristics investigation on supersonic inlet buzz with dynamic mode decomposition method [J]. Journal of Aerospace Power ， 2019 , 34 （ 5 ）: 1076 ⁃ 1084 . （in Chinese）

孙晓峰 , 何晨 , 刘小华 , 等 . 航空压气机流动稳定性预测研究进展 [J]. 推进技术 , 2017 , 38 （ 10 ）: 2172 ⁃ 2185 .

SUN Xiaofeng , HE Chen , LIU Xiaohua , et al . Research progress in prediction of flow instability of aero⁃compressor [J]. Journal of Propulsion Technology , 2017 , 38 （ 10 ）: 2172 ⁃ 2185 . （in Chinese）

李长征 , 韩伟 , 熊兵 . 压气机喘振模式识别与在线检测 [J]. 推进技术 , 2011 , 32 （ 3 ）: 318 ⁃ 322 .

LI Changzheng , HAN Wei , XIONG Bing . Pattern recognition and on⁃line detection for compressor surge [J]. Journal of Propulsion Technology , 2011 , 32 （ 3 ）: 318 ⁃ 322 . （in Chinese）

旷桂兰 , 姚峥嵘 , 王道波 , 等 . 某涡轴发动机整机逼喘试验研究 [J]. 航空动力学报 , 2009 , 24 （ 3 ）: 588 ⁃ 595 .

KUANG Guilan , YAO Zhengrong , WANG Daobo , et al . Application of fractional Fourier transform in one turbine⁃shaft engine surge analyse [J]. Journal of Aerospace Power , 2009 , 24 （ 3 ）: 588 ⁃ 595 . （in Chinese）

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 .

PETER J , PARDOWITZ B , ECK M , et al . Advanced stereo high⁃speed PIV in an annular cascade without clearance:evidences of rotating instability [R]. Stockholm,Swede : European Conference on Turbomachinery Fluid Dynamics and Thermodynamics , 2017 .

ECK M , RÜCKERT R , PEITSCH D . Advanced application of a sublayer fence probe in highly instationary turbomachinery flows:observations on prestall instabilities [J]. Experiments in Fluids , 2019 , 60 （ 3 ）: 47 .1⁃47. 17 .

桂幸民 , 滕金芳 , 刘宝杰 , 等 . 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 .

贺象 , 马宏伟 , 银越千 , 等 . 小尺寸多级轴流压气机喘振现象试验 [J]. 航空动力学报 , 2016 , 31 （ 8 ）: 1957 ⁃ 1963 .

HE Xiang , MA Hongwei , YIN Yueqian , et al . Experiment on surge phenomenon of small multistage axial compressor [J]. Journal of Aerospace Power , 2016 , 31 （ 8 ）: 1957 ⁃ 1963 . （in Chinese）

潘天宇 , 贺雷 , 王正鹤 , 等 . 局部喘振频率特性及估算方法 [J]. 航空动力学报 , 2015 , 30 （ 11 ）: 2666 ⁃ 2672 .

PAN Tianyu , HE Lei , WANG Zhenghe , et al . Study on the frequency of partial surge and a frequency prediction method [J]. Journal of Aerospace Power , 2015 , 30 （ 11 ）: 2666 ⁃ 2672 . （in Chinese）

王玉东 . 基于压气机出口静压变化率的喘振检测方法 [J]. 航空动力学报 , 2020 , 35 （ 6 ）: 1131 ⁃ 1139 .

WANG Yudong . Surge detection method based on rate of change of compressor discharge static pressure [J]. Journal of Aerospace Power , 2020 , 35 （ 6 ）: 1131 ⁃ 1139 . （in Chinese）

李小彪 , 余海生 , 孙建国 , 等 . 一种涡扇发动机喘振信号判定方法 [J]. 推进技术 , 2009 , 30 （ 6 ）: 727 ⁃ 729，739 .

