期刊文献+

用小波变换对机匣处理抑制旋转失速的机理研究 被引量:2

MECHANISM INVESTIGATION ON CASING TREATMENT FOR RESTRAINING ROTATING STALL BY MEANS OF WAVELET TRANSFORM
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摘要 本文利用小波变换对轴流压气机旋转失速时的压力信号进行时频分析。通过Morlet连续小波变换,详细分析压气机失稳过程中非定常信号的变化,并研究旋转失速初始扰动信号在处理机匣气室中的局部行为。通过对比实壁机匣与处理机匣的失速初始信号相干波形的结构特性,发现不同机匣结构对相干波形结构中压力脉动信号的不同影响,提出处理机匣抑制旋转失速初始扰动发展的机理。 Wavelet transform,as a tool for signal analysis,is applied to analysis of compressor rotating stall signals.With the Morlet wavelet transform,the time-evolution of the unsteady signals during the stall inception and the local behavior in the casing treatment plenum are investigated.By comparison with structure characteristics of the coherent waves in the casing without treatment,it is shown that the casing treatment do has different influences on pressure impulse signals.A mechanism for restraining perturbations of stall inception via casing treatment is proposed.
出处 《航空动力学报》 EI CAS CSCD 北大核心 1998年第2期133-138,共6页 Journal of Aerospace Power
关键词 机匣 旋转失速抑制 航空器 压气机 小波变换 Axial fan Treatment Casing Coherent detection
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参考文献2

  • 1Liao Shengfang,ASME 96-GT-57,1996年
  • 2秦前清,实用小波分析,1993年

同被引文献22

  • 1江勇,张发启,张百灵,孔卫东.基于实验的插板式进气畸变稳态压力场估计[J].空军工程大学学报(自然科学版),2007,8(2):1-3. 被引量:16
  • 2曹人靖,周盛.扰动波对轴流压气机旋转失速的影响[J].航空动力学报,1997,12(2):201-202. 被引量:2
  • 3Emmons H W,Pearson C E,Grant H P. Compressor surge and stall propagation[J]. Transactions of the ASME, 1955,77(3) :455-469.
  • 4Moore F K,Greitzer E M. A theory of post-stall transients in axial compressor systems Part I :development of equa- tions[R]. ASME Paper 85-GT-171,1985.
  • 5Camp T R,Day I J. A study of spike and modal stall phe- nomena in a low-speed axial compressor[J]. ASME J. Tur- bomach,1998,120(3) :393-401.
  • 6Freeman C,Wilson A G,Day I J,et al. Experiments in ac- tive control of stall on an aeroengine gas turbine [J]. ASME J Turbomach,1998,120(4) :637-647.
  • 7Day I J,Breuer T, Escuret J, et al. Stall inception and the prospects for active control in ~our high-speed compressors [J]. ASME J. Turbomach, 19 9 9,12 (1): 18-2 7.
  • 8Vahdati M, Simpson G,Imregun M. Un-steady flow and aeroelasticity behavior of aeroengine core compressors dur- ing rotating stall and surge [J]. ASME J. Turbomach, 2008,130(3):031017.1-031017.9.
  • 9Cumpsty N A. Compressor aerodynamics[M]. US:Krieger Publishing Company, 2004.
  • 10Epstein A H, Ffowcs W J E,Greitzer E M. Active suppres- sion of compressor instabilities[R]. AIAA Paper AIAA- 86-1994,1986.

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