Volume 35 Issue 6
Jun.  2020
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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. doi: 10.13224/j.cnki.jasp.2020.06.002
Citation: 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. doi: 10.13224/j.cnki.jasp.2020.06.002
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Surge detection method based on rate of change of compressor discharge static pressure

doi: 10.13224/j.cnki.jasp.2020.06.002
  • Received Date: 2019-11-07
  • Publish Date: 2020-06-28
    Abstract
  • The parameters of the compressor’s discharge static pressure and rotor speed were used to establish the surge detection method based on the first-order and the second-order rate of change. According to dozens of surge detection verifications in core-engine and whole-engine tests, when the threshold was exceeded, the stall or surge could be detected by the first-order change rate of compressor discharge static pressure, and then the possibility of occurrence was confirmed by the second-order change rate and the follow-up exceeding value of the first-order change rate of static pressure or speed. Those tests proved that this method had short response time, and the detection time was less than half of the surge period. The successful detection rate was as high as 100%, and the false alarm rate was as low as 0. and. With this method, no false or missed detection had been found.

     

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    • References(20)
  • [1]
    HILLER S J,HERMANN J,WIDHOPF-FENK R.High pressure compressor stabilization by controlled pulsed injection［R］.ASME Paper GT2012-68460,2012.
    [2]
    SCHEIDLER S G,MUNDT C.Active stability control of the compression system in a twin-spool turbofan engine by air injection［C］∥Proceedings of the 10th of International Symposium on Transport Phenomena and Dynamics of Rotating Machinery.Honolulu:International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,2004:1-10.
    [3]
    张绍基.航空发动机防喘控制系统设计和热扰动参数研究［J］.航空发动机,2005,31(3):8-12. ZHANG Shaoji.Design of anti-surge control system and research on heat disturbance parameters for aeroengine［J］.Aeroengine,2005,31(3):8-12.(in Chinese)
    [4]
    吴云,李应红,张朴,等.某轴流式压气机气动不稳定的相关积分分析［J］.热能动力工程,2006,21(2):145-149. WU Yun,LI Yinghong,ZHANG Pu,et al.Correlation-in-tegral analysis of the aerodynamic instability of an axial-flow compressor［J］.Journal of Engineering for Thermal Engine and Power,2006,21(2):145-149.(in Chinese)
    [5]
    孙涛,徐光华,张春梅.基于相关积分法的离心压气机喘振过程的非线性监测［J］.航空动力学报,2006,21(6):1092-1097. SUN Tao,XU Guanghua,ZHANG Chunmei.Nolinear monitoring of the centrifugal compressor surge process based on the correlation integral method［J］.Journal of Aerospace Power,2006,21(6):1092-1097.(in Chinese)
    [6]
    李扬,李应红,吴云.基于方差分析的某轴流式压气机失速征兆起始检测［J］.航空计算技术,2005,35(1):104-105. LI Yang,LI Yinghong,WU Yun.Detection of rotating stall inception precursor of axial flow compressor with variance analysis［J］.Aeronautical Computer Technique,2005,35(1):104-105.(in Chinese)
    [7]
    张靖煊.一种捕捉预示压气机失稳预警信号的新方法的研究［J］.航空动力学报,2004,19(2):270-277. ZHANG Jingxuan.Study of a new method for giving warning signals of instability［J］.Journal of Aerospace Power,2004,19(2):270-277.(in Chinese)
    [8]
    李长征,熊兵,韩伟.基于统计特征的轴流压气机喘振检测［J］.航空动力学报,2010,25(12):2656-2659. LI Changzheng,XIONG Bing,HAN Wei.Surge detection of an axial compressor based on statistical characteristics［J］.Journal of Aerospace Power,2010,25(12):2656-2659.(in Chinese)
    [9]
    李长征,熊兵,韩伟.基于时间序列分析的压气机喘振检测［J］.测控技术,2011,30(1):100-104. LI Changzheng,XIONG Bing,HAN Wei.Compressor surge detecting based on time series analysis［J］.Measurement and Control Technology,2011,30(1):100-104.(in Chinese)
    [10]
    李美林,张春梅,王尚锦,等.用小波和分维数方法处理喘振试验数据［J］.工程热物理学报,2002,23(2):175-178. LI Meilin,ZHANG Chunmei,WANG Shangjin,et al.Surge data processing based on wavelet analysis and fractal methods［J］.Journal of Engineering Thermophysics,2002,23(2):175-178.(in Chinese)
    [11]
    DREMIN I M,FURLETOV V I,IVANOV O V,et al.Precursors of stall and surge processes in gas turbines revealed by wavelet analysis［J］.Control Engineering Practice,2002,10(6):599-604.
    [12]
    谢锋,谢寿生.基于小波分析的航空发动机旋转失速检测方法［J］.航空动力学报,2006,21(4):754-758. XIE Feng,XIE Shousheng.Detection of rotating stall in aircraft engine based on wavelet analysis［J］.Journal of Aerospace Power,2006,21(4):754-758.(in Chinese)
    [13]
    宋慧敏,李应红,吴云,等.基于自相关函数的压气机气动不稳定监测方法［J］.空军工程大学学报(自然科学版),2005,6(3):7-9. SONG Huimin,LI Yinghong,WU Yun,et al.Sensing the aerodynamic instability of a compressor using auto-correlation function［J］.Journal of Air Force Engineering University(Natural Science Edition),2005,6(3):7-9.(in Chinese)
    [14]
    TAHARA N,NAKAJIMA T,KUROSAKI M,et al.Active stall control with practicable stall prediction system using auto-correlation coefficient［R］.Salt Lake City,Utah,US:AIAA,2001.
    [15]
    张海波,华伟,吴伟超.一种基于发动机喘振实时模型的主动稳定性控制方法［J］.航空动力学报,2013,28(5):1150-1158. ZHANG Haibo,HUA Wei,WU Weichao.Active stability control method for turbofan engine based on post-stall model［J］.Journal of Aerospace Power,2013,28(5):1150-1158.(in Chinese)
    [16]
    郭贵喜,王振华,王洪祥,等.基于HHT的航空发动机气动失稳信号时频分析方法［J］,航空发动机,2013,39(3):62-67. GUO Guixi,WANG Zhenhua,WANG Hongxiang,et al.Time-frequency analysis method of aeroengine aerodynamic instability signal based on Hilbert-Huang transform［J］.Aeroengine,2013,39(3):62-67.(in Chinese)
    [17]
    刘美凤，黄波，吴施志，等.航空燃气涡轮发动机喘振控制方法和电子控制器:CN106523163B［P］.2018-03-02.
    [18]
    李长征,胡智琦,许思琦.基于D-S证据融合的压气机气动失稳检测［J］.推进技术,2017,38(8):1870-1877. LI Changzheng,HU Zhiqi,XU Siqi.Aerodynamic instability detection for compressor based on D-S evidence fusion［J］.Journal of Propulsion Technology,2017,38(8):1870-1877.(in Chinese)
    [19]
    沃尔什 P P,弗莱彻 P.燃气涡轮发动机性能［M］.郑建弘,胡忠志,华清,等译.上海:上海交通大学出版社,2014.
    [20]
    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.
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