LI Xiaobiao , YU Haisheng , SUN Jianguo , et al . A surge signal judge method for turbofan engine [J]. Journal of Propulsion Technology , 2009 , 30 （ 6 ）: 727 ⁃ 729,739 . （in Chinese）

LI J C . Self⁃adaptive stability enhancing technology with tip air injection in an axial flow compressor [J]. Journal of Turbomachinery , 2017 , 139 （ 1 ）: 1 ⁃ 9 .

LI J C , LIU Y , DU J , et al . Automatic stability control using tip air injection in a multi⁃stage axial compressor [J]. Aerospace Science and Technology , 2020 , 98 （ 2 ）: 1 ⁃ 12 .

LI J C , DU J , GENG S J , et al . Tip air injection to extend stall margin of multi⁃stage axial flow compresso with inlet radial distortion [J]. Aerospace Science and Technology , 2020 , 96 （ 1 ）: 1 ⁃ 13 .

吴学辉 , 伍友利 , 李志刚 , 等 . 轴流压缩系统的 Lyapunov指数谱分析及应用 [J]. 推进技术 , 2006 , 27 （ 1 ）: 37 ⁃ 39 .

WU Xuehui , WU Youli , LI Zhigang , et al . Analysis and application of Lyapunov exponent spectra of axial⁃flow compression system [J]. Journal of Propulsion Technology , 2006 , 27 （ 1 ）: 37 ⁃ 39 . （in Chinese）

王占学 , 王鹏 , 乔渭阳 . 畸变进气时涡扇发动机整机环境下压缩部件气动稳定性评定 [J]. 推进技术 , 2007 , 28 （ 1 ）: 20 ⁃ 25 .

WANG Zhanxue , WANG Peng , QIAO Weiyang . Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow [J]. Journal of Propulsion Technology , 2007 , 28 （ 1 ）: 20 ⁃ 25 . （in Chinese）

HAGINO N , KASHIWABARA Y . Experimental study of surge and rotating stall occurring in small centrifugal compressor [R]. Denver,USA : the 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit , 2009 .

LIN F , CHEN J Y , LI M L . Wavelet analysis of rotor⁃tip disturbances in an axial⁃flow compressor [J]. Journal of Propulsion and Power , 2004 , 20 （ 2 ）: 319 ⁃ 334 .

LIN F , LI M L , CHEN J Y . Long⁃to⁃short length⁃scale transition:a stall inception phenomenon in an axial compressor with inlet distortion [J]. Journal of Turbomachinery , 2006 , 128 （ 1 ）: 130 ⁃ 140 .

LIU Y , LI J C , DU J , et al . Application of fast wavelet analysis on early stall warning in axial compressors [J]. Journal of Thermal Science , 2019 , 28 （ 5 ）: 837 ⁃ 849 .

刘洋 , 李继超 , 杜娟 , 等 . 周向畸变下轴流压气机的失速预警方法研究及应用 [J]. 推进技术 , 2020 , 41 （ 9 ）: 1967 ⁃ 1974 .

LIU Yang , LI Jichao , DU Juan , et al . Stall warning method investigation and application in an axial⁃flow compressor with circumferential distortion [J]. Journal of Propulsion Technology , 2020 , 41 （ 9 ）: 1967 ⁃ 1974 . （in Chinese）

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Rolling bearing collaborative fault diagnosis technology for casing vibration signal

Application of neural network model in compressor through⁃flow analysis

Experiment of Reynolds number effects on subsonic compressor plane cascade

Unknown fault diagnosis of rolling bearing based on improved GWO⁃LightGBM

Fault diagnosis of tooth surface spalling of planetary gearbox based on GWO⁃TVF⁃EMD method

Related Author

林桐

陈果

滕春禹

王云

欧阳文理

肖圣迪

Teng FEI

Lucheng JI

Related Institution

南京航空航天大学民航学院

中国航空工业集团有限公司中国航空综合技术研究所

School of Aerospace Engineering，Beijing Institute of Technology

Institute for Aero Engine，Tsinghua University

Aerospace Technology Institute，China Aerodynamics Research and Development Center

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