缝式机匣处理及其轴向偏转角对跨声速轴流压气机稳定性的改善

Haoguang Zhang, Feng Tan, Kang An, Wuli Chu, Yanhui Wu

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

The unsteady numerical simulation method is utilized to carry out the investigation on slot casting treatment and the effect of its axial deflection angle on the stability of the transonic axial flow compressor-NASA Rotor 67. The effect of the variation of axial deflection angle on the ability and mechanism of expanding stability for slots is revealed. The results show that all the slots with different axial deflection angles can improve the compressor stability margin, but reduce the compressor peak efficiency. The improvements of stability margin and peak efficiency generated by the reversed blade angle slot are about 24.22% and -1.19%, respectively. As the axial deflection angle of the slot is changed from negative to positive, the ability of expanding stability of the slot is weakened gradually, and the loss of peak efficiency caused by the slot is reduced gradually. An analysis of the flow field shows that the stall of the compressor is spike stall in the form of the blade tip blockage when the casing is solid wall. By feeling the pressure difference between the upstream and downstream of the blade passage and the pressure difference between the suction and pressure surface of the blade tip, the slot with the reversed blade angle can suck and inject the leakage flow. Therefore, the negative effects of the leakage flow diffusing and the corresponding vortex are eliminated; the leakage flow is also excited, and it leads to the improvement of the leakage flow velocity, the decrease of the total pressure loss of the leakage flow and the enhancement of the work ability for the blade. When the axial deflection angle of the slot is changed from negative to positive, the blade tip load, which can be use by the slot, is reduced from two to one. So, the suction and injection ability of the slots are weakened, and the velocity of leakage flow is lowered. Consequently, the total pressure loss of leakage flow is improved, and the work ability of blade is weakened. As a result, the expanding stability of the slot is weakened.

投稿的翻译标题Effect of slot casing treatment and it's axial deflection angle on stability of transonic axial flow compressor
源语言繁体中文
文章编号122101
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
39
8
DOI
出版状态已出版 - 25 8月 2018

关键词

  • Axial deflection angle
  • Axial flow compressor
  • Slot casing treatment
  • Stability
  • Transonic

指纹

探究 '缝式机匣处理及其轴向偏转角对跨声速轴流压气机稳定性的改善' 的科研主题。它们共同构成独一无二的指纹。

引用此