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一种捕捉预示压气机失稳预警信号的新方法的研究 被引量:23

Study of a New Method for Giving Warning Signals of Instability
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摘要 本文旨在寻求预示压气机失稳发生的预警信号。通过对失稳产生的物理机制的分析可知,压气机系统内脉动压力能量的积累有可能作为失稳先兆的外部表征。据此,本文从能量的角度出发,对多组压气机失稳的实验数据进行了频域,时域分析。结果发现,在压缩系统完全进入失稳以前,动态压力的方差值有一明显的增长过程,而且这一异常现象距失稳有1~2秒的时间间隔,这对实现压气机失稳的在线预报有十分重要意义。 A new method has been developed to give early warning signals just before a compressor runs into instability. Analyses based on prestall pressure signals of several axial compressors reveal that the dynamic pressure energy accumulation in a compressor just before the instability can be used as a precursor signature of the instability. It is illustrated that by using the appropriate RMS of the casing static pressure over the rotor tip an early warning can be obtained about 1-2 seconds before the onset of the instability. This is particularly important because the method is applicable to the spike type stall inceptions as well as the model type ones, the former usually appears abruptly and does not have a precursor.
作者 张靖煊
出处 《航空动力学报》 EI CAS CSCD 北大核心 2004年第2期270-277,共8页 Journal of Aerospace Power
基金 国家自然科学基金资助项目(59525612)
关键词 压气机失稳 预警信号 旋转失速 失速先兆 时域分析 Accident prevention Aerospace engineering Alarm systems Pressure Propulsion Signal processing Stability
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参考文献9

  • 1Inoue M,Kuroumaru M,Iwamoto T,et al. Detection of a Rotating Stall Pricursor in Isolated Axial Flow Compressor Rotors[R]. ASME Paper 90-GT- 157.
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二级参考文献11

  • 1[1]Day I J. Active Suppression of Rotating Stall and Surge in Axial Compressors. ASME J. Turbomachinery, 1993,115:40-47
  • 2[2]Paduano J D, Epstein A H, Valavani L, et al. Active Control of Rotating Stall in a Low-Speed Axial Compressor.ASME J. Turbomachinery, 1993, 115:48-56
  • 3[3]Behnken R L, Leung M, Murray R M. Characterizing the Effects of Air Injection on Compressor Performance for Use in Active Control of Rotating Stall. ASME 97-GT316, 1997
  • 4[4]Weigl H J, Paduano J D, Frechette L G, et al. Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor. ASME 97-GT-411, 1997
  • 5[5]Suder K L, Hathaway M D, Thorp S A, et al. Compressor Stability Enhancement using Discrete Tip Injection.ASME 2000-GT-650, 2000
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  • 10陈芳,航空动力学报,1989年,4卷,2期,4页

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同被引文献201

引证文献23

二级引证文献79

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