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机匣处理若干问题探讨 被引量:3

A DISCUSSION OF SOME QUESTIONS ABOUTCASING TREATMENT
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摘要 本文在机匣处理设计中对关键级与危险截面、机匣处理与扩稳、弯槽与直斜槽进行了一些研究。发现各国对关键级与危险截面的判定不一。机匣处理的作用在于消除堵塞,提高叶排临界攻角,减小下一叶排近壁面攻角,扩大了压气机稳定工作范围。弯槽吸收了直斜槽和角向槽的长处,因而兼有显著的扩稳效果和较高的效率。 Discussion is given in this paper about such questions in casing treatment, asjudgement of initial stall stage and critical section, correlation between casing treatment andenhancing stability, and difference of straight skewed slots and curved slots on performanceinfluence. It is found that there are different opinions and judgement methods for initialstall stage and critical section. Casing treatment can eliminate blockage and increase criticalincidence angle of the blade rows as well as decrease incidence near blade tip of next row.Therefore, it is main cause for enhancing stability of axial flow compressor. The curved slotscasing treatment possesses advantages both straight skewed slots and blade angle slots, sothat it can enhance stability and receive high efficiency at the same time.
作者 蒋世亮
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2000年第1期46-49,共4页 Journal of Engineering Thermophysics
关键词 轴流式压气机 机匣处理 压气机 燃气轮机 axial flow compressor casing treatment
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参考文献6

  • 1[1]Smith G D J, et al. Flow Phenomena in Compressor Casing Treatment. ASME 532/106:1984 被引量:1
  • 2[2] Takata H, et al. Stall Margin Improvement by Casing Treatment - Its Mechanism and Effectiveness.ASME Journal of Engineering for Power, 1977, 99 被引量:1
  • 3[3] Prince D C, et al. A Study of Casing Treatment Stall Margin lmprovement Phenomena. NASACR 134552, 1975 被引量:1
  • 4[4]Osborn W M, et al. Effect of Several Porous Casing Treatment on Stall Limit and on Overall Performance of An Axial-flow Compressor Rotor. NASA TN D-6537, 1971 被引量:1
  • 5[5] Fabri J, et al. Effect of Outer Casing Treatment on Stall Margin of A Supersonic Rotating Cascade.ASME 75-GT-95 , 1975 被引量:1
  • 6[6]dward J Hall, et al. Aerodynamic Analysis of Compressor Casing Treatment with A 3-D Navier-Stokes Solver.AIAA 94 2796, 1994 被引量:1

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